CN204945292U - One patrols and examines rotor wing unmanned aerial vehicle - Google Patents
One patrols and examines rotor wing unmanned aerial vehicle Download PDFInfo
- Publication number
- CN204945292U CN204945292U CN201520643718.2U CN201520643718U CN204945292U CN 204945292 U CN204945292 U CN 204945292U CN 201520643718 U CN201520643718 U CN 201520643718U CN 204945292 U CN204945292 U CN 204945292U
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- CN
- China
- Prior art keywords
- guide rail
- horizontal guide
- semicircular ring
- unmanned plane
- aerial vehicle
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Abstract
The utility model discloses one and patrol and examine rotor wing unmanned aerial vehicle, comprise unmanned plane, along described unmanned plane middle vertical plane symmetry, a pair horizontal guide rail is installed, described horizontal guide rail material is insulating material, conduction joint strip is connected with bottom described horizontal guide rail, two conduction joint strips are electrically connected with the voltage detection unit in unmanned plane, each horizontal guide rail are all provided with a running gear, each described running gear are provided with a hall sensor component.The utility model owing to being provided with a pair horizontal guide rail on unmanned plane, between two wires stopping dropping on hi-line by controlling unmanned plane, the conduction joint strip of both sides and two conductive contact, the voltage on hi-line can be detected easily, and the hall sensor component on horizontal guide rail can detect the electric current on hi-line, this is used to patrol and examine rotor wing unmanned aerial vehicle, without the need to manually climbing high-tension line tower, testing staff's Distance High Voltage Electricity Transfer distance, non-contact electric is dangerous.
Description
Technical field
The utility model relates to unmanned air vehicle technique field, particularly relates to one and patrols and examines rotor wing unmanned aerial vehicle.
Background technology
At small-sized depopulated helicopter civil area, it is the airborne application of one the most common that unmanned plane is taken photo by plane, in prior art, hi-line needs regular visit, or when there is electric leakage or partial short-circuit in hi-line, need the place on line being calculated electric leakage or short circuit by the voltage on detection line or electric current, and hi-line detects now basic by manual detection, detecting workman has Danger Electric shock risk.
Utility model content
The utility model mainly solves technical matters existing in prior art, thus provides a kind of security performance high, detects and patrols and examines rotor wing unmanned aerial vehicle quickly and easily.
Above-mentioned technical matters of the present utility model is mainly solved by following technical proposals:
The one that the utility model provides patrols and examines rotor wing unmanned aerial vehicle, comprise unmanned plane, along described unmanned plane middle vertical plane symmetry, a pair horizontal guide rail is installed, described horizontal guide rail material is insulating material, conduction joint strip is connected with bottom described horizontal guide rail, two conduction joint strips are electrically connected with the voltage detection unit in unmanned plane, each horizontal guide rail are all provided with a running gear, each described running gear are provided with a hall sensor component.
Further, described hall sensor component comprises the insulation C type frame be connected with running gear, described insulation C type frame top and bottom are hinged with conduction semicircular ring and lower conduction semicircular ring respectively, described upper conduction semicircular ring and lower conduction semicircular ring inner ring are also provided with insulation course, and in the middle part of described insulation C type frame also level be provided with spring fitting cylinder, in spring fitting cylinder, Compress Spring is installed, described Compress Spring holds out against one end of conduction semicircular ring and one end of lower conduction semicircular ring, and upper conduction semicircular ring and lower conduction semicircular ring are also electrically connected with Hall current detecting unit.
Further, described horizontal guide rail is arranged on above described unmanned plane center of gravity.
Further, described horizontal guide rail is I-beam, and described running gear comprises roller and motor, be equipped with a described roller, and one of them roller is connected in the groove of the described I-beam left and right sides with motor.
Further, described motor and hall sensor component are distributed in both sides before and after horizontal guide rail.
The beneficial effects of the utility model are: owing to being provided with a pair horizontal guide rail on unmanned plane, between two wires stopping dropping on hi-line by controlling unmanned plane, the conduction joint strip of both sides and two conductive contact, the voltage on hi-line can be detected easily, and the hall sensor component on horizontal guide rail can detect the electric current on hi-line, this is used to patrol and examine rotor wing unmanned aerial vehicle, without the need to manually climbing high-tension line tower, testing staff's Distance High Voltage Electricity Transfer distance, non-contact electric is dangerous.
