Power transmission line spacer unmanned aerial vehicle installation control method and system

Abstract

The invention relates to the technical field of spacer installation, in particular to a power transmission line spacer unmanned aerial vehicle installation control method and system, which comprises an unmanned aerial vehicle installation base, a satellite positioning module, a sensor module, a controller, a spacer and an installation assembly, and is characterized in that the satellite positioning module, the sensor module and the controller are arranged on the unmanned aerial vehicle installation base; the mounting assembly comprises a hanging ring, a storage bin, a plurality of clamping claws and an overturning unit, the hanging ring is adjusted to hook the spacer, the position of the power transmission line is accurately positioned by means of the satellite positioning module, then the environment of the surrounding and the power transmission line is monitored through the sensor module, and finally the unmanned aerial vehicle is controlled to run through the controller. And then moving to a power transmission line for installation. After the installation is completed, the spacer is continuously hooked by the hanging ring; therefore, frequent return voyage for supplementing the spacer is not needed, and the spacer installation efficiency is remarkably improved.

Description

Technical Field

[0001] The present invention relates to the technical field of spacer installation, and in particular to a transmission line spacer drone installation control method and system. Background Art

[0002] At present, under the action of wind, breeze vibration of transmission lines occurs frequently, resulting in fatigue breakage of wires and damage to hardware and tower components, and limiting the service stress value of the conductors; therefore, multiple sub-conductors are generally used in parallel to transmit power. In order to prevent the sub-conductors from adhering to each other, multiple spacers need to be installed in each gear. The use of spacers can ensure that the phase line spacing of the sub-conductors remains unchanged to meet the electrical performance, reduce the surface potential gradient, and in the case of a short circuit, no electromagnetic force is generated between the wire bundles, resulting in mutual attraction and collision, and also play a certain inhibitory role on the solitary swing and breeze vibration of the sub-span.

[0003] However, in the aforementioned prior art, in order to improve the installation safety of the spacer bars, drones are usually used to lift the spacer bars, thereby replacing manual operations. However, the drone can only lift one spacer bar at a time, and each time the installation is completed, it needs to return to the base for reassembly, resulting in very low efficiency in the installation of spacer bars for transmission lines. Summary of the Invention

[0004] The purpose of the present invention is to provide a method and system for controlling the installation of transmission line spacer rods by drones, so as to solve the problem that in the prior art, in order to improve the installation safety of spacer rods, drones are usually used to lift spacer rods, thereby replacing manual operation. However, drones can only lift one spacer rod at a time, and each time the installation is completed, the drone needs to return and be reassembled, resulting in a very low installation efficiency of transmission line spacer rods.

[0005] To achieve the above-mentioned object, the present invention provides a transmission line spacer UAV installation control system, comprising a UAV mounting base, a satellite positioning module, a sensor module, a controller, a spacer, and an installation assembly, wherein the satellite positioning module, the sensor module, and the controller are all disposed on the UAV mounting base, and the spacer is disposed below the UAV mounting base; The mounting assembly includes a hanging ring, a storage bin, a plurality of clamping claws and a flip unit. The hanging ring is arranged below the drone mounting base, the spacer rod is arranged on the hanging ring, the storage bin is arranged on one side of the drone mounting base, and a plurality of the spacer rods are stored in the storage bin. The flip unit is arranged below the storage bin, and a plurality of the clamping claws are arranged on the flip unit.

[0006] Wherein, the mounting assembly further includes a winding unit, and the winding unit is arranged on the drone mounting base; The winding unit includes a winding shaft, a rotating component, a connecting rope and a transverse moving component. The transverse moving component is arranged below the drone mounting base. The output end of the transverse moving component is fixedly connected to the winding shaft. The rotating component is arranged on the winding shaft. One end of the connecting rope is sleeved on the winding shaft, and the other end of the connecting shaft is fixedly connected to the hanging ring.

