CN108086781A - A kind of power cable stringer of stabilization - Google Patents
A kind of power cable stringer of stabilization Download PDFInfo
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- CN108086781A CN108086781A CN201710931539.2A CN201710931539A CN108086781A CN 108086781 A CN108086781 A CN 108086781A CN 201710931539 A CN201710931539 A CN 201710931539A CN 108086781 A CN108086781 A CN 108086781A
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- tail end
- beam column
- guide groove
- extension
- wall
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- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
- E04H12/00—Towers; Masts or poles; Chimney stacks; Water-towers; Methods of erecting such structures
- E04H12/34—Arrangements for erecting or lowering towers, masts, poles, chimney stacks, or the like
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- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Devices Affording Protection Of Roads Or Walls For Sound Insulation (AREA)
Abstract
The invention discloses a kind of power cable stringers of stabilization, including matrix and it is fixedly mounted on the fuselage of baseline top, perforation body bottom surface is equipped in fuselage installs chamber, install the first beam column and the second beam column for matching above and below intracavitary portion and extending equipped with left and right and setting, extension tail end is fixedly connected respectively with installing inner wall at left and right sides of chamber at left and right sides of first beam column and the second beam column, the matrix top surface for installing bottom of chamber portion is installed with and puts in the first motor for installing intracavitary, the first rotation axis for extending set upwards is connected at the top of first motor, extension penetrates through the second beam column and the first beam column from bottom to up at the top of first rotation axis and rotatable engagement connects, what extension tail end put in the first beam column over top at the top of the first rotation axis installs intracavitary, first rotation axis outer surface of the first beam column over top is installed with male rotor；The configuration of the present invention is simple, easy to operate, efficient, soil layer is closely knit, electric pole fixing-stable, reduces the time of work.
Description
Technical field
The present invention relates to the power cable stringers of power cable technical field, specifically a kind of stabilization.
Background technology
Annual China is required for newly setting up substantial amounts of electric wire to accelerate the connection of communication network, in order to avoid power line
Road is destroyed by powerful load due to wind pressure, needs to increase the stability of electric pole in the soft area of soil property, presently mainly in earth's surface
It digs pit fixed electric pole, reality is struck with spade in earth's surface after back fill course, this mode is time-consuming and laborious, and soil density is low, meets heavy rain
Soil matrix easily settles, and easily hack lever is caused to be toppled over, and especially needs to pile surface soil layer into the feelings of ramp shaped for reinforcement fixed effect
Under condition, real be difficult to so that soil density is consistent is struck by hand.
The content of the invention
The technical problems to be solved by the invention are to provide a kind of power cable stringer of stabilization, can solve
The problem of stating now in the art.
The present invention is achieved through the following technical solutions：A kind of power cable stringer of stabilization of the present invention,
It is equipped with including matrix and the fuselage being fixedly mounted at the top of described matrix, in the fuselage and penetrates through installing for the body bottom surface
Chamber, it is described install intracavitary portion up and down match equipped with left and right extend set the first beam column and the second beam column, first beam column and
Extension tail end is fixedly connected respectively with the chamber left and right sides inner wall of installing at left and right sides of second beam column, described to install bottom of chamber
The described matrix top surface in portion, which is installed with, puts in first motor for installing intracavitary, is connected at the top of first motor
Have the first rotation axis for extending set upwards, at the top of first rotation axis extension penetrate through from bottom to up second beam column and
First beam column and rotatable engagement connection, the first rotation axis top extension tail end put in the first beam column over top
It is described install intracavitary, the first rotation axis outer surface of the first beam column over top is installed with male rotor, described convex
Described above shape wheel installs intracavitary and installs that intracavitary roof slides mating connection and what is set extended in left and right with described equipped with top surface
Push rod, push rod left side extension penetrate through outer wall on the left of the fuselage and slide mating connection, extension on the right side of the push rod
It penetrating through the fuselage outer right wall and slides mating connection, extension tail end is visited to outside the fuselage right flank on the right side of the push rod,
It visits to sliding in the push rod outside the fuselage right flank to be connected with and strikes actual load and put, the institute on the right side of first rotation axis
It states to be equipped in the first beam column and slides conduction device, first rotation axis in fact to slide striking for mating connection with the male rotor
It is equipped with sealed adjusting apparatus in second beam column on right side, the second beam column top surface on the upside of the sealed adjusting apparatus is set
Have to strike the real sealed conduction device for sliding conduction device and coordinating sealed connection with described, described matrix top surface is fixedly installed
Lamppost, the fore-set right flank are fixedly installed headlamp, and the headlamp periphery is fixedly installed focused lamp cover, described matrix
Bottom is provided with brake stop device.
