CN206727403U - Aviation plug assembles and detection means - Google Patents
Aviation plug assembles and detection means Download PDFInfo
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- CN206727403U CN206727403U CN201720555710.XU CN201720555710U CN206727403U CN 206727403 U CN206727403 U CN 206727403U CN 201720555710 U CN201720555710 U CN 201720555710U CN 206727403 U CN206727403 U CN 206727403U
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- shell fragment
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Abstract
The utility model provides a kind of aviation plug assembling detection device and production technology for collecting assembling and detecting integrated full-automatic.Aviation plug assembles and detection means, station dispenser, feeding assembly unit, dynamics detection unit and screening unit including mounting base and on bottom plate, also include control device, the control device couples with station dispenser and feeding assembly unit, dynamics detection unit and screening unit, and controls each unit to be sequentially completed the assembling of aviation plug feeding, dynamics detection and the work for screening blanking in contact pin mould.The utility model has the advantage of：The utility model is compact-sized, province place, is easy to tissue to produce；Operation and Maintenance is more convenient, and securely and reliably, stability is high.Ensure precision；Ensure production efficiency；It is simple, rapid to change operation of components, so as to reduce labor intensity, reduces operating personnel, reduces cost of labor, improve automaticity.
Description
Technical field
The present invention relates to the assembling device of aviation plug, the assembling of especially a kind of aviation plug and detection means.
Background technology
In an assembling process, majority is assembled, detected for artificial multistation current aviation plug successively.People's work point positive pole and
Negative pole produces, and because both positive and negative polarity material is different with length, used mould is also different.Contact pin is first manually put into mould
Tool, then shell fragment is handled and is placed on 75 ° of contact pin end circular hole position inclination（Due to shell fragment very little, can not manually ensure to put
The accuracy of seated position）, another hand presses red needle and shell fragment is pressed into contact pin, then carry out detection sorting, test shell fragment pressure
The elastic force for coming part is exposed after entering.Due to the ordinary use of aviation multi-cable plug in recent years, plant produced index is continuously increased,
And factory's man efficiency does not catch up with requirement much, the artificial matter of great urgency that not only can't resolve factory of increase increases on the contrary
The burden of factory.
The content of the invention
The technical problem that unresolved manual assembly detection aviation plug efficiency is low, defect rate is high and cost is high, the present invention carry
Collect assembling and the aviation plug assembling detection device and production technology of detection integrated full-automatic for a kind of.
Aviation plug assembles and detection means, including mounting base and station dispenser, feeding dress on bottom plate
With unit, dynamics detection unit and screening unit, the station dispenser is provided with some contact pin moulds, and the feeding assembling is single
Member, dynamics and visual detection unit and screening unit prolong contact pin die location matching distribution on station dispenser, in addition to middle control
Device, the control device couple with station dispenser and feeding assembly unit, dynamics and visual detection unit and screening unit,
And each unit is controlled to be sequentially completed the assembling of aviation plug feeding, the detection of dynamics outward appearance and the work for screening blanking in contact pin mould
Make.
On the basis of above-mentioned technical proposal, further, the feeding assembly unit includes contact pin assembling device and bullet
On chip to match somebody with somebody device, contact pin is assembled to contact pin mould by the control device control contact pin assembling device successively with shell fragment assembling device
In, and shell fragment is pressed into contact pin mould.
On the basis of above-mentioned technical proposal, further, the contact pin assembling device includes contact pin feed mechanism and inserted
Pin assemble mechanism, the contact pin assemble mechanism include base support, rack-mount removable clamping jaw, the removable folder
Pawl can be captured in the contact pin implantation contact pin mould in contact pin feed mechanism.
On the basis of above-mentioned technical proposal, further, the shell fragment assembling device includes shell fragment feed mechanism, shell fragment
Adjustment mechanism and shell fragment assemble mechanism；The shell fragment adjustment mechanism is placed in shell fragment feed mechanism exit, including fixed support and
The rotating mechanism that the clamp system of installation on a mounting board is connected with clamp system, the clamp system fixation spring tab feed mechanism
The shell fragment and exposed portion shell fragment of submitting, the rotating mechanism holding shrapnel simultaneously drive clamp system integral-rotation；The shell fragment
Assemble mechanism includes mount support, and rack-mount punching mechanism, and removable clamping jaw, institute are housed on the punching mechanism
State the removable clamping jaw of control device control and clamp postrotational shell fragment, and take and be moved to contact pin mold station, will by punching mechanism
The interior simultaneously exposed portion shell fragment of shell fragment press-in contact pin mould.
