CN109773064A - A kind of full-automatic draw machining center of full SERVO CONTROL - Google Patents
A kind of full-automatic draw machining center of full SERVO CONTROL Download PDFInfo
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- CN109773064A CN109773064A CN201811439783.8A CN201811439783A CN109773064A CN 109773064 A CN109773064 A CN 109773064A CN 201811439783 A CN201811439783 A CN 201811439783A CN 109773064 A CN109773064 A CN 109773064A
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- fuselage
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- machining center
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- 230000000712 assembly Effects 0.000 claims abstract description 12
- 238000000429 assembly Methods 0.000 claims abstract description 12
- 210000000078 claw Anatomy 0.000 claims description 25
- 238000006073 displacement reaction Methods 0.000 claims description 7
- 230000006835 compression Effects 0.000 claims description 2
- 238000007906 compression Methods 0.000 claims description 2
- 238000000034 method Methods 0.000 abstract description 7
- 238000012545 processing Methods 0.000 abstract description 7
- 238000003754 machining Methods 0.000 abstract description 2
- 238000004904 shortening Methods 0.000 abstract 1
- 230000002093 peripheral effect Effects 0.000 description 5
- 238000013461 design Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 2
- 239000003638 chemical reducing agent Substances 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 238000005056 compaction Methods 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
- 238000013519 translation Methods 0.000 description 1
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Abstract
The present invention relates to the technical fields of machining equipment, especially a kind of full-automatic draw machining center of full SERVO CONTROL, with fuselage, the waist opens up open slot along its length, the open slot both ends are symmetrically arranged the first driving motor and the second driving motor, and the first driving motor output end and the second driving motor output end are separately connected the first lead screw；Pipe-reduction mold is connected by thread bush on first lead screw, waist setting is located between the pipe-reduction mold and is held down assembly；The fuselage side also sets up loading assemblies, and blanking component is arranged in the fuselage other side.The structure of the complete full-automatic draw machining center of SERVO CONTROL is simple, and primary feed may be implemented, and draw processing and forming, shortening draw process time improve the efficiency of the draw simultaneously at a both ends, guarantee draw quality, convenient for being widely popularized and using.
Description
Technical field
The present invention relates to the technical field of machining equipment, in especially a kind of full-automatic draw processing of full SERVO CONTROL
The heart.
Background technique
With the continuous development of society, mechanical processing industry has obtained quick development.Product is carried out plus is processed a bit
There are many mode, and wherein the draw is important component part.The draw is the procedure shunk to tubing products diameter.Tradition
The draw generally use machine for shrinking, run using hydraulic control, but find usually tubing products be made to occur after long-term use
The phenomenon that evaporating, emitting, dripping or leaking of liquid or gas, the serious processing quality for affecting pipe fitting；And current machine for shrinking can only also be carried out for single head
The draw can only carry out the secondary draw, cause the whole draw inefficient in this way when needing the double end draw, it has not been convenient to
Necking operation while people's sight realizes double end simultaneously.
Summary of the invention
The technical problem to be solved by the present invention is being provided a kind of complete to solve the problems, such as above-mentioned background technique
The full-automatic draw machining center of SERVO CONTROL, structure is simple, and primary feed may be implemented, and the draw molding simultaneously of a both ends adds
Work shortens draw process time, improves the efficiency of the draw, guarantees draw quality, convenient for being widely popularized and using.
The technical solution adopted by the present invention to solve the technical problems is: in a kind of full-automatic draw processing of full SERVO CONTROL
The heart has fuselage, and the waist opens up open slot along its length, and the open slot both ends are symmetrically arranged the
One driving motor and the second driving motor, the first driving motor output end are separately connected with the second driving motor output end
First lead screw；Pipe-reduction mold is connected by thread bush on first lead screw, is located at waist between the pipe-reduction mold
Setting holds down assembly；The fuselage side also sets up loading assemblies；Blanking component is arranged in the fuselage other side.
Specifically, described to hold down assembly including guide post, upper pressure seat, down pressing seat, upper and lower clamping platform, upper and lower motor and second
Lead screw；The guide post is vertically set on fuselage, and the guide post upper end is fixed by horizontally disposed clamping platform up and down, institute
The motor up and down stated is vertically set on clamping platform upper end up and down, and second lead screw is vertically plugged in motor side up and down, institute
The second lead screw stated passes through the fixed upper pressure seat in clamping platform rear end up and down from top to bottom, and the down pressing seat is fixed at pressure
The lower section of seat, such design is fixed during the draw to processed pipe fitting to realize.
