CN112968549A - Rotor assembly and self-starting permanent magnet synchronous reluctance motor - Google Patents
Rotor assembly and self-starting permanent magnet synchronous reluctance motor Download PDFInfo
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- CN112968549A CN112968549A CN202110102648.XA CN202110102648A CN112968549A CN 112968549 A CN112968549 A CN 112968549A CN 202110102648 A CN202110102648 A CN 202110102648A CN 112968549 A CN112968549 A CN 112968549A
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- 230000001360 synchronised effect Effects 0.000 title claims abstract description 19
- 241000555745 Sciuridae Species 0.000 claims description 34
- 239000012811 non-conductive material Substances 0.000 claims description 3
- 230000004907 flux Effects 0.000 description 14
- 230000004888 barrier function Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- 230000008859 change Effects 0.000 description 3
- 230000006698 induction Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000005347 demagnetization Effects 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000000696 magnetic material Substances 0.000 description 1
- 239000003507 refrigerant Substances 0.000 description 1
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K1/00—Details of the magnetic circuit
- H02K1/06—Details of the magnetic circuit characterised by the shape, form or construction
- H02K1/22—Rotating parts of the magnetic circuit
- H02K1/27—Rotor cores with permanent magnets
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K1/00—Details of the magnetic circuit
- H02K1/06—Details of the magnetic circuit characterised by the shape, form or construction
- H02K1/22—Rotating parts of the magnetic circuit
- H02K1/27—Rotor cores with permanent magnets
- H02K1/2706—Inner rotors
- H02K1/272—Inner rotors the magnetisation axis of the magnets being perpendicular to the rotor axis
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K21/00—Synchronous motors having permanent magnets; Synchronous generators having permanent magnets
- H02K21/02—Details
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K2213/00—Specific aspects, not otherwise provided for and not covered by codes H02K2201/00 - H02K2211/00
- H02K2213/03—Machines characterised by numerical values, ranges, mathematical expressions or similar information
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Abstract
The application provides a rotor assembly and a self-starting permanent magnet synchronous reluctance motor. This rotor subassembly includes rotor core (1), on the cross section of rotor core (1), be provided with slot (2) and permanent magnet (3) on rotor core (1), permanent magnet (3) set up in slot (2), and arrange at least two-layer along d axle direction, along the outside direction of d axle radial, permanent magnet (3) increase progressively along the length of q axle direction, the polar arc angle of permanent magnet (3) diminishes progressively, the polar arc angle is the contained angle that the line formed between the central axis of both ends edge of permanent magnet (3) and rotor core (1). According to the rotor subassembly of this application, can guarantee the maximize utilization of inlayer permanent magnet, avoid taking place the magnetic saturation phenomenon simultaneously, improve motor output torque and efficiency.
Description
Technical Field
The application relates to the technical field of motors, in particular to a rotor assembly and a self-starting permanent magnet synchronous reluctance motor.
Background
The self-starting permanent magnet synchronous reluctance motor combines the structural characteristics of an induction motor and a synchronous permanent magnet reluctance motor, realizes starting by generating torque through cage induction, realizes constant-speed operation by the difference of magnetic fluxes of d and q axes of a rotor and the torque generated by a permanent magnet, and can be directly connected with a power supply to realize starting operation. The self-starting permanent magnet synchronous reluctance motor can utilize reluctance torque to improve the output torque of the motor, and compared with the self-starting permanent magnet motor, the self-starting permanent magnet synchronous reluctance motor has the advantages that the consumption of permanent magnets is reduced, and the cost is reduced; compared with an asynchronous motor, the self-starting permanent magnet synchronous reluctance motor has high efficiency, the rotating speed is constant and synchronous, and the rotating speed cannot change along with the load.
The traditional permanent magnet motor and the permanent magnet synchronous reluctance motor need a driver to start and control operation, the cost is high, the control is complex, and the driver occupies part of loss, so that the efficiency of the whole motor system is reduced.
Chinese patent publication No. CN107994698A provides a self-starting permanent magnet synchronous reluctance motor to reduce the cost of a permanent magnet, but the structure arrangement between the permanent magnet and a magnetic conduction channel in the self-starting permanent magnet synchronous reluctance motor is not reasonable, so that the magnetic saturation phenomenon easily occurs in the magnetic conduction channel, and the output torque and efficiency of the motor are reduced.
Disclosure of Invention
Therefore, the technical problem that this application will be solved lies in providing a rotor subassembly and self-starting permanent magnet synchronous reluctance motor, can guarantee that the inner permanent magnet maximize utilizes, avoids taking place the magnetic saturation phenomenon simultaneously, improves motor output torque and efficiency.
