CN105322732A - Assembly technology of fan-shaped slice rotor core - Google Patents
Assembly technology of fan-shaped slice rotor core Download PDFInfo
- Publication number
- CN105322732A CN105322732A CN201410378731.XA CN201410378731A CN105322732A CN 105322732 A CN105322732 A CN 105322732A CN 201410378731 A CN201410378731 A CN 201410378731A CN 105322732 A CN105322732 A CN 105322732A
- Authority
- CN
- China
- Prior art keywords
- dove tail
- iron core
- tail block
- wheel disk
- assembly technology
- 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.)
- Pending
Links
- 238000005516 engineering process Methods 0.000 title claims abstract description 17
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 32
- 238000003475 lamination Methods 0.000 claims abstract description 14
- 238000004080 punching Methods 0.000 claims abstract description 14
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 13
- 229910052802 copper Inorganic materials 0.000 claims abstract description 13
- 239000010949 copper Substances 0.000 claims abstract description 13
- 238000003466 welding Methods 0.000 claims abstract description 7
- 230000004323 axial length Effects 0.000 claims abstract description 4
- 230000000149 penetrating effect Effects 0.000 claims abstract description 4
- 230000033001 locomotion Effects 0.000 claims description 4
- 238000001816 cooling Methods 0.000 claims description 3
- 238000000034 method Methods 0.000 claims 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
Landscapes
- Manufacture Of Motors, Generators (AREA)
Abstract
The invention relates to an assembly technology of a fan-shaped slice rotor core. The assembly technology comprises the following steps: evenly putting gaskets between a wheel disk connected with a wheel disk shaft and dovetail blocks in an axial length, and then screwing hexagon socket screws; taking off the gaskets, carrying out an iron core lamination; penetrating into copper bars after the lamination is ended, and then axially pre-tightening the iron core; tightening taper keys under the condition of ensuring circumferential gaps between the dovetail blocks and a punching plate; pre-tightening the iron core again after preheating the iron core, and tightening the taper keys between the dovetail blocks and the punching plate; and welding the wheel disk of the wheel disk shaft and the dovetail blocks. The assembly technology provided by the invention has the characteristics that the iron core is convenient to laminate; the copper bars are easy to penetrate; and a rotor does not deform after a motor runs.
Description
Technical field
The present invention relates to a kind of fanning strip rotor core assembly technology.
Background technology
General fanning strip rotor core assembly technology is with Bolt Connection wheel disk shaft disc and dove tail block, but not pretension bolt, after pre-installing axial upper, middle and lower three iron leg core and determining the locus of dove tail block, the location hole that drills and reams in the non-lamination position of dove tail block also makes alignment pin, then remove three iron leg cores of prepackage, after welding wheel disk shaft disc and dove tail block after coupling bolt, carry out lamination; Due to the existence of welding deformation, the locus of dove tail block is changed, can not carry out smoothly during fanning strip 1/2 closed assembly, and cause the iron core gap after lamination to diminish, grooved size can not be ensured, make copper bar penetrate difficulty; Also cause during taper key hammering is that punching is moved simultaneously, cannot ensure iron core and key contacts area and quality, occur the phenomenons such as iron core side rejection tablet, taper key loosen after motor runs a period of time, and initiation motor oscillating, copper bar snap fracture etc.
Summary of the invention
The present invention seeks to solve that the iron core slot molded dimension that causes of general fanning strip rotor core assembly technology can not ensure, copper bar penetrates the defects such as difficulty, iron core and key contacts area deficiency after lamination, avoids the generation of associated motor quality problems.
The present invention is achieved in that a kind of fanning strip rotor core assembly technology, comprises the following steps:
Step one, when wheel disk shaft disc connects with dove tail block, wheel disk shaft disc and dove tail interblock axial length is evenly placed after adjusting pad, is screwed by attachment bolt;
Step 2, takes away wheel disk shaft disc and dove tail interblock adjusts pad, ensures dove tail block energy circumference and radial direction slightly movement when stressed, and carries out lamination in this case;
Step 3, after completing lamination, is having precompressed iron core in groove lining bar situation to drawing requirement length, to remove pressure, after penetrating copper bar in a free state, is exerting pressure and pretension tightening bolt to iron core by adjustment dove tail block;
Step 4, rotor is set level, and squeezes into the taper key between dove tail block and punching, symmetrical urgent taper key under each dove tail block of guarantee and punching circular gap deviation are less than 0.15mm situation;
Step 5, by iron core preheating more than 100 DEG C, pretension iron core tightening bolt, taper key between urgent dove tail block and punching ensure gap uniformity again;
Step 6, until iron core cooling after, wheel disk shaft disc and dove tail block are symmetrically welded integral after carry out copper bar and end ring medium frequency welding;
By producing checking, assembly technology core lamination stack of the present invention is convenient, copper bar penetrates easily, iron core coordinates with the enough gross areas of bond energy, both improves production efficiency, and in turn ensure that the total quality of rotor.
Accompanying drawing explanation
Fig. 1 is the schematic diagram after a kind of fanning strip rotor core assembly technology completing steps six of the present invention, in figure: 1. wheel disk shaft; 2. fanning strip; 3. dove tail block; 4. taper key; 5. attachment bolt; 6. copper bar.
