CN116111700A

CN116111700A - Unmanned energy supplementing system of automatic electric power inspection equipment and use method

Info

Publication number: CN116111700A
Application number: CN202310087325.7A
Authority: CN
Inventors: 许钒; 孟强龙; 刘莉; 刘香君; 汤红
Original assignee: MaAnshan Power Supply Co of State Grid Anhui Electric Power Co Ltd
Current assignee: MaAnshan Power Supply Co of State Grid Anhui Electric Power Co Ltd
Priority date: 2023-02-09
Filing date: 2023-02-09
Publication date: 2023-05-12

Abstract

The invention discloses an unattended energy supplementing system of electric power automatic inspection equipment and a use method thereof. The main structure of the bicycle comprises a hollow wheel internally provided with a hub motor, an auxiliary frame is erected between the two hollow wheels, the front end of the main frame is erected on the hollow wheel, and the rear end of the main frame is hinged to the middle position of the auxiliary frame through a movable pin; the main frames are fastened on two sides of the base frame; the bottom of the base frame is welded with a short pipe, the tail end of the short pipe is provided with an electric pulley, and the pulley is movably embedded into two side edges of the sliding frame; the invention has the beneficial effects that: the energy storage module is respectively composed of a fuel oil power generation unit, a storage battery and an electric control system, and whether the solar sailboard generates electricity or stores energy by the fuel oil power generation unit can be switched according to actual conditions by the electric control system; a photosensitive element is arranged on a sailboard base table; the light tracking device can provide signals for the light tracking of the sailboard module; the folding mode of the sailboard module is adopted, so that the function of fully storing the sailboard module in the sailboard box body is realized.

Description

Unmanned energy supplementing system of automatic electric power inspection equipment and use method

Technical Field

The invention relates to the technical field of inspection only, in particular to an unattended energy supplementing system of electric power automatic inspection equipment and a use method thereof.

Background

The power is required to be subjected to power generation, power transmission and transformation, power distribution and other links from production to use. In the power transmission and transformation link, the power transmission line is equivalent to a large artery of electric power, the power transmission is seriously consumed in the transportation process, hidden dangers exist in the transportation process, and if weather factors and the like are encountered, material loss can be caused. The reliability and the safety of power supply of the power grid are guaranteed while the electric energy loss is reduced as much as possible, and the electric power personnel inspection work is emphasized. Various sensors are installed for the power equipment, the running condition of the power equipment is monitored on line in real time, and once abnormality exists, an maintainer is reminded in time to check faults on site. The inspection personnel can only finish ten kilometers of inspection work in one day along one foundation of the line pole tower, so that the inspection personnel are time-consuming and labor-consuming and have low efficiency; the traditional electric power line inspection adopts an inspection mode of manual recording, and the manual recording sometimes causes that information cannot be timely and accurately reported, and the problems of omission and the like exist; the patrol personnel are exposed to the sun at high temperature in the process of patrol, and insect bites, scratches and scratches are all household mess. With the wide application of the 5G unmanned aerial vehicle, the 5G+ camera and the state online monitoring technology, the problems are not difficult.

However, due to the short board of the current battery technology, the automatic inspection work time of the unmanned aerial vehicle is too short, and due to the too short work time, the inspection work of the unmanned aerial vehicle is often interrupted, and is frequently interrupted, so that the work efficiency is greatly reduced. Moreover, because the storage battery is replaced by manual intervention, unmanned operation cannot be realized, so that the unmanned aerial vehicle inspection mode is adopted at present, and the unmanned aerial vehicle inspection mode can be realized only by the matched working personnel. In short, the real unmanned operation and the unattended function cannot be realized.

Disclosure of Invention

(one) solving the technical problems

Aiming at the defects of the prior art, the invention provides an unmanned energy supplementing system of an automatic electric power inspection device and a use method thereof, and solves the technical problems in the background art.

