CN209380802U - A kind of modularization cable stock-removing machine - Google Patents
A kind of modularization cable stock-removing machine Download PDFInfo
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- CN209380802U CN209380802U CN201822146174.5U CN201822146174U CN209380802U CN 209380802 U CN209380802 U CN 209380802U CN 201822146174 U CN201822146174 U CN 201822146174U CN 209380802 U CN209380802 U CN 209380802U
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Abstract
The utility model discloses a kind of modularization cable stock-removing machines, including fuselage, cable clamp mechanism on the outer end face of fuselage rear and front end, in fuselage interior and cable clamp mechanism cable cutting mechanism disposed in parallel, in the turntable mechanism of cable cutting mechanism rear driving cable cutting mechanism rotation, and the axial feed mechanism for driving turntable mechanism to be axially moved along fuselage；Cable cutting mechanism includes the turntable that can be rotated under turntable mechanism driving, the center of turntable is equipped with the turntable through-hole passed through for cable, the front end face of turntable is equipped with the cutter that point of a knife is directed toward the center of circle of turntable through-hole, connect cutter, for controlling the cutting servo motor of radial motion of the cutter along turntable through-hole, for monitoring the turntable grating scale of the position of tool tip of cutter, and two range sensors corresponding with turntable grating scale and cutting servo motor.
Description
Technical field
The utility model relates to a kind of modularization cable stock-removing machines of cable insulating process field.
Background technique
Become, in power engineering, one end of high voltage cable needs to cut suitable shape, to connect another termination
Head.The construction for making a general survey of domestic most such engineerings is all by manual cutting, and manual cutting is long there are the cutting time, and precision is difficult to
Control, and it is related with artificial qualification, while if the increasing for cutting difficulty can be caused by carrying out cutting in narrow place
Add, and the phenomenon relatively high there are recruitment cost.It is shown for domestic high voltage cable automatic cutting this respect data, it is domestic at present
It there is no this automatic cutting equipment, more simply for the hand-operated simple peeling machine within 30mm, simple peeling machine is not only not
It is able to satisfy the size requirement of Large-scale High-Pressure cable, the construction requirement at scene is also not achieved in precision, while also can not the line of cut
Insulating layer inside cable.
The working principle of the cable insulating processing equipment of foreign countries' exploitation is that stepper motor drives swivel head to rotate, on swivel head
Stepper motor band cutting blade move up and down, to realize the cutting of cable insulation layer.But the equipment can only handle Nippon Standard
Cable, and it is expensive.
The application for a patent for invention of 106513712 A of Publication No. CN is a kind of traditional stock-removing machine, passes through workpiece
Rotatable engagement cutter rotates to realize the cutting to workpiece.This cutting way positioning accuracy is poor, and is difficult to long axis large size
Cable is cut.
The application for a patent for invention of 104057102 A of Publication No. CN, increases thimble, centainly on the basis of above-mentioned patent
Cutting precision is improved in degree.But it since the copper core of cable end face can be destroyed by thimble, is not particularly suited for cable
It is cut.
The utility model patent of 104617524 B of Publication No. CN can only carry out at peeling some small size cables
Reason is not able to satisfy the size requirement of Large-scale High-Pressure cable, high requirement is also not achieved in precision, while can not cut cable yet
Internal insulating layer.
Utility model content
The purpose of this utility model is to overcome the deficiencies in the prior art, provide a kind of modularization cable stock-removing machine,
It can accurately cut the insulating layer of cable according to the shape of cable.
Realizing a kind of technical solution of above-mentioned purpose is: a kind of modularization cable stock-removing machine, including fuselage are located at fuselage
Cable clamp mechanism on the outer end face of rear and front end, in the fuselage interior and the cable clamp mechanism line disposed in parallel
Cable cutting mechanism drives the turntable mechanism of the cable cutting mechanism rotation at cable cutting mechanism rear, and is used for
The axial feed mechanism for driving the turntable mechanism to be axially moved along the fuselage；
The cable cutting mechanism includes the turntable that can be rotated under turntable mechanism driving, and the center of the turntable is set
There is the turntable through-hole passed through for cable, the front end face of the turntable is equipped with the knife that point of a knife is directed toward the center of circle of the turntable through-hole
Tool, connects the cutter, for controlling the cutting servo motor of radial motion of the cutter along the turntable through-hole, for supervising
The turntable grating scale of the position of tool tip of the cutter is controlled, and corresponding with the turntable grating scale and the cutting servo motor
Two range sensors.
