CN115224632B - Unmanned aerial vehicle frame line structure for electric power iron tower - Google Patents
Unmanned aerial vehicle frame line structure for electric power iron tower Download PDFInfo
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- CN115224632B CN115224632B CN202210943659.5A CN202210943659A CN115224632B CN 115224632 B CN115224632 B CN 115224632B CN 202210943659 A CN202210943659 A CN 202210943659A CN 115224632 B CN115224632 B CN 115224632B
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- hanging ring
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- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 title claims abstract description 36
- 229910052742 iron Inorganic materials 0.000 title claims abstract description 18
- 238000004804 winding Methods 0.000 claims description 7
- 238000001179 sorption measurement Methods 0.000 claims description 5
- 230000000694 effects Effects 0.000 description 6
- 238000000034 method Methods 0.000 description 5
- 239000000725 suspension Substances 0.000 description 5
- 230000000712 assembly Effects 0.000 description 3
- 238000000429 assembly Methods 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 238000010521 absorption reaction Methods 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- PMVSDNDAUGGCCE-TYYBGVCCSA-L Ferrous fumarate Chemical compound [Fe+2].[O-]C(=O)\C=C\C([O-])=O PMVSDNDAUGGCCE-TYYBGVCCSA-L 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
Classifications
-
- 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
-
- 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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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Load-Engaging Elements For Cranes (AREA)
Abstract
The application discloses an unmanned frame line structure for electric power iron tower, including the organism, hang through the stay cord on the organism and be equipped with rings, install the mounting bracket on the rings, install the coaster on the mounting bracket, be equipped with the clamping assembly on the organism, fine rule one end passes the mounting bracket and passes the clamping assembly to be fixed on the organism; the mounting bracket includes fixed section and rotation section, the mounting bracket is fixed in the fixed section lower extreme, the mount is used for being connected with the stay cord, the rotation section rotates to be connected in the fixed section upper end, it makes rings closure in order to hoist and mount rings on the jib to rotate the section with the cooperation fixed section, be equipped with on the fixed section and be used for driving rotation section rotation in order to close torsional spring one of rings, be equipped with on the stay cord and be used for restricting rotation section rotation in order to close the locating part of rings, be equipped with the dismantlement subassembly that is used for making the fixed section break away from the stay cord on the fixed section, this application is through installing the coaster on unmanned aerial vehicle, and accomplish the work that the fine rule penetrated the coaster mounting bracket at subaerial, thereby need not to make the fine rule pass the mounting bracket in the sky, convenient operation.
Description
Technical Field
The invention relates to the field of electric power iron tower wire erection, in particular to an unmanned rack wire structure for an electric power iron tower.
Background
When a cable is erected between two electric power towers, an unmanned aerial vehicle is used at present, and when the cable is erected, as the cable has a certain weight, the other end of a fine wire is pulled to the other tower from one tower by the unmanned aerial vehicle, and on the other tower, a worker operates a tractor to pull the cable through the fine wire; in the process, the unmanned aerial vehicle mainly aims at pulling a fine wire from one iron tower to the other iron tower; for cable erection among large-span iron towers, a plurality of support iron towers are erected between two iron towers, and pulleys for supporting the cables are hoisted on the support iron towers through hanging rods so as to ensure stable stress of the cables; when the unmanned aerial vehicle is used for wire laying, the unmanned aerial vehicle needs to be operated to enable the fine wire to pass through the pulley, so that the cable can be enabled to pass through the pulley when the tractor pulls the fine wire, the pulley can be enabled to support the cable, and the stability of the stress of the cable is guaranteed.
In the related art, the coaster generally includes the type of falling U mounting bracket, and mounting bracket one side is equipped with the opening, and the mounting bracket rotates in opening position department to be connected with the baffle, and the baffle is closed the opening all the time under the effect of torsional spring, when operation unmanned aerial vehicle makes the fine rule pass the coaster, moves the fine rule to baffle one side of mounting bracket earlier, and the unmanned aerial vehicle of then operation makes the fine rule promote the baffle and rotates, and the opening is opened to the fine rule enters into in the mounting bracket, and the baffle closes the opening under the effect of torsional spring.
With respect to the above-mentioned related art, the inventor believes that when the unmanned aerial vehicle is operated to make the thin wire enter the mounting frame, since the thin wire is of a soft structure and the pulley is hung on the iron tower, the pulley is easy to shake, and the thin wire is difficult to enter the mounting frame.