On the basis of above-mentioned technical proposal, further, the dynamics detection unit includes base, on base
Cylinder and the pressure sensor that is fixed on cylinder mobile terminal, the cylinder can push exposing for pressure sensor touching shell fragment
Part, also being set up in the dynamics detection unit has vision inspection apparatus, realizes whether shell fragment deforms for detecting.
On the basis of above-mentioned technical proposal, further, the screening unit includes base, installing plate, removable folder
Pawl and lateral cylinder, the installing plate are fixed on base, and the lateral cylinder is fixed on a mounting board, the removable clamping jaw
It is fixedly connected with cylinder free end.
On the basis of above-mentioned technical proposal, further, the removable clamping jaw includes cross translation stage and is fixed on
The clamping jaw of cross translation stage free end, be additionally provided between cross translation stage free end and clamping jaw chain connecting plate, rotary cylinder and/or
Single-acting cylinder.
On the basis of above-mentioned technical proposal, further, the contact pin feed mechanism and shell fragment feed mechanism are vibrations
Platform, the discharging opening of the shake table are additionally provided with material separation device.
On the basis of above-mentioned technical proposal, further, in addition to the man-machine interface input dress being connected with control device
Put.
A kind of aviation plug assembling and detection platform, including installation frame, the installation frame is interior to be provided with above-mentioned aviation
Plug assembles and detection means.
The advantage of the invention is that：The present invention is compact-sized, province place, is easy to tissue to produce；Operation and Maintenance is more convenient, peace
Complete reliable, stability is high.Manipulator clamping is flexible, and feeding, feeding action be accurate, in place, accurate positioning when making component assembly, protects
Demonstrate,prove precision；The productive temp of part is fitted close, ensures production efficiency；It is simple, rapid to change operation of components, so as to lighten one's labor
Intensity, operating personnel are reduced, reduce cost of labor, improve automaticity.
Brief description of the drawings
Fig. 1 is aviation plug assembling and detection platform general assembly schematic diagram；
Fig. 2 is aviation plug assembling and detection means station schematic diagram；
Fig. 3 is contact pin assembling apparatus structure schematic diagram；
Fig. 4 is shell fragment assembling apparatus structure schematic diagram；
Fig. 5 is shell fragment assembling device rotation clamping structural scheme of mechanism；
Fig. 6 is dynamics detection unit structural representation；
Fig. 7 is screening unit structural representation；
Fig. 8 is station dispenser structural representation；
Fig. 9 is shell fragment schematic shapes；
Description of reference numerals：
1- lighting apparatus；2- human-computer interaction interface touch screens；3- installation frames；4- safe gratings；5- electric appliance control boxes；6-
Universal wheel；7- contact pins assemble device；8- shell fragments assemble device；9- dynamics detection units；10- screening units one；11- screening units
Two；12- station dispensers；13- bottom plates；
011- clamping jaw lift cylinders；012- buffering stands；013- line rails；014- clamping jaws rotate gear train；015- clamping jaw gas
Cylinder；016- supporting plates；017- base supports；018- gear-boxes；019- installation side plates；020- slide units are displaced sideways cylinder； 021-
Clamping jaw rotary cylinder；022- vibrating disks；023- vibrating disk bottom plates；024- linear vibration feeders；025- oil buffers；
026- shell fragments are pressed into cylinder；027- cylinder mounting plates；028- supporting pillars；029- flange bearings；030- guide rods；
The 031- switching anti-sticking stripping cylinders of pressing plate 032-；033- shells plate；034- shell fragment compression cylinders；035- rotary cylinders；036- contact pins
Mould；037- clamping jaw lift cylinders；038- buffers mounting bracket；039- installing plates；040- slide units are displaced sideways cylinder；041- shakes
Moving plate；042- chain connecting plates；The micro mobile cylinder of 043- clamping jaws；044- rotating cylinder installing plates；045- separated material cylinders；046- straight lines shake
Dynamic feed appliance；047- vibrating disk bottom plates；The micro mobile cylinder of 048- pressure sensors；049- line rails；050- installing plates
051- support column 052- pressure sensor installing plates；053- pressure sensor connectors；054- is displaced sideways cylinder；
055- pressure sensors；056- hydraulic bjuffers；057- buffer mounting brackets；058- installing plates；059- clamping jaw installing plates；
060- clamping jaw cylinders；061- supporting plates；062- mounting bases；063- x wire rails；064- clamping jaw lift cylinders；065- vertical lines
Rail；066- transverse shifting cylinders；067- universal joints；
0551- cameras；0552- light compensating lamps；0553- installing plates；0554- reinforcements；0555- adjustable plates；0556- is supported
Plate；
068- turntables；069- contact pin moulds；070- dispensers；071- isometry blocks.
