CN106025981B - A kind of electric power transmission line deicing aircraft - Google Patents
A kind of electric power transmission line deicing aircraft Download PDFInfo
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- CN106025981B CN106025981B CN201610463221.1A CN201610463221A CN106025981B CN 106025981 B CN106025981 B CN 106025981B CN 201610463221 A CN201610463221 A CN 201610463221A CN 106025981 B CN106025981 B CN 106025981B
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- 230000007246 mechanism Effects 0.000 claims abstract description 60
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- 230000033228 biological regulation Effects 0.000 claims description 25
- 238000009434 installation Methods 0.000 claims description 23
- 230000005611 electricity Effects 0.000 claims description 17
- 210000000078 claw Anatomy 0.000 claims description 12
- 239000000463 material Substances 0.000 claims description 9
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- 238000004458 analytical method Methods 0.000 description 3
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Classifications
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
- H02G7/00—Overhead installations of electric lines or cables
- H02G7/16—Devices for removing snow or ice from lines or cables
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- Current-Collector Devices For Electrically Propelled Vehicles (AREA)
Abstract
The present invention relates to a kind of electric power transmission line deicing aircraft, including unmanned plane main body, six-degree-of-freedom parallel connection mechanism and deicer；Described six-degree-of-freedom parallel connection mechanism is located between unmanned plane main body and deicer, and six-degree-of-freedom parallel connection mechanism upper end is connected with unmanned plane main body, and six-degree-of-freedom parallel connection mechanism lower end is connected with deicer.The present invention can carry out automation deicing operation to overhead transmission line, and deicing effect is obvious, safe and stability is strong, the problem of solving artificial deicing difficulty after being frozen under overhead transmission line low temperature environment, it is ensured that the stability of power Transmission in adverse circumstances.
Description
Technical field
The present invention relates to electric power maintenance technical field, specifically a kind of electric power transmission line deicing aircraft.
Background technology
In recent years, with information-based development, the laying of overhead transmission line in all parts of the country is seen everywhere, and passes through transmission of electricity
Circuit is that the people is transmitted electricity and transmitted information, and it serves vital effect to daily life, but
It it is the annual time, especially the northern area of China in winter, because outdoor environment temperature is low, and sleety weather is on the high side, makes
Easily frozen into many overhead transmission lines of electricity, the overhead transmission line weight after icing substantially increases weight so that make somebody a mere figurehead everywhere
There is the phenomenon sunk or be broken in transmission line of electricity, and causes and has a strong impact on to transmission of electricity, the life for giving people the masses brings pole
Big inconvenience, also brings great economic loss to country, and current China is for being people mostly overhead transmission line deicing operation
Work, which climbs up steel tower using climbing apparatus or takes raising apparatus, carries out artificial deicing, and artificial deicing is not only slow except speed of icing, removes
Ice DeGrain, occupies substantial amounts of manpower, and there is great potential safety hazard in artificial ice detachment, easily causes tactile
Electricity or the security incident such as fall.In consideration of it, the invention provides a kind of electric power transmission line deicing aircraft.
The content of the invention
In order to make up the deficiencies in the prior art, the invention provides a kind of electric power transmission line deicing aircraft.
The present invention to be solved its technical problem and use following technical scheme to realize.
A kind of electric power transmission line deicing aircraft, including unmanned plane main body, six-degree-of-freedom parallel connection mechanism and deicer；
Described six-degree-of-freedom parallel connection mechanism is located between unmanned plane main body and deicer, and six-degree-of-freedom parallel connection mechanism upper end and nothing
Man-machine main body is connected, and six-degree-of-freedom parallel connection mechanism lower end is connected with deicer.
