CN115224632A - A unmanned aerial vehicle stringing structure for electric power iron tower - Google Patents
A unmanned aerial vehicle stringing structure for electric power iron tower Download PDFInfo
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- CN115224632A CN115224632A CN202210943659.5A CN202210943659A CN115224632A CN 115224632 A CN115224632 A CN 115224632A CN 202210943659 A CN202210943659 A CN 202210943659A CN 115224632 A CN115224632 A CN 115224632A
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- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 title claims abstract description 52
- 229910052742 iron Inorganic materials 0.000 title claims abstract description 26
- 238000004804 winding Methods 0.000 claims description 9
- 238000009434 installation Methods 0.000 claims description 7
- 238000001179 sorption measurement Methods 0.000 claims description 6
- 238000000034 method Methods 0.000 description 8
- 230000000694 effects Effects 0.000 description 7
- 240000007643 Phytolacca americana Species 0.000 description 6
- 238000003780 insertion Methods 0.000 description 5
- 230000037431 insertion Effects 0.000 description 5
- 238000000926 separation method Methods 0.000 description 2
- 239000000725 suspension Substances 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
- 238000010586 diagram Methods 0.000 description 1
- 238000010030 laminating Methods 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
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Classifications
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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
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
Abstract
The application discloses an unmanned aerial vehicle stringing structure for an electric power iron tower, which comprises an engine body, wherein a hanging ring is hung on the engine body through a pull rope, a mounting frame is mounted on the hanging ring, a pulley is mounted on the mounting frame, a clamping assembly is arranged on the engine body, and one end of a thin wire penetrates through the mounting frame and is fixed on the engine body through the clamping assembly; the mounting bracket includes canned paragraph and rotation section, the mounting bracket is fixed at the canned paragraph lower extreme, the mount is used for connecting with the stay cord, rotation section rotates and connects in the canned paragraph upper end, rotation section rotates to make rings closed with the cooperation canned paragraph in order to hoist rings on the jib, be equipped with on the canned paragraph and be used for ordering about rotation section and rotate the torsional spring one with closed rings, be equipped with on the stay cord and be used for restricting rotation section and rotate the locating part with closed rings, be equipped with the dismantlement subassembly that is used for making the canned paragraph break away from the stay cord on the canned paragraph, this application is through installing the coaster on unmanned aerial vehicle, and accomplish the work that the fine rule penetrated the coaster mounting bracket subaerial, thereby need not to make the fine rule pass the mounting bracket aloft, and convenient for operation.
Description
Technical Field
The invention relates to the field of stringing of electric power iron towers, in particular to an unmanned aerial vehicle stringing structure for an electric power iron tower.
Background
When a cable is erected between two power towers, an unmanned aerial vehicle is used at present, and when the cable is erected, the unmanned aerial vehicle is used for pulling the other end of the thin wire from one tower to the other tower, and on the other tower, a worker operates a tractor to pull the cable through the thin wire; in the process, the purpose of the unmanned aerial vehicle is mainly to pull the thin wire from one iron tower to the other iron tower; for the erection of cables between large-span iron towers, a plurality of supporting iron towers are also required to be erected between the two iron towers, and pulleys for supporting the cables are hoisted on the supporting iron towers through suspenders so as to ensure the stable stress of the cables; and when utilizing unmanned aerial vehicle stringing, need operate unmanned aerial vehicle and make the fine rule pass the coaster to follow-up when the tractor pulling fine rule, enable the cable and pass the coaster, so that the coaster supports the cable, guarantees that the atress of cable is stable.
Among the correlation technique, the coaster generally includes the type of falling U mounting bracket, mounting bracket one side is equipped with the opening, and the mounting bracket rotates in open position department and is connected with the baffle, the opening is closed all the time to the baffle under the effect of torsional spring, when operation unmanned aerial vehicle made the fine rule pass the coaster, earlier remove the fine rule to baffle one side of mounting bracket, operate unmanned aerial vehicle again, make the fine rule promote the baffle and rotate, the opening is opened to in the fine rule entered into the mounting bracket, and the opening is closed to the baffle under the effect of torsional spring.
