CN110224558A - A kind of flying trident winding mechanism - Google Patents
A kind of flying trident winding mechanism Download PDFInfo
- Publication number
- CN110224558A CN110224558A CN201910354470.0A CN201910354470A CN110224558A CN 110224558 A CN110224558 A CN 110224558A CN 201910354470 A CN201910354470 A CN 201910354470A CN 110224558 A CN110224558 A CN 110224558A
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- China
- Prior art keywords
- main shaft
- axle sleeve
- flying trident
- coiling
- winding mechanism
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- 230000007246 mechanism Effects 0.000 title claims abstract description 32
- 238000004804 winding Methods 0.000 title claims abstract description 26
- 238000000926 separation method Methods 0.000 claims description 7
- 230000000694 effects Effects 0.000 claims description 2
- 230000001360 synchronised effect Effects 0.000 description 4
- 238000007667 floating Methods 0.000 description 3
- 230000001939 inductive effect Effects 0.000 description 3
- 238000005299 abrasion Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 244000025254 Cannabis sativa Species 0.000 description 1
- 235000012766 Cannabis sativa ssp. sativa var. sativa Nutrition 0.000 description 1
- 235000012765 Cannabis sativa ssp. sativa var. spontanea Nutrition 0.000 description 1
- 235000009120 camo Nutrition 0.000 description 1
- 235000005607 chanvre indien Nutrition 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 210000000887 face Anatomy 0.000 description 1
- 239000011487 hemp Substances 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K15/00—Methods or apparatus specially adapted for manufacturing, assembling, maintaining or repairing of dynamo-electric machines
- H02K15/04—Methods or apparatus specially adapted for manufacturing, assembling, maintaining or repairing of dynamo-electric machines of windings, prior to mounting into machines
- H02K15/0435—Wound windings
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- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Power Engineering (AREA)
- Manufacture Of Motors, Generators (AREA)
- Coil Winding Methods And Apparatuses (AREA)
Abstract
Present invention discloses a kind of flying trident winding mechanisms, it includes coiling unit, coiling unit includes fourth drive member, the coiling main shaft rotated is driven by fourth drive member, the movable plate that can be moved axially along coiling main shaft, coiling main shaft includes the first axle sleeve being erected on a fixed frame by first bearing, it is fixed on first axle and covers upper synchronizing wheel, axially movable the second axle sleeve being arranged in the first axle sleeve, the central spindle in the second axle sleeve is erected at by second bearing, the main shaft of central spindle front end is set, the conducting wire wheel seat being fixedly connected with the second axle sleeve rear end, the conduit being axially disposed in the first axle sleeve eccentric region, be fixed at the first axle sleeve front end and it is parallel to the line mouth of main shaft setting, the other end of conducting wire wheel seat is erected on movable plate by 3rd bearing.The present invention realizes threading by spindle eccentricity position, so that threading is easier；Main shaft does not rotate, and forms rib using the tight product side surface of spindle end face paste, ensures around line mass.
Description
[technical field]
The invention belongs to spooling equipment technical fields, more particularly to a kind of flying trident winding mechanism.
[background technique]
Smart phone auto-focusing, camera lens or far or is closely realized by the way that camera is locked voice coil motor.Voice coil motor
Abbreviation VCM (Voice Coil Motor), coil is core part.The coiling position of VCM motor skeleton does not have a rib, and coil
It is distributed on two different faces of skeleton, the end of a thread line tail is also wrapped on other two face, is equivalent to four of a square
Side will carry out operation, and production technology is more complex, and required precision is also high.Therefore, then it needs that product is first rotated to a side
Then face carries out coil-winding to the side, then rotate to another side and carry out hanging wire；Then it is rotated again to a side
Coil-winding is carried out, another side is rotated again to and carries out hanging wire.Since the coiling position of VCM motor skeleton does not have rib, in coiling
It is easy to appear the phenomenon that coiling is scattered in the process；And the most of line of winding mechanism of the prior art is worn across central spindle
Hemp is tired and difficult.
Therefore, it is necessary to provide the new flying trident winding mechanism of one kind to solve the above problems.
