Permanent magnet rotor having a combined laminated stack and method of assembly
10027190 ยท 2018-07-17
Assignee
Inventors
- Evgeny Victorovich Kazmin (Moscow, RU)
- Gary Randall Barnes (Schenectady, NY, US)
- Yury Danilovich Vinitzky (Moscow, RU)
- Ronghai Qu (Wuhan, CN)
- Mikhail Avramovich Avanesov (Moscow, RU)
Cpc classification
H02K2213/03
ELECTRICITY
International classification
Abstract
A rotor for an electromagnetic apparatus including: ferromagnetic laminates stacked along a longitudinal axis of the rotor; non-magnetic laminates stacked along the longitudinal axis, wherein the non-magnetic laminates are between the ferromagnetic annular laminates; cavities in the rotor formed by aligned slots in the ferromagnetic and non-magnetic laminates, wherein the cavities are parallel to the axis of the rotor, and a permanent magnet(s) in each of the aligned cavities. The laminates may each be an annular disc or may be segments arranged in an annular array around a shaft of the rotor.
Claims
1. A rotor for an electromagnetic apparatus comprising: a plurality of ferromagnetic disc laminates stacked along a longitudinal axis of the rotor; a plurality of non-magnetic disc laminates stacked along the longitudinal axis, wherein the non-magnetic disc laminates are between the ferromagnetic disc laminates; a plurality of cavities in the rotor formed by aligned slots in the ferromagnetic and non-magnetic disc laminates, wherein the cavities are parallel to the axis of the rotor and a perimeter of each of the cavities is entirely bordered by one of the ferromagnetic and non-magnetic disc laminates, wherein the aligned slots in the non-magnetic disc laminates each have a radially outward surface which extends radially inward further than a radially outer surface of each of the aligned slots in the ferromagnetic disc laminates, and a plurality of permanent magnets, wherein each of the cavities includes a respective one of the plurality of permanent magnets.
2. The rotor of claim 1 wherein the non-magnetic disc laminates are each sandwiched between two of the ferromagnetic disc laminates.
3. The rotor of claim 1 wherein the permanent magnets are inclined such that one side of each permanent magnet is radially outward from the axis further than the opposite side of the permanent magnet.
4. The rotor of claim 1 wherein the non-magnetic disc laminates constitute 10 percent to 25 percent of a length of the non-magnetic and ferromagnetic disc laminates stacked for the rotor.
5. The rotor of claim 1 further comprising a plurality of rods extending through the non-magnetic and ferromagnetic disc laminates, wherein the rods are radially inward of the aligned slots and radially outward of an inner perimeter of the non-magnetic and ferromagnetic disc laminates.
6. The rotor of claim 1 wherein an insulation layer is between opposing pairs of the non-magnetic and ferromagnetic disc laminates in the stack.
7. A cylindrical rotor for an electromagnetic apparatus comprising: ferromagnetic disc laminates stacked along a longitudinal axis of the rotor; non-magnetic disc laminates stacked along the longitudinal axis, wherein the non-magnetic disc laminates are stacked between the ferromagnetic disc laminates; cavities formed by slots in the ferromagnetic and non-magnetic disc laminates, wherein the slots extend through the disc laminates, a perimeter of each of the slots is entirely bordered by one of the disc laminates, and the cavities are parallel to the axis of the rotor, and wherein the slots in the non-magnetic disc laminates each have a radially outer surface extending radially inward further than a radially outer surface of each of the aligned slots in the ferromagnetic disc laminates; and a plurality of permanent bar magnets, wherein each of the cavities includes a respective one of the plurality of permanent bar magnets and wherein the permanent bar magnet extends parallel to the axis of the rotor.
8. The rotor of claim 7 wherein the non-magnetic disc laminates constitute 10 percent to 25 percent of a length of the non-magnetic and ferromagnetic disc laminates stacked for the rotor.
9. The rotor of claim 7 further comprising a plurality of rods extending through the disc laminates, wherein the rods are radially inward of the slots and radially outward of an inner perimeter of the disc laminates.
10. The rotor of claim 7 wherein the permanent magnet abuts the radially outer surface of the aligned slots in the non-magnetic disc laminates and does not abut the radially outer surface of the aligned slots of the ferromagnetic disc laminates.
