Motor, compressor, air conditioner, and method for manufacturing motor

文档序号:411848 发布日期:2021-12-17 浏览:7次 中文

阅读说明:本技术 电动机、压缩机、空调装置及电动机的制造方法 (Motor, compressor, air conditioner, and method for manufacturing motor ) 是由 广泽勇二 仁吾昌弘 于 2019-05-20 设计创作,主要内容包括:电动机具备能够以轴线为中心旋转的转子、具有从以轴线为中心的径向上的外侧包围转子的定子芯的定子以及在内侧固定有定子芯的环状的壳体。壳体具有:在径向上与定子芯相向并具有内径D1的第一壳体部、在径向上与定子芯抵接并具有内径D2的第二壳体部以及在轴线的方向上从定子芯突出并具有内径D3的第三壳体部。内径D1、D2及D3满足D1>D2及D1>D3。(The motor includes a rotor rotatable about an axis, a stator having a stator core surrounding the rotor from an outer side in a radial direction about the axis, and an annular housing having the stator core fixed to an inner side thereof. The housing has: the stator includes a first housing portion that faces the stator core in the radial direction and has an inner diameter D1, a second housing portion that abuts the stator core in the radial direction and has an inner diameter D2, and a third housing portion that protrudes from the stator core in the axial direction and has an inner diameter D3. The inner diameters D1, D2, and D3 satisfy D1> D2 and D1> D3.)

1. An electric motor, wherein the electric motor comprises:

a rotor rotatable about an axis;

a stator having a stator core that surrounds the rotor from an outer side in a radial direction centered on the axis; and

an annular housing to which the stator core is fixed on an inner side,

the housing has:

a first housing portion that faces the stator core in the radial direction and has an inner diameter D1;

a second housing portion that abuts the stator core in the radial direction and has an inner diameter D2; and

a third housing portion that protrudes from the stator core in the direction of the axis and has an inner diameter D3,

the inner diameters D1, D2, and D3 satisfy D1> D2 and D1> D3.

2. The motor according to claim 1, wherein,

the inner diameters D2 and D3 satisfy D2 ≧ D3.

3. The motor according to claim 1 or 2,

the first housing portion has a recess on a side facing the stator core.

4. The motor according to any one of claims 1 to 3,

the stator core is fixed to the housing by a caulking portion or a welding portion.

5. The motor according to any one of claims 1 to 4,

the stator core is a member in which a plurality of core elements are connected in a circumferential direction around the axis.

6. The motor according to any one of claims 1 to 5,

the first housing portion is formed at a position corresponding to a central portion of the stator core in the direction of the axis.

7. The motor according to any one of claims 1 to 6,

the second housing portion is formed at a position corresponding to an end portion of the stator core in the direction of the axis.

8. The motor according to any one of claims 1 to 5,

the second housing portion is formed at a position corresponding to a central portion of the stator core in the direction of the axis.

9. The motor according to any one of claims 1 to 5 and 8,

the first housing portion is formed at a position corresponding to an end portion of the stator core in the direction of the axis.

10. The motor according to any one of claims 1 to 9,

the third housing portion is adjacent to the first housing portion or the second housing portion in the direction of the axis.

11. The motor according to any one of claims 1 to 10,

the area of a surface of the first housing portion facing the stator core is larger than the area of a surface of the second housing portion abutting the stator core.

12. The motor according to any one of claims 1 to 11,

a length of the first housing portion in a direction of the axis is longer than a length of the second housing portion in a direction of the axis.

13. The motor according to any one of claims 1 to 12,

a groove is formed in a surface of the first housing portion facing the stator core.

14. A compressor, wherein,

the compressor comprises the motor according to any one of claims 1 to 13 and a compression mechanism driven by the motor.

15. An air conditioning apparatus, wherein,

the air conditioner includes the compressor, the condenser, the pressure reducing device, and the evaporator according to claim 14.

