CN113815876A - Intelligent power inspection unmanned aerial vehicle for high-voltage overhead line - Google Patents
Intelligent power inspection unmanned aerial vehicle for high-voltage overhead line Download PDFInfo
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- CN113815876A CN113815876A CN202111167181.3A CN202111167181A CN113815876A CN 113815876 A CN113815876 A CN 113815876A CN 202111167181 A CN202111167181 A CN 202111167181A CN 113815876 A CN113815876 A CN 113815876A
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- 238000007689 inspection Methods 0.000 title claims abstract description 17
- 238000004891 communication Methods 0.000 claims abstract description 20
- 238000007789 sealing Methods 0.000 claims abstract description 17
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 16
- 238000001179 sorption measurement Methods 0.000 claims abstract description 15
- 238000012423 maintenance Methods 0.000 claims abstract description 10
- 229910052742 iron Inorganic materials 0.000 claims abstract description 8
- 230000005540 biological transmission Effects 0.000 claims description 26
- 238000009434 installation Methods 0.000 claims description 10
- 238000010521 absorption reaction Methods 0.000 description 3
- 244000309464 bull Species 0.000 description 3
- 230000005389 magnetism Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000012546 transfer Methods 0.000 description 3
- 230000007704 transition Effects 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000033001 locomotion Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000008054 signal transmission Effects 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
- H02G1/00—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines
- H02G1/02—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines for overhead lines or cables
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The invention discloses an intelligent power inspection unmanned aerial vehicle for a high-voltage overhead line, which comprises a shell, a power unit, a shooting unit and a control unit, wherein the shell is provided with a power supply unit; the shell is provided with a power unit and a shooting unit; the control unit comprises a sealing plate, a single chip microcomputer, an adsorption block, a magnet, a communication module and a battery, the single chip microcomputer and the communication module are arranged on the right side inside the casing, the input and output ends of the communication module are connected with the I/O end of the single chip microcomputer, a sliding groove is formed in the right side of the casing and is communicated with a maintenance port of the casing, the sealing plate and the sliding groove slide longitudinally, the adsorption block is arranged on the right side of the sealing plate, an iron sheet is embedded in the adsorption block, the magnet is embedded in the right side of the casing, the sealing plate and the magnet are matched for attraction, and the battery is installed inside the casing; the input end of the single chip microcomputer is electrically connected with the output end of the battery through the external control switch group, the functions are multiple, the disassembly and assembly are convenient, and the maintenance is convenient.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to an intelligent power inspection unmanned aerial vehicle for a high-voltage overhead line.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.
Application number 202022026323.1 provides an unmanned aerial vehicle is patrolled and examined to intelligent electric power for high-tension overhead line among the prior art, including connecting the transition piece, the positive fixedly connected with signal transmission case of connecting the transition piece, connect the equal fixedly connected with motor base in both sides about the transition piece, motor base's top fixedly connected with rotates the motor.
And the function is simple, the disassembly is inconvenient, and the maintenance is inconvenient.
Disclosure of Invention
The invention aims to overcome the existing defects and provides an intelligent power inspection unmanned aerial vehicle for a high-voltage overhead line, which has multiple functions, is convenient to disassemble and assemble and maintain and can effectively solve the problems in the background technology.