Preferably technical solution, the left and right sides bottom of the fuselage outer side and top at left and right sides of described matrix
Between be installed with the first solid bar, outer wall is installed with the push rod for extending to upper left side and setting on the left of the fuselage.
Preferably technical solution, the first motor left and right sides outer wall are installed with described at left and right sides of chamber respectively
Match between inner wall equipped with the second solid bar, the left and right sides described second consolidates top portion and do not install inner wall at left and right sides of chamber with described
Between match the 3rd solid bar.
Preferably technical solution, it is described strike actual load put including with the push rod slide mating connection and up and down extend set
The support rod put, extension tail end is visited to outside the push rod top surface and outer surface and is installed with restricted driving block at the top of the support rod, described
Extension tail end in support rod bottom is visited to outside the push rod bottom surface and tail end is equipped with and strikes solid plate, it is described strike solid plate and the push rod it
Between the supporting rod outer surface be installed with solid block, the solid supporting rod outer surface between block and the push rod is equipped with spring
Circle.
Preferably technical solution, it is described to strike the real conduction device that slides and include the first guide groove and slide to be equipped with
Extend in first guide groove and up and down the 3rd guide rod set, and cooperation is slided in the 3rd guide rod in first guide groove
The first guide rod that left and right extension is set is connected with, tail end fixes company with the first guide groove inner left wall on the left of first guide rod
It connects, tail end is fixedly connected with inner wall on the right side of first guide groove on the right side of first guide rod, extension at the top of the 3rd guide rod
Put on the upside of first beam column described installs intracavitary and top tail end is fixedly connected with the push rod bottom, first beam
The 3rd guide rod that intracavitary is installed described on the upside of column is located at the male rotor right positions, and chamber is installed described in the first beam column upside
The 3rd interior guide rod right flank peace opposite with the 3rd guide rod right flank that intracavitary is installed described in first beam column upside
If being equipped with the first spring coil on the right side of chamber between inner wall, the 3rd guide rod bottom extension tail end puts in first beam column and described the
Intracavitary is installed described between two beam columns.
Preferably technical solution, the sealed conduction device is interior to be equipped with the second guide groove, is equipped in second guide groove
Extend the first spiral shell shape bar set for left and right, and extension tail end is rotated with the second guide groove inner left wall on the left of the first spiral shell shape bar
It being connected, extension tail end is connected with second guide groove right side inner wall rotatable engagement on the right side of the first spiral shell shape bar, and described the
It is installed with the first taper cone pulley on the left of one spiral shell shape bar on section outer surface, spiral shell on the first spiral shell shape bar on the right side of first taper cone pulley
Shape line is connected with the guide block for extending set upwards, and extension tail end is visited to the sealed conduction device top surface at the top of the guide block
Outer and tail end is installed with the cross bar for setting of extending to the left, and extension tail end is installed with the sealed of setting that extend upwards on the left of the cross bar
Bar, the locking pole are located at the leftward position of the 3rd guide rod bottom extension tail end and are oppositely arranged, first taper cone pulley
It is slided in the guide block of upside and is connected with the second guide rod that left and right extension is set, extended at left and right sides of second guide rod
Tail end is fixedly connected respectively with inner wall at left and right sides of second guide groove.
Preferably technical solution, the sealed adjusting apparatus include the 3rd guide groove and slide to be equipped with described
Adjustment block in 3rd guide groove, connect at the top of the 3rd guide groove setting with the second guide groove left bottom, the adjustment
Block inner spiral line is connected with left and right and extends the second spiral shell shape bar set, on the left of the second spiral shell shape bar extension tail end with it is described
3rd guide groove inner left wall rotatable engagement connects, and extension tail end is connected with adjustment motor on the right side of the second spiral shell shape bar,
The adjustment motor outer surface is arranged on the right side of the 3rd guide groove in inner wall and is fixedly connected, on front side of the second spiral shell shape bar
The adjustment block in rotation be connected with the second rotation axis for extending set up and down, extension tail at the top of second rotation axis
End is put in second guide groove and tail end is installed with to the second taper cone pulley with the ratcheting connection of the first taper cone pulley, described
What the second rotation axis bottom extension tail end put on the downside of second beam column described installs intracavitary and tail end is installed with the first tooth form
Wheel.
