CN107134899B - A method of dovetail groove armature stamping processed - Google Patents
A method of dovetail groove armature stamping processed Download PDFInfo
- Publication number
- CN107134899B CN107134899B CN201710343966.9A CN201710343966A CN107134899B CN 107134899 B CN107134899 B CN 107134899B CN 201710343966 A CN201710343966 A CN 201710343966A CN 107134899 B CN107134899 B CN 107134899B
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- CN
- China
- Prior art keywords
- line
- point
- armature stamping
- dovetail groove
- parallel lines
- 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.)
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Links
- 238000000034 method Methods 0.000 title claims abstract description 20
- 238000004080 punching Methods 0.000 claims description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 abstract description 3
- 229910052802 copper Inorganic materials 0.000 abstract description 3
- 239000010949 copper Substances 0.000 abstract description 3
- 230000007812 deficiency Effects 0.000 abstract description 3
- 238000007796 conventional method Methods 0.000 abstract 1
- 230000004907 flux Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 238000004804 winding Methods 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
- H02K15/02—Methods or apparatus specially adapted for manufacturing, assembling, maintaining or repairing of dynamo-electric machines of stator or rotor bodies
- H02K15/024—Methods or apparatus specially adapted for manufacturing, assembling, maintaining or repairing of dynamo-electric machines of stator or rotor bodies with slots
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K2213/00—Specific aspects, not otherwise provided for and not covered by codes H02K2201/00 - H02K2211/00
- H02K2213/03—Machines characterised by numerical values, ranges, mathematical expressions or similar information
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Power Engineering (AREA)
- Manufacture Of Motors, Generators (AREA)
Abstract
The invention discloses a kind of new methods for making ideal dovetail groove armature stamping, by finding intersection dovetail groove armature stamping method processed as parallel lines to improve the deficiency of conventional method, motor copper factor and thermic load can be reduced, the motor lead time is shortened, improves motor operation efficiency.
Description
Technical field
The present invention relates to find intersection dovetail groove armature stamping method processed as parallel lines, specially a kind of dovetail groove armature processed is rushed
The method of piece.
Background technique
The design of traditional dovetail groove armature stamping is utilized based on the ideal groove parameters of ansoft simulation software gained
It draws circle and finds intersection legal system dovetail groove armature stamping;Make circle using tradition and finds intersection the made armature stamping dovetail groove parameter of method and ideal
Dovetail groove parameter has differences, if will increase armature copper factor with such dovetail groove armature stamping, reduces wire winding
Property, the delay product production cycle, increase motor thermic load and armature teeth portion flux density, reduces Rated motor point load efficiency.
Summary of the invention
It is all because of the made dovetail groove parameter of Traditional Method that present invention consideration tradition work circle, which finds intersection and makes the deficiency of trapezoidal channel process,
It is not consistent with ideal dovetail groove parameter, therefore proposes to find intersection the ideal dovetail groove armature stamping method of system as parallel lines, with such side
The made dovetail groove parameter of method is consistent completely with ideal dovetail groove parameter.
The technical scheme is that a kind of method of dovetail groove armature stamping processed, includes the following steps:
Step 1. enables circular diameter in armature stamping based on the final ideal dovetail groove parameter of Ansoft calculating gained respectively
For φ a, outside diameter is φ b, and is justified respectively with φ a, φ b work, remakes center line A, B right-angled intersection in point O;
A center line is replicated 10 ° of rotation using O as basic point by step 2. clockwise, obtains C line, hands over the circle of φ a in point u;With
Bs0/2 is that width makees C line parallel lines D, hands over φ a circle in v point;Make A line parallel lines E and F respectively with Bs1/2 and Bs2/2;And it puts down
Line E, F are located at the same side of A line, and D line is between A line and E line, and F line is between E line and C line;
Step 3. is line segment vm=Hs0 along D line using v point as starting point, and m point is on the outside of φ a circle, then by point m to make B line parallel
Line G;Make G line parallel lines J, K, L by spacing of Hs0+Hs1, Hs0+Hs1+Hs2 and Hs0+Hs1+Hs2+Rs respectively along D line, wherein
J line hands over E line in n point, and K line hands over F line in x point, and L line hands over A line respectively at y point;Be sequentially distributed from lower to upper above B line G line, J line,
K line and L line;
Step 4. makees the chamfering of L line Yu F line, and connecting line segment mn, nx with Rs;Retain camber line uv, punching outer circle φ b, in
Heart line A, B and vmnxy line, deletes remaining line;
Step 5. is using A line as center line, to vmnxy line mirror image, then using O as basic point, carries out to vmnxy line and its image line
Array finally obtains and ideal dovetail groove parameter;Wherein:
Bs1 is the slot wedge maximum width of armature stamping;
Bs2 is the groove body bottom width of armature stamping;
Hs0 is the channel opening height of armature stamping;
Hs1 is the slot wedge height of armature stamping;
Hs2 is the groove body height of armature stamping;
Rs is the groove body bottom chamfer of armature stamping.
