CN203967931U - Automatic rotor winding machine - Google Patents
Automatic rotor winding machine Download PDFInfo
- Publication number
- CN203967931U CN203967931U CN201420340821.5U CN201420340821U CN203967931U CN 203967931 U CN203967931 U CN 203967931U CN 201420340821 U CN201420340821 U CN 201420340821U CN 203967931 U CN203967931 U CN 203967931U
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- CN
- China
- Prior art keywords
- rotor
- flying trident
- winding machine
- coiling
- wire clamp
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Abstract
A kind of automatic rotor winding machine, comprise: two coiling flying tridents, two wire clamps, rotor is fixed on the calibration main shaft of coil winding machine, described coiling flying trident, wire clamp are positioned at the central point of spaced coiling flying trident, wire clamp around the axis setting of rotor and described rotor, the axis of described coiling flying trident is vertical with the axis of rotor, a corresponding wire clamp of flying trident, and the position of described wire clamp can regulate along coiling flying trident axis direction.The utility model adopts two symmetrical coilings of coiling flying trident, coiling quality is symmetrical, dynamic balance is good, and the position of wire clamp can regulate along coiling flying trident axis direction, thereby can be easy to the first inclination angle between wire clamp and the flying trident head of the coiling flying trident in zero-bit to regulate, be convenient to line hook.
Description
Technical field
The utility model relates to coil winding machine, relates in particular to a kind of automatic rotor winding machine.
Background technology
In prior art, toward coiling line in the groove of rotor core, mostly still adopt the manual semi-automatic mode of being responsible for of false hook.This mode, in the time of coiling, manual is put on false hook after inflection line hook enclosing around neck place " α " shape coiling one, continues afterwards coiling, and groove of every coiling just must enclose around neck place " α " shape coiling one.After coiling, the line of hook being put on hook in the outside of steering gear rise piece is cut off, then the end riveting of two lines is entered in the cell body of rise piece, adopts afterwards electric welding that the end of two lines and steering gear are conducted.The rotor coil that the auxiliary semi-automatic mode of this craft winds up exists a lot of deficiencies, groove of coiling just must enclose and cut hook around neck place " α " shape coiling one and put the line on false hook, cause the waste of line raw material, production cost is improved a lot.Be exactly that coiling operation is numerous and diverse in addition, labour intensity is high, is difficult to ensure the stable and consistent of coiling quality, and production efficiency is low, also can cause the raising of production cost.
Utility model content
The problem that the utility model solves is to provide a kind of automatic rotor winding machine, can be to guarantee that rotor performance is qualified, stable, and production cost is low.
For addressing the above problem, the utility model embodiment provides a kind of automatic rotor winding machine, comprise: two coiling flying tridents, two wire clamps, rotor is fixed on the calibration main shaft of coil winding machine, described coiling flying trident, wire clamp are positioned at the central point of spaced coiling flying trident, wire clamp around the axis setting of rotor and described rotor, the axis of described coiling flying trident is vertical with the axis of rotor, a corresponding wire clamp of flying trident, and the position of described wire clamp can regulate along coiling flying trident axis direction.
Optionally, also comprise inner sleeve and outer sleeve, inner sleeve is fixed on the interior bar of calibration main shaft, outer sleeve is fixed on the outer bar of calibration main shaft and can moves forward and backward along calibration main-shaft axis direction, described inner sleeve is enclosed within rotor commutator outside and has leading groove, utilize described leading groove by wire-wound on the hook of rotor commutator.
Optionally, described wire clamp can move up and down.
Optionally, the second inclination angle of described leading groove aperture position is corresponding with the first inclination angle.
Optionally, when described outer sleeve retraction, expose the leading groove of inner sleeve, when described outer sleeve advances described in outer sleeve entangle inner sleeve.
Optionally, the opening size of described leading groove is less than the bottom size of leading groove.
Optionally, described leading groove is peariform slot.
Optionally, the bottom position of described leading groove is corresponding to the position of rotor commutator.
Optionally, also comprise, be positioned at the clamping element in described coiling flying trident centre position, for clamping rotor to be processed.
