CN202084432U - Control system of dual-fork alternating-current servo numerical-control winding machine - Google Patents
Control system of dual-fork alternating-current servo numerical-control winding machine Download PDFInfo
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- CN202084432U CN202084432U CN2011201538117U CN201120153811U CN202084432U CN 202084432 U CN202084432 U CN 202084432U CN 2011201538117 U CN2011201538117 U CN 2011201538117U CN 201120153811 U CN201120153811 U CN 201120153811U CN 202084432 U CN202084432 U CN 202084432U
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Abstract
The utility model relates to a control system of a dual-fork alternating-current servo numerical-control winding machine, which comprises a PLC (programmable logic controller), a touch screen, a full-automatic winding tension control subsystem, an indexing control subsystem, a left fork control subsystem and a right fork control subsystem. The PLC is respectively connected with the touch screen, the full-automatic winding tension control subsystem, the indexing control subsystem, the left fork control subsystem and the right fork control subsystem. Compared with the prior art, the control system of the dual-fork alternating-current servo numerical-control winding machine has the advantages of simplicity, compactness, low fault rate, high reliability, wide application range and the like.
Description
Technical field
The utility model relates to a kind of coil winding machine correlation technique, especially relates to a kind of control system of round trip flight fork AC servo numerical control filament winder.
Background technology
Coil winding machine is mainly used in the manufacturing of motor, electrical equipment winding, is the important tooling device in the electronics industry.Problems such as there are some functional defects in use in old-fashioned coil winding machine: number of turn numeration is unclear, occurs reaching neat winding displacement when the trickle enamelled wire of coiling, and winding tension is uncontrollable, these have had a strong impact on the quality of coiling.And PLC is widely used in every field with its modular structure, abundant I/O interface, many advantages such as programming is easy to learn and antijamming capability is strong, reliability height in recent years, particularly in the automatic control of industrial processes.
The utility model content
The purpose of this utility model is exactly the control system that a kind of concision and compact, failure rate is low, reliability is high, applied widely round trip flight fork AC servo numerical control filament winder are provided in order to overcome the defective that above-mentioned prior art exists.
The purpose of this utility model can be achieved through the following technical solutions:
A kind of control system of round trip flight fork AC servo numerical control filament winder, it is characterized in that, comprise PLC, touch-screen, full-automatic winding tension control subsystem, calibration control subsystem, left flying trident control subsystem, right flying trident control subsystem, described PLC is connected with touch-screen, full-automatic winding tension control subsystem, calibration control subsystem, left flying trident control subsystem, right flying trident control subsystem respectively.
Described full-automatic winding tension control subsystem comprises the tension detector that connects successively, full-automatic tension controller, magnetic powder brake, and described full-automatic tension controller is connected with PLC.
Described calibration control subsystem comprises calibration positioning unit, calibration servo amplifier, the indexing motor that connects successively, and described calibration positioning unit is connected with PLC.
Described left flying trident control subsystem comprises left flying trident positioning unit, left flying trident servo amplifier, the left flying trident coiling electric motor that connects successively, and described left flying trident positioning unit is connected with PLC.
Described right flying trident control subsystem comprises right flying trident positioning unit, right flying trident servo amplifier, the right flying trident coiling electric motor that connects successively, and described right flying trident positioning unit is connected with PLC.
Compared with prior art, the utlity model has following advantage:
1) mode that adopts PLC and touch-screen to combine is carried out flexibility control, makes its concision and compact, failure rate low, is convenient to revise and safeguard to have high reliability, can boost productivity greatly;
2) with PLC be the control core, utilize touch-screen that friendly man-machine interface is provided, adopt AC servo motor to carry out coiling of round trip flight fork and rotor calibration location, adopt full-automatic winding tension control subsystem, make coil winding machine coiling enamelled wire speed faster, the rotor indexing accuracy improves, and the coiling quality also obviously improves.
3) Installation and Debugging are very convenient, simplified execute-in-place, improved the flexibility of control program and man-machine interface, make systematic function more safe and reliable, the convenient monitoring production that realizes full-automatic assembly line.
4) popularizing application prospect is more widely arranged, change to be applied directly in the other industries such as automobile, dust catcher a little and go.
Description of drawings
Fig. 1 is a mechanical structure schematic diagram of the present utility model;
Fig. 2 is a structured flowchart of the present utility model.
Embodiment
Below in conjunction with the drawings and specific embodiments the utility model is elaborated.
Embodiment
As shown in Figure 1, two bobbin winding heads are driven respectively by left and right sides motor, and coiling electric motor drives on the coiling main shaft by synchronous band.Two transmission case bodies are fixed on the deck plate by linear bearing, and the side-to-side movement of transmission case body is driven by thick clamping cylinder and the smart cylinder that clamps.Indexing motor is passed to dividing spindle by synchronous band, clamps cylinder promotion dividing spindle and makes collet clamp rotor.Parallel cylinder promotes hook line overcoat, cooperates indexing motor to realize the automatic coupling of rotor commutator.
As shown in Figure 2, a kind of control system of round trip flight fork AC servo numerical control filament winder, comprise PLC1, touch-screen 2, full-automatic winding tension control subsystem 3, calibration control subsystem, left flying trident control subsystem, right flying trident control subsystem, described PLC1 is connected with touch-screen 2, full-automatic winding tension control subsystem 3, calibration control subsystem, left flying trident control subsystem, right flying trident control subsystem respectively.