[0007] Wherein, the installation assembly further includes a storage unit, and the storage unit is arranged inside the storage bin; The storage unit includes two slides, two first electromagnets, two supporting mechanisms, multiple end protection sleeves, multiple metal sliders, two end protection sleeve transfer mechanisms and multiple second electromagnets. The two slides are symmetrically arranged inside the storage bin, the two first electromagnets are respectively arranged inside the corresponding slides, the two supporting mechanisms are respectively arranged below the corresponding slides, the multiple end protection sleeves are respectively sleeved on the two ends of the corresponding spacer rods, the multiple metal sliders are respectively arranged on one side of the corresponding end protection sleeves, the metal sliders are slidably connected to the slides, the two end protection sleeve transfer mechanisms are symmetrically arranged inside the storage bin, and the multiple second electromagnets are respectively arranged on one side of the corresponding slides.

[0008] In which, the flip unit includes a first flip component, a first flip plate, a second flip component, a second flip plate, two first flip locking mechanisms and two second flip locking mechanisms, the first flip component is arranged below the storage bin, the output end of the first flip component is provided with the first flip plate, the second flip component is arranged at one end of the first flip plate, the output end of the second flip component is provided with the second flip plate, two first flip locking mechanisms are arranged below the storage bin, and two second flip locking mechanisms are symmetrically arranged on both sides of the second flip component.

[0009] The first flip locking mechanism includes a first telescopic component and a first locking block. The first telescopic component is arranged below the storage bin. The output end of the first telescopic component is fixedly connected to the first locking block. The first flip plate has a first slot, and the first slot and the first locking block are adapted to each other. The second flip locking mechanism includes a second telescopic component and a second locking block. The second telescopic component is arranged on the first flip plate and is located on one side of the second flip component. The output end of the second telescopic component is fixedly connected to the second locking block. The first flip plate has a second card slot, and the second card slot and the second locking block are adapted to each other.

[0010] The abutting mechanism includes two abutting components and two abutting plates. The two abutting components are symmetrically arranged below the chute. The output ends of the two abutting components are fixedly connected to the corresponding abutting plates respectively. The abutting plates are adapted to the bottom of the chute. The end protective cover transfer mechanism includes a lifting screw machine, two protective cover moving parts, a protective cover support plate, a third electromagnet telescopic part and a third electromagnet. The lifting screw machine is arranged on the inner wall of the storage bin, and the output end of the lifting screw machine is fixedly connected to the two protective cover moving parts, and the output end of the protective cover moving part is fixedly connected to the protective cover support plate. The end protective cover is placed on the protective cover support plate. The third electromagnet telescopic part is arranged inside the storage bin and is located between the two protective cover moving parts. The output end of the third electromagnet telescopic part is fixedly connected to the third electromagnet, and the third electromagnet and the metal slider attract each other.

[0011] Wherein, the mounting assembly further comprises two clamping units, and the two clamping units are sequentially arranged on the second flip plate; The clamping unit includes a placement seat, a cushion and two clamping components. The placement seat is arranged on one side of the second flip plate, the cushion is arranged on one side of the placement seat, the spacer rod is placed above the cushion, and the two clamping components are symmetrically arranged on the placement seat. The output ends of the two clamping components are respectively fixedly connected to the corresponding clamping claws.

[0012] The spacer bar comprises a spacer bar body, two mounting heads, two hooks and two bayonet mechanisms, wherein the two mounting heads are symmetrically arranged at both ends of the spacer bar body, the two hooks are respectively arranged on one side of the corresponding mounting heads, and the two bayonet mechanisms are respectively arranged on the other side of the corresponding mounting heads; The latch mechanism includes a telescopic motor, a socket, a geared clamping wheel and a clamping block. The telescopic motor is arranged inside the mounting head, and the socket is provided at the output end of the telescopic motor. The geared clamping wheel is arranged on one side of the socket. The clamping block is arranged inside the mounting head and is adapted to the geared clamping wheel.

[0013] The present invention also provides a transmission line spacer UAV installation control method, which uses the transmission line spacer UAV installation control system described above and includes the following steps: By fixing the drone mounting base under the drone and installing the storage bin on the drone mounting base; Placing a plurality of the spacer rods inside the storage bin; The clamping claws clamp the spacer rods in the storage bin; Relying on the flip unit to flip and adjust the clamped spacer rod so that it is aligned with the hanging ring; The hanging ring is adjusted to hook the spacer bar and then moved to the power transmission line for installation; After the installation is completed, continue to use the hanging ring to hook the spacer rod, thereby repeating the operation without frequent return.