Preferably technical solution, is installed on the first rotation axis outer surface on the downside of second beam column and institute
State the second toothed wheel that the first toothed wheel left-hand end is oppositely arranged.
Preferably technical solution, the brake that the brake stop device includes being fixed at described matrix bottom surface are stopped lock and are consolidated
Surely it is arranged on the left side brake stopped on the left of lock of stopping and stops sole, the brake stops the outside that lock is separately positioned on bottom surface wheel.
The beneficial effects of the invention are as follows：
1. by the first fixed male rotor in rotation axis outer surface of the first beam column over top, the intracavitary of installing above male rotor is set
Top surface slides the push rod that mating connection and left and right extension are set with installing intracavitary roof, and extension is penetrated through on the left of fuselage on the left of push rod
Outer wall and mating connection is slided, extension perforation fuselage outer right wall and slide matings connection on the right side of push rod, extension on the right side of push rod
Tail end is visited to outside fuselage right flank, is visited to sliding mating connection in the push rod outside fuselage right flank and strike actual load and is put, the first rotation axis
It is set in first beam column on right side and slides conduction device in fact to slide striking for mating connection with male rotor, on the right side of the first rotation axis
Set sealed adjusting apparatus in second beam column, the second beam column top surface on the upside of sealed adjusting apparatus sets real to slide conduction dress with striking
It puts the sealed conduction device for coordinating sealed connection, continues back and forth to carry out slope to strike positive activity so as to fulfill automatically controlling, together
When, it can realize the sealed work of adjust automatically control push rod, stability when improving transport or carrying.
2. it is put by striking actual load including sliding the support rod set that is connected and extends up and down, support rod top with push rod
Extension tail end is visited to outside push rod top surface and the fixed restricted driving block in outer surface, and extension tail end in support rod bottom is visited to outside push rod bottom surface and tail
Solid plate is struck in end installation, strikes the fixed solid block of supporting rod outer surface between solid plate and push rod, Gu outside the support rod between block and push rod
Surface sets spring coil, generates larger impact force in real time so as to fulfill reducing to strike, plays preferable cushioning effect, improves and use the longevity
Life.
3. the configuration of the present invention is simple, easy to operate, can realize automatically control continue back and forth to carry out slope strike positive activity,
Meanwhile can realize the sealed work of adjust automatically control push rod, stability when improving transport or carrying, and time saving and energy saving, effect
Rate is high, and soil layer is closely knit, and electric pole fixing-stable reduces the time of work, reduces financial cost, shortens the work of construction
Phase.
Description of the drawings
For ease of explanation, the present invention is described in detail by following specific embodiment and attached drawing.
Fig. 1 is overall structure diagram outside a kind of power cable stringer of stabilization of the present invention；
Fig. 2 is overall structure diagram inside a kind of power cable stringer of stabilization of the present invention；
Structure diagram when Fig. 3 is after a kind of power cable stringer of stabilization of the present invention is sealed；
Fig. 4 is the partial structural diagram of the present invention.