16. A method of manufacturing a motor, comprising:

a step of preparing a casing which is an annular casing centered on an axis and has: a first housing portion having an inner diameter D1, a second housing portion having an inner diameter D2 less than inner diameter D1, and a third housing portion having an inner diameter D3 less than inner diameter D1;

fixing a stator core inside the housing such that the first housing portion faces the stator core in a radial direction about the axis, the second housing portion abuts against the stator core in the radial direction, and the third housing portion protrudes from the stator core in the direction of the axis; and

and a step of mounting a rotor inside the stator core.

17. The manufacturing method of an electric motor according to claim 16,

in the step of fixing the stator core inside the housing, the stator core is fixed inside the housing by shrink fitting or press fitting.

18. The manufacturing method of an electric motor according to claim 17,

the average surface roughness of the inner peripheral surface of the case before the shrink fitting is performed is larger than the shrink fit of the shrink fitting.

19. The method for manufacturing a motor according to any one of claims 16 to 18,

in the step of fixing the stator inside the housing, the housing and the stator core are fixed to each other by heat caulking or welding.

Technical Field

The invention relates to a motor, a compressor, an air conditioner and a method for manufacturing the motor.

Background

A stator of an electric motor includes a stator core formed by laminating laminated steel plates. The stator core is fixed to the inside of a casing of a compressor or the like by shrink fitting or press fitting (for example, patent document 1).

Prior art documents

Patent document

Patent document 1: japanese patent laid-open publication No. 2005-151648 (see FIG. 1)

Disclosure of Invention

Problems to be solved by the invention

However, when the stator core is fixed to the housing, the magnetic characteristics of the stator core may change due to the compressive stress that the stator core receives from the housing, and the iron loss may increase.

The present invention has been made to solve the above problems, and an object of the present invention is to firmly fix a stator core to a housing and reduce iron loss.

Means for solving the problems

An electric motor according to an aspect of the present invention includes: a rotor rotatable about an axis; a stator having a stator core surrounding the rotor from an outer side in a radial direction centered on the axis; and an annular housing to which a stator core is fixed inside. The housing has: a first housing portion radially opposed to the stator core and having an inner diameter D1; a second housing portion that radially abuts the stator core and has an inner diameter D2; and a third housing portion that protrudes from the stator core in the direction of the axis and has an inner diameter D3. The inner diameters D1, D2, and D3 satisfy D1> D2 and D1> D3.

ADVANTAGEOUS EFFECTS OF INVENTION

According to the above configuration, the stator core can be firmly fixed to the housing by the abutment of the second housing portion with the stator core. In addition, since the first housing portion does not abut against the stator core, an increase in iron loss in the stator core can be suppressed. In addition, the third housing portion can suppress the stator core from coming off the housing. That is, the stator core can be firmly fixed to the housing, and the iron loss can be reduced.

Drawings

Fig. 1 is a cross-sectional view showing a motor of embodiment 1.

Fig. 2 is a cross-sectional view showing a stator core and a housing in embodiment 1.

Fig. 3 is a perspective view showing a part of the stator core of embodiment 1.

Fig. 4 is a perspective view showing a part of a stator core according to embodiment 1, and an insulator and an insulating film mounted thereon.

Fig. 5 is a longitudinal sectional view showing the motor of embodiment 1.

Fig. 6 is a longitudinal sectional view showing a stator core and a housing according to embodiment 1.

Fig. 7 is a flowchart showing a manufacturing process of the motor according to embodiment 1.

Fig. 8 is schematic diagrams (a) and (B) illustrating an example of a method of forming the first case portion according to embodiment 1.

Fig. 9 is schematic diagrams (a) and (B) illustrating a process of shrink-fitting the stator into the housing according to embodiment 1.

Fig. 10 is a vertical cross-sectional view showing the stator core and the housing after the shrink-fitting process in embodiment 1.

Fig. 11 is a schematic view showing a method of fixing the stator core and the housing in embodiment 1.

Fig. 12 is a longitudinal sectional view showing a motor of a comparative example.

Fig. 13 is a graph showing a relationship between the compressive stress received by the stator core and the rate of increase in iron loss.