[summary of the invention]
The main purpose of the present invention is to provide a kind of flying trident winding mechanisms, are realized and are threaded by spindle eccentricity position, made
It must thread and be easier；Main shaft does not rotate, and forms rib using the tight product side surface of spindle end face paste, ensures around line mass.
The present invention is achieved through the following technical solutions above-mentioned purpose: a kind of flying trident winding mechanism comprising coiling unit, institute
State coiling unit include fourth drive member, by the fourth drive member driving rotated coiling main shaft, can be along the coiling
Main shaft axial movement movable plate, the coiling main shaft include the first axle sleeve being erected at by first bearing on a fixed frame,
The first axle is fixed on to cover upper synchronizing wheel, axially movable the second axle sleeve being arranged in first axle sleeve, pass through
Central spindle that second bearing is erected in second axle sleeve, the main shaft that the central spindle front end is set, with after second axle sleeve
Hold the conducting wire wheel seat being fixedly connected, the conduit being axially disposed in the first axle sleeve eccentric region, be fixed at it is described
First axle sleeve front end and be parallel to the line mouth of main shaft setting, the other end of the conducting wire wheel seat passes through 3rd bearing erection
On the movable plate.
It further, further include three mould group transfer mechanisms, the three moulds group transfer mechanism includes the first actuator, by described
The driving of first actuator carries out the second actuator of side-to-side movement, is driven the third moved forward and backward by second actuator
Actuator is carried out second support plate that moves up and down by third actuator driving.
Further, the fixed frame, the fourth drive member are fixed in second support plate.
Further, the coiling main shaft further includes the flying trident mounting base for being fixed on first axle sleeve front end, is fixed on
Flying trident in the flying trident mounting base, the line mouth are fixed on the flying trident.
Further, the front end sleeve of the central spindle is equipped with the elastic component for supporting the main shaft.
Further, the central spindle is linked together with the main shaft by a pin, and restriction is provided on the main shaft
The strip groove of the pin shaft orientation moving range.
Further, it is provided with the first guide roller on the conducting wire wheel seat, the second guide roller is provided on the flying trident；Line
Body enters from one end of the conducting wire wheel seat to be entered in the conduit around first guide roller, out after around described
Second guide roller is extend into above product surface inside the line mouth.
Further, the incoming line and line outlet of the incoming line of the conducting wire wheel seat and line outlet, the conduit both ends
It is provided with the magnetic eye for preventing wire rod from rubbing.
Further, the coiling unit further includes the cylinder for driving the movable plate movement.
Further, there are two the first bearing settings, and upper first isolation is covered by being set in the first axle
Set is isolated and limits its position；Wherein,
The another side of one first bearing covers upper bulge loop positioning by first axle；
The second separation sleeve is provided between another first bearing and the synchronizing wheel；
The mounting plate positioning that the other end of the synchronizing wheel is connect by one with the first axle sleeve axial restraint.
Compared with prior art, a kind of beneficial effect of flying trident winding mechanism of the present invention is: wire rod only central spindle, but
By spindle eccentricity position, threading is easier；When spindle end face paste stringing circle side, axis and coil are opposing stationary, avoid line
Circle abrasion；Main shaft is adjacent to coil side using elastic floating mode, avoids hard collision；The axial of central spindle is cleverly designed to move
Dynamic, the whole axis for avoiding coiling main shaft is mobile, and coiling precision and winding efficiency are higher.
[Detailed description of the invention]
Fig. 1 is the structural schematic diagram of the embodiment of the present invention；
Fig. 2 is the structural schematic diagram of coiling unit in the embodiment of the present invention；
Fig. 3 is the schematic cross-sectional view of coiling main shaft in the embodiment of the present invention；
Digital representation in figure:
100 flying trident winding mechanisms；
1 three mould group transfer mechanisms, 11 first actuators, 12 second actuators, 13 first support plates, 14 third actuators,
15 second support plates；
2 coiling units, 21 fixed frames, 22 fourth drive members, 23 coiling main shafts, 231 first bearings, 232 first axle sleeves,
233 synchronizing wheels, 234 second axle sleeves, 235 second bearings, 236 central spindles, 237 main shafts, 238 conducting wire wheel seats, 239 conduits, 240 fly
Fork mounting base, 241 flying tridents, 242 line mouths, 243 3rd bearings, 244 first separation sleeves, 245 second separation sleeves, 246 mounting plates,
247 support sleeves, 248 elastic components, 249 pins, 250 first guide rollers, 251 second guide rollers, 252 magnetic eyes, 24 movable plates, 25
Cylinder, 26 inductive disks, 27 photoelectric sensors.