Disclosure of Invention
In order to improve the problem that fine lines are difficult to enter into a pulley mounting frame, the application provides an unmanned aerial vehicle frame line structure for an electric power iron tower.
The application provides an unmanned aerial vehicle frame line structure for electric power iron tower adopts following technical scheme:
the unmanned aerial vehicle frame line structure for the electric power iron tower comprises a machine body, wherein a lifting ring is hung on the machine body through a pull rope, a mounting frame is mounted on the lifting ring, a pulley is mounted on the mounting frame, a clamping assembly is arranged on the machine body, and one end of a fine line penetrates through the mounting frame and is fixed on the machine body through the clamping assembly; the mounting bracket comprises a fixed section and a rotating section, the mounting bracket is fixed at the lower end of the fixed section, the fixing bracket is used for being connected with a pull rope, the rotating section is rotationally connected at the upper end of the fixed section, the rotating section rotates to be matched with the fixed section to enable the lifting ring to be closed so as to lift the lifting ring on the lifting rod, a torsion spring I for driving the rotating section to rotate so as to close the lifting ring is arranged on the fixed section, a limiting part for limiting the rotating section to rotate so as to close the lifting ring is arranged on the pull rope, and a dismounting assembly for enabling the fixed section to be separated from the pull rope is arranged on the fixed section.
Through the technical scheme, when the wire is erected, one end of a fine wire penetrates through the mounting frame and is fixed on the machine body through the clamping assembly on the machine body, then the unmanned aerial vehicle is controlled to fly to the position of the hanging rod for supporting the iron tower, the hanging rod enters the range of the rotating section and the fixed section, then the limiting of the rotating section by the limiting piece is canceled, the rotating section rotates under the action of the torsion spring and closes the hanging ring, the hanging ring is hoisted on the hanging rod, and then the pull rope is separated from the fixed section through the dismounting assembly, so that the installation of the pulley is completed; through the mounting bracket that passes the coaster with the fine rule in advance, then with the mounting bracket hoist on the jib to need not to make the fine rule pass the mounting bracket in the sky, convenient operation, and install the process on the jib with rings simple, adopt this overhead line mode to compare in traditional overhead line mode labour saving and time saving more.
Optionally, the locating part includes the electro-magnet, electro-magnet fixed connection is in on the stay cord, fixedly connected with supplies on the rotating section outer wall the absorption piece of electro-magnet absorption.
By adopting the technical scheme, the electromagnet is electrified to generate magnetic force so as to position the adsorption block, the rotating section is prevented from rotating, the electromagnet is powered off, and the rotating section rotates under the action of the torsion spring I to close the hanging ring; the limiting piece is simple in structure and convenient to operate.
Optionally, the dismounting component comprises a hanging ring, the lower end of the pull rope is fixedly connected with a rope ring for hanging the hanging ring, the hanging ring comprises a positioning section and a movable section, the positioning section is fixedly connected to the fixed section, the movable section is rotatably connected to the fixed section, the movable section rotates to enable the hanging ring to be closed or opened, and the fixed section is provided with a torsion spring II for driving the movable section to rotate to close the hanging ring; the hanging ring is provided with a driving piece for driving the movable section to rotate so as to enable the rope ring to be separated from the hanging ring.
Through adopting above-mentioned technical scheme, when making stay cord and fixed section separation, through driving piece drive movable section rotation, make the link open, then the rope loop can break away from the link, and torsional spring two can prevent that the movable section from rotating to when unmanned aerial vehicle drives the coaster and fly, prevent that the stay cord from breaking away from rings.
Optionally, the driving piece includes a first piston plate, a first inner cavity is formed in the fixed section, a first fixed plate is fixedly connected to the fixed section, a first air groove for inserting the first piston plate is formed in the first fixed plate, the first air groove is communicated with the first inner cavity, a push block is connected in the first inner cavity in a sliding manner, a toggle rod is fixedly connected to the movable section, the push block slides to enable the toggle rod to rotate, and when the rotating section rotates to close the hanging ring, the rotating section pushes the first piston plate to move to enable the push block to slide; and a spring I for resetting the piston plate I is arranged in the air groove I.
By adopting the technical scheme, when the stay rope is separated from the fixed section, the electromagnet is powered off, the rotating section rotates under the action of the first torsion spring to close the hanging ring, so that the hanging ring is hung on the hanging rod, and when the rotating section rotates to close the hanging ring, the rotating section pushes the first piston plate to move, so that the pushing block is pushed to slide under the action of air pressure, the pushing block slides to push the toggle rod to rotate, the movable section is driven to rotate, the hanging ring is opened, and the rope ring can be separated from the hanging ring; the driving assembly is simple in structure and convenient to operate.
