CN204895854U - Aircraft is patrolled and examined to high pressure overhead wire intelligence - Google Patents
Aircraft is patrolled and examined to high pressure overhead wire intelligence Download PDFInfo
- Publication number
- CN204895854U CN204895854U CN201520689028.0U CN201520689028U CN204895854U CN 204895854 U CN204895854 U CN 204895854U CN 201520689028 U CN201520689028 U CN 201520689028U CN 204895854 U CN204895854 U CN 204895854U
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- drain pan
- motor
- aircraft
- high voltage
- support beam
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Abstract
The utility model relates to an aircraft is patrolled and examined to high pressure overhead wire intelligence, a supporting beam's one end is connected with the drain pan, and a supporting beam upper end is equipped with the wire casing, and a supporting beam's the other end is equipped with the motor cabinet, installs the motor in the motor cabinet, and the screw is installed to the last axle head of motor, and the motor passes through holding screw to be fixed in the motor cabinet, and the supporting leg is installed to a supporting beam lower extreme, the solar panel upper shield is installed to the drain pan upper end, and the plug setting is in one side of solar panel upper shield lower extreme, and the jack setting is in the inside one side of drain pan, and the plug is connected with the jack, and remote -control receiving module is installed to one side of drain pan lower extreme, and department of drain pan lower extreme central authorities installs infrared camera, and the thermal imaging module is installed to the opposite side of drain pan lower extreme. The utility model discloses the structure is reliable, and is energy -concerving and environment -protective, tours degree of accuracy height, is convenient for to install and carry, and longer continuation of the journey ability improves transmission line and tours efficiency to can there be hidden danger by the high transmission line of discovery promptly and accurately, reduces maintainer's working strength.
Description
Technical field
The utility model relates to digital automation equipment, specifically a kind of high voltage overhead lines intelligent patrol detection aircraft.
Background technology
High pressure overhead power line is the sustainer of electric system, due to long transmission distance, branch is many, physical features is complicated on the way, awful weather, along with industrial expansion, production and domestic load are also presenting the trend increased progressively year by year, high power consumption sharply adds the pressure of supply line, and especially some overhead transmission lines are easy to all kinds of fault occurs.Once break down, will rely on and manually carry out troubleshooting and eliminating, the difficulty of handling failure is very large, can increase the working strength of power off time and maintainer, waste a large amount of manpower and materials.
Utility model content
The purpose of this utility model is for solving above-mentioned deficiency, a kind of high voltage overhead lines intelligent patrol detection aircraft is provided, use battery as the energy, and charge to battery by solar electrical energy generation, improve the flying power of aircraft, green non-pollution, and multiple sensors on bonding apparatus, to under varying environment and situation, can complete the task of the line walking to high pressure overhead power line comprehensively, accurately, indirect labor keeps in repair.
The purpose of this utility model is achieved through the following technical solutions:
Provide a kind of high voltage overhead lines intelligent patrol detection aircraft, one end of support beam is connected with drain pan, support beam upper end is provided with wire casing, the other end of support beam is provided with motor cabinet, in motor cabinet, electrical motor is installed, the upper axle head of electrical motor is provided with screw propeller, and electrical motor is fixed in motor cabinet by holding screw, and support beam lower end is provided with supporting leg; Drain pan upper end is provided with solar panels upper cover, plug is arranged on the side of solar panels upper cover lower end, jack is arranged on the side of bottom shell, plug is connected with jack, and the centre of bottom shell is provided with battery, and the opposite side of bottom shell is provided with flight control modules, drain pan circumferentially read-out is installed, the side of drain pan lower end is provided with remote control reception module, and drain pan lower end centre is provided with infrared camera, and the opposite side of drain pan lower end is provided with thermal imaging module.
Further, described solar panels upper cover is semicircular structure.
Further, described support beam side is provided with rectangular opening structure.
Further, described flight control modules is made up of Signal reception feedback unit, GPS locating module and control module.
Further, described thermal imaging module is made up of thermal imaging sensor and mount pad.
Further, described electrical motor is brushless motor.
The utility model has effect useful as follows: the utility model structure is reliable, energy-conserving and environment-protective, make an inspection tour accuracy high, be convenient to install and carry, longer continuation of the journey energy, improve patrolling transmission line efficiency, and hidden danger can be there is by the high transmission line of electricity of discovery promptly and accurately, reduce the working strength of service personnel.