[0014] The present invention provides a transmission line spacer drone installation control method and system, which comprises the following steps: fixing the drone installation base under the drone and installing the storage bin on the drone installation base; placing a plurality of the spacer bars inside the storage bin; the clamping claw clamping the spacer bars in the storage bin; relying on the flip unit to flip and adjust the clamped spacer bars so that they are aligned with the hanging ring; the hanging ring is adjusted to hook the spacer bars, at which time the position of the transmission line is accurately located by relying on the satellite positioning module, and then monitoring the surrounding environment and the transmission line environment through the sensor module, and finally controlling the operation of the drone through the controller, and then moving to the transmission line for installation; after the installation is completed, continuing to use the hanging ring to hook the spacer bars; through the above-mentioned structural setting, a plurality of the spacer bars are placed inside the storage bin, and the spacer bars can be automatically installed on the hanging ring by using the cooperation of the clamping claw and the flip unit, so that there is no need to frequently return to replenish the spacer bars, thereby significantly improving the spacer bar installation efficiency. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the following briefly introduces the drawings required for use in the embodiments or the description of the prior art.

[0016] Figure 1 It is a structural schematic diagram of the transmission line spacer UAV installation control system of the present invention.

[0017] Figure 2 It is a cross-sectional view of the transmission line spacer UAV installation control system of the present invention.

[0018] Figure 3 The present invention Figure 2 AA line section view.

[0019] Figure 4 The present invention Figure 1 A magnified view of the local structure at point B.

[0020] Figure 5 The present invention Figure 2 A magnified view of the local structure at point C.

[0021] Figure 6 It is a diagram of the internal structure of the storage bin of the present invention.

[0022] Figure 7 It is a structural schematic diagram of the mounting head of the present invention.

[0023] Figure 8 It is a structural schematic diagram of the bayonet mechanism of the present invention.

[0024] Figure 9 It is a structural schematic diagram of the winding unit of the present invention.

[0025] Figure 10 The present invention is a flowchart of the steps of the transmission line spacer drone installation control method.

[0026] 1-UAV mounting base, 2-satellite positioning module, 3-sensor module, 4-controller, 5-spacer, 6-storage bin, 7-clamping claw, 8-reeling shaft, 9-rotating component, 10-connecting rope, 11-transverse component, 12-slide, 13-first electromagnet, 14-end protection sleeve, 15-metal slider, 16-second electromagnet, 17-first flip component, 18-first flip plate, 19-second flip component, 20-second flip plate, 21-first telescopic component, 22-first locking block, 2 3-first slot, 24-second telescopic component, 25-second locking block, 26-second slot, 27-holding component, 28-holding plate, 29-lifting screw machine, 30-protective cover moving component, 31-protective cover support plate, 32-third electromagnet telescopic component, 33-third electromagnet, 34-placement seat, 35-cushion, 36-clamping component, 37-spacer rod body, 38-mounting head, 39-hook, 40-telescopic motor, 41-seat, 42-toothed card wheel, 43-block, 44-hanging ring. DETAILED DESCRIPTION

[0027] The embodiments of the present invention are described in detail below. Examples of the embodiments are shown in the accompanying drawings. The embodiments described below with reference to the accompanying drawings are exemplary and are intended to be used to explain the present invention, but should not be understood as limiting the present invention.

