CN104882820B - A kind of device of the removing high-altitude circuit ribbon thing carried by aircraft - Google Patents
A kind of device of the removing high-altitude circuit ribbon thing carried by aircraft Download PDFInfo
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- CN104882820B CN104882820B CN201510282552.0A CN201510282552A CN104882820B CN 104882820 B CN104882820 B CN 104882820B CN 201510282552 A CN201510282552 A CN 201510282552A CN 104882820 B CN104882820 B CN 104882820B
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- guiding groove
- aircraft
- stock
- erecting bed
- heating wire
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Abstract
The present invention provides a kind of device of the removing high-altitude circuit ribbon thing carried by aircraft, and it is engaged with aircraft, including stock, the first guiding groove, the second guiding groove, electronic voltage controller, electric lead and heating wire；Wherein, one end of stock is provided with the erecting bed for being used for fixing aircraft, and the other end each extends over out the first guiding groove and the second guiding groove from its end face along away from erecting bed direction；Electronic voltage controller is fixed on stock, including voltage source；The two ends of heating wire are individually fixed on the first guiding groove and the second guiding groove, and are connected respectively with the two ends of electronic voltage controller by electric lead.Implement the present invention, coordinate with aircraft, its is easy to operate, easy popularization and do not have burning things which may cause a fire disaster potential safety hazard, improves operating efficiency and security.
Description
Technical field
The present invention relates to power network high-altitude circuit ribbon thing clearance technique field, more particularly to it is a kind of by aircraft carry it is clear
Except the device of high-altitude circuit ribbon thing.
Background technology
In recent years, with the rapid growth of the power equipment contradiction not enough with producers, transmission line of electricity is patrolled
Apparent mass can not be lifted effectively all the time, and opened gradually and used with park, and the citizen of kiteflying are more and more, Shi Youfa
The ribbon things such as raw kite, ad banner are wrapped in the situation of transmission line of electricity so that above-mentioned contradiction is further upgraded.In order to ensure electricity
The safe operation of net, therefore when transmission line of electricity floats extension ribbon thing, should in time be handled according to field condition, take effective method
Removed.
In the prior art, carry action bars removing ribbon thing to solve this thorny problem by using aircraft, its profit
Ribbon thing is removed with fuel injector igniter is powered, with reduction labor intensity, advantage in terms of operating efficiency is improved, to ensureing electricity
Web, high efficiency, stable operation, Electrial Power Industrial Automation play vital effect, but shortcoming is：The operation water of operating personnel
It is flat to require higher；There is burning things which may cause a fire disaster potential safety hazard during burning floating object；It is difficult to promote.
The content of the invention
Technical problem to be solved of the embodiment of the present invention is that there is provided a kind of removing high-altitude circuit carried by aircraft
The device of ribbon thing, coordinates with aircraft, and its is easy to operate, easy popularization and do not have burning things which may cause a fire disaster potential safety hazard, improve operating efficiency and
Security.
In order to solve the above-mentioned technical problem, the embodiments of the invention provide a kind of removing high-altitude circuit carried by aircraft
The device of ribbon thing, it is engaged with aircraft, and described device includes stock, the first guiding groove, the second guiding groove, electronic voltage
Adjuster, electric lead and heating wire；Wherein,
One end of the stock is provided with the erecting bed for being used for fixing the aircraft, and the other end is from its end face along away from described
Erecting bed direction each extends over out first guiding groove and second guiding groove；
The electronic voltage controller is fixed on the stock, and it includes voltage source；
The two ends of the heating wire are individually fixed on first guiding groove and second guiding groove, and pass through conductance
Two ends of the line respectively with the electronic voltage controller are connected；
Wherein, the erecting bed is towards being provided with the electronic voltage controller on the side end face of aircraft one.
Wherein, first guiding groove, which is provided with, is used to fixing first fixed part of described heating wire one end, and described the
Two guiding grooves are provided with the second fixed part for being used for fixing the heating wire other end；Wherein, first fixed part and described
Second fixed part is made by heat proof material.
Wherein, described device also includes damping pipe clamp, and the damping tube sandwiched is placed in the stock, and it is installed away from described
One end of platform, it includes vibration damper plate and the pipe clamp being arranged on the vibration damper plate.
Wherein, when the pipe clamp and the stock are mutually fixed, the vibration damper plate is away from one end of the erecting bed along institute
State stock it is axially extending go out the stock and positioned at the formation of first guiding groove and second guiding groove plane towards institute
State aircraft side；Wherein, radial diameter of the vibration damper plate away from described erecting bed one end is straight more than the radial direction of the stock
Footpath.
Wherein, the erecting bed is mutually fixed by metal connecting pole with the aircraft.
Wherein, the stock be hollow carbon fiber pipe, and the electric lead through the stock hollow pipeline with it is described
Heating wire two ends are connected.
