10KV overhead line acousto-optic electricity testing device carried by unmanned aerial vehicle

Abstract

The utility model relates to the technical field of electric power overhaul, in particular to a 10KV overhead line acousto-optic electricity testing device carried by an unmanned aerial vehicle. Comprising an unmanned aerial vehicle body, a working platform arranged on the unmanned aerial vehicle body, a fixed sleeve arranged on the working platform, an insulating rod arranged on the fixed sleeve in a sliding mode, a base arranged on the insulating rod, a magnetic attraction assembly arranged on the base, an assembling assembly arranged on the base in a sliding mode and an electroscope arranged between the assembling assembly and the magnetic attraction assembly. One end of the electroscope is in threaded connection with the assembling component, the other end of the electroscope is provided with an adsorption steel plate, and the electroscope is in magnetic connection with the magnetic component through the adsorption steel plate. According to the utility model, the problem of potential safety hazards occurring in the high-voltage electricity testing process is effectively solved, personal electric shock risks are avoided, the operation is simple, time-saving and labor-saving, and the on-site safe operation efficiency is improved.

Description

TECHNICAL FIELD

[0001] The utility model relates to power maintenance technical field especially relates to a unmanned aerial vehicle carries 10KV overhead line sound light electricity testing device. BACKGROUND

[0002] The electricity testing before the grounding wire is installed can determine whether the power-off equipment is voltageless, so as to ensure the safety of the personnel installing the grounding wire and prevent the occurrence of malignant accidents such as live-line installation of the grounding wire or live-line combination of the grounding isolation switch, and the electricity testing work needs to use the corresponding voltage grade and qualified contact type electricity tester, but the existing high-voltage electricity testing work is generally carried out by professional personnel who carry the electricity tester to climb the pole to test the electricity, in the process of climbing the pole, the professional personnel consume a large amount of physical strength, in addition to overcoming the psychological barrier of acrophobia, the professional personnel also need to prevent the operation mistakes caused by their own tension and fear, therefore, the climbing speed is slow, and it is easy to cause the safety hidden danger such as pole slipping and pole falling, and even in the process of electricity testing, the human body is close to the conductor, and it is easy to cause the risk of electric shock, which affects the efficiency of the on-site safety operation. SUMMARY

[0003] The utility model discloses to the shortage of prior art, provide a unmanned aerial vehicle carries 10KV overhead line sound light electricity testing device, effectively solve the safety hidden danger problem that occurs in the process of high-voltage electricity testing, avoid the risk of personal electric shock, it is easy to operate and save time and labor, improve the efficiency of on-site safety operation.

[0004] To achieve the above object, the utility model discloses a unmanned aerial vehicle carries 10KV overhead line sound light electricity testing device, including unmanned aerial vehicle body, the operation platform of setting in unmanned aerial vehicle body, the fixed sleeve of setting in operation platform, the insulating rod of sliding setting in fixed sleeve, the base of setting in insulating rod, the magnetic attraction subassembly of setting in base, the assembly component of sliding setting in base and the electricity tester of setting between assembly component and magnetic attraction subassembly, one end of electricity tester is connected with assembly component screw thread, the other end of electricity tester is provided with adsorption steel sheet, and electricity tester is connected with magnetic attraction subassembly through adsorption steel sheet.

[0005] Preferably, the assembly component includes an assembly seat, an assembly screw rod arranged on the assembly seat, a sliding block arranged on the assembly seat, and a guide rail slidably connected with the sliding block, the electricity tester is provided with a threaded hole, the electricity tester is threadedly connected with the assembly screw rod through the threaded hole, the outer side of the sliding block is provided with a first manual locking knob, and the guide rail is arranged on the base.

[0006] Preferably, the magnetic attraction subassembly includes a magnetic attraction seat, outer side wings arranged on both sides of the magnetic attraction seat, a threaded sleeve arranged on the outer side wings, a connecting screw rod threadedly connected with the threaded sleeve, and a clamping block arranged on the connecting screw rod, the connecting screw rod penetrates through the threaded sleeve and protrudes into the magnetic attraction seat, so that the clamping block clamps against the outer wall of the electricity tester.

[0007] Preferably, the outside of the electroscope is provided with a lifting ring, the lifting ring is provided with an insulating rope, one end of the insulating rope is wound on the outside of the lifting ring, and the other end of the insulating rope is connected to the bottom of the operation platform.

