CN1473681A - Automatic rotor spot welder - Google Patents
Automatic rotor spot welder Download PDFInfo
- Publication number
- CN1473681A CN1473681A CNA021345236A CN02134523A CN1473681A CN 1473681 A CN1473681 A CN 1473681A CN A021345236 A CNA021345236 A CN A021345236A CN 02134523 A CN02134523 A CN 02134523A CN 1473681 A CN1473681 A CN 1473681A
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- loading
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- welding
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Abstract
The automatic rotor spot welder is for connection between the rotor winding and the commutator in miniature motor. The automatic rotor spot welder consists of frame, welding unit, feeding rail, material guide plate, support, welding head, electric system, welding cylinder, manipulator, feeding cylinder, sensor, discharge rail, vibration rack, pneumatic system, charge and discharge cylinder and cooling system. The automatic rotor spot welder can realize automatic charge and discharge, automatic location, automatic welding, automatic counting and programmed operation, and may be used in welding various rotor and commutator in different specifications at high efficiency and high precision.
Description
This machine relates to a kind of invention of welding the automation special equipment that the micro-motor rotor winding is connected with commutator.
In welding micro-motor rotor winding and operation that commutator is connected, the mostly manual or semi-automatic welding of employing at present, thereby can not adapt to suitability for industrialized production, work efficiency is lower, poor reliability, cost height.
Purpose of the present invention changes manual and semi-automatic welding into automatic welding, thereby improves work efficiency and reliability, reaches the purpose that automatic industrial is produced.
Purpose of the present invention realizes in the following manner.
Automatic rotor spot welder of the present invention is to be made of fuselage 1, welding machine 2, blanking track 3, loading and unloading guide plate 4, support 5, soldering tip 6, support 7, electrical system 8, weld cylinder 9, manipulator 10, feeding cylinder 11, sensor 12, material loading track 13, vibrations tooth bar 14, pneumatic system 15, loading and unloading cylinder 16, cooling system 17.It is characterized in that (as shown in the figure):
In this fuselage 1 welding machine 2 is housed, loading and unloading cylinder 16, cooling system 17.This is equipped with blanking track 3 above fuselage 1, material loading track 13, and loading and unloading guide plate 4, it is by 16 transmissions of last therapeutic method to keep the adverse qi flowing downward material cylinder.Vibrations tooth bar 14 is equipped with in these loading and unloading guide plate 4 both sides, when loading and unloading guide plate 4 moves up and down, and material loading track 13,3 vibrations of blanking track, rotor is along track material loading and blanking.On this fuselage 1, soldering tip 6 is housed in the loading and unloading guide plate 4, support 7, weld cylinder 9, and support 5, sensor 12.On this blanking track 13 feeding cylinder 11 is housed, manipulator 10.Be used for feeding and promote rotor transposition welding.Electrical system 8 and pneumatic system 15 also are housed on this fuselage 1.This electrical system is provided with programmable, welding settings of counting, voltage, current settings, the welding cycle is set, time set, and automatically, manual, counting, disorderly closedown function.
These facility have compact conformation, and volume is little, and performance is good, automatic loading/unloading, location, transposition, welding automatically automatically, automatically count programmable, efficient height, the precision height, good reliability, applied widely, change the rotor commutator that frock can be welded different size, and can realize people's multi-machine operation, saved artificial greatly and improved precision.
Claims (6)
- Automatic rotor spot welder of the present invention includes fuselage 1, blanking track 3, loading and unloading guide plate 4, support 5, soldering tip 6, support 7, electrical system 8, weld cylinder 9, manipulator 10, feeding cylinder 11, sensor 12, material loading track 13, vibrations tooth bar 14, pneumatic system 15, loading and unloading cylinder 16, cooling system 17 formations.It is characterized in that (as shown in the figure):1, in this fuselage 1 welding machine 2 is housed, loading and unloading cylinder 16, cooling system 17.
- 2, this is equipped with blanking track 3 above fuselage 1, material loading track 13, and loading and unloading guide plate 4, it is by 16 transmissions of loading and unloading cylinder.
- 3, vibrations tooth bar 14 is equipped with in the both sides of loading and unloading guide plate, when loading and unloading guide plate 4 moves up and down, and material loading track 13,3 vibrations of blanking track, rotor is along track material loading and blanking.
- 4, on this fuselage 1, soldering tip 6 is housed in the loading and unloading guide plate 4, support 7, weld cylinder 9, and support 5, sensor 12.
- 5, on this blanking track 13 feeding cylinder 11 is housed, manipulator 10 is used for feeding and promotes rotor transposition welding.
- 6, on this fuselage 1 electrical system 8 and pneumatic system 15 are housed also.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNA021345236A CN1473681A (en) | 2002-08-07 | 2002-08-07 | Automatic rotor spot welder |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNA021345236A CN1473681A (en) | 2002-08-07 | 2002-08-07 | Automatic rotor spot welder |
Publications (1)
Publication Number | Publication Date |
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CN1473681A true CN1473681A (en) | 2004-02-11 |
Family
ID=34145835
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CNA021345236A Pending CN1473681A (en) | 2002-08-07 | 2002-08-07 | Automatic rotor spot welder |
Country Status (1)
Country | Link |
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CN (1) | CN1473681A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN100534694C (en) * | 2007-09-24 | 2009-09-02 | 浙江巨力电机成套设备有限公司 | Single cylinder dual-action type spot welding machine welding head |
CN103028857A (en) * | 2012-12-19 | 2013-04-10 | 上海博泽电机有限公司 | Method and device for welding motor rotor |
CN103706934A (en) * | 2013-12-24 | 2014-04-09 | 湖州凯合电机有限公司 | Automatic wire feeding welding system of starter armature |
CN103706935A (en) * | 2013-12-24 | 2014-04-09 | 湖州凯合电机有限公司 | Automatic wire feeding welding system of starter armature and method for manufacturing the starter armature |
CN103921094A (en) * | 2013-01-15 | 2014-07-16 | 苏州工业园区高登威科技有限公司 | Auxiliary assembly device |
CN103921093A (en) * | 2013-01-15 | 2014-07-16 | 苏州工业园区高登威科技有限公司 | Auxiliary assembly device |
CN103921092A (en) * | 2013-01-15 | 2014-07-16 | 苏州工业园区高登威科技有限公司 | Auxiliary assembly device |
-
2002
- 2002-08-07 CN CNA021345236A patent/CN1473681A/en active Pending
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN100534694C (en) * | 2007-09-24 | 2009-09-02 | 浙江巨力电机成套设备有限公司 | Single cylinder dual-action type spot welding machine welding head |
CN103028857A (en) * | 2012-12-19 | 2013-04-10 | 上海博泽电机有限公司 | Method and device for welding motor rotor |
CN103921094A (en) * | 2013-01-15 | 2014-07-16 | 苏州工业园区高登威科技有限公司 | Auxiliary assembly device |
CN103921093A (en) * | 2013-01-15 | 2014-07-16 | 苏州工业园区高登威科技有限公司 | Auxiliary assembly device |
CN103921092A (en) * | 2013-01-15 | 2014-07-16 | 苏州工业园区高登威科技有限公司 | Auxiliary assembly device |
CN103706934A (en) * | 2013-12-24 | 2014-04-09 | 湖州凯合电机有限公司 | Automatic wire feeding welding system of starter armature |
CN103706935A (en) * | 2013-12-24 | 2014-04-09 | 湖州凯合电机有限公司 | Automatic wire feeding welding system of starter armature and method for manufacturing the starter armature |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
WD01 | Invention patent application deemed withdrawn after publication |