CN203039526U - Motor rotor winding machine - Google Patents
Motor rotor winding machine Download PDFInfo
- Publication number
- CN203039526U CN203039526U CN 201220756051 CN201220756051U CN203039526U CN 203039526 U CN203039526 U CN 203039526U CN 201220756051 CN201220756051 CN 201220756051 CN 201220756051 U CN201220756051 U CN 201220756051U CN 203039526 U CN203039526 U CN 203039526U
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- China
- Prior art keywords
- rotor
- flying trident
- winding
- coiling
- flying
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- Expired - Fee Related
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- Manufacture Of Motors, Generators (AREA)
Abstract
The utility model discloses a motor rotor winding machine, which comprises a base, a motor rotor fixing seat, a motor rotor driving shaft, two groups of winding flying forks symmetrically arranged corresponding to the motor rotor driving shaft and a winding former. Two arms of each winding flying fork rotate round a flying fork rotation shaft, no interference happens between the two arms of the flying fork and the motor rotor, the front end of the flying fork arm is provided with a wire hole, and an enamelled wire winding the rotor coil passes through the wire hole; the winding former is made up of two formers, each former is corresponding with one flying fork, the height of the former does not interfere with the rotating flying fork, the opposite faces between the formers are two isosceles faces of a triangle of the convex motor rotor axis, the vertex of the isosceles face is provided with a winding mouth to wrap the motor rotor, an interval exists between the two winding mouths, and the distance of the interval is corresponding to the wire groove of the wound motor rotor; and the isosceles face of the former extends out of the boundary formed by rotation of the front end winding hole of the flying fork to form the winding guide face of the former. Through arranging two groups of winding flying forks which work at the same time and are symmetrically arranged at two axial sides of the rotor, fast winding of the motor rotor can be realized, and the work efficiency can be improved in a doubling way.
Description
Technical field
The utility model relates to a kind of Winder of motor coil, particularly a kind of coil winding machine of rotor.
Background technology
Each winding of rotor will be worn the wire casing around two intervals simultaneously, and again around next group coil, the prior motor rotor winding machine adopts one group of coiling fork wound rotor coil behind intact one group of coil, and its shortcoming is that threading speed is slower, inefficiency.
The utility model content
The utility model is in order to overcome defective in the above-mentioned prior art, by two groups of coiling flying tridents of working simultaneously are set, to realize the fast speed winding of rotor, doubling to increase work efficiency.
For achieving the above object, the utility model provides a kind of rotor coil winding machine, comprises base, rotor holder and rotor driving shaft, comprises that also two groups is symmetrically arranged coiling flying trident and winding former with the rotor driving shaft; The coiling flying trident, be fork configuration, be installed on the flying trident holder separately, its two arm is that symmetrical centre and the fork rotating shaft of being diversion are rotated with the flying trident rotating shaft, the pivot center of flying trident rotating shaft is radially vertical with the pivot center of rotor, distance between two front ends of flying trident is greater than the length of rotor, do not interfere with rotor between two arms of flying trident, the front end of flying trident arm is provided with the line hole, the enamelled wire of wound rotor coil passes from the line hole, when flying trident rotates with enamelled wire around to the wire casing of rotor; Winding former, formed by two templates, each template is corresponding with a flying trident respectively, and fixedly connected with the holder of corresponding flying trident, the height of template is between two arms of flying trident, the coiling template does not interfere with it when flying trident rotates, the length of the rotor axis direction of template and the rotor of institute's coiling are suitable, opposite face between the template is protruding leg-of-mutton two central planes such as grade to the rotor axis, be provided with half-terete coiling mouth on the summit of waiting central plane, coiling mouthful axially and rotor axial consistent, in the middle of the coiling mouth is enclosed in rotor with the rotor gap is adaptive, keep the gap between the corresponding axial edge between two coilings mouthful, the distance in gap is corresponding with the wire casing of the rotor of institute coiling; Beyond the border that the rotation that waits central plane to extend to flying trident front end of line hole of described template forms, constitute the coiling guiding face of template, the line of flying trident rotation time institute's coiling drops on the guiding face and enters the rotor wire casing along guiding face and forms continuous coil, after the coiling of finishing one group of coil, the rotor drive shaft turns, needing the wire casing of coiling to aim at coiling mouthful edge next group continues coiling, finishes until whole coiling.
In the technique scheme, the rotor transverse horizontal is placed, and flying trident rotating shaft level is stretched to rotor.
In the technique scheme, the rotor driving shaft is provided with supporting seat, and the rotor driving shaft passes the axis hole of supporting seat and is subjected to the support of axis hole, guarantees the running of rotor driving shaft steadily.
In the technique scheme, the supporting seat of rotor driving shaft is arranged on the middle part of axle, the coiling flying trident interference during not with rotation.
In the technique scheme, winding former is fastenedly connected by cylindrical joint pin and flying trident holder, the rotating shaft of flying trident is hollow shaft, is socketed in the outside of described winding former joint pin, and the end of flying trident rotating shaft stretches in the flying trident holder and is subjected to the interior transmission mechanism of holder and drives.