Specific embodiment
As Figure 1-Figure 4, the power cable stringer of a kind of stabilization of the invention, including matrix 5 and fixed peace
Fuselage 6 mounted in the top of described matrix 5, be equipped in the fuselage 6 penetrate through 6 bottom surface of fuselage install chamber 61, it is described to install
The inside of chamber 61 matches the first beam column 62 and the second beam column 63 for extending equipped with left and right and setting up and down, first beam column 62 and described
Second beam column, 63 left and right sides extension tail end is fixedly connected respectively with 61 left and right sides inner wall of chamber of installing, described to install chamber 61
5 top surface of described matrix of bottom, which is installed with, puts in first motor 52 installed in chamber 61, and first motor 52 pushes up
Portion is connected with the first rotation axis 55 for extending set upwards, and the 55 top extension of the first rotation axis penetrates through from bottom to up
Second beam column 63 is connected with first beam column 62 and rotatable engagement, and the 55 top extension tail end of the first rotation axis is put in
The described of first beam column, 62 over top is installed in chamber 61, first rotation axis of 62 over top of the first beam column
55 outer surfaces are installed with male rotor 552, and described install in chamber 61 of 552 top of male rotor installs chamber equipped with top surface with described
61 inner roof walls slide the push rod 610 that mating connection and left and right extension are set, and the 610 left side extension of push rod penetrates through the fuselage
6 left side outer walls and mating connection is slided, the 610 right side extension of push rod penetrates through 6 outer right wall of fuselage and slides cooperation
Connection, the 610 right side extension tail end of push rod are visited to outside 6 right flank of fuselage, visited described in outside 6 right flank of fuselage
It slides to be connected in push rod 610 and strikes actual load and put 7, be equipped with and use in first beam column 62 on 55 right side of the first rotation axis
With with the male rotor 552 slide mating connection strike it is real slide conduction device, described the of 55 right side of the first rotation axis
Be equipped with sealed adjusting apparatus in two beam columns 63,63 top surface of the second beam column on the upside of the sealed adjusting apparatus be equipped with to
Described to strike the real sealed conduction device 64 for sliding conduction device and coordinating sealed connection, 5 top surface of described matrix is fixedly installed lamppost
8,8 right flank of fore-set is fixedly installed headlamp 82, and 82 periphery of headlamp is fixedly installed focused lamp cover 81, convenient
Night work, 5 bottom of described matrix are provided with brake stop device.
Valuably, it is installed between 5 left and right sides top of the left and right sides bottom in 6 outside of fuselage and described matrix
First solid bar 51, the 6 left side outer wall of fuselage is installed with the push rod for extending to upper left side and setting, so as to improve fuselage 6 and matrix 5
Stable connection.
Valuably, 52 left and right sides outer wall of the first motor is installed with described between 61 left and right sides inner wall of chamber respectively
Match equipped with the second solid bar 53, the left and right sides described second consolidate at the top of bar 53 respectively with it is described install 61 left and right sides inner wall of chamber it
Between match the 3rd solid bar 54, so as to improve the stability when operation of the first motor 52, when preventing that the first motor 52 from running
Generation, which is rocked, causes equipment fluctuation of service.
Valuably, the actual load of striking puts 7 including sliding the supporting set that is connected and extends up and down with the push rod 610
Bar 71, the 71 top extension tail end of support rod is visited to outside 610 top surface of push rod and outer surface and is installed with restricted driving block 73, described
71 bottom extension tail end of support rod is visited to outside 610 bottom surface of push rod and tail end is equipped with and strikes solid plate 74, it is described strike solid plate 74 with
71 outer surface of the support rod between the push rod 610 is installed with solid block 72, described to consolidate between block 72 and the push rod 610
71 outer surface of support rod is equipped with spring coil 75, and larger impact force is generated in real time so as to fulfill reducing to strike, and plays preferable slow
Punching acts on, and improves service life.
Valuably, it is described to strike the real conduction device that slides and include the first guide groove 621 and slide to be equipped with described first
Extend in guide groove 621 and up and down the 3rd guide rod 623 set, is slided in the 3rd guide rod 623 in first guide groove 621
It is connected with the first guide rod 622 that left and right extension is set, the 622 left side tail end of the first guide rod and first guide groove 621
Inner left wall is fixedly connected, and the 622 right side tail end of the first guide rod is fixedly connected with the 621 right side inner wall of the first guide groove, institute
State 623 top extension of the 3rd guide rod put in first beam column, 62 upside it is described install in chamber 61 and top tail end with it is described
610 bottom of push rod is fixedly connected, and the 3rd guide rod 623 installed described in 62 upside of the first beam column in chamber 61 is located at the convex
552 right positions are taken turns, 623 right flank of the 3rd guide rod and first beam in chamber 61 are installed described in 62 upside of the first beam column
It opposite described of 623 right flank of the 3rd guide rod in chamber 61 is installed described in the upside of column 62 installs and the is equipped between 61 right side inner wall of chamber
One spring coil 624, the 623 bottom extension tail end of the 3rd guide rod are put between first beam column 62 and second beam column 63
It is described to install in chamber 61, since the 3rd guide rod 623 is subject to the elastic top pressure active force of the first spring coil 624, so as to by male rotor 552
Cooperation realization of persistently sliding with the 3rd guide rod 623 back and forth strikes positive activity.
