Tower operation anti-falling rope installation method

Abstract

The invention relates to the field of power construction, in particular to a tower operation anti-falling rope installation method. The method comprises the steps that S1, an anti-falling rope is fixed to an anti-falling mechanism, and the unmanned aerial vehicle and the anti-falling mechanism are locked; s2, the anti-falling mechanism is driven by the unmanned aerial vehicle to fly to the set height, the anti-falling mechanism is released to the angle steel of the angle steel tower, and the anti-falling mechanism is locked to the angle steel; s3, the unmanned aerial vehicle and the anti-falling mechanism are unlocked, and the unmanned aerial vehicle is recycled; s4, a limiting ring is fixed in the carrying cabin, and the anti-falling rope penetrates through the limiting ring; s5, the carrying cabin is started to climb upwards along the anti-falling rope, after the carrying cabin climbs to the set height, the carrying cabin is opened, the limiting ring is released, and the limiting ring is fixedly connected with foot nails on the angle steel tower; and S6, the carrying cabin is closed to enable the carrying cabin to climb downwards along the anti-falling rope, and installation is completed after the carrying cabin is recycled. According to the angle steel tower anti-falling device, angle steel of different sizes can be clamped and fixed in a self-adaptive mode, and an anti-falling rope is firmly installed on an angle steel tower.

Description

Technical Field

[0001] The invention relates to the field of electric power construction, and in particular to a method for installing a falling prevention rope for a pole tower operation. Background Art

[0002] During the daily maintenance work of the power transmission and transformation line tower, it is necessary to climb up to inspect the distribution line. Before the climbing work, it is necessary to install protective measures in advance. The commonly used protective measures are to fix the anti-fall rope on the angle steel of the tower. The anti-fall rope is an important component connecting the safety belt and the anchor point. It is usually made of high-strength materials. In the event of a fall accident, the anti-fall rope can quickly play a role, absorb the impact force, and reduce the damage caused by the fall to the high-altitude workers. The current installation device of the anti-fall rope is shown in the patent number "CN220842989U". A hanging ring is set on the inner ring of the landing gear. The hook of the tower anti-fall device is hung in the hanging ring. The hook is set at the top of the hook. The bottom of the hook is fixedly connected to the top of the speed difference automatic controller. The anti-fall rope is set on the speed difference automatic controller. The drone hangs the hook of the anti-fall device on the angle steel of the tower, thereby completing the installation of the anti-fall rope.

[0003] Due to the different widths of the angle steels on the angle steel tower, the hook cannot adapt to angle steels of different sizes. When the angle steel is too narrow, the hook is prone to swing back and forth after being hung. When the angle steel is too wide, the opening size of the hook is insufficient and it cannot be smoothly hung on the angle steel. Even if the hook is successfully hung on the angle steel, the hook and the angle steel are not locked and the hook is prone to slide along the angle steel. The maintenance personnel have a high operating risk, so this problem needs to be solved urgently. Summary of the invention

[0004] In order to avoid and overcome the technical problems existing in the prior art, the present invention provides a method for installing a fall prevention rope for pole tower operation. The present invention can realize adaptive clamping and fixing of angle steels of different sizes, so that the fall prevention rope can be firmly installed on the angle steel tower.

[0005] To achieve the above object, the present invention provides the following technical solutions:

[0006] A method for installing a tower operation anti-falling rope comprises the following steps:

[0007] S1. Fix the anti-fall rope to the anti-fall mechanism and lock the drone with the anti-fall mechanism.

[0008] S2. Use the drone to drive the anti-fall mechanism to fly to a set height, release the anti-fall mechanism to the angle steel of the angle steel tower, and lock the anti-fall mechanism on the angle steel;

[0009] S3, unlock the drone and the anti-fall mechanism, and recover the drone;

[0010] S4. Fix the limiting ring in the carrying cabin and pass the anti-fall rope through the limiting ring;

[0011] S5, start the transport cabin to make it climb up along the anti-fall rope. After climbing to the set height, open the transport cabin and release the limit ring so that the limit ring is connected and fixed with the foot nails on the angle steel tower;

[0012] S6. Close the transport cabin and allow the user to climb down along the anti-fall rope. Recover the transport cabin and complete the installation.

[0013] As a further scheme of the present invention: the anti-fall mechanism includes an anti-fall seat in a right-angle bend, and the anti-fall seat and the angle steel form a right-angle abutment and positioning; a sliding seat and an angle steel clamp mounted on the outer ring of the sliding seat are arranged in the horizontal direction inside the anti-fall seat, and a linear power source drives the angle steel clamp to slide along the sliding seat; an angle steel locking tongue is hingedly provided at the bottom of the opening of the angle steel clamp away from the side of the angle steel to be clamped, and the hinge axis is arranged parallel to the angle steel to be clamped; the positioning section of the angle steel locking tongue is located within the projection range of the opening of the angle steel clamp along the length direction of the angle steel clamp, and the sliding seat abuts against the positioning section of the angle steel clamp after passing through the opening of the angle steel clamp to drive the angle steel clamp to flip around the hinge axis, and an opening is provided at the bottom of the horizontal section of the anti-fall seat for the angle steel clamp to pass through.