To above-mentioned correlation technique, the inventor thinks, when operation unmanned aerial vehicle made the fine rule enter into the mounting bracket, because the fine rule is soft structure, and the coaster hangs on the iron tower, rocks easily, and the fine rule is difficult to enter into in the mounting bracket.
Disclosure of Invention
In order to improve the problem that the fine rule is difficult to enter into in the coaster mounting bracket, this application provides an unmanned aerial vehicle stringing structure for electric power iron tower.
The application provides a pair of an unmanned aerial vehicle stringing structure for electric power iron tower adopts following technical scheme:
an unmanned aerial vehicle stringing structure for an electric power iron tower comprises an engine body, wherein a hanging ring is hung on the engine body through a pull rope, a mounting frame is mounted on the hanging ring, a pulley is mounted on the mounting frame, a clamping assembly is arranged on the engine body, and one end of a thin wire penetrates through the mounting frame and is fixed on the engine body through the clamping assembly; the mounting bracket includes canned paragraph and rotation section, the mounting bracket is fixed at the canned paragraph lower extreme, the mount is used for connecting with the stay cord, the rotation section rotates and connects in the canned paragraph upper end, the rotation section rotates and makes rings closed in order to hoist and mount rings on the jib with the cooperation canned paragraph, be equipped with on the canned paragraph and be used for ordering about the rotation section rotates with the torsional spring of closed rings one, be equipped with on the stay cord and be used for the restriction the rotation section rotates with the locating part of closed rings, be equipped with on the canned paragraph and be used for making the canned paragraph break away from the detaching module of stay cord.
By adopting the technical scheme, during stringing, one end of a thin 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 suspender for supporting the iron tower, the suspender enters the range of the rotating section and the fixed section, then the limiting of the limiting part on the rotating section is cancelled, the rotating section rotates under the action of the torsional spring and closes the hanging ring, the hanging ring is hoisted on the suspender, and then the pull rope is separated from the fixed section through the disassembling assembly, so that the installation of the tackle is completed; through passing the mounting bracket of coaster with the fine rule in advance, then hoist and mount the mounting bracket on the jib to need not to make the fine rule pass the mounting bracket aloft, convenient operation, and install the process on the jib with rings simple, adopt this stringing mode to compare in traditional stringing mode labour saving and time saving more.
Optionally, the limiting part comprises an electromagnet, the electromagnet is fixedly connected to the pull rope, and an adsorption block for adsorbing the electromagnet is fixedly connected to the outer wall of the rotating section.
By adopting the technical scheme, the electromagnet is electrified to generate magnetic force, so that the positioning adsorption block can be prevented from rotating, the rotating section is prevented from rotating, the electromagnet is powered off, and the rotating section rotates under the action of the first torsion spring, so that the hanging ring is closed; the limiting part is simple in structure and convenient to operate.
Optionally, the detaching assembly includes 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 includes 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 close or open the hanging ring, and the fixed section is provided with a second torsion spring for driving the movable section to rotate to close the hanging ring; and the lifting ring is provided with a driving piece for driving the movable section to rotate so as to separate the rope ring from the hanging ring.
Through adopting above-mentioned technical scheme, when making stay cord and canned paragraph separation, rotate through driving piece drive movable section, make the link open, then the link 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 flight, prevent that the stay cord from breaking away from rings.
Optionally, the driving piece comprises 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 into which the first piston plate is inserted 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 poke rod is fixedly connected to the movable section, the push block slides to enable the poke 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 first spring for resetting the first piston plate is arranged in the first air groove.
By adopting the technical scheme, when the pull 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 poke rod to rotate, so that 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, the inner wall of the fixed section is fixedly connected with a first air bag, and the first air bag is communicated with the first air groove.
Through adopting above-mentioned technical scheme, when the rotation section rotates with closed rings, the rotation section promotes piston plate one and removes to under the effect of atmospheric pressure, the inflation of gasbag one, thereby can keep the stability of rings on the jib.
Optionally, a second fixed plate is fixedly connected to the rotating section, a second piston plate is inserted into the second fixed plate, a second air groove for inserting the second piston plate is formed in the second fixed plate, a second air bag is fixedly connected to the inner wall of the rotating section, the second air bag is communicated with the second air groove, and when the rotating section rotates to close the hanging ring, the second fixed plate pushes the second piston plate to move so as to inflate the second air bag; and a second spring for resetting the second piston plate is arranged in the second air groove.