[0028] See also Figures 1 to 9The present invention provides a transmission line spacer UAV installation control system, including a UAV installation base 1, a satellite positioning module 2, a sensor module 3, a controller 4, a spacer 5 and an installation assembly, the installation assembly includes a hanging ring 44, a storage bin 6, a plurality of clamping claws 7 and a flip unit, the installation assembly also includes a winding unit, the winding unit includes a winding shaft 8, a rotating component 9, a connecting rope 10 and a transverse component 11, the installation assembly also includes a storage unit, the storage unit includes two slide grooves 12, two first electromagnets 13, two abutting mechanisms, a plurality of end protection sleeves 14, a plurality of metal sliders 15, two end protection sleeve 14 transfer mechanisms and a plurality of second electromagnets 16, the flip unit includes a first flip component 17, a first flip plate 18, a second flip component 19, a second flip plate 20, two A first flip locking mechanism and two second flip locking mechanisms, the first flip locking mechanism includes a first telescopic part 21 and a first locking block 22, the second flip locking mechanism includes a second telescopic part 24 and a second locking block 25, the abutting mechanism includes two abutting parts 27 and two abutting plates 28, the end protective cover 14 transfer mechanism includes a lifting screw machine 29, two protective cover moving parts 30, a protective cover support plate 31, a third electromagnet telescopic part 32 and a third electromagnet 33, the installation assembly also includes two clamping units, the clamping unit includes a placement seat 34, a cushion 35 and two clamping parts 36, the spacer rod 5 includes a spacer rod 5 body 37, two mounting heads 38, two hooks 39 and two pin mechanisms, the pin mechanism includes a telescopic motor, a clamping seat, a geared clamping wheel and a clamping block.

[0029] Among them, the satellite positioning module 2, the sensor module 3 and the controller 4 are all arranged on the drone mounting base 1, the spacer rod 5 is arranged below the drone mounting base 1, the hanging ring 44 is arranged below the drone mounting base 1, the spacer rod 5 is arranged on the hanging ring 44, the storage bin 6 is arranged on one side of the drone mounting base 1, and a plurality of the spacer rods 5 are stored in the storage bin 6. The flip unit is arranged below the storage bin 6, and a plurality of the clamping claws 7 are arranged on the flip unit. The UAV mounting base 1 is fixed under the UAV, and the storage bin 6 is installed on the UAV mounting base 1; a plurality of the spacer bars 5 are placed inside the storage bin 6; the clamping claws 7 clamp the spacer bars 5 in the storage bin 6; the clamped spacer bars 5 are flipped and adjusted by the flip unit to align with the hanging ring 44; the hanging ring 44 is adjusted to hook the spacer bars 5, and at this time, the position of the power transmission line is accurately located by the satellite positioning module 2, and then the environment of the surroundings and the power transmission line is monitored by the sensor module 3, and finally the UAV is controlled to operate by the controller 4, and then moved to the power transmission line for installation; after the installation is completed, the hanging ring 44 is continued to be used to hook the spacer bars 5.

[0030] Secondly, the winding unit is arranged on the drone mounting base 1; the transverse moving component 11 is arranged below the drone mounting base 1, the output end of the transverse moving component 11 is fixedly connected to the winding shaft 8, the rotating component 9 is arranged on the winding shaft 8, one end of the connecting rope 10 is sleeved on the winding shaft 8, and the other end of the connecting shaft is fixedly connected to the hanging ring 44. The rotating component 9 is a self-locking motor. When the rotating component 9 is started, it drives the winding shaft 8 to rotate, thereby allowing the connecting rope 10 to be unwound and reeled on the winding shaft 8, thereby adjusting the height of the hanging ring 44. At the same time, the transverse moving component 11 is an electric slide rail. When the transverse moving component 11 is started, it drives the hanging ring 44 to approach the spacer 5, thereby allowing the spacer 5 to be hooked by the hanging ring 44 for subsequent installation.