[0008] Preferably, the insulating rod is provided with a connecting hole, the outside of the fixing sleeve is provided with a second manual locking knob, and the connecting hole is provided with a plurality of connecting holes which are arranged at intervals along the length direction of the insulating rod.

[0009] Preferably, the top of the unmanned aerial vehicle body is provided with a first side clamping piece and a second side clamping piece, a solar panel is arranged between the first side clamping piece and the second side clamping piece, and the first side clamping piece and the second side clamping piece are arranged at intervals and located on the two sides of the unmanned aerial vehicle body respectively.

[0010] Preferably, the bottom of the unmanned aerial vehicle body is provided with an electronic eye.

[0011] Preferably, the operation platform is provided with a lighting lamp.

[0012] Preferably, the remote controller is further included, the remote controller is in signal connection with the unmanned aerial vehicle body, the remote controller comprises a first control rocker, a second control rocker, a homing key, a gear shifting key, a key, a display screen and an indicator light, and the outside of the remote controller is provided with an antenna.

[0013] Preferably, the electroscope is an audible and visual type electroscope.

[0014] The utility model discloses beneficial effects: effectively solve the security risk problem that occurs in the high pressure electroscope work process, avoid the risk of personal electric shock, simple operation and save time and labor, improve the on-site safety operation efficiency. BRIEF DESCRIPTION OF DRAWINGS

[0015] Fig. 1 It is the structure schematic diagram of the utility model.

[0016] Fig. 2 It is the structure schematic diagram of the utility model in the working state.

[0017] Fig. 3 It is the structure schematic diagram of the remote controller of the utility model.

[0018] The attached drawing mark includes:

[0019] 1---unmanned aerial vehicle body 11---first side clamping piece 12---second side clamping piece

[0020] 13---solar panel 14---electronic eye

[0021] 2---operation platform 21---lighting lamp

[0022] 3 - fixed sleeve 31 - second manual locking knob

[0023] 4 - insulating rod 41 - connecting hole

[0024] 5 - base

[0025] 6 - magnetic assembly 61 - magnetic seat 62 - outer wing

[0026] 63 - threaded sleeve 64 - connecting screw 65 - clamping block

[0027] 7 - assembly component 71 - assembly seat 72 - assembly screw

[0028] 73 - slider 74 - guide rail 75 - first manual locking knob

[0029] 8 - electroscope 81 - adsorption steel plate 82 - threaded hole

[0030] 83 - lifting ring 84 - insulating rope

[0031] 9 - remote control 91 - first control joystick 92 - second control joystick

[0032] 93 - return key 94 - gear shift key 95 - key

[0033] 96 - display screen 97 - indicator light 98 - antenna. DETAILED DESCRIPTION

[0034] The utility model is described in detail below in combination with the drawings.

[0035] As Figs. 1 to 3 shown, the utility model discloses a 10KV overhead line sound and light electricity testing device carried by unmanned plane, including unmanned plane body 1, setting in the operation platform 2 of unmanned plane body 1, setting in the fixed sleeve 3 of operation platform 2, slidingly setting in the insulating rod 4 of fixed sleeve 3, setting in the base 5 of insulating rod 4, setting in the magnetic assembly 6 of base 5, slidingly setting in the assembly component 7 of base 5 and setting in the electroscope 8 between assembly component 7 and magnetic assembly 6, one end of electroscope 8 is connected in screw thread with assembly component 7, the other end of electroscope 8 is provided with adsorption steel plate 81, and electroscope 8 is connected with magnetic assembly 6 by adsorption steel plate 81 and magnetic attraction.

[0036] First, one end of the electroscope 8 is threadedly connected and fixed on the assembly component 7, since the assembly component 7 can slide back and forth along the length direction of the base 5, thereby leading the other end of the electroscope 8 to be inserted into the magnetic attraction component 6, based on the magnetic force, the magnetic attraction component 6 generates a strong magnetic field, so that the ferromagnetic material on the steel plate 81 is stably adsorbed on the magnetic attraction component 6 under the action of the magnetic force, so as to stably install the electroscope 8 between the assembly component 7 and the magnetic attraction component 6, effectively avoid the electroscope 8 from being accidentally separated from the base 5 due to the influence of strong wind and rain, ensure the working safety of the electroscope 8, the base 5 is slidably connected with the fixed sleeve 3 through the insulating rod 4, further telescopic adjustment of the working position of the electroscope 8 is realized, and the efficient electroscope working of the electroscope 8 is ensured. When working, the professional personnel controls the unmanned aerial vehicle body 1 to ascend and descend around the 10KV high-voltage line iron tower, and uses the electroscope 8 to check and verify that the equipment to be contacted is really free of voltage to ground, so as to ensure that the equipment is installed with a safety measure, according to the high-voltage field operation needs, the unmanned aerial vehicle body 1 can replace the professional personnel to perform the electroscope work, and then the personal risk occurring in the electroscope work process is prevented from the root. The utility model effectively solves the safety hidden trouble problem occurring in the high-voltage electroscope working process, avoids the personal electric shock risk, is simple and easy to operate, saves time and effort, and improves the field safety operation efficiency.