Further, the front end face of the turntable be equipped with for fix the cutter and with the cutter axially parallel rolling
Ballscrew, the ball-screw be equipped with feed screw nut, the feed screw nut be equipped with nut platform, the turntable grating scale with
The ball-screw is parallel and connects side of the nut platform far from the cutting servo motor, the cutting servo motor
By deceleration band connection between the feed screw nut, the turntable grating scale is equipped with original far from one end of respective distances sensor
Level sensor.
Further, the front end face of the turntable is equipped with the chip breaking serrated knife that point of a knife is directed toward the turntable through hole center.
Further, the turntable mechanism includes running through the turntable positioned at the turntable at the turntable rear and front end,
And fixed with the center of the turntable, for driving the turntable to rotate, hollow multi-diameter shaft；
It is coaxially socketed with slip ring on the multi-diameter shaft, and is socketed in the ladder shaft end and coaxially consolidates with the slip ring
Fixed circular grating, the rear of the circular grating is coaxially fixed with end flange, between the end flange and the turntable
Equipped with turntable bearing support.
Further, the turntable bearing being socketed with the multi-diameter shaft is equipped between the turntable and the multi-diameter shaft, with
And it is socketed in the turntable bearing radial outside, and the bearing flange fixed with the turntable；
The rear of the bearing flange, equipped with fixed with the turntable rear end face and with the excircle of the multi-diameter shaft be socketed
First sleeve, and be socketed with the multi-diameter shaft and the second sleeve fixed with the first sleeve rear end face；
It between the second sleeve and the slip ring, is equipped with and is socketed with the multi-diameter shaft, for driving the multi-diameter shaft to revolve
The belt wheel turned.
Further, the axial feed mechanism is fixed in the fuselage, including in the fuselage from back to front
Axial feed servo motor, shaft coupling and the linear mould group set gradually；
The axial feed servo motor connects the shaft coupling, and the shaft coupling connects the linear mould group, the line
Property mould group top be equipped in fuselage with the linear mould group axial grating scale disposed in parallel, meet institute by the linear mould group
State turntable.
Further, the cable clamp mechanism includes being fixed on the three-jaw clamping of the outer end face of the fuselage corresponding end
Mechanism, and set gradually from top to bottom handle, torque force limiting device, transmission shaft and the transmission is socketed in by flat key
The scroll bar of the diameter of axle outward, the scroll bar and the three-jaw clamping mechanism are tangent；
By being fixed on the first of the outer end face of the fuselage corresponding end between the handle and the torque force limiting device
Bearing block connection, by being fixed on the outer end face of the fuselage corresponding end between the torque force limiting device and the transmission shaft
Second bearing seat connection, the bottom end of the transmission shaft is sleeved and fixed the outer end face 3rd bearing seat in the fuselage corresponding end.
Further, proximity sensor is fixed at the top of the torque force limiting device.
Further, the three-jaw clamping structure includes chuck, turbine and three claws；
The chuck is fixed on the outer end face of fuselage corresponding end, the chuck be equipped with chuck through-hole and with the card
The corresponding chuck axis of disk through-hole, the turbine is in the chuck back to one end of the fuselage and the excircle set of the chuck axis
It connects, is cooperated between the excircle of the chuck axis and the turbine by deep groove ball bearing；
The chuck is led towards three claws that the side of the fuselage is equipped with the circumference uniform distribution around the chuck through-hole
Rail, the claw guide rail is radial parallel with the chuck through-hole, axial direction of the claw along corresponding claw guide rail, clamping
In corresponding claw guide rail, axial parallel, the guide rail of kidney ellipsoid with the claw guide rail is equipped on each claw guide rail
Through-hole；
Three vortex filament sliding slots of the circumference uniform distribution around the chuck axis are additionally provided on the turbine；The vortex filament sliding slot with
The slide bar connected with corresponding claw is equipped between corresponding guide rail through-hole.