In order to solve the problem, the application provides a rotor assembly, including rotor core, on rotor core's cross section, last slot and the permanent magnet of being provided with of rotor core, the permanent magnet sets up in the slot to arrange at least two-layer along d axle direction, along the outside direction of d axle radial, the length of permanent magnet along q axle direction increases progressively, the polar arc angle of permanent magnet diminishes progressively, the polar arc angle is the contained angle that the line formed between the central axis of the both ends edge of permanent magnet and rotor core.
Preferably, the thickness of the permanent magnet increases in a direction radially outward of the d-axis.
Preferably, the permanent magnet and the slit groove are symmetrical with respect to the d-axis or the q-axis; and/or the slit groove comprises an arc-shaped section and parallel sections, the parallel sections are arranged at two ends of the arc-shaped section, the arc-shaped section protrudes outwards along the radial direction, and the permanent magnet is arranged in the arc-shaped section.
Preferably, both ends of the slit groove are provided with q-axis cage grooves extending in a direction parallel to the q-axis.
Preferably, an independent squirrel cage groove is further arranged on the rotor iron core.
Preferably, under the same pole, the independent squirrel-cage grooves and the q-axis squirrel-cage grooves are alternately arranged along the circumferential direction of the rotor core; and/or the individual cage grooves extend in a direction parallel to the q-axis.
Preferably, the q-axis cage grooves and the individual cage grooves are symmetrically distributed with respect to the q-axis.
Preferably, the sum of the minimum widths of the magnetic conduction channels between the independent squirrel cage groove and the q-axis squirrel cage grooves on the two sides is greater than the minimum width of the magnetic conduction channel in which the independent squirrel cage groove is positioned.
Preferably, the minimum width of the magnetic conduction channel between the adjacent slit grooves is T23, and the minimum width between two q-axis squirrel cage grooves adjacent to the q axis is T1, wherein T23 is more than T1.
Preferably, a d-axis squirrel-cage groove is further formed in the rotor core and is located on one side, close to the outer circle of the rotor, of the permanent magnet on the outermost side in the radial direction of the d axis.
Preferably, the d-axis cage grooves extend in a direction parallel to the d-axis; and/or the number of the d-axis squirrel-cage grooves is multiple, and the multiple d-axis squirrel-cage grooves are symmetrically distributed around the d axis.
Preferably, the minimum width of the q-axis cage groove along the d-axis direction is m1, the maximum width of the independent cage groove along the d-axis direction is m2, and the maximum width of the d-axis cage groove along the q-axis direction is m3, wherein m2 < m1, and m3 < m 1; and/or the maximum width of the d-axis cage grooves along the q-axis direction is m3, and the minimum distance between the adjacent d-axis cage grooves is m4, wherein m3 is less than m 4.
Preferably, each of the q-axis cage grooves, the independent cage grooves and the d-axis cage grooves has a length greater than 2 times its own width.
Preferably, the q-axis cage groove, the independent cage groove and the d-axis cage groove are filled with conductive and non-conductive materials.
Preferably, end rings are arranged at two ends of the rotor core, and the q-axis squirrel-cage groove, the d-axis squirrel-cage groove and the independent squirrel-cage groove are in short-circuit connection through the end rings to form a squirrel-cage structure.
Preferably, at least one side edge of the slit groove at the end part of the two ends of the permanent magnet is provided with a limiting bulge for limiting the permanent magnet.
Preferably, the two ends of the rotor core are provided with non-magnetic baffles, and the non-magnetic baffles can shield the permanent magnet.
According to another aspect of the present application, there is provided a self-starting permanent magnet synchronous reluctance machine comprising a stator and a rotor assembly, the rotor assembly being as described above.
Preferably, when the rotor core is provided with a q-axis squirrel cage groove, an independent squirrel cage groove and a d-axis squirrel cage groove, the widths of magnetic bridges between the q-axis squirrel cage groove, the independent squirrel cage groove and the d-axis squirrel cage groove and the outer circle of the rotor and the widths of magnetic bridges between the q-axis squirrel cage groove and the slit groove are L, wherein L is more than or equal to 0.5 sigma and less than or equal to 1.5 sigma, and sigma is the radial width of an air gap between the stator and the rotor core.