Valuably, the second guide groove 641 is equipped in the sealed conduction device 64, left and right is equipped in second guide groove 641
Extend the first spiral shell shape bar 642 set, in 641 left side of the 642 left side extension tail end of the first spiral shell shape bar and second guide groove
Wall rotatable engagement connects, the 642 right side extension tail end of the first spiral shell shape bar and the 641 right side inner wall rotatable engagement of the second guide groove
It connects, the first taper cone pulley 643,643 right side of the first taper cone pulley is installed on the 642 left side section outer surface of the first spiral shell shape bar
The first spiral shell shape bar 642 on whorl be connected with the guide block 644 for extending set upwards, 644 top of the guide block is prolonged
Exhibition tail end is visited to outside sealed 64 top surface of conduction device and tail end is installed with the cross bar 646 for setting of extending to the left, the cross bar
646 left side extension tail ends are installed with the locking pole 647 for extending set upwards, and the locking pole 647 is located at the 3rd guide rod 623
It the leftward position of bottom extension tail end and is oppositely arranged, cooperation is slided in the guide block 644 of 643 upside of the first taper cone pulley
It is connected with left and right to extend the second guide rod 645 set, 645 left and right sides extension tail end of the second guide rod is respectively with described second
641 left and right sides inner wall of guide groove is fixedly connected, so as to by sealed adjusting apparatus and the second toothed wheel 551 and sealed conduction device 64
Conduction be connected, realize to automatically control sealed conduction device 64 and strike the real automatic locking for sliding conduction device and be connected
Work.
Valuably, the sealed adjusting apparatus includes the 3rd guide groove 631 and slides to be equipped in the 3rd guide groove
Adjustment block 634 in 631,631 top of the 3rd guide groove and 641 left bottom of the second guide groove connect setting, described
634 inner spiral line of adjustment block is connected with the second spiral shell shape bar 632 that left and right extension is set, 632 left side of the second spiral shell shape bar
Extension tail end is connected with the 631 inner left wall rotatable engagement of the 3rd guide groove, the 632 right side extension tail end of the second spiral shell shape bar with
Adjustment motor 633 is connected, and 633 outer surface of the adjustment motor is arranged in the 631 right side inner wall of the 3rd guide groove
And be fixedly connected, rotation is connected in the adjustment block 634 of 632 front side of the second spiral shell shape bar extends what is set up and down
Second rotation axis 635, the 635 top extension tail end of the second rotation axis is put in second guide groove 641 and tail end is installed with
To the second taper cone pulley 636 with the 643 ratcheting connection of the first taper cone pulley, the 635 bottom extension tail end of the second rotation axis
It puts in the described of second beam column, 63 downside to install in chamber 61 and tail end is installed with the first toothed wheel 637, so as to fulfill automatic
Control adjustment work, improves work efficiency.
Valuably, it is installed with and first tooth on 55 outer surface of the first rotation axis of 63 downside of the second beam column
The second toothed wheel 551 that 637 left-hand end of shape wheel is oppositely arranged.
Valuably, the brake stop device stops lock 502 and is fixed at including being fixed at the brake of 5 bottom surface of described matrix
The brake that the left side brake stops 502 left side of lock stops sole 501, and the brake stops the outside that lock 502 is separately positioned on bottom surface wheel, when need
When stopping, step on the brake and stop the i.e. controllable brake of sole 501 and stop the holding wheel of lock 502.
During original state, adjustment block 634 is located at the right-most position in the 3rd guide groove 631, at this point, making 634 band of adjustment block
The first toothed wheel 637 is moved utmostly away from the second toothed wheel 551, meanwhile, adjustment block 634 is made to drive the second taper cone pulley 636 most
Big degree is away from the first taper cone pulley 643, at this point, 647 right flank of locking pole and the first guide groove 621 are in same perpendicular position
It puts.
