CN107134899B - A method of dovetail groove armature stamping processed - Google Patents

A method of dovetail groove armature stamping processed Download PDF

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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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line
point
armature stamping
dovetail groove
parallel lines
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CN201710343966.9A
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CN107134899A (en
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李玉刚
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Suzhou Branch Of Guizhou Spaceflight Linquan Motor Co ltd
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Suzhou Aerosapce Linquan Motor Co Ltd
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    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K15/00Methods or apparatus specially adapted for manufacturing, assembling, maintaining or repairing of dynamo-electric machines
    • H02K15/02Methods or apparatus specially adapted for manufacturing, assembling, maintaining or repairing of dynamo-electric machines of stator or rotor bodies
    • H02K15/024Methods or apparatus specially adapted for manufacturing, assembling, maintaining or repairing of dynamo-electric machines of stator or rotor bodies with slots
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K2213/00Specific aspects, not otherwise provided for and not covered by codes H02K2201/00 - H02K2211/00
    • H02K2213/03Machines characterised by numerical values, ranges, mathematical expressions or similar information

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  • 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

A method of dovetail groove armature stamping processed
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.
CN201710343966.9A 2017-05-16 2017-05-16 A method of dovetail groove armature stamping processed Active CN107134899B (en)

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CN107134899B true CN107134899B (en) 2019-06-25

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Citations (7)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (7)

* Cited by examiner, † Cited by third party
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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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.