[0031] At the same time, the storage unit is arranged inside the storage bin 6; the two slide grooves 12 are symmetrically arranged inside the storage bin 6, the two first electromagnets 13 are respectively arranged inside the corresponding slide grooves 12, the two supporting mechanisms are respectively arranged below the corresponding slide grooves 12, and the multiple end protection sleeves 14 are respectively sleeved on the two ends of the corresponding spacer rods 5, and the multiple metal sliders 15 are respectively arranged on one side of the corresponding end protection sleeves 14, and the metal sliders 15 are slidingly connected to the slide groove 12. The two end protection sleeves 14 transfer mechanisms are symmetrically arranged inside the storage bin 6, and the multiple second electromagnets 16 are respectively arranged on one side of the corresponding slide groove 12. When the spacer bar 5 is stored inside the storage bin 6, the first electromagnet 13 is started and attracts the metal slider 15 to fix the end protection sleeve 14 and the spacer bar 5 to prevent them from sliding downward. At the same time, the end protection sleeve 14 supports and protects the spacer bar 5. When the spacer bar 5 needs to fall for clamping, the holding mechanism is opened and the first electromagnet 13 is powered off. The metal slider 15 slides down in the chute 12, and the lowest spacer bar 5 falls to one side of the clamping claw 7 and is then fixed by the clamping claw 7. At the same time, the other metal sliders 15 above the clamping claw 7 are held in place by the end protection sleeve 14. 4 are mutually supported, and thus still located inside the slide groove 12, at this time the supporting mechanism closes the slide groove 12, thereby the spacer bar 5 clamped below can be flipped and installed, and after completion the above-mentioned spacer bar 5 sliding operation is repeated; in addition, after the spacer bar 5 is located on one side of the clamping claw 7, it is necessary to rely on the end protection sleeve 14 transfer mechanism and the third electromagnet to remove the end protection sleeve 14 so as to expose all the spacer bars 5 for installation; in addition, after the end protection sleeve 14 is removed, it is moved up by relying on the lifting screw machine, and then the third electromagnet is energized to magnetically fix the metal slider and the end protection sleeve after moving up.

[0032] In addition, the first flip component 17 is arranged below the storage bin 6, the output end of the first flip component 17 is provided with the first flip plate 18, the second flip component 19 is provided at one end of the first flip plate 18, and the output end of the second flip component 19 is provided with the second flip plate 20. The first flip locking mechanism is arranged below the storage bin 6, and two second flip locking mechanisms are symmetrically arranged on both sides of the second flip component 19. The first flip component 17 and the second flip component 19 are both self-locking motors. First, the first flip component 17 is started to drive the first flip plate 18 to flip downward and away from the storage bin 6. Then, the second flip component 19 is started to drive the second flip plate 20 to rotate so that the spacer bar 5 faces the hanging ring 44 for installation. At the same time, after the first flip and the second flip are reset close to the storage bin 6, the first flip locking mechanism and the second flip locking mechanism can respectively perform a limit reinforcement operation.

[0033] Then, the first telescopic component 21 is arranged below the storage bin 6, the output end of the first telescopic component 21 is fixedly connected to the first locking block 22, the first flip plate 18 has a first card slot 23, and the first card slot 23 and the first locking block 22 are adapted to each other; the second telescopic component 24 is arranged on the first flip plate 18 and is located on one side of the second flip component 19, the output end of the second telescopic component 24 is fixedly connected to the second locking block 25, the first flip plate 18 has a second card slot 26, and the second card slot 26 and the second locking block 25 are adapted to each other. The first telescopic component 21 is a self-locking electric push rod. When the first telescopic component 21 is started, it drives the first locking block 22 to move and enter the first slot 23, thereby limiting the rotation operation of the first flip plate 18, improving stability, and avoiding shaking and breakage when supporting the spacer bar 5 above; the second telescopic component 24 is a self-locking electric push rod. When the second telescopic component 24 is started, it drives the second locking block 25 to move and enter the second slot 26, thereby limiting the rotation of the second flip plate 20, so that it can more stably support the spacer bar 5 above and avoid accidental rotation.