(II) technical scheme

In order to achieve the above purpose, the invention is realized by the following technical scheme: an unmanned energy supplementing system of an automatic electric power inspection device mainly comprises a hollow wheel, a hub motor, an auxiliary frame, a main frame, a movable pin and a power supply device, wherein the hub motor is arranged in the hollow wheel; the main frames are fastened on two sides of the base frame; the bottom of the base frame is welded with a short pipe, the tail end of the short pipe is provided with an electric pulley, and the pulley is movably embedded into two side edges of the sliding frame;

the top of the base frame is fixedly provided with a sailboard box body, and the whole sailboard box body is of a trapezoid structure; jet grooves are formed in two sides of the opening position of the top of the sailboard box body, and the jet grooves are used for exhausting air through a blower communicated with the bottom of the jet grooves; the rail is fixed on the vertical position of the inner wall of the sailboard box body;

the electric climbing wheels are arranged on two sides of the sailboard base table, a driving motor module is arranged in the middle of the sailboard base table, and the driving motor module is divided into a motor and a pinion part; the sailboard base table is also provided with a big fluted disc which is driven by a pinion; the electric climbing wheel is movably embedded in the rail;

an energy supplementing rod is fixed at the top of the coaxial unmanned aerial vehicle;

the energy storage module is arranged in the sailboard box body and is respectively composed of a fuel oil generator set, a storage battery and an electric control system; a data interaction system is also arranged in the sailboard box body; the top of the sailboard box body is provided with an electric door.

Further, a cover piece is fixed on the sliding frame, T-shaped workpieces are respectively and movably hinged to two sides of the top end of the cover piece, and a second electric air rod is movably hinged between the bottom ends of the two T-shaped workpieces; one end of each T-shaped workpiece is fixed with a rotating shaft, a first electrode wheel is sleeved on one rotating shaft, and a second electrode wheel is sleeved on the other rotating shaft; one side of the top ends of the two T-shaped workpieces are hinged with two lower end angles of the cover piece through short shaft air bars.

Further, the big fluted discs are respectively hinged with a supporting rod and a first electric air rod; the tail end of the supporting rod is fixed on a rotor of the first gear motor, and a first gear is sleeved outside a body of the first gear motor; the first gear is meshed with the second gear; the tail end of the first electric air rod is fixed in the jacket clamp; the second gear is fixed with a short lifting arm, the tail end of the short lifting arm is fixed with a second gear motor body, a rotor of the second gear motor is fixed on a jacket base, the other surface of the jacket base is fixed on two rotors of a third gear motor, and the bodies of the two third gear motors are respectively fixed with a first stay bar and a second stay bar.

Further, the second stay bar is hollow, and a winding motor module is arranged in the second stay bar, and the winding motor module is formed by: the motor comprises a motor body, a winding roll and steel wires, wherein the winding roll is fixed on a rotor of the motor body, and the steel wires are wound on the winding roll; the top end of the steel wire penetrates out of the middle position of the second supporting rod and is fixed at the position corresponding to the first supporting rod; the ends of the first stay bar and the second stay bar are fixed on the back surface of the sailboard module.

Further, the sailboard module is formed by: the quadrangular sailboard is parallelogram, and the matched triangular sailboard is matched with the inclination of the quadrangular sailboard; the four sides of the quadrangular sailboard are provided with hinged notches, and two adjacent sides of the triangular sailboard are provided with hinged notches; the quadrilateral sailboards are hinged with each other, and the two quadrilateral sailboards are hinged with two triangular sailboards which are hinged with each other at the head end and the tail end.

Further, the two triangular sailboards are hinged to form a wind trough area; and each wind groove area is opposite to the position of the air injection groove.

Further, the energy supplementing rod is formed by: the energy supplementing rod is divided into a straight rod piece part and a hook part, and the two sides of the straight rod piece part are respectively fixed with a first electrode piece and a second electrode piece; the outer side surface of the bottom of the hook part is provided with a communication electrode plate group; correspondingly, a receiving base of the communication electrode plate group is arranged on the base frame; the first electrode wheel is abutted against the first electrode plate; the second electrode plate is abutted against the second electrode wheel.

Further, the data interaction system mainly comprises a positioning module, a 3D obstacle avoidance camera module, a 4G/5G data module and an identity verification module.

Further, a flexible solar power generation panel is arranged on the sailboard module, and a photosensitive element is arranged on the sailboard base table; the photosensitive element provides signals for the light following performance of the sailboard module.

(III) beneficial effects

The invention provides an unattended energy supplementing system of an automatic electric power inspection device. The beneficial effects are as follows:

the unmanned energy supplementing system of the automatic electric power inspection equipment adopts an energy storage module which is respectively composed of a fuel oil generator set, a storage battery and an electric control system, and whether a solar sailboard is used for generating electricity or the fuel oil generator set is used for storing energy can be switched according to actual conditions through the electric control system; a photosensitive element is arranged on a sailboard base table; the light tracking device can provide signals for the light tracking of the sailboard module; the function of fully storing the sailboard module in the sailboard box body is realized by adopting a folding mode of the sailboard module; the structure that the air injection groove is arranged in the sailboard box body is adopted, so that a power source is provided in the unfolding process of the sailboard module; the second stay bar is internally provided with a winding motor module, and the winding motor module is used for rewinding the steel wires, so that the function of accommodating the sailboard module is realized at intervals.