Described full-automatic winding tension control subsystem 3 comprises by the full-automatic tension controller of LE-40MTB type, LX-TD type tension detector, ZKG-YN type magnetic powder brake and forming.Full-automatic tension controller is directly to measure the tension force that winds the line by tension detector, then tension data is become tension signal and pass full-automatic tension controller back, thereby the exciting curent of adjusting magnetic powder brake is automatically controlled the tension force of coiling.Enamelled wire produces certain pretension by clamping felt, twines several circles then on the straining pulley of tension detector, enters elasticity arm by guide wheel and makes enamelled wire be in tension all the time, enters the coiling main shaft by guide wheel again.By touch-screen hook wire-wound line tension data are set, add different aanalogvoltages to tension controller, adjust the tension force of enamelled wire by PLC.
Described calibration control subsystem comprises calibration positioning unit 31, calibration servo amplifier 32, the indexing motor 33 that connects successively, and described calibration positioning unit 31 is connected with PLC1.Described left flying trident control subsystem comprises left flying trident positioning unit 41, left flying trident servo amplifier 42, the left flying trident coiling electric motor 43 that connects successively, and described left flying trident positioning unit 41 is connected with PLC1.Described right flying trident control subsystem comprises right flying trident positioning unit 51, right flying trident servo amplifier 52, the right flying trident coiling electric motor 53 that connects successively, and described right flying trident positioning unit 51 is connected with PLC1.
Left side flying trident positioning unit 41, right flying trident positioning unit 51 all adopt the FX2N-1PG of MIT, left side flying trident servo amplifier 42, right flying trident servo amplifier 52 all adopt the MR-J2-70A of MIT, and left flying trident coiling electric motor 43, right flying trident coiling electric motor 53 all adopt the HC-MF73 of MIT.
Calibration positioning unit 31 adopts the FX2N-1PG of MIT, and calibration servo amplifier 32 adopts the MR-J2-40A of MIT, and indexing motor 33 adopts the HC-MF43 of MIT.
PLC1 adopts the FX2-80MR of MIT type PLC; Touch-screen 2 adopts the touch color liquid crystal monitor screen of MIT.
Claims (5)
1. the control system of round trip flight fork AC servo numerical control filament winder, it is characterized in that, comprise PLC, touch-screen, full-automatic winding tension control subsystem, calibration control subsystem, left flying trident control subsystem, right flying trident control subsystem, described PLC is connected with touch-screen, full-automatic winding tension control subsystem, calibration control subsystem, left flying trident control subsystem, right flying trident control subsystem respectively.
2. the control system of a kind of round trip flight fork AC servo numerical control filament winder according to claim 1, it is characterized in that, described full-automatic winding tension control subsystem comprises the tension detector that connects successively, full-automatic tension controller, magnetic powder brake, and described full-automatic tension controller is connected with PLC.
3. the control system of a kind of round trip flight fork AC servo numerical control filament winder according to claim 1, it is characterized in that, described calibration control subsystem comprises calibration positioning unit, calibration servo amplifier, the indexing motor that connects successively, and described calibration positioning unit is connected with PLC.
4. the control system of a kind of round trip flight fork AC servo numerical control filament winder according to claim 1, it is characterized in that, described left flying trident control subsystem comprises left flying trident positioning unit, left flying trident servo amplifier, the left flying trident coiling electric motor that connects successively, and described left flying trident positioning unit is connected with PLC.
5. the control system of a kind of round trip flight fork AC servo numerical control filament winder according to claim 1, it is characterized in that, described right flying trident control subsystem comprises right flying trident positioning unit, right flying trident servo amplifier, the right flying trident coiling electric motor that connects successively, and described right flying trident positioning unit is connected with PLC.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011201538117U CN202084432U (en) | 2011-05-13 | 2011-05-13 | Control system of dual-fork alternating-current servo numerical-control winding machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011201538117U CN202084432U (en) | 2011-05-13 | 2011-05-13 | Control system of dual-fork alternating-current servo numerical-control winding machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202084432U true CN202084432U (en) | 2011-12-21 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011201538117U Expired - Fee Related CN202084432U (en) | 2011-05-13 | 2011-05-13 | Control system of dual-fork alternating-current servo numerical-control winding machine |
Country Status (1)
| Country | Link |
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| CN (1) | CN202084432U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102780335A (en) * | 2011-05-13 | 2012-11-14 | 上海工程技术大学 | Novel winding machine control system |
| CN103050276A (en) * | 2012-12-27 | 2013-04-17 | 中国船舶重工集团公司第七二五研究所 | Constant-tension nondestructive superconducting winding device and method |
-
2011
- 2011-05-13 CN CN2011201538117U patent/CN202084432U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102780335A (en) * | 2011-05-13 | 2012-11-14 | 上海工程技术大学 | Novel winding machine control system |
| CN103050276A (en) * | 2012-12-27 | 2013-04-17 | 中国船舶重工集团公司第七二五研究所 | Constant-tension nondestructive superconducting winding device and method |
| CN103050276B (en) * | 2012-12-27 | 2015-11-18 | 中国船舶重工集团公司第七二五研究所 | A kind of identical tension can't harm superconduction Winder and method for winding |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20111221 Termination date: 20140513 |