Further, described unmanned plane main body includes frame, servomotor, motor support base, propeller and tight locking button, and watches
The quantity for taking motor, motor support base, propeller and tight locking button is six；Described shell outside along its center axis symmetrically
It is provided with support, central rack position and uniformly offers material reducing hole, lower end offers installation screw thread at frame central position
Hole, servomotor is fixed on the support front end of frame by motor support base, and propeller is arranged on servomotor spindle, and spiral
It is locked between oar and servomotor spindle by tight locking button；The rotation of propeller is driven by the rotation of servomotor
Turn, so as to produce lift, and then power support is provided for aerial work of the present invention.
Further, described six-degree-of-freedom parallel connection mechanism includes fixed platform, moving platform, connecting seat, upper spherical hinge, electronic pushed away
Bar, block plate seat, lower spherical hinge, Triangulum and limit spring；Described connecting seat and Triangulum quantity are three, upper spherical hinge, electricity
The quantity of dynamic push rod, block plate seat and lower spherical hinge is six, and described fixed platform and moving platform is disc-shaped structure, and dynamic flat
Platform is located at immediately below fixed platform, and fixed platform upper part and moving platform end portion are respectively provided with installation screw thread, connecting seat
On the lower surface of fixed platform, and connecting seat is in equilateral triangle location arrangements on fixed platform, and Triangulum is arranged on dynamic flat
On platform upper surface, and installation site between connecting seat and Triangulum is interlocked two-by-two, and Triangulum is in equilateral triangle column structure,
Triangulum is respectively symmetrically provided with inclined plane, inclined plane along its vertical center line to be offered and lower spherical hinge lower end external screw thread phase
The installation screwed hole of cooperation, electric pushrod bottom is connected by upper spherical hinge with connecting seat, electric pushrod top and block plate seat
Upper end is connected, and block plate seat lower end is connected with lower spherical hinge one end, and the lower spherical hinge other end is arranged on Triangulum, spacing bullet
Spring is around being enclosed on electric pushrod, and limit spring one end is connected with electric pushrod, and the limit spring other end is connected with block plate seat
Connect；Six-degree-of-freedom parallel connection mechanism uses 6-SPS six-degree-of-freedom parallel connection mechanism, and rigidity is big compared with serial mechanism, six degree of freedom
Parallel institution Stability Analysis of Structures, kinematic dexterity are high, bearing capacity is strong and fine motion precision is high, and six-degree-of-freedom parallel connection mechanism is in space
The motion that three translations three rotate six-freedom degree direction altogether can be carried out, and space is small, movement velocity fast and kinematic dexterity
It is good, in the present invention, drive whole deicer to carry out the rotation of three translation three in space by six-degree-of-freedom parallel connection mechanism
The motion in six-freedom degree direction, is easy to deicer accurate micro-dimension and orientation when to overhead transmission line deicing operation altogether
Regulation, be easy to mobile operation of present invention when to removing ice of power transmission line and flexible job, reduce the present invention and make in deicing
The breakage caused in itself to transmission line of electricity during industry.
Further, described deicer includes connecting platform and deicing mechanism, and deicing mechanism quantity is six, and connection is flat
Platform lower end is square platy structure, and connecting platform upper end is to offer to put down with dynamic on cylindrical-shaped structure, and connecting platform upper surface
Threaded portion lower installation screwed hole in mating connection is installed in platform lower end, and the mode being connected through a screw thread is easy to the dismounting of the present invention
And installation, deicing mechanism is located at below connecting platform, and central transverse axis of the deicing mechanism along connecting platform distinguishes two two-phases
To being arranged symmetrically；Described deicing mechanism includes regulation guide rail, regulation guide block, the first ear mount, first rotating shaft, first connecting rod, the
Two ear mounts, the second rotating shaft, deicing claw, third ear seat, the 3rd rotating shaft, upper support bar, extension spring, lower support bar, the 4th ear mount and
4th rotating shaft；Described regulation guide rail left and right ends are respectively arranged with baffle plate, and regulation guide block is arranged on regulation guide rail, the first ear