The application provides a rotor subassembly, including rotor core, on rotor core's cross section, last slit groove and the permanent magnet of being provided with of rotor core, the permanent magnet setting is in the slit inslot to arrange at least two-layer along d axle direction, along the outside direction of d axle radial direction, the permanent magnet increases progressively along the length of q axle direction, the polar arc angle of permanent magnet subtracts progressively, the polar arc angle is the contained angle that line formed between the both ends edge of permanent magnet and rotor core's the central axis. This rotor subassembly can rationally prescribe a limit to the structure of permanent magnet through prescribing a limit to the permanent magnet along the length variation and the change of polar arc angle of d axle direction to can guarantee the maximize utilization of inlayer permanent magnet, avoid taking place the magnetic saturation phenomenon simultaneously, improve motor output torque and efficiency.
Drawings
FIG. 1 is a schematic structural view of a rotor assembly according to an embodiment of the present application;
FIG. 2 is an enlarged, fragmentary, schematic structural view of a rotor assembly according to one embodiment of the present application;
FIG. 3 is an enlarged, fragmentary, schematic view of a rotor assembly according to one embodiment of the present application;
FIG. 4 is an axial view of a rotor assembly of an embodiment of the present application;
FIG. 5 is a schematic structural view of a non-magnetic conductive baffle of a rotor assembly according to an embodiment of the present application;
FIG. 6 is an axial view of a rotor assembly of an embodiment of the present application;
fig. 7 is a torque curve comparison diagram of the motor according to the embodiment of the present application and the motor according to the related art.
The reference numerals are represented as:
1. a rotor core; 2. a slit groove; 3. a permanent magnet; 4. a q-axis squirrel cage slot; 5. a d-axis squirrel cage groove; 6. an independent squirrel cage groove; 7. a shaft hole; 8. an end ring; 9. a limiting bulge; 10. a non-magnetic baffle; 11. and (4) riveting.
Detailed Description
With combined reference to fig. 1 to 7, according to an embodiment of the present application, the rotor assembly includes a rotor core 1, on a cross section of the rotor core 1, a slot 2 and a permanent magnet 3 are disposed on the rotor core 1, the permanent magnet 3 is disposed in the slot 2, and at least two layers are disposed along a d-axis direction, along a d-axis radially outward direction, a length of the permanent magnet 3 along a q-axis direction increases progressively, a polar arc angle of the permanent magnet 3 decreases progressively, and the polar arc angle is an included angle formed by a connecting line between edges at two ends of the permanent magnet 3 and a central axis of the rotor core 1.
This rotor subassembly can rationally prescribe a limit to the structure of permanent magnet 3 through prescribing a limit to the permanent magnet 3 along the length variation and the change of polar arc angle of d axle direction to can guarantee 3 maximize utilizations of inlayer permanent magnet, avoid taking place the magnetic saturation phenomenon simultaneously, improve motor output torque and efficiency.
The length of the permanent magnet 3 along the q-axis direction is increased progressively along the outward radial direction of the d-axis, so that the length of the outer permanent magnet 3 is longer, sufficient permanent magnet magnetic flux is provided, the permanent magnet torque is increased, and the motor efficiency is improved. In one embodiment, two layers of permanent magnets 3 are arranged in the direction of the d axis, the permanent magnet 3 positioned at the inner layer has a length of K1 in the direction of the q axis, and the permanent magnet 3 positioned at the outer layer has a length of K2 in the direction of the q axis, where K2 > K1.
The polar arc angle of the permanent magnet 3 is gradually decreased along the radial outward direction of the d axis, so that the polar arc angle of the inner layer permanent magnet 3 is larger, the magnetic flux of the inner layer magnetic channel is increased, and meanwhile, the magnetic flux is connected with the outer layer permanent magnet in series to provide partial magnets for the d axis, and the utilization rate of the permanent magnet is maximized. In one embodiment, two layers of permanent magnets 3 are arranged along the direction of the d axis, the pole arc angle of the permanent magnet 3 positioned at the inner layer is A1, the pole arc angle of the permanent magnet 3 positioned at the outer layer is A2, and A1 is greater than A2.
In one embodiment, the thickness of the permanent magnet 3 increases in the direction radially outward along the d-axis, so that the thickness of the outer permanent magnet 3 is greater than that of the inner permanent magnet 3. The outer permanent magnet 3 is closer to the air gap, the demagnetization resistance of the outer permanent magnet 3 can be improved by increasing the thickness of the outer permanent magnet 3, and more permanent magnet magnetic fluxes are provided, so that the torque output of the motor is increased. In one embodiment, two layers of permanent magnets 3 are arranged along the direction of the d axis, the thickness of the permanent magnet 3 positioned at the inner layer is L1, the pole arc angle of the permanent magnet 3 positioned at the outer layer is L2, and L2 is more than L1.