Optionally, an air bag I is fixedly connected to the inner wall of the fixing section, and the air bag I is communicated with the air groove I.
Through adopting above-mentioned technical scheme, when rotating the section of rotating with closed rings, rotate the section and promote first removal of piston board to under the effect of atmospheric pressure, the gasbag is inflated, thereby can keep rings stable on the jib.
Optionally, a second fixing plate is fixedly connected to the rotating section, a second piston plate is inserted onto the second fixing plate, an air groove for inserting the second piston plate is formed in the second fixing plate, an air bag second is fixedly connected to the inner wall of the rotating section, the air bag second is communicated with the air groove second, and when the rotating section rotates to close the hanging ring, the fixing section pushes the second piston plate to move so as to enable the air bag second to be inflated; and a second spring for resetting the second piston plate is arranged in the second air groove.
Through adopting above-mentioned technical scheme, when rotating the section rotation with closed rings, fixed plate two rotates along with the section rotation of rotating, and fixed section promotes piston plate two and slides, then under the effect of atmospheric pressure, gasbag two is expanded, further keeps rings stable on the jib.
Optionally, the rotating section rotates to abut against one face of the fixed section is fixedly connected with a rubber pad in an attaching mode.
Through adopting above-mentioned technical scheme, when rotating the section and rotate with closed rings, the rubber pad can play certain cushioning effect.
Optionally, the last wind-up roll that rotates of organism is connected with, stay cord winding fixed connection is in on the wind-up roll, be equipped with on the organism and be used for driving wind-up roll pivoted motor.
Through adopting above-mentioned technical scheme, be convenient for rolling stay cord and can adjust the height of rings to rings can be better the articulate on the jib.
In summary, the present application includes the following beneficial technical effects:
1. according to the trolley mounting frame, the trolley is mounted on the unmanned aerial vehicle, the fine wires penetrate into the trolley mounting frame on the ground, so that the fine wires do not need to penetrate through the mounting frame in the air, the operation is convenient, the process of mounting the lifting rings on the lifting rods is simple, and the trolley mounting mode is more time-saving and labor-saving compared with the traditional trolley mounting mode;
2. according to the suspension rod, through rotation of the rotating section, under the action of the first piston plate and the second piston plate, inflation of the first air bag and the second air bag is completed so as to keep stability of the suspension ring on the suspension rod, and meanwhile, the pull rope and the suspension ring are separated, so that the suspension rod is simple and convenient.
Drawings
Fig. 1 is a schematic overall structure of a unmanned aerial vehicle frame line structure for a power pylon according to an embodiment of the present application;
FIG. 2 is a partial cross-sectional view of the structure of FIG. 1;
FIG. 3 is a partial schematic view of the structure of FIG. 1;
FIG. 4 is an enlarged schematic view of area A of FIG. 3;
fig. 5 is an enlarged schematic view of region B in fig. 2.
Reference numerals illustrate:
1. a body; 2. a mounting box; 3. a wind-up roll; 4. a clamping plate; 5. a hanging ring; 6. a mounting frame; 7. a pulley; 8. a fixed section; 9. a rotating section; 10. a torsion spring I; 11. a pull rope; 12. an electromagnet; 13. an adsorption block; 14. hanging rings; 15. a rope loop; 16. a movable section; 17. a positioning section; 18. a torsion spring II; 19. inserting blocks; 20. a slot; 21. a first piston plate; 22. an inner cavity I; 23. an air tank I; 24. a first fixing plate; 25. a pushing block; 26. a toggle rod; 27. a first spring; 28. an air bag I; 29. a second fixing plate; 30. an air groove II; 31. a second piston plate; 32. an air bag II; 33. a second spring; 34. a tower body; 35. a boom; 36. a thin wire.
Detailed Description
The present application is described in further detail below in conjunction with figures 1-5.
Referring to fig. 1, the support tower in the present application includes a tower body 34, and a boom 35 is fixedly connected to the tower body 34.
The embodiment of the application discloses an unmanned frame wire structure for electric power iron tower. Referring to fig. 1 and 2, the structure comprises a machine body 1, a mounting box 2 is fixedly connected to the machine body 1, pulley 7 assemblies are hoisted on the mounting box 2 through a pull rope 11, the number of the pulley 7 assemblies is plural, in the embodiment, the number of the pulley 7 assemblies is two, and a clamping assembly for clamping a fine wire 36 is arranged on the mounting box 2; in stringing, one end of the wire 36 is passed through the trolley 7 assembly and then secured to the mounting box 2 by the clamping assembly.