Wherein, the electric lead is mutually fixed with the heating wire two ends by screw.
Wherein, the angle formed between first guiding groove and second guiding groove is more than 30 degree and less than 60 degree.
Wherein, first guiding groove is made with second guiding groove by carbon fiber.
Implement the embodiment of the present invention, have the advantages that：
1st, in embodiments of the present invention, heating wire is realized because device adjusts voltage swing by electronic voltage controller
Gradient of temperature, reach the ribbon thing purpose removed on the transmission line of electricity of high-altitude, therefore effectively prevent burning things which may cause a fire disaster potential safety hazard, have
Ease for operation and easy generalization；
2nd, in embodiments of the present invention, because the stock, the first guiding groove and the second guiding groove of device are by carbon fiber system
Form, with the features such as material is light, hardness is strong, therefore, it is possible to effectively lifting aircraft overall cruising time and cruising speed；
3rd, in embodiments of the present invention, due to device by damping pipe clamp reduce remove high-altitude transmission line of electricity on ribbon thing
When aircraft flight dynamics, therefore, it is possible to effectively lifting aircraft overall cruising time and cruising speed.
Brief description of the drawings
In order to illustrate more clearly about the embodiment of the present invention or technical scheme of the prior art, below will be to embodiment or existing
There is the accompanying drawing used required in technology description to be briefly described, it should be apparent that, drawings in the following description are only this
Some embodiments of invention, for those of ordinary skill in the art, without having to pay creative labor, according to
These accompanying drawings obtain other accompanying drawings and still fall within scope of the invention.
Fig. 1 is the device and aircraft provided in an embodiment of the present invention that remove high-altitude circuit ribbon thing carried by aircraft
Configuration diagram is installed；
Fig. 2 is the device stereochemical structure provided in an embodiment of the present invention that remove high-altitude circuit ribbon thing carried by aircraft
Schematic diagram；
Fig. 3 installs for the device direction of the removing high-altitude circuit ribbon thing provided in an embodiment of the present invention carried by aircraft
The dimensional structure diagram of platform direction one end；
Fig. 4 for the removing high-altitude circuit ribbon thing provided in an embodiment of the present invention carried by aircraft device towards electric heating
The dimensional structure diagram of silk direction one end；
Fig. 5 is electronics electricity in the device of the removing high-altitude circuit ribbon thing provided in an embodiment of the present invention carried by aircraft
Press the circuit connection diagram of adjuster and heating wire；
In figure：1- stocks, 11- erecting beds, 111- metal connecting poles, the guiding grooves of 2- first, the fixed parts of 21- first, 3-
Two guiding grooves, the fixed parts of 31- second, 4- electronic voltage controllers, 5- electric leads, 6- heating wire, 7- damping pipe clamps, 71- dampings
Plate, 72- pipe clamps, M- aircraft.
Embodiment
To make the object, technical solutions and advantages of the present invention clearer, the present invention is made into one below in conjunction with accompanying drawing
It is described in detail on step ground.
As shown in Figures 1 to 5, it is a kind of removing high-altitude circuit carried by aircraft of proposition in the embodiment of the present invention
The device of ribbon thing, it is engaged with aircraft M, and device includes stock 1, the first guiding groove 2, the second guiding groove 3, electronic voltage
Adjuster 4, electric lead 5 and heating wire 6；Wherein,
One end of stock 1 is provided with the erecting bed 11 for being used for fixing aircraft M, and the other end is from its end face along away from erecting bed 11
Direction each extends over out the first guiding groove 2 and the second guiding groove 3；
Electronic voltage controller 4 is fixed on stock 1, and it includes voltage source；
The two ends of heating wire 6 are individually fixed on the first guiding groove 2 and the second guiding groove 3, and by electric lead 5 respectively with
The two ends of electronic voltage controller 4 are connected.
It should be noted that the device energy of the removing high-altitude circuit ribbon thing carried by aircraft in the embodiment of the present invention
Enough using electronic voltage controller 4 come control voltage source voltage swing, so as to change by the electric current of heating wire 6, heating wire 6 is realized
Temperature adjustment so that the heating wire 6 of high temperature can blow the ribbon thing being wrapped on the transmission line of electricity of high-altitude, reaches that removing high-altitude is defeated
Ribbon thing purpose in electric line, therefore burning things which may cause a fire disaster potential safety hazard effectively is prevented, with ease for operation and easy generalization.
It should be noted that stock 1, the first guiding groove 2 and the second guiding groove 3 can be made by carbon fiber, with material
The features such as material is light, hardness is strong, therefore, it is possible to effectively lifting aircraft overall cruising time and cruising speed.