[specific embodiment]
Embodiment:
Fig. 1-Fig. 3 is please referred to, the present embodiment is flying trident winding mechanism 100 comprising three mould group transfer mechanisms 1, setting exist
The coiling unit 2 of three mould group transfer mechanisms, 1 movable end.
Three mould group transfer mechanisms 1 include the first actuator 11, are driven the second of progress side-to-side movement by the first actuator 11
Actuator 12, is fixed on 13 front end of the first support plate at the first support plate 13 moved forward and backward by the driving of the second actuator 12
The third actuator 14 of lower surface is carried out second support plate 15 that moves up and down, the first support plate 12 by the driving of third actuator 14
On be fixed with a vertical lead screw, the round end of third actuator 14 passes through lead screw rotation described in synchronous belt and synchronous wheel drive
Turn, the bottom of the lead screw is fixed in a fixed plate, and the fixed plate is fixedly connected with the first support plate 13, the second support plate
It is provided with the nut with lead screw cooperation on 15, is driven by lead screw rotary motion and realizes up and down motion.Three mould group transfer mechanisms 1
Structure is compact to design, saves space.
Coiling unit 2 includes the fixed frame 21 being fixed in the second support plate 15 and fourth drive member 22, is erected at fixation
Several coiling main shafts 23 rotated are driven on frame 21 and by fourth drive member 22, scalable are moved along coiling main shaft 23 is axial
Movable plate 24, driving movable plate 24 move cylinder 25.
The piston end of cylinder 25 is fixed on fixed frame 21, and 25 cylinder body of cylinder is fixed on movable plate 24 with movable plate 24
Stretching motion together.
Coiling main shaft 23 includes the first axle sleeve 232 being erected on fixed frame 21 by a pair of of first bearing 231, is fixed on
Synchronizing wheel 233 on first axle sleeve 232, passes through the at axially movable the second axle sleeve 234 being arranged in the first axle sleeve 232
Central spindle 236 that two bearings 235 are erected in the second axle sleeve 234, the main shaft 237 that 236 front end of central spindle is set, with the second axle sleeve
It is conducting wire wheel seat 238 that 234 rear ends are fixedly connected, the conduit 239 being axially disposed in 232 eccentric region of the first axle sleeve, fixed
232 front end of the first axle sleeve flying trident mounting base 240, be fixed in flying trident mounting base 240 flying trident 241, be fixed on flying trident 241
The other end of front end and the line mouth 242 for being parallel to the setting of main shaft 237, conducting wire wheel seat 238 is erected at activity by 3rd bearing 243
On plate 24.
Two first bearings 231 are isolated by the first separation sleeve 244 being set on the first axle sleeve 232 and limit its position
It sets.The another side of one of first bearing 231 positioning is realized by the bulge loop on the first axle sleeve 232.Another first bearing
The second separation sleeve 245 is provided between 231 and synchronizing wheel 233.The other end of synchronizing wheel 233 passes through one and 232 axis of the first axle sleeve
Positioning is realized to the mounting plate 246 being fixedly connected.
The both sides of second axle sleeve 234 pass through a pair of of support sleeve 247 and are arranged in the first axle sleeve 232, realize axially-displaceable
It is dynamic.
Synchronizing wheel 233 is connect with the round end of fourth drive member 22 by synchronous belt and realizes synchronous rotary.