Embodiment：
Embodiments of the invention are described below in detail, the example of the embodiment is shown in the drawings, wherein from beginning to end
Same or similar label represents same or similar original paper or the element with same or like function.Below with reference to attached
The embodiment of figure description is exemplary, it is intended to for explaining the present invention, and is not considered as limiting the invention.
As shown in figure 1, a kind of assembling of aviation plug and detection platform, including installation frame 3, set in the installation frame 3
There are described aviation plug assembling and detection means.The upper beam and frame perimeter of the security framework 3 can set lighting apparatus 1；
The electric control box for placing control device in the bottom of security framework, for ease of operate on framework also set up with it is hollow
The human-computer interaction interface touch screen 2 of device connection, safety is installed on the peripheral frame of aviation plug assembling and detection means
Grating 4, the safe grating 4 are connected with control device, once have the part in workbench fly out or staff and other
Object stretches into frame work region internal trigger safe grating 4, and control device can stop aviation plug assembling and detection means in time
Work, avoids causing the generation of security incident；Move aviation plug assembling and detection means for convenience simultaneously, the platform
Bottom is additionally provided with some universal wheels 6, and the universal wheel 6 also can be replaced other travel mechanisms.
As shown in Fig. 2 aviation plug assembling and detection means, including mounting base 13 and installation station on base 13
Dispenser 12, feeding assembly unit, dynamics detection unit 9 and screening unit 10, the station dispenser are provided with some contact pins
Mould 069, the feeding assembly unit, dynamics detection unit 9 and screening unit 10 surround the cloth of turntable 068 of station dispenser 12
Put, in addition to control device, the control device and station dispenser and feeding assembly unit, dynamics detection unit and screening are single
Member connection, and control each unit to be sequentially completed the assembling of aviation plug feeding, dynamics detection and screening blanking in contact pin mould
Work.
Likewise, the station dispenser can be replaced with conveyer belt, each unit is arranged by workflow successively along conveyer belt
Sequence, on the conveyor belt provided with some contact pin moulds 069.
Wherein, the feeding assembly unit includes contact pin assembling device and shell fragment assembling device, the control device control
Contact pin assembles device and contact pin is assembled in contact pin mould successively with shell fragment assembling device, and shell fragment is pressed into contact pin mould.
As shown in figure 3, the contact pin assembling device includes shake table 022 and contact pin assemble mechanism, the contact pin assembly machine
Structure includes base support 017, the removable clamping jaw on support 017, and the removable clamping jaw includes cross translation stage, rotation
Rotaring cylinder and clamping jaw, the cross translation stage is fixed on support 017 vertically, lateral by clamping jaw lift cylinder 011 and slide unit
Rail 013 controls clamping jaw moves vertically and horizontally by gear-box 013 along mobile cylinder 020, the lower end of clamping jaw lift cylinder 011 dress
There are clamping jaw rotary cylinder 021 and clamping jaw rotation gear train 014 to be connected with clamping jaw, clamping jaw can be controlled to rotate freely, position, it is described
Clamping jaw is controlled the contact pin in clamping jaw motion capture contact pin feed mechanism by clamping jaw cylinder 015, and is implanted into contact pin mould.
