Axial flux switched reluctance motor and generator, and related systems and methods
US-12149134-B2 · Nov 19, 2024 · US
US10367382B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10367382-B2 |
| Application number | US-201515502233-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 17, 2015 |
| Priority date | Aug 7, 2014 |
| Publication date | Jul 30, 2019 |
| Grant date | Jul 30, 2019 |
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A laminated core can be contained in a rotor and/or in a stator and include at least one first sheet metal part assembly and at least one second sheet metal part assembly. The two sheet metal part assemblies are arranged alternately lying one against the other in a stacking direction. Every first sheet metal part has first teeth projecting from a connecting part radially relative to the axis of rotation. Correspondingly, every second sheet metal part has second teeth projecting from a second connecting part. The first teeth extend from the axis of rotation at a distance different from how far the second teeth extends from the axis of rotation to form a step to mesh the rotor with an associated stator and increase the air gap between them without increasing dimensions of the laminated cores in the stacking direction.
Opening claim text (preview).
The invention claimed is: 1. A laminated core ( 14 ) of a stator ( 15 ) or a rotor ( 11 ), the laminated core comprising: first sheet metal parts ( 10 ) which each have a first connecting part ( 18 ) and a plurality of first teeth ( 19 ), wherein each first tooth ( 19 ) extends from the first connecting part ( 18 ) to a free end ( 20 ), and wherein the free ends ( 20 ) of the first teeth ( 19 ) individually define a first distance (R 1 ) from a reference axis (BA) or a reference plane (BE) of the laminated core ( 14 ), second sheet metal parts ( 13 ) which each have a second connecting part ( 25 ) and a plurality of second teeth ( 26 ), wherein each second tooth ( 26 ) extends from the second connecting part ( 25 ) to a free end ( 27 ), and wherein the free ends ( 27 ) of the second teeth ( 26 ) individually define a second distance (R 2 ) from the reference axis (BA) or the reference plane (BE), at least one first sheet metal part assembly ( 35 ) comprising at least one of the first sheet metal parts ( 10 ), at least one second sheet metal part assembly ( 36 ) comprising at least one of the second sheet metal parts ( 13 ), and wherein the at least one first sheet metal part assembly ( 35 ) and the at least one second sheet metal part assembly ( 36 ) are arranged alternately in a stacking direction (A) wherein at least some of the first sheet metal parts ( 10 a ) have a first thickness (d 1 ), and the second sheet metal parts ( 13 ) have a second thickness (d 2 ); wherein the first sheet metal part assembly ( 35 ) comprises a plurality of the first sheet metal parts ( 10 ), wherein two of the first sheet metal parts ( 10 ) form outer sheet metal parts ( 10 a ) and at least one further of the first sheet metal parts ( 10 ) forms an inner sheet metal part ( 10 i ) arranged between the two outer sheet metal parts ( 10 a ), the at least one inner sheet metal part ( 10 i ) has a first thickness (d 1 ), and at least one of the two outer sheet metal parts ( 10 a ) has a third thickness (d 3 ), which is greater than the first thickness (d 1 ). 2. The laminated core according to claim 1 , further comprising a plurality of first sheet metal part assemblies ( 35 ) and/or a plurality of second sheet metal part assemblies ( 36 ). 3. The laminated core according to claim 1 , wherein each first sheet metal part assembly ( 35 ) comprises a plurality of first sheet metal parts ( 10 ), and/or each second sheet metal part assembly ( 36 ) comprises a plurality of second sheet metal parts ( 13 ). 4. The laminated core according to claim 1 , wherein the first thickness (d 1 ) and the second thickness (d 2 ) are a same size. 5. The laminated core according to claim 1 , wherein some of the first sheet metal parts ( 10 ) have a third thickness (d 3 ), which is greater than the first thickness (d 1 ). 6. The laminated core according to claim 1 , further comprising at least two first sheet metal part assemblies and wherein a free space (F) is formed between two consecutive ones of the at least two first sheet metal part assemblies ( 35 ) in the stacking direction (A). 7. The laminated core according to claim 1 , wherein the first connecting parts ( 18 ) and the second connecting parts ( 25 ) are closed annularly around the reference axis (BA) and the first teeth ( 19 ) and the second teeth ( 26 ) extend radially relative to the reference axis (BA). 8. The laminated core according to claim 7 , wherein the first distance (R 1 ) is greater than the second distance (R 2 ), and the first teeth ( 19 ) and the second teeth ( 26 ) extend radially outwardly from an axis of rotation (M) from the first connecting part ( 18 ) and the second connecting part ( 25 ), respectively. 9. The laminated core according to claim 7 , wherein the first distance (R 1 ) is smaller than the second distance (R 2 ), and the first teeth ( 19 ) and the second teeth ( 26 ) extend radially inwardly relative to an axis of rotation (M) from the first connecting part ( 18 ) and the second connecting part ( 25 ), respectively. 10. The laminated core according to claim 1 , wherein the first and second connecting parts ( 18 , 25 ) extend in a straight line or in a curved manner along a path of movement of the rotor ( 11 ) and the first and second teeth ( 19 , 26 ) extend at a right angle relative to the reference plane (BE) from the first and second connecting parts ( 18 , 25 ), respectively. 11. The laminated core according to claim 1 , wherein the first sheet metal part assembly ( 35 ) and/or the second sheet metal part assembly ( 36 ) comprises at least one sheet metal part ( 10 or 13 ) made of one material and at least one other sheet metal part ( 10 of 13 ) made of another material. 12. The laminated core according to claim 1 , wherein the at least one inner sheet metal part ( 10 i ) is made of one material and at least one of the two outer sheet metal parts ( 10 a ) is made another material. 13. An electrical machine ( 12 ) comprising a rotor ( 11 ) and a stator ( 15 ), wherein the rotor ( 11 ) and/or the stator ( 15 ) comprises a laminated core ( 14 ) according to claim 1 . 14. The electrical machine according to claim 13 , wherein the first teeth ( 19 ) of a first sheet metal part assembly ( 35 ) of the rotor ( 11 ) protrude into a free space (F) between two first sheet metal part assemblies ( 35 ) of the stator ( 15 ), and/or the first teeth ( 19 ) of a first sheet metal part assembly ( 35 ) of the stator ( 15 ) protrude into a free space (F) between two first sheet metal part assemblies ( 35 ) of the rotor ( 11 ). 15. The electrical machine according to claim 13 , wherein a first sheet metal part assembly ( 35 ) of the stator ( 15 ), at a right angle relative to the reference axis (BA) or the reference plane (BE), faces a second sheet metal part assembly ( 36 ) of the rotor ( 11 ), and/or a first sheet metal part assembly ( 35 ) of the rotor ( 11 ), at a right angle relative to the reference axis (BA) or the reference plane (BE), faces a second sheet metal part assembly ( 36 ) of the stator ( 15 ). 16. The laminated core according to claim 1 , wherein the at least one of the two outer sheet metal parts ( 10 a ) comprises at least two first sheet metal parts that are stacked together and are not electrically insulated with respect to one another. 17. A laminated core ( 14 ) of a stator ( 15 ) or a rotor ( 11 ), the laminated core comprising: first sheet metal parts ( 10 ) which each have a first connecting part ( 18 ) and a plurality of first teeth ( 19 ), wherein each first tooth ( 19 ) extends from the first connecting part ( 18 ) to a free end ( 20 ), and wherein the free ends ( 20 ) of the first teeth ( 19 ) individually define a first distance (R 1 ) from a reference axis (BA) or a reference plane (BE) of the laminated core ( 14 ), second sheet metal parts ( 13 ) which each have a second connecting part ( 25 ) and a plurality of second teeth ( 26 ), wherein each second tooth ( 26 ) extends from the second connecting part ( 25 ) to a free end ( 27 ), and wherein the free ends ( 27 ) of the second teeth ( 26 ) individually define a second distance (R 2 ) from the reference axis (BA) or the reference plane (BE), at least one first sheet metal part assembly ( 35 ) comprising at least one of the first sheet metal parts ( 10 ), at least one second sheet metal part assembly ( 36 ) comprising at least one of the second sheet metal parts ( 13 ), and wherein the at least one first sheet metal part assembly ( 35 ) and the at least one second sheet metal part assembly ( 36 ) are arranged alternately in a stackin
Shape, form or location of the slots · CPC title
Machines characterised by aspects of the air-gap between rotor and stator · CPC title
Stator cores with salient poles · CPC title
Rotor cores with salient poles {; Variable reluctance rotors} · CPC title
Machines characterised by numerical values, ranges, mathematical expressions or similar information · CPC title
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