Seat is fixed on regulation guide block, and first connecting rod upper end is arranged in the first ear mount by first rotating shaft, and first connecting rod lower end passes through
Second rotating shaft is arranged in the second ear mount, and the second ear mount is fixed on deicing claw upper right side lateral surface, and upper support bar upper end leads to
The 3rd rotating shaft is crossed on third ear seat, extension spring is located between upper support bar and lower support bar, and extension spring one end and upper support
Bar lower end is connected, and the extension spring other end is connected with lower support bar upper end, and lower support bar lower end is arranged on the by the 4th rotating shaft
In four ear mounts, the 4th ear mount is fixed on deicing claw bottom righthand side lateral surface；Described deicing claw includes fixed mount, positioning
Block, except crampon and vibrating head；Described fixed mount is in be provided with installation cavity, locating piece on the inside of semi-circular shape structure, and fixed mount
Quantity is two, and locating piece is separately fixed at fixed mount upper and lower ends, except crampon and vibrating head quantity are no less than ten, except crampon is located at
On the inside of fixed mount, and except central axis of the crampon along fixed mount is in being arranged circumferentially, except crampon rear end offers " Ω " type groove,
And be arranged on except crampon rear end inside the installation cavity on the inside of fixed mount, except crampon front end is cone-shaped, except crampon material is stainless
Steel material, vibrating head is arranged in " Ω " type groove except crampon rear end；During specific operation, first by the deicing installed in opposite directions two-by-two
Mechanism is adjusted to open configuration, then starts servomotor, the rotation of propeller is driven by the rotation of servomotor, so that band
The flight of the present invention is moved, when deicer is close to whne deicing power transmission line, deicing mechanism is fastened on the outside of transmission line of electricity, so
Start regulation guide rail and regulation guide block afterwards so that the deicing mechanism installed in opposite directions two-by-two is synchronous to medial motion, is connect when except crampon
When contacting ice cube surface, Vibration on Start-up rod drives the vibration of deicing pawl by the vibration of vibrating head, and except crampon front end is taper
Structure, advantageously abolishing in ice cube, and deicing mechanism are by the way of swing crushing to the ice cube on overhead transmission line
Crushed, deicing effect is good, and deicing mechanism position is adjustable, be adaptable to the built on stilts defeated of different icing thickness and different thicknesses
The deicing operation of electric line, while can prevent from removing the damage of outer surface of the crampon to transmission line of electricity in itself by locating piece and break
It is bad so that safe during deicer deicing operation, deicing effect is obvious and job stabilization is strong.
Compared with prior art, the present invention has advantages below：
(1) present invention can to overhead transmission line carry out automation deicing operation, and deicing effect it is obvious, safe and
Stability is strong, the problem of solving artificial deicing difficulty after being frozen under overhead transmission line low temperature environment, it is ensured that adverse circumstances
The stability of middle power Transmission.
(2) six-degree-of-freedom parallel connection mechanism of the invention uses 6-SPS six-degree-of-freedom parallel connection mechanism, six-degree-of-freedom parallel
Structure Stability Analysis of Structures, kinematic dexterity are high, bearing capacity is strong and fine motion precision is high, and it can drive whole deicer can in space
The motion that three translations three rotate six-freedom degree direction altogether is carried out, is easy to deicer when to overhead transmission line deicing operation
The regulation of accurate micro-dimension and orientation, is easy to mobile operation and flexible job of the present invention when to removing ice of power transmission line, reduction
The breakage that the present invention is caused in deicing operation process in itself to transmission line of electricity.
(3) deicer of the invention is crushed by the way of swing crushing to the ice cube on overhead transmission line,
Deicing effect is good, and deicing mechanism position is adjustable, is adaptable to different icing thickness and the overhead transmission line of different thicknesses
Deicing operation, while the damage and destruction except outer surface of the crampon to transmission line of electricity in itself can be prevented by locating piece so that remove
It is safe during ice production apparatus deicing operation, deicing effect is obvious and job stabilization is strong.
Brief description of the drawings
The present invention is further described with reference to the accompanying drawings and examples.