Drawings

Fig. 1 is a block diagram of an unmanned energy supply system of an automatic electric power inspection device according to the present invention.

Fig. 2 is a diagram of a sailboard box portion of an unattended energy recovery system of an automatic electric power inspection apparatus according to the present invention.

Fig. 3 is a diagram of a sailboard module and a sailboard base station of an unattended energy supply system of the automatic electric power inspection device according to the invention.

Fig. 4 is a diagram of a sailboard base station of an unattended energy supply system of the automatic electric power inspection equipment according to the invention.

Fig. 5 is a coaxial unmanned aerial vehicle structure diagram of an unmanned energy supplementing system of the automatic electric power inspection equipment.

Fig. 6 is a schematic diagram of an energy supplementing rod structure of an unattended energy supplementing system of the automatic electric power inspection equipment.

Fig. 7 is a single block diagram of a sailboard module of an unattended energy supply system of the automatic electric power inspection device.

Fig. 8 is a block diagram of a sailboard module unit and a supporting brace of an unattended energy supply system of the automatic electric power inspection equipment.

Fig. 9 is a schematic diagram of an unfolding structure of a sailboard module of an unmanned energy supplementing system of an automatic electric power inspection device.

Fig. 10 is a detail view at a of fig. 1.

Fig. 11 is a block diagram of an energy supplementing pinch roller of an unattended energy supplementing system of an automatic electric power inspection device.

Fig. 12 is a block diagram of a carriage and a base frame of an unattended energy replenishment system of an automatic electric power inspection apparatus according to the present invention.

Fig. 13 is a front view of a sailboard module moving rack of an unattended energy replenishment system of an automatic electric power inspection device according to the present invention.

FIG. 14 is a cross-sectional view of the structure at A-A of FIG. 13.

Fig. 15 is a diagram of a sailboard module moving support of an unattended energy supply system of an automatic electric power inspection device according to the invention.

In the figure: the device comprises a 1-hollow wheel, a 2-auxiliary frame, a 3-main frame, a 4-sailboard box body, 41-rail bars, a 5-jet tank, a 6-carriage, a 7-base frame, a 71-electric pulley, an 8-sailboard module, an 81-quadrilateral sailboard, an 82-triangular sailboard, a 9-sailboard base table, a 91-electric climbing wheel, a 10-driving motor module, an 11-large fluted disc, a 12-supporting rod, a 13-first electric air pole, a 14-jacket clamp, a 15-first gear, a 16-first gear, a 161-second gear, a 17-short lifting arm, a 171-second gear motor, a 172-jacket base, an 18-first supporting rod, a 19-second supporting rod, a 191-winding motor module, a 1911-steel wire, a 20-third gear motor, a 21-coaxial unmanned aerial vehicle, a 22-energy supplementing pole, a 221-first electrode pole piece, a 222-second electrode piece, a 223-communication electrode group, a 23-first electrode pole piece, a 24-second electrode pole piece, a 25-second electrode piece, a 25-T-shaped workpiece, a 27-second electric pole piece, and a short shaft cover.

Detailed Description

The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.

Examples: as shown in fig. 1 and 2, the structure is designed as a whole, and in the design, three groups of hollow wheels 1 are adopted as the whole chassis; and a suspension structure is formed by the connection of the auxiliary frame 2 between two groups of hollow wheels 1; the main frame 3 and the auxiliary frame 2 are movably hinged; the whole scheme can walk on a steep slope road surface.