In this embodiment, the wind-up roller 3 is fixedly connected with in the installation box 2 in a rotating way, the pull rope 11 is fixedly connected on the wind-up roller 3 in a winding way, and a motor for driving the wind-up roller 3 to rotate is fixedly connected in the installation box 2.
In this embodiment, the clamping assembly includes two clamping plates 4 slidably connected to the mounting box 2, the two clamping plates 4 are close to each other to clamp the thin line 36, the clamping plates 4 are driven by a bi-directional screw and a motor, and the bi-directional screw is driven by the motor to rotate so as to drive the two clamping plates 4 to be close to each other.
Referring to fig. 3 and 4, the pulley 7 assembly includes a hanging ring 5, a mounting frame 6 and a pulley 7, the pulley 7 is mounted on the mounting frame 6, the hanging ring 5 includes a fixed section 8 and a rotating section 9, the rotating section 9 is hinged at one end of the fixed section 8, and the rotating section 9 rotates to close the hanging ring 5 so that the hanging ring 5 is hung on a hanging rod 35; the mounting frame 6 is fixedly connected to the lower end of the fixed section 8, the first torsion spring 10 is fixedly connected to the fixed section 8, the other end of the first torsion spring 10 is fixedly connected with the rotating section 9, and the first torsion spring 10 is not deformed when the hanging ring 5 is closed; the stay cord 11 is provided with a limiting piece for limiting the rotation of the rotating section 9 to close the hanging ring 5; the fixed section 8 is provided with a dismounting component for separating the fixed section 8 from the pull rope 11.
The limiting piece comprises an electromagnet 12, the electromagnet 12 is fixedly connected to the pull rope 11, and an adsorption block 13 for the electromagnet 12 to adsorb is fixedly connected to the outer wall of the rotating section 9; when the electromagnet 12 adsorbs the adsorption block 13, the hanging ring 5 is opened.
Referring to fig. 3 and 5, the disassembly assembly comprises a hanging ring 14, a rope ring 15 for hanging the hanging ring 14 is fixedly connected to the lower end of a pull rope 11, the hanging ring 14 comprises a positioning section 17 and a movable section 16, the positioning section 17 is fixedly connected to a fixed section 8, the movable section 16 is rotatably connected to the fixed section 8, the movable section 16 is rotated to enable the hanging ring 14 to be closed or opened, a torsion spring II 18 is fixedly connected to the fixed section 8, the other end of the torsion spring II 18 is fixedly connected with the movable section 16, and the torsion spring II 18 is not deformed when the hanging ring 14 is closed; the hanging ring 5 is provided with a driving piece for driving the movable section 16 to rotate so as to separate the rope ring 15 from the hanging ring 14.
In another embodiment, the disassembling component can also be an electromagnet 12, the electromagnet 12 is fixed on the pull rope 11, and the connection and separation of the pull rope 11 and the pulley 7 component are realized through the on-off of the electromagnet 12.
In this embodiment, in order to ensure stability of the hanging ring 14, an insert block 19 is fixedly connected to one end of the movable section 16, a slot 20 into which the insert block 19 rotates to insert is formed in the positioning section 17, and when the insert block 19 is inserted into the slot 20, the hanging ring 14 is closed.
The driving piece comprises a piston plate I21, an inner cavity I22 is formed in a fixed section 8, the lower end of the fixed section 8 is fixedly connected with a fixed plate I24, an air groove I23 for the piston plate I21 to insert is formed in the fixed plate I24, the piston plate I21 and the air groove I23 are in closed arrangement, the air groove I23 is communicated with the inner cavity I22, a push block 25 is slidingly connected in the inner cavity I22 along the self path direction, a toggle rod 26 is fixedly connected to a movable section 16, one end of the toggle rod 26 is positioned on the sliding path of the push block 25, the push block 25 slides to push the toggle rod 26 to rotate, and when a rotating section 9 rotates to close a hanging ring 5, the rotating section 9 pushes the piston plate I21 to move so as to slide the push block 25; a first spring 27 is fixedly connected in the first air groove 23 along the sliding direction of the first piston plate 21, the other end of the first spring 27 is fixedly connected to the first piston plate 21, and when the first spring 27 deforms, a part of the first piston plate 21 is positioned outside the first air groove 23.