Fig. 1 is the dimensional structure diagram of the present invention；
Fig. 2 is six-degree-of-freedom parallel connection mechanism of the present invention and dimensional structure diagram when deicer is engaged；
Fig. 3 is the dimensional structure diagram of six-degree-of-freedom parallel connection mechanism of the present invention；
Fig. 4 is the dimensional structure diagram of deicer of the present invention；
Fig. 5 is dimensional structure diagram when two deicing mechanisms of the present invention coordinate；
Fig. 6 is the dimensional structure diagram of deicing mechanism of the present invention.
Embodiment
In order that the technical means, the inventive features, the objects and the advantages of the present invention are easy to understand, tie below
Conjunction is specifically illustrating, and the present invention is expanded on further.
As shown in Figures 1 to 6, a kind of electric power transmission line deicing aircraft, including unmanned plane main body 1, six degree of freedom are simultaneously
Online structure 2 and deicer 3；Described six-degree-of-freedom parallel connection mechanism 2 is located between unmanned plane main body 1 and deicer 3, and six
The upper end of freedom degree parallel connection mechanism 2 is connected with unmanned plane main body 1, and the lower end of six-degree-of-freedom parallel connection mechanism 2 is connected with deicer 3
Connect.
As shown in figure 1, described unmanned plane main body 1 includes frame 11, servomotor 12, motor support base 13, propeller 14
With tight locking button 15, and servomotor 12, motor support base 13, the quantity of propeller 14 and tight locking button 15 are six；Described frame
11 outsides are symmetrically provided with support, the medium position of frame 11 along its center axis uniformly offers material reducing hole, frame 11
Center position lower end offers installation screwed hole, and servomotor 12 is fixed on by motor support base 13 before the support of frame 11
End, propeller 14 is arranged on the main shaft of servomotor 12, and passes through tight locking button 15 between propeller 14 and the main shaft of servomotor 12
It is locked；The rotation of propeller 14 is driven by the rotation of servomotor 12, so as to produce lift, and then is the present invention
Aerial work provides power support.
As shown in Figures 2 and 3, described six-degree-of-freedom parallel connection mechanism 2 include fixed platform 21, moving platform 22, connecting seat 23,
Upper spherical hinge 24, electric pushrod 25, block plate seat 26, lower spherical hinge 27, Triangulum 28 and limit spring 29；Described connecting seat 23
It is three with the quantity of Triangulum 28, upper spherical hinge 24, electric pushrod 25, block plate seat 26 and the quantity of lower spherical hinge 27 are six, institute
The fixed platform 21 and moving platform 22 stated are disc-shaped structure, and moving platform 22 is immediately below fixed platform 21, on fixed platform 21
End part and the end portion of moving platform 22 are respectively provided with installation screw thread, and connecting seat 23 is arranged on the lower surface of fixed platform 21
On, and connecting seat 23 is in equilateral triangle location arrangements on fixed platform 21, Triangulum 28 is arranged on the upper surface of moving platform 22, and
Installation site between connecting seat 23 and Triangulum 28 is interlocked two-by-two, and Triangulum 28 is in equilateral triangle column structure, Triangulum
28 are respectively symmetrically provided with inclined plane, inclined plane along its vertical center line and offer and the lower end external screw thread of lower spherical hinge 27 matches
The installation screwed hole of conjunction, the bottom of electric pushrod 25 is connected by upper spherical hinge 24 with connecting seat 23, the top of electric pushrod 25 with
26 upper ends of block plate seat are connected, and 26 lower ends of block plate seat are connected with lower one end of spherical hinge 27, and the lower other end of spherical hinge 27 is arranged on
On Triangulum 28, limit spring 29 is around being enclosed on electric pushrod 25, and the one end of limit spring 29 is connected with electric pushrod 25, limit
The position other end of spring 29 is connected with block plate seat 26；Six-degree-of-freedom parallel connection mechanism 2 uses 6-SPS six-degree-of-freedom parallel connection mechanism,
Rigidity is big compared with serial mechanism, and the Stability Analysis of Structures of six-degree-of-freedom parallel connection mechanism 2, kinematic dexterity are high, bearing capacity is strong and fine motion
Precision is high, and six-degree-of-freedom parallel connection mechanism 2 can carry out the motion that three translations three rotate six-freedom degree direction altogether, and fortune in space
Dynamic space is small, movement velocity is fast and kinematic dexterity is good, in the present invention, is driven and entirely removed by six-degree-of-freedom parallel connection mechanism 2
Ice production apparatus 3 can carry out the motion that three translations three rotate six-freedom degree direction altogether in space, be easy to deicer 3 to built on stilts
The regulation in accurate micro-dimension and orientation during removing ice of power transmission line operation, is easy to mobile work of present invention when to removing ice of power transmission line
Industry and flexible job, reduce the breakage that the present invention is caused in itself in deicing operation process to transmission line of electricity.
