CN204028208U - The unmanned electroscope of high pressure microminiature - Google Patents
The unmanned electroscope of high pressure microminiature Download PDFInfo
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- CN204028208U CN204028208U CN201420486229.6U CN201420486229U CN204028208U CN 204028208 U CN204028208 U CN 204028208U CN 201420486229 U CN201420486229 U CN 201420486229U CN 204028208 U CN204028208 U CN 204028208U
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- electrical verification
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Abstract
The utility model relates to a kind of safety appliance of electric system, the unmanned electroscope of especially a kind of high pressure microminiature.Described comprise unmanned plane, strong-electromagnetic field interval shielding wire, electrical verification system, image pick-up device system and wire touch line device; Electrical verification system comprises electrical verification and transmitter module and receiver module; Electrical verification and transmitter module are made up of electrical verification sensor, amplifying circuit, coding circuit, radio transmitter and high-altitude Signal Monitor; Receiver module is made up of wireless receiving module, decoding scheme, unmanned aerial vehicle controller and information display; Wire touches line device and is connected with electrical verification sensor electrical; The side of unmanned plane bottom is fixedly installed image pick-up device system, and image pick-up device system comprises shooting information sensor, transmission circuit, computer control system and actuator.The utility model electrical verification is safe and reliable, significantly reduces the work of workman, simple to operate.
Description
Technical field
The utility model relates to a kind of safety appliance of electric system, the unmanned electroscope of especially a kind of high pressure microminiature.
Background technology
As everyone knows, closely, the amplification of development on net capacity or electrical network scale of electric system is all unprecedented for the quick growth of national economy and the development relationship of electric system.Electrification in high voltage circuit and equipment are the main tool of electric energy transmitting in power network, along with the expansion of net capacity and electrical network scale, the electric pressure of transmission constantly rises, staff must identify it and locate before the detection carrying out high-tension line and equipment, determine that whether it is charged, thus safety when ensureing circuit stable operation and staff's interruption maintenance of electrical network.
Electroscope is used to detect the usual means whether power equipment existing voltage, electroscope mainly contains the contact electroscopes such as high-tension electricity condensing type electroscope, sparking distance method electroscope and divider resistance formula electroscope, also comprise some non-contact type electricity checking devices, as infrared thermoviewer, ultraviolet imager and ultrasonic wave detector etc.At present in the electrical verification occasion of high-tension line and equipment, because phase-ground distance is large, insulating bar needs longer length, add the weight of electroscopic device on the one hand, improve the labour intensity of operating personnel, insulating bar easily bends on the other hand, be not easy to operation, very large potential safety hazard is there is in staff when work high above the ground, in addition, because the space field intensity around high-tension line and equipment is higher, have higher requirement to galvanoscopic antijamming capability and reliability, therefore there is significant limitation in the galvanoscopic application of existing contact.For non-contact type electricity checking device on the application scenario of high-tension line and equipment, there is complicated operation in existing non-contact type electricity checking technology, cost is high, sensitivity is not high, not enough and can not the defect such as quantificational expression degree of discharge to the dangerous prediction ability of electric discharge, so non-contact type electricity checking device still requires further improvement and improves.
Utility model content
Technical problem to be solved in the utility model is to provide high pressure microminiature electroscope, utilize unmanned air vehicle technique and wireless electrical verification technology, realize the contactless special minute vehicle electrical verification of human body, described can avoid that intensity of workers is large, operation inconvenience, potential safety hazard are large, electrical verification sensitivity and the low problem of reliability, guarantee between transmission line of electricity or electrical equipment safety.