[0014] As a further solution of the present invention: a magnetic block is provided in the opening of the angle steel clamp away from the side of the angle steel to be clamped, and when the slide is located in the opening cavity of the angle steel clamp, the positioning section of the angle steel lock tongue is magnetically attracted by the magnetic block and enters the opening cavity of the angle steel clamp, so that the angle between the angle steel lock tongue and the angle steel clamp is not less than ninety degrees; after the slide passes through the opening of the angle steel clamp and pushes the angle steel lock tongue to flip, the angle between the angle steel lock tongue and the angle steel clamp is less than ninety degrees.

[0015] As a further solution of the present invention: the linear power source includes a pull rod which is vertically slidably arranged in the vertical section of the anti-fall seat, the pull rod is pulled by the lifting mechanism to produce a vertical lifting action, and a bent connecting rod is arranged in the anti-fall seat, one end of the connecting rod is hingedly cooperated with the angle steel clamp block, and the other end of the connecting rod is hingedly cooperated with the pull rod, and each hinge axis is parallel to the hinge axis of the angle steel lock tongue; while the pull rod moves vertically, the angle steel clamp block is driven to slide along the slide seat through the connecting rod.

[0016] As a further solution of the present invention: the lifting mechanism includes a tension spring that applies a downward pulling force to the pull rod along the vertical direction within the vertical section, and a drone that applies a vertical upward pulling force to the pull rod, and the gravity of the anti-fall mechanism is greater than the elastic force of the tension spring; a pin seat is provided on the pull rod and is located above the anti-fall seat, and at least two groups of elastic pins are provided at intervals at the bottom of the pin seat along the direction parallel to the axis of the angle steel clamp block, and the elastic pins can float along the vertical direction; a guide hole corresponding to the vertical position of the elastic pin is opened on the anti-fall seat for the elastic pin to pass through; at least two rows of pin holes are evenly arranged on the angle steel clamp block along the length direction to correspond to the positions of each elastic pin, and the pin holes in two adjacent rows are staggered front and back, and the diameter of the elastic pin is smaller than the diameter of the pin hole.

[0017] As a further solution of the present invention: the anti-fall mechanism also includes a guide seat for connecting to the drone, a docking channel is provided on the guide seat along the plumb direction, and a lifting seat is provided on the drone, which is plugged and matched with the docking channel along the plumb direction. After the lifting seat is inserted into the docking channel, it is locked or unlocked by a locking mechanism; the locking mechanism includes a positioning groove provided in the docking channel along the plumb direction, a telescopic channel is provided in the lifting seat along the plumb direction, the telescopic rod is arranged in the telescopic channel along the plumb direction, and a locking block is also hingedly provided at the opening of the telescopic channel, and the hinge axis is arranged horizontally, and a locking block spring is arranged radially in the telescopic channel, and the two ends of the locking block spring are respectively abutted against the inner wall of the telescopic channel and the locking block, thereby applying an elastic force toward the axial direction of the telescopic channel to the locking block; the vertical telescopic trajectory of the telescopic rod intersects with the position of the locking block, and after the telescopic rod is extended and retracted and produces a radial pushing action on the locking block, the locking block enters the positioning groove of the docking channel to abut against the limit, thereby producing a locking action on the lifting seat.

[0018] As a further solution of the present invention: the transport cabin includes a cabin body that can generate opening and closing actions and a swivel seat that drives the cabin body to rotate, the swivel axis of the swivel seat is arranged along the plumb direction, and an upper guide cover and a lower guide cover are respectively provided on the top of the cabin body and the bottom of the swivel seat. The upper guide cover is a conical structure with the tip facing upward, and the lower guide cover is a conical structure with the tip facing downward; a climbing rope seat for climbing an anti-fall rope is fixed on the swivel seat, and the anti-fall rope passes through the upper guide cover, the climbing rope seat and the lower guide cover in sequence along the axial direction of the transport cabin.

[0019] As a further solution of the present invention: the cabin body of the carrier cabin is arranged in a split type and is arranged symmetrically along the vertical direction. Two groups of rocker arms hinged to the swivel seat are provided on the rotating end of the swivel seat. The two rocker arms are respectively hinged to the two sections of the cabin body of the carrier cabin, and the hinge axis is arranged parallel to the rotation axis of the swivel seat. When the two rocker arms rotate, the two sections of the cabin body of the carrier cabin are driven to open and close. The upper guide cover is arranged in a split type and symmetrically, thereby corresponding to the two sections of the cabin body of the carrier cabin respectively. The two sections of the cover body of the upper guide cover are hinged to the carrier cabin, and the hinge axis is arranged parallel to the hinge axis of the rocker arm. The upper guide cover is driven by a power source to open and close.

[0020] As a further solution of the present invention: a lower guide cover is arranged under the rotating seat, and the lower guide cover is in a conical structure with the tip pointing downward; the rotating seat includes a rotating end for fixing the cabin body and a non-rotating end coaxially rotating with the rotating end, and the non-rotating end of the rotating seat is evenly provided with telescopic guide forks extending from the inside to the outside of the rotating seat along the radial direction, and two adjacent telescopic guide forks clamp the angle steel of the angle steel tower to limit the rotation of the carrier cabin.