11. A rotor for an electromagnetic apparatus comprising: ferromagnetic disc laminates stacked along a longitudinal axis of the rotor, wherein a first slot in each of the ferromagnetic disc laminates has a perimeter entirely bordered by a respective one of the ferromagnetic disc laminate; non-magnetic disc laminates stacked along the longitudinal axis and the non-magnetic disc laminates are between the ferromagnetic disc laminates, wherein a second slot in each of the non-magnetic disc laminates has a perimeter entirely bordered by a respective one of the non-magnetic disc laminates and each of the second slots has a radially outer surface extending radially inward further than a radially outer surface of each of the first slots; cavities in the rotor formed by aligning the first and second slots along the longitudinal axis, and a plurality of permanent magnets, wherein each of the cavities receives a respective one of the plurality of permanent magnets.
12. The rotor of claim 11 wherein the non-magnetic disc laminates are sandwiched between the ferromagnetic disc laminates.
13. The rotor of claim 11 wherein the permanent magnets are inclined such that one side of each of the permanent magnets is radially outward from the axis further than the opposite side of the permanent magnet.
14. The rotor of claim 11 wherein the non-magnetic disc laminates constitute 10 percent to 25 percent of a length of the non-magnetic and ferromagnetic disc laminates stacked for the rotor.
15. The rotor of claim 11 further comprising rods extending through the ferromagnetic laminates and the non-magnetic disc laminates, wherein the rods are radially inward of the first and second slots.
16. The rotor of claim 11 further comprising an insulation layer between each of the ferromagnetic disc laminates and the non-magnetic disc laminates.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1)
(2)
(3)
(4)
(5)
(6)
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(8)
(9)
DETAILED DESCRIPTION OF THE INVENTION
(10)
(11) The rotor 10 includes permanent magnets (PM) within the laminated rotor. The rotor may be a cylindrical stack of laminations, e.g., laminates or laminate segments, 16, 17, mounted on a cylindrical rim 18 or directly to the rotor shaft 20. The rim 18 may be coaxially fitted to the rotor shaft 20 that is mounted on bearings in a casing that houses the rotor and stator. The rim is optional and the laminates may be mounted directly to the rotor shaft.
(12) The laminations 16, 17 may be separated by insulation layers or coatings 19, formed of materials such as resins and non-conductive laminates. The laminates in the rotor are a mix of ferromagnetic laminates 16 and non-magnetic laminates 17.
(13) The ferromagnetic laminates 16 are formed of or include a ferromagnetic material, such as iron. The non-magnetic laminates 17 may be formed of a high-strength material, which need not be magnetic. Examples of the high-strength materials for the laminate 17 include stainless-steel and other types of non-magnetic metals. The non-magnetic laminates may also be formed of materials that have the same strength or less strength than the ferromagnetic material forming the magnetic laminations. If the non-magnetic laminates have a material strength the same or less than the magnetic laminates, the bridges in the non-magnetic laminations may be thicker than the bridges in the magnetic laminates.
(14) The laminates may be stacked on the rotor rim such that the ferromagnetic laminates 16 alternate with the non-magnetic laminates 17. The alternating arrangement may be that at least one non-magnetic laminate is between adjacent ferromagnetic laminates. Similarly, the alternating arrangements may that two, three or more ferromagnetic laminates 16 are stacked together in groups and a non-magnetic laminate 17 is between each group of ferromagnetic laminates 16. An insulation layer 19, such as a resin or non-conductive material, may be between each of the laminates 16 and 17.
(15) The laminates need not all be of the same thickness. For example the ferromagnetic laminates 16 may be relatively thick, e.g., 1.5 mm if formed of iron. Ferromagnetic laminates formed of silicon steel may have a thickness of 0.35 to 0.65 mm. Generally, the higher the frequency of the power in the device, the thinner the magnetic laminations. The thickness of the non-magnetic laminations may be the same, thinner or thicker than the magnetic laminations. The non-magnetic laminations may have a thickness no greater than 2 mm.