The front end sleeve of central spindle 236 is equipped with the elastic component 248 for supporting main shaft 237, and central spindle 236 and main shaft 237 pass through a pin
249 link together, and the strip groove (not identifying in figure) for limiting 249 shaft orientation moving range of pin is provided on main shaft 237, works as axis
When core 236 moves axially, the axial side surface for supporting product with certain elastic floating of main shaft 237 is realized to product side
The rib in face guarantees so that there is enclosing on the both sides in coiling face around line mass.
Be provided with the first guide roller 250 on conducting wire wheel seat 238, be provided with the second guide roller 251 on flying trident 241, wire body from
One end of conducting wire wheel seat 238, which enters, to be entered in conduit 239 around the first guide roller 250, out after bypass the second guide roller
It is extend into inside 251 warp mouths 242 above product surface.The incoming line and line outlet, 239 both ends of conduit of conducting wire wheel seat 238
Incoming line and line outlet be provided with the magnetic eye 252 for preventing wire rod from rubbing.
It is provided with an inductive disks 26 on one of coiling main shaft 23, is fixed on fixed frame 21 and inductive disks 26 is felt
The photoelectric sensor 27 answered.
The working principle of coiling unit 2 are as follows: cylinder 25 drives movable plate 24 to move axially, and movable plate 24 is with 3rd bearing
243, conducting wire wheel seat 238, the second axle sleeve 234, central spindle 236, pin 249, main shaft 237 move axially together, and 237 front end of main shaft is supported
Handle product side；Fourth drive member 22 drives the rotation of the first axle sleeve 232 with synchronizing wheel 233, in addition to central spindle 236, pin
249, main shaft 237 does not turn, and the remaining part in coiling main shaft 23 is as the first axle sleeve 232 rotates together；The online mouth 242 of wire rod
End is rotated around the side surface that 237 end of main shaft supports, and realizes coiling；After the completion of the coiling of one side, cylinder 25 is retracted,
The revocation of main shaft 237 supports product side surface；Product rotates an angle, carries out the coiling or other operations of lower one side,
Until all side coilings are completed.
Realize that the three-dimensional space of coiling unit 2 is mobile by three mould group transfer mechanisms 1.
The beneficial effect of the present embodiment flying trident winding mechanism 100 is: wire rod only central spindle, but passes through spindle eccentricity position
It sets, threading is easier；When spindle end face paste stringing circle side, axis and coil are opposing stationary, avoid coil abrasion；Main shaft uses
Elastic floating mode is adjacent to coil side, avoids hard collision；The axial movement for cleverly designing central spindle, avoids coiling master
The whole axis of axis is mobile, and coiling precision and winding efficiency are higher.
Above-described is only some embodiments of the present invention.For those of ordinary skill in the art, not
Under the premise of being detached from the invention design, various modifications and improvements can be made, these belong to protection model of the invention
It encloses.
Claims (10)
1. a kind of flying trident winding mechanism, it is characterised in that: it includes the coiling main shaft for carrying out coiling to product, the coiling main shaft
Including be erected on a fixed frame by first bearing the first axle sleeve, be fixed on the first axle and cover upper synchronizing wheel, axial direction
The second axle sleeve for being movably disposed in first axle sleeve is erected at the axis in second axle sleeve by second bearing
Core, the conducting wire wheel seat being fixedly connected with second axle sleeve rear end, is axially disposed within institute at the main shaft that the central spindle front end is arranged in
State the conduit in the first axle sleeve eccentric region, be fixed at first axle sleeve front end and be parallel to the main shaft setting
Line mouth.
2. flying trident winding mechanism as described in claim 1, it is characterised in that: it further include coiling unit, the coiling unit packet
The movable plate that includes fourth drive member, can move axially along the coiling main shaft, the coiling main shaft are driven by the fourth drive member
Dynamic to be rotated, the other end of the conducting wire wheel seat is erected on the movable plate by 3rd bearing.
3. flying trident winding mechanism as claimed in claim 2, it is characterised in that: further include three mould group transfer mechanisms, three mould
Group transfer mechanism include the first actuator, by first actuator drive carry out side-to-side movement the second actuator, by described
Second actuator drives the third actuator moved forward and backward, move up and down second by third actuator driving
Fagging；The fixed frame, the fourth drive member are fixed in second support plate.