When needing to strike positive activity, be moved to matrix 5 needs to strike at real position first, then passes through the first motor
52 the first rotation axis 55 of drive rotate, and then by the first rotation axis 55 the second toothed wheel 551 and male rotor 552 are driven to rotate,
At this point, the second toothed wheel 551 is in idling conditions, simultaneously as the 3rd guide rod 623 is subject to the top pressure of the first spring coil 624 to act on
Power makes 623 left-hand end of the 3rd guide rod slide mating connection with 552 right side outer surface of male rotor, at this point, being rotated by male rotor 552
The 3rd guide rod 623 is driven to be slided toward 622 left and right directions of the first guide rod of complex edge, meanwhile, by the 3rd guide rod 623 push rod 610 is driven to hold
Continuous reciprocal left and right is slided, so as to fulfill by striking on 623 right-hand end of the 3rd guide rod, actual load puts 7 carry out slopes strikes positive activity；
When strike it is real complete to need to pack up and transport when, at this point, the first motor 52 of control stops rotating, meanwhile, control adjustment motor
633 the second spiral shell shape bars 632 of drive rotate, and drive adjustment block 634 gradually along the left side in the 3rd guide groove 631 by the second spiral shell shape bar 63
Direction is slided, until when adjustment block 634 is moved to the left-most position in the 3rd guide groove 631, at this point, making 634 bottom of adjustment block
The 551 ratcheting connection of the first toothed wheel 637 and the second toothed wheel, meanwhile, make 643 tooth of the second taper cone pulley 636 and the first taper cone pulley
Connection is closed, at this point, the first motor 52 of control drives the first rotation axis 55 to rotate, and then first is driven by the second toothed wheel 551
637 and second rotation axis 635 of toothed wheel rotates, meanwhile, by the second rotation axis 635 the second taper cone pulley 636 is driven to rotate, this
When, the first spiral shell shape bar 642 on the first taper cone pulley 643 and the first taper cone pulley 643 is driven to rotate by the second taper cone pulley 636, together
When, by the first spiral shell shape bar 642 guide block 644 is driven gradually to be slided along the right direction in the second guide rod 645, at this point, by guide block 644
The locking pole 647 of 646 left side tail end of cross bar 646 and cross bar is driven to be moved towards 623 opposite side of the 3rd guide rod, until locking pole
647 abut against with the 3rd guide rod 623 and drive the 3rd guide rod 623 that 624 pressure on top surface of the first spring coil is overcome to slide to the right, when the 3rd
When guide rod 623 is slided to right-most position in the first guide groove 621, at this point, the guide block 644 in the second guide groove 641 is slided to
Then right-most position in two guide grooves 641 controls the first motor 52 to stop rotating, at this point, completing the sealed company of push rod 610
It connects, generating to rock when preventing mobile causes equipment damage, improves service life.
The beneficial effects of the invention are as follows：
1. by the first fixed male rotor in rotation axis outer surface of the first beam column over top, the intracavitary of installing above male rotor is set
Top surface slides the push rod that mating connection and left and right extension are set with installing intracavitary roof, and extension is penetrated through on the left of fuselage on the left of push rod
Outer wall and mating connection is slided, extension perforation fuselage outer right wall and slide matings connection on the right side of push rod, extension on the right side of push rod
Tail end is visited to outside fuselage right flank, is visited to sliding mating connection in the push rod outside fuselage right flank and strike actual load and is put, the first rotation axis
It is set in first beam column on right side and slides conduction device in fact to slide striking for mating connection with male rotor, on the right side of the first rotation axis
Set sealed adjusting apparatus in second beam column, the second beam column top surface on the upside of sealed adjusting apparatus sets real to slide conduction dress with striking
It puts the sealed conduction device for coordinating sealed connection, continues back and forth to carry out slope to strike positive activity so as to fulfill automatically controlling, together
When, it can realize the sealed work of adjust automatically control push rod, stability when improving transport or carrying.
2. it is put by striking actual load including sliding the support rod set that is connected and extends up and down, support rod top with push rod
Extension tail end is visited to outside push rod top surface and the fixed restricted driving block in outer surface, and extension tail end in support rod bottom is visited to outside push rod bottom surface and tail
Solid plate is struck in end installation, strikes the fixed solid block of supporting rod outer surface between solid plate and push rod, Gu outside the support rod between block and push rod
Surface sets spring coil, generates larger impact force in real time so as to fulfill reducing to strike, plays preferable cushioning effect, improves and use the longevity
Life.
3. the configuration of the present invention is simple, easy to operate, can realize automatically control continue back and forth to carry out slope strike positive activity,
Meanwhile can realize the sealed work of adjust automatically control push rod, stability when improving transport or carrying, and time saving and energy saving, effect
Rate is high, and soil layer is closely knit, and electric pole fixing-stable reduces the time of work, reduces financial cost, shortens the work of construction
Phase.