In one embodiment, the permanent magnet 3 and the slit groove 2 are symmetrical with respect to the d-axis or the q-axis. Referring to fig. 2, in the present embodiment, the slit groove 2 includes arc-shaped sections and parallel sections, the parallel sections being disposed at both ends of the arc-shaped sections, the arc-shaped sections protruding outward in the radial direction, and the permanent magnets 3 being installed in the arc-shaped sections.
The permanent magnet 3 is arc-shaped, the structure of the permanent magnet is matched with that of the slit groove 2 at the position of the permanent magnet, and the permanent magnet 3 can be conveniently installed in the slit groove 2.
In other embodiments, the middle protruding part of the slit groove 2 may also be formed by combining a plurality of straight line segments, in which case the permanent magnet 3 is also correspondingly adjusted to a rectangular block structure adapted to the straight line segment slit groove 2, as shown in fig. 3. In some embodiments, the slit groove 2 may be composed of a plurality of arc-shaped segments or rectangular segments, and the overall shape protrudes radially outward. Each layer of permanent magnet 3 can be formed by combining a plurality of arc-shaped sections or rectangular sections, and the overall shape of each layer of permanent magnet 3 protrudes outwards along the radial direction.
The q-axis squirrel-cage grooves 4 are formed in the two ends of the slit groove 2, the q-axis squirrel-cage grooves 4 extend in the direction parallel to the q axis, the influence of the q-axis squirrel-cage grooves 4 on q-axis magnetic flux can be reduced, the q-axis magnetic flux is increased, and reluctance torque is improved.
In one embodiment, the rotor core 1 is further provided with independent squirrel-cage grooves 6, and the independent squirrel-cage grooves 6 and the q-axis squirrel-cage grooves 4 are alternately arranged along the circumferential direction of the rotor core 1 under the same pole. By adding the independent squirrel-cage grooves 6, the number of the squirrel-cage grooves can be increased, the squirrel-cage resistance of the rotor assembly is reduced, and the starting capability of the motor is improved.
The independent squirrel cage grooves 6 extend in the direction parallel to the q axis, so that the influence of the independent squirrel cage grooves 6 on the q-axis magnetic flux can be reduced, the q-axis magnetic flux is increased, and the reluctance torque is improved.
In one embodiment, the q-axis squirrel-cage grooves 4 and the independent squirrel-cage grooves 6 are symmetrically distributed relative to the q axis, so that the distribution structure of the q-axis squirrel-cage grooves 4 and the independent squirrel-cage grooves 6 on the rotor core 1 can be optimized, and the starting capability of the motor is further improved.
The sum of the minimum widths of the magnetic conduction channels between the independent squirrel cage groove 6 and the q-axis squirrel cage grooves 4 on the two sides is larger than the minimum width of the magnetic conduction channel where the independent squirrel cage groove 6 is located. In one embodiment, two layers of permanent magnets 3 are arranged along the d-axis direction, the minimum width of a magnetic conduction channel between the independent cage groove 6 positioned between the two layers of permanent magnets 3 and the q-axis cage groove 4 positioned at the radial inner side along the d-axis direction is T21, the minimum width of a magnetic conduction channel between the independent cage groove 6 positioned between the two layers of permanent magnets 3 and the q-axis cage groove 4 positioned at the radial outer side along the d-axis direction is T22, the minimum width of the magnetic conduction channel in which the independent cage groove 6 is positioned is T23, and T21+ T22 is greater than T23. By limiting the width relation of the magnetic conduction channels, the magnetic flux can be ensured to smoothly pass through the magnetic conduction channels on the two sides of the independent squirrel cage groove 6, the magnetic saturation phenomenon is avoided, and the reluctance torque of the motor is improved.
In one embodiment, two layers of permanent magnets 3 are arranged along the d-axis direction, the minimum width of a magnetic conduction channel between two adjacent slit grooves 2 is T23, the minimum width of a magnetic conduction channel between two q-axis squirrel-cage grooves 4 adjacent to the q-axis is T1, wherein T23 is greater than T1, the width of the magnetic conduction channel between two q-axis squirrel-cage grooves 4 adjacent to the q-axis can be reduced as much as possible, the width of the magnetic conduction channel between two adjacent permanent magnets 3 can be increased as much as possible, so that the width of the magnetic conduction channel is more reasonably distributed, the magnetic flux of the permanent magnets 3 can be ensured to maximally pass through the magnetic conduction channel, the width of the magnetic conduction channel at a position with larger magnetic flux can be increased, the magnetic saturation phenomenon is avoided, and the torque output and the motor efficiency of the motor are integrally improved.