[0037] The assembly component 7 of the embodiment comprises an assembly seat 71, an assembly screw rod 72 arranged on the assembly seat 71, a sliding block 73 arranged on the assembly seat 71 and a guide rail 74 slidably connected with the sliding block 73, the electroscope 8 is provided with a threaded hole 82, the electroscope 8 is threadedly connected with the assembly screw rod 72 through the threaded hole 82, the outer side of the sliding block 73 is provided with a first manual locking knob 75, and the guide rail 74 is arranged on the base 5. Specifically, since the electroscope 8 is provided with the threaded hole 82, the electroscope 8 is threadedly connected with the assembly screw rod 72 through the threaded hole 82, the assembly seat 71 slides back and forth along the length direction of the guide rail 74 through the sliding block 73, then the first manual locking knob 75 is rotated and tightened, thereby fixing the position of the sliding block 73 on the guide rail 74, the operation is simple and the positioning effect is good, so that the position of the electroscope 8 is adjusted accordingly, so that the electroscope 8 is magnetically and fixedly connected with the magnetic attraction component 6.

[0038] The magnetic attraction assembly 6 of the embodiment comprises a magnetic attraction seat 61, outer side wings 62 arranged on both sides of the magnetic attraction seat 61, threaded sleeves 63 arranged on the outer side wings 62, connecting screws 64 threadedly connected with the threaded sleeves 63, and clamping blocks 65 arranged on the connecting screws 64, the connecting screws 64 penetrating through the threaded sleeves 63 and protruding into the magnetic attraction seat 61 so that the clamping blocks 65 clamp against the outer wall of the electroscope 8. Specifically, preferably, two threaded sleeves 63, two connecting screws 64, and two clamping blocks 65 are arranged respectively, the two threaded sleeves 63 are fixedly arranged on the two outer side wings 62 respectively, the two connecting screws 64 are threadedly connected with the two threaded sleeves 63 respectively, the two connecting screws 64 penetrate through the two threaded sleeves 63 and protrude into the magnetic attraction seat 61 respectively, so that the two clamping blocks 65 clamp against the two sides of the electroscope 8, the electroscope 8 is clamped and fixed in the magnetic attraction seat 61, and a strong magnetic field is generated based on the magnetic force of the magnetic attraction seat 61, so that the electroscope 8 is stably adsorbed on the magnetic attraction seat 61 by the adsorption steel plate 81 under the action of the magnetic field, to ensure the working safety performance of the electroscope 8.

[0039] The electroscope 8 of the embodiment is provided with a lifting ring 83 on the outer side, the lifting ring 83 is provided with an insulating rope 84, one end of the insulating rope 84 is wound on the outer side of the lifting ring 83, and the other end of the insulating rope 84 is connected to the bottom of the operation platform 2. Specifically, the electroscope 8 is connected with the insulating rope 84 through the lifting ring 83, and the insulating rope 84 is connected and fixed on the operation platform 2, effectively preventing the electroscope 8 from accidentally falling off the base 5 and directly causing damage to the electroscope 8, even if the electroscope 8 accidentally falls off the base 5, it can also ensure that the electroscope 8 is hung on the operation platform 2, and the safety in use is guaranteed.

[0040] The insulating rod 4 of the embodiment is provided with a connecting hole 41, the outer side of the fixing sleeve 3 is provided with a second manual locking knob 31, and the connecting hole 41 is arranged in plurality and arranged along the length direction of the insulating rod 4. Specifically, the plurality of connecting holes 41 are arranged along the length direction of the insulating rod 4, when the insulating rod 4 slides along the length direction of the fixing sleeve 3, the base 5 is driven to adjust the position, and then the second manual locking knob 31 is turned to fix the position of the insulating rod 4 on the fixing sleeve 3, which is simple and convenient to operate and has good positioning effect, and the position of the base 5 can be adjusted according to different working requirements, so as to facilitate the smooth progress of the electroscope work.