The whole structure in this case divide into: the walking part, the base and the sailboard box body 4; the walking part described here has been described in the above paragraph, and the base structure is shown with reference to fig. 2 and 12, which are mainly interconnected by a carriage 6 and a base frame 7 by means of an electric pulley 71; thereby realizing that the carriage 6 and the base frame 7 can slide freely with each other; the base frame 7 is installed at the bottom of the sailboard case 4, and both sides of the base frame 7 are also installed with the main frame 3;

as shown in the structures in fig. 10, 11 and 12, a set of electrode clamp devices is also mounted on the freely slidable carriage 6, and the electrode clamp devices are formed by: a cover piece 29 is fixed on the carriage 6, T-shaped workpieces 26 are respectively and movably hinged to two sides of the top end of the cover piece 29, and a second electric air rod 28 is movably hinged between the bottom ends of the two T-shaped workpieces 26; one end of each T-shaped workpiece 26 is fixed with a rotating shaft, a first electrode wheel 23 is sleeved on one rotating shaft, and a second electrode wheel 24 is sleeved on the other rotating shaft; one side of the top ends of the two T-shaped workpieces 26 are hinged with two lower end corners of the cover piece 29 through short shaft air bars 27.

The windsurfing board case 4 as shown in fig. 1 and 2 has three main functions: one provides a storage space for the folded triangular sailboard 82, and the other two is that the two sides of the sailboard box body 4 are of an inclined plane structure, and an air injection groove 5 is arranged on the inner wall of the inclined plane structure; auxiliary force can be provided for unfolding the triangular sailboard 82 through the air jet grooves 5; thirdly, rail bars 41 are arranged on the two inner sides of the vertical surface of the sailboard box body 4; providing a track for lifting and lowering the windsurfing board base 9.

The lifting and steering structure of the triangular sailboard 82 in this case is described with reference to fig. 13, 14 and 15: the big fluted disc 11 is respectively hinged with a supporting rod 12 and a first electric air rod 13; the tail end of the supporting rod 12 is fixed on a rotor of the first gear motor 15, and a first gear 16 is sleeved outside a body of the first gear motor 15; the first gear 16 is meshed with the second gear 161; the tail end of the first electric air rod 13 is fixed in the jacket clamp 14; the second gear 161 is fixed with a short lifting arm 17, the tail end of the short lifting arm 17 is fixed with a second gear motor 171 body, the rotor of the second gear motor 171 is fixed on a jacket base 172, the other surface of the jacket base 172 is fixed on the rotors of two third gear motors 20, and the bodies of the two third gear motors 20 are respectively fixed with a first stay bar 18 and a second stay bar 19;

the second stay 19 is hollow, and a winding motor module 191 is built in the second stay 19, and the winding motor module 191 is formed by: the motor comprises a motor body, a winding roll and a steel wire 1911, wherein the winding roll is fixed on a rotor of the motor body, and the steel wire 1911 is wound on the winding roll; the top end of the steel wire 1911 penetrates out from the middle position of the second stay bar 19 and is fixed at the position corresponding to the first stay bar 18; the tail ends of the first stay bar 18 and the second stay bar 19 are fixed on the back surface of the sailboard module 8;

the lifting part is obviously composed of the following parts by the structure: the first electric air rod 13, the first gear motor 15 and the second gear motor 171 are matched with each other; when the sailboard module 8 extends out of the sailboard box 4 completely, the steering is completed by the steering of the big fluted disc 11.

As shown in fig. 2 and 4, the rail 41 is installed in the windsurfing board case 4; while the two ends of the sailboard base seat 9 are respectively provided with a climbing wheel 91; therefore, when the wheel 91 engages with the rail 41, the sailboard base 9 can be lifted up and down by driving the wheel 91.

The structure of the windsurfing board 8 is described in connection with fig. 7, 8 and 9, wherein the windsurfing board 8 comprises: the quadrangular sailboard 81 is in a parallelogram shape, and the matched triangular sailboard 82 is matched with the inclination of the quadrangular sailboard 81; the four sides of the quadrangular sailboard 81 are provided with hinged notches, and two adjacent sides of the triangular sailboard 82 are provided with hinged notches; the quadrangular sailboards 81 are hinged with each other, and the two quadrangular sailboards 81 are hinged with two triangular sailboards 82 hinged with each other at the transverse head and tail ends;

from the above described construction it is readily apparent that the volume of the windsurfing board 8 after it has been folded is much smaller than it would otherwise be;

for the folding of the windsurfing board modules 8: the first stay bar 18 and the second stay bar 19 are mutually tied by driving the steel wire 1911 of the winding motor module 191; thereby linking the whole sailboard module 8 for folding;

for the opening of the windsurfing modules 8: the third gear motor 20 provides an auxiliary force for movement so that the first stay bar 18 and the second stay bar 19 are opened; the air sprayed by the air spraying grooves 5 in the inclined plane structure of the sailboard box body 4 provides most of unfolding force, and the air sprayed by the air spraying grooves 5 is just blown into the folded grooves of the sailboard modules 8, so that the sailboard modules 8 are unfolded.