In one embodiment, the rotor core 1 is further provided with d-axis squirrel cage grooves 5, the d-axis squirrel cage grooves 5 are positioned on one side, close to the outer circle of the rotor, of the permanent magnet 3 on the outermost side in the radial direction of the d axis, and are arranged between the independent squirrel cage grooves 6 on two sides of the d axis in the circumferential direction.
The d-axis cage grooves 5 extend in a direction parallel to the d-axis; the number of the d-axis squirrel cage grooves 5 is multiple, and the plurality of the d-axis squirrel cage grooves 5 are symmetrically distributed around the d axis. The extending direction of the d-axis squirrel cage groove 5 is parallel to the d axis, so that the magnetic flux of the permanent magnet 3 can be ensured to smoothly enter the stator through the d axis, the permanent magnet torque is improved, and the motor performance is improved.
In one embodiment, the minimum width of the q-axis cage groove 4 along the d-axis direction is m1, the maximum width of the independent cage groove 6 along the d-axis direction is m2, and the maximum width of the d-axis cage groove 5 along the q-axis direction is m3, wherein m2 < m1, m3 < m 1; the maximum width of the d-axis squirrel-cage grooves 5 along the q-axis direction is m3, the minimum distance between the adjacent d-axis squirrel-cage grooves 5 is m4, wherein m3 is smaller than m4, and therefore the problem that the independent squirrel-cage grooves 6 and the d-axis squirrel-cage grooves 5 occupy too much space of the rotor core 1 to cause magnetic field saturation can be avoided.
In one embodiment, each of the q-axis cage grooves 4, the independent cage grooves 6 and the d-axis cage grooves 5 has a length greater than 2 times its own width. Taking the d-axis squirrel-cage groove 5 as an example, the maximum width of the d-axis squirrel-cage groove 5 along the q-axis direction is m3, the minimum length of the d-axis squirrel-cage groove 5 along the d-axis direction is m5, and m5 is greater than 2 × m3, so that the ratio between the length and the width of the d-axis squirrel-cage groove 5 can meet certain limitation, the problem that the width of a magnetic conduction channel is influenced by the overlarge width of the d-axis squirrel-cage groove 5 to cause magnetic field saturation is avoided, meanwhile, a certain squirrel-cage groove area can be ensured by increasing the length of the d-axis squirrel-cage groove 5, the squirrel-cage resistance of a rotor assembly is reduced, and the starting synchronization capacity of the motor is improved.
The length-to-width ratio definition of the q-axis cage grooves 4 and the independent cage grooves 6 can also play the same role.
The slit grooves 2 and the q-axis squirrel cage grooves 4 corresponding to the two ends of the slit grooves are combined to form a magnetic barrier layer, and the number of the magnetic barrier layer in the radial direction of the rotor core 1 is at least more than two. A certain number of magnetic barriers are formed on the rotor core 1, a certain salient pole difference can be guaranteed, the reluctance torque of the motor is increased, and the output capacity and efficiency of the motor are improved. Therefore, the difference between the magnetic fluxes of the d and q axes of the motor can be increased, and the reluctance torque can be increased.
The q-axis squirrel cage groove 4, the independent squirrel cage groove 6 and the d-axis squirrel cage groove 5 are filled with conductive and non-magnetic materials. The electrically and magnetically non-conductive material is, for example, aluminum or an aluminum alloy.
End rings 8 are arranged at two ends of the rotor core 1, the q-axis squirrel-cage grooves 4, the d-axis squirrel-cage grooves 5 and the independent squirrel-cage grooves 6 jointly form squirrel-cage grooves which are distributed along the circumferential direction of the rotor core 1, and the squirrel-cage grooves are connected in a short circuit mode through the end rings 8 to form a squirrel-cage structure. The material of the end ring 8 is the same as the filling material in the cage grooves. The self-short-circuited squirrel-cage structure provides asynchronous torque in the starting stage of the motor so as to realize the self-starting of the motor. The rotor multilayer permanent magnetic barrier structure consisting of the slot 2, the squirrel cage slot and the permanent magnet 3 provides permanent magnet torque and reluctance torque for the motor so as to realize synchronous operation of the motor.
In one embodiment, limiting protrusions 9 for limiting the permanent magnet 3 are arranged on at least one side edge of the slit groove 2 at the end positions of the two ends of the permanent magnet 3, the limiting protrusions 9 protrude towards the opposite side edge, the permanent magnet 3 can be limited from the two ends of the permanent magnet 3, the permanent magnet 3 is placed to slide, and stability and reliability of the installation position of the permanent magnet 3 are improved.