It is understood that stock 1 uses hollow carbon fiber pipe, the hollow pipeline that electric lead 5 may pass through stock 1 exists respectively
Be connected on first guiding groove 2 and the second guiding groove 3 by screw with the two ends of heating wire 6, can thus reduce electric lead 5 it is exposed
The danger of outer damage, extends the service life of electric lead 5.
In order to realize the ribbon thing best results removed on the transmission line of electricity of high-altitude, therefore the first guiding can be set in a device
The angle formed between the guiding groove 3 of groove 2 and second is more than 30 degree and less than 60 degree.
Because heating wire 6 is installed on the first guiding groove 2 and the second guiding groove 3, therefore the first guiding groove 2 is provided with being used for
First fixed part 21 of fixed one end of heating wire 6, and the second guiding groove 3 is provided with for fixing the second of the other end of heating wire 6
Fixed part 31.Meanwhile, destruction, loss are produced to the first guiding groove 2 and the second guiding groove 3 in order to avoid the temperature of heating wire 6 is too high
The service life of device, therefore the first fixed part 21 and the second fixed part 31 be made by heat proof material.
Aircraft M flight dynamics during in order to further reduce the drift on high-altitude transmission line of electricity is removed, can be effective
Aircraft M overall cruising time and cruising speed are lifted, therefore device also includes damping pipe clamp 7, damping pipe clamp 7 is arranged at stock
1 its deviate from erecting bed 11 one end, it includes vibration damper plate 71 and the pipe clamp 72 being arranged on vibration damper plate 71.
In order to avoid in operating process, foreign object (such as high pressure may be touched due to the first guiding groove 2 and the second guiding groove 3
Transmission line of electricity) when bend, so as to reach the purpose of protection whole device stability, therefore by pipe clamp 72 and the phase of stock 1
When fixed, vibration damper plate 71 away from one end of erecting bed 11 along stock 1 it is axially extending go out stock 1 and positioned at the first guiding groove 2 and the
The plane of two guiding grooves 3 formation is towards aircraft M sides；Wherein, radial diameter of the vibration damper plate 71 away from the one end of erecting bed 11 is big
In the radial diameter of stock 1, so that the first guiding groove 2 and the second guiding groove 3 are towards the end of stock 1 all in vibration damper plate 71
Protection domain in.
Certainly, vibration damper plate 71 extends one end of stock 1 and can also formed positioned at the first guiding groove 2 with the second guiding groove 3
Plane deviate from aircraft M sides, it is possibility to have two vibration damper plates 71, two vibration damper plates 71 extend stock 1 one end difference
Positioned at the first guiding groove 2 and the plane of the second guiding groove 3 formation away from aircraft M sides and towards aircraft M sides.
Further, erecting bed 11 is mutually fixed by metal connecting pole 111 with aircraft, in order to protect electronic voltage to adjust
Save device 4, it is to avoid aircraft M in-flight damaged in collision, therefore erecting bed 11 is towards being provided with electronics on the side end faces of aircraft M mono-
Voltage regulator 4.
The operation principle of the device of the removing high-altitude circuit ribbon thing carried in the embodiment of the present invention by aircraft is：Manipulation
Aircraft M is to high-altitude transmission line of electricity ribbon thing neighbouring position and is aligned, it is further provided pwm signal electron voltage regulator 4
Control voltage source output voltage size, so as to change by the electric current of heating wire 6, realizes the temperature adjustment of heating wire 6, utilizes electric heating
The high temperature of silk 6 blows the ribbon thing being wrapped on the transmission line of electricity of high-altitude.
Implement the embodiment of the present invention, have the advantages that：
1st, in embodiments of the present invention, heating wire is realized because device adjusts voltage swing by electronic voltage controller
Gradient of temperature, reach the ribbon thing purpose removed on the transmission line of electricity of high-altitude, therefore effectively prevent burning things which may cause a fire disaster potential safety hazard, have
Ease for operation and easy generalization；
2nd, in embodiments of the present invention, because the stock, the first guiding groove and the second guiding groove of device are by carbon fiber system
Form, with the features such as material is light, hardness is strong, therefore, it is possible to effectively lifting aircraft overall cruising time and cruising speed；
3rd, in embodiments of the present invention, due to device by damping pipe clamp reduce remove high-altitude transmission line of electricity on drift
When aircraft flight dynamics, therefore, it is possible to effectively lifting aircraft overall cruising time and cruising speed.
Above disclosed is only a kind of preferred embodiment of the invention, can not limit the power of the present invention with this certainly
Sharp scope, therefore the equivalent variations made according to the claims in the present invention, still belong to the scope that the present invention is covered.