Fig. 14 is a graph showing a relationship between the breakout load and the rate of increase in iron loss.

Fig. 15 is a graph showing a relationship between the hot-load and the rate of increase in iron loss.

Fig. 16 is a vertical cross-sectional view showing a stator core and a housing according to a modification of embodiment 1.

Fig. 17 is a cross-sectional view showing a stator core and a housing according to embodiment 2.

Fig. 18 is a longitudinal sectional view showing a stator core and a housing according to embodiment 3.

Fig. 19 is a vertical sectional view showing a stator core and a housing according to embodiment 4.

Fig. 20 is a longitudinal sectional view showing a stator core and a housing according to embodiment 5.

Fig. 21 is a view (a) showing the inner peripheral surface of the case of embodiment 6 and a view (B) showing the surface roughness of the inner peripheral surface of the case before the shrink-fitting step.

Fig. 22 is a cross-sectional view showing another configuration example of the stator core and the housing.

Fig. 23 is a sectional view showing a compressor to which the motor of each embodiment can be applied.

Fig. 24 is a diagram showing an air conditioner provided with the compressor of fig. 23.

Detailed Description

Embodiment 1.

< Structure of Motor >

First, the motor 100 of embodiment 1 is explained. Fig. 1 is a cross-sectional view showing a motor 100 of embodiment 1. The motor 100 is a permanent magnet embedded motor in which a permanent magnet 55 is embedded in a rotor 5, and is used in a compressor 500 (fig. 23), for example.

The motor 100 is a so-called inner rotor type motor, and includes a rotatable rotor 5, a stator 1 provided so as to surround the rotor 5, and an annular housing 3 to which the stator 1 is fixed. An air gap of, for example, 0.3 to 1.0mm is formed between the stator 1 and the rotor 5.

Hereinafter, the direction of the axis C1 as the rotation axis of the rotor 5 is simply referred to as "axial direction". The circumferential direction (indicated by an arrow R1 in fig. 1) centered on the axis C1 is simply referred to as the "circumferential direction". The radial direction centered on the axis C1 is simply referred to as the "radial direction". The cross-sectional view in the plane perpendicular to the axis C1 is referred to as a "transverse cross-sectional view", and the cross-sectional view in the plane parallel to the axis C1 is referred to as a "longitudinal cross-sectional view".

< Structure of rotor >

The rotor 5 includes a cylindrical rotor core 50, a permanent magnet 55 attached to the rotor core 50, and a shaft 56 fixed to a central portion of the rotor core 50. The shaft 56 is, for example, a shaft of a compressor 500 (fig. 23).

The rotor core 50 is a member in which laminated steel plates are laminated in the axial direction and integrated by caulking or the like. The laminated steel sheet is, for example, an electromagnetic steel sheet. The thickness of the laminated steel sheet is, for example, 0.1 to 0.7mm, and in this case 0.35 mm. A shaft hole 54 is formed at the radial center of the rotor core 50, and the shaft 56 is fixed thereto.

A plurality of magnet insertion holes 51 into which the permanent magnets 55 are inserted are formed along the outer circumferential surface of the rotor core 50. The magnet insertion hole 51 is formed from one end to the other end in the axial direction of the rotor core 50. Each magnet insertion hole 51 corresponds to one magnetic pole. Here, the number of the magnet insertion holes 51 is 6, and thus the number of the magnetic poles is 6. However, the number of magnetic poles is not limited to 6, and two or more magnetic poles may be used.

The magnet insertion hole 51 extends linearly in a plane orthogonal to the axis C1. One permanent magnet 55 is disposed in each magnet insertion hole 51. The permanent magnets 55 disposed in the adjacent magnet insertion holes 51 are magnetized so that opposite poles thereof face radially outward.

The permanent magnet 55 is a flat plate-like member that is long in the axial direction, has a width in the circumferential direction of the rotor core 50, and has a thickness in the radial direction. The thickness of the permanent magnet 55 is, for example, 2 mm. The permanent magnet 55 is made of, for example, a rare earth magnet containing neodymium (Nd), iron (Fe), and boron (B). The permanent magnet 55 is magnetized in the thickness direction.