Compared with prior art, the utility model is realized the fast speed winding of rotor by two groups of coiling flying tridents of working simultaneously are set in the rotor axial bilateral symmetry, doubles to increase work efficiency.
Description of drawings
Fig. 1 is the schematic perspective view of a kind of rotor coil winding machine of the utility model.
Mark the following drawings mark thereon by reference to the accompanying drawings:
The 1-base, 2-rotor holder, the 21-supporting seat, 3-rotor driving shaft, the 4-template, central planes such as 41-, 42-wind the line mouthful, 5-flying trident holder, the rotating shaft of 51-flying trident, the 52-flying trident, 53-flying trident arm, 54-flying trident front end, 55-line hole,
Embodiment
Below in conjunction with accompanying drawing, an embodiment of the present utility model is described in detail, but is to be understood that protection range of the present utility model is not subjected to the restriction of embodiment.
A kind of rotor coil winding machine of the present utility model as shown in Figure 1, comprises base 1, rotor holder 2 and rotor driving shaft 3, comprises that also two groups is symmetrically arranged coiling flying trident 52 and winding former 4 with the rotor driving shaft; Coiling flying trident 52 is fork configuration, be installed on the flying trident holder 5 separately, flying trident holder 5 is connected (or being fastenedly connected) with base 1 one, two arms 53 of flying trident serve as that symmetry and the fork rotating shaft 51 of being diversion are rotated with flying trident rotating shaft 51, pivot center and the rotor of flying trident rotating shaft 51 are (not shown, the rotor axis is consistent with the axis of rotor driving shaft 3) pivot center radially vertical, distance between two front ends 54 of flying trident arm is greater than the length of rotor, do not interfere with rotor between two arms 53 of flying trident, the front end of flying trident is provided with line hole 55, the enamelled wire of wound rotor coil passes from line hole 55, when flying trident 52 rotates with enamelled wire around to the wire casing of rotor; Winding former is made up of two templates 4, each template 4 is corresponding with a flying trident 52 respectively, the height of template is between two arms of flying trident, the template 4 of winding former is fastenedly connected by cylindrical joint pin and flying trident holder 1, flying trident rotating shaft 51 is the hollow shaft (not shown), be socketed in the outside of described winding former joint pin, the end of flying trident rotating shaft 51 stretches in the flying trident holder 5 and is subjected to the interior transmission mechanism of holder and drives (not shown, be generally gear, chain, the band transmission), coiling template 4 does not interfere with it when flying trident rotates, the length of the rotor axis direction of template 4 and the rotor of institute's coiling suitable (slightly being longer than rotor usually), opposite face between the template 4 is protruding leg-of-mutton two central planes 41 such as grade to the rotor axis, be provided with half-terete coiling mouth 42 on the summit of waiting central plane 41, coiling mouthfuls 42 axially and rotor axial consistent, coiling mouth 42 is adaptive with the rotor gap, rotor is enclosed in middle, keep the gap between the corresponding axial edge between two coilings mouthful, the distance in gap is corresponding with the wire casing of the rotor of institute coiling; Beyond the border that the rotation that waits central plane 41 to extend to flying trident front end of line hole 55 of described template 4 forms, constitute the coiling guiding face of template, the line of flying trident rotation time institute's coiling drops on the guiding face and enters the rotor wire casing along guiding face and forms continuous coil, after the coiling of finishing one group of coil, the rotor drive shaft turns, needing the wire casing of coiling to aim at coiling mouthful edge next group continues coiling, finishes until whole coiling.
Further as shown in Figure 1, the rotor transverse horizontal is placed (coaxial with the rotor driving shaft), flying trident rotating shaft level is stretched to rotor, the rotor driving shaft is provided with supporting seat 21,, rotor driving shaft 3 passes the axis hole of supporting seat 21 and is subjected to the support of axis hole, guarantee 3 runnings of rotor driving shaft steadily, the support of rotor driving shaft, 21 are arranged on the middle part of axle, the coiling flying trident interference during not with rotation.
Compared with prior art, the utility model is realized the fast speed winding of rotor by two groups of coiling flying tridents of working simultaneously are set in the rotor axial bilateral symmetry, doubles to increase work efficiency.
More than disclosed only be a specific embodiment of the present utility model, still, the utility model is not limited thereto, any those skilled in the art can think variation all should fall into protection range of the present utility model.