In order to solve the problems of the technologies described above, the technical solution of the utility model is achieved in that
The unmanned electroscope of high pressure microminiature, comprises unmanned plane, strong-electromagnetic field interval shielding wire, electrical verification system, image pick-up device system and wire touches line device; The bottom of unmanned plane fixedly mounts the interval shielding wire of strong-electromagnetic field, electrical verification and transmitter module in turn and wire touches line device; Electrical verification system comprises electrical verification and transmitter module and receiver module; Electrical verification and transmitter module are made up of electrical verification sensor, amplifying circuit, coding circuit, radio transmitter and high-altitude Signal Monitor; Receiver module is made up of wireless receiving module, decoding scheme, unmanned aerial vehicle controller and information display; Wire touches line device and is connected with electrical verification sensor electrical; The side of unmanned plane bottom is fixedly installed image pick-up device system, and image pick-up device system comprises shooting information sensor, transmission circuit, computer control system and actuator.
Further, described electrical verification and transmitter module are positioned in enclosed external shield box and enclosed inner screening box; Wherein external shield box one end and wire touch line device and are electrically connected, and the external shield box other end is connected with electrical verification sensor electrical, inner screening box with " " be connected; Insulation voltage between inner screening box and external shield box is 50V, and inner screening box and external shield box are all made up of the thin iron of conductive magneto-conductive material;
Further, described radio transmitter passes through by the electroscope remote-transmitter antenna transmission electrical verification information of drawing in inner screening box and external shield box; Electroscope remote-transmitter antenna is insulating sleeve;
Further, the interval shielding wire of described strong-electromagnetic field makes unmanned plane control system away from high pressure or UHV (ultra-high voltage) electrified body strong-electromagnetic field segment part, avoids the transmitting and receiving affecting signal, ensures the stability that unmanned plane control system controls;
Further, described electrical verification sensor is by Information Receiving Circuits, and differential circuit and filtering circuit composition, for the acquisition and processing of electrified body electric signal;
Further, the shape that described wire touches line device is claw-like, and claw-like type wire touches line device and conductive contact to be measured is reliable and stable, is convenient to the monitoring whether electrified body is charged;
Further, described wire touches line device and is made up of carbon fiber guiding electric material, and quality is light, can not cause damage when contacting to electrified body;
Further, described high-altitude Signal Monitor is made up of the LED of high brightness and sounder.
The utility model beneficial effect compared to existing technology:
The utility model electrical verification is safe and reliable, significantly reduces the work of workman, simple to operate.Utilize unmanned air vehicle technique and wireless electrical verification technology, realize the contactless special minute vehicle electrical verification of human body, described can avoid that intensity of workers is large, operation inconvenience, potential safety hazard are large, electrical verification sensitivity and the low problem of reliability, guarantee between transmission line of electricity or electrical equipment safety.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Fig. 2 is the fundamental diagram of the utility model electrical verification and transmitter module.
Fig. 3 is the fundamental diagram of the utility model receiver module.
Fig. 4 is the circuit diagram of the utility model electrical verification sensor.
Fig. 5 is the fundamental diagram of the utility model image pick-up device system.
Fig. 6 is the structural representation of the utility model double-enclosure shielding box.
Embodiment
Below in conjunction with accompanying drawing, the utility model is described in further detail.
As shown in Figure 1, the unmanned electroscope of high pressure microminiature, comprises unmanned plane 1, strong-electromagnetic field interval shielding wire 2, electrical verification system 3, image pick-up device system 4 and wire touches line device 5.
As shown in Figure 1, 2, the bottom of unmanned plane 1 fixedly mounts the interval shielding wire 2 of strong-electromagnetic field, electrical verification and transmitter module 7 and wire touches line device 5 in turn; The interval shielding wire 2 of strong-electromagnetic field makes unmanned plane control system away from high pressure or UHV (ultra-high voltage) electrified body strong-electromagnetic field segment part, avoids the transmitting and receiving affecting signal, ensures the stability that unmanned plane control system controls; The shape that wire touches line device 5 is claw-like, claw-like type wire touches line device and conductive contact to be measured is reliable and stable, is convenient to the monitoring whether electrified body is charged, and wire touches line device and is made up of carbon fiber guiding electric material, quality is light, can not cause damage when contacting to electrified body.