[0041] The top of the unmanned aerial vehicle body 1 of the embodiment is provided with a first side edge clamping piece 11 and a second side edge clamping piece 12, and a solar panel 13 is arranged between the first side edge clamping piece 11 and the second side edge clamping piece 12. The first side edge clamping piece 11 and the second side edge clamping piece 12 are arranged at intervals and are respectively located on the two sides of the unmanned aerial vehicle body 1. Specifically, the solar panel 13 does not need to be screwed when disassembled, and only needs to be horizontally inserted between the first side edge clamping piece 11 and the second side edge clamping piece 12, that is, the solar panel 13 can be connected and installed with the unmanned aerial vehicle body 1. At the same time, the male plug and the female plug are inserted, so that the solar panel 13 and the battery are connected, and there is no need to additionally disconnect the solar panel 13 and the battery. It is convenient to disassemble and can significantly improve the endurance of the unmanned aerial vehicle body 1. By using solar charging, the unmanned aerial vehicle body 1 can continuously supplement the electric energy during flight, thereby prolonging the flight time. Secondly, the solar panel 13 can reduce the dependence on the charging station. The traditional unmanned aerial vehicle needs to return to the charging station for charging after the battery is consumed. This not only limits the use range of the unmanned aerial vehicle, but also needs to build and maintain the charging station. The unmanned aerial vehicle body 1 provided with the solar panel 13 can charge by using sunlight when going out, thereby reducing the dependence on the charging station.

[0042] The bottom of the unmanned aerial vehicle body 1 of the embodiment is provided with an electronic eye 14. Specifically, the electronic eye 14 can improve the work efficiency and accuracy. Through the image recognition function of the electronic eye 14, the electric test position can be effectively identified, and the purpose of accurate electric test work is achieved.

[0043] The work platform 2 of the embodiment is provided with a lighting lamp 21. Specifically, in the night or low light environment, the vision of the unmanned aerial vehicle body 1 is limited, and the flight safety is difficult to guarantee. The installation of the lighting lamp 21 can break the darkness and provide sufficient illumination, so as to ensure that the unmanned aerial vehicle body 1 can normally operate in the night or in bad weather conditions, thereby improving the safety of flight. Moreover, the lighting lamp 21 can improve the quality of night scene shooting. Through different color and brightness adjustment, the lighting lamp 21 can make the shooting picture clearer.

[0044] The embodiment further comprises a remote controller 9, which is in signal connection with the unmanned aerial vehicle body 1, and the remote controller 9 comprises a first control rocker 91, a second control rocker 92, a homing key 93, a gear switching key 94, an on-off key 95, a display screen 96 and an indicator light 97, and an antenna 98 is arranged on the outer side of the remote controller 9. Specifically, the remote controller 9 adds the remote electric testing function, which is more convenient for professionals to carry out electric testing work. The first control rocker 91 is rotated to control the flight height of the unmanned aerial vehicle body 1, the second control rocker 92 is rotated to control the flight direction of the unmanned aerial vehicle body 1, the homing key 93 is long-pressed to realize calling the unmanned aerial vehicle to return, the gear switching key 94 is dialled to the left, the center or the right to respectively switch the slow, medium and fast speed modes of the unmanned aerial vehicle body 1, the on-off key 95 is short-pressed to check the actual power, and is long-pressed for 2 to 3 seconds to realize the on and off of the machine, the display screen 96 is used to display the image information captured by the unmanned aerial vehicle, the antenna 98 is used to transmit and receive wireless signals, and the indicator light 97 is used to display the current working state of the unmanned aerial vehicle body 1, and the indicator light 97 is mainly realized by an LED lamp set, which is generally composed of a plurality of LED lamps connected in series or in parallel, and the light effects of different colors and brightness are realized by controlling the size and direction of the current.

[0045] The electric tester 8 of the embodiment is an acousto-optic type electric tester. Specifically, the acousto-optic type electric tester is a device for testing whether the equipment and line are electrified by detecting the current flowing through the stray capacitance of the electric tester 8, detecting whether there is a power frequency voltage on the high-voltage alternating current line and equipment, having the functions of acousto-optic alarm and double display, ensuring the safety of work, being convenient to carry, high in sensitivity, not being interfered by strong electric field, having the functions of full-circuit self-checking, long standby time and the like. The high-voltage electric tester put into use must be qualified through electrical test, must be tested regularly to ensure its good performance, the electric testing on the line should be carried out on each phase, the electric testing on the circuit breaker or disconnector or other maintenance equipment for connection should be carried out on each phase on the two sides of the incoming and outgoing lines, and the electric testing on the multi-layer power line erected on the 10KV high-voltage line tower should be carried out in the order of first testing low voltage, then testing high voltage, first testing the lower layer and then testing the upper layer.