Compared with prior art, the technical program has the following advantages:
Due to two symmetrical coilings of coiling flying trident of the utility model embodiment, coiling quality is symmetrical, dynamic balance is good, and the position of wire clamp can regulate along coiling flying trident axis direction, thereby can be easy to the first inclination angle between wire clamp and the flying trident head of the coiling flying trident in zero-bit to regulate, be convenient to line hook, and by mobile wire clamp, be convenient to break line.
Further, the utility model utilizes that the leading groove of sleeve is auxiliary to be hung over line on the hook of rotor, simple in structure, easy to maintenance, need to be on hook coiling multiturn line, can improve work efficiency, the cost saving the thread.
Brief description of the drawings
The structural representation of automatic rotor winding machine when Fig. 1 is winding the line of the utility model embodiment;
Fig. 2 is the front view of the automatic rotor winding machine of Fig. 1;
Fig. 3 is the structural representation of removing the automatic rotor winding machine of clamping element and sleeve;
Fig. 4 is the structural representation of the sleeve of the utility model embodiment;
Fig. 5 is the schematic flow sheet of the rotor winding method of the utility model embodiment.
Embodiment
Below in conjunction with accompanying drawing, by specific embodiment, the technical solution of the utility model is carried out to clear, complete description.
Please refer to Fig. 1, Fig. 2 and Fig. 3, automatic rotor winding machine when Fig. 1 is winding the line of the utility model embodiment, Fig. 2 is the front view of the automatic rotor winding machine of Fig. 1, Fig. 3 is the automatic rotor winding machine of removing clamping element and inner sleeve, described automatic rotor winding machine specifically comprises: two coiling flying tridents 1, two wire clamps 2, rotor 3 is fixed on the calibration main shaft of coil winding machine, inner sleeve 7 (please refer to Fig. 4) is fixed on the interior bar of calibration main shaft, outer sleeve 4 is enclosed within the outside of inner sleeve 7, described inner sleeve, in calibration main shaft, the position of bar immobilizes, described outer sleeve 4 can move forward and backward along calibration main shaft axial direction, described inner sleeve 7 is enclosed within rotor 3 outsides and has leading groove 8 (please refer to Fig. 4), utilize described leading groove 8 by wire-wound on the hook of rotor commutator, described coiling flying trident 1, wire clamp 2 is around the axis setting of rotor 3, the axis of described coiling flying trident 1 is vertical with the axis of rotor 3, a corresponding wire clamp 2 of coiling flying trident 1, and the position of described wire clamp 2 can regulate along coiling flying trident 1 axis direction.
In the present embodiment, described inner sleeve 7 is fixed on the interior bar of calibration main shaft 1, can advance or bounce back with the outer bar of calibration main shaft in the position of outer sleeve 4 and calibration main shaft.When after outer sleeve 4 retractions, expose inner sleeve 7, make line enter the leading groove of inner sleeve 7; Utilize rotating and reverse wire-wound on the hook of rotor commutator of rotor, outer sleeve 4 advances, and described outer sleeve 4 entangles inner sleeve 7, and the line in leading groove is released to leading groove.
In the present embodiment, the coiling axis direction of flying trident and the axis direction of rotor are all horizontal direction, and therefore the line direction of described two wire clamps 2 is approximately vertical direction.In other embodiments, in the time that the axis direction of coiling flying trident and rotor changes, the line direction of described two wire clamps is vertical with the axis direction of rotor, with the axis direction near normal of coiling flying trident.
Because the position of described wire clamp 2 can regulate along coiling flying trident 1 axis direction, therefore can regulate the first inclination angle between wire clamp and the flying trident head of the coiling flying trident in zero-bit, make in the time of hanging wire, the line between wire clamp and the flying trident head in zero-bit can successfully enter the leading groove of inner sleeve 7.In the present embodiment, between described wire clamp and the flying trident head of the coiling flying trident in zero-bit, be the first inclination angle, the second inclination angle of sleeve leading groove aperture position is corresponding with the first inclination angle.The first inclination angle of described the utility model embodiment is line between the flying trident head of wire clamp, coiling flying trident in zero-bit and the angle between vertical direction, the second inclination angle is line between sleeve leading groove aperture position, rotor axis and the angle between vertical direction, and the size of the size at described the second inclination angle and the size of rotor, model, rotor commutator matches, when needs more exchanging rotor add man-hour, in changing the position of inner sleeve leading groove, only need to regulate the position of wire clamp 2 can change the first inclination angle.In the present embodiment, described wire clamp can also move through the position that regulates wire clamp up or down, can also realize and break line.