[0021] As a further solution of the present invention: the limit ring includes a connecting rod arranged along the vertical direction, and a coaxially arranged upper limit ring and a lower limit ring are fixed on the connecting rod. The upper limit ring and the lower limit ring are both provided with notches for the rope body to pass through, and the directions of the notches are opposite to each other. A clamping seat for clamping the foot nail is also provided on the connecting rod, and the clamping seat and the upper limit ring and the lower limit ring are avoided in the vertical direction.

[0022] Compared with the prior art, the present invention has the following beneficial effects:

[0023] 1. The drone of the present invention first drives the anti-fall mechanism to rise. At this time, the elongation of the tension spring reaches the maximum, the connecting rod swings upward with the rotating shaft, and drives the angle steel clamp to slide in the direction away from the pull rod. At this time, the end of the slide is located in the opening of the angle steel clamp, and the angle between the angle steel lock tongue and the angle steel clamp is a right angle or an obtuse angle. After reaching the set working height, the drone drives the anti-fall mechanism to buckle onto the angle steel from top to bottom, and drives the pull rod downward. Under the action of the tension spring, the connecting rod drives the angle steel clamp to slide along the slide toward the pull rod until the end of the slide passes through the opening of the angle steel clamp, and the angle steel lock tongue is pushed by the slide, so that the angle between it and the angle steel clamp is an acute angle. The drone drives the anti-fall mechanism to move downward until it is finally unlocked with the anti-fall mechanism. Under the action of the tension spring, the angle steel clamp continues to slide in the direction of the pull rod until the angle steel lock tongue abuts against the angle steel to be clamped, completing the clamping and positioning of the angle steel, and can realize adaptive clamping and fixing of angle steels of different sizes.

[0024] 2. When the present invention needs to complete the locking of the drone and the anti-fall mechanism, the drone first drives the lifting seat to move downward so that the lifting seat is inserted into the docking channel. The telescopic rod is driven to extend and retract outside the telescopic channel. When the telescopic rod moves downward, it pushes the locking block outward in the radial direction, so that the step surface of the locking block moves outward into the positioning groove. Then the drone flies upward, and the step surface of the locking block abuts and positions with the positioning groove. At this time, the locking of the drone and the anti-fall mechanism is completed, and the drone drives the anti-fall mechanism to fly synchronously. When it is necessary to unlock the anti-fall mechanism and the drone, the telescopic rod is retracted into the telescopic channel, and at this time, the telescopic rod is out of contact with the locking block. Under the elastic force of the locking block spring, the locking block resets and retracts, and is out of contact with the positioning groove. At this time, the locking block is located within the projection range of the telescopic channel along the plumb direction. When the drone flies upward, the lifting seat is out of contact with the docking channel, completing the unlocking process.

[0025] 3. The two rows of pin holes of the present invention are staggered front and back, so at least one group of elastic pins can be inserted into one of the groups of pin holes to complete the pin positioning to limit the relative sliding between the angle steel clamping block and the slide seat; through the magnetic attraction of the magnetic block, the angle steel lock tongue is in an open state in the flight state, which is convenient for subsequent clamping of the angle steel from top to bottom.

[0026] 4. The present invention first passes the anti-fall rope through the upper guide cover, the limiting ring, the climbing rope seat and the lower guide cover on the ground, and drives the carrier cabin to climb along the anti-fall rope through the climbing rope seat. During the climbing process, when encountering the foot nails, the conical surface of the upper guide cover slides through the foot nails alternately. After climbing to the set height, extend the telescopic guide fork to clamp and position the angle steel tower. Then rotate the swivel seat to make the limiting ring correspond to the foot nail position on the angle steel tower. Open the upper guide cover and the cabin body, so that the clamping seat of the limiting ring is clamped and fixed on the foot nail, and the limiting ring is now separated from the carrier cabin. After the carrier cabin moves downward, close the cabin body and the upper guide cover, and return to the ground to complete the installation of the limiting ring. BRIEF DESCRIPTION OF THE DRAWINGS

[0027] Figure 1 It is a schematic diagram of the coordination state between the anti-fall device of the present invention and the UAV.

[0028] Figure 2 It is a structural schematic diagram of the anti-fall seat in the present invention.

[0029] Figure 3 It is a schematic diagram of the state when the lifting seat and the guide seat are docked in the present invention.

[0030] Figure 4 It is a schematic diagram of the locking state of the anti-fall seat in the present invention.

[0031] Figure 5 It is a schematic diagram of the first working state of the carrier cabin in the present invention.

[0032] Figure 6 It is a schematic diagram of the second working state of the carrier cabin in the present invention.

[0033] Figure 7 It is a schematic diagram of the third working state of the carrier cabin in the present invention.

[0034] Figure 8 It is a schematic diagram of the fourth working state of the carrier cabin in the present invention.

[0035] Fig. 9 It is a schematic diagram of the fifth working state of the carrier cabin in the present invention.

[0036] Fig.10 It is a schematic diagram of the internal structure of the carrier cabin in the present invention.