The rare-earth magnet has a property that the coercive force decreases with an increase in temperature, and the rate of decrease is-0.5 to-0.6%/K. In order to prevent demagnetization of a rare earth magnet when a maximum load expected in a compressor occurs, a coercive force of 1100 to 1500A/m is required. In order to ensure the coercive force at an ambient temperature of 150 ℃, the coercive force at normal temperature (20 ℃) needs to be 1800 to 2300A/m.

Therefore, dysprosium (Dy) may be added to the rare earth magnet. The coercive force of the rare earth magnet at room temperature was 1800A/m without Dy added thereto, and was 2300A/m by 2 wt% of Dy added thereto. However, the addition of Dy causes an increase in manufacturing cost and also causes a decrease in residual magnetic flux density. Therefore, it is preferable to reduce the amount of Dy added as much as possible or to add no Dy.

The magnet insertion hole 51 may be V-shaped with its circumferential center protruding radially inward. In this case, two permanent magnets 55 can be disposed in each magnet insertion hole 51.

Flux barriers 52 as leakage flux suppression holes are formed at both circumferential end portions of the magnet insertion hole 51. The flux barriers 52 suppress leakage flux between adjacent magnetic poles. The core portion between the flux barrier 52 and the outer periphery of the rotor core 50 becomes a thin portion for suppressing short-circuiting of magnetic fluxes between adjacent magnetic poles. The thickness of the thin portion is preferably the same as the thickness of the laminated steel sheets of the rotor core 50.

A slit 53 is formed radially outside the magnet insertion hole 51. The slits 53 are used to smooth the distribution of magnetic flux from the permanent magnets 55 to the stator 1 and suppress torque ripple. The number, arrangement and shape of the slits 53 are arbitrary. Further, the rotor core 50 may not have the slit 53.

Holes 57 and 58, which serve as passages for the refrigerant of the compressor 500 (fig. 23), are formed radially inside the magnet insertion hole 51. The hole 57 is formed at a position corresponding to the inter-electrode gap, and the hole 58 is formed at a position corresponding to the center of the electrode. However, the arrangement of the holes 57 and 58 can be changed as appropriate.

< construction of stator >

The stator 1 includes a stator core 10, an insulator 20 and an insulating film 25 attached to the stator core 10, and a coil 15 wound around the stator core 10 via the insulator 20 and the insulating film 25.

Fig. 2 is a cross-sectional view showing the stator core 10 and the housing 3. The stator core 10 is a member in which laminated steel plates 14 (fig. 3) are laminated in the axial direction and integrally fixed by a caulking portion 17. The laminated steel sheet 14 is, for example, an electromagnetic steel sheet. The thickness of the laminated steel sheet 14 is, for example, 0.1 to 0.7mm, and herein is 0.35 mm.

Stator core 10 includes an annular yoke 11 centered on axis C1, and a plurality of teeth 12 extending radially inward from yoke 11. The yoke 11 has an inner peripheral surface 11a and an outer peripheral surface 11b, and the outer peripheral surface 11b of the yoke 11 is fixed to the inner peripheral surface of the housing 3. The outer peripheral surface 11b of the yoke 11 forms the outer peripheral surface of the stator core 10.

The teeth 12 are formed at constant intervals in the circumferential direction. Here, the number of teeth 12 is 9, but it is only necessary to be 2 or more. A slot 13 for accommodating a coil 15 is formed between adjacent teeth 12.

The stator core 10 has a structure in which a plurality of divided cores 8 are connected in the circumferential direction by teeth 12. The number of the split cores 8 is, for example, 9. These split cores 8 are joined to each other at split surface portions 16 formed in the yoke 11. The split surface portion 16 is formed at, for example, an intermediate position between the circumferentially adjacent teeth 12.