The two ends of the rotor core 1 are provided with non-magnetic baffles 10, and the non-magnetic baffles 10 can shield the permanent magnets 3 but do not shield all the slit grooves 2. The non-magnetic baffle 10 can fix the two ends of the permanent magnet 3 along the axial direction of the rotor core 1, and the part of the slit groove 2 which is not shielded can form a through hole in the axial direction of the rotor core 1, so that the flow of air or a refrigerant is facilitated, the heat dissipation of the rotor is improved, and the motor efficiency is improved.
Still be equipped with the rivet hole on the rotor core 1, the rotor subassembly compresses tightly the magnetic conduction baffle 10 of not leading at rotor core 1 both ends along the axial through rivet 11 to constitute the rotor subassembly. The non-magnetic baffle 10 can axially fix the permanent magnet 3 and prevent the permanent magnet 3 from falling out.
Referring to fig. 7, a torque curve comparison diagram of the motor according to the embodiment of the present application and a torque curve comparison diagram of a motor according to the related art is shown, and it can be seen from the diagrams that, under the same stator and current, the motor efficiency is significantly improved by using the torque improvement of the motor according to the embodiment of the present application.
According to an embodiment of the present application, a self-starting permanent magnet synchronous reluctance machine includes a stator and a rotor assembly, which is the above-described rotor assembly.
In one embodiment, when the rotor core 1 is provided with the q-axis cage groove 4, the independent cage groove 6 and the d-axis cage groove 5, the widths of the q-axis cage groove 4, the independent cage groove 6, the d-axis cage groove 5 and the rotor excircle and the widths of the q-axis cage groove 4 and the slit groove 2 are L, wherein L is more than or equal to 0.5 sigma and less than or equal to 1.5 sigma, and sigma is the radial width of the air gap between the stator and the rotor core 1. By limiting the relationship between the width of the magnetic bridge and the width of the air gap, the width of the magnetic bridge can be prevented from being too small, so that the mechanical strength of the rotor assembly is improved, and the width of the magnetic bridge can be prevented from being too large, so that the magnetic leakage is reduced.
It is readily understood by a person skilled in the art that the advantageous ways described above can be freely combined, superimposed without conflict.
The present invention is not intended to be limited to the particular embodiments shown and described, but is to be accorded the widest scope consistent with the principles and novel features herein disclosed. The foregoing is only a preferred embodiment of the present application, and it should be noted that, for those skilled in the art, several modifications and variations can be made without departing from the technical principle of the present application, and these modifications and variations should also be considered as the protection scope of the present application.
Claims (19)
1. The utility model provides a rotor subassembly, its characterized in that includes rotor core (1) on the cross section of rotor core (1), be provided with slot (2) and permanent magnet (3) on rotor core (1), permanent magnet (3) set up in slot (2) to arrange at least two-layer along d axle direction, along the outside direction of d axle radial, permanent magnet (3) increase progressively along the length of q axle direction, the polar arc angle of permanent magnet (3) diminishes progressively, the polar arc angle does the both ends edge of permanent magnet (3) with the contained angle that line between the central axis of rotor core (1) formed.
2. The rotor assembly according to claim 1, wherein the thickness of the permanent magnets (3) increases in a direction radially outward of the d-axis.
3. The rotor assembly according to claim 1, wherein the permanent magnets (3) and the slit grooves (2) are symmetrical with respect to a d-axis or a q-axis; and/or the slit groove (2) comprises an arc-shaped section and parallel sections, the parallel sections are arranged at two ends of the arc-shaped section, the arc-shaped section protrudes outwards along the radial direction, and the permanent magnet (3) is arranged in the arc-shaped section.
4. The rotor assembly according to claim 1, wherein both ends of the slit groove (2) are provided with q-axis cage grooves (4), the q-axis cage grooves (4) extending in a direction parallel to the q-axis.
5. The rotor assembly according to claim 4, characterized in that an independent cage groove (6) is further provided on the rotor core (1).
6. The rotor assembly according to claim 5, wherein the independent cage grooves (6) alternate with the q-axis cage grooves (4) along the circumferential direction of the rotor core (1) under the same pole; and/or the individual cage grooves (6) extend in a direction parallel to the q-axis.
7. The rotor assembly according to claim 5, wherein the q-axis squirrel cage slots (4) and the independent squirrel cage slots (6) are symmetrically distributed with respect to the q-axis.