In order to achieve the purpose, the invention provides the following technical scheme: an intelligent power inspection unmanned aerial vehicle for a high-voltage overhead line comprises a shell, a power unit, a shooting unit and a control unit;
a shell: a power unit and a shooting unit are arranged on the camera;
a control unit: the portable storage battery comprises a sealing plate, a single chip microcomputer, an adsorption block, a magnet, a communication module and a battery, wherein the single chip microcomputer and the communication module are arranged on the right side in the casing, the input end and the output end of the communication module are connected with the I/O end of the single chip microcomputer, a sliding groove is formed in the right side of the casing and is communicated with a maintenance port of the casing, the sealing plate longitudinally slides with the sliding groove, the adsorption block is arranged on the right side of the sealing plate, an iron sheet is embedded in the adsorption block, the magnet is embedded in the right side of the casing, the sealing plate and the magnet are matched to attract each other, and the battery is installed in the casing;
wherein, the input end of the singlechip is electrically connected with the output end of the battery through an external control switch group. Through the operation of the electronic component of single chip microcomputer control equipment, the battery provides the energy, and communication module makes things convenient for data transfer, has inlayed an iron sheet through the inboard at the absorption piece, makes its and the magnet actuation on casing right side, makes the inside of casing be in the encapsulated situation, and magnetism is inhaled fixedly and can be made things convenient for the inside maintenance in later stage.
Further, the power unit comprises a transmission assembly, a first power assembly, a first motor and four propellers, the first motor is installed on the transmission assembly through a motor frame, the propeller is arranged on an output shaft of the first motor, and an input end of the first motor is electrically connected with an output end of the battery through the single chip microcomputer. The first motor drives the propeller to rotate, so that the equipment is controlled to take off.
Further, the transmission assembly comprises a second rotating rod and a transmission rod, the four corners of the upper side of the casing are respectively provided with the second rotating rod, the bottom end of the transmission rod is rotatably connected with the upper side of the casing, the upper end of the second rotating rod is respectively provided with the transmission rod, and the upper side of the transmission rod is provided with a first motor. The four rotating rods are controlled to rotate in the same direction through the power assembly I, so that the four transmission rods are controlled to be folded, the propeller is contracted or expanded, and the storage of the propeller is facilitated.
Furthermore, the first power assembly comprises a first rotating rod and a first gear, the bottom end of the first rotating rod is rotatably connected with the upper side of the casing, the center of the first gear is located at the middle end of the first rotating rod, a toothed ring is arranged on the outer side of the second rotating rod, and the second rotating rod is meshed with the first gear through the toothed ring. The first rotating rod is rotated to drive the first gear to move in a meshed mode with the second four rotating rods and drive the first gear to rotate in the same direction, and therefore the folding of the four transmission rods is controlled.
Furthermore, the shooting unit comprises a rotating assembly, a fixing assembly, a second power assembly, a clamping hole, a camera body and an installation block, wherein the camera body is arranged on the bottom side of the installation block, and the clamping hole is formed in the left side and the right side of the installation block. The camera main body is fixed through the fixing assembly, the clamping hole and the mounting block assist the camera main body to be fixed, and data shot by the camera main body can be uploaded to a network terminal through the single chip microcomputer and the communication module.
Further, fixed subassembly contains kelly and fixed block, the fixed block has two and installs on the runner assembly, all be equipped with a kelly on the fixed block, the middle-end of kelly is equipped with the screw thread, and kelly and fixed block threaded connection, kelly and card hole cooperation joint. The position of the clamping rod is limited through the fixing block, the clamping rod is rotated through twisting, the clamping rod and the fixing block are threaded, the clamping rod is clamped with the clamping hole in a matched mode, and therefore the camera shooting main body is fixed.
Furthermore, the rotating assembly comprises a third rotating rod and a mounting plate, fixed blocks are arranged at the left end and the right end of the bottom side of the mounting plate, the bottom end of the third rotating rod is connected with the center of the upper side of the mounting plate, and the third rotating rod is mounted on the power assembly. The second power assembly indirectly controls the camera main body to rotate by three hundred and sixty degrees through the third rotating rod and the mounting plate.
Furthermore, the power assembly II comprises a motor II, the motor II is fixed to the bottom side of the interior of the shell through the electric rack, an output shaft of the motor II extends to the outer side of the shell and is connected with the upper side of the rotating rod III, and the input end of the motor II is electrically connected with the output end of the battery through the single chip microcomputer. The rotation of the rotating rod three is controlled by the motor two, and the camera shooting main body is indirectly controlled to rotate by three hundred and sixty degrees.