As shown in Figure 4 and Figure 5, the shell fragment assembling device includes shell fragment feeding vibrating disk 041, shell fragment adjustment mechanism and bullet
Piece assemble mechanism；The material baffle of the control of separated material cylinder 045, the shell fragment adjustment are additionally provided with the discharging opening of feeding vibrating disk 041
Mechanism is placed in shell fragment feed mechanism exit, including the clamping device that shell fragment clamping cylinder 034 controls revolves with control clamping device
The rotary cylinder 035 turned, the shell fragment and exposed portion shell fragment that the clamp system fixation spring tab feed mechanism is sent out, the rotation
Mechanism drives clamp system integral-rotation；The shell fragment is as shown in figure 8, both ends are bent, and one end is special-shaped head, the other end side of being
Head；Shell fragment assemble mechanism is disposed with the side of shell fragment adjustment mechanism, the shell fragment assemble mechanism includes mount support, and installation
Punching mechanism on support, equipped with removable clamping jaw, the removable clamping jaw folder of control device control on the punching mechanism
Shell fragment after tight rotation, and grab to contact pin mold station, shell fragment is pressed into contact pin mould simultaneously exposed portion bullet by punching mechanism
Piece.The punching mechanism includes shell fragment press-in cylinder 026, cylinder mounting plate 027 for punching press, holds on 028, flange bearing
029th, guide rod and switching pressing plate, in addition to the anti-sticking stripping cylinder for preventing adhesion and stripping plate；The removable clamping jaw includes
Cross translation stage, chain connecting plate 042 and clamping jaw, the cross translation stage are fixed on shell fragment by installing plate 039 and are pressed into cylinder vertically
On 026 free end, rail along cylinder 040 is displaced sideways by clamping jaw lift cylinder 037 and slide unit and controls clamping jaw vertical and water
Translation is dynamic, and the lower end of clamping jaw lift cylinder 011 is equipped with chain connecting plate 042, and the micro mobile cylinder 043 of clamping jaw is fixedly mounted in chain connecting plate 042
Control clamping jaw action.
As shown in fig. 6, the dynamics detection unit includes base, the lateral movement cylinder 054 on base and consolidated
The pressure sensor 055 being scheduled on cylinder mobile terminal, the lateral movement cylinder treat that station dispenser 12 transports contact pin mould
After in place, pressure sensor 055 can be pushed and moved to the direction of contact pin mould 069, the exposed portion of shell fragment is touched, in real time by shell fragment
Dynamics measurement data is sent to control device.
Also being set up in the dynamics detection unit has vision inspection apparatus, and the vision inspection apparatus includes supporting plate
0556th, camera 0551, light compensating lamp 0552, installing plate 0553, reinforcement 0554 and adjustable plate 0555, the solid frame of the supporting plate 0556
It is located at outside dynamics detection unit, there is installing plate 0553 and reinforcement 0554 in supporting plate 0556, is equipped with the front end of reinforcement 0554
Adjustable plate 0555, and camera 0551 is housed on adjustable plate 0555, light compensating lamp 0552 is had in camera 0551, is detected in dynamics
Unit pushes shell fragment
As shown in fig. 7, the screening unit includes base, installing plate, removable clamping jaw and transverse shifting cylinder 066, institute
Stating base includes the supporting plate 061 that mounting base 062 and bottom plate 062 are hindered, and the installing plate 058 is fixed in supporting plate 061, institute
State transverse shifting cylinder 066 to be fixed on installing plate 062, the removable clamping jaw is fixedly connected with the free end of cylinder 066, described
Removable clamping jaw includes cross translation stage, clamping jaw installing plate 059 and clamping jaw, and the cross translation is provided with horizontal stroke on installing plate 058
To path 063, by clamping jaw lift cylinder 037 and transverse shifting cylinder 066, transversely Control of Trajectory clamping jaw vertically and horizontally moves
Dynamic, the lower end of clamping jaw lift cylinder 011 is equipped with clamping jaw installing plate 059, and clamping jaw installing plate 059 is fixedly mounted clamping jaw cylinder 060 and controlled
Clamping jaw acts；In the end of x wire rail 063, the liquid being fixed in buffer mounting bracket 057 is additionally provided with installing plate 058
Compression buffer 056, it is spacing for transverse shifting cylinder.