It further limits, in above-mentioned technical proposal, the two sides of the open slot are located on fuselage upper surface along length
Direction also sets up guide rail, and the pipe-reduction mold lower end two sides pass through the first sliding block and are slidably arranged on guide rail, can be improved
The guiding role of pipe-reduction mold guarantees the accuracy of draw position.
It further limits, in above-mentioned technical proposal, the side of the guide rail, which is located on fuselage end face, to be also fixedly installed
Magnetostrictive displacement sensor, it is such design be in order to guarantee during carrying out the draw, the essence of pipe-reduction mold shift position
Really control.
Specifically, the loading assemblies include crossbeam, connector, fixed block, feeding flat-removing air cyclinder and the first claw；Institute
The crossbeam stated is fixed on guide post in parallel up and down, and the connector is fixed between crossbeam, the connector
Lower end fixed by fixed block, the feeding flat-removing air cyclinder is horizontally set on lower end of fixing block, and first claw is solid
The output end of feeding flat-removing air cyclinder is set calmly, the clamping feeding for being processed pipe fitting may be implemented.
Specifically, the blanking component includes fixed beam, blanking flat-removing air cyclinder, link block and the second claw；Described
Fixed beam is horizontally fixed on guide post, and the blanking flat-removing air cyclinder level is fixed at fixed beam lower end, the blanking
Flat-removing air cyclinder lower end is fixedly connected with block, and the second claw is fixedly installed in the link block side, and such design is to realize
To the folder removal piece of the pipe fitting of completion of processing.
It further limits, in above-mentioned technical proposal, the down pressing seat lower end is slidably arranged in by the second sliding block is led
On rail, the adjustment that the position of down pressing seat may be implemented is fixed.
It further limits, in above-mentioned technical proposal, gyro black assembly is also set up below the loading assemblies, it is described
Gyro black assembly includes turning motor, articulated arm and revolution claw；The turning motor is fixed on fuselage side wall, described
The fixed articulated arm of turning motor output end, the fixed revolution claw in the end of the articulated arm may be implemented in loading assemblies
The supply of pipe fitting.
It further limits, in above-mentioned technical proposal, the gyro black assembly side is located at one middle side part of fuselage and also sets up
Unloader, such design are the fast supplies in order to meet the pipe fitting of whole machine for shrinking.
The beneficial effects of the present invention are: a kind of complete full-automatic draw machining center of SERVO CONTROL proposed by the present invention, structure
Simply, primary feed, a both ends while draw processing and forming may be implemented, shorten draw process time, improve the effect of the draw
Rate guarantees draw quality, convenient for being widely popularized and using.
Detailed description of the invention
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below
There is attached drawing needed in technical description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this
The some embodiments recorded in application, for those of ordinary skill in the art, without creative efforts,
It is also possible to obtain other drawings based on these drawings.
Fig. 1 is structural schematic diagram of the invention；
Fig. 2 is side structure schematic diagram of the invention；
Fig. 3 is the structural schematic diagram of loading assemblies and blanking component in the present invention；
Fig. 4 is the structural schematic diagram of gyro black assembly in the present invention.
Label in attached drawing are as follows: 1, fuselage；2, open slot；3, the first driving motor；4, the second driving motor；5, first
Thick stick；6, thread bush；7, pipe-reduction mold；8, guide post；9, upper pressure seat；10, down pressing seat；11, upper and lower clamping platform；12, upper and lower motor；
13, the second lead screw；14, guide rail；15, magnetostrictive displacement sensor；16, crossbeam；17, connector；18, fixed block；19, feeding
Flat-removing air cyclinder；20, the first claw；21, fixed beam；22, blanking flat-removing air cyclinder；23, link block；24, the second claw；25, it turns round
Motor；26, articulated arm；27, claw is turned round；28, unloader.
Specific embodiment
In order to which the technical problems, technical solutions and beneficial effects solved by the present invention is more clearly understood, below in conjunction with
Accompanying drawings and embodiments, the present invention will be described in further detail.It should be appreciated that specific embodiment described herein is only used
To explain the present invention, it is not intended to limit the present invention.
In the description of the present invention, it is to be understood that, term " side ", " other side ", " two sides ", " between ", " in
The orientation or positional relationship of the instructions such as portion ", " upper end ", " lower end " be based on the orientation or positional relationship shown in the drawings, be only for
Convenient for the description present invention and simplify description, rather than the device or element of indication or suggestion meaning there must be specific side
Position is constructed and operated in a specific orientation, therefore is not considered as limiting the invention.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " setting " " connects
Connect " it shall be understood in a broad sense, for example, it may be being fixedly connected, it may be a detachable connection, or be integrally connected；It can be straight
Connect it is connected, can also be indirectly connected through an intermediary.For the ordinary skill in the art, it can be managed with concrete condition
Solve the concrete meaning of above-mentioned term in the present invention.