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.
Fig. 1 is the structural representation that the utility model patrols and examines rotor wing unmanned aerial vehicle;
Fig. 2 is the partial enlarged view at I place in Fig. 1;
Fig. 3 is structural representation when conduction semicircular ring and lower conduction semicircular ring close in I place in Fig. 1;
Fig. 4 be in Fig. 1 A to partial schematic diagram.
Embodiment
Below in conjunction with accompanying drawing, preferred embodiment of the present utility model is described in detail, to make advantage of the present utility model and feature can be easier to be readily appreciated by one skilled in the art, thus more explicit defining is made to protection domain of the present utility model.
Consult shown in Fig. 1, one of the present utility model patrols and examines rotor wing unmanned aerial vehicle, comprise unmanned plane 1, along unmanned plane 1 middle vertical plane symmetry, a pair horizontal guide rail 2 is installed, horizontal guide rail 2 material is insulating material, is connected with conduction joint strip 3, two conduction joint strip 3 and is electrically connected with the voltage detection unit 4 in unmanned plane bottom horizontal guide rail 2, each horizontal guide rail 2 is all provided with a running gear 5, each running gear 5 is provided with a hall sensor component 6.Owing to being provided with a pair horizontal guide rail 2 on unmanned plane 1, between two wires 7 stopping dropping on hi-line by controlling unmanned plane 1, the conduction joint strip 3 of both sides contacts with two wires 7, the voltage on hi-line can be detected easily, and the hall sensor component 6 on horizontal guide rail 2 can detect the electric current on hi-line, uses this to patrol and examine rotor wing unmanned aerial vehicle, without the need to manually climbing high-tension line tower, testing staff's Distance High Voltage Electricity Transfer distance, non-contact electric is dangerous.
Consult Fig. 2, shown in Fig. 3, hall sensor component 6 comprises the insulation C type frame 61 be connected with running gear 5, insulation C type frame 61 top and bottom are hinged with conduction semicircular ring 62 and lower conduction semicircular ring 63 respectively, upper conduction semicircular ring 62 and lower conduction semicircular ring 63 inner ring are also provided with insulation course 64, and in the middle part of insulation C type frame 61 also level be provided with spring fitting cylinder 65, Compress Spring 66 is installed in spring fitting cylinder 65, Compress Spring 66 holds out against one end of conduction semicircular ring 62 and one end of lower conduction semicircular ring 63, and upper conduction semicircular ring 62 and lower conduction semicircular ring 63 are also electrically connected with Hall current detecting unit 67.When unmanned plane needs the electric current detecting hi-line, move to unmanned plane direction by driving running gear 5, upper conduction semicircular ring 62 and lower conduction semicircular ring 63 start to touch wire 7, upper conduction semicircular ring 62 and lower conduction semicircular ring 63 are compressed to Compress Spring 66 direction by wire 7, and upper conduction semicircular ring 62 and lower conduction semicircular ring 63 begin to rotate along hinged establishing by cable, until upper conduction semicircular ring 62 and lower conduction semicircular ring 63 are encircled into an annular electric conductor, your current detecting unit 67 detects the induction current in this annular electric conductor, thus the electric current detected in wire 7.After detection completes, running gear 5 moves to horizontal guide 2 two ends, and Compress Spring 66 is by one end jack-up of upper conduction semicircular ring 62 and lower conduction semicircular ring 63, and wire 7 shifts out from this annular electric conductor.
Preferably, horizontal guide rail 2 is arranged on above unmanned plane 1 center of gravity.When unmanned plane stops dropping between two wires 7, good stability.Also can not roll when being subject to wind.
Consult shown in Fig. 4, horizontal guide rail 2 is I-beam, and running gear 5 comprises roller 51 and motor 52, is equipped with a roller 51 in the groove of the I-beam left and right sides, and one of them roller 51 is connected with motor 52.This motor 52 can directly be connected with roller 51, also can be connected with roller 51 by gear.In order to keep the stable of center of gravity, motor 52 and hall sensor component 6 are distributed in both sides before and after horizontal guide rail 2.