Further, the side of the fuselage is bolted display bracket, fixes on the display bracket
There is touch screen.
Using a kind of technical solution of modularization cable stock-removing machine of the utility model, including fuselage, it is located at fuselage
Cable clamp mechanism on the outer end face of rear and front end, in the fuselage interior and the cable clamp mechanism line disposed in parallel
Cable cutting mechanism drives the turntable mechanism of the cable cutting mechanism rotation at cable cutting mechanism rear, and is used for
The axial feed mechanism for driving the turntable mechanism to be axially moved along the fuselage；The cable cutting mechanism includes can be described
The lower turntable rotated of turntable mechanism driving, the center of the turntable are equipped with the turntable through-hole passed through for cable, before the turntable
End face is equipped with the cutter that point of a knife is directed toward the center of circle of the turntable through-hole, the cutter is connected, for controlling the cutter along institute
The cutting servo motor for stating the radial motion of turntable through-hole, the turntable grating scale of the position of tool tip for monitoring the cutter, with
And two range sensors corresponding with the turntable grating scale and the cutting servo motor.Its technical effect is that: use pair
The module answered completes cable clamp, the circumference fortune of cable depth of cut, cable Cutting Length and the cutter for cutting to cable
It is dynamic to be controlled, have many advantages, such as that control precision is high, high-efficient, stability is good, job security is good, it is user-friendly for operation, for
The remodeling of lathe, upgrading, assembly and mass production to numerically-controlled machine tool are all of great significance, and modularized design makes the numerical control
Stock-removing machine is convenient for safeguarding and repairs.
Detailed description of the invention
Fig. 1 is a kind of perspective view of modularization cable stock-removing machine of the utility model.
Fig. 2 is a kind of main view of the cable clamp mechanism of modularization cable stock-removing machine of the utility model.
Fig. 3 is a kind of A-A of the cable clamp mechanism of modularization cable stock-removing machine of the utility model to cross-sectional view.
Fig. 4 is a kind of structure chart of the turbine of modularization cable stock-removing machine of the utility model.
Fig. 5 is a kind of structure chart of the chuck of modularization cable stock-removing machine of the utility model.
Fig. 6 is a kind of perspective view of the cutting mechanism of modularization cable stock-removing machine of the utility model.
Fig. 7 is a kind of perspective view of the axial feed mechanism of modularization cable stock-removing machine of the utility model.
Fig. 8 is a kind of structure chart of the turntable of modularization cable stock-removing machine of the utility model.
Specific embodiment
Please refer to Fig. 1 to Fig. 8, the inventor of the utility model in order to preferably to the technical solution of the utility model into
Row understands, below by specifically embodiment, and will be described in detail with reference to the accompanying drawings:
Referring to Fig. 1, a kind of modularization cable stock-removing machine of the utility model includes fuselage 1, cable clamp mechanism 2,
Cable cutting mechanism 3, axial feed mechanism 5 and turntable mechanism 6.A kind of modularization cable stock-removing machine of the utility model uses
Modularized design can be realized the processing and fabricating of complex configuration.
In a kind of modularization cable stock-removing machine of the utility model, fuselage 1 include front console 11, rear end panel 12,
First side plate 13 and second side plate 14.To enable a kind of modularization cable stock-removing machine of the utility model flexibly to move
Dynamic, four idler wheels 15 that can be stuck are added in the bottom surface of fuselage 1.It is correspondingly provided on the front console 11 and rear end panel 12 of fuselage 1
The faceplate through holes passed through for cable.The top surface of fuselage 1 is equipped with shield 18.
The quantity of cable clamp mechanism 2 is two, is located at the front console 11 of fuselage 1 and the outer end of rear end panel 12
On face.Cable cutting mechanism 3, axial feed mechanism 5 and turntable 6 are respectively positioned on inside fuselage 1.
Fig. 2~5 are please referred to, cable clamp mechanism 2 includes the three-jaw clamping machine that chuck 21, turbine 22 and claw 23 form
Structure.