As shown in fig. 5 and 6, fig. 5 shows a structure of the coaxial unmanned aerial vehicle 21, and the innovation part of the scheme is mainly an energy supplementing rod 22 below the coaxial unmanned aerial vehicle 21; and the energy supplementing rod 22 is formed by: the energy supplementing rod 22 is divided into a straight rod part and a hook part, and the two sides of the straight rod part are respectively fixed with a first electrode plate 221 and a second electrode plate 222; the outer side surface of the bottom of the hook part is provided with a communication electrode plate group 223; correspondingly, the base frame 7 is provided with a receiving base of the communication electrode plate group 223; the first electrode wheel 23 abuts against the first electrode plate 221; the second electrode piece 222 abuts against the second electrode wheel 24.

The application method of the unmanned energy supplementing system of the automatic electric power inspection equipment comprises the following steps:

s1, an internal system of the coaxial unmanned aerial vehicle 21 sends out a low-electricity alarm, alarm information data are sent to a server main platform, after the server main platform receives signals, the equipment closest to the coaxial unmanned aerial vehicle 21 sending out the low-electricity alarm is calculated through positioning checking of background data, the server main platform sends signals to the equipment, and a working system is activated after the equipment receives instructions.

S2, after the system is activated in S1, the equipment is in butt joint with the coaxial unmanned aerial vehicle 21 which is in low-electric alarm nearby, and data exchange is realized after the equipment and the coaxial unmanned aerial vehicle are in butt joint, so that a proper position is determined for butt joint; the hub motor in the hollow wheel 1 is started, so that the equipment has walking capability, and the intervention of the auxiliary frame 2 provides walking capability for the bumpy road surface of the equipment; the equipment is stopped when walking to a preset position, and the electric pulley 71 is started at the moment, so that the carriage 6 slides out of the base frame 7; the second electric air rod 28 is started to shrink, so that the first electrode wheel 23 and the second electrode wheel 24 are in an open state; the coaxial unmanned aerial vehicle 21 flies to the upper side, and the energy supplementing rod 22 is accurately inserted between the first electrode wheels 23 and the second electrode wheels 24 through the 3D obstacle avoidance camera module;

s3, in the step S2, the communication electrode plate group 223 at the bottom of the energy supplementing rod 22 is firstly abutted to a receiving base arranged on the base frame 7; the process is that the equipment reads data information of internal power transmission of the coaxial unmanned aerial vehicle 21 for supplementing energy, wherein the read data comprises a charging voltage value, a rated current value, the health condition of a battery pack and the like required by the type of equipment; when the read data information is free of problems, the second electric air rod 28 is started to stretch, the first electrode wheel 23 and the second electrode wheel 24 are closed, the first electrode wheel 23 and the second electrode wheel 24 are in contact with the corresponding first electrode plate 221 respectively, and the second electrode plate 222 is charged;

s4, after the coaxial unmanned aerial vehicle 21 is charged, starting the second electric air rod 28 to shrink, and separating the first electrode wheel 23 and the second electrode wheel 24 at the moment; starting the fan blades of the coaxial unmanned aerial vehicle 21, and separating the communication electrode plate group 223 from the receiving base by using the lifting force of the coaxial unmanned aerial vehicle 21, so as to complete energy supplementing;

unmanned energy storage to present case equipment:

s1, when an electric control system provided with an energy storage module in a sailboard box body 4 detects that the energy storage of a storage battery is in a low-electricity alarm state, a photosensitive element arranged on a sailboard base table 9 is started at the moment, and the photosensitive element detects whether the current position is in a sufficient illumination state or not, so that the working requirement of a minimum flexible solar power generation panel is met; if the requirements are not met, starting the fuel generator set to charge the storage battery, if the requirements are met, opening an electric door arranged at the top of the sailboard box body 4, then starting the first electric air rod 13 to shrink so as to enable the support rod 12 of the electric air rod to obliquely lift, and simultaneously starting the first speed reducing motor 15 so as to enable the first gear 16 to drive the second gear 161 to rotate, further enabling the short lifting arm 17 to obliquely lift, wherein the oblique lifting angle and the oblique lifting speed of the support rod 12 are identical to those of the short lifting arm 17 in mirror symmetry;