[0034] Again, the two abutting parts 27 are symmetrically arranged below the slide 12, and the output ends of the two abutting parts 27 are fixedly connected to the corresponding abutting plates 28, and the abutting plates 28 are adapted to the bottom of the slide 12; the lifting screw machine 29 is arranged on the inner wall of the storage bin 6, and the output end of the lifting screw machine 29 is fixedly connected to the two protective cover moving parts 30, and the output end of the protective cover moving part 30 is fixedly connected to the protective cover support plate 31, and the end protective cover 14 is placed on the protective cover support plate 31, and the third electromagnet telescopic part 32 is arranged inside the storage bin 6 and is located between the two protective cover moving parts 30, and the output end of the third electromagnet telescopic part 32 is fixedly connected to the third electromagnet 33, and the third electromagnet 33 and the metal slider 15 attract each other. The abutting component 27 is a self-locking electric push rod. When the abutting component 27 is started, it drives the abutting plate 28 to move, thereby sealing and closing the bottom of the slide groove 12 to prevent the metal slider 15 from continuing to slide down, thereby limiting the other spacer bars 5 stored on the clamping claw 7 and preventing them from falling; when the spacer bars 5 and the end protective sleeves 14 fall, they first fall on the soft pad 35. At this time, the protective sleeve support plate 31 does not contact the end protective sleeve 14; then, after the first flip plate 18 is rotated downward by a certain angle, the end protective sleeves 14 of the upper and lower spacer bars 5 are separated to reduce friction so that the end protective sleeves 14 can be removed later The end protective cover 14, after the two spacer bars 5 are separated, the lower end protective cover 14 contacts the end support plate due to the downward movement of the first flip plate 18, and the third electromagnet telescopic component 32 can be started at this time to drive the third electromagnet 33 to move, and then power is turned on to adsorb the metal slider 15, and at the same time cooperate with the support of the protective cover support plate 31, and then the protective cover moving component 30 is started to shrink, and then the end protective covers 14 at both ends of the spacer bar 5 are removed at the same time. At this time, the spacer bar 5 falls again on top of the soft pad 35, and is then clamped and fixed by the clamping claw 7, and then flipped and moved to the hanging ring 44 for installation and use.

[0035] Furthermore, the two clamping units are sequentially mounted on the second flip plate 20; the mounting seat 34 is mounted on one side of the second flip plate 20, and the soft pad 35 is mounted on one side of the mounting seat 34. The spacer bar 5 is positioned above the soft pad 35. Two clamping components 36 are symmetrically mounted on the mounting seat 34, with the output ends of the two clamping components 36 fixedly connected to the corresponding clamping claws 7. The mounting seat 34 supports the soft pads 35 and provides a certain height to allow the soft pads 35 to contact the spacer bar 5. The clamping components 36 are self-locking electric push rods. When the clamping components 36 are activated, they drive the clamping claws 7 to move, thereby clamping and securing the spacer bar 5.

[0036] Finally, the two mounting heads 38 are symmetrically arranged at both ends of the main body 37 of the spacer rod 5, the two hooks 39 are respectively arranged on one side of the corresponding mounting head 38, and the two latch mechanisms are respectively arranged on the other side of the corresponding mounting head 38; the telescopic motor 40 is arranged inside the mounting head 38, and the output end of the telescopic motor 40 is provided with the card seat 41, the geared card wheel 42 is arranged on one side of the card seat 41, and the card block 43 is arranged inside the mounting head 38 and is adapted to the geared card wheel 42. The two mounting heads 38 can be used to be installed on the power transmission line and support the main body 37 of the spacer bar 5 in the middle. When the main body 37 of the spacer bar 5 is adjusted, the hook 39 is located on one side of the hanging ring 44, and then the hanging ring 44 is moved horizontally and lifted to adapt to the hook 39. At this time, the mounting head 38 is moved to the power transmission line, and the power transmission line is fixed to the mounting head 38 by the pin mechanism, thereby realizing the installation of the spacer bar 5; when fixing the power transmission line: the mounting head 38 is adjusted so that the power transmission line is located inside the clamping seat 41. At this time, the telescopic motor 40 is started to drive the clamping seat 41 to move and resist, thereby fixing the power transmission line. At the same time, when the clamping seat 41 moves, it drives the geared clamping wheel 42 to rotate continuously. At the same time, a torsion spring is provided on the clamping block 43, and then the geared clamping wheel 42 is limited by the clamping block 43, so that it cannot rotate in the opposite direction, thereby avoiding loosening. At this time, the hanging ring 44 can be separated from the hook 39 and the next group of spacer bars 5 can be installed.

[0037] When using a transmission line spacer drone installation control system of this embodiment, the drone installation base 1 is fixed under the drone, and the storage bin 6 is installed on the drone installation base 1; a plurality of the spacer bars 5 are placed inside the storage bin 6; the clamping claws 7 clamp the spacer bars 5 in the storage bin 6; the clamped spacer bars 5 are flipped and adjusted by the flip unit to align with the hanging ring 44; the hanging ring 44 is adjusted to hook the spacer bars 5, and at this time, the position of the transmission line is accurately located by the satellite positioning module 2, and then the environment of the surroundings and the transmission line is monitored by the sensor module 3, and finally the drone is controlled to operate by the controller 4, and then moved to the transmission line for installation; after the installation is completed, the hanging ring 44 is continued to be used to hook the spacer bars 5; Through the above-mentioned structural setting, a plurality of the spacer bars 5 are placed inside the storage bin 6, and the clamping claws 7 and the flipping unit can be used to cooperate to automatically install the spacer bars 5 on the hanging ring 44, thereby eliminating the need to frequently return to replenish the spacer bars 5, thereby significantly improving the installation efficiency of the spacer bars 5.