As shown in Fig. 2 it is respectively used to stacking conjunction equipped with screening unit 1 and screening unit 2 11 on mounting base 13
Lattice product and substandard product.
In the description of this specification, reference term " one embodiment ", " some embodiments ", " example ", " specifically show
The description of example " or " some examples " etc. means specific features, structure, material or the spy for combining the embodiment or example description
Point is contained at least one embodiment or example of the present invention.In this manual, to the schematic representation of above-mentioned term not
Necessarily refer to identical embodiment or example.Moreover, specific features, structure, material or the feature of description can be any
One or more embodiments or example in combine in an appropriate manner.
Claims (10)
1. aviation plug assembles and detection means, it is characterised in that the station segmentation including mounting base and on bottom plate
Device, feeding assembly unit, dynamics detection unit and screening unit, the station dispenser is provided with some contact pin moulds, described
Feeding assembly unit, dynamics and visual detection unit and screening unit prolong contact pin die location matching distribution on station dispenser,
Also include control device, the control device and station dispenser and feeding assembly unit, dynamics and visual detection unit and sieve
Element connection is selected, and controls each unit to be sequentially completed the assembling of aviation plug feeding, the detection of dynamics outward appearance and sieve in contact pin mould
Select the work of blanking.
2. aviation plug assembling according to claim 1 and detection means, it is characterised in that the feeding assembly unit bag
Contact pin assembling device and shell fragment assembling device are included, the control device control contact pin assembling device successively will with shell fragment assembling device
Contact pin is assembled in contact pin mould, and shell fragment is pressed into contact pin mould.
3. aviation plug assembling according to claim 2 and detection means, it is characterised in that the contact pin assembles device bag
Contact pin feed mechanism and contact pin assemble mechanism are included, the contact pin assemble mechanism includes base support, and rack-mount is removable
Dynamic clamping jaw, the removable clamping jaw can be captured in the contact pin implantation contact pin mould in contact pin feed mechanism.
4. aviation plug assembling according to claim 2 and detection means, it is characterised in that the shell fragment assembles device bag
Include shell fragment feed mechanism, shell fragment adjustment mechanism and shell fragment assemble mechanism；The shell fragment adjustment mechanism is placed in shell fragment feed mechanism and gone out
At mouthful, including the rotating mechanism that the clamp system of fixed support and installation on a mounting board is connected with clamp system, the clamping
The shell fragment and exposed portion shell fragment that mechanism fixation spring tab feed mechanism is sent out, the rotating mechanism holding shrapnel simultaneously drive clamping machine
Structure integral-rotation；The shell fragment assemble mechanism includes mount support, and rack-mount punching mechanism, the punching mechanism
Upper that removable clamping jaw is housed, the removable clamping jaw of control device control clamps postrotational shell fragment, and takes and be moved to contact pin mould
Have station, shell fragment is pressed into contact pin mould simultaneously exposed portion shell fragment by punching mechanism.
5. aviation plug assembling according to claim 4 and detection means, it is characterised in that the dynamics detection unit bag
Base, the cylinder on base and the pressure sensor being fixed on cylinder mobile terminal are included, the cylinder can push pressure
Sensor touches the exposed portion of shell fragment, and also being set up in the dynamics detection unit has vision inspection apparatus, for detecting reality
Whether existing shell fragment deforms.
6. aviation plug assembling according to claim 1 and detection means, it is characterised in that the screening unit includes bottom
Seat, installing plate, removable clamping jaw and lateral cylinder, the installing plate are fixed on base, and the lateral cylinder is fixed on installation
On plate, the removable clamping jaw is fixedly connected with cylinder free end.
7. aviation plug assembling and detection means according to claim 3,4 or 6, it is characterised in that the removable folder
Pawl includes cross translation stage and is fixed on the clamping jaw of cross translation stage free end, between cross translation stage free end and clamping jaw also
Provided with chain connecting plate, rotary cylinder and/or single-acting cylinder.
8. aviation plug assembling and detection means according to claim 3 or 4, it is characterised in that the contact pin feeder
Structure and shell fragment feed mechanism are shake tables, and the discharging opening of the shake table is additionally provided with material separation device.