Embodiment
A kind of fanning strip rotor core assembly technology of the present invention, comprises the following steps:
Step one, when wheel disk shaft disc connects with dove tail block, after wheel disk shaft disc and dove tail interblock axial length evenly put 0.5mm pad, screws attachment bolt torque spanner with identical power;
Step 2, takes away wheel disk shaft disc and dove tail interblock adjusts pad, ensures dove tail block energy circumference and radial direction slightly movement when being subject to impulsive force, and carries out lamination in this case;
Step 3, after completing lamination, is having precompressed iron core in groove lining bar situation to drawing requirement length, to remove pressure, after penetrating copper bar in a free state, is exerting pressure and pretension tightening bolt to iron core by fine setting dove tail block;
Step 4, rotor is set level, and squeezes into the taper key between dove tail block and punching, symmetrical urgent taper key under each dove tail block of guarantee and punching circular gap deviation are less than 0.15mm situation;
Step 5, by iron core preheating more than 100 DEG C, pretension iron core stretching screw, taper key between urgent dove tail block and punching ensure gap uniformity again;
Step 6, until iron core cooling after, wheel disk shaft disc and dove tail block are symmetrically welded integral after carry out copper bar and end ring medium frequency welding.
Claims (4)
1. a fanning strip rotor core assembly technology, is characterized in that, described assembly method comprises the following steps:
Step one, when wheel disk shaft disc connects with dove tail block, wheel disk shaft disc and dove tail interblock axial length is evenly placed after adjusting pad, is screwed by attachment bolt;
Step 2, takes away wheel disk shaft disc and dove tail interblock adjusts pad, ensures dove tail block energy circumference and radial direction slightly movement when stressed, and carries out lamination in this case;
Step 3, after completing lamination, is having precompressed iron core in groove lining bar situation to drawing requirement length, to remove pressure, after penetrating copper bar in a free state, is exerting pressure and pretension tightening bolt to iron core by adjustment dove tail block;
Step 4, rotor is set level, and squeezes into the taper key between dove tail block and punching, symmetrical urgent taper key under each dove tail block of guarantee and punching circular gap deviation are less than 0.15mm situation;
Step 5, by iron core preheating more than 100 DEG C, pretension iron core tightening bolt, taper key between urgent dove tail block and punching ensure gap uniformity again;
Step 6, until iron core cooling after, wheel disk shaft disc and dove tail block are symmetrically welded integral after carry out copper bar and end ring medium frequency welding.
2. a kind of fanning strip rotor core assembly technology as claimed in claim 1, is characterized in that: perform step and place adjustment pad for the moment, and take away adjustment pad when step 2, ensure that can according to punching inching dove tail block position in lamination process.
3. a kind of fanning strip rotor core assembly technology as claimed in claim 1, is characterized in that: when performing step 4, and dove tail block and punching are relative motions simultaneously, ensure that the cooperation area of key and iron core.
4. a kind of fanning strip rotor core assembly technology as claimed in claim 1, is characterized in that: carry out disc and the block welding of dove tail when performing step 6, ensure that the position of related features of iron core and axle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410378731.XA CN105322732A (en) | 2014-08-04 | 2014-08-04 | Assembly technology of fan-shaped slice rotor core |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410378731.XA CN105322732A (en) | 2014-08-04 | 2014-08-04 | Assembly technology of fan-shaped slice rotor core |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105322732A true CN105322732A (en) | 2016-02-10 |
Family
ID=55249521
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410378731.XA Pending CN105322732A (en) | 2014-08-04 | 2014-08-04 | Assembly technology of fan-shaped slice rotor core |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105322732A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107742959A (en) * | 2017-11-22 | 2018-02-27 | 四川金英科技有限责任公司 | Water sends out machine rotor yoke block more than one piece one hot cover process |
| CN110445271A (en) * | 2019-09-05 | 2019-11-12 | 常州神力电机股份有限公司 | A kind of type fanning strip easy to disassemble of wind power generator rotor |
| CN112187000A (en) * | 2020-09-12 | 2021-01-05 | 中船重工电机科技股份有限公司 | High-power density squirrel-cage generator rotor structure and assembling method thereof |
| CN113541415A (en) * | 2021-09-16 | 2021-10-22 | 江苏博润图制造有限公司 | Generator stator lamination device |
-
2014
- 2014-08-04 CN CN201410378731.XA patent/CN105322732A/en active Pending
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107742959A (en) * | 2017-11-22 | 2018-02-27 | 四川金英科技有限责任公司 | Water sends out machine rotor yoke block more than one piece one hot cover process |
| CN110445271A (en) * | 2019-09-05 | 2019-11-12 | 常州神力电机股份有限公司 | A kind of type fanning strip easy to disassemble of wind power generator rotor |
| CN112187000A (en) * | 2020-09-12 | 2021-01-05 | 中船重工电机科技股份有限公司 | High-power density squirrel-cage generator rotor structure and assembling method thereof |
| CN113541415A (en) * | 2021-09-16 | 2021-10-22 | 江苏博润图制造有限公司 | Generator stator lamination device |
| CN113541415B (en) * | 2021-09-16 | 2021-11-26 | 江苏博润图制造有限公司 | Generator stator lamination device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20160210 |
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| WD01 | Invention patent application deemed withdrawn after publication |