(16) The proportion of the length of the stacked rotor formed of the non-magnetic laminates 17 is preferred to be as large as possible, but such that it does not reduce an useful air-gap flux. An exemplary range of the amount of non-magnetic laminates in a rotor stack is 10 percent to 25 percent. Further increase of amount of non-magnetic laminates could provide reduction of an air-gap flux, and lead to a negative overall effect.
(17)
(18) The permanent magnets 24 may be arranged in the rotor such that magnetic poles 30 are symmetrically arranged around the circumference of the rotor. The poles are alternating North and South poles. The magnets need to be arranged such that the sides of adjacent magnets 24 have the same polarity, which define the polarity of the respective pole of the rotor. The rotor may have full symmetry of the permanent magnets about each pole 30. In particular, each half of a pole in the rotor may be symmetrical with respect to the other half of the pole. Further, the angular pole pitch between each of the poles 30 may be uniform for all poles in the rotor. The number of poles in a rotor may be greater than shown in
(19) The slots 22 in the annular laminates 16, 17 may be positioned near the outer cylindrical surface 28 of the rotor laminates 16. Bridges 32, 34, also referred to as saturation bridges, are regions in the annular laminates between the slot and the outer perimeter of the disc. An outer bridge 32 is formed by the rotor material between radially outer corner of the slot and the outer surface 28 of the rotor. The outer bridges tend to be the narrowest region of the annular laminates. An inner bridge 34 is formed in each laminate between the radially inward outer corner of the slots. The bridges 32, 34 provide structural support to the permanent magnets 24 in the slots. The bridges 32, 34 withstand the centrifugal forces resulting from the rotating applied to the magnets 24 and stack of rotor laminates 16, 17.
(20)
(21) Non-magnetic spacers 36 in the slots support the magnets and prevent the magnets from sliding in the slots. The non-magnetic spacers may be conventional bars adjacent the sides of the magnets. The cross-sectional shape of the spacers conforms to the sidewalls of the slots. The spacers may be bars extending the length of the stacked rotor or a series of blocks arranged end to end in the rotor. The spacers may be formed of a ductile material, such as a plastic or soft metal. Alternatively the spacers may be an epoxy filled region.
(22)
(23) Lamination segments may be suited for large rotors. Each lamination segment may have a span, e.g., an arc, of at least twice the span angle of one pole in the rotor. By way of example, a lamination segment may span of three poles.
(24) Each pole has a pair of associated internal magnets. There may be one pole angle shift between adjacent layers to provide overlapping.
(25) The segments may be arranged in an annular array directly on the rotor shaft or around a ring, collar or rim on the rotor shaft. The arrays of segments are stacked layer by layer on the rotor.
(26)
(27) At the bridges, the flux density reaches saturation that limits the leakage flux. Nevertheless, leakage flux through the bridges may be, as an example, as much as thirty percent (30%) of the air-gap flux. The total PM flux is a sum of air-gap and leakage fluxes. A 30% loss to flux leakage through the bridges is a concern.
(28)
(29) The addition of non-magnetic laminations to a rotor stack having magnetic laminations leads to an increase in the resistances Rbr and Ri, such as by about twenty percent (20%). Because Ri is relatively small, the increase in. Ri does not substantially affect PM and the air-gap flux. The increase in the magnetic resistance at the bridges (Rbr) resulting from the non-magnetic laminations results in slight reduction in the total PM flux and a substantial increase in the desired air-gap flux. The substantial increase in the air-gap flux is because of the significant reduction in leakage flux through the bridges which is allowed for by the use of the non-magnetic laminations.