[0037] In the figure:

[0038] 1. UAV; 11. Lifting seat; 111. Telescopic rod; 112. Locking block; 113. Locking block spring;

[0039] 2. Anti-fall mechanism; 21. Pull rod; 22. Latch seat; 221. Elastic latch;

[0040] 23. Guide seat; 231. Docking channel; 232. Positioning groove;

[0041] 24. anti-fall seat; 241. connecting rod; 242. guide groove; 243. guide hole;

[0042] 244, angle steel clamp block; 2441, latch hole; 245, angle steel lock tongue; 2451, magnetic suction block;

[0043] 25. Sliding seat; 26. Tension spring; 27. Rotating shaft;

[0044] 3. Anti-fall rope; 4. Carrying cabin; 41. Upper guide cover;

[0045] 42. swivel seat; 421. telescopic guide fork; 422. lower guide cover;

[0046] 43. Rope climbing seat; 44. Swinging pole;

[0047] 5. Limiting ring; 51. Connecting rod; 52. Upper limiting ring; 53. Lower limiting ring; 54. Clamping seat. DETAILED DESCRIPTION

[0048] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0049] See also Figures 1 to 10 In an embodiment of the present invention, a method for installing a tower operation anti-falling rope includes the following steps:

[0050] S1, fix the anti-fall rope 3 on the anti-fall mechanism 2, and lock the drone 1 and the anti-fall mechanism 2;

[0051] S2, driving the anti-fall mechanism 2 to fly to a set height by the drone 1, releasing the anti-fall mechanism 2 to the angle steel of the angle steel tower, and locking the anti-fall mechanism 2 on the angle steel;

[0052] S3, unlocking the drone 1 and the anti-fall mechanism 2, and recovering the drone 1;

[0053] S4, fix the limiting ring 5 in the carrying cabin 4, and pass the anti-falling rope 3 through the limiting ring 5;

[0054] S5, start the carrying cabin 4 to make it climb upward along the anti-fall rope 3. After climbing to the set height, open the carrying cabin 4 and release the limiting ring 5, so that the limiting ring 5 is connected and fixed with the foot nails on the angle steel tower;

[0055] S6, close the carrying cabin 4 and allow the user to climb down along the anti-fall rope 3, and complete the installation after recovering the carrying cabin 4.

[0056] According to the different heights of the angle steel tower, steps S4 to S6 are repeated to install the limiting rings 5 ​​at different height intervals to ensure the stability of the anti-fall rope 3.

[0057] The following is a detailed description of each structural part:

[0058] Drone 1

[0059] The drone 1 includes a lifting seat 11 arranged along a vertical direction at the bottom of the drone 1, and a cross-staggered guide fork is arranged radially on the lifting seat 11. A telescopic channel is vertically arranged in the lifting seat 11, and the bottom of the telescopic channel is open. Two groups of locking blocks 112 are hingedly arranged at the opening. The two groups of locking blocks 112 are arranged symmetrically on the left and right, and the outer side surfaces of the locking blocks 112 are provided with step surfaces for positioning. A locking block spring 113 is radially arranged in the telescopic channel, and the locking block spring 113 applies elastic force to the locking block 112 so that the step surface of the locking block 112 is located in the telescopic channel.

[0060] The drone 1 is docked with the guide seat 23 of the anti-fall mechanism 2 through the lifting seat 11. A docking channel 231 is provided in the guide seat 23 along the vertical direction. A guide fork with a V-shaped opening is provided at the top of the docking channel 231 for the lifting seat 11 to be inserted into the docking channel 231. A positioning groove 232 is provided on the inner wall of the docking channel 231 along the vertical direction. The positioning groove 232 is used to position the locking block 112.

[0061] A telescopic rod 111 is axially arranged in the telescopic channel, the diameter of the telescopic rod 111 is smaller than the diameter of the telescopic channel, and the top surface of the locking block 112 and the bottom surface of the telescopic rod 111 are conical.

[0062] When it is necessary to complete the locking of the drone 1 and the anti-fall mechanism 2, the drone 1 first drives the lifting seat 11 to move downward so that the lifting seat 11 is inserted into the docking channel 231. The telescopic rod 111 is driven to extend and retract outside the telescopic channel. When the telescopic rod 111 moves downward, it pushes the locking block 112 outward in the radial direction, so that the step surface of the locking block 112 moves outward to the positioning groove 232. Then the drone 1 flies upward, and the step surface of the locking block 112 abuts and positions with the positioning groove 232. At this time, the locking of the drone 1 and the anti-fall mechanism 2 is completed, and the drone 1 drives the anti-fall mechanism 2 to fly synchronously. When it is necessary to unlock the anti-fall mechanism 2 and the drone 1, the telescopic rod 111 is retracted into the telescopic channel, and at this time, the telescopic rod 111 is out of contact with the locking block 112. Under the elastic force of the lock block spring 113, the lock block 112 resets and retracts, and disengages from the positioning groove 232. At this time, the lock block 112 is located within the projection range of the telescopic channel along the vertical direction. When the drone 1 flies upward, the lifting seat 11 disengages from the docking channel 231, completing the unlocking process.

[0063] Anti-fall mechanism 2

[0064] The anti-fall mechanism 2 includes an anti-fall seat 24, which is bent at a right angle to match the shape of the angle steel, and there is a right-angled cavity inside the anti-fall seat 24. The anti-fall seat 24 includes a plumb section and a horizontal section to form a right-angle abutment positioning for the clamped angle steel. A pull rod 21 is provided in the plumb section of the anti-fall seat 24, which passes through the anti-fall seat 24 and slides with the anti-fall seat 24, and a guide seat 23 is fixed on the top of the pull rod 21 for docking and locking with the drone 1.