As shown in Figure 1, 2, 3, electrical verification system 3 comprises electrical verification and transmitter module 7 and receiver module 13; Electrical verification and transmitter module 7 are made up of electrical verification sensor 8, amplifying circuit 9, coding circuit 10, radio transmitter 11 and high-altitude Signal Monitor 12; Described high-altitude Signal Monitor 12 is made up of the LED of high brightness and sounder; Receiver module 13 is made up of wireless receiving module 14, decoding scheme 15, unmanned aerial vehicle controller 16 and information display 17; Wire touches line device 5 and is electrically connected with electrical verification sensor 8.
As shown in Figure 4, electrical verification sensor 8 is by Information Receiving Circuits, and differential circuit and filtering circuit composition, for the acquisition and processing of electrified body 6 electric signal.
As shown in Figure 1,5, the side of unmanned plane 1 bottom is fixedly installed image pick-up device system 4, and image pick-up device system 4 comprises shooting information sensor 18, transmission circuit 19, computer control system 20 and actuator 21.
As shown in Figure 6, for the strong-electromagnetic field of prevention under high pressure and UHV (ultra-high voltage) is to the interference of electroscope circuit, electrical verification and transmitter module 7 are positioned in enclosed external shield box 22 and enclosed inner screening box 23, thus form double layer screen; Wherein external shield box 22 one end and wire touch line device 5 and are electrically connected, and external shield box 22 other end is electrically connected with electrical verification sensor 8, external shield box 22 and electrified body 6 same current potential during electrical verification, inner screening box 23 with " " be connected; Insulation voltage between inner screening box 23 and external shield box 24 is 50V, and inner screening box 23 and external shield box 24 are all made up of the thin iron of conductive magneto-conductive material.Radio transmitter 11 is by launching electrical verification information by inner screening box 23 and the interior electroscope remote-transmitter antenna 24 of drawing of external shield box 24; Electroscope remote-transmitter antenna 24 is insulating sleeve.
Existing composition graphs 1,2,3,4 and 5 describes electrical verification operating process of the present utility model:
The first step: utilize the image pick-up device system 4 on unmanned plane 1 to locate wire 6 to be measured, after the position of wire 6 to be measured is determined, makes the wire on unmanned plane 1 touch line device 5 and contacts with wire 6 is stable.
Second step: wire 6 and wire touch line device 5 and formed and be electrically connected, voltage signal in wire 6 enters in electrical verification on unmanned plane 1 and transmitter module 7, after electrical verification sensor 8, amplifying circuit 9 process, enter in the module and high-altitude Signal Monitor 12 be made up of coding circuit 10 and radio transmitter 11 respectively, described high-altitude Signal Monitor 12 is made up of the LED of high brightness and sounder, can show high-voltage signal and the early warning to high-voltage signal; Electrical verification information is transmitted in receiver module 13 by coding circuit 10 and radio transmitter 11, receiver module 13 receives electrical verification information, electrical verification information through amplifying and decodes transport, delivers to unmanned aerial vehicle controller 16 by interface circuit and information display 17 carries out result display again.
In sum, these are only preferred embodiment of the present utility model, be not intended to limit protection domain of the present utility model.All within spirit of the present utility model and principle, any amendment done, equivalent replacement, improvement etc., all should be included within protection domain of the present utility model.