[0038] See also Figure 10 The present invention also provides a transmission line spacer 5 UAV installation control method, comprising the following steps: S1: Fixing the drone mounting base 1 under the drone and installing the storage bin 6 on the drone mounting base 1; S2: placing a plurality of the spacer rods 5 inside the storage bin 6; S3: The clamping claw 7 clamps the spacer rod 5 in the storage bin 6; S4: Relying on the flip unit to flip and adjust the clamped spacer rod 5 so that it is aligned with the hanging ring 44; S5: The hanging ring 44 is adjusted to hook the spacer 5 and then moved to the power transmission line for installation; S6: After the installation is completed, continue to use the hanging ring 44 to hook the spacer rod 5, and repeat the operation without frequent return.

[0039] Among them, the UAV mounting base 1 is fixed under the UAV, and the storage bin 6 is installed on the UAV mounting base 1; a plurality of the spacer bars 5 are placed inside the storage bin 6; the clamping claws 7 clamp the spacer bars 5 in the storage bin 6; the clamped spacer bars 5 are flipped and adjusted by the flip unit to align them with the hanging ring 44; the hanging ring 44 is adjusted to hook the spacer bars 5, and then moved to the power transmission line for installation; after the installation is completed, the hanging ring 44 is continued to be used to hook the spacer bars 5, thereby repeating the operation without the need for frequent returns.

[0040] The above disclosure is merely one or more preferred embodiments of the present application and is not intended to limit the scope of the present application. A person skilled in the art will understand that all or part of the processes of the above embodiments and equivalent changes made in accordance with the claims of the present application are still within the scope of the present application.

Claims

1. A transmission line spacer rod UAV installation control system, comprising a UAV mounting base, a satellite positioning module, a sensor module, a controller and spacer rods, wherein the satellite positioning module, the sensor module and the controller are all arranged on the UAV mounting base, and the spacer rods are arranged below the UAV mounting base, characterized in that: Also included are installation components; The mounting assembly includes a hanging ring, a storage bin, a plurality of clamping claws and a flip unit. The hanging ring is arranged below the drone mounting base, the spacer rod is arranged on the hanging ring, the storage bin is arranged on one side of the drone mounting base, and a plurality of the spacer rods are stored in the storage bin. The flip unit is arranged below the storage bin, and a plurality of the clamping claws are arranged on the flip unit.

2. The transmission line spacer UAV installation control system according to claim 1, characterized in that: The mounting assembly further includes a winding unit, which is disposed on the drone mounting base; The winding unit includes a winding shaft, a rotating component, a connecting rope and a transverse moving component. The transverse moving component is arranged below the drone mounting base. The output end of the transverse moving component is fixedly connected to the winding shaft. The rotating component is arranged on the winding shaft. One end of the connecting rope is sleeved on the winding shaft, and the other end of the connecting shaft is fixedly connected to the hanging ring.

3. The transmission line spacer UAV installation control system according to claim 2, characterized in that: The installation assembly further includes a storage unit, which is disposed inside the storage bin; The storage unit includes two slides, two first electromagnets, two supporting mechanisms, multiple end protection sleeves, multiple metal sliders, two end protection sleeve transfer mechanisms and multiple second electromagnets. The two slides are symmetrically arranged inside the storage bin, the two first electromagnets are respectively arranged inside the corresponding slides, the two supporting mechanisms are respectively arranged below the corresponding slides, the multiple end protection sleeves are respectively sleeved on the two ends of the corresponding spacer rods, the multiple metal sliders are respectively arranged on one side of the corresponding end protection sleeves, the metal sliders are slidably connected to the slides, the two end protection sleeve transfer mechanisms are symmetrically arranged inside the storage bin, and the multiple second electromagnets are respectively arranged on one side of the corresponding slides.