The inner wall of the fixed section 8 is fixedly connected with an air bag I28, the air bag I28 is in an arc shape matched with the inner wall of the fixed section 8, the air bag I28 is communicated with an air groove I23, and the communication position of the air bag I28 and the air groove I23 is positioned at the initial position of the push block 25, namely, the air bag I28 and the air groove I23 are communicated in the process that the push block 25 pushes the toggle rod 26 to rotate.
The end of the rotating section 9 far away from the fixed section 8 is fixedly connected with a second fixing plate 29, a second piston plate 31 is inserted on the second fixing plate 29, an air groove second 30 for inserting the second piston plate 31 is formed in the second fixing plate 29, the second piston plate 31 and the second air groove 30 are in sealing arrangement, an air bag second 32 is fixedly connected to the inner wall of the rotating section 9, the air bag second 32 is arc-shaped and is matched with the inner wall of the rotating section 9, the air bag second 32 and the second air groove 30 are communicated, a second spring 33 is fixedly connected to the second air groove 30 along the sliding direction of the second piston plate 31, the other end of the second spring 33 is fixedly connected to the second piston plate 31, when the second spring 33 is not deformed, a part of the second piston plate 31 is positioned outside the second air groove 30, when the rotating section 9 rotates to close the hanging ring 5, the first fixing plate 24 is attached to the second fixing plate 29, and the first piston plate 21 and the second piston plate 31 interact to enter the first air groove 23 and the second air groove 30 respectively.
In this embodiment, in order to slow down the collision between the rotating section 9 and the fixed section 8 when the rotating section 9 rotates to close the hanging ring 5, the rotating section 9 rotates to abut against one surface of the fixed section 8 to be fixedly connected with a rubber pad.
The implementation principle of the unmanned rack wire structure for the electric power iron tower is as follows: during wire laying, one end of the thin wire 36 passes through the pulley 7 assembly and is then fixed on the mounting box 2 through the clamping assembly; when the unmanned aerial vehicle flies to the position of the hanging rod 35, the hanging rod 35 enters the range of the rotating section 9 and the fixed section 8, the electromagnet 12 is powered off, the rotating section 9 rotates under the action of the torsion spring I10 to close the hanging ring 5, the hanging ring 5 is hung on the hanging rod 35, in the rotating process of the rotating section 9, the piston plate I21 and the piston plate II 31 collide with each other and respectively enter the air groove I23 and the air groove II 30, under the action of air pressure, the pushing block 25 pushes the toggle rod 26 to rotate, so that the movable section 16 is driven to rotate, the hanging ring 14 is opened, and the rope ring 15 and the hanging ring 14 are separated; at the same time, the first and second air bags 28, 32 are inflated to lock the boom 35, ensuring the stability of the assembly of the trolley 7.
The foregoing are all preferred embodiments of the present application, and are not intended to limit the scope of the present application in any way, therefore: all equivalent changes in structure, shape and principle of this application should be covered in the protection scope of this application.
Claims (6)
1. An unmanned aerial vehicle frame line structure for electric power iron tower, includes organism (1), its characterized in that: hanging rings (5) are hung on the machine body (1) through pull ropes (11), mounting frames (6) are mounted on the hanging rings (5), pulleys (7) are mounted on the mounting frames (6), clamping components are arranged on the machine body (1), and one ends of thin wires (36) penetrate through the mounting frames (6) and are fixed on the machine body (1) through the clamping components; the mounting frame (6) comprises a fixed section (8) and a rotating section (9), the mounting frame (6) is fixed at the lower end of the fixed section (8), the fixed section (8) is used for being connected with a pull rope (11), the rotating section (9) is rotationally connected at the upper end of the fixed section (8), the rotating section (9) rotates to be matched with the fixed section (8) to enable the hanging ring (5) to be closed so as to enable the hanging ring (5) to be hung on a hanging rod (35), a torsion spring I (10) for driving the rotating section (9) to rotate so as to close the hanging ring (5) is arranged on the fixed section (8), a limiting piece for limiting the rotating section (9) to rotate so as to close the hanging ring (5) is arranged on the pull rope (11), and a disassembling component for enabling the fixed section (8) to be separated from the pull rope (11) is arranged on the fixed section (8). The disassembly assembly comprises a hanging ring (14), the lower end of the pull rope (11) is fixedly connected with a rope ring (15) for hanging the hanging ring (14), the hanging ring (14) comprises a positioning section (17) and a movable section (16), the positioning section (17) is fixedly connected to the fixed section (8), the movable section (16) is rotationally connected to the fixed section (8), the movable section (16) rotates to enable the hanging ring (14) to be closed or opened, and a torsion spring II (18) for driving the movable section (16) to rotate to close the hanging ring (14) is arranged on the fixed section (8); the lifting ring (5) is provided with a driving piece for driving the movable section (16) to rotate so as to separate the rope ring (15) from the hanging ring (14); the driving piece comprises a first piston plate (21), an inner cavity (22) is formed in the fixed section (8), a first fixed plate (24) is fixedly connected to the fixed section (8), an air groove (23) for the first piston plate (21) to be inserted is formed in the first fixed plate (24), the first air groove (23) is communicated with the first inner cavity (22), a push block (25) is connected in the first inner cavity (22) in a sliding manner, a toggle rod (26) is fixedly connected to the movable section (16), the push block (25) slides to enable the toggle rod (26) to rotate, and when the rotating section (9) rotates to close the hanging ring (5), the rotating section (9) pushes the first piston plate (21) to move so as to enable the push block (25) to slide; a first spring (27) for resetting the first piston plate (21) is arranged in the first air groove (23).