Chuck 21 is bolted on fuselage 1.The center of chuck 21 is equipped with chuck corresponding with corresponding panel through-hole
Axis, and the chuck through-hole 211 positioned at the chuck axis center.Turbine 22 is in one side of the chuck 21 back to fuselage 1 and the card
The excircle of dish axle is socketed.The center of turbine 22 is equipped with turbine through-hole 221.The excircle and turbine through-hole 221 of the chuck axis
Between cooperated by deep groove ball bearing 251, deep groove ball bearing 251 realizes the axial limiting to turbine 22 and reduces whirlpool
Sliding friction between wheel 22 and chuck 21.It is correspondingly provided with and is used on the excircle of turbine through-hole 221 and the chuck axis simultaneously
It is clamped the groove of bearing sealed ring 252, bearing sealed ring 252 realizes the sealing to deep groove ball bearing 251.
The inner periphery of the excircle and the faceplate through holes of corresponding end panel of side of the chuck axis towards fuselage 11 is matched
It closes, and on the side end face of the chuck axis, surrounds chuck through-hole 211, uniformly distributed there are three radial parallel with chuck through-hole 211
Claw guide rail 212, claw 23 is connected to pair along the axial direction of corresponding claw guide rail 212 with the snap fit of wedge shape clamping
In the claw guide rail 212 answered.It is clamped between claw 23 and corresponding claw guide rail 212 in staged.In other words claw guide rail
212 be stepped claw guide rail 212, and the cross sectional shape of claw guide rail 212 is convex shape in other words.Claw guide rail 212 includes
Slot bottom 212a, and in the two sides the slot bottom 212a stepped first rail groove 212b set gradually and the second guide-track groove 212c.
Slot bottom 212a is equipped with and axial parallel, the guide rail through-hole 213 of kidney ellipsoid of claw guide rail 212.
Three vortex filament sliding slots 222 of the circumference uniform distribution around turbine through-hole 221, vortex filament sliding slot 222 are additionally provided on turbine 22
Shape be the long axis of kidney ellipsoid and vortex filament sliding slot 222 be a vortex filament tangent with the excircle of turbine through-hole 221.Vortex filament
Slide bar 24 is equipped between sliding slot 222 and corresponding guide rail through-hole 213, one end of slide bar 24 is plugged on corresponding vortex filament sliding slot 222
It is interior, and can be along the axial direction sliding in corresponding vortex filament sliding slot 222.The other end of slide bar 24 runs through corresponding guide rail through-hole 213,
Corresponding claw 23 is connected, and can be slid along the axial direction of corresponding rails through-hole 213.
When turbine 22 rotates, drive claw 23 along the axial movement of corresponding claw guide rail 212 by slide bar 24, it is real
Existing movement of the claw 23 in chuck 21 in the radial direction, to realize the clamping to cable.
Measure as a further improvement, along the axial direction of corresponding claw guide rail 212, claw 210 is divided into front claw with after
Claw clamps slide bar 24, consequently facilitating the processing and replacement of claw 23.
Cable clamp mechanism 2 further includes the handle 201 set gradually from top to bottom, torque force limiting device 202, transmission shaft
203 and the scroll bar 204 of 203 radial outside of transmission shaft is socketed in by flat key.Scroll bar 204 and turbine 22 are tangent.
Wherein connected between handle 201 and torque force limiting device 202 by being fixed on the first bearing seat 205 at 21 top of chuck
It connects.It is connected between torque force limiting device 202 and transmission shaft 203 by the second bearing seat 206 being fixed on chuck 21.Third axis
Seat 207 is held to be socketed in the bottom end of transmission shaft 203 and be fixed on chuck 21.Torque force limiting device 202 is fixed on close to switch 200
Top.Close to switch 208 will whether clamping be fed back to cable.
Meanwhile torque force limiting device 202 is supported by the first square groove 202a being fixed on chuck 21, scroll bar 204
It is supported by the second square groove 204a being fixed on chuck 21.
Meanwhile the square hole of the first square groove 202a and second square groove 204a for fixing are provided on chuck 21, on
The design stated, so that 2 structure of cable clamp mechanism is more compact.
Torque force limiting device 202 works cable clamp is next, prevents handle 201 from skidding.It is realized pair by scroll bar 204
Claw 23 it is self-locking.