The invention has the advantages that the present invention will be to find intersection dovetail groove armature stamping method substitution tradition system ladder processed as parallel lines
Shape slot armature stamping method can reduce motor copper factor and thermic load, shorten the motor lead time, and improve motor operation effect
Rate.
Detailed description of the invention
The invention will be further described with reference to the accompanying drawings and embodiments:
Fig. 1 is to calculate resulting final ideal dovetail groove parameter described in step 1 with Ansoft;
Fig. 2 is the result figure of step 1;
Fig. 3 is the result figure of step 2 and step 3;
Fig. 4 is the result figure of step 4;
Fig. 5 is the result figure of step 5.
Specific embodiment
Embodiment: by taking certain model unmanned plane rudder motor as an example, in conjunction with shown in FIG. 1 to FIG. 5, elaborate that tradition is made to justify
The shortcomings that selecting dovetail groove armature stamping method processed and deficiency are asked, and is elaborated to find intersection dovetail groove armature stamping method processed as parallel lines
Employ all means available;A method of dovetail groove armature stamping processed includes the following steps:
Step 1. enables circular diameter in armature stamping based on the final ideal dovetail groove parameter of Ansoft calculating gained respectively
For φ a, outside diameter is φ b, and is justified respectively with φ a, φ b work, remakes center line A, B right-angled intersection in point O;
A center line is replicated 10 ° of rotation using O as basic point by step 2. clockwise, obtains C line, hands over the circle of φ a in point u;With
Bs0/2 is that width makees C line parallel lines D, hands over φ a circle in v point;Make A line parallel lines E and F respectively with Bs1/2 and Bs2/2;And it puts down
Line E, F are located at the same side of A line, and D line is between A line and E line, and F line is between E line and C line;
Step 3. is line segment vm=Hs0 along D line using v point as starting point, and m point is on the outside of φ a circle, then by point m to make B line parallel
Line G;Make G line parallel lines J, K, L by spacing of Hs0+Hs1, Hs0+Hs1+Hs2 and Hs0+Hs1+Hs2+Rs respectively along D line, wherein
J line hands over E line in n point, and K line hands over F line in x point, and L line hands over A line respectively at y point;Be sequentially distributed from lower to upper above B line G line, J line,
K line and L line;
Step 4. makees the chamfering of L line Yu F line, and connecting line segment mn, nx with Rs;Retain camber line uv, punching outer circle φ b, in
Heart line A, B and vmnxy line, deletes remaining line;
Step 5. is using A line as center line, to vmnxy line mirror image, then using O as basic point, carries out to vmnxy line and its image line
Array finally obtains and ideal dovetail groove parameter;Wherein:
Bs1 is the slot wedge maximum width of armature stamping;
Bs2 is the groove body bottom width of armature stamping;
Hs0 is the channel opening height of armature stamping;
Hs1 is the slot wedge height of armature stamping;
Hs2 is the groove body height of armature stamping;
Rs is the groove body bottom chamfer of armature stamping.
Certainly the above embodiments merely illustrate the technical concept and features of the present invention, and its object is to allow be familiar with technique
People can understand the content of the present invention and implement it accordingly, it is not intended to limit the scope of the present invention.It is all according to this hair
The modification that the Spirit Essence of bright main technical schemes is done, should be covered by the protection scope of the present invention.