Claims (5)
1. a rotor coil winding machine comprises base, rotor holder and rotor driving shaft, it is characterized in that, comprises that also two groups is symmetrically arranged coiling flying trident and winding former with the rotor driving shaft;
The coiling flying trident, be fork configuration, be installed on the flying trident holder separately, its two arm is that symmetrical centre and the fork rotating shaft of being diversion are rotated with the flying trident rotating shaft, the pivot center of flying trident rotating shaft is radially vertical with the pivot center of rotor, and the distance between two front ends of flying trident arm does not interfere with rotor between two arms of flying trident greater than the length of rotor, the front end of flying trident is provided with the line hole, and the enamelled wire of wound rotor coil passes from the line hole;
Winding former, formed by two templates, each template is corresponding with a flying trident respectively, and fixedly connected with the holder of corresponding flying trident, the height of template is between two arms of flying trident, winding former does not interfere with it when flying trident rotates, the length of the rotor axis direction of template and the rotor of institute's coiling are suitable, opposite face between the template is protruding leg-of-mutton two central planes such as grade to the rotor axis, be provided with half-terete coiling mouth on the summit of waiting central plane, coiling mouthful axially and rotor axial consistent, in the middle of the coiling mouth is enclosed in rotor with the rotor gap is adaptive, keep the gap between the corresponding axial edge between two coilings mouthful, the distance in gap is corresponding with the wire casing of the rotor of institute coiling;
Beyond the border that the rotation that waits central plane to extend to flying trident front end of line hole of described template forms, constitute the coiling guiding face of template.
2. a kind of rotor coil winding machine according to claim 1 is characterized in that, described rotor transverse horizontal is placed, and flying trident rotating shaft level is stretched to rotor.
3. a kind of rotor coil winding machine according to claim 1 and 2 is characterized in that, described rotor driving shaft is provided with supporting seat.
4. a kind of rotor coil winding machine according to claim 3 is characterized in that, the supporting seat of described rotor driving shaft is arranged on the middle part of axle, the coiling flying trident interference during not with rotation.
5. a kind of rotor coil winding machine according to claim 1 and 2, it is characterized in that, described winding former is fastenedly connected by cylindrical joint pin and flying trident holder, the rotating shaft of flying trident is hollow shaft, be socketed in the outside of described winding former joint pin, the end of flying trident rotating shaft stretches in the flying trident holder and is subjected to the interior transmission mechanism of holder and drives.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201220756051 CN203039526U (en) | 2012-12-31 | 2012-12-31 | Motor rotor winding machine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201220756051 CN203039526U (en) | 2012-12-31 | 2012-12-31 | Motor rotor winding machine |
Publications (1)
Publication Number | Publication Date |
---|---|
CN203039526U true CN203039526U (en) | 2013-07-03 |
Family
ID=48691611
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 201220756051 Expired - Fee Related CN203039526U (en) | 2012-12-31 | 2012-12-31 | Motor rotor winding machine |
Country Status (1)
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CN (1) | CN203039526U (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103500648A (en) * | 2013-09-27 | 2014-01-08 | 四川风发电气科技有限公司 | Coil winding machine for stereoscopic wound iron core transformer |
CN106144783A (en) * | 2016-08-31 | 2016-11-23 | 天津甘泉集团有限公司 | A kind of electric machine winding equipment |
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 |
CN108880145A (en) * | 2018-09-14 | 2018-11-23 | 苏州市帅睿自动化设备有限公司 | A kind of completely new coil winding machine |
CN109921584A (en) * | 2018-09-25 | 2019-06-21 | 广东顺德三合工业自动化设备股份有限公司 | A kind of conducting wire baffle mechanism of half iron core stator pin type coil winding machine |
CN113629963A (en) * | 2021-09-16 | 2021-11-09 | 杭州合慧智能装备有限公司 | Fly fork spool holding mechanism based on permanent magnetic force |
CN113937968A (en) * | 2021-11-18 | 2022-01-14 | 康平科技(苏州)股份有限公司 | Rotor winding device and method |
-
2012
- 2012-12-31 CN CN 201220756051 patent/CN203039526U/en not_active Expired - Fee Related
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103500648A (en) * | 2013-09-27 | 2014-01-08 | 四川风发电气科技有限公司 | Coil winding machine for stereoscopic wound iron core transformer |
CN103500648B (en) * | 2013-09-27 | 2015-12-30 | 四川风发电气科技有限公司 | A kind of tri-dimensional wound |
CN106144783A (en) * | 2016-08-31 | 2016-11-23 | 天津甘泉集团有限公司 | A kind of electric machine winding equipment |
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 |
CN108880145A (en) * | 2018-09-14 | 2018-11-23 | 苏州市帅睿自动化设备有限公司 | A kind of completely new coil winding machine |
CN109921584A (en) * | 2018-09-25 | 2019-06-21 | 广东顺德三合工业自动化设备股份有限公司 | A kind of conducting wire baffle mechanism of half iron core stator pin type coil winding machine |
CN113629963A (en) * | 2021-09-16 | 2021-11-09 | 杭州合慧智能装备有限公司 | Fly fork spool holding mechanism based on permanent magnetic force |
CN113629963B (en) * | 2021-09-16 | 2022-06-10 | 杭州合慧智能装备有限公司 | Fly fork spool holding mechanism based on permanent magnetic force |
CN113937968A (en) * | 2021-11-18 | 2022-01-14 | 康平科技(苏州)股份有限公司 | Rotor winding device and method |
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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: 20130703 Termination date: 20131231 |