Claims (9)
1. a kind of device of the removing high-altitude circuit ribbon thing carried by aircraft, it is engaged with aircraft, it is characterised in that
Described device includes stock（1）, the first guiding groove（2）, the second guiding groove（3）, electronic voltage controller（4）, electric lead（5）With
Heating wire（6）；Wherein,
The stock（1）One end be provided with and be used to fix the erecting bed of the aircraft（11）, the other end is from its end face along deviating from
The erecting bed（11）Direction each extends over out first guiding groove（2）And second guiding groove（3）；
The electronic voltage controller（4）It is fixed on the stock（1）On, it includes voltage source；
The heating wire（6）Two ends be individually fixed in first guiding groove（2）And second guiding groove（3）On, and lead to
Cross electric lead（5）Respectively with the electronic voltage controller（4）Two ends be connected；
Wherein, the erecting bed（11）Towards being provided with the electronic voltage controller on the side end face of aircraft one（4）.
2. device as claimed in claim 1, it is characterised in that first guiding groove（2）Being provided with is used to fix the electricity
Heated filament（6）First fixed part of one end（21）, and second guiding groove（3）Being provided with is used to fix the heating wire（6）Separately
Second fixed part of one end（31）；Wherein, first fixed part（21）With second fixed part（31）By heat proof material
It is made.
3. device as claimed in claim 2, it is characterised in that described device also includes damping pipe clamp（7）, the damping pipe clamp
（7）It is arranged at the stock（1）It deviates from the erecting bed（11）One end, it includes vibration damper plate（71）Be arranged at described subtract
Shake plate（71）On pipe clamp（72）.
4. device as claimed in claim 3, it is characterised in that the pipe clamp（72）With the stock（1）It is mutually fixed, it is described to subtract
Shake plate（71）Away from the erecting bed（11）One end along the stock（1）It is axially extending go out the stock（1）And positioned at described
First guiding groove（2）With second guiding groove（3）The plane of formation is towards the aircraft side；Wherein, the vibration damper plate
（71）Away from the erecting bed（11）The radial diameter of one end is more than the stock（1）Radial diameter.
5. device as claimed in claim 4, it is characterised in that the erecting bed（11）Pass through metal connecting pole（111）With institute
Aircraft is stated mutually to fix.
6. device as claimed in claim 5, it is characterised in that the stock（1）For hollow carbon fiber pipe, and the electric lead
（5）Through the stock（1）Hollow pipeline and the heating wire（6）Two ends are connected.
7. device as claimed in claim 6, it is characterised in that the electric lead（5）With the heating wire（6）Two ends pass through
Screw is mutually fixed.
8. device as claimed in claim 7, it is characterised in that first guiding groove（2）With second guiding groove（3）It
Between the angle that is formed be more than 30 degree and be less than 60 degree.
9. device as claimed in claim 8, it is characterised in that first guiding groove（2）With second guiding groove（3）
It is made by carbon fiber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510282552.0A CN104882820B (en) | 2015-05-29 | 2015-05-29 | A kind of device of the removing high-altitude circuit ribbon thing carried by aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510282552.0A CN104882820B (en) | 2015-05-29 | 2015-05-29 | A kind of device of the removing high-altitude circuit ribbon thing carried by aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104882820A CN104882820A (en) | 2015-09-02 |
| CN104882820B true CN104882820B (en) | 2017-09-22 |
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| CN201510282552.0A Active CN104882820B (en) | 2015-05-29 | 2015-05-29 | A kind of device of the removing high-altitude circuit ribbon thing carried by aircraft |
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Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
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| US9753461B1 (en) * | 2016-04-07 | 2017-09-05 | Google Inc. | Autonomous aerial cable inspection system |
| CN107706814B (en) * | 2017-10-26 | 2020-02-21 | 国网河南省电力公司濮阳供电公司 | Transmission line foreign matter clearing device based on hot melt technique |
| CN107732770B (en) * | 2017-10-27 | 2023-09-01 | 广东电网有限责任公司揭阳供电局 | Cutting device for removing foreign matters of power transmission line |
| CN112003190B (en) * | 2020-09-03 | 2021-09-24 | 湖南大学 | Aerial work robot for maintaining power transmission line |
| WO2022048112A1 (en) * | 2020-09-03 | 2022-03-10 | 湖南大学 | Aerial operation robot for power transmission line maintenance and automatic stability augmentation control method therefor |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| US8156624B2 (en) * | 2007-08-07 | 2012-04-17 | Gunair LLC | Apparatus and method for stringing aerial cables using aircraft |
| CN203722130U (en) * | 2014-01-14 | 2014-07-16 | 国网山东齐河县供电公司 | High-voltage wire attachment removing device |
| CN204210732U (en) * | 2014-11-05 | 2015-03-18 | 国网辽宁省电力有限公司检修分公司 | A kind of four rotor wing unmanned aerial vehicles for removing the flammable foreign matter in high-altitude |
| CN104682267B (en) * | 2015-03-26 | 2017-02-22 | 国家电网公司 | Power transmission line fault removal device based on multi-axle air vehicle |
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