Described inner sleeve 7 is enclosed within rotor outside and has leading groove 8, utilize described leading groove 8 by wire-wound on the hook of rotor commutator.In the present embodiment, the opening size of described leading groove is less than the bottom size of leading groove, is peariform slot.In other embodiments, the shape of described leading groove can be also other shapes.By regulating the position of wire clamp 2, make the second inclination angle of sleeve leading groove aperture position corresponding with the first inclination angle, when outer sleeve retreats, wind the line that flying trident is counter to be put, wire clamp and the line between flying trident head enter in the leading groove of sleeve just.And by controlling the degree of depth of leading groove, in the time that inner sleeve entangles rotor, the bottom position of described leading groove is corresponding to the hook position of rotor, and because line enters after wire casing, rotor can just reverse and detorsion along with calibration main shaft, larger bottom size and the leading groove of circular arc easily allow line hang on the hook of rotor, and simultaneously less opening difference easily allows the line leading groove that flies out.
In the present embodiment, also comprise the clamping element 6 that is positioned at described coiling flying trident centre position, clamp the rotor for the treatment of fixing processing by clamping cylinder.
The utility model embodiment also provides a kind of rotor winding method of utilizing described automatic rotor winding machine, please refer to Fig. 5, comprising:
Step S101, initialization automatic rotor winding machine;
Step S102, utilizes inner sleeve, outer sleeve and flying trident by wire-wound on the first hook of rotor commutator;
Step S103, is just forwarding rotor to the first groove coiling position corresponding with the first hook and is winding the line;
Step S104, is reversed and is made wire clamp break line by rotor the first groove coiling position after complete line;
Step S105, rotor forwards the position of the second hook correspondence to, utilizes inner sleeve and outer sleeve that wire-wound is linked up with at second of rotor, and winds the line in the second groove coiling position;
Step S106, the like, the groove coiling positions all when rotor all complete after coiling, adjust coiling flying trident pivot angle and rotor rotational angle and flying trident and have moved left and right the clamp of wire clamp and broken line, unclamp rotor, coiling flying trident back to zero position.
Concrete, before formal coiling, first initialization automatic rotor winding machine, first utilizes locked mode that rotor is fixed on calibration main shaft and to rotor and is positioned, coiling flying trident back to zero position.
Before line is imported the leading groove of sleeve by utilization coiling flying trident hanging wire, also comprise and rotor just need to forwarded to suitable hook angle, utilize calibration main shaft correction angle, make the position of the rotor hook for the treatment of hanging wire corresponding with the position of leading groove.
When utilizing after calibration main shaft correction angle, rotor is just forwarding the first hook angle to; By two coiling flying tridents simultaneously to the rotor direction location of advancing, coiling flying trident is put certain angle counterclockwise, outer sleeve retreats, flying trident turns after an angle at the bottom of line slips into rotor commutator hook by inner sleeve leading groove clockwise, an angle of rotor reversion, overcoat advances line is released from inner sleeve leading groove, and the first hook finishes.Assist because the utility model adopts inner sleeve, outer sleeve, do not need need on hook, to ensure certain fastness, can reduce use amount and the process time of line by coiling multiturn line as prior art, and there will not be the problem of mistake hanging wire.
Then start rotor to wind the line, the concrete steps that wind the line in the first groove coiling position of the first hook correspondence comprise:
Just forwarding rotor to first groove coiling position and winding the line, number of turns is than few approximately 0.5 circle of the default number of turn, the flying trident stop place winding the line after finishing in the outside of winding former near operating table surface end; Rotor is inverted to an angle, and wire clamp moves upward and breaks line, then rotor forward equal angular; The counterclockwise forward swing of coiling flying trident, 0.5 circle of compensate for residual.
