CN204216681U - A kind of aerofoil fan iron core - Google Patents
A kind of aerofoil fan iron core Download PDFInfo
- Publication number
- CN204216681U CN204216681U CN201420724696.8U CN201420724696U CN204216681U CN 204216681 U CN204216681 U CN 204216681U CN 201420724696 U CN201420724696 U CN 201420724696U CN 204216681 U CN204216681 U CN 204216681U
- Authority
- CN
- China
- Prior art keywords
- silicon steel
- steel sheet
- iron core
- aerofoil fan
- hole
- 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.)
- Expired - Fee Related
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Abstract
A kind of aerofoil fan iron core, comprise some silicon steel sheets mutually stacked vertically, described silicon steel sheet circle center is the shaft through-hole of a circle, and each described silicon steel sheet comprises some circumferentially equally distributed magnetic flux holes, adjacent described silicon steel sheet, at axial deflection certain angle, the angle ranging from acute angle; After all described silicon steel sheets are stacked, the described shaft through-hole of all same positions forms the magnetic channel that a sidewall favouring described silicon steel sheet axis has some steps.The utility model magnetic resistance is little, makes motor efficiency high.
Description
Technical field
The utility model relates to a kind of aerofoil fan iron core, belongs to aerofoil fan and manufactures field.
Background technology
Iron core is one of most important parts in fan, and traditional iron core is laminated by a large amount of silicon steel sheet, and the actual magnetic resistance that uses is higher, and efficiency is not high.
Utility model content
The utility model, for solving prior art problem, provides the aerofoil fan iron core that a kind of low magnetic resistance, efficiency are high.
The technical solution of the utility model is: a kind of aerofoil fan iron core, comprise some silicon steel sheets mutually stacked vertically, described silicon steel sheet circle center is the shaft through-hole of a circle, each described silicon steel sheet comprises some circumferentially equally distributed magnetic flux holes, adjacent described silicon steel sheet, at axial deflection certain angle, the angle ranging from acute angle; After all described silicon steel sheets are stacked, the described shaft through-hole of all same positions forms the magnetic channel that a sidewall favouring described silicon steel sheet axis has some steps.
As preferably, each described silicon steel sheet is provided with several Access Division being uniformly distributed in described shaft through-hole outer circumference, and described Access Division comprises the clamping groove that is positioned at described silicon steel sheet front and is positioned at the protruding with the clamping of described clamping fit depressions of the back side.
As preferably, described clamping projection is along the circumferential direction obliquely installed, and the deflection angle between angle of inclination with adjacent described silicon steel sheet is identical.
As preferably, described clamping groove is along the circumferential direction obliquely installed, and incline direction is contrary with the incline direction of described clamping projection and angle is identical.
As preferably, described magnetic flux hole comprises straight sided that described in two edges, silicon steel sheet radial direction is arranged, outside the arc inner edge and the arc relative with described arc inner edge of described shaft through-hole.
As preferably, the angle between two described straight sided is 8 ~ 15 degree.
As preferably, described arc inner edge is the semi arch that a center of circle is positioned at two inner connecting line mid points of described straight sided.
As preferably, be one section of circular arc concentric with described shaft through-hole outside described arc, its two ends terminate in the outer end of two described straight sided.
As preferably, outside described arc, center is provided with the magnetic groove of outwardly convex.
As preferably, the outermost end of described magnetic groove and the edge minimum range of described silicon steel sheet are not more than 1/100 of described silicon steel sheet diameter.
As preferably, described yawing moment is identical with direction of motor rotation.
Compared with stacked with traditional coincidence system, the utility model adopts deflection stacked, the magnetic line of force is made to produce deflection, due in actual motion, in motor winding, electric current can not be parallel to iron mandrel completely and produces deflection to, the magnetic line of force, keeps vertical with electric current, guarantee motor torque is maximum, most effective.
Adjacent silicon steel sheet adopts clamping groove and clamping projection to fix.The Access Division with certain deflection angle makes adjacent silicon steel sheet can keep unified deflection angle at a touch, is convenient to manufacture.
The setting of magnetic groove can guide magnetic line of force trend, reduces magnetic resistance simultaneously, produces magnetic line of force eddy current, promote magnetic field intensity.
In sum, the utility model has the following advantages:
1, magnetic resistance is little, makes motor efficiency high;
2, structure is simple, and improving cost is low.
Accompanying drawing explanation
Fig. 1 is the utility model perspective view;
Fig. 2 is the utility model side-looking structural representation.
In figure, 1, silicon steel sheet, 2, shaft through-hole, 3, magnetic flux hole, 31, straight sided, 32, outside arc, 33, arc inner edge, 34, magnetic groove, 4, Access Division.
Embodiment
With embodiment, the utility model is described in further detail below.