[0065] The pull rod 21 is symmetrically arranged in two groups, and a rotating shaft 27 is arranged between the bottoms of the two pull rods 21. The rotating shaft 27 is rotatably matched with the two pull rods 21, and the rotation axis is arranged in parallel with the angle steel to be clamped. A tension spring 26 is arranged in the vertical section of the anti-fall seat 24. The tension spring 26 is arranged in the vertical direction, and its end is hung on the rotating shaft 27, so as to apply a vertical downward elastic tension to the rotating shaft 27 and the pull rod 21, and the number is preferably two groups. The overall gravity of the anti-fall seat 24 is greater than the maximum elastic tension of the tension spring 26. When the drone 1 drives the anti-fall mechanism 2 to fly upward, the tension spring 26 is in the maximum tension state, and at this time, the extension length of the pull rod 21 outside the anti-fall seat 24 is in the maximum state.

[0066] A sliding seat 25 is horizontally arranged in the horizontal section of the anti-fall seat 24, and an outer sleeve of the sliding seat 25 is provided with an angle steel clamp 244. The angle steel clamp 244 is downwardly extended away from the opening at one end of the pull rod 21 and is provided with a hinged joint. The angle steel clamp 244 is hingedly provided with an angle steel locking tongue 245 through the hinged joint. The angle steel locking tongue 245 is hingedly flipped and matched with the angle steel clamp 244 to clamp the angle steel.

[0067] The bottom of the horizontal section of the anti-fall seat 24 is open, thus forming a U-shaped structure with the opening facing downward, and the opening is used as an escape passage for the action path of the angle steel lock tongue 245. A connecting rod 241 is arranged on the rotation axis 27 of the pull rod 21, and the connecting rod 241 is arranged in a multi-section bent shape.

[0068] In this embodiment, the connecting rod 241 is arranged in a three-section bending shape, and the angle between adjacent bending sections is an obtuse angle. The bending sections on both sides are respectively located in the horizontal section and the vertical section of the anti-fall seat 24, and the bending section in the middle corresponds to the right-angle bending position of the anti-fall seat 24. One end of the connecting rod 241 away from the rotating shaft 27 is hinged with the angle steel clamp 244. When the pull rod 21 is raised or lowered, the anti-fall seat 24 is driven to slide along the slide seat 25 by the connecting rod 241. A guide groove 242 is provided on the surface of the anti-fall seat 24 for the connecting rod 241 to pass through when swinging.

[0069] Taking the hinge point of the angle steel lock tongue 245 as the boundary, one side of the hinge point is the positioning section of the angle steel lock tongue 245, and the other side of the hinge point is the clamping section of the angle steel lock tongue 245, and the clamping section is used to cooperate with the angle steel clamp block 244 to clamp the angle steel. The length of the positioning section of the angle steel lock tongue 245 is less than the length of the clamping section, and a magnetic block 2451 is provided at the opening of the angle steel clamp block 244 away from the side of the angle steel to be clamped. In the non-clamping angle steel state, the magnetic block 2451 cooperates with the positioning section of the angle steel lock tongue 245 by magnetic attraction, so that the positioning section of the angle steel lock tongue 245 rotates into the opening of the angle steel clamp block 244, and under the magnetic attraction, the angle between the angle steel lock tongue 245 and the angle steel clamp block 244 is a right angle or an obtuse angle. When the end of the slide 25 passes through the opening of the angle steel clamp 244, the angle steel lock tongue 245 rotates under the pushing action of the slide 25, and the angle between the angle steel lock tongue 245 and the angle steel clamp 244 is an acute angle. In this embodiment, when the slide 25 is located in the opening of the angle steel clamp 244, the contact surface between the angle steel lock tongue 245 and the slide 25 is in a vertical state, and after the slide 25 passes through the opening of the angle steel clamp 244 and contacts the angle steel lock tongue 245, the contact surface between the angle steel lock tongue 245 and the slide 25 is in a horizontal state.

[0070] During the actual working process, the drone 1 first drives the anti-fall mechanism 2 to rise. At this time, the elongation of the tension spring 26 reaches the maximum, the connecting rod 241 swings upward with the rotating shaft 27, and drives the angle steel clamp 244 to slide in the direction away from the pull rod 21. At this time, the end of the slide seat 25 is located in the opening of the angle steel clamp 244, and the angle between the angle steel lock tongue 245 and the angle steel clamp 244 is a right angle or an obtuse angle. After reaching the set working height, the drone 1 drives the anti-fall mechanism 2 to buckle onto the angle steel from top to bottom, and drives the pull rod 21 downward. Under the action of the tension spring 26, the connecting rod 241 drives the angle steel clamp 244 to slide along the slide 25 toward the pull rod 241 until the end of the slide 25 passes through the opening of the angle steel clamp 244, and the angle steel locking tongue 245 is pushed by the slide 25, so that the angle between it and the angle steel clamp 244 is acute. After the drone 1 drives the anti-fall mechanism 2 to move downward until it is finally unlocked with the anti-fall mechanism 2, under the action of the tension spring 26, the angle steel clamp 244 continues to slide toward the pull rod 21 until the angle steel locking tongue 245 abuts against the angle steel to be clamped, completing the clamping and positioning of the angle steel.