Referring to Fig. 6, cable cutting mechanism 3 includes turntable 30, cutter 31, cutting servo motor 32, deceleration strip 33, rolling
Ballscrew 34 and turntable grating scale 35.Turntable 30 is located at 1 middle part of fuselage, is arranged in parallel with front console 11 and rear end panel 12.
The center of turntable 30 is equipped with the turntable through-hole 301 passed through for cable.Turntable grating scale 35, cutting servo motor 32 and ball-screw
34 are each attached to the front end face of turntable 30, and wherein by fixed frame 340, radially fixed along turntable 30 is turning ball-screw 34
The front end face of disk 30, turntable grating scale 35 and cutting servo motor 32 are set the two sides of ball-screw 34 are parallel with ball-screw 34
It sets.Wherein cutting servo motor 32 is fixed on the front end face of turntable 30 by motor cabinet 321.Cutting servo motor 32 is by subtracting
Speed belt 33 is connect with ball-screw 34.Nut platform 341 is installed on the feed screw nut of ball-screw 34.Turntable grating scale 35
It is mounted on side of the nut platform far from cutting servo motor 31, turntable grating scale 35 and turntable 30 are fixed.Cutter 31 is solid
It is scheduled on nut platform 341, and the point of a knife of cutter 31 is directed toward the center of circle of turntable through-hole 301.It is also equipped on turntable 30 positioned at lead screw
34 two sides of nut, two range sensors 36 corresponding with cutting servo motor 32 and 35 position of turntable grating scale.Turntable light
Grid ruler 35 can feed back the displacement of cutter 31, and two range sensors 36 can realize the real-time detection to cable shape.
By the two Feedback Designs, realizes and the high-precision of cable cutting depth is controlled.The front end face of turntable 30 also fixes one
The chip breaking serrated knife 37 for being directed toward the center of circle of turntable through-hole 301 avoids clast pair so that the clast that cutter 31 is cut be cut off
Unnecessary influence caused by cutting.The string holes 302 being arranged there are three being also distributed on turntable 30 around turntable through-hole 301.
As a further improvement, in one end addition in situ sensing of the turntable grating scale 35 far from respective distances sensor 36
Device, thus guarantee cutter 31 can rapid return return to dead-center position.
As a further improvement, by the front end face of turntable 30 be equipped with threaded hole, so as to ball-screw 34 feed screw nut with
And nut platform 341 passes through one piece of connecting plate cooperation.
Referring to Fig. 8, turntable mechanism 6 includes turntable 60, table servo motor 61, planetary reduction gear 62, and through same
Axis runs through turntable 60, fixes with the center of turntable 30, hollow multi-diameter shaft 63.Table servo motor 61 and planetary reduction gear 62 are same
Axis connection, wherein the rear end panel 12 of table servo motor 61 and fuselage 1 is fixed, and planetary reduction gear 62 is fixed on by fixed plate
Turntable 60 is back to the side of turntable 30.The front end of multi-diameter shaft 63 is bolted with turntable 30.The excircle of multi-diameter shaft 63 is set
There are three wire casings 631, is corresponded with three string holes 302 on turntable 30.
The inner periphery of turntable 60 is equipped with hollow bearing flange 64.It is bolted between bearing flange 64 and turntable 60
Connection.The inner ring of bearing flange 64 is equipped with turntable bearing 65.The inner ring of turntable bearing 65 and the excircle of multi-diameter shaft 63 cooperate,
The excircle of turntable bearing 65 and the inner periphery of bearing flange 64 cooperate.
First sleeve 66 is close to the rear end face of turntable bearing 65 and bearing flange 64, and fixes with the rear end face of turntable 60,
Second sleeve 67 and first sleeve 66 are coaxially disposed, and are close to the rear end face of first sleeve 66, and fixed with first sleeve 66, on
The design stated makes first sleeve 66 and second sleeve 67 squeezes the Internal and external cycle of turntable bearing 65, and the preceding shaft shoulder with multi-diameter shaft 63
With 64 collective effect of bearing flange in turntable bearing 65, to make transmitting of 63 or so the axial force of multi-diameter shaft to turntable 60.Turntable
Bearing 65 is deep groove ball bearing.
