CN206362918U - Remote control termination for altitude test wiring unmanned aerial vehicle platform - Google Patents
Remote control termination for altitude test wiring unmanned aerial vehicle platform Download PDFInfo
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- CN206362918U CN206362918U CN201621139346.0U CN201621139346U CN206362918U CN 206362918 U CN206362918 U CN 206362918U CN 201621139346 U CN201621139346 U CN 201621139346U CN 206362918 U CN206362918 U CN 206362918U
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- 238000012360 testing method Methods 0.000 title claims abstract description 42
- 239000000758 substrate Substances 0.000 claims description 12
- 238000012544 monitoring process Methods 0.000 claims description 6
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 3
- 229910052802 copper Inorganic materials 0.000 claims description 3
- 239000010949 copper Substances 0.000 claims description 3
- 238000009434 installation Methods 0.000 claims 1
- 238000002474 experimental method Methods 0.000 abstract description 13
- 238000013461 design Methods 0.000 abstract description 3
- 239000002184 metal Substances 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- 230000009194 climbing Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000001174 ascending effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
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- 238000005516 engineering process Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
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Abstract
The utility model is related to a kind of remote control termination for altitude test wiring unmanned aerial vehicle platform, the present apparatus is arranged on unmanned motor spindle, and termination includes three parts：Base, wiring link assembly and binding clip, base are fixed on the fuselage lower end of unmanned plane, and one end of wiring connecting rod is provided with base lower end, and the other end of wiring connecting rod installs binding clip.Using device of the present utility model, by manipulating unmanned plane, high-altitude is arrived into experiment cable lifting, and be reliably connected cable with high-altitude circuit and equipment by manipulating unmanned plane mechanical arm, just can realize that experiment is safe and reliable must be carried out, the design can simplify wiring program and time, it is often more important that ensure that the security of field test personnel and equipment.
Description
Technical field
The utility model belongs to high-altitude power test wiring technique, and especially a kind of altitude test wiring unmanned plane that is used for is put down
The remote control termination of platform.
Background technology
Power equipment experiment in high-altitude is defined as that test height is higher, and testing crew is difficult to enter by methods such as climbing or ascending stairs
The experiment of row wiring test.Type testing is 220kV framework voltage transformer commissioning tests, and its testing equipment is main by testing
The compositions such as instrument, pressure regulator, standard mutual inductor, subject transformer, load box.Standard mutual inductor needs with subject transformer during experiment
Be reliably connected by a test wire, due on 220kV voltage transformers shaft tower framework installed outdoors, because setting height(from bottom) compared with
Height, needs technical staff to climb operation during wiring, the security incident that personal height falls occurs often.Arm can be passed through in addition
Personnel are raised to high-altitude wiring by car, but are due to nearby there is charging operation high voltage bus, the danger that there is personnel's electric shock, also
There are some newly-built transformer station's test site road surfaces not repair also, vehicle cannot be introduced into transformer station test site.
Current unmanned air vehicle technique is ripe to be applied to civilian, military multiple fields, and its platform lifting capacity is constantly lifted, can
To carry the plurality of devices such as shooting, fire-fighting, ground remote control system can monitor high-altitude picture in real time by camera device, and to flat
Platform equipment remote-control is operated.By designing a remote-controlled termination suitable for unmanned aerial vehicle platform, pass through ground remote control system
Monitoring in real time and control, primary equipment test wire is reliably connected on the power equipment of high-altitude, it is ensured that high-altitude power equipment is tested
It is safe and smooth to carry out.
Utility model content
The purpose of this utility model be to overcome in place of the deficiencies in the prior art there is provided one kind be used for altitude test wiring without
The remote control termination of people's machine platform, the difficult situation design of wiring, ensure that experiment when being for the test of high-altitude power equipment
Personnel without climbing shaft tower in the case of test wire is stepped up with transformer metal end, the personnel of effectively prevent ascend a height the danger of operation
It is dangerous, while ensureing field test reliability.