4. The transmission line spacer UAV installation control system according to claim 3, characterized in that: The flip unit includes a first flip component, a first flip plate, a second flip component, a second flip plate, two first flip locking mechanisms and two second flip locking mechanisms. The first flip component is arranged below the storage bin, the output end of the first flip component is provided with the first flip plate, the second flip component is arranged at one end of the first flip plate, the output end of the second flip component is provided with the second flip plate, two first flip locking mechanisms are arranged below the storage bin, and two second flip locking mechanisms are symmetrically arranged on both sides of the second flip component.

5. The transmission line spacer UAV installation control system according to claim 4, characterized in that: The first flip locking mechanism includes a first telescopic component and a first locking block. The first telescopic component is arranged below the storage bin. The output end of the first telescopic component is fixedly connected to the first locking block. The first flip plate has a first slot. The first slot and the first locking block are adapted to each other. The second flip locking mechanism includes a second telescopic component and a second locking block. The second telescopic component is arranged on the first flip plate and is located on one side of the second flip component. The output end of the second telescopic component is fixedly connected to the second locking block. The first flip plate has a second card slot, and the second card slot and the second locking block are adapted to each other.

6. The transmission line spacer UAV installation control system according to claim 5, characterized in that: The abutting mechanism includes two abutting components and two abutting plates. The two abutting components are symmetrically arranged below the chute. The output ends of the two abutting components are fixedly connected to the corresponding abutting plates respectively. The abutting plates are adapted to the bottom of the chute. The end protective cover transfer mechanism includes a lifting screw machine, two protective cover moving parts, a protective cover support plate, a third electromagnet telescopic part and a third electromagnet. The lifting screw machine is arranged on the inner wall of the storage bin, and the output end of the lifting screw machine is fixedly connected to the two protective cover moving parts, and the output end of the protective cover moving part is fixedly connected to the protective cover support plate. The end protective cover is placed on the protective cover support plate. The third electromagnet telescopic part is arranged inside the storage bin and is located between the two protective cover moving parts. The output end of the third electromagnet telescopic part is fixedly connected to the third electromagnet, and the third electromagnet and the metal slider attract each other.

7. The transmission line spacer UAV installation control system according to claim 6, characterized in that: The mounting assembly further comprises two clamping units, and the two clamping units are sequentially arranged on the second flip plate; The clamping unit includes a placement seat, a cushion and two clamping components. The placement seat is arranged on one side of the second flip plate, the cushion is arranged on one side of the placement seat, the spacer rod is placed above the cushion, and the two clamping components are symmetrically arranged on the placement seat. The output ends of the two clamping components are respectively fixedly connected to the corresponding clamping claws.

8. The transmission line spacer UAV installation control system according to claim 7, characterized in that: The spacer bar includes a spacer bar body, two mounting heads, two hooks and two bayonet mechanisms, wherein the two mounting heads are symmetrically arranged at both ends of the spacer bar body, the two hooks are respectively arranged on one side of the corresponding mounting heads, and the two bayonet mechanisms are respectively arranged on the other side of the corresponding mounting heads; The latch mechanism includes a telescopic motor, a socket, a geared clamping wheel and a clamping block. The telescopic motor is arranged inside the mounting head, and the socket is provided at the output end of the telescopic motor. The geared clamping wheel is arranged on one side of the socket. The clamping block is arranged inside the mounting head and is adapted to the geared clamping wheel.

9. A transmission line spacer UAV installation control method, using the transmission line spacer UAV installation control system according to claim 8, characterized in that: The steps include: By fixing the drone mounting base under the drone and installing the storage bin on the drone mounting base; Placing a plurality of the spacer rods inside the storage bin; The clamping claws clamp the spacer rods in the storage bin; Relying on the flip unit to flip and adjust the clamped spacer rod so that it is aligned with the hanging ring; The hanging ring is adjusted to hook the spacer bar and then moved to the power transmission line for installation; After the installation is completed, continue to use the hanging ring to hook the spacer rod, thereby repeating the operation without frequent return.

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