s2, after the step S1 is completed, the body of the sailboard module 8 extends out of the sailboard box 4, at the moment, a blower below the air injection groove 5 is started to enable the air injection groove 5 to spray air, and the sprayed air is opposite to the air groove area, so that the sailboard module 8 at the moment is spread by wind power, and at the same time, two third gear motors 20 on the jacket base 172 are started to enable the first brace 18 and the second brace 19 to be assisted and gathered;

s3, according to the position of a light source provided by a photosensitive original, starting a driving motor module 10 to enable a large fluted disc 11 to control the direction through the large fluted disc 11, and positioning at any position of 360 degrees can be provided for a sailboard module 8; and the rotation of the second gear motor 171 can provide support for the adjustment of the plane angle of the windsurfing board module 8;

s4, folding the sailboard module 8; starting the driving motor module 10 again to enable the large fluted disc 11 to enable the position of the sailboard module 8 to be matched with the sailboard box body 4; starting the winding motor module 191 to shrink the steel wire 1911, so that the first brace 18 and the second brace 19 are closed, and because the quadrangular windsurfing board 81 and the triangular windsurfing board 82 between the windsurfing board modules 8 are hinged with each other, when the first brace 18 and the second brace 19 fixed on the back of the windsurfing board module 8 are closed, all the quadrangular windsurfing board 81 and the triangular windsurfing board 82 are closed;

s5, the first electric air rod 13 and the short lifting arm 17 descend; so that the windsurfing board module 8 is accommodated in the windsurfing board case 4, and finally the electric door arranged at the top of the windsurfing board case 4 is closed.

It should be noted that, in the description of the present invention, the positional or positional relation indicated by the terms such as "upper", "lower", "left", "right", "front", "rear", etc. are merely for convenience of describing the present invention based on the description of the present invention shown in the drawings, and are not intended to indicate or imply that the apparatus or element to be referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus should not be construed as limiting the present invention.

The terms "first" and "second" in this technical solution are merely references to the same or similar structures, or corresponding structures that perform similar functions, and are not an arrangement of the importance of these structures, nor are they ordered, or are they of a comparative size, or other meaning.

In addition, unless explicitly stated and limited otherwise, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., the connection may be a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communicated with the inside of two structures. It will be apparent to those skilled in the art that the specific meaning of the terms described above in this application may be understood in the light of the general inventive concept in connection with the present application.

Claims

1. An unmanned energy supplementing system of electric power automatic inspection equipment comprises a hollow wheel (1) and an in-wheel motor arranged in the hollow wheel, wherein an auxiliary frame (2) is erected between the two hollow wheels (1), the front end of a main frame (3) is erected on the hollow wheel (1), and the rear end of the main frame is hinged to the middle position of the auxiliary frame (2) through a movable pin; the method is characterized in that: the main frame (3) is fastened on two sides of the base frame (7); the bottom of the base frame (7) is welded with a short pipe, the tail end of the short pipe is provided with an electric pulley (71), and the pulley (71) is movably embedded into two side edges of the sliding frame (6);

the top of the base frame (7) is fixed with a sailboard box body (4), and the whole sailboard box body (4) is of a trapezoid structure; air injection grooves (5) are formed in two sides of the opening position of the top of the sailboard box body (4), and the air injection grooves (5) are used for exhausting air through an air blower communicated with the bottom; the rail (41) is fixed on the vertical position of the inner wall of the sailboard box body (4);

the two sides of the sailboard base table (9) are respectively provided with an electric climbing wheel (91), a driving motor module (10) is arranged in the middle of the sailboard base table (9), and the driving motor module (10) comprises a motor and a pinion part; the sailboard base table (9) is also provided with a big fluted disc (11), and the big fluted disc (11) is driven by a pinion; the electric climbing wheel (91) is movably embedded into the rail (41);

an energy supplementing rod (22) is fixed at the top of the coaxial unmanned aerial vehicle (21);

an energy storage module is arranged in the sailboard box body (4), and the energy storage module is respectively composed of a fuel oil generator set, a storage battery and an electric control system; a data interaction system is also arranged in the sailboard box body (4); the top of the sailboard box body (4) is provided with an electric door.

2. The unmanned energy supply system of the automatic electric power inspection equipment according to claim 1, wherein: a cover piece (29) is fixed on the sliding frame (6), T-shaped workpieces (26) are respectively and movably hinged to two sides of the top end of the cover piece (29), and a second electric air rod (28) is movably hinged between the bottom ends of the two T-shaped workpieces (26); one end of each T-shaped workpiece (26) is fixed with a rotating shaft, a first electrode wheel (23) is sleeved on one rotating shaft, and a second electrode wheel (24) is sleeved on the other rotating shaft; one side of the top ends of the two T-shaped workpieces (26) are hinged with two lower end angles of the cover piece (29) through short shaft air bars (27).