The utility model solves its technical problem and takes following technical scheme to realize：
A kind of remote control termination for altitude test wiring unmanned aerial vehicle platform, the present apparatus is arranged on unmanned motor spindle,
It is characterized in that：Termination include three parts：Base, wiring link assembly and binding clip, base are fixed on unmanned plane
Fuselage lower end, one end of wiring connecting rod is installed in base lower end, the other end of wiring connecting rod installs binding clip；
Base includes substrate, electric-controlled box, bolt, electro-motor and rotating shaft, and substrate is a lightweight rectangular flat, in substrate
Middle part is coaxially installed with electric-controlled box, the substrate of electric-controlled box surrounding is provided with multiple bolts vertically installed uniformly at intervals, and this is more
Individual bolt is used for the fuselage for connecting unmanned plane；Signal receiver and electro-motor, the output of electro-motor are installed in electric-controlled box
Axle Driven by Coaxial is provided with a rotating shaft being vertically arranged, and rotating shaft lower end stretches out electric-controlled box and is coaxially fixed with wiring connection rod set
Part；
Wiring link assembly includes bearing bracket stand, comprehensive control shaft and expansion link, and a bearing is packed in rotating shaft lower end
The upper center of frame, is hinged with an expansion link, in the external part of expansion link in bearing bracket stand lower end inside by comprehensive control shaft
End is installed by binding clip.
Moreover, the binding clip includes location-plate, pull bar, jig arm, positioning drawing plate and locating shaft, one end of location-plate is consolidated
Mounted in the telescopic end end of expansion link, the other end of location-plate is symmetrically hinged with one end of two pull bars, two pull bars it is another
One end is cut with scissors mounted in the middle part of a jig arm respectively, and two arm clamping structures are symmetrical；Positioning drawing is hinged with below one end of jig arm
Plate, two positioning drawing plates are mounted in location-plate lower end by a positioning axial symmetry hinge respectively；
Moreover, the other end of the jig arm is fixed with plush copper.
Moreover, the unmanned plane uses the branched rotor of radial equipartition, unmanned plane on multi-rotor unmanned aerial vehicle, the fuselage of unmanned plane
Fuselage lower end fuselage support is installed, monitoring unmanned device is installed on the fuselage of unmanned plane, in the fuselage of unmanned plane
Bottom is installed by this termination.
Advantage of the present utility model and good effect are：
Using device of the present utility model, by manipulating unmanned plane, high-altitude is arrived into experiment cable lifting, and by manipulating nothing
Cable is reliably connected by man-machine mechanical arm with high-altitude circuit and equipment, and just can realize that experiment is safe and reliable must be carried out, and the design can
To simplify wiring program and time, it is often more important that ensure that the security of field test personnel and equipment.
Brief description of the drawings
Fig. 1 is unmanned plane mounting structure schematic diagram；
Fig. 2 is termination schematic diagram；
Fig. 3 is another view of termination.
Embodiment
Below in conjunction with the accompanying drawings and the utility model is described in further detail by specific embodiment, following examples are to retouch
The property stated, be not limited, it is impossible to limit protection domain of the present utility model with this.
A kind of remote control termination for altitude test wiring unmanned aerial vehicle platform, the unmanned plane of the present embodiment is using many rotations
The branched rotor 2 of radial equipartition on wing unmanned plane, the fuselage 1 of unmanned plane, the fuselage lower end of unmanned plane is provided with fuselage support 4,
Monitoring unmanned device (camera or Airborne Camera, figure not shown in) is installed, camera can be real on the fuselage of unmanned plane
When collection unmanned plane position shooting picture be transferred to ground, be easy to technical staff's reference, so as to accurately control unmanned plane,
The bottom of unmanned aerial vehicle body is slab construction, installs this termination 3 in the fuselage bottom of unmanned plane, termination is than fuselage branch
The length of frame is short, prevents when unmanned plane from landing termination is bottomed out to cause damage.
The concrete structure of the termination includes three parts：Base, wiring link assembly and binding clip, base are fixed
In the fuselage lower end of unmanned plane, one end of wiring connecting rod is installed in base lower end, the other end of wiring connecting rod installs binding clip,
The base, wiring connecting rod and binding clip are provided with connection, and control wiring action, the wiring construction of circuit uses existing
Some conventional connections modes, are not described in detail.