Through adopting above-mentioned technical scheme, when the rotation section rotates with closed rings, the rotation section is followed to the fixed plate two, and the fixed section promotes two slides of piston plate, then under the effect of atmospheric pressure, and gasbag two inflation further keep rings stable on the jib.
Optionally, the rotating section rotates to abut against one surface of the fixed section and is fixedly connected with a rubber pad in a fitting mode.
Through adopting above-mentioned technical scheme, when the rotation section rotates with closed rings, the rubber pad can play certain cushioning effect.
Optionally, the winding roller is rotatably connected to the machine body, the pull rope is wound and fixedly connected to the winding roller, and a motor for driving the winding roller to rotate is arranged on the machine body.
Through adopting above-mentioned technical scheme, be convenient for the rolling stay cord and can adjust the height of rings to rings can be better articulate on the jib.
To sum up, the application comprises the following beneficial technical effects:
1. according to the method, the tackle is installed on the unmanned aerial vehicle, and the thin wire penetrates into the tackle installation frame on the ground, so that the thin wire does not need to penetrate through the installation frame in the air, the operation is convenient, the process of installing the hanging ring on the hanging rod is simple, and the stringing mode is time-saving and labor-saving compared with the traditional stringing mode;
2. this application is through the rotation of rotation section, under the effect of piston board one and piston board two, accomplishes inflating of gasbag one and gasbag two in order to keep the stability of rings on the jib, makes the separation of stay cord and link simultaneously, and is simple and convenient.
Drawings
Fig. 1 is a schematic overall structure diagram of an unmanned aerial vehicle stringing structure for an electric iron tower 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 the region B in fig. 2.
Description of reference numerals:
1. a body; 2. installing a box; 3. a wind-up roll; 4. a splint; 5. a hoisting ring; 6. a mounting frame; 7. a pulley; 8. a fixed section; 9. a rotating section; 10. a first torsion spring; 11. pulling a rope; 12. an electromagnet; 13. an adsorption block; 14. hanging a ring; 15. a rope loop; 16. an active segment; 17. a positioning section; 18. a second torsion spring; 19. inserting a block; 20. inserting slots; 21. a first piston plate; 22. a first inner cavity; 23. a first air groove; 24. a first fixing plate; 25. a push block; 26. a poke rod; 27. a first spring; 28. a first air bag; 29. a second fixing plate; 30. a second air tank; 31. a second piston plate; 32. a second air bag; 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 with reference to figures 1-5.
Referring to fig. 1, the support tower in the present application includes a tower body 34, and a suspension rod 35 is fixedly connected to the tower body 34.
The embodiment of the application discloses an unmanned aerial vehicle stringing structure for electric power iron tower. Referring to fig. 1 and 2, the structure includes a machine body 1, a mounting box 2 is fixedly connected to the machine body 1, a plurality of pulleys 7 are hoisted on the mounting box 2 through a pull rope 11, in this embodiment, two pulleys 7 are provided, and a clamping assembly for clamping a thin wire 36 is provided on the mounting box 2; in stringing, one end of the filament 36 is threaded through the sled 7 assembly and then secured to the mounting box 2 by the clamping assembly.
In this embodiment, fixed rotation is connected with wind-up roll 3 in the install bin 2, and 11 winding fixed connections of stay cord are on wind-up roll 3, and fixed connection is used for driving 3 pivoted motors of wind-up roll in the install bin 2.
In this embodiment, the centre gripping subassembly includes two splint 4 of sliding connection on install bin 2, and two splint 4 are close to each other with centre gripping fine rule 36, and splint 4 passes through two-way lead screw and motor drive, drives two-way lead screw through the motor and rotates to drive two splint 4 and be close to each other.