[0071] In order to improve the stability of clamping, the pull rod 21 is connected to the guide seat 23 through the pin seat 22. Two groups of elastic pins 221 that can float elastically up and down in the vertical direction are arranged at the bottom of the pin seat 22. The connecting line between the two elastic pins 221 is arranged parallel to the rotating shaft 27. Two rows of pin holes 2441 are evenly arranged along the length direction on the angle steel clamp block 244, and the two rows of pin holes 2441 are arranged front and back staggered. The anti-fall seat 24 is provided with a guide hole 243 corresponding to the vertical position of the elastic pin 221 for the elastic pin 221 to pass through. After the angle steel is clamped and positioned, the latch seat 22 abuts against the anti-fall seat 24. At this time, the elastic latch 221 passes through the guide hole 243 and is inserted into the elastic latch 221. Since the two rows of latch holes 2441 are staggered front and back, at least one group of elastic latches 221 can be inserted into one group of latch holes 2441 to complete the latch positioning and limit the relative sliding between the angle steel clamp 244 and the slide seat 25.

[0072] Anti-fall rope 3

[0073] The anti-fall rope 3 is directly hung on the bottom of the anti-fall seat 24 through a hook or other locking parts, so that it is transported to the set working height by the drone 1 together with the anti-fall mechanism 2.

[0074] Carrier 4

[0075] The carrier cabin 4 includes a swivel seat 42, which is composed of a rotating end and a non-rotating end. A lower guide cover 422 is provided at the bottom of the non-rotating end of the swivel seat 42. The lower guide cover 422 is a conical structure with the tip arranged downward. Telescopic guide forks 421 are evenly arranged radially along the inner side of the non-rotating end of the swivel seat 42. The telescopic guide forks 421 are preferably arranged in four groups, which can produce telescopic movements along the radial direction of the swivel seat 42. The telescopic guide forks 421 are completely retracted into the inside of the swivel seat 42 in the non-working state. When the position of the carrier cabin 4 needs to be positioned, the telescopic guide forks 421 are extended, and two groups of telescopic guide forks 421 are clamped and positioned with the tower body of the angle steel tower, thereby limiting the rotation and shaking of the non-rotating end of the carrier cabin 4.

[0076] Two sets of swing rods 44 are symmetrically arranged on the rotating end of the swivel seat 42, and the hinge axis of the swing rods 44 is arranged horizontally. A set of split cabins are arranged on each of the two swing rods 44, and the split cabins on the two swing rods 44 are closed to form a columnar cabin body, and the limit ring 5 is arranged inside the cabin body.

[0077] A group of split guide covers are also provided on the top of the two groups of split cabins of the carrier cabin 4. When the cabins are closed, the two groups of split guide covers are also closed to form an upper guide cover 41. The upper guide cover 41 and the lower guide cover 422 are arranged symmetrically up and down. When the swing rod 44 is driven by a motor or a gear to rotate, it drives the cabin to open and close from top to bottom, and after unfolding, the limit ring 5 in the cabin is exposed. A group of power sources can be added to the split guide covers to open the upper guide cover 41 separately, so that the upper guide cover 41 can have an independent opening and closing action.

[0078] A rope climbing seat 43 is also fixed in the cabin of the carrier cabin 4. The rope climbing seat 43 uses an existing rope climbing mechanism, and can climb along the anti-fall rope by friction climbing rope or inchworm climbing mechanism. The structure is not repeated. The anti-fall rope 3 passes through the upper guide cover 41, the rope climbing seat 43 and the lower guide cover 422 in sequence along the axial direction of the carrier cabin 4.

[0079] During operation, first pass the anti-fall rope through the upper guide cover 41, the limiting ring 5, the climbing rope seat 43 and the lower guide cover 422 on the ground, and drive the carrier cabin 4 to climb along the anti-fall rope 3 through the climbing rope seat 43. During the climbing process, when encountering the foot nails, the conical surface of the upper guide cover 41 slides through the foot nails alternately. After climbing to the set height, extend the telescopic guide fork 421 to clamp and position the angle steel tower. Then rotate the swivel seat to make the limiting ring 5 correspond to the foot nail position on the angle steel tower. Open the upper guide cover 41 and the cabin body, so that the clamping seat 54 of the limiting ring 5 is clamped and fixed on the foot nail. At this time, the limiting ring 5 is separated from the carrier cabin 4. After the carrier cabin 4 moves down, close the cabin body and the upper guide cover 41, and return to the ground to complete the installation of the limiting ring 5.

[0080] Limiting ring 5

[0081] The limit ring 5 includes a connecting rod 51 arranged in the vertical direction, and an upper limit ring 52 and a lower limit ring 53 arranged coaxially are fixed on the connecting rod 51. The upper limit ring 52 and the lower limit ring 53 are both provided with notches for the rope to pass through, and the notches are in opposite directions. Through the two sets of notches, the anti-fall rope 3 can be smoothly placed in the limit ring when on the ground, and the opposite notches can prevent the anti-fall rope 3 from escaping from the limit ring 5.

[0082] The connecting rod 51 is also provided with a clamping seat 54 for clamping the foot spike, and the clamping seat 54 is vertically arranged with the upper limit ring 52 and the lower limit ring 53. The clamping seat 54 clamps and fixes the foot spike by opening and closing.