Furthermore, the portable electronic device further comprises support rods, wherein the support rods are arranged at four corners of the bottom side of the casing. The support rod supports the casing.
Furthermore, the support rod support device also comprises a base plate, wherein the base plate is arranged at the bottom side of the support rod at the left end, and the base plate is also arranged at the bottom side of the support rod at the right end. The ground contact area of the equipment is enlarged through the backing plate, so that the equipment is supported more stably.
Compared with the prior art, the invention has the beneficial effects that: this unmanned aerial vehicle has following benefit:
1. an iron sheet is embedded in the inner side of the adsorption block, so that the adsorption block and the magnet on the right side of the machine shell are attracted, the inside of the machine shell is in a closed state, and the magnetic attraction is fixed, so that the later-stage internal maintenance can be facilitated.
2. Through rotating the first rotating rod, the first gear and the second four rotating rods are driven to move in a meshed mode to drive the first gear and the second four rotating rods to rotate in the same direction, so that the folding of the four transmission rods is controlled to shrink the propeller, and the first gear and the second four rotating rods are convenient to store.
3. The position of the clamping rod is limited through the fixing block, the clamping rod is rotated through twisting, the clamping rod and the fixing block are made to be in threaded connection, the clamping rod is made to be matched and clamped with the clamping hole, and therefore the camera shooting main body is fixed and easy to detach.
4. The camera main body is fixed on the bottom side of the mounting plate, the rotating rod III is controlled by the motor II to drive the mounting plate to rotate, and the camera main body can be indirectly controlled to rotate by three hundred and sixty degrees.
Drawings
FIG. 1 is a schematic side view of the present invention;
FIG. 2 is a schematic cross-sectional view of the present invention;
FIG. 3 is a schematic side view of the present invention.
In the figure: the camera comprises a machine shell 1, a power unit 2, a first rotating rod 21, a first gear 22, a second rotating rod 23, a transmission rod 24, a first motor 25, a propeller 26, a shooting unit 3, a third rotating rod 31, a mounting plate 32, a clamping rod 33, a clamping hole 34, a mounting block 35, a fixed block 36, a shooting main body 37, a second motor 38, a control unit 4, a sealing plate 41, a singlechip 42, an adsorption block 43, a magnet 44, a communication module 45, a battery 46, a support rod 5 and a backing plate 6.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-3, the present embodiment provides a technical solution: an intelligent electric power inspection unmanned aerial vehicle for a high-voltage overhead line comprises a shell 1, a power unit 2, a shooting unit 3 and a control unit 4;
a machine shell 1: a power unit 2 and a shooting unit 3 are arranged on the bracket;
the portable computer case further comprises support rods 5, and the four corners of the bottom side of the case 1 are provided with the support rods 5. The support bar 5 supports the cabinet 1.
The support rod support device further comprises a base plate 6, the base plate 6 is arranged on the bottom side of the support rod 5 at the left end, and the base plate 6 is also arranged on the bottom side of the support rod 5 at the right end. The base plate 6 enlarges the ground contact area of the equipment, so that the equipment is supported more stably.
The control unit 4: the portable electronic device comprises a sealing plate 41, a single chip 42, an adsorption block 43, a magnet 44, a communication module 45 and a battery 46, wherein the single chip 42 and the communication module 45 are arranged on the right side in the casing 1, the input and output ends of the communication module 45 are connected with the I/O end of the single chip 42, a sliding groove is formed in the right side of the casing 1 and is communicated with a maintenance port of the casing 1, the sealing plate 41 and the sliding groove longitudinally slide, the adsorption block 43 is arranged on the right side of the sealing plate 41, an iron sheet is embedded in the inner side of the adsorption block 43, the magnet 44 is embedded in the right side of the casing 1, the sealing plate 41 and the magnet 44 are matched for attraction, and the battery 46 is arranged in the casing 1;
wherein, the input end of the singlechip 42 is electrically connected with the output end of the battery 46 through an external control switch group. Through the operation of singlechip 42 controlgear's electronic component, battery 46 provides the energy, and communication module 45 makes things convenient for data transfer, has inlayed an iron sheet through the inboard at absorption piece 43, makes its and the magnet 44 actuation on casing 1 right side, makes the inside of casing 1 be in the encapsulated situation, and the fixed inside maintenance that can make things convenient for the later stage of magnetism is inhaled.