Accompanying drawing explanation
In order to be illustrated more clearly in the utility model embodiment or technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment or description of the prior art below, apparently, accompanying drawing in the following describes is only embodiments more of the present utility model, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
The overall perspective view that Fig. 1 provides for the utility model embodiment;
What Fig. 2 provided for the utility model embodiment totally looks up structural representation;
The general internal structure schematic diagram that Fig. 3 provides for the utility model embodiment;
The solar panels upper cover perspective view that Fig. 4 provides for the utility model embodiment;
The flight control modules composition schematic diagram that Fig. 5 provides for the utility model embodiment;
Wherein, 1. solar panels upper cover, 1.1. plug, 2. drain pan, 3. support beam, 3.1. motor cabinet, 3.2. wire casing, 4. electrical motor, 5. screw propeller, 6. holding screw, 7. supporting leg, 8. thermal imaging module, 9. infrared camera, 10. remote control reception module, 11. batteries, 12. flight control modules, 13. jacks, 14. read-outs.
Detailed description of the invention
Below in conjunction with specific embodiment, such scheme is described further.Should to understand these embodiments be for illustration of the utility model instead of limit scope of the present utility model.The implementation condition adopted in embodiment can do further adjustment according to the condition of concrete producer, and not marked implementation condition is generally the condition in normal experiment.
Please refer to Fig. 1, the overall perspective view that Fig. 1 provides for the utility model embodiment, please refer to Fig. 2, what Fig. 2 provided for the utility model embodiment totally looks up structural representation, please refer to Fig. 3, the general internal structure schematic diagram that Fig. 3 provides for the utility model embodiment, please refer to Fig. 4, the solar panels upper cover perspective view that Fig. 4 provides for the utility model embodiment, please refer to Fig. 5, the flight control modules composition schematic diagram that Fig. 5 provides for the utility model embodiment.
In a kind of specific embodiment, provide a kind of high voltage overhead lines intelligent patrol detection aircraft, one end of support beam 3 is connected with drain pan 2, support beam 3 upper end is provided with wire casing 3.2, the other end of support beam 3 is provided with motor cabinet 3.1, is provided with electrical motor 4 in motor cabinet 3.1, and the upper axle head of electrical motor 4 is provided with screw propeller 5, electrical motor 4 is fixed in motor cabinet 3.1 by holding screw 6, and support beam 3 lower end is provided with supporting leg 7; Drain pan 2 upper end is provided with solar panels upper cover 1, plug 1.1 is arranged on the side of solar panels upper cover 1 lower end, jack 13 is arranged on the side of drain pan 2 inside, plug 1.1 is connected with jack 13, the centre of drain pan 2 inside is provided with battery 11, the opposite side of drain pan 2 inside is provided with flight control modules 12, drain pan 2 read-out 14 is circumferentially installed, the side of drain pan 2 lower end is provided with remote control reception module 10, drain pan 2 lower end centre is provided with infrared camera 9, and the opposite side of drain pan 2 lower end is provided with thermal imaging module 8.
Concrete working process, during on site fault clearing, tentatively determine the Position Approximate of faulty line, check whether surrounding exists the obstacle affecting aircraft flight, after confirmation, the electricity of aircraft is checked by read-out 14, the flying power of aircraft can be met, and whether the signal wiring of check flight device is fastening, then, by remote controller, aircraft is controlled, and utilize the control module in flight control modules 12 to control electrical motor 4, the flight in adjustment aircraft energy friction speed and direction, start thermal imaging module 8 and infrared camera 9 simultaneously, by shooting results, by transmission over radio in flight course, video shooting is transferred to ground, and utilize GPS locating module by Aerial vehicle position in position of fault, circuit damaged condition and position is determined after surface personnel analyzes, carrying implement carries out maintenance of track again, make whole troubleshooting and exclusion process simple and fast, reduce the working strength of maintainer, power off time is shortened greatly, loss is dropped to minimum.
Further, described solar panels upper cover 1 is semicircular structure, therefore, when patrolling and examining by day, be provided with solar panels by solar panels upper cover 1 to generate electricity, and electricity is filled with battery 11, improve the flying power of aircraft, and circular shape can increase the daylighting area of solar panels, and make monnolithic case more attractive in appearance.
Further, described support beam 3 side is provided with rectangular opening structure, therefore, alleviates the quality of aircraft, improves the flying power of aircraft.
Further, described flight control modules 12 is made up of Signal reception feedback unit, GPS locating module and control module.
Further, described thermal imaging module 8 is made up of thermal imaging sensor and mount pad.
Further, described electrical motor 4 is brushless motor, and each electrical motor 4 can control separately and drive, and therefore when turning to, regulating the different rotating speeds of each motor, realizing turning to of aircraft.