Embodiment one:
A kind of aerofoil fan iron core, comprise some silicon steel sheets 1 mutually stacked vertically, silicon steel sheet 1 circle center is the shaft through-hole 2 of a circle, each silicon steel sheet 1 comprises some circumferentially equally distributed magnetic flux holes 3, adjacent silicon steel sheet 1 is at axial deflection certain angle, yawing moment is identical with direction of motor rotation, and angle is acute angle; After all silicon steel sheets 1 are stacked, the shaft through-hole 2 of all same positions forms the magnetic channel that a sidewall favouring silicon steel sheet 1 axis has some steps.
Each silicon steel sheet 1 is provided with several Access Division 4 being uniformly distributed in shaft through-hole 2 outer circumference, and Access Division 4 comprises the clamping groove that is positioned at silicon steel sheet 1 front and is positioned at the protruding with the clamping of clamping fit depressions of the back side.Clamping projection is along the circumferential direction obliquely installed, and the deflection angle between angle of inclination with adjacent silicon steel sheet 1 is identical; Clamping groove is along the circumferential direction obliquely installed, and incline direction is contrary with the incline direction of clamping projection and angle is identical.
Magnetic flux hole 3 comprises straight sided 31 that two edge silicon steel sheets 1 radial directions arrange, outside the arc inner edge 33 of shaft through-hole 2 and the arc relative with arc inner edge 33 32.Angle between two straight sided 31 is 8 ~ 15 degree, and arc inner edge 33 is the semi arch that a center of circle is positioned at two inner connecting line mid points of straight sided 31, and outside arc, 32 is one section of circular arc concentric with shaft through-hole 2, and its two ends terminate in the outer end of two straight sided 31.Outside arc, 32 centers are provided with the magnetic groove 34 of outwardly convex, and the outermost end of magnetic groove 34 and the edge minimum range of silicon steel sheet 1 are not more than 1/100 of silicon steel sheet 1 diameter.
Claims (8)
1. an aerofoil fan iron core, comprise some silicon steel sheets (1) mutually stacked vertically, described silicon steel sheet (1) circle center is the shaft through-hole (2) of a circle, it is characterized in that: each described silicon steel sheet (1) comprises some circumferentially equally distributed magnetic flux holes (3), described magnetic flux hole (3) comprises outside the straight sided (31) of silicon steel sheet (1) radial direction setting described in two edges, the arc inner edge (33) of close described shaft through-hole (2) and the arc relative with described arc inner edge (33) (32).
2. aerofoil fan iron core according to claim 1, is characterized in that: the angle between two described straight sided (31) is 8 ~ 15 degree.
3. aerofoil fan iron core according to claim 1 or 2, is characterized in that: described arc inner edge (33) is the semi arch that a center of circle is positioned at two inner connecting line mid points of described straight sided (31).
4. aerofoil fan iron core according to claim 3, is characterized in that: outside described arc, (32) are one section of circular arc concentric with described shaft through-hole (2), and its two ends terminate in the outer end of two described straight sided (31).
5. aerofoil fan iron core according to claim 4, is characterized in that: outside described arc, (32) center is provided with the magnetic groove (34) of outwardly convex.
6. aerofoil fan iron core according to claim 5, is characterized in that: the outermost end of described magnetic groove (34) and the edge minimum range of described silicon steel sheet (1) are not more than 1/100 of described silicon steel sheet (1) diameter.
7. aerofoil fan iron core according to claim 1, is characterized in that: adjacent described silicon steel sheet (1), at axial deflection certain angle, the angle ranging from acute angle; After all described silicon steel sheets (1) are stacked, the described shaft through-hole (2) of all same positions forms one and favours the magnetic channel that the axial sidewall of described silicon steel sheet (1) has some steps.
8. aerofoil fan iron core according to claim 7, is characterized in that: described yawing moment is identical with direction of motor rotation.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420724696.8U CN204216681U (en) | 2014-11-28 | 2014-11-28 | A kind of aerofoil fan iron core |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420724696.8U CN204216681U (en) | 2014-11-28 | 2014-11-28 | A kind of aerofoil fan iron core |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204216681U true CN204216681U (en) | 2015-03-18 |
Family
ID=52985316
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420724696.8U Expired - Fee Related CN204216681U (en) | 2014-11-28 | 2014-11-28 | A kind of aerofoil fan iron core |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204216681U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104467211A (en) * | 2014-11-28 | 2015-03-25 | 德清振达电气有限公司 | Axial fan iron core |
-
2014
- 2014-11-28 CN CN201420724696.8U patent/CN204216681U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104467211A (en) * | 2014-11-28 | 2015-03-25 | 德清振达电气有限公司 | Axial fan iron core |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150318 Termination date: 20151128 |