2. An unmanned aerial vehicle frame line structure for a power pylon according to claim 1, wherein: the limiting piece comprises an electromagnet (12), the electromagnet (12) is fixedly connected to the pull rope (11), and an adsorption block (13) for the electromagnet (12) to adsorb is fixedly connected to the outer wall of the rotating section (9).
3. An unmanned aerial vehicle frame line structure for a power pylon according to claim 1, wherein: the inner wall of the fixing section (8) is fixedly connected with an air bag I (28), and the air bag I (28) is communicated with the air groove I (23).
4. An unmanned aerial vehicle frame line structure for a power pylon according to claim 1, wherein: the device is characterized in that a fixed plate II (29) is fixedly connected to the rotating section (9), a piston plate II (31) is inserted onto the fixed plate II (29), an air groove II (30) for inserting the piston plate II (31) is formed in the fixed plate II (29), an air bag II (32) is fixedly connected to the inner wall of the rotating section (9), the air bag II (32) is communicated with the air groove II (30), and when the rotating section (9) rotates to close the hanging ring (5), the fixed section (8) pushes the piston plate II (31) to move so as to enable the air bag II (32) to be inflated; and a second spring (33) for resetting the second piston plate (31) is arranged in the second air groove (30).
5. An unmanned aerial vehicle frame line structure for a power pylon according to claim 1, wherein: the rotating section (9) rotates to abut against one surface of the fixed section (8) to be fixedly connected with a rubber pad in an attaching mode.
6. An unmanned aerial vehicle frame line structure for a power pylon according to claim 1, wherein: the winding machine is characterized in that a winding roller (3) is rotationally connected to the machine body (1), the pull rope (11) is fixedly connected to the winding roller (3) in a winding mode, and a motor for driving the winding roller (3) to rotate is arranged on the machine body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN202210943659.5A CN115224632B (en) | 2022-08-08 | 2022-08-08 | Unmanned aerial vehicle frame line structure for electric power iron tower |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202210943659.5A CN115224632B (en) | 2022-08-08 | 2022-08-08 | Unmanned aerial vehicle frame line structure for electric power iron tower |
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| CN115224632B true CN115224632B (en) | 2024-02-13 |
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| JP2005184927A (en) * | 2003-12-17 | 2005-07-07 | Kansai Electric Power Co Inc:The | Device for lifting overhead wire |
| JP2016208625A (en) * | 2015-04-20 | 2016-12-08 | 株式会社システック・エンジニアリング | Extension method for pilot rope, removal method for final rope, and unmanned multicopter used therefor |
| CN109473910A (en) * | 2018-10-17 | 2019-03-15 | 北京科技大学 | Unmanned plane stringing system and stringing method |
| CN209461906U (en) * | 2018-12-13 | 2019-10-01 | 国网浙江省电力有限公司杭州供电公司 | A kind of sister block coaster easy to use |
| KR20210094957A (en) * | 2020-01-22 | 2021-07-30 | 한국전력공사 | Apparatus and method for wire installation using AI drone |
| CN113746028A (en) * | 2021-10-14 | 2021-12-03 | 南京王府电力工程设备有限公司 | Erection device for power transmission and distribution network |
| CN216546691U (en) * | 2022-02-21 | 2022-05-17 | 成都庆军科技有限公司 | Rotor electric power stringing unmanned aerial vehicle |
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