8. The rotor assembly according to claim 5, wherein the sum of the minimum widths of the magnetic conducting channels between the independent cage groove (6) and the q-axis cage grooves (4) at both sides is greater than the minimum width of the magnetic conducting channel in which the independent cage groove (6) is located.
9. The rotor assembly according to claim 4, wherein the minimum width of the magnetic conduction channel between adjacent slot grooves (2) is T23, and the minimum width between two q-axis cage grooves (4) adjacent to the q-axis is T1, wherein T23 > T1.
10. The rotor assembly according to any one of claims 5 to 8, wherein a d-axis cage groove (5) is further formed in the rotor core (1), and the d-axis cage groove (5) is located on one side, close to the outer circle of the rotor, of the permanent magnet (3) on the outermost side in the radial direction of the d-axis direction.
11. The rotor assembly according to claim 10, wherein the d-axis cage grooves (5) extend in a direction parallel to the d-axis; and/or the number of the d-axis squirrel-cage grooves (5) is multiple, and the multiple d-axis squirrel-cage grooves (5) are symmetrically distributed around the d axis.
12. The rotor assembly of claim 10, wherein the q-axis cage groove (4) has a minimum width of m1 in the d-axis direction, the independent cage groove (6) has a maximum width of m2 in the d-axis direction, and the d-axis cage groove (5) has a maximum width of m3 in the q-axis direction, wherein m2 < m1, m3 < m 1; and/or the maximum width of the d-axis squirrel-cage grooves (5) along the q-axis direction is m3, and the minimum distance between the adjacent d-axis squirrel-cage grooves (5) is m4, wherein m3 is less than m 4.
13. The rotor assembly of claim 10, wherein each of the q-axis cage slots (4), the independent cage slots (6) and the d-axis cage slots (5) has a length greater than 2 times its width.
14. The rotor assembly of claim 10, wherein the q-axis cage slots (4), the independent cage slots (6) and the d-axis cage slots (5) are filled with an electrically and magnetically non-conductive material.
15. The rotor assembly according to claim 10, wherein end rings (8) are provided at both ends of the rotor core (1), and the q-axis cage grooves (4), the d-axis cage grooves (5) and the independent cage grooves (6) are short-circuited by the end rings (8) to form a cage structure.
16. The rotor assembly according to claim 1, wherein at least one side edge of the slit groove (2) at the end positions of both ends of the permanent magnet (3) is provided with a limiting protrusion (9) for limiting the permanent magnet (3).
17. The rotor assembly according to claim 1, wherein both ends of the rotor core (1) are provided with non-magnetically conductive baffles (10), the non-magnetically conductive baffles (10) being capable of shielding the permanent magnets (3).
18. A self-starting permanent magnet synchronous reluctance machine comprising a stator and a rotor assembly, wherein the rotor assembly is as claimed in any one of claims 1 to 17.
19. Self-starting permanent magnet synchronous reluctance machine according to claim 18, wherein when said rotor core (1) is provided with q-axis cage slots (4), independent cage slots (6) and d-axis cage slots (5), the magnetic bridge width between said q-axis cage slots (4), independent cage slots (6) and d-axis cage slots (5) and the rotor outer circle and between said q-axis cage slots (4) and said slot slots (2) is L, wherein 0.5 σ ≦ L ≦ 1.5 σ, σ being the radial width of the air gap between said stator and said rotor core (1).