[0046] The above is only a preferred embodiment of the present application, and for those skilled in the art, the specific implementation manner and application range can be changed according to the idea of the present application, and the content of the specification should not be understood as a limitation of the present application.

Claims

1. An unmanned aerial vehicle-mounted 10KV overhead line acousto-optic electricity testing device, characterized in that: The unmanned aerial vehicle body, the operation platform arranged on the unmanned aerial vehicle body, the fixing sleeve arranged on the operation platform, the insulating rod slidingly arranged in the fixing sleeve, the base arranged on the insulating rod, the magnetic attraction assembly arranged on the base, the assembly assembly slidingly arranged on the base, and the electroscope arranged between the assembly assembly and the magnetic attraction assembly, one end of the electroscope is threadedly connected with the assembly assembly, the other end of the electroscope is provided with an adsorption steel plate, and the electroscope is magnetically connected with the magnetic attraction assembly through the adsorption steel plate.

2. The unmanned aerial vehicle-mounted 10KV overhead line audible and visual electricity testing device according to claim 1, characterized in that: The assembly assembly comprises an assembly seat, an assembly screw rod arranged on the assembly seat, a sliding block arranged on the assembly seat, and a guide rail in sliding connection with the sliding block, the electroscope is provided with a threaded hole, the electroscope is threadedly connected with the assembly screw rod through the threaded hole, the outer side of the sliding block is provided with a first manual locking knob, and the guide rail is arranged on the base. 3.The 10KV overhead line audible and visual electricity testing device carried by the unmanned aerial vehicle according to claim 2, characterized in that: The magnetic attraction assembly comprises a magnetic attraction seat, outer side wings arranged on both sides of the magnetic attraction seat, a threaded sleeve arranged on the outer side wings, a connecting screw rod in threaded connection with the threaded sleeve, and a clamping block arranged on the connecting screw rod, the connecting screw rod penetrates through the threaded sleeve and protrudes into the magnetic attraction seat, so that the clamping block clamps against the outer wall of the electroscope.

4. The unmanned aerial vehicle-mounted 10KV overhead line audible and visual electricity testing device according to claim 3, characterized in that: The outer side of the electroscope is provided with a lifting ring, the lifting ring is provided with an insulating rope, one end of the insulating rope is wound on the outer side of the lifting ring, and the other end of the insulating rope is connected to the bottom of the operation platform.

5. The unmanned aerial vehicle-mounted 10KV overhead line audible and visual electricity testing device according to claim 1, characterized in that: The insulating rod is provided with a connecting hole, the outer side of the fixing sleeve is provided with a second manual locking knob, the connecting hole is provided with a plurality of connecting holes, and the plurality of connecting holes are arranged at intervals along the length direction of the insulating rod.

6. The unmanned aerial vehicle-mounted 10KV overhead line audible and visual electricity testing device according to claim 1, characterized in that: The top of the unmanned aerial vehicle body is provided with a first side edge clamping piece and a second side edge clamping piece, a solar panel is arranged between the first side edge clamping piece and the second side edge clamping piece, and the first side edge clamping piece and the second side edge clamping piece are arranged at intervals and located on the two sides of the unmanned aerial vehicle body respectively.

7. The unmanned aerial vehicle-mounted 10KV overhead line audible and visual electricity testing device according to claim 6, characterized in that: The bottom of the unmanned aerial vehicle body is provided with an electronic eye. 8.The unmanned aerial vehicle-mounted 10 KV overhead line sound-light electricity testing device according to claim 1, characterized in that: The operation platform is provided with a lighting lamp. 9.The 10KV overhead line audible and visual electricity testing device carried by the unmanned aerial vehicle according to claim 1, characterized in that: A remote controller is further included, the remote controller is in signal connection with the unmanned aerial vehicle body, the remote controller comprises a first control joystick, a second control joystick, a homing key, a gear shifting key, a key, a display screen and an indicator light, and the outer side of the remote controller is provided with an antenna.

10. The unmanned aerial vehicle-mounted 10KV overhead line audible and visual electricity testing device according to claim 1, characterized in that: The electroscope is an audible and visual type electroscope.

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