See described in Fig. 1~4 it is a kind of full-automatic draw machining center of full SERVO CONTROL, there is fuselage 1,1 middle part of fuselage
Open slot 2 is opened up along its length, 2 both ends of open slot are symmetrically arranged the first driving motor 3 and the second driving motor 4, the
One driving motor, 3 output end and 4 output end of the second driving motor are separately connected the first lead screw 5；Pass through screw thread on first lead screw 5
Set 6 connects pipe-reduction mold 7, is arranged in the middle part of fuselage 1 between pipe-reduction mold 7 and holds down assembly；1 side of fuselage also sets up feeding group
Part；Blanking component is arranged in 1 other side of fuselage.
Wherein, it holds down assembly including guide post 8, upper pressure seat 9, down pressing seat 10, upper and lower clamping platform 11, upper and lower motor 12 and second
Lead screw 13；Guide post 8 is vertically arranged on the fuselage 1, and 8 upper end of guide post is fixed by horizontally disposed clamping platform 11 up and down, power-on and power-off
Machine 12 is vertically set on 11 upper end of clamping platform up and down, and the second lead screw 13 is vertically plugged in 12 side of motor up and down, the second lead screw 13
The fixed upper pressure seat 9 in upper and lower 11 rear end of clamping platform is passed through from top to bottom, and down pressing seat 10 is fixed at the lower section of upper pressure seat 9.It opens
The two sides of mouthful slot 2 are located on 1 upper surface of fuselage also sets up guide rail 14 along its length, and 7 lower end two sides of pipe-reduction mold pass through the
One sliding block is slidably arranged on guide rail 14.The side of guide rail 14, which is located on 1 end face of fuselage, is also fixedly installed magnetostrictive displacement biography
Sensor 15.Loading assemblies include crossbeam 16, connector 17, fixed block 18, feeding flat-removing air cyclinder 19 and the first claw 20；Crossbeam 16
It is fixed on guide post 8 in parallel up and down, connector 17 is fixed between crossbeam 16, and the lower end of connector 17 passes through fixation
Block 18 is fixed, and feeding flat-removing air cyclinder 19 is horizontally set on 18 lower end of fixed block, and the first claw 20 is fixed at feeding translation gas
The output end of cylinder 19.Blanking component includes fixed beam 21, blanking flat-removing air cyclinder 22, link block 23 and the second claw 24；Fixed beam
21 are horizontally fixed on guide post 8, and 22 level of blanking flat-removing air cyclinder is fixed at 21 lower end of fixed beam, under blanking flat-removing air cyclinder 22
End is fixedly connected with block 23, and the second claw 24 is fixedly installed in 23 side of link block.10 lower end of down pressing seat is set by the sliding of the second sliding block
It sets on guide rail 14.Gyro black assembly is also set up below loading assemblies, gyro black assembly includes turning motor 25, articulated arm 26 and returns
Turn claw 27；Turning motor 25 is fixed on 1 side wall of fuselage, the fixed articulated arm 26 of 25 output end of turning motor, articulated arm
The fixed revolution claw 27 in 26 end.Gyro black assembly side is located at 1 one middle side part of fuselage and also sets up unloader 28.
See figure and Fig. 2, the up and down motion to hold down assembly is to run by upper and lower motor 12, so that upper and lower motor 12 is defeated
Outlet with driving gear you and connect the rotation to drive the second lead screw 13, to realize the up and down motion of upper pressure seat 9；Folder up and down
It is connected through a screw thread between tight platform 11 and the second screw rod 13.
See that Fig. 4, gyro black assembly are fixed on 1 side wall of fuselage by fixed plate, the working principle of gyro black assembly are as follows: first
First, it controls articulated arm 26 by peripheral control unit to rotate downwards, after articulated arm 26 is downward, the revolution claw 27 of end is to
Pipe fitting in place is grabbed, and is then controlled turning motor 25 and is rotated, and the rotation of articulated arm 26 is delivered up to loading assemblies.