Referring to fig. 3 and 4, the tackle 7 assembly comprises a lifting ring 5, a mounting frame 6 and a tackle 7, the tackle 7 is mounted on the mounting frame 6, the lifting ring 5 comprises 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 lifting ring 5 so that the lifting ring 5 is lifted on the suspension 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 to the rotating section 9, and when the hanging ring 5 is closed, the first torsion spring 10 is not deformed; the pull rope 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 disassembling component used 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 adsorbed by the electromagnet 12 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 dismounting 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 rotatably connected to the fixed section 8, the movable section 16 rotates to close or open the hanging ring 14, a second torsion spring 18 is fixedly connected to the fixed section 8, the other end of the second torsion spring 18 is fixedly connected with the movable section 16, and when the hanging ring 14 is closed, the second torsion spring 18 is not deformed; the lifting ring 5 is provided with a driving part 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 detaching assembly can also be an electromagnet 12, the electromagnet 12 is fixed on the pull rope 11, and the pull rope 11 and the pulley 7 assembly are connected and separated through the power on and off of the electromagnet 12.
In this embodiment, in order to ensure the stability of the hanging ring 14, an insertion block 19 is fixedly connected to one end of the movable section 16, an insertion slot 20 for the insertion block 19 to rotate to be inserted is formed in the positioning section 17, and when the insertion block 19 is inserted into the insertion slot 20, the hanging ring 14 is closed.
The driving piece comprises a piston plate I21, an inner cavity I22 is formed in the fixed section 8, a fixed plate I24 is fixedly connected to the lower end of the fixed section 8, 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 arranged in a closed mode, the air groove I23 is communicated with the inner cavity I22, a pushing block 25 is connected to the inner cavity I22 in a sliding mode along the direction of a path of the inner cavity I22, a poking rod 26 is fixedly connected to the movable section 16, one end of the poking rod 26 is located on the sliding path of the pushing block 25, the pushing block 25 slides to push the poking rod 26 to rotate, and when the rotating section 9 rotates to close the hanging ring 5, the rotating section 9 pushes the piston plate I21 to move so that the pushing block 25 slides; 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 is deformed, the first piston plate 21 is partially positioned outside the first air groove 23.
The inner wall of the fixed section 8 is fixedly connected with a first air bag 28, the first air bag 28 is in an arc shape matched with the inner wall of the fixed section 8, the first air bag 28 is communicated with the first air groove 23, the position where the first air bag 28 is communicated with the first air groove 23 is located at the initial position of the push block 25, namely, the first air bag 28 is communicated with the first air groove 23 in the process that the push block 25 pushes the poke rod 26 to rotate.
The end, far away from the fixed section 8, of the rotating section 9 is fixedly connected with a second fixed plate 29, a second piston plate 31 is inserted into the second fixed plate 29, a second air groove 30 for inserting the second piston plate 31 is formed in the second fixed plate 29, the second piston plate 31 and the second air groove 30 are arranged in a sealing mode, a second air bag 32 is fixedly connected to the inner wall of the rotating section 9, the second air bag 32 is in an arc shape and is matched with the inner wall of the rotating section 9, the second air bag 32 is communicated with the second air groove 30, a second spring 33 is fixedly connected to the second air groove 30 in 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, the second piston plate 31 is partially located outside the second air groove 30, when the rotating section 9 rotates to close the hanging ring 5, the first fixed plate 24 is attached to the second fixed 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 of rotation section 9 and stationary segment 8 when rotation section 9 rotates with closed rings 5, rotation section 9 rotates with the one side laminating fixedly connected with rubber pad of butt stationary segment 8.
The implementation principle of the unmanned aerial vehicle stringing structure for the electric power iron tower is as follows: during stringing, one end of the thin wire 36 penetrates through the pulley 7 assembly and is fixed on the installation box 2 through the clamping assembly; when the unmanned aerial vehicle flies to the position of the suspender 35, the suspender 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 first torsion spring 10 to close the hanging ring 5, the hanging ring 5 is hung on the suspender 35, in the rotating process of the rotating section 9, the first piston plate 21 and the second piston plate 31 collide with each other and respectively enter the first air groove 23 and the second air groove 30, and under the action of air pressure, the push block 25 pushes the poke 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 is separated from the hanging ring 14; meanwhile, the first air bag 28 and the second air bag 32 are expanded to lock the suspender 35, so that the stability of the pulley 7 assembly is ensured.
The above embodiments are preferred embodiments of the present application, and the protection scope of the present application is not limited by the above embodiments, so: all equivalent changes made according to the structure, shape and principle of the present application shall be covered by the protection scope of the present application.