The above description is merely a specific embodiment, but protection scope of the present invention is not limited thereto, any
The change or replacement expected without creative work, should be covered by the protection scope of the present invention.Therefore, it is of the invention
Protection domain should be determined by the scope of protection defined in the claims.
Claims (9)
1. a kind of power cable stringer of stabilization, including matrix and the fuselage of baseline top, feature are fixedly mounted on
It is：Perforation body bottom surface is equipped in fuselage installs chamber, installs first for matching above and below intracavitary portion and extending equipped with left and right and setting
Extension tail end is fixed respectively with installing inner wall at left and right sides of chamber at left and right sides of beam column and the second beam column, the first beam column and the second beam column
Connection, the matrix top surface for installing bottom of chamber portion are installed with and put in the first motor for installing intracavitary, at the top of the first motor cooperation connect
The first rotation axis for extending set upwards is connected to, extension penetrates through the second beam column and the first beam from bottom to up at the top of the first rotation axis
Column and rotatable engagement connection, the first rotation axis top extension tail end put in the intracavitary of installing of the first beam column over top, the first beam
The first rotation axis outer surface above column top is installed with male rotor, installing intracavitary equipped with top surface and install chamber above male rotor
Inner roof wall slides mating connection and left and right the is extended push rod set, outer wall and sliding is matched somebody with somebody on the left of extension perforation fuselage on the left of push rod
Connection is closed, extension penetrates through fuselage outer right wall and slides mating connection on the right side of push rod, and extension tail end is visited to fuselage on the right side of push rod
Outside right flank, visit to sliding in the push rod outside fuselage right flank to be connected with and strike actual load and put, first on the right side of the first rotation axis
It is equipped in beam column and slides conduction device in fact to slide striking for mating connection with male rotor, the second beam column on the right side of the first rotation axis
Interior to be equipped with sealed adjusting apparatus, the second beam column top surface on the upside of sealed adjusting apparatus is equipped with real to slide conduction device with striking and match somebody with somebody
The sealed conduction device of sealed connection is closed, matrix top surface is fixedly installed lamppost, and fore-set right flank is fixedly installed headlamp, shines
Bright lamp periphery is fixedly installed focused lamp cover, and base bottom is provided with brake stop device.
2. a kind of power cable stringer of stabilization according to claim 1, it is characterised in that：The fuselage outer side
The first solid bar is installed at left and right sides of left and right sides bottom and described matrix between top, outer wall is installed on the left of the fuselage
Extend the push rod set to upper left side.
3. a kind of power cable stringer of stabilization according to claim 1, it is characterised in that：First motor
Left and right sides outer wall matches equipped with the second solid bar, the left and right sides described second respectively with described install at left and right sides of chamber between inner wall
Gu top portion does not install the 3rd solid bar that matches at left and right sides of chamber between inner wall with described.
4. a kind of power cable stringer of stabilization according to claim 1, it is characterised in that：The actual load of striking puts bag
It includes and the support rod set that is connected and extends up and down is slided with the push rod, extension tail end is visited to described at the top of the support rod
Push rod top surface is outer and outer surface is installed with restricted driving block, and the support rod bottom extension tail end is visited to outside the push rod bottom surface and tail end
Be equipped with and strike solid plate, the supporting rod outer surface struck between solid plate and the push rod is installed with solid block, the solid block with
The supporting rod outer surface between the push rod is equipped with spring coil.
5. a kind of power cable stringer of stabilization according to claim 1, it is characterised in that：Described strike slides biography in fact
Leading device includes the first guide groove and slides the 3rd guide rod set that is equipped in first guide groove and extends up and down, institute
It states to slide in the 3rd guide rod in the first guide groove and is connected with the first guide rod that left and right extension is set, first guide rod
Left side tail end is fixedly connected with the first guide groove inner left wall, tail end and first guide groove right side on the right side of first guide rod
Inner wall is fixedly connected, and what extension put on the upside of first beam column at the top of the 3rd guide rod described installs intracavitary and top tail
End is fixedly connected with push rod bottom, and the 3rd guide rod that intracavitary is installed described on the upside of first beam column is located on the right side of the male rotor
Position, installed described on the upside of first beam column the 3rd guide rod right flank of intracavitary on the upside of first beam column described in install chamber
The 3rd interior guide rod right flank opposite described install is equipped with the first spring coil between inner wall on the right side of chamber, the 3rd guide rod bottom is prolonged
What exhibition tail end put between first beam column and second beam column described installs intracavitary.