The power unit 2 comprises a transmission assembly, a first power assembly, a first motor 25 and four propellers 26, the first motor 25 is mounted on the transmission assembly through a motor frame, the propeller 26 is arranged on an output shaft of each first motor 25, and an input end of the first motor 25 is electrically connected with an output end of the battery 46 through the single chip microcomputer 42. The first motor 25 drives the propeller 26 to rotate, so that the equipment is controlled to take off.
The transmission assembly comprises a second rotating rod 23 and a transmission rod 24, the four corners of the upper side of the machine shell 1 are respectively provided with the second rotating rod 23, the bottom end of the transmission rod 24 is rotatably connected with the upper side of the machine shell 1, the upper end of the second rotating rod 23 is respectively provided with the transmission rod 24, and the upper side of the transmission rod 24 is provided with a first motor 25. The first power assembly controls the second four rotating rods 23 to rotate in the same direction, so that the folding and unfolding of the four driving rods 24 are controlled, the propeller 26 is contracted or expanded, and the storage is facilitated.
The first power assembly comprises a first rotating rod 21 and a first gear 22, the bottom end of the first rotating rod 21 is rotatably connected with the upper side of the machine shell 1, the center of the first gear 22 is located at the middle end of the first rotating rod 21, a toothed ring is arranged on the outer side of the second rotating rod 23, and the second rotating rod 23 is in meshed connection with the first gear 22 through the toothed ring. The first rotating rod 21 is rotated to drive the first gear 22 to move in meshing engagement with the second four rotating rods 23, so as to drive the gears to rotate in the same direction, and thus the folding of the four transmission rods 24 is controlled.
The shooting unit 3 comprises a rotating component, a fixing component, a second power component, a clamping hole 34, a shooting main body 37 and an installation block 35, wherein the shooting main body 37 is arranged on the bottom side of the installation block 35, and the clamping holes 34 are formed in the left side and the right side of the installation block 35. Fix camera body 37 through fixed subassembly, the supplementary camera body 37 of card hole 34 and installation piece 35 is fixed, and the data that camera body 37 was shot can be uploaded to network terminal through singlechip 42 and communication module 45.
Fixed subassembly contains kelly 33 and fixed block 36, and fixed block 36 has two and installs on the runner assembly, all is equipped with a kelly 33 on the fixed block 36, and the middle-end of kelly 33 is equipped with the screw thread, and kelly 33 and fixed block 36 threaded connection, kelly 33 and calorie hole 34 cooperation joint. The position of the clamping rod 33 is limited by the fixing block 36, the clamping rod 33 is rotated by twisting, the clamping rod is threaded with the fixing block 36, the clamping rod 33 is matched and clamped with the clamping hole 34, and the camera shooting main body 37 is fixed.
The rotating assembly comprises a third rotating rod 31 and a mounting plate 32, fixing blocks 36 are arranged at the left end and the right end of the bottom side of the mounting plate 32, the bottom end of the third rotating rod 31 is connected with the center of the upper side of the mounting plate 32, and the third rotating rod 31 is mounted on the power assembly. The second power assembly indirectly controls the camera main body 37 to rotate three hundred and sixty degrees through the third rotating rod 31 and the mounting plate 32.