[0083] The basic principles of the present application are described above in conjunction with specific embodiments. However, it should be noted that the advantages, strengths, effects, etc. mentioned in the present application are only examples and not limitations, and it cannot be considered that these advantages, strengths, effects, etc. are required by each embodiment of the present application. In addition, the specific details disclosed above are only for the purpose of illustration and ease of understanding, not for limitation, and the above details do not limit the present application to being implemented by adopting the above specific details.

[0084] The block diagrams of the devices, apparatuses, equipment, and systems involved in this application are only illustrative examples and are not intended to require or imply that they must be connected, arranged, and configured in the manner shown in the block diagram. As will be appreciated by those skilled in the art, these devices, apparatuses, equipment, and systems can be connected, arranged, and configured in any manner. Words such as "including", "comprising", "having", etc. are open words, referring to "including but not limited to", and can be used interchangeably with them. The words "or" and "and" used here refer to the words "and / or" and can be used interchangeably with them, unless the context clearly indicates otherwise. The words "such as" used here refer to the phrase "such as but not limited to", and can be used interchangeably with them.

Claims

1. A method for installing a tower operation anti-fall rope, characterized in that: The method comprises the following steps: S1. Fix the anti-fall rope (3) on the anti-fall mechanism (2), and lock the drone (1) and the anti-fall mechanism (2); S2, driving the anti-fall mechanism (2) to fly to a set height by the drone (1), releasing the anti-fall mechanism (2) onto the angle steel of the angle steel tower, and locking the anti-fall mechanism (2) onto the angle steel; S3, unlocking the drone (1) and the anti-fall mechanism (2), and recovering the drone (1); S4. Fix the limiting ring (5) in the carrying cabin (4) so ​​that the anti-fall rope (3) passes through the limiting ring (5); S5, start the carrying cabin (4) to make it climb upward along the anti-fall rope (3), after climbing to the set height, open the carrying cabin (4) and release the limiting ring (5), so that the limiting ring (5) is connected and fixed with the foot nails on the angle steel tower; S6, close the carrying cabin (4) and allow the person to climb down along the anti-fall rope (3), and then retract the carrying cabin (4) to complete the installation.

2. A tower operation anti-falling rope installation method according to claim 1, characterized in that: The anti-fall mechanism (2) comprises an anti-fall seat (24) in a right-angled shape, wherein the anti-fall seat (24) and the angle steel are in right-angled contact positioning; a sliding seat (25) and an angle steel clamping block (244) sleeved on the outer ring of the sliding seat (25) are arranged in the horizontal direction inside the anti-fall seat (24); a linear power source drives the angle steel clamping block (244) to slide along the sliding seat (25); an angle steel locking tongue (245) is hingedly arranged at the bottom of the opening of the angle steel clamping block (244) away from the side of the angle steel to be clamped, The hinge axis is arranged in parallel with the angle steel to be clamped; the positioning section of the angle steel locking tongue (245) is located within the projection range of the opening of the angle steel clamp block (244) along the length direction of the angle steel clamp block (244); the sliding seat (25) abuts against the positioning section of the angle steel clamp block (244) after passing through the opening of the angle steel clamp block (244) to drive the angle steel clamp block (244) to generate a flipping action around the hinge axis; and the bottom of the horizontal section of the anti-fall seat (24) is provided with an opening for the angle steel clamp block (244) to pass through.

3. A tower operation anti-falling rope installation method according to claim 2, characterized in that: A magnetic attraction block (2451) is arranged in an opening of the angle steel clamping block (244) away from one side of the angle steel to be clamped. When the slide seat (25) is located in the opening cavity of the angle steel clamping block (244), the positioning section of the angle steel locking tongue (245) is magnetically attracted by the magnetic attraction block (2451) and enters the opening cavity of the angle steel clamping block (244), so that the angle between the angle steel locking tongue (245) and the angle steel clamping block (244) is not less than ninety degrees; after the slide seat (25) passes through the opening of the angle steel clamping block (244) and pushes the angle steel locking tongue (245) to turn over, the angle between the angle steel locking tongue (245) and the angle steel clamping block (244) is less than ninety degrees.

4. A tower operation anti-falling rope installation method according to claim 2, characterized in that: The linear power source comprises a pull rod (21) vertically slidably arranged in the vertical section of the anti-fall seat (24), the pull rod (21) is pulled by the lifting mechanism to generate a vertical lifting action, a bent connecting rod (241) is arranged in the anti-fall seat (24), one end of the connecting rod (241) is hingedly matched with the angle steel clamp (244), and the other end of the connecting rod (241) is hingedly matched with the pull rod (21), and each hinge axis is parallel to the hinge axis of the angle steel lock tongue (245); while the pull rod (21) moves vertically, the angle steel clamp (244) is driven to slide along the slide seat (25) through the connecting rod (241).