Belt wheel 68 is located at the rear side of second sleeve 67, and is socketed on the axle journal of multi-diameter shaft 63 by flat key.Planetary reduction gear
It is connected between device 62 and belt wheel 68 by synchronous belt, table servo motor 61 makes belt wheel 68 by putting down by planetary reduction gear 62
Key imparts power to multi-diameter shaft 63, then turntable 30 has been imparted power to by multi-diameter shaft 63, since cutter 31 is assemblied in
On turntable 30, to realize rotate in a circumferential direction movement of the cutter 31 with respect to cable.
The rear side of belt wheel 68 is additionally provided with the slip ring 69 being socketed on 63 excircle of multi-diameter shaft, and the rear end of slip ring 69 passes through spiral shell
The coaxially connected circular grating 610 for being socketed in 63 rear end face of multi-diameter shaft of bolt.The rear end of circular grating 610 is coaxially connected by bolt
End flanges 611 afterwards are connected with three horizontal turntable bearing supports 612 between rear end flanges 611 and turntable 60.
Power is transmitted to belt wheel 68 by synchronous belt by planetary reduction gear 62, and belt wheel 68 imparts power to ladder by flat key
Axis 63 rotates multi-diameter shaft 63, has then imparted power to turntable 30 by multi-diameter shaft 63, and turntable 30 rotates.Circular grating
The movement that rotates in a circumferential direction of 610 pairs of multi-diameter shafts 63 and turntable 30 carries out position feedback, to ensure that essence when cutter 31 rotates
Degree requires.Pass through rear end flanges 611, circular grating 610, slip ring 69, belt wheel 68, second sleeve 67, first sleeve 66, turntable axis
65 are held, bearing flange 64, multi-diameter shaft 63, turntable 60 realize the whole axial restraint of cutting mechanism 3 Yu turntable mechanism 6, make line
Cable cutting mechanism 3 and turntable mechanism 6 can with axial feed mechanism 5 together relative to cable synchronize axially move.Planet subtracts
It can be by flanged joint, to realize solid to axial between belt wheel 68 to it between fast device 62 and table servo motor 61
It is fixed.It is provided with the square hole of fixed table servo motor 61 on the rear end panel 12 of fuselage 1, prevents table servo motor 61 and slip ring 68
Between interfere.
Three wire casings 631 of 63 outer circumference surface of multi-diameter shaft communicate, cable cutter with three string holes 302 in turntable 30
The control line of structure 3 and turntable mechanism 6 successively passes through the corresponding string holes 302 in turntable 30 and the wire casing 631 in multi-diameter shaft 63, with
The connection of 69 internal layer of slip ring, avoids since cable cutting mechanism 3 is with cutting tip control line caused by 63 axial-rotation of multi-diameter shaft
The problem of winding.
Referring to Fig. 7, axial feed mechanism 5 includes the axial direction successively axially connected in the first side plate 13 of fuselage 1
Feed servo motor 51, shaft coupling 52 and linear mould group 53, wherein axial feed servo motor 51 is located at close to the rear end of fuselage 1
The side of panel 12, linear mould group 53 are located at close to the side of front console 11.The top of linear mould group 53, which is equipped with, is fixed on machine
Axial grating scale 54 in the first side plate 13 of body 1.Axial feed of the axial grating scale 54 to axial feed servo motor 51
It is fed back, improves axial feed motion precision, control the length cut to cable.Linear mould group 53 includes horizontal ball
Lead screw and turntable feed screw nut, turntable feed screw nut by gusset and bolt and the turntable 60 in turntable mechanism 6 by connecing.Axis
It is connect to feed servo motor 51 by shaft coupling 52 with the horizontal ball-screw, to realize the axial movement of turntable 60.
Meanwhile three rigid supports 55, three rigid supports are equipped between the front console 11 and rear end panel 12 of fuselage 1
Support sleeve 56 is equipped between 55 and turntable 60, three support sleeves 56 are fixed by bolt and turntable 60, reach realization and bear
The purpose of entire cable cutting mechanism 3 and 6 weight of turntable mechanism.As a further improvement, rigid support 55 is processed as spending
Bond type, so that it is guaranteed that axial precision when being axially moved.