See Fig. 3, the operating principle of loading assemblies and blanking component is as follows: firstly, passing through the first card of peripheral control unit control
The pipe fitting of the crawl revolution of pawl 20 27 upper end of claw, is then run by control feeding flat-removing air cyclinder 19, by 20 upper tube of the first claw
Part is pushed in down pressing seat 9；The operating principle of blanking component are as follows: blanking flat-removing air cyclinder 22 is controlled by peripheral control unit and is run to
The position of down pressing seat 10 realizes the clamping to the pipe fitting processed by the second claw 24, controls blanking flat-removing air cyclinder 22
After contraction, pipe fitting is taken out.
In this application, the first driving motor 3, the second driving motor 4, upper and lower motor 12, pipe-reduction mold 7, magnetostriction
Displacement sensor 15, guide rail 14, turning motor 25, unloader 28, feeding flat-removing air cyclinder 19 and blanking flat-removing air cyclinder 22 are all roots
According to concrete model, directly commercially Matching installation is used, and is controlled and is run by peripheral control unit.
See Fig. 1~4, the working principle of the full SERVO CONTROL draw machining center is as follows:
Firstly, operator is pushed to gyro black assembly corresponding position after filling pipe fitting on unloader 28, pass through revolution group
The cooperation of part and loading assemblies is held down assembly by peripheral control unit control and is processed to needs realizing the feeding push of pipe fitting
Pipe fitting carries out compression controller and controls the first driving cylinder 3 and the second driving cylinder 4 respectively, can make the first screw rod 5 in this way
It is rotated, so that pipe-reduction mold 7 slides on the first lead screw 5, to carry out the draw to pipe fitting end；It is easy to operate fast
Victory, may be implemented draw while pipe fitting, and the specific location of the draw can control contracting by magnetostrictive displacement sensor 15
The range ability of pipe mold 7.
The relatively traditional machine for shrinking of the application has the advantages that
1, the equipment uses full SERVO CONTROL, and X-axis two sides couple the by shaft coupling by servo motor band speed reducer respectively
One lead screw 5 drives pipe-reduction mold 7 to be X to movement, while by magnetostrictive displacement sensor 15, closed-loop control is realized, to reach
To X-axis double end draw synchronous shift, the double end draw simultaneously is realized.
2, X-axis pipe-reduction mold 7 is designed using double-station, and primary feed completes two steps of the pre- draw and the secondary draw, with
Reach a draw molding.
3, the driving of Z axis pressure pressure pipe mould drives the second lead screw 13 to move up and down using servo motor band speed reducer.Simultaneously
Compaction mold is designed using adjustable structure, to realize a wide range of size covering.
4, it is combined using actuating cylinder, realizes whole automatic charging blanking circulation.
It is above-described, it is merely preferred embodiments of the present invention, but protection scope of the present invention is not limited to
This, anyone skilled in the art in the technical scope disclosed by the present invention, according to the technique and scheme of the present invention
And its inventive concept is subject to equivalent substitution or change, should be covered by the protection scope of the present invention.
Claims (9)
1. a kind of full-automatic draw machining center of full SERVO CONTROL, it is characterized in that: there is fuselage (1), in the middle part of the fuselage (1)
It opens up along its length open slot (2), the open slot (2) both ends are symmetrically arranged the first driving motor (3) and second
Driving motor (4), the first driving motor (3) output end and the second driving motor (4) output end are separately connected first
Thick stick (5)；Pass through thread bush (6) connection pipe-reduction mold (7), the meta position of the pipe-reduction mold (7) on first lead screw (5)
Setting holds down assembly in the middle part of fuselage (1)；Described fuselage (1) side also sets up loading assemblies, under the setting of fuselage (1) other side
Expect component.
2. a kind of complete full-automatic draw machining center of SERVO CONTROL according to claim 1, it is characterized in that: the compression
Component includes guide post (8), upper pressure seat (9), down pressing seat (10), upper and lower clamping platform (11), upper and lower motor (12) and the second lead screw
(13)；The guide post (8) is vertically set on fuselage (1), and guide post (8) upper end passes through horizontally disposed clamping platform (11) up and down
Fixed, the motor up and down (12) is vertically set on clamping platform (11) upper end up and down, and second lead screw (13) is vertically inserted
It is located at motor (12) side up and down, the second lead screw (13) passes through the fixed upper pressure seat in upper and lower clamping platform (11) rear end from top to bottom
(9), the down pressing seat (10) is fixed at the lower section of upper pressure seat (9).
3. a kind of complete full-automatic draw machining center of SERVO CONTROL according to claim 2, it is characterized in that: the opening
The two sides of slot (2) are located on fuselage (1) upper surface to be also set up guide rail (14) along its length, the pipe-reduction mold (7) lower end
Two sides pass through the first sliding block and are slidably arranged on guide rail (14).