3. The unmanned energy supply system of the automatic electric power inspection equipment according to claim 1, wherein: the large fluted disc (11) is respectively hinged with a supporting rod (12), and a first electric air rod (13); the tail end of the supporting rod (12) is fixed on a rotor of a first gear motor (15), and a first gear (16) is sleeved outside a body of the first gear motor (15); the first gear (16) is meshed with the second gear (161); the tail end of the first electric air rod (13) is fixed in the jacket clamp (14); the second gear (161) is fixed with a short lifting arm (17), the tail end of the short lifting arm (17) is fixed with a second gear motor (171) body, the rotor of the second gear motor (171) is fixed on a jacket base (172), the other surface of the jacket base (172) is fixed on the rotors of two third gear motors (20), and the bodies of the two third gear motors (20) are respectively fixed with a first stay bar (18) and a second stay bar (19).

4. An unmanned energy supply system for an automatic power inspection device according to claim 3, wherein: the second stay bar (19) is hollow, and is internally provided with a winding motor module (191), and the winding motor module (191) consists of: the motor comprises a motor body, a winding roll and a steel wire (1911), wherein the winding roll is fixed on a rotor of the motor body, and the steel wire (1911) is wound on the winding roll; the top end of the steel wire (1911) penetrates out of the middle position of the second supporting rod (19) and is fixed at a position corresponding to the first supporting rod (18); the tail ends of the first stay bar (18) and the second stay bar (19) are fixed on the back surface of the sailboard module (8).

5. The unmanned energy supply system of the automatic electric power inspection equipment according to claim 1, wherein: the sailboard module (8) comprises a quadrilateral sailboard (81), wherein the quadrilateral sailboard (81) is a parallelogram, and the matched triangular sailboard (82) is matched with the inclination of the quadrilateral sailboard (81); the four sides of the quadrangular sailboard (81) are provided with hinged notches, and two adjacent sides of the triangular sailboard (82) are provided with hinged notches; the quadrangular sailboards (81) are hinged with each other, and two triangular sailboards (82) hinged with each other are used for the transverse head end and the transverse tail end to be hinged with the two quadrangular sailboards (81).

6. The unmanned energy supply system of the automatic electric power inspection equipment according to claim 5, wherein: two triangular sailboards (82) are hinged to form a wind trough area; each air groove area is opposite to the position of the air injection groove (5).

7. The unmanned energy supply system of the automatic electric power inspection equipment according to claim 1, wherein: the energy supplementing rod (22) comprises a straight rod piece part and a hook part, wherein a first electrode piece (221) and a second electrode piece (222) are respectively fixed on two sides of the straight rod piece part; the outer side surface of the bottom of the hook part is provided with a communication electrode plate group (223); correspondingly, a receiving base of the communication electrode plate group (223) is arranged on the base frame (7); the first electrode wheel (23) is abutted against the first electrode plate (221); the second electrode plate (222) is abutted against the second electrode wheel (24).

8. An unmanned energy supply system for an automatic power inspection device according to claim 3, wherein: the data interaction system mainly comprises a positioning module, a 3D obstacle avoidance camera module, a 4G/5G data module and an identity verification module.

9. The unmanned energy supply system of the automatic electric power inspection equipment according to claim 1, wherein: the flexible solar power generation panel is arranged on the sailboard module (8), and the photosensitive element is arranged on the sailboard base table (9); the photosensitive element provides signals for light following of the sailboard module (8).

10. The method for using an unattended energy charging system of an automatic electric power inspection device according to any one of claims 1-9, wherein the method comprises the following steps: the method comprises the following steps:

energy supplementing step for the coaxial unmanned aerial vehicle (21):

s1, an internal system of the coaxial unmanned aerial vehicle (21) sends out a low-electricity alarm, alarm information data are sent to a server main platform, after the server main platform receives signals, the server main platform calculates equipment in the scheme closest to the coaxial unmanned aerial vehicle (21) sending out the low-electricity alarm through positioning checking of background data, the server main platform sends signals to the equipment in the scheme, and a working system is activated after the equipment in the scheme receives instructions.