As shown in Fig. 2, Fig. 4, Fig. 5 and Fig. 6, described deicer 3 includes connecting platform 31 and deicing mechanism 32, and removes
The quantity of mechanism of ice 32 is six, and the lower end of connecting platform 31 is square platy structure, and the upper end of connecting platform 31 is cylindrical-shaped structure, and even
Connect to offer on the upper surface of platform 31 and threaded portion lower installation screwed hole in mating connection is installed with the lower end of moving platform 22, pass through
The mode of threaded connection is easy to the dismounting and installation of the present invention, and deicing mechanism 32 is located at below connecting platform, and deicing mechanism 32
It is arranged symmetrically in opposite directions two-by-two respectively along the central transverse axis of connecting platform 31；Described deicing mechanism 32 includes regulation guide rail
321st, regulation guide block 322, the first ear mount 323, first rotating shaft 324, first connecting rod 325, the second ear mount 326, the second rotating shaft 327,
Deicing claw 328, the 329, the 3rd rotating shaft 3210 of third ear seat, upper support bar 3211, extension spring 3212, lower support bar the 3213, the 4th
The rotating shaft 3215 of ear mount 3214 and the 4th；The described left and right ends of regulation guide rail 321 are respectively arranged with baffle plate, and regulation guide block 322 is pacified
On regulation guide rail 321, the first 323, ear is fixed on regulation guide block 322, and the upper end of first connecting rod 325 passes through first rotating shaft
324 are arranged in the first ear mount 323, and the lower end of first connecting rod 325 is arranged in the second ear mount 326 by the second rotating shaft 327, and second
Ear mount 326 is fixed on the upper right side lateral surface of deicing claw 328, and the upper end of upper support bar 3211 is arranged on by the 3rd rotating shaft 3210
On third ear seat 329, extension spring 3212 is located between upper support bar 3211 and lower support bar 3213, and the one end of extension spring 3212 and upper branch
The lower end of strut 3211 is connected, and the other end of extension spring 3212 is connected with the upper end of lower support bar 3213, and the lower end of lower support bar 3213 leads to
The 4th rotating shaft 3215 is crossed in the 4th ear mount 3214, the 4th ear mount 3214 is fixed on the bottom righthand side lateral surface of deicing claw 328
On；Described deicing claw 328 includes fixed mount 3281, locating piece 3282, except crampon 3283 and vibrating head 3284；Described consolidates
Frame 3281 is determined in semi-circular shape structure, and the inner side of fixed mount 3281 is provided with installation cavity, the quantity of locating piece 3282 is two, locating piece
3282 are separately fixed at the upper and lower ends of fixed mount 3281, except crampon 3283 and the quantity of vibrating head 3284 are no less than ten, except crampon
3283 are located at the inner side of fixed mount 3281, and except central axis of the crampon 3283 along fixed mount 3281 is in be arranged circumferentially, deicing
The rear end of pawl 3283 offers " Ω " type groove, and is arranged on except the rear end of crampon 3283 inside the installation cavity of the inner side of fixed mount 3281, removes
The front end of crampon 3283 is cone-shaped, and except the material of crampon 3283 is stainless steel material, vibrating head 3284, which is arranged on, to be removed after crampon 3283
In " Ω " type groove at end；During specific operation, the deicing mechanism 32 installed in opposite directions two-by-two is adjusted to open configuration, Ran Houqi first
Dynamic servomotor 12, the rotation of propeller 14 is driven by the rotation of servomotor 12, so as to drive the flight of the present invention, when except
Deicing mechanism 32 is fastened on the outside of transmission line of electricity by ice production apparatus 3 close to when deicing power transmission line, then starts regulation guide rail
321 and regulation guide block 322 so that the deicing mechanism 32 installed in opposite directions two-by-two is synchronous to medial motion, is contacted when except crampon 3283
During to ice cube surface, Vibration on Start-up rod 3284 drives the vibration of deicing pawl 3283 by the vibration of vibrating head 3284, and except crampon