The second power assembly comprises a second motor 38, the second motor 38 is fixed on the bottom side of the interior of the machine shell 1 through a motor frame, an output shaft of the second motor 38 extends to the outer side of the machine shell 1 to be connected with the upper side of the third rotating rod 31, and an input end of the second motor 38 is electrically connected with an output end of the battery 46 through the single chip microcomputer 42. The second motor 38 controls the third rotating rod 31 to rotate, and indirectly controls the camera body 37 to rotate by three hundred and sixty degrees.
The working principle of the intelligent power inspection unmanned aerial vehicle for the high-voltage overhead line provided by the invention is as follows: control motor 25 through singlechip 42 and start, drive screw 26 and rotate, thereby controlgear takes off, it drives mounting panel 32 through three 31 of two 38 control bull sticks of motor and rotates when shooing, can indirectly control main part 37 of making a video recording and carry out three hundred sixty degrees rotations, the data that main part 37 of making a video recording was shot can pass through singlechip 42 and communication module 45 and upload to network terminal, an iron sheet has been inlayed through the inboard at absorption piece 43, make its magnet 44 actuation with the casing 1 right side, make the inside of casing 1 be in the encapsulated situation, magnetism is fixed can make things convenient for the inside maintenance in later stage, when not using equipment, through rotating bull stick one 21, thereby drive gear one 22 and four bull stick two 23 mesh motions, drive it and rotate to same direction, thereby the receipts of controlling four transfer lines 24 are closed and are carried out the shrink screw 26, make things convenient for it to accomodate.
It should be noted that the model of the single chip microcomputer 42 disclosed in the above embodiments is STM32F103RCT6, the model of the first motor 25 is ZWBMD003003, the model of the second motor 38 is CHS-GM20-20BY, the model of the communication module 45 is LTE-364, the common method in the prior art is adopted for controlling the single chip microcomputer 42 to work, and the common method in the prior art is adopted for controlling the first motor 25, the second motor 38 and the communication module 45 to work BY the single chip microcomputer 42.
The above description is only an embodiment of the present invention, and not intended to limit the scope of the present invention, and all modifications of equivalent structures and equivalent processes, which are made by using the contents of the present specification and the accompanying drawings, or directly or indirectly applied to other related technical fields, are included in the scope of the present invention.
Claims (10)
1. The utility model provides an unmanned aerial vehicle is patrolled and examined to intelligent electric power for high-voltage overhead line which characterized in that: comprises a shell (1), a power unit (2), a shooting unit (3) and a control unit (4);
case (1): a power unit (2) and a shooting unit (3) are arranged on the bracket;
control unit (4): the portable power box is characterized by comprising a sealing plate (41), a single chip microcomputer (42), an adsorption block (43), a magnet (44), a communication module (45) and a battery (46), wherein the single chip microcomputer (42) and the communication module (45) are arranged on the right side inside the shell (1), the input end and the output end of the communication module (45) are connected with the I/O end of the single chip microcomputer (42), a sliding groove is formed in the right side of the shell (1) and communicated with a maintenance opening of the shell (1), the sealing plate (41) and the sliding groove longitudinally slide, the adsorption block (43) is arranged on the right side of the sealing plate (41), an iron sheet is embedded in the inner side of the adsorption block (43), the magnet (44) is embedded in the right side of the shell (1), the sealing plate (41) and the magnet (44) are matched for attraction, and the battery (46) is installed inside the shell (1);
wherein, the input end of the singlechip (42) is electrically connected with the output end of the battery (46) through an external control switch group.
2. The intelligent power inspection unmanned aerial vehicle for the high-voltage overhead line according to claim 1, wherein: the power unit (2) comprises a transmission assembly, a first power assembly, a first motor (25) and four propellers (26), wherein the first motor (25) is installed on the transmission assembly through a motor frame, and the output shaft of each first motor (25) is provided with one propeller (26) and one first motor (25).