Claims (1)
1. a kind of method of dovetail groove armature stamping processed, characterized by the following steps:
For step 1. based on the final ideal dovetail groove parameter of Ansoft calculating gained, enabling circular diameter in armature stamping respectively is φ
A, outside diameter are φ b, and are justified respectively with φ a, φ b work, remake center line A, B right-angled intersection in point O;
A center line is replicated 10 ° of rotation using O as basic point by step 2. clockwise, obtains C line, hands over the circle of φ a in point u;It is flat to make A line
Line D hands over φ a circle in v point, and width is Bs0/2 between A, D;Make A line parallel lines E and F simultaneously, and width is Bs1/ between A, E
Width is Bs2/2 between 2, A, F;And parallel lines E, F are located at the same side of A line, and between A line and E line, F line is located at D line
Between E line and C line;
Step 3. is line segment vm=Hs0 along D line using v point as starting point, and m point makees B line parallel lines G on the outside of φ a circle, then through point m;
Make G line parallel lines J, K, L by spacing of Hs0+Hs1, Hs0+Hs1+Hs2 and Hs0+Hs1+Hs2+Rs respectively along D line, wherein J line
Hand over E line in n point, K line hands over F line in x point, and L line hands over A line respectively at y point;It is sequentially distributed G line, J line, K line from lower to upper above B line
With L line;
Step 4. makees the chamfering of L line Yu F line, and connecting line segment mn, nx with Rs;Retain camber line uv, punching outer circle φ b, center line
A, B and vmnxy line deletes remaining line;
Step 5. is using A line as center line, to vmnxy line mirror image, then using O as basic point, carries out battle array to vmnxy line and its image line
Column finally obtain and ideal dovetail groove parameter;Wherein:
Bs1 is the slot wedge maximum width of armature stamping;
Bs2 is the groove body bottom width of armature stamping;
Hs0 is the channel opening height of armature stamping;
Hs1 is the slot wedge height of armature stamping;
Hs2 is the groove body height of armature stamping;
Rs is the groove body bottom chamfer of armature stamping.
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CN201710343966.9A CN107134899B (en) | 2017-05-16 | 2017-05-16 | A method of dovetail groove armature stamping processed |
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CN201710343966.9A CN107134899B (en) | 2017-05-16 | 2017-05-16 | A method of dovetail groove armature stamping processed |
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CN107134899B true CN107134899B (en) | 2019-06-25 |
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Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS61135343A (en) * | 1984-12-03 | 1986-06-23 | Ebara Corp | Wedge for submersible motor |
CN201163729Y (en) * | 2008-03-11 | 2008-12-10 | 麦德添 | Stator lamination of industrial sewing machine enamel-insulated aluminum wire electric motor |
CN201378758Y (en) * | 2008-11-14 | 2010-01-06 | 中山大洋电机股份有限公司 | Structure of motor stator iron core punching plate |
CN201518433U (en) * | 2009-07-16 | 2010-06-30 | 湖州南洋电机有限公司 | Big and small slot motor stator |
CN102222989A (en) * | 2011-06-17 | 2011-10-19 | 大连鹏迪电动车辆有限公司 | Motor iron core and method for processing silicon steel sheet forming iron core |
CN102332760A (en) * | 2011-09-09 | 2012-01-25 | 山东大学威海分校 | Stator core and processing method thereof |
CN104467227A (en) * | 2014-12-09 | 2015-03-25 | 江苏爱尔玛科技有限公司 | Rotor slot of high-efficiency permanent-magnet synchronous motor and rotor sheet with same |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7692350B2 (en) * | 2007-02-28 | 2010-04-06 | Emerson Electric Co. | Horizontal axis washing machine having 4 pole 36 slot motor |
-
2017
- 2017-05-16 CN CN201710343966.9A patent/CN107134899B/en active Active
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS61135343A (en) * | 1984-12-03 | 1986-06-23 | Ebara Corp | Wedge for submersible motor |
CN201163729Y (en) * | 2008-03-11 | 2008-12-10 | 麦德添 | Stator lamination of industrial sewing machine enamel-insulated aluminum wire electric motor |
CN201378758Y (en) * | 2008-11-14 | 2010-01-06 | 中山大洋电机股份有限公司 | Structure of motor stator iron core punching plate |
CN201518433U (en) * | 2009-07-16 | 2010-06-30 | 湖州南洋电机有限公司 | Big and small slot motor stator |
CN102222989A (en) * | 2011-06-17 | 2011-10-19 | 大连鹏迪电动车辆有限公司 | Motor iron core and method for processing silicon steel sheet forming iron core |
CN102332760A (en) * | 2011-09-09 | 2012-01-25 | 山东大学威海分校 | Stator core and processing method thereof |
CN104467227A (en) * | 2014-12-09 | 2015-03-25 | 江苏爱尔玛科技有限公司 | Rotor slot of high-efficiency permanent-magnet synchronous motor and rotor sheet with same |
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CN107134899A (en) | 2017-09-05 |
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Effective date of registration: 20240112 Address after: No. 268 Songshan Road, High tech Zone, Suzhou City, Jiangsu Province, China Patentee after: SUZHOU BRANCH OF GUIZHOU SPACEFLIGHT LINQUAN MOTOR Co.,Ltd. Address before: 215000 No.268 Songshan Road, high tech Zone, Suzhou City, Jiangsu Province Patentee before: SUZHOU AEROSAPCE LINQUAN MOTOR Co.,Ltd. |