3283 front ends be pyramidal structure, advantageously abolishing in ice cube, and deicing mechanism 32 using swing crushing by the way of to making somebody a mere figurehead
Ice cube on transmission line of electricity is crushed, and deicing effect is good, and the position of deicing mechanism 32 is adjustable, is adaptable to different icing thickness
With the deicing operation of the overhead transmission line of different thicknesses, while by locating piece 3282 can prevent except crampon 3283 to power transmission line
The damage and destruction of the outer surface of road in itself so that safe during 3 deicing operation of deicer, deicing effect is substantially and operation
Stability is strong.
The basic principles, principal features and advantages of the present invention have been shown and described above.The technical staff of the industry should
Understand, the present invention is not limited to the above embodiments, the simply explanation present invention of the description in above-described embodiment and specification
Principle, without departing from the spirit and scope of the present invention, various changes and modifications of the present invention are possible, and these change and changed
Enter all fall within the protetion scope of the claimed invention.The claimed scope of the invention is by appended claims and its equivalent
Define.
Claims (2)
1. a kind of electric power transmission line deicing aircraft, it is characterised in that：Including unmanned plane main body, six-degree-of-freedom parallel connection mechanism and
Deicer；Described six-degree-of-freedom parallel connection mechanism is located between unmanned plane main body and deicer, and six-degree-of-freedom parallel
Structure upper end is connected with unmanned plane main body, and six-degree-of-freedom parallel connection mechanism lower end is connected with deicer；Wherein：
Described unmanned plane main body includes frame, servomotor, motor support base, propeller and tight locking button, and servomotor, motor
The quantity of bearing, propeller and tight locking button is six；Described shell outside is symmetrically provided with support along its center axis,
Lower end at material reducing hole, frame central position is uniformly offered at central rack position and offers installation screwed hole, servomotor
The support front end of frame is fixed on by motor support base, propeller is arranged on servomotor spindle, and propeller and servo electricity
It is locked between owner's axle by tight locking button；
Described six-degree-of-freedom parallel connection mechanism include fixed platform, moving platform, connecting seat, upper spherical hinge, electric pushrod, block plate seat,
Lower spherical hinge, Triangulum and limit spring；Described connecting seat and Triangulum quantity are three, upper spherical hinge, electric pushrod, block plate
The quantity of seat and lower spherical hinge is six；Described fixed platform and moving platform is disc-shaped structure, and moving platform is located at and allocated
Immediately below platform, fixed platform upper part and moving platform end portion are respectively provided with installation screw thread, and connecting seat is arranged on and allocated
On the lower surface of platform, and connecting seat is in equilateral triangle location arrangements on fixed platform, and Triangulum is arranged on moving platform upper surface,
And the installation site between connecting seat and Triangulum is interlocked two-by-two, and Triangulum be in equilateral triangle column structure, Triangulum along its
Vertical center line is respectively symmetrically provided with the installation for offering and being engaged with lower spherical hinge lower end external screw thread in inclined plane, inclined plane
Screwed hole, electric pushrod bottom is connected by upper spherical hinge with connecting seat, and electric pushrod top is connected with block plate seat upper end,
Block plate seat lower end is connected with lower spherical hinge one end, and the lower spherical hinge other end is on the Triangulum, and limit spring is around being enclosed on electricity
On dynamic push rod, and limit spring one end is connected with electric pushrod, and the limit spring other end is connected with block plate seat；