(30)
(31) The magnetic flux lines 38 shown in
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(33) The uniform flux distribution in a conventional, all ferromagnetic laminated rotor 40 is in contrast to the concentration of flux in the ferromagnetic laminates in the rotor 14 formed of non-magnetic and ferromagnetic laminates 16, 17, illustrated in
(34) A comparison was made between a generator with a rotor of entirely ferromagnetic laminates and a similar generator except its rotor was eighty-four percent (84%) ferromagnetic laminates and sixteen percent (16%) non-magnetic (stainless steel) laminates, wherein the percentages are with respect to the axial length of the rotor. Both generators were designed to deliver the same output power while being operated at the same fixed rotational speed and same fixed line-voltage. Table 1 below provides a comparison of these two generators:
(35) TABLE-US-00001 TABLE 1 Entirely 84% ferromag. ferromag. and 16% non-mag. Parameter Unit laminates laminates Rotor Stacking Factor 0.96 0.8 Back-emf per unit axial V/m 1218 1265 length(RMS) Stator and rotor stack % 100% 96% length Total Active Mass % 100% 96%
(36) In the exampled shown in Table 1, a PM generator having a rotor with non-magnetic and ferromagnetic laminates has an higher back-emf and output power for each unit length of the rotor, as compared to the generator having a rotor formed entirely of ferromagnetic laminates. Due to the higher back-emf and output power per rotor unit length, the active length of a rotor having some non-magnetic laminates may be shorter, e.g., four percent shorter, for a comparable rotor that is formed entirely of ferromagnetic laminates. The reduced rotor length allows for a reduction in the size, e.g., volume and mass, of the electrical machine due to the rotor having non-magnetic and ferromagnetic laminates. Reducing the mass of the machine generally results in a reduction in the cost of the machine.
(37) Other advantages provided by incorporating non-magnetic and ferromagnetic laminates in a rotor with interior permanent magnets include: (i) relatively thin saturation bridges in the ferromagnetic laminates, (ii) increased rotor strength due to the high strength or thickness of the non-magnetic laminates, (iii) enhanced thermal conductivity and improved rotor heat removal due to the high conductivity of the non-magnetic laminates.
(38)
(39) The slots 56 in ferromagnetic laminates 52 are slightly offset in a radially outward direction from the slots 58 in the non-magnetic laminates 54. The slots 56 in the non-magnetic laminates may be a few millimeters, e.g., 1 to 3 mm, offset from the slots 58 in the ferromagnetic laminates in a radially inward direction. This radial offset may be created by making the slots 58 in the non-magnetic laminates narrower than the slots 56 in the ferromagnetic laminates.
(40) The radial offset causes the slots 58 of the non-magnetic laminates to abut against the permanent magnet while the slots of the ferromagnetic laminate may not abut against the magnet 60. The abutment between the magnet and the slot of the non-magnetic laminate may include a wrapping or other film or thin sheet which protects the magnet. The radial offset is minimized to avoid flux reduction. The radial offset may be less than 1 mm.
(41) Because of the abutting relationship, the non-magnetic laminates support the permanent magnet. The tensile strength and ductility of the non-magnetic disc, e.g., stainless steel, are better suited to supporting the magnets than are the ferromagnetic laminates. The offset or narrower slots in the non-magnetic laminates ensure that they bear the centrifugal load of the permanent magnets. Because of their wider slots or radially outward offset slots, the ferromagnetic laminates do not bear the centrifugal forces of the permanent magnet.
(42)
(43) The rods ensure that the laminates remained aligned in the stack forming the rotor, and that the slots of the laminates remain aligned in the rotor. In addition, the rods may allow centrifugal forces from the ferromagnetic laminates to be distributed, at least in part, to the non-magnetic laminates. Further, the rods may be used to clamp together the laminates by using threaded ends of the rods and bolts to secure end plates at opposite ends of the rotor.
(44) While the invention has been described in connection with what is presently considered to be the most practical and preferred embodiment, it is to be understood that the invention is not to be limited to the disclosed embodiment, but on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the appended claims.
(45) TABLE-US-00002 Ref. Nos. Description 10 Rotating machine 12 Stator 14 rotor 16, 17 discs 18 Rotor rim 19 Insulation layer 20 Rotor shaft 22 Slots in rotor discs 24 Permanent magnets 26 Rotor axis 28 Cylindrical surface of rotor 30 Magnetic poles 32 Outer bridge 34 Inner bridge 36 Non-magnetic spacer 38 magnetic flux lines 40 Conventional rotor FIG. 7 42 Magnetic flux - FIG. 7 44 Lamination in FIG. 4 46 Magnetic flux lines 48 Magnetic circuit 50 Rotor - FIG. 8 52 Ferromagnetic laminate 54 Non-ferromagnetic laminate 56 Slots 58 Slots 60 magnet 62 Rotor of FIG. 9 64 Rods