To the first groove coiling position, after complete line, rotor forwards the position of the second hook correspondence to, utilizes inner sleeve and outer sleeve that wire-wound is linked up with at second of rotor, and winds the line in the second groove coiling position; The like when all groove of rotor coiling position all completes after coiling, adjust coiling flying trident pivot angle and rotor rotational angle and complete the clamp of wire clamp and break line, unclamp rotor, coiling flying trident back to zero position.
Wherein, rotor winding former in the time rotating and reverse is backed out or is not backed out.
Although the utility model with preferred embodiment openly as above; but it is not for limiting the utility model; any those skilled in the art are not departing from spirit and scope of the present utility model; can utilize method and the technology contents of above-mentioned announcement to make possible variation and amendment to technical solutions of the utility model; therefore; every content that does not depart from technical solutions of the utility model; any simple modification, equivalent variations and the modification above embodiment done according to technical spirit of the present utility model, all belong to the protection range of technical solutions of the utility model.
Claims (9)
1. an automatic rotor winding machine, it is characterized in that, comprise: two coiling flying tridents, two wire clamps, rotor is fixed on the calibration main shaft of coil winding machine, described coiling flying trident, wire clamp are positioned at the central point of spaced coiling flying trident, wire clamp around the axis setting of rotor and described rotor, the axis of described coiling flying trident is vertical with the axis of rotor, a corresponding wire clamp of flying trident, and the position of described wire clamp can regulate along coiling flying trident axis direction.
2. automatic rotor winding machine as claimed in claim 1, it is characterized in that, also comprise inner sleeve and outer sleeve, inner sleeve is fixed on the interior bar of calibration main shaft, outer sleeve is fixed on the outer bar of calibration main shaft and can moves forward and backward along calibration main-shaft axis direction, described inner sleeve is enclosed within rotor commutator outside and has leading groove, utilize described leading groove by wire-wound on the hook of rotor commutator.
3. automatic rotor winding machine as claimed in claim 2, is characterized in that, and the second inclination angle of described leading groove aperture position is corresponding with the first inclination angle.
4. automatic rotor winding machine as claimed in claim 2, is characterized in that, exposes the leading groove of inner sleeve when described outer sleeve retraction, when described outer sleeve advances described in outer sleeve entangle inner sleeve.
5. automatic rotor winding machine as claimed in claim 2, is characterized in that, the opening size of described leading groove is less than the bottom size of leading groove.
6. automatic rotor winding machine as claimed in claim 2, is characterized in that, described leading groove is peariform slot.
7. automatic rotor winding machine as claimed in claim 2, is characterized in that, the bottom position of described leading groove is corresponding to the position of rotor commutator.
8. automatic rotor winding machine as claimed in claim 1, is characterized in that, described wire clamp can move up and down.
9. automatic rotor winding machine as claimed in claim 1, is characterized in that, also comprises, is positioned at the clamping element in described coiling flying trident centre position, for clamping rotor to be processed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420340821.5U CN203967931U (en) | 2014-06-24 | 2014-06-24 | Automatic rotor winding machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420340821.5U CN203967931U (en) | 2014-06-24 | 2014-06-24 | Automatic rotor winding machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203967931U true CN203967931U (en) | 2014-11-26 |
Family
ID=51928475
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420340821.5U Expired - Fee Related CN203967931U (en) | 2014-06-24 | 2014-06-24 | Automatic rotor winding machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203967931U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107394978A (en) * | 2017-05-04 | 2017-11-24 | 陈敬恩 | Rotor round trip flight fork coil winding machine can winding displacement mould, coil winding machine and its method for winding |
| CN109936262A (en) * | 2019-04-11 | 2019-06-25 | 中山市蒙力电机电器有限公司 | Full automatic car starts motor and oil pump rotor multilayer winding machine |
-
2014
- 2014-06-24 CN CN201420340821.5U patent/CN203967931U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107394978A (en) * | 2017-05-04 | 2017-11-24 | 陈敬恩 | Rotor round trip flight fork coil winding machine can winding displacement mould, coil winding machine and its method for winding |
| CN109936262A (en) * | 2019-04-11 | 2019-06-25 | 中山市蒙力电机电器有限公司 | Full automatic car starts motor and oil pump rotor multilayer winding machine |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20141126 Termination date: 20200624 |