Finally it should be noted that the restriction of above embodiment only for illustration of the technical solution of the utility model but not to the utility model protection domain.Although be explained in detail the utility model with reference to preferred embodiment, those of ordinary skill in the art should be appreciated that and can modify to the technical solution of the utility model or equivalent replacement, and does not depart from essence and the scope of technical solutions of the utility model.
Claims (6)
1. a high voltage overhead lines intelligent patrol detection aircraft, it is characterized in that, one end of support beam is connected with drain pan, support beam upper end is provided with wire casing, the other end of support beam is provided with motor cabinet, is provided with electrical motor in motor cabinet, and the upper axle head of electrical motor is provided with screw propeller, electrical motor is fixed in motor cabinet by holding screw, and support beam lower end is provided with supporting leg; Drain pan upper end is provided with solar panels upper cover, plug is arranged on the side of solar panels upper cover lower end, jack is arranged on the side of bottom shell, plug is connected with jack, and the centre of bottom shell is provided with battery, and the opposite side of bottom shell is provided with flight control modules, drain pan circumferentially read-out is installed, the side of drain pan lower end is provided with remote control reception module, and drain pan lower end centre is provided with infrared camera, and the opposite side of drain pan lower end is provided with thermal imaging module.
2. a kind of high voltage overhead lines intelligent patrol detection aircraft as claimed in claim 1, it is characterized in that, described solar panels upper cover is semicircular structure.
3. a kind of high voltage overhead lines intelligent patrol detection aircraft as claimed in claim 1, it is characterized in that, described support beam side is provided with rectangular opening structure.
4. a kind of high voltage overhead lines intelligent patrol detection aircraft as claimed in claim 1, it is characterized in that, described flight control modules is made up of Signal reception feedback unit, GPS locating module and control module.
5. a kind of high voltage overhead lines intelligent patrol detection aircraft as claimed in claim 1, it is characterized in that, described thermal imaging module is made up of thermal imaging sensor and mount pad.
6. a kind of high voltage overhead lines intelligent patrol detection aircraft as claimed in claim 1, it is characterized in that, described electrical motor is brushless motor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520689028.0U CN204895854U (en) | 2015-09-08 | 2015-09-08 | Aircraft is patrolled and examined to high pressure overhead wire intelligence |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520689028.0U CN204895854U (en) | 2015-09-08 | 2015-09-08 | Aircraft is patrolled and examined to high pressure overhead wire intelligence |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204895854U true CN204895854U (en) | 2015-12-23 |
Family
ID=54918052
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520689028.0U Expired - Fee Related CN204895854U (en) | 2015-09-08 | 2015-09-08 | Aircraft is patrolled and examined to high pressure overhead wire intelligence |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204895854U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105610088A (en) * | 2016-02-26 | 2016-05-25 | 国网山东省电力公司蓬莱市供电公司 | Automatic inspection device for power device |
| CN108298080A (en) * | 2017-12-20 | 2018-07-20 | 易瓦特科技股份公司 | The method, system and device of rope ladder are hung on target cable based on earth station |
| CN108313286A (en) * | 2017-12-20 | 2018-07-24 | 易瓦特科技股份公司 | The method, system and device of rope ladder are hung based on unmanned plane |
| CN110112674A (en) * | 2019-05-13 | 2019-08-09 | 国电南瑞科技股份有限公司 | A kind of autonomous crusing robot of transmission line of electricity based on flight obstacle detouring and obstacle-detouring method |
-
2015
- 2015-09-08 CN CN201520689028.0U patent/CN204895854U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105610088A (en) * | 2016-02-26 | 2016-05-25 | 国网山东省电力公司蓬莱市供电公司 | Automatic inspection device for power device |
| CN108298080A (en) * | 2017-12-20 | 2018-07-20 | 易瓦特科技股份公司 | The method, system and device of rope ladder are hung on target cable based on earth station |
| CN108313286A (en) * | 2017-12-20 | 2018-07-24 | 易瓦特科技股份公司 | The method, system and device of rope ladder are hung based on unmanned plane |
| CN108313286B (en) * | 2017-12-20 | 2021-03-09 | 易瓦特科技股份公司 | Method, system and device for hanging rope ladder based on unmanned aerial vehicle |
| CN108298080B (en) * | 2017-12-20 | 2021-08-10 | 易瓦特科技股份公司 | Method, system and device for hanging rope ladder on target cable based on ground station |
| CN110112674A (en) * | 2019-05-13 | 2019-08-09 | 国电南瑞科技股份有限公司 | A kind of autonomous crusing robot of transmission line of electricity based on flight obstacle detouring and obstacle-detouring method |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20151223 Termination date: 20160908 |