5. A tower operation anti-falling rope installation method according to claim 4, characterized in that: The lifting mechanism comprises a tension spring (26) applying a downward pulling force to a pull rod (21) in a vertical direction within a vertical section, and a drone (1) applying a vertical upward pulling force to the pull rod (21), wherein the gravity of the anti-fall mechanism (2) is greater than the elastic force of the tension spring (26); a latch seat (22) located above the anti-fall seat (24) is arranged on the pull rod (21), and at least two groups of elastic latches (221) are arranged at intervals along the axial direction of a parallel angle steel clamp block (244) at the bottom of the latch seat (22), and the elastic latches (221) are arranged at an angle of 100° to 100°. (221) can float in the vertical direction; a guide hole (243) corresponding to the vertical position of the elastic plug pin (221) is opened on the anti-fall seat (24) for the elastic plug pin (221) to pass through; at least two rows of plug holes (2441) are evenly arranged along the length direction on the angle steel clamp block (244) so ​​as to correspond to the position of each elastic plug pin (221), and the adjacent two rows of plug holes (2441) are staggered in front and back, and the diameter of the elastic plug pin (221) is smaller than the diameter of the plug hole (2441).

6. A tower operation anti-falling rope installation method according to any one of claims 1 to 5, characterized in that: The anti-fall mechanism (2) also includes a guide seat (23) for connecting to the unmanned aerial vehicle (1), a docking channel (231) is provided on the guide seat (23) along the vertical direction, and a lifting seat (11) is provided on the unmanned aerial vehicle (1) and is plugged and matched with the docking channel (231) along the vertical direction. After the lifting seat (11) is inserted into the docking channel (231), it is locked or unlocked by a locking mechanism; the locking mechanism includes a positioning groove (232) provided in the docking channel (231) along the vertical direction, a telescopic channel is provided in the lifting seat (11) along the vertical direction, and a telescopic rod (111) is arranged in the telescopic channel along the vertical direction, and the opening of the telescopic channel is A locking block (112) is also hingedly provided, the hinge axis is arranged horizontally, a locking block spring (113) is arranged radially in the telescopic channel, and the two ends of the locking block spring (113) respectively abut against the inner wall of the telescopic channel and the locking block (112), thereby applying an elastic force toward the axial direction of the telescopic channel to the locking block (112); the vertical telescopic trajectory of the telescopic rod (111) and the position of the locking block (112) intersect, and after the telescopic rod (111) is telescoped and exerts a radial pushing action on the locking block (112), the locking block (112) enters the positioning groove (232) of the docking channel (231) to abut against the limit position, thereby generating a locking action on the lifting seat (11).

7. A tower operation anti-falling rope installation method according to any one of claims 1 to 5, characterized in that: The transport cabin (4) comprises a cabin body capable of opening and closing and a swivel seat (42) for driving the cabin body to rotate. The swivel seat (42) has a swivel axis arranged in a vertical direction. An upper guide cover (41) and a lower guide cover (422) are respectively arranged on the cabin body top of the transport cabin (4) and the swivel seat (42) bottom. The upper guide cover (41) is in a conical structure with the tip pointing upward, and the lower guide cover (422) is in a conical structure with the tip pointing downward. A climbing rope seat (43) for climbing an anti-fall rope (3) is fixed on the swivel seat (42). The anti-fall rope (3) passes through the upper guide cover (41), the climbing rope seat (43) and the lower guide cover (422) in sequence along the axial direction of the transport cabin (4).

8. A tower operation anti-falling rope installation method according to claim 7, characterized in that: The cabin body of the carrier cabin (4) is arranged in a split type and is arranged symmetrically along the vertical direction. Two groups of swing rods (44) are arranged on the rotating end of the rotating seat (42) and are hinged to the rotating seat (42). The two swing rods (44) are respectively hinged to the two sections of the cabin body of the carrier cabin (4). The hinge axis is arranged parallel to the rotating axis of the rotating seat (42). When the two swing rods (44) rotate, they drive the two sections of the cabin body of the carrier cabin (4) to produce an opening and closing action; the upper guide cover (41) is arranged in a split type and symmetrically, so as to correspond to the two sections of the cabin body of the carrier cabin (4). The two sections of the cover body of the upper guide cover (41) are hinged to the carrier cabin (4). The hinge axis is arranged parallel to the hinge axis of the swing rod (44). The upper guide cover (41) is driven by a power source to produce an opening and closing action.

9. A tower operation anti-falling rope installation method according to claim 8, characterized in that: A lower guide cover (422) is arranged below the swivel seat (42), and the lower guide cover (422) is in a conical structure with the tip facing downward; the swivel seat (42) comprises a rotating end for fixing the cabin body and a non-rotating end coaxially rotatably matched with the rotating end, and the non-rotating end of the swivel seat (42) is evenly arranged with telescopic guide forks (421) extending from the inside of the swivel seat (42) to the outside along the radial direction, and two adjacent telescopic guide forks (421) clamp the angle steel of the angle steel tower to limit the rotation of the carrier cabin (4).

10. A tower operation anti-falling rope installation method according to claim 7, characterized in that: The limiting ring (5) comprises a connecting rod (51) arranged in a vertical direction, an upper limiting ring (52) and a lower limiting ring (53) arranged coaxially are fixed on the connecting rod (51), the upper limiting ring (52) and the lower limiting ring (53) are both provided with notches for the rope to pass through, and the directions of the notches are opposite to each other, and a clamping seat (54) for clamping a foot nail is also provided on the connecting rod (51), and the clamping seat (54) and the upper limiting ring (52) and the lower limiting ring (53) are arranged in a positional manner in the vertical direction.

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