9. aviation plug assembling according to claim 1 and detection means, it is characterised in that also include connecting with control device
The man-machine interface input unit connect.
10. a kind of aviation plug assembling and detection platform, it is characterised in that including installation frame, be provided with the installation frame
Aviation plug assembling and detection means described in any one of claim 1 to 9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720555710.XU CN206727403U (en) | 2017-05-18 | 2017-05-18 | Aviation plug assembles and detection means |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720555710.XU CN206727403U (en) | 2017-05-18 | 2017-05-18 | Aviation plug assembles and detection means |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206727403U true CN206727403U (en) | 2017-12-08 |
Family
ID=60512369
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720555710.XU Active CN206727403U (en) | 2017-05-18 | 2017-05-18 | Aviation plug assembles and detection means |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206727403U (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108213944A (en) * | 2017-12-13 | 2018-06-29 | 无锡昌至盛机械制造有限公司 | Oxygen valve assembling device |
| CN109261814A (en) * | 2018-09-19 | 2019-01-25 | 广东中都知识产权运营有限公司 | Gear mounting plate assembly machine |
| CN109444479A (en) * | 2018-11-07 | 2019-03-08 | 恒银金融科技股份有限公司 | Multi-functional pressure test platform |
| JP2020004704A (en) * | 2018-06-22 | 2020-01-09 | 東莞理工学院 | Bendable terminal assembly machine |
| CN110961877A (en) * | 2019-11-11 | 2020-04-07 | 西安空间无线电技术研究所 | Array antenna TR module intelligence assembly system |
| CN111982185A (en) * | 2020-09-03 | 2020-11-24 | 杭州彩兔贸易有限公司 | Rapid detection case is used to aviation safety |
| CN112005452A (en) * | 2018-04-27 | 2020-11-27 | 克龙贝格和舒伯特两合有限公司 | Automatic assembly or insertion method |
| CN112517774A (en) * | 2020-11-09 | 2021-03-19 | 沈阳兴华航空电器有限责任公司 | Automatic assembling equipment and assembling method for riveting and extruding jack and protective sleeve |
-
2017
- 2017-05-18 CN CN201720555710.XU patent/CN206727403U/en active Active
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108213944A (en) * | 2017-12-13 | 2018-06-29 | 无锡昌至盛机械制造有限公司 | Oxygen valve assembling device |
| CN112005452A (en) * | 2018-04-27 | 2020-11-27 | 克龙贝格和舒伯特两合有限公司 | Automatic assembly or insertion method |
| CN112005452B (en) * | 2018-04-27 | 2022-07-19 | 克龙贝格和舒伯特两合有限公司 | Automatic assembly or insertion method |
| JP2020004704A (en) * | 2018-06-22 | 2020-01-09 | 東莞理工学院 | Bendable terminal assembly machine |
| CN109261814A (en) * | 2018-09-19 | 2019-01-25 | 广东中都知识产权运营有限公司 | Gear mounting plate assembly machine |
| CN109444479A (en) * | 2018-11-07 | 2019-03-08 | 恒银金融科技股份有限公司 | Multi-functional pressure test platform |
| CN110961877A (en) * | 2019-11-11 | 2020-04-07 | 西安空间无线电技术研究所 | Array antenna TR module intelligence assembly system |
| CN110961877B (en) * | 2019-11-11 | 2021-02-05 | 西安空间无线电技术研究所 | Array antenna TR module intelligence assembly system |
| CN111982185A (en) * | 2020-09-03 | 2020-11-24 | 杭州彩兔贸易有限公司 | Rapid detection case is used to aviation safety |
| CN112517774A (en) * | 2020-11-09 | 2021-03-19 | 沈阳兴华航空电器有限责任公司 | Automatic assembling equipment and assembling method for riveting and extruding jack and protective sleeve |
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| GR01 | Patent grant | ||
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Address after: 201306 Shanghai, Nanhui, a new town around the Lake West Road, building A201-100, room 99, No. 16, room Patentee after: Shanghai west code machine tool Polytron Technologies Inc Address before: 201611 Shanghai City, Songjiang District export processing zone and Road No. 1155 Patentee before: Shanghai west code machine tool Polytron Technologies Inc |