The side of the front console 11 of fuselage 1 is bolted display bracket 16, the freedom of display bracket 16
Degree is two, and touch screen 17 is fixed by bolt and display bracket 16, and connects the cutting in cutting mechanism 3 by control line
Servo motor 32, turntable grating scale 35, range sensor 36, home position sensing, 61 He of table servo motor in turntable mechanism 6
Axial feed servo motor 51, linear mould group 53 and axial grating scale 54 in circular grating 610 and axial feed mechanism 5,
Consequently facilitating personnel operate.
A kind of modularization cable stock-removing machine of the utility model completes cable clamp using corresponding module, and cable is cut
The circular motion for cutting depth, cable Cutting Length and the cutter for cutting to cable controls, and has control precision height, effect
The advantages that rate is high, stability is good, job security is good, user-friendly for operation.For the remodeling of lathe, upgrading, to numerically-controlled machine tool
Assembly and mass production are all of great significance, and modularized design keeps the numerically controlled machine tool convenient for safeguarding and repairs.
Those of ordinary skill in the art it should be appreciated that more than embodiment be intended merely to illustrate that this is practical new
Type, and be not used as the restriction to the utility model, as long as in the spirit of the utility model, to the above
Variation, the modification of embodiment will all be fallen in the Claims scope of the utility model.
Claims (10)
1. a kind of modularization cable stock-removing machine, including fuselage, it is characterised in that:
It further includes the cable clamp mechanism on the outer end face of fuselage rear and front end, in the fuselage interior and the cable
Clamping device cable cutting mechanism disposed in parallel drives the cable cutting mechanism rotation at cable cutting mechanism rear
Turntable mechanism, and the axial feed mechanism for driving the turntable mechanism to be axially moved along the fuselage；
The cable cutting mechanism includes the turntable that can be rotated under turntable mechanism driving, and the center of the turntable, which is equipped with, to be supplied
The turntable through-hole that cable passes through, the front end face of the turntable are equipped with the cutter that point of a knife is directed toward the center of circle of the turntable through-hole, even
The cutter is connect, for controlling the cutting servo motor of radial motion of the cutter along the turntable through-hole, for monitoring
The turntable grating scale of the position of tool tip of cutter is stated, and two corresponding with the turntable grating scale and the cutting servo motor
Range sensor.
2. a kind of modularization cable stock-removing machine according to claim 1, it is characterised in that: the front end face of the turntable is set
Have for fixing the cutter and axially parallel ball-screw, the ball-screw are equipped with feed screw nut with the cutter,
The feed screw nut is equipped with nut platform, and the turntable grating scale is parallel with the ball-screw and connects the nut platform
Side far from the cutting servo motor, passes through deceleration band connection between the cutting servo motor and the feed screw nut,
The turntable grating scale is equipped with home position sensing far from one end of respective distances sensor.
3. a kind of modularization cable stock-removing machine according to claim 1, it is characterised in that: the front end face of the turntable is set
There is point of a knife to be directed toward the chip breaking serrated knife of the turntable through hole center.
4. a kind of modularization cable stock-removing machine according to claim 1, it is characterised in that: the turntable mechanism includes position
Run through the turntable in the turntable at the turntable rear and front end, and is fixed with the center of the turntable, it is described for driving
Turntable rotation, hollow multi-diameter shaft；
Slip ring, the ladder shaft end socket and the co-axially fixed ring light of the slip ring are coaxially socketed on the multi-diameter shaft
Grid, the rear of the circular grating are coaxially fixed with end flange, and turntable branch is equipped between the end flange and the turntable
Bolster.
5. a kind of modularization cable stock-removing machine according to claim 4, it is characterised in that: the turntable and the ladder
Be equipped with the turntable bearing that is socketed with the multi-diameter shaft between axis, and be socketed in the turntable bearing radial outside, and with it is described
The fixed bearing flange of turntable；
The rear of the bearing flange, equipped with fixed with the turntable rear end face and with the socket of the excircle of the multi-diameter shaft the
One sleeve, and the second sleeve for being socketed with the multi-diameter shaft and being fixed with the first sleeve rear end face；
The rear of the second sleeve is equipped with and is socketed with the multi-diameter shaft, for driving the belt wheel of the multi-diameter shaft rotation.