Claims (8)
1. The utility model provides an unmanned aerial vehicle stringing structure for electric power iron tower, includes organism (1), its characterized in that: a lifting ring (5) is hung on the machine body (1) through a pull rope (11), an installation frame (6) is installed on the lifting ring (5), a pulley (7) is installed on the installation frame (6), a clamping assembly is arranged on the machine body (1), and one end of a thin wire (36) penetrates through the installation frame (6) and is fixed on the machine body (1) through the clamping assembly; mounting bracket (6) are including canned paragraph (8) and rotation section (9), mounting bracket (6) are fixed at canned paragraph (8) lower extreme, canned paragraph (8) are used for connecting with stay cord (11), rotation section (9) rotate to be connected in canned paragraph (8) upper end, rotation section (9) rotate and make rings (5) closed in order to hoist rings (5) on jib (35) with cooperation canned paragraph (8), be equipped with on canned paragraph (8) and be used for ordering about rotate section (9) rotate with the torsional spring (10) of closed rings (5), be equipped with on stay cord (11) and be used for the restriction rotation section (9) rotate with the locating part of closed rings (5), be equipped with on canned paragraph (8) and be used for making canned paragraph (8) break away from the dismantlement subassembly of stay cord (11).
2. The unmanned aerial vehicle stringing structure for an electric power iron tower according to claim 1, wherein: the locating part comprises an electromagnet (12), the electromagnet (12) is fixedly connected to the pull rope (11), and an adsorption block (13) for adsorbing the electromagnet (12) is fixedly connected to the outer wall of the rotating section (9).
3. The unmanned aerial vehicle stringing structure for electric power iron tower according to claim 1, wherein: the disassembling component 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 rotatably connected to the fixed section (8), the movable section (16) rotates to close or open the hanging ring (14), and a second torsion spring (18) for driving the movable section (16) to rotate to close the hanging ring (14) is arranged on the fixed section (8); the hanging ring (5) is provided with a driving piece for driving the movable section (16) to rotate so as to enable the rope ring (15) to be separated from the hanging ring (14).
4. The unmanned aerial vehicle stringing structure for an electric power iron tower according to claim 3, wherein: the driving piece comprises a first piston plate (21), a first inner cavity (22) is formed in the fixed section (8), a first fixed plate (24) is fixedly connected to the fixed section (8), a first air groove (23) for the first piston plate (21) to insert is formed in the first fixed plate (24), the first air groove (23) is communicated with the first inner cavity (22), a pushing block (25) is connected to the first inner cavity (22) in a sliding mode, a poking rod (26) is fixedly connected to the movable section (16), the pushing block (25) slides to enable the poking 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 to enable the pushing block (25) to slide; a first spring (27) for resetting the first piston plate (21) is arranged in the first air groove (23).
5. The unmanned aerial vehicle stringing structure for an electric power iron tower according to claim 4, wherein: the inner wall of the fixed section (8) is fixedly connected with a first air bag (28), and the first air bag (28) is communicated with the first air groove (23).
6. The unmanned aerial vehicle stringing structure for an electric power iron tower according to claim 1, wherein: the rotating section (9) is fixedly connected with a second fixed plate (29), a second piston plate (31) is inserted into the second fixed plate (29), a second air groove (30) for inserting the second piston plate (31) is formed in the second fixed plate (29), a second air bag (32) is fixedly connected to the inner wall of the rotating section (9), the second air bag (32) is communicated with the second air groove (30), and when the rotating section (9) rotates to close the hanging ring (5), the second piston plate (31) is pushed by the fixed section (8) to move to inflate the second air bag (32); and a second spring (33) for resetting the second piston plate (31) is arranged in the second air groove (30).
7. The unmanned aerial vehicle stringing structure for an electric power iron tower according to claim 1, wherein: the rotating section (9) rotates to abut against one surface of the fixed section (8) and is fixedly connected with a rubber pad in a fitting mode.
8. The unmanned aerial vehicle stringing structure for an electric power iron tower according to claim 1, wherein: the winding machine is characterized in that a winding roller (3) is rotatably connected to the machine body (1), the stay cord (11) is fixedly connected to the winding roller (3) in a winding mode, and a motor used 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 |
|---|---|---|---|
| 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 CN115224632B (en) | 2024-02-13 |
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| 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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