The base includes substrate 301, electric-controlled box 302, bolt 303, electro-motor and rotating shaft, and substrate is a light rectangular
Shape flat board, in a substrate portion be coaxially installed with electric-controlled box, the substrate of electric-controlled box surrounding to be provided with uniformly at intervals and multiple vertically wear
The bolt of dress, the plurality of bolt is used for the fuselage for connecting unmanned plane；Signal receiver and electronic horse are installed in the electric-controlled box
Reach, the output shaft Driven by Coaxial of electro-motor is provided with a rotating shaft being vertically arranged, and electric-controlled box is stretched out and coaxial in rotating shaft lower end
Wiring link assembly is fixed with, electrical motor driven wiring link assembly is horizontally rotated, so that termination can be by
The horizontal direction for realizing package unit according to control instruction is rotated；
Wiring link assembly includes bearing bracket stand 304, comprehensive control shaft (non-label) and expansion link 305, under rotating shaft
End is packed in the upper center of a bearing bracket stand, and the bearing bracket stand is the C glyph frameworks of a lower ending opening, logical in bearing bracket stand lower end inside
Cross comprehensive control shaft and be hinged with an expansion link 305, expansion link is driven rotation in bearing bracket stand and expansion link is experienced certainly
Control is stretched, and binding clip is installed in the external part end of expansion link.Binding clip is arranged on wiring connecting rod by Spring connector plug
On, wiring link assembly can carry out all-direction rotation and flexible according to control instruction control binding clip, by controlling wiring to connect
Test wire chuck is extracted/inserted to bar assembly, can also have by controlling opened/closed test wire chuck on test wire chuck
Fasten test wire terminal 306；
Binding clip includes location-plate 310, pull bar 308, jig arm 307, positioning drawing plate 309 and locating shaft 312, location-plate
One end is packed in the telescopic end end of expansion link, and the other end of location-plate is symmetrically hinged with one end of two pull bars, this two drawings
The other end of bar is cut with scissors mounted in the middle part of a jig arm respectively, and two arm clamping structures are symmetrical；One is hinged with below one end of jig arm
Positioning drawing plate, two positioning drawing plates are mounted in location-plate lower end by a positioning axial symmetry hinge respectively；The other end of jig arm is solid
Strengthen firm grip equipped with plush copper 311.
Test wire is fastened on chuck before experiment, unmanned plane is operated by ground staff by monitoring system and is added in chuck
In altitude test facility metal end, being reliably connected for test wire and altitude plant is realized, connection is the test wire other end on ground
Can guarantee test smoothly carry out safely.
The circuit structure of the present apparatus can be realized using the conventional connections of prior art, be not described in detail.
Concretely comprising the following steps for wiring is carried out using the present apparatus：
(1) termination is installed on unmanned plane；
Termination is arranged on unmanned motor spindle, and termination is the special high-altitude wiring dress suitable for unmanned aerial vehicle platform
Put, including supervising device and connector assembly, control of the ground control personnel by remote control realization to the device, including left and right/
Above-below direction is rotated, junction pole elongation/retraction, binding clip opened/closed etc.；
(2) control unmanned plane reaches wiring position：Test wire is first fixed on the binding clip of termination by testing crew
On head, near control unmanned plane during flying to high-altitude power equipment wiring metal end, technical staff is existed by monitoring unmanned device
Ground observation altitude plant surrounding environment, chooses best safety position；
(3) high-altitude wiring：Choose behind best safety position, chuck opening is clamped to altitude test and set by control termination
Standby wiring metal end, after subsequent technical staff is confirmed firmly by supervising device, control unmanned plane flies back ground；
(4) tested on ground：Technical staff completes connection of the test wire other end with testing relevant device on ground and opened
Exhibition experiment；
(5) experiment is completed, wiring is pulled down：After the completion of experiment, control unmanned plane flies back former high empty position, remote control termination
The wiring collet being clipped in equipment is removed by junction pole, control unmanned plane is flown back ground, and experiment is completed.
Although disclosing embodiment of the present utility model and accompanying drawing for the purpose of illustration, those skilled in the art can be with
Understand：Do not departing from spirit and scope of the present utility model, it is various replace, change and modifications all be it is possible, therefore, this reality
Embodiment and accompanying drawing disclosure of that are not limited to new scope.
Claims (4)
1. a kind of remote control termination for altitude test wiring unmanned aerial vehicle platform, the present apparatus is arranged on unmanned motor spindle, its
It is characterised by：Termination include three parts：Base, wiring link assembly and binding clip, base are fixed on unmanned plane
Fuselage lower end, one end of wiring connecting rod is provided with base lower end, and the other end of wiring connecting rod installs binding clip；
Base includes substrate, electric-controlled box, bolt, electro-motor and rotating shaft, and substrate is a lightweight rectangular flat, in a substrate portion
It is coaxially installed with electric-controlled box, the substrate of electric-controlled box surrounding and is provided with multiple bolts vertically installed uniformly at intervals, the plurality of spiral shell
Bolt is used for the fuselage for connecting unmanned plane；Signal receiver and electro-motor are installed, the output shaft of electro-motor is same in electric-controlled box
Axle drive installation has a rotating shaft being vertically arranged, and rotating shaft lower end stretches out electric-controlled box and is coaxially fixed with wiring link assembly；
Wiring link assembly includes bearing bracket stand, comprehensive control shaft and expansion link, and a bearing bracket stand is packed in rotating shaft lower end
Upper center, an expansion link is hinged with bearing bracket stand lower end inside by comprehensive control shaft, in the external part end of expansion link
Binding clip is installed.