6. a kind of power cable stringer of stabilization according to claim 5, it is characterised in that：The sealed conduction dress
The second guide groove is equipped in putting, extend the first spiral shell shape bar set in second guide groove equipped with left and right, and the first spiral shell shape bar is left
Extension tail end in side is connected with the second guide groove inner left wall rotatable engagement, on the right side of the first spiral shell shape bar extension tail end with it is described
Inner wall rotatable engagement connection on the right side of second guide groove, the first spiral shell shape bar left side are installed with the first taper cone pulley, institute on section outer surface
It states whorl on the first spiral shell shape bar on the right side of the first taper cone pulley and is connected with the guide block for extending set upwards, the guide block
Top extension tail end is visited to outside the sealed conduction device top surface and tail end is installed with the cross bar for setting of extending to the left, the cross bar
Left side extension tail end is installed with the locking pole for extending set upwards, and the locking pole is located at the 3rd guide rod bottom extension tail end
Leftward position and be oppositely arranged, slided in the guide block on the upside of first taper cone pulley be connected with left and right extend set
The second guide rod, extension tail end is fixed respectively with inner wall at left and right sides of second guide groove at left and right sides of second guide rod connects
It connects.
7. a kind of power cable stringer of stabilization according to claim 6, it is characterised in that：The sealed adjustment dress
Put including the 3rd guide groove and slide the adjustment block being equipped in the 3rd guide groove, at the top of the 3rd guide groove with it is described
Second guide groove left bottom connects setting, and the adjustment block inner spiral line is connected with left and right and extends the second spiral shell shape set
Bar, the second spiral shell shape bar left side extension tail end are connected with the 3rd guide groove inner left wall rotatable engagement, the second spiral shell shape
Extension tail end is connected with adjustment motor on the right side of bar, and the adjustment motor outer surface is arranged on the right side of the 3rd guide groove
It in inner wall and is fixedly connected, rotation is connected in the adjustment block on front side of the second spiral shell shape bar extends what is set up and down
Second rotation axis, at the top of second rotation axis extension tail end put in second guide groove and tail end be installed with to it is described
Second taper cone pulley of the ratcheting connection of the first taper cone pulley, the second rotation axis bottom extension tail end are put on the downside of second beam column
Described install intracavitary and tail end is installed with the first toothed wheel.
8. a kind of power cable stringer of stabilization according to claim 7, it is characterised in that：Under second beam column
The second toothed wheel being oppositely arranged with the first toothed wheel left-hand end is installed on the first rotation axis outer surface of side.
9. a kind of power cable stringer of stabilization according to claim 1, it is characterised in that：The brake stop device bag
It includes and is fixed at the brake of described matrix bottom surface and stops lock and be fixed at the left side brake stopped on the left of lock of stopping to stop sole, it is described
Brake stops the outside that lock is separately positioned on bottom surface wheel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710931539.2A CN108086781A (en) | 2017-10-09 | 2017-10-09 | A kind of power cable stringer of stabilization |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710931539.2A CN108086781A (en) | 2017-10-09 | 2017-10-09 | A kind of power cable stringer of stabilization |
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| Publication Number | Publication Date |
|---|---|
| CN108086781A true CN108086781A (en) | 2018-05-29 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710931539.2A Pending CN108086781A (en) | 2017-10-09 | 2017-10-09 | A kind of power cable stringer of stabilization |
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| Country | Link |
|---|---|
| CN (1) | CN108086781A (en) |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2328824A1 (en) * | 1975-10-22 | 1977-05-20 | Risler Robert | Overhead power cable support - comprises tubular base section anchored to concrete slab with cable stayed support masts |
| CN105442521A (en) * | 2015-12-26 | 2016-03-30 | 刘汉佑 | Multifunctional tamping machine |
-
2017
- 2017-10-09 CN CN201710931539.2A patent/CN108086781A/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2328824A1 (en) * | 1975-10-22 | 1977-05-20 | Risler Robert | Overhead power cable support - comprises tubular base section anchored to concrete slab with cable stayed support masts |
| CN105442521A (en) * | 2015-12-26 | 2016-03-30 | 刘汉佑 | Multifunctional tamping machine |
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Application publication date: 20180529 |
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