4. flying trident winding mechanism as described in claim 1, it is characterised in that: the coiling main shaft further includes being fixed on described
The flying trident mounting base of one axle sleeve front end, the flying trident being fixed in the flying trident mounting base, the line mouth are fixed on the flying trident.
5. flying trident winding mechanism as described in claim 1, it is characterised in that: the front end sleeve of the central spindle is equipped with and supports the master
The elastic component of axis.
6. flying trident winding mechanism as claimed in claim 5, it is characterised in that: the central spindle and the main shaft are connected by a pin
It is connected together, the strip groove for limiting the pin shaft orientation moving range is provided on the main shaft.
7. flying trident winding mechanism as claimed in claim 4, it is characterised in that: be provided with the first conducting wire on the conducting wire wheel seat
It takes turns, is provided with the second guide roller on the flying trident；Wire body enters from one end of the conducting wire wheel seat bypasses first guide roller
Enter in the conduit, out after extend into inside the line mouth above product surface around second guide roller.
8. flying trident winding mechanism as described in claim 1, it is characterised in that: the incoming line and line outlet of the conducting wire wheel seat,
The incoming line and line outlet at the conduit both ends are provided with the magnetic eye for preventing wire rod from rubbing.
9. flying trident winding mechanism as described in claim 1, it is characterised in that: the coiling unit further includes driving the activity
The cylinder of plate movement.
10. flying trident winding mechanism as described in claim 1, it is characterised in that: there are two the first bearing settings, and passes through
Upper first separation sleeve of the first axle set is set in be isolated and limit its position；Wherein,
The another side of one first bearing covers upper bulge loop positioning by first axle；
The second separation sleeve is provided between another first bearing and the synchronizing wheel；
The mounting plate positioning that the other end of the synchronizing wheel is connect by one with the first axle sleeve axial restraint.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910354470.0A CN110224558B (en) | 2019-04-29 | 2019-04-29 | Flying fork winding mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910354470.0A CN110224558B (en) | 2019-04-29 | 2019-04-29 | Flying fork winding mechanism |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN110224558A true CN110224558A (en) | 2019-09-10 |
| CN110224558B CN110224558B (en) | 2024-03-19 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910354470.0A Active CN110224558B (en) | 2019-04-29 | 2019-04-29 | Flying fork winding mechanism |
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| Country | Link |
|---|---|
| CN (1) | CN110224558B (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20050061906A1 (en) * | 2003-09-23 | 2005-03-24 | Burch Jerry C. | Horizontal winding machine |
| CN203301326U (en) * | 2013-06-09 | 2013-11-20 | 江苏星光发电设备有限公司 | Winding mechanism for generator rotor coil |
| US20150042194A1 (en) * | 2013-08-09 | 2015-02-12 | Johnson Electric S.A. | Single-phase brushless motor |
| CN106549540A (en) * | 2016-12-14 | 2017-03-29 | 东莞拓蓝自动化科技有限公司 | The scratch resistant line mechanism of coil winding machine |
| CN209948909U (en) * | 2019-04-29 | 2020-01-14 | 苏州恊合自动化科技有限公司 | Flying fork winding mechanism |
-
2019
- 2019-04-29 CN CN201910354470.0A patent/CN110224558B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20050061906A1 (en) * | 2003-09-23 | 2005-03-24 | Burch Jerry C. | Horizontal winding machine |
| CN203301326U (en) * | 2013-06-09 | 2013-11-20 | 江苏星光发电设备有限公司 | Winding mechanism for generator rotor coil |
| US20150042194A1 (en) * | 2013-08-09 | 2015-02-12 | Johnson Electric S.A. | Single-phase brushless motor |
| CN106549540A (en) * | 2016-12-14 | 2017-03-29 | 东莞拓蓝自动化科技有限公司 | The scratch resistant line mechanism of coil winding machine |
| CN209948909U (en) * | 2019-04-29 | 2020-01-14 | 苏州恊合自动化科技有限公司 | Flying fork winding mechanism |
Also Published As
| Publication number | Publication date |
|---|---|
| CN110224558B (en) | 2024-03-19 |
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