2. the remote control termination according to claim 1 for altitude test wiring unmanned aerial vehicle platform, it is characterised in that：
The binding clip includes location-plate, pull bar, jig arm, positioning drawing plate and locating shaft, and one end of location-plate is packed in expansion link
Telescopic end end, the other end of location-plate is symmetrically hinged with one end of two pull bars, and the other end of two pull bars cuts with scissors dress respectively
At the middle part of a jig arm, two arm clamping structures that two pull bars cut with scissors dress are symmetrical；It is hinged with below one end of jig arm certain
Position arm-tie, two positioning drawing plates are mounted in location-plate lower end by a positioning axial symmetry hinge respectively.
3. the remote control termination according to claim 2 for altitude test wiring unmanned aerial vehicle platform, it is characterised in that：
The other end of the jig arm is fixed with plush copper.
4. the remote control termination according to claim 1 for altitude test wiring unmanned aerial vehicle platform, it is characterised in that：
The unmanned plane uses the branched rotor of radial equipartition on multi-rotor unmanned aerial vehicle, the fuselage of unmanned plane, the fuselage lower end peace of unmanned plane
Equipped with fuselage support, monitoring unmanned device is installed on the fuselage of unmanned plane, installs and originally connects in the fuselage bottom of unmanned plane
Line apparatus.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621139346.0U CN206362918U (en) | 2016-10-20 | 2016-10-20 | Remote control termination for altitude test wiring unmanned aerial vehicle platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621139346.0U CN206362918U (en) | 2016-10-20 | 2016-10-20 | Remote control termination for altitude test wiring unmanned aerial vehicle platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206362918U true CN206362918U (en) | 2017-07-28 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621139346.0U Active CN206362918U (en) | 2016-10-20 | 2016-10-20 | Remote control termination for altitude test wiring unmanned aerial vehicle platform |
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| Country | Link |
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| CN (1) | CN206362918U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110702950A (en) * | 2019-09-06 | 2020-01-17 | 广西电网有限责任公司电力科学研究院 | Wiring clamp hung and taken by unmanned aerial vehicle |
| CN111463710A (en) * | 2020-05-15 | 2020-07-28 | 广东电网有限责任公司东莞供电局 | Temporary maintenance method for overhead transmission line and high-voltage conducting wire assembly |
| CN112243422A (en) * | 2018-04-16 | 2021-01-19 | 普瑞佛姆兰工业有限公司 | Unmanned aerial vehicle for mounting a clamp onto an electric power line |
| CN112782432A (en) * | 2020-12-25 | 2021-05-11 | 广东电网有限责任公司 | Wiring device and method for high-voltage circuit breaker test |
| CN114715400A (en) * | 2022-05-06 | 2022-07-08 | 薛继斌 | High-altitude operation equipment based on tethered unmanned aerial vehicle and control method thereof |
| CN116908499A (en) * | 2023-09-11 | 2023-10-20 | 山西天禄电力工程有限公司 | Junction device for electric power intelligent test |
-
2016
- 2016-10-20 CN CN201621139346.0U patent/CN206362918U/en active Active
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112243422A (en) * | 2018-04-16 | 2021-01-19 | 普瑞佛姆兰工业有限公司 | Unmanned aerial vehicle for mounting a clamp onto an electric power line |
| US11905015B2 (en) | 2018-04-16 | 2024-02-20 | Preformed Line Products Co. | Mounting assembly for mounting clamp |
| CN110702950A (en) * | 2019-09-06 | 2020-01-17 | 广西电网有限责任公司电力科学研究院 | Wiring clamp hung and taken by unmanned aerial vehicle |
| CN111463710A (en) * | 2020-05-15 | 2020-07-28 | 广东电网有限责任公司东莞供电局 | Temporary maintenance method for overhead transmission line and high-voltage conducting wire assembly |
| CN112782432A (en) * | 2020-12-25 | 2021-05-11 | 广东电网有限责任公司 | Wiring device and method for high-voltage circuit breaker test |
| CN114715400A (en) * | 2022-05-06 | 2022-07-08 | 薛继斌 | High-altitude operation equipment based on tethered unmanned aerial vehicle and control method thereof |
| CN116908499A (en) * | 2023-09-11 | 2023-10-20 | 山西天禄电力工程有限公司 | Junction device for electric power intelligent test |
| CN116908499B (en) * | 2023-09-11 | 2023-12-05 | 山西天禄电力工程有限公司 | Junction device for electric power intelligent test |
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