6. a kind of modularization cable stock-removing machine according to claim 4, it is characterised in that: the axial feed mechanism is solid
It is scheduled in the fuselage, including axial feed servo motor, shaft coupling and the line set gradually from back to front in the fuselage
Property mould group；
The axial feed servo motor connects the shaft coupling, and the shaft coupling connects the linear mould group, the linear mould
The top of group be equipped in fuselage with the linear mould group axial grating scale disposed in parallel, connect described turn by the linear mould group
Platform.
7. a kind of modularization cable stock-removing machine according to claim 1, it is characterised in that: cable clamp mechanism packet
Include the three-jaw clamping mechanism for being fixed on the outer end face of the fuselage corresponding end, and set gradually from top to bottom handle, turn round
Force-limiting device, transmission shaft and the scroll bar that the transmission shaft radial outside is socketed in by flat key, the scroll bar and the three-jaw
Clamping mechanism is tangent；
By being fixed on the first bearing of the outer end face of the fuselage corresponding end between the handle and the torque force limiting device
Seat connection, by being fixed on the second of the outer end face of the fuselage corresponding end between the torque force limiting device and the transmission shaft
Bearing block connection, the bottom end of the transmission shaft is sleeved and fixed the outer end face 3rd bearing seat in the fuselage corresponding end.
8. a kind of modularization cable stock-removing machine according to claim 7, it is characterised in that: the top of the torque force limiting device
Portion is fixed with proximity sensor.
9. a kind of modularization cable stock-removing machine according to claim 7, it is characterised in that: the three-jaw clamping structure packet
Include chuck, turbine and three claws；
The chuck is fixed on the outer end face of the fuselage corresponding end, the chuck be equipped with chuck through-hole and with the card
The corresponding chuck axis of disk through-hole, the turbine is in the chuck back to one end of the fuselage and the excircle set of the chuck axis
It connects, is cooperated between the excircle of the chuck axis and the turbine by deep groove ball bearing；
The chuck is equipped with three claw guide rails of the circumference uniform distribution around the chuck through-hole, institute towards the side of the fuselage
State the radial parallel of claw guide rail and the chuck through-hole, the claw is connected to pair along the axial direction of corresponding claw guide rail
In the claw guide rail answered, axial parallel, the guide rail through-hole of kidney ellipsoid with the claw guide rail is equipped on each claw guide rail；
Three vortex filament sliding slots of the circumference uniform distribution around the chuck axis are additionally provided on the turbine；The vortex filament sliding slot with it is corresponding
Guide rail through-hole between be equipped with the slide bar that connects with corresponding claw.
10. a kind of modularization cable stock-removing machine according to claim 1, it is characterised in that: the side of the fuselage is logical
The fixed display bracket of bolt is crossed, is fixed with touch screen on the display bracket.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201822146174.5U CN209380802U (en) | 2018-12-20 | 2018-12-20 | A kind of modularization cable stock-removing machine |
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| CN209380802U true CN209380802U (en) | 2019-09-13 |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109454677A (en) * | 2018-12-20 | 2019-03-12 | 上海久隆电力（集团）有限公司 | A kind of modularization cable stock-removing machine |
| CN111687489A (en) * | 2020-05-26 | 2020-09-22 | 河钢乐亭钢铁有限公司 | Nylon pin continuous processing machine |
| CN112421349A (en) * | 2020-11-30 | 2021-02-26 | 济南大学 | Reaction force cone cutting device |
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2018
- 2018-12-20 CN CN201822146174.5U patent/CN209380802U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109454677A (en) * | 2018-12-20 | 2019-03-12 | 上海久隆电力（集团）有限公司 | A kind of modularization cable stock-removing machine |
| CN109454677B (en) * | 2018-12-20 | 2024-02-02 | 上海久隆电力（集团）有限公司 | Modularized cable cutting machine tool |
| CN111687489A (en) * | 2020-05-26 | 2020-09-22 | 河钢乐亭钢铁有限公司 | Nylon pin continuous processing machine |
| CN112421349A (en) * | 2020-11-30 | 2021-02-26 | 济南大学 | Reaction force cone cutting device |
| CN112421349B (en) * | 2020-11-30 | 2021-12-21 | 济南大学 | Reaction force cone cutting device |
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