Above, be only embodiment of the present utility model, but protection domain of the present utility model is not limited thereto, any change of expecting without creative work or replacement, all should be encompassed within protection domain of the present utility model.Therefore, the protection domain that protection domain of the present utility model should limit with claims is as the criterion.
Claims (5)
1. patrol and examine rotor wing unmanned aerial vehicle for one kind, comprise unmanned plane (1), it is characterized in that: along described unmanned plane (1) middle vertical plane symmetry, a pair horizontal guide rail (2) is installed, described horizontal guide rail (2) material is insulating material, described horizontal guide rail (2) bottom is connected with conduction joint strip (3), two conductions joint strip (3) are electrically connected with the voltage detection unit (4) in unmanned plane, each horizontal guide rail (2) is all provided with a running gear (5), each described running gear (5) is provided with a hall sensor component (6).
2. patrol and examine rotor wing unmanned aerial vehicle as claimed in claim 1, it is characterized in that: described hall sensor component (6) comprises the insulation C type frame (61) be connected with running gear (5), described insulation C type frame (61) top and bottom are hinged with conduction semicircular ring (62) and lower conduction semicircular ring (63) respectively, described upper conduction semicircular ring (62) and lower conduction semicircular ring (63) inner ring are also provided with insulation course (64), and described insulation C type frame (61) middle part also level be provided with spring fitting cylinder (65), Compress Spring (66) is installed in spring fitting cylinder (65), described Compress Spring (66) holds out against one end of conduction semicircular ring (62) and one end of lower conduction semicircular ring (63), and upper conduction semicircular ring (62) and lower conduction semicircular ring (63) are also electrically connected with Hall current detecting unit (67).
3. patrol and examine rotor wing unmanned aerial vehicle as claimed in claim 2, it is characterized in that: described horizontal guide rail (2) is arranged on above described unmanned plane (1) center of gravity.
4. patrol and examine rotor wing unmanned aerial vehicle as claimed in claim 3, it is characterized in that: described horizontal guide rail (2) is I-beam, described running gear (5) comprises roller (51) and motor (52), be equipped with a described roller (51) in the groove of the described I-beam left and right sides, and one of them roller (51) is connected with motor (52).
5. patrol and examine rotor wing unmanned aerial vehicle as claimed in claim 4, it is characterized in that: described motor (52) and hall sensor component (6) are distributed in both sides before and after horizontal guide rail (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520643718.2U CN204945292U (en) | 2015-08-24 | 2015-08-24 | One patrols and examines rotor wing unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520643718.2U CN204945292U (en) | 2015-08-24 | 2015-08-24 | One patrols and examines rotor wing unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204945292U true CN204945292U (en) | 2016-01-06 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520643718.2U Expired - Fee Related CN204945292U (en) | 2015-08-24 | 2015-08-24 | One patrols and examines rotor wing unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204945292U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106428558A (en) * | 2016-11-28 | 2017-02-22 | 北京交通大学 | Rail comprehensive inspection method based on air-rail double-purpose unmanned aerial vehicle |
| CN106494611A (en) * | 2016-11-28 | 2017-03-15 | 北京交通大学 | A kind of dual-purpose patrol unmanned machine of empty rail |
| CN109164306A (en) * | 2018-07-27 | 2019-01-08 | 国网山东省电力公司电力科学研究院 | The anti-touching line electric field probe of high sensitivity unmanned plane |
-
2015
- 2015-08-24 CN CN201520643718.2U patent/CN204945292U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106428558A (en) * | 2016-11-28 | 2017-02-22 | 北京交通大学 | Rail comprehensive inspection method based on air-rail double-purpose unmanned aerial vehicle |
| CN106494611A (en) * | 2016-11-28 | 2017-03-15 | 北京交通大学 | A kind of dual-purpose patrol unmanned machine of empty rail |
| CN106428558B (en) * | 2016-11-28 | 2018-06-01 | 北京交通大学 | A kind of track synthesis method for inspecting based on the dual-purpose unmanned plane of sky-rail |
| CN109164306A (en) * | 2018-07-27 | 2019-01-08 | 国网山东省电力公司电力科学研究院 | The anti-touching line electric field probe of high sensitivity 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: 20160106 Termination date: 20160824 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |