Laminated core for a magnetic bearing having individual laminations with at least one physical interruption and method for constructing such a laminated core

Abstract

The core inside a combined radial-axial magnetic bearing is stacked with coated laminations each equipped with at least one radial cut. These cuts prevent the inducement of circulating currents caused by varying axial control fluxes through the central hole of the stack. Magnetic symmetry is preserved by pivoting every lamination with respect to the previous one over a particular angle. This arrangement not only reduces the losses in the bearing, but improves the performance of the axial channel as well.

Claims

1. A laminated core of a stator or a rotor of a permanent magnet biased or current biased combined radial-axial magnetic bearing, comprising: a solid stack of flat soft-magnetic individual laminations; each of said individual laminations comprising a substantially circular structure and at least one physical interruption in the substantially circular structure, wherein said at least one physical interruption physically interrupts circulating currents in the plane of the individual lamination; wherein said solid stack of flat-soft-magnetic individual laminations forms a cylindrical structure, wherein said cylindrical structure is configured in a way so as to create magnetic symmetry in the solid stack; said at least one physical interruption being filled with an electrically insulating material; and said at least one physical interruption in adjacent laminations being rotated with respect to each other in a way such that the at least one physical interruption of each individual lamination is evenly distributed over a circumference of the solid stack.

2. The laminated core of claim 1, wherein a circulating eddy current due to a varying control flux cannot develop.

3. The laminated core according to claim 1, wherein none of said individual laminations are in electric contact with each other.

4. The laminated core according to claim 1, wherein said at least one physical interruption is straight and radially-oriented.

5. The laminated core according to claim 1, wherein said at least one physical interruption is straight and not radially-oriented.

6. The laminated core according to claim 1, wherein said at least one physical interruption is shaped in the form of a dovetail-connection.

7. The laminated core according to claim 1, wherein a cross section of said solid stack reveals no magnetic poles.

8. The laminated core according to claim 1, wherein a cross section of said solid stack reveals more than one lamination.

9. The laminated core according to claim 1, wherein said at least one physical interruption is provided on a symmetry axis of the individual lamination.

10. The laminated core according to claim 1, wherein said at least one physical interruption is provided in a way such that said at least one physical interruption does not coincide with a symmetry axis of the individual lamination.

11. A method for constructing a laminated core for a stator or a rotor of a combined radial-axial magnetic bearing, comprising the steps: providing a set of flat soft-magnetic laminations, wherein each of said laminations comprises a substantially circular structure; arranging a first soft-magnetic layer in such a way that at least one physical interruption for induced circulating currents is obtained, wherein said at least one physical interruption in provided in the substantially circular structure of each lamination; rotating all subsequent soft-magnetic layers with respect to their previous soft magnetic layers so that said at least one physical interruption in adjacent laminations is rotated with respect to each other in a way such that the at least one physical interruption of each individual lamination is evenly distributed over a circumference of the set of flat soft-magnetic laminations to create magnetic symmetry in the set of flat soft-magnetic laminations; and solidifying the resulting set of soft-magnetic layers.

12. The method according to claim 11, wherein an electrically insulating material is provided inside said at least one physical interruption.

13. A method for constructing a laminated core for a stator or a rotor of a combined radial-axial magnetic bearing, comprising the steps: providing a set of flat soft-magnetic laminations, wherein each of said flat soft-magnetic laminations comprises a substantially circular structure having at least one physical interruption in the substantially circular structure; assembling a first substack by arranging a first plurality of soft-magnetic layers in such a way that said at least one physical interruption for induced circulating currents is obtained per lamination layer, and in such a way that said at least one physical interruption in all adjacent lamination layers coincide; assembling subsequent substacks by arranging subsequent pluralities of soft-magnetic layers in the same way as the first substack with the first plurality of soft-magnetic layers, but in such a way that all subsequent substacks with their pluralities of soft-magnetic layers and said at least one physical interruption are rotated with respect to their previous substack with a plurality of soft-magnetic layers in a way such that the at least one physical interruption of each substack is evenly distributed over a circumference of the set of flat soft-magnetic laminations to create magnetic symmetry in the set of flat soft-magnetic laminations; and solidifying the resulting set of soft-magnetic layers.

14. The method according to claim 13, including providing an electrically insulating material inside said at least one physical interruption.

15. The method according to claim 13, further comprising assembling the set of flat soft-magnetic laminations as the stator or the rotor of the combined radial-axial magnetic bearing.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) With the intention of better showing the characteristics of the invention, hereafter, by way of example without being limitative in any way, a description is given of some preferred embodiments of a laminated core for a stator or a rotor of a combined radial-axial magnetic bearing according to the invention, reference being made to the accompanying drawings, wherein:

(2) FIG. 1 represents a half longitudinal cross section of a first combo bearing type with permanent magnet bias, according to prior art;

(3) FIG. 2 represents a longitudinal cross section of a second combo bearing type with permanent magnet bias, according to prior art;

(4) FIG. 3 represents a longitudinal cross section of a third combo bearing type with current bias, according to prior art;

(5) FIG. 4 represents a cross section of the four-pole radial actuator part of a first combo bearing type, according to prior art;

(6) FIG. 5 represents a cross section of the three-pole radial actuator part of a second combo bearing type, according to prior art;

(7) FIG. 6 represents a cross section of a 360.sub.< lamination of a four-pole radial actuator part of a combo bearing, split on a symmetry axis;

(8) FIG. 7 represents all possible positions to which the lamination of FIG. 6 can be pivoted, with preservation of the position of the poles;

(9) FIG. 8 represents the distribution of magnetic field lines in the vicinity of a split having tangential dimension 0.5 mm, for a stack being composed of four double-sided 10 m coated lamination sheets of thickness 0.35 mm;

(10) FIG. 9 represents the distribution of the magnetic flux density in the vicinity of a split having tangential dimension 0.5 mm, for a stack being composed of four double-sided 10 m coated lamination sheets of thickness 0.35 mm;

(11) FIG. 10 represents a cross section of a 360.sub.< lamination of a four-pole radial actuator part of a combo bearing, not split on a symmetry axis;

(12) FIG. 11 represents all possible positions to which the lamination of FIG. 10 can be rotated (pivoted and/or flipped), with preservation of the position of the poles;

(13) FIG. 12 represents a cross section of a 360.sub.< lamination of a three-pole radial actuator part of a combo bearing, split on a symmetry axis;

(14) FIG. 13 represents all possible positions to which the lamination of FIG. 12 can be rotated, with preservation of the position of the poles;

(15) FIG. 14 represents a cross section of a 360.sub.< lamination of a three-pole radial actuator part of a combo bearing, not split on a symmetry axis;

(16) FIG. 15 represents all possible positions to which the lamination of FIG. 14 can be rotated (pivoted and/or flipped), with preservation of the position of the poles;

(17) FIG. 16 represents a cross section of a 180.sub.< lamination segment of a four-pole radial actuator part of a combo bearing;

(18) FIG. 17 represents all possible positions to which the lamination segment of FIG. 16 can be rotated (pivoted and/or flipped), with preservation of the position of the poles;

(19) FIG. 18 represents a cross section of a 120.sub.< lamination segment of a three-pole radial actuator part of a combo bearing;

(20) FIG. 19 represents all possible positions to which the lamination segment of FIG. 18 can be rotated (pivoted and/or flipped), with preservation of the position of the poles;

(21) FIG. 20 represents a cross section of a splitted 360.sub.< lamination for an actuator target stack;

(22) FIG. 21 represents a cross section of a 360.sub.< lamination with a non-straight cut and an insulating spacer.

DETAILED DESCRIPTION OF THE DRAWINGS

(23) Some longitudinal cross sections of existing combo bearing types are shown in FIGS. 1, 2 and 3. Two possible radial cross sections of existing combo bearing types are shown in FIGS. 4 and 5. The alternative designs depicted, are all composed of a laminated rotor stack 1 with a geometric rotation axis X-X, a laminated stator stack 2, a stator yoke 3, two axial poles 4a and 4b and at least three radial poles 5. Axial forces are controlled by an axial control coil 6, whose construction is rotationally symmetric. Radial forces are controlled by radial control coils 7. They are wound around the radial poles 5. If the bias field is not generated by permanent magnets 8, it may be generated by adding a bias current in some particular way to the axial control current or by supplying a bias current to a separate bias coil, having a rotationally symmetric shape as well and being located close to the axial control coil 6.

(24) If a current is supplied to a radial control coil 7, flux starts flowing in the plane of the laminations of the stator stack 2. The flux generated by a current supplied to the axial control coil 6 flows through the stator yoke 3, subsequently passes into an axial pole 4a, crosses the gap towards the rotor stack 1, crosses the gap towards the opposite axial pole 4b and eventually returns into the stator yoke 3. Consequently, since the axial control current varies in time, a time-varying flux crosses the central hole of the stator stack 2. According to Faraday-Lenz' and Ohm's laws, circular currents are induced in the laminations of the stator stack 2. Therefore, it is the object of the present invention to physically interrupt the path for these induced circulating currents.

(25) One possibility to realize this physical interruption is providing a single cut 9 in each 360.sub.< lamination 10 of the stator stack 2, as shown in FIG. 6 for the case of a four-pole stator stack 2. The notation 360.sub.< indicates that the lamination covers an angle just under 360, because of the present cut 9. Obviously, such a cut 9 introduces a considerable tangential reluctance in practice, as cutting widths below 0.25 mm are difficult to obtain. Therefore, the lamination 10 looses part of its magnetic symmetry for the radial control field. A hypothetical stator stack having only one single lamination 10 would exhibit significant radial channel performance loss due the cut. However, the stacking of laminations 10 provides a way of avoiding this performance loss.

(26) FIG. 7 shows all possible positions to which the 360.sub.< lamination 10 with a single cut 9 of FIG. 6 can be pivoted, without having an effect on the position of the four poles 5. Hence, if the stator is stacked in such a way that the cuts 9 of adjacent 360.sub.< laminations 10 are always separated from each other, a magnetic field line can cross a cut by changing from 360.sub.< lamination 10. It thereby needs to traverse twice through the coatings of adjacent laminations 10. The key issue here is that lamination coatings can be made much thinner than the width of a cut, e.g. 1 m compared to at least 250 m.

(27) FIG. 8 shows a cross-section of a stator stack 2, composed out of four laminations 10. The figure is a cross-section orthogonal to the plane of the laminations 10, tangential with respect to the center of the stack, made on the position of a cut 9 in one of the laminations 10. The distribution of the magnetic field lines of the radial control fields in the vicinity of the cut 9 is shown in FIG. 8. In this particular example, the laminations 10 have a thickness of 0.35 mm; the width B of the cut 9 is 0.5 mm; the thickness D of the coating is 10 m, implying 20 m in between the soft-magnetic parts (double-sided coating). When approaching the cut 9, the field lines split up in two halves. Inside the cut 9 there are hardly any field lines. Once beyond the cut 9, the field lines come back together in the original lamination 10.

(28) Obviously, this influences the local magnetic flux density in the vicinity of the cut 9, as shown in FIG. 9 for an identical stator stack 2 as the one depicted in FIG. 8. Inside the cut 9, there are hardly any magnetic field lines, causing the flux density to be almost zero there. This is expressed by the dark blue (DB) shading in FIG. 9. When leaving the area of the cut along the plane of the lamination, the flux density gradually increases up to its nominal value, as expressed by the color change from dark blue (DB) via lighter blue (LB) and cyan (CN) and further from green (GR) to yellow (GL). In adjacent laminations, the flux density increases when approaching the cut, as expressed by the color change from yellow (GL) via orange (OR) to red (RD).

(29) In this particular example, in which the coating is fairly thick, the flux density is predominantly affected in the adjacent laminations 10 only. The other laminations are only slightly affected. In theory, the flux density in a lamination may locally increase up to 1.5 times its normal value. However, the thinner the coatings are, the more spreading of the field lines may be expected, causing further reduction of the local peak flux density.

(30) From FIGS. 8 and 9, it may also be concluded that the size of the region in which the flux density is influenced by the cut 9 is not bigger than a few millimeters. Consequently, when large radial control currents are to be supplied, there may be some local saturation, but its impact on the global performance of the bearing will remain small.

(31) In order to globally restore the original magnetic symmetry, it is advised to evenly distribute the cuts 9 over the circumference of the stator stack 2. Given the alternative positions of the 360.sub.< laminations 10 in FIG. 7, it is e.g. possible to create a stator stack 2 with a repetitive pattern of four 360.sub.< laminations. The shortest axial distance between cuts 9 then equals about 4 times the thickness of the laminations 10.

(32) The 360.sub.< lamination 10 depicted in FIG. 6 is provided with a cut 9 that coincides with a symmetry axis. However, this is not imperative. On the contrary, a cut non-coinciding with the symmetry axis can be considered to further increase the minimal axial distance between the cuts 9. For example, the 360.sub.< lamination 10 depicted in FIG. 10, having four poles 5, is equipped with a cut 9 that does not coincide with a symmetry axis. By pivoting and/or flipping this lamination 10, eight different positions can be found in which the position of the poles 5 is preserved, as demonstrated by FIG. 11. Stacking those yields a magnetically symmetric stator stack 2 with a repetitive pattern of eight laminations 10 and the shortest axial distance between the cuts is eight laminations 10 as well.

(33) FIG. 12 shows a 360.sub.< lamination 10 with only three poles 5, where a single cut 9 is provided on a symmetry axis. FIG. 13 shows that pivoting the lamination 10 of FIG. 12 only yields three different positions in which the position of the poles 5 is preserved. After stacking those in such a way that the entire stack is magnetically symmetric, the minimal axial distance between the cuts 9 equals three laminations 10. In this particular configuration, the magnetic field lines can only spread out over a distance of one lamination 10, thus the flux density increase nearby the cut 9 is likely to be close to 50%.

(34) In order to increase the minimal axial distance between cuts 9 in the case of a stator stack 2 having three poles 5, it is required to make a cut 9 which does not coincide with a symmetry axis, as shown in FIG. 14. In that case, rotating (pivoting and/or flipping) the lamination 10 of FIG. 14 yields six alternative positions for the cut 9, with preservations of the position of the poles 5, as depicted in FIG. 15. The shortest axial distance between cuts 9 then equals about six times the thickness of the laminations 10.

(35) Until now, only examples with a single cut 9 were given. However, this is not a restriction. For example, a stator stack 2 with four poles 5 can be constructed using 180.sub.< laminations 11 as the ones shown in FIG. 16. When properly arranged, two such 180.sub.< laminations 11 form a composed lamination construction 13 having an equivalent of two cuts 9. By rotating (pivoting and/or flipping) the 180.sub.< lamination 11 of FIG. 16, four arrangements can be found for which the cuts 9 are in different positions, with preservation of the position of the poles 5, as shown in FIG. 17. Stacking these yields a stator stack 2 with a repetitive axial pattern of four 180.sub.< laminations 11 and a minimal axial distance between the cuts 9 of four 180.sub.< laminations 11 as well. One reason to choose for such an arrangement with 180.sub.< laminations 11 instead of 360.sub.< laminations 10 with a single cut 9 is the potential waste reduction with, for instance, punching.

(36) It is remarked that the composed lamination construction 13 in FIG. 17 has two cuts that do not coincide with a symmetry axis. If they would have coincided, only two alternative arrangements could have been found. This is less attractive since it implies a doubling of the flux density nearby the cuts 9. A similar situation occurs with 120.sub.< laminations 12 for a design with three poles 5 and three cuts 9, as the one shown in FIG. 18. In this case, only two possible arrangements can be found, provided the three cuts 9 do not coincide with a symmetry axis, as demonstrated by FIG. 19. A symmetric 120.sub.< lamination 12 cannot be used here, since all cuts would coincide.

(37) The previous discussion focused on some alternatives for three and four pole designs. However, without any loss of generality, the same ideas can be extended to designs with larger number of poles 5 or even to designs without any poles 5. An example of a lamination 10 without poles 5 is given in FIG. 20. Such a design could be used e.g. to assemble the actuator target stack 1 on the rotating part.

(38) The inclusion of a single cut 9 in a 360.sub.< lamination 10 dramatically reduces its mechanical stiffness. However, when stacking them according to the principles of this invention, the stiffness and mechanical integrity of the resulting stack is hardly reduced when compared to the case without cuts 9. If 180.sub.< laminations 11 or 120< laminations 12 or other composed lamination constructions 13 are used, it is harder but not impossible to obtain similar mechanical properties.

(39) In all previous examples, the cut 9 was drawn radially and, in case there were poles 5, through the thinnest part of the stack. The ideas of the present invention are not restricted to these particular cases. It may e.g. be thought of having a cut through the poles 5. In the same way, it may be considered to realize the physical interruption by straight non-radial cuts 9 or even non-straight cuts 9. A reason for applying non-radial cuts can be to further reduce the flux density increase in the vicinity of the cut. A reason for applying non-straight cuts can be to improve the structural properties of the stack when the stack is rotating in operation or when the stack is assembled with 180.sub.< laminations 11 or 120.sub.< laminations 12. In such cases, one could e.g. consider a cut 9 that is shaped like a dovetail-connection, and preferably with an insulating spacer material 14 in between, to avoid any possible electrical contact. This idea is illustrated in FIG. 21.

(40) In all possible embodiments covered by the previous descriptions, the cuts 9 in adjacent lamination layers never coincided. This condition may be relaxed slightly. One can also assemble an actuator target stack 1 or a stator stack 2 as a series of rotated (pivoted and/or flipped) substacks, in which each substack is itself a stack of at least two adjacent lamination layers, having the property that some or all of the cuts 9 in adjacent lamination layers coincide. In this case, magnetic symmetry can be safeguarded by evenly distributing the entire set of cuts 9 over the circumference of the complete stack. Doing so yields a configuration in which the magnetic field can always find a low-reluctant path in the vicinity of a cut, via an adjacent substack. However, since the magnetic field lines must cross more coating layers in this configuration, it may be considered a less favorable arrangement. On the other hand, constructional issues may make this concept a feasible alternative.

(41) The invention is in no way limited to the forms of embodiment of a laminated core as described above or shown in the drawings, however, such a laminated core can be made in all shapes and dimensions without departure from the scope of the invention.