4. a kind of complete full-automatic draw machining center of SERVO CONTROL according to claim 3, it is characterized in that: the guide rail
(14) side, which is located on fuselage (1) end face, is also fixedly installed magnetostrictive displacement sensor (15).
5. a kind of complete full-automatic draw machining center of SERVO CONTROL according to claim 2, it is characterized in that: the feeding
Component includes crossbeam (16), connector (17), fixed block (18), feeding flat-removing air cyclinder (19) and the first claw (20)；Described
Crossbeam (16) is fixed in parallel up and down on guide post (8), and the connector (17) is fixed between crossbeam (16), even
The lower end of fitting (17) is fixed by fixed block (18), and the feeding flat-removing air cyclinder (19) is horizontally set under fixed block (18)
End, first claw (20) are fixed at the output end of feeding flat-removing air cyclinder (19).
6. a kind of complete full-automatic draw machining center of SERVO CONTROL according to claim 2, it is characterized in that: the blanking
Component includes fixed beam (21), blanking flat-removing air cyclinder (22), link block (23) and the second claw (24)；The fixed beam (21)
It is horizontally fixed on guide post (8), described blanking flat-removing air cyclinder (22) level is fixed at fixed beam (21) lower end, and blanking is flat
It moves cylinder (22) lower end to be fixedly connected block (23), the second claw (24) are fixedly installed in the link block (23) side.
7. a kind of complete full-automatic draw machining center of SERVO CONTROL according to claim 3, it is characterized in that: the pushing
Seat (10) lower end is slidably arranged on guide rail (14) by the second sliding block.
8. a kind of complete full-automatic draw machining center of SERVO CONTROL according to claim 5, it is characterized in that: the feeding
Gyro black assembly is also set up below component, the gyro black assembly includes turning motor (25), articulated arm (26) and revolution claw
(27)；The turning motor (25) is fixed on fuselage (1) side wall, the fixed articulated arm of turning motor (25) output end
(26), fixed revolution claw (27) in the end of the articulated arm (26).
9. a kind of complete full-automatic draw machining center of SERVO CONTROL according to claim 8, it is characterized in that: the revolution
Component side is located at (1) one middle side part of fuselage and also sets up unloader (28).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811439783.8A CN109773064A (en) | 2018-11-29 | 2018-11-29 | A kind of full-automatic draw machining center of full SERVO CONTROL |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811439783.8A CN109773064A (en) | 2018-11-29 | 2018-11-29 | A kind of full-automatic draw machining center of full SERVO CONTROL |
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| Publication Number | Publication Date |
|---|---|
| CN109773064A true CN109773064A (en) | 2019-05-21 |
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ID=66496525
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811439783.8A Pending CN109773064A (en) | 2018-11-29 | 2018-11-29 | A kind of full-automatic draw machining center of full SERVO CONTROL |
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| CN (1) | CN109773064A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202539397U (en) * | 2012-03-21 | 2012-11-21 | 浙江罗森博格机床有限公司 | Efficient pipe reducing machine |
| CN103752711A (en) * | 2014-01-08 | 2014-04-30 | 华南理工大学 | High-precision heat pipe shrinking device |
| CN107790569A (en) * | 2017-09-27 | 2018-03-13 | 安徽杰曼汽车零部件有限公司 | A kind of automatic hydraulic double end machine for shrinking |
| CN207981936U (en) * | 2017-12-24 | 2018-10-19 | 江苏合丰机械制造有限公司 | A kind of pipe end production line |
| CN209465579U (en) * | 2018-11-29 | 2019-10-08 | 江苏锐成机械有限公司 | The full-automatic draw machining center of full SERVO CONTROL |
-
2018
- 2018-11-29 CN CN201811439783.8A patent/CN109773064A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202539397U (en) * | 2012-03-21 | 2012-11-21 | 浙江罗森博格机床有限公司 | Efficient pipe reducing machine |
| CN103752711A (en) * | 2014-01-08 | 2014-04-30 | 华南理工大学 | High-precision heat pipe shrinking device |
| CN107790569A (en) * | 2017-09-27 | 2018-03-13 | 安徽杰曼汽车零部件有限公司 | A kind of automatic hydraulic double end machine for shrinking |
| CN207981936U (en) * | 2017-12-24 | 2018-10-19 | 江苏合丰机械制造有限公司 | A kind of pipe end production line |
| CN209465579U (en) * | 2018-11-29 | 2019-10-08 | 江苏锐成机械有限公司 | The full-automatic draw machining center of full SERVO CONTROL |
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