Claims (6)
1. the unmanned electroscope of high pressure microminiature, is characterized in that: comprise unmanned plane (1), the interval shielding wire (2) of strong-electromagnetic field, electrical verification system (3), image pick-up device system (4) and wire and touch line device (5); The bottom of unmanned plane (1) fixedly mounts the interval shielding wire (2) of strong-electromagnetic field, electrical verification and transmitter module (7) in turn and wire touches line device (5); Electrical verification system (3) comprises electrical verification and transmitter module (7) and receiver module (13); Electrical verification and transmitter module (7) are made up of electrical verification sensor (8), amplifying circuit (9), coding circuit (10), radio transmitter (11) and high-altitude Signal Monitor (12); Receiver module (13) is made up of wireless receiving module (14), decoding scheme (15), unmanned aerial vehicle controller (16) and information display (17); Wire touches line device (5) and is electrically connected with electrical verification sensor (8); The side of unmanned plane (1) bottom is fixedly installed image pick-up device system (4), and image pick-up device system (4) comprises shooting information sensor (18), transmission circuit (19), computer control system (20) and actuator (21).
2. the unmanned electroscope of high pressure microminiature according to claim 1, is characterized in that: described electrical verification system (3) is positioned in enclosed external shield box (22) and enclosed inner screening box (23); Wherein external shield box (22) one end and wire touch line device (5) and are electrically connected, and external shield box (22) other end is electrically connected with electrical verification sensor (8), inner screening box (23) with " " be connected; Insulation voltage between inner screening box (23) and external shield box (24) is 50V, and inner screening box (23) and external shield box (24) are all made up of the thin iron of conductive magneto-conductive material.
3. the unmanned electroscope of high pressure microminiature according to claim 1, is characterized in that: described radio transmitter (11) is by launching electrical verification information by the interior electroscope remote-transmitter antenna (24) of drawing of inner screening box (23) and external shield box (24); Electroscope remote-transmitter antenna (24) is insulating sleeve.
4. the unmanned electroscope of high pressure microminiature according to claim 1, is characterized in that: described electrical verification sensor (8) is made up of Information Receiving Circuits, differential circuit and filtering circuit.
5. the unmanned electroscope of high pressure microminiature according to claim 1, is characterized in that: the shape that described wire touches line device (5) is claw-like.
6. the unmanned electroscope of high pressure microminiature according to claim 1, is characterized in that: described high-altitude Signal Monitor (12) is made up of LED and sounder.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420486229.6U CN204028208U (en) | 2014-08-27 | 2014-08-27 | The unmanned electroscope of high pressure microminiature |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420486229.6U CN204028208U (en) | 2014-08-27 | 2014-08-27 | The unmanned electroscope of high pressure microminiature |
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| Publication Number | Publication Date |
|---|---|
| CN204028208U true CN204028208U (en) | 2014-12-17 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420486229.6U Expired - Fee Related CN204028208U (en) | 2014-08-27 | 2014-08-27 | The unmanned electroscope of high pressure microminiature |
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| CN (1) | CN204028208U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104181377A (en) * | 2014-08-27 | 2014-12-03 | 李明明 | High-voltage ultra-small unmanned electroscope |
| CN105929219A (en) * | 2016-05-10 | 2016-09-07 | 保定瑞隆电力器材有限公司 | Improved full loop electroscope and method for controlling same |
| CN109470909A (en) * | 2018-06-21 | 2019-03-15 | 国网浙江江山市供电有限公司 | Distribution overhead line electroscope based on unmanned plane |
-
2014
- 2014-08-27 CN CN201420486229.6U patent/CN204028208U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104181377A (en) * | 2014-08-27 | 2014-12-03 | 李明明 | High-voltage ultra-small unmanned electroscope |
| CN105929219A (en) * | 2016-05-10 | 2016-09-07 | 保定瑞隆电力器材有限公司 | Improved full loop electroscope and method for controlling same |
| CN105929219B (en) * | 2016-05-10 | 2018-10-26 | 保定瑞隆电力器材有限公司 | A kind of improved full loop electroscope and its control method |
| CN109470909A (en) * | 2018-06-21 | 2019-03-15 | 国网浙江江山市供电有限公司 | Distribution overhead line electroscope based on unmanned plane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20141217 Termination date: 20170827 |
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| CF01 | Termination of patent right due to non-payment of annual fee |