3. The intelligent power inspection unmanned aerial vehicle for the high-voltage overhead line according to claim 2, wherein: the transmission assembly comprises two rotating rods (23) and a transmission rod (24), the four corners of the upper side of the casing (1) are respectively provided with the two rotating rods (23), the bottom end of the transmission rod (24) is rotatably connected with the upper side of the casing (1), the upper end of the two rotating rods (23) is respectively provided with the transmission rod (24), and the upper side of the transmission rod (24) is provided with a motor I (25).
4. The intelligent power inspection unmanned aerial vehicle for the high-voltage overhead line according to claim 3, wherein: the power component I comprises a first rotating rod (21) and a first gear (22), the bottom end of the first rotating rod (21) is rotatably connected with the upper side of the machine shell (1), the central position of the first gear (22) is located at the middle end of the first rotating rod (21), a toothed ring is arranged on the outer side of the second rotating rod (23), and the second rotating rod (23) is meshed with the first gear (22) through the toothed ring.
5. The intelligent power inspection unmanned aerial vehicle for the high-voltage overhead line according to claim 1, wherein: the shooting unit (3) comprises a rotating assembly, a fixing assembly, a power assembly II, clamping holes (34), a shooting main body (37) and an installation block (35), wherein the shooting main body (37) is arranged on the bottom side of the installation block (35), and the clamping holes (34) are formed in the left side and the right side of the installation block (35).
6. The intelligent power inspection unmanned aerial vehicle for the high-voltage overhead line according to claim 5, wherein: fixed subassembly contains kelly (33) and fixed block (36), fixed block (36) have two and install on rotating assembly, all be equipped with one kelly (33) on fixed block (36), the middle-end of kelly (33) is equipped with the screw thread, and kelly (33) and fixed block (36) threaded connection, kelly (33) and calorie hole (34) cooperation joint.
7. The intelligent power inspection unmanned aerial vehicle for the high-voltage overhead line according to claim 6, wherein: the rotating assembly comprises a rotating rod III (31) and a mounting plate (32), fixed blocks (36) are arranged at the left end and the right end of the bottom side of the mounting plate (32), the bottom end of the rotating rod III (31) is connected with the center of the upper side of the mounting plate (32), and the rotating rod III (31) is mounted on the power assembly.
8. The intelligent power inspection unmanned aerial vehicle for the high-voltage overhead line according to claim 7, wherein: the second power assembly comprises a second motor (38), the second motor (38) is fixed on the bottom side of the interior of the machine shell (1) through a motor frame, an output shaft of the second motor (38) extends to the outer side of the machine shell (1) and is connected with the upper side of the rotating rod III (31), and the input end of the second motor (38) is electrically connected with the output end of the battery (46) through the single chip microcomputer (42).
9. The intelligent power inspection unmanned aerial vehicle for the high-voltage overhead line according to claim 1, wherein: the portable computer case is characterized by further comprising support rods (5), wherein the support rods (5) are arranged at four corners of the bottom side of the case (1).
10. The intelligent power inspection unmanned aerial vehicle for the high-voltage overhead line according to claim 1, wherein: the support rod is characterized by further comprising a base plate (6), wherein the base plate (6) is arranged on the bottom side of the support rod (5) at the left end, and the base plate (6) is also arranged on the bottom side of the support rod (5) at the right end.
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| CN202111167181.3A CN113815876A (en) | 2021-10-03 | 2021-10-03 | Intelligent power inspection unmanned aerial vehicle for high-voltage overhead line |
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| CN202111167181.3A CN113815876A (en) | 2021-10-03 | 2021-10-03 | Intelligent power inspection unmanned aerial vehicle for high-voltage overhead line |
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Cited By (1)
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| CN115117782A (en) * | 2022-07-11 | 2022-09-27 | 重庆小目科技有限责任公司 | Clamping device of crawler-type overhead transmission line inspection robot |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115117782A (en) * | 2022-07-11 | 2022-09-27 | 重庆小目科技有限责任公司 | Clamping device of crawler-type overhead transmission line inspection robot |
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Application publication date: 20211221 |
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