Described deicer includes connecting platform and deicing mechanism, and deicing mechanism quantity is six, and connecting platform lower end is side
Shape platy structure, connecting platform upper end is to offer to install with moving platform lower end on cylindrical-shaped structure, and connecting platform upper surface
Threaded portion lower installation screwed hole in mating connection, deicing mechanism is located at below connecting platform, and deicing mechanism is flat along connection
The central transverse axis of platform is arranged symmetrically in opposite directions two-by-two respectively；
Described deicing mechanism include regulation guide rail, regulation guide block, the first ear mount, first rotating shaft, first connecting rod, the second ear mount,
Second rotating shaft, deicing claw, third ear seat, the 3rd rotating shaft, upper support bar, extension spring, lower support bar, the 4th ear mount and the 4th turn
Axle；Described regulation guide rail left and right ends are respectively arranged with baffle plate, and regulation guide block is arranged on regulation guide rail, and the first ear mount is fixed
On regulation guide block, first connecting rod upper end is arranged in the first ear mount by first rotating shaft, and first connecting rod lower end passes through second turn
Axle is arranged in the second ear mount, and the second ear mount is fixed on deicing claw upper right side lateral surface, and upper support bar upper end passes through the 3rd
Rotating shaft is arranged on third ear seat, and extension spring is located between upper support bar and lower support bar, and extension spring one end and upper support bar lower end
It is connected, the extension spring other end is connected with lower support bar upper end, lower support bar lower end is arranged on the 4th ear mount by the 4th rotating shaft
On, the 4th ear mount is fixed on deicing claw bottom righthand side lateral surface.
2. a kind of electric power transmission line deicing aircraft according to claim 1, it is characterised in that：Described deicing claw
Including fixed mount, locating piece, except crampon and vibrating head；Described fixed mount is in be set on the inside of semi-circular shape structure, and fixed mount
There is installation cavity, positioning number of blocks is two, and locating piece is separately fixed at fixed mount upper and lower ends, except crampon and vibrating head quantity are many
In ten, except crampon is located on the inside of fixed mount, and except central axis of the crampon along fixed mount is in being arranged circumferentially, except crampon rear end
" Ω " type groove is offered, and is arranged on except crampon rear end inside the installation cavity on the inside of fixed mount, except crampon front end is cone-shaped, is removed
Crampon material is stainless steel material, and vibrating head is arranged in " Ω " type groove except crampon rear end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610463221.1A CN106025981B (en) | 2016-06-23 | 2016-06-23 | A kind of electric power transmission line deicing aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610463221.1A CN106025981B (en) | 2016-06-23 | 2016-06-23 | A kind of electric power transmission line deicing aircraft |
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| Publication Number | Publication Date |
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| CN106025981A CN106025981A (en) | 2016-10-12 |
| CN106025981B true CN106025981B (en) | 2017-10-24 |
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| CN201610463221.1A Active CN106025981B (en) | 2016-06-23 | 2016-06-23 | A kind of electric power transmission line deicing aircraft |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106921137B (en) * | 2016-11-28 | 2018-11-06 | 国网江西省电力公司景德镇供电分公司 | A kind of power cable automatic de-icing unmanned plane |
| CN107039943B (en) * | 2017-05-19 | 2019-02-12 | 合肥尚强电气科技有限公司 | A kind of intelligent deicer for power transmission and transformation line |
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| CN109066459A (en) * | 2018-08-21 | 2018-12-21 | 陈二东 | A kind of power transmission line pipeline quick-speed first-aid repair method |
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