S2, after the system is activated in S1, the equipment is in butt joint with a coaxial unmanned aerial vehicle (21) which is in low-electric alarm nearby, and data exchange is realized after the equipment and the coaxial unmanned aerial vehicle are in butt joint, so that a proper position is determined for butt joint; the hub motor in the hollow wheel (1) is started, so that the equipment has walking capability, and the intervention of the auxiliary frame (2) provides the walking capability for the bumpy road surface of the equipment; the equipment is stopped when walking to a preset position, and an electric pulley (71) is started at the moment to enable the sliding frame (6) to slide out of the base frame (7); starting the second electric air rod (28) to shrink so as to enable the first electrode wheel (23) and the second electrode wheel (24) to be in an open state; the coaxial unmanned aerial vehicle (21) flies to the upper part, and the energy supplementing rod (22) is accurately inserted between the first electrode wheels (23) and the second electrode wheels (24) through the 3D obstacle avoidance camera module;

s3, in the step S2, the communication electrode plate group (223) at the bottom of the energy supplementing rod (22) is firstly abutted to a receiving base arranged on the base frame (7); the process is that the equipment reads data information of internal power transmission of the coaxial unmanned aerial vehicle (21) for supplementing energy, and the read data comprises a charging voltage value, a rated current value, the health condition of a battery pack and the like required by the type equipment; when the read data information is free of problems, a second electric air rod (28) is started to stretch, the first electrode wheel (23) and the second electrode wheel (24) are close, the first electrode wheel (23) is in contact with the second electrode wheel (24) respectively, and the second electrode plates (222) are charged;

s4, after the coaxial unmanned aerial vehicle (21) is charged, starting a second electric air rod (28) to shrink, and separating the first electrode wheel (23) and the second electrode wheel (24) at the moment; starting the fan blades of the coaxial unmanned aerial vehicle (21), and separating the communication electrode plate group (223) from the receiving base by using the lifting force of the coaxial unmanned aerial vehicle (21), so as to complete energy supplementing;

unmanned energy storage to present case equipment:

s1, when an electric control system provided with an energy storage module in a sailboard box body (4) detects that the energy storage of a storage battery is in a low-electricity alarm state, a photosensitive element arranged on a sailboard base table (9) is started at the moment, and the photosensitive element detects whether the current position is in a sufficient illumination state or not, so that the working requirement of the minimum flexible solar power generation panel is met; if the working requirement is met, the top of the sailboard box body (4) is provided with an electric door which is opened, then the first electric air rod (13) is started to shrink, so that the supporting rod (12) of the electric air rod is obliquely lifted, and meanwhile, the first gear motor (15) is started, so that the first gear (16) drives the second gear (161) to rotate, and further, the short lifting arm (17) is obliquely lifted, and the angle and the speed of the oblique lifting of the supporting rod (12) are identical to those of the short lifting arm (17) in mirror symmetry;

s2, after the step S1 is completed, the body of the sailboard module (8) extends out of the sailboard box body (4), at the moment, a blower below the air injection groove (5) is started to spray air to the air injection groove (5), and the sprayed air is opposite to the air injection groove area, so that the sailboard module (8) is spread by wind power, and at the same time, two third gear motors (20) on the jacket base (172) are started to make the first support rods (18) and the second support rods (19) close in an auxiliary manner;

s3, starting a driving motor module (10) according to the position of a light source provided by a photosensitive original, so that a large fluted disc (11) can control the direction through the large fluted disc (11), and positioning at any position of 360 degrees can be provided for a sailboard module (8); and the rotation of the second gear motor (171) can provide support for the adjustment of the plane angle of the sailboard module (8);

s4, folding the sailboard module (8); starting the driving motor module (10) again to enable the big fluted disc (11) to enable the position of the sailboard module (8) to be matched with the sailboard box body (4); starting the winding motor module (191) to enable the steel wire (1911) to shrink, so that the first brace rods (18) and the second brace rods (19) are close, and as the quadrangular sailboards (81) and the triangular sailboards (82) between the sailboard modules (8) are hinged with each other, when the first brace rods (18) and the second brace rods (19) fixed on the back surfaces of the sailboard modules (8) are close, all the quadrangular sailboards (81) and the triangular sailboards (82) are close;

s5, the first electric air rod (13) and the short lifting arm (17) descend; therefore, the sailboard module (8) is contained in the sailboard box body (4), and finally, the electric door arranged at the top of the sailboard box body (4) is closed.