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114123577A (en) * | 2021-11-05 | 2022-03-01 | 珠海格力电器股份有限公司 | Magnetic steel assembly, rotor assembly and motor |
Citations (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2014100048A (en) * | 2012-10-19 | 2014-05-29 | Toshiba Corp | Permanent magnet type rotary electric machine |
| EP2741402A1 (en) * | 2011-08-05 | 2014-06-11 | Gree Electric Appliances, Inc. of Zhuhai | Motor and rotor thereof |
| US20140167550A1 (en) * | 2011-08-05 | 2014-06-19 | Gree Green Refrigeration Technology Center Co., Ltd. Of Zhuhai | Motor rotor and motor having same |
| CN106256079A (en) * | 2014-04-22 | 2016-12-21 | 三菱电机株式会社 | Permanent magnet submerged formula motor, compressor, refrigerating air conditioning device |
| CN107834800A (en) * | 2017-11-08 | 2018-03-23 | 卧龙电气集团股份有限公司 | One kind is without controller self-starting permanent magnetism assist in synchronization reluctance motor |
| CN108199509A (en) * | 2017-12-27 | 2018-06-22 | 江苏大学 | A kind of fractional-slot concentratred winding permanent magnet synchronous motor and its design method for improving reluctance torque |
| US20180198356A1 (en) * | 2017-01-06 | 2018-07-12 | Hamilton Sundstrand Corporation | Line-start synchronous reluctance motor with improved performance |
| CN109309414A (en) * | 2017-11-30 | 2019-02-05 | 珠海格力节能环保制冷技术研究中心有限公司 | Rotor structure, asynchronous starting synchronous magnetic resistance motor and compressor |
| CN109494903A (en) * | 2017-12-14 | 2019-03-19 | 珠海格力节能环保制冷技术研究中心有限公司 | Asynchronous starting synchronous magnetic resistance motor rotor, motor and compressor |
| CN110138116A (en) * | 2019-06-19 | 2019-08-16 | 珠海格力电器股份有限公司 | Synchronous reluctance motor rotor structure, motor and compressor |
| CN110138117A (en) * | 2019-06-19 | 2019-08-16 | 珠海格力电器股份有限公司 | Synchronous reluctance motor rotor structure, motor and manufacturing method of rotor structure |
| CN112104180A (en) * | 2020-08-21 | 2020-12-18 | 石镇德 | Asynchronous starting permanent magnet auxiliary type synchronous reluctance motor |
| CN112186921A (en) * | 2019-07-04 | 2021-01-05 | 艾默生环境优化技术(苏州)有限公司 | Rotor for asynchronous starting permanent magnet motor and asynchronous starting permanent magnet motor |
-
2021
- 2021-01-26 CN CN202110102648.XA patent/CN112968549B/en active Active
Patent Citations (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2741402A1 (en) * | 2011-08-05 | 2014-06-11 | Gree Electric Appliances, Inc. of Zhuhai | Motor and rotor thereof |
| US20140167550A1 (en) * | 2011-08-05 | 2014-06-19 | Gree Green Refrigeration Technology Center Co., Ltd. Of Zhuhai | Motor rotor and motor having same |
| JP2014100048A (en) * | 2012-10-19 | 2014-05-29 | Toshiba Corp | Permanent magnet type rotary electric machine |
| CN106256079A (en) * | 2014-04-22 | 2016-12-21 | 三菱电机株式会社 | Permanent magnet submerged formula motor, compressor, refrigerating air conditioning device |
| US20180198356A1 (en) * | 2017-01-06 | 2018-07-12 | Hamilton Sundstrand Corporation | Line-start synchronous reluctance motor with improved performance |
| CN107834800A (en) * | 2017-11-08 | 2018-03-23 | 卧龙电气集团股份有限公司 | One kind is without controller self-starting permanent magnetism assist in synchronization reluctance motor |
| CN109309414A (en) * | 2017-11-30 | 2019-02-05 | 珠海格力节能环保制冷技术研究中心有限公司 | Rotor structure, asynchronous starting synchronous magnetic resistance motor and compressor |
| CN109494903A (en) * | 2017-12-14 | 2019-03-19 | 珠海格力节能环保制冷技术研究中心有限公司 | Asynchronous starting synchronous magnetic resistance motor rotor, motor and compressor |
| EP3672026A1 (en) * | 2017-12-14 | 2020-06-24 | Gree Green Refrigeration Technology Center Co., Ltd. of Zhuhai | Asynchronous starting and synchronous reluctance electric motor rotor, electric motor and compressor |
| CN108199509A (en) * | 2017-12-27 | 2018-06-22 | 江苏大学 | A kind of fractional-slot concentratred winding permanent magnet synchronous motor and its design method for improving reluctance torque |
| CN110138116A (en) * | 2019-06-19 | 2019-08-16 | 珠海格力电器股份有限公司 | Synchronous reluctance motor rotor structure, motor and compressor |
| CN110138117A (en) * | 2019-06-19 | 2019-08-16 | 珠海格力电器股份有限公司 | Synchronous reluctance motor rotor structure, motor and manufacturing method of rotor structure |
| CN112186921A (en) * | 2019-07-04 | 2021-01-05 | 艾默生环境优化技术(苏州)有限公司 | Rotor for asynchronous starting permanent magnet motor and asynchronous starting permanent magnet motor |
| CN112104180A (en) * | 2020-08-21 | 2020-12-18 | 石镇德 | Asynchronous starting permanent magnet auxiliary type synchronous reluctance motor |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114123577A (en) * | 2021-11-05 | 2022-03-01 | 珠海格力电器股份有限公司 | Magnetic steel assembly, rotor assembly and motor |
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