The split cores 8 are joined to each other by welding at the split surface portions 16. The joining of the split cores 8 is not limited to welding, and for example, concave and convex portions may be formed on the split surface portions 16 and fitted to each other.

Fig. 3 is a perspective view showing the segment core 8. The teeth 12 have an extension 12b extending radially inward from the yoke 11 and a tooth tip 12a facing the rotor 5 (fig. 1). The circumferential width of the extending portion 12b is constant in the radial direction, and the circumferential width of the tooth tip portion 12a is wider than the extending portion 12 b. The side surfaces of the extended portions 12b of the teeth 12 and the inner peripheral surface 11a of the yoke 11 face the groove 13.

The yoke 11 is formed with a caulking portion 17. The caulking portion 17 integrally fixes the plurality of laminated steel plates 14 constituting the split core 8. The caulking portions 17 are formed at two positions symmetrical with respect to the circumferential center of the teeth 12. However, the number and arrangement of the caulking portions 17 can be changed as appropriate.

A recess 18 is formed in the outer peripheral surface 11b of the yoke 11 at a position corresponding to the circumferential center of the tooth 12. The recess 18 is a portion to which the caulking portion 34 (fig. 11) of the housing 3 is engaged, and also functions as a passage for the refrigerant in the compressor 500 (fig. 23).

Fig. 4 is a perspective view showing the divided core 8, and the insulator 20 and the insulating film 25 attached to the divided core 8. The insulators 20 are attached to both ends of the stator core 10 in the axial direction, respectively. The insulating member 20 is made of resin such as polybutylene terephthalate (PBT).

Each insulator 20 has a wall portion 23 attached to the yoke 11, a body portion 22 attached to the extension portion 12b (fig. 3) of the tooth 12, and a flange portion 21 attached to the tooth top portion 12 a.

The coil 15 (fig. 1) is wound around the body portion 22. The flange portion 21 and the wall portion 23 guide the coil 15 wound around the body portion 22 from both sides in the radial direction. The flange portion 21 and the wall portion 23 may be provided with a step portion for positioning the coil 15 wound around the body portion 22.

Holes 19 are formed at both axial ends of the teeth 12 (fig. 3). Each insulator 20 has a protruding portion fitted into the hole 19. The protrusion of the insulator 20 is fitted into the hole 19 of the tooth 12, whereby the insulator 20 is fixed to the tooth 12.

An insulating film 25 is attached to the side surface of the extending portion 12b (fig. 3) of the tooth 12 and the inner peripheral surface 11a (fig. 3) of the yoke 11. The insulating film 25 is made of, for example, polyethylene terephthalate (PET) resin. The insulator 20 and the insulating film 25 constitute an insulating portion that electrically insulates the stator core 10 from the coil 15.

Returning to fig. 1, the coil 15 is made of, for example, a magnetic wire, and is wound around the teeth 12 via the insulator 20 and the insulating film 25. The wire diameter of the coil 15 is, for example, 1.0 mm. The coil 15 is wound on each tooth 12 by concentrated winding, for example, 80 turns. The wire diameter and the number of turns of the coil 15 are determined according to a required rotation speed, torque, applied voltage, or area of the slot 13.

Fig. 5 is a longitudinal sectional view showing the motor 100. The stator 1 is fixed inside the annular housing 3. More specifically, the stator core 10 of the stator 1 is fitted to the inside of the housing 3 by shrink fitting or press fitting. Casing 3 is a part of hermetic container 507 in which compressor 500 (fig. 23) of motor 100 is mounted. The length of the housing 3 in the axial direction is longer than the length of the stator 1 in the axial direction.

Fig. 6 is a longitudinal sectional view showing the stator core 10 and the housing 3. The housing 3 includes a first housing portion 31, a second housing portion 32, and a third housing portion 33 in the axial direction. The first housing portion 31 is radially opposed to the stator core 10 and has an inner diameter D1. The second housing portion 32 abuts the stator core 10 and has an inner diameter D2 smaller than the inner diameter D1. The third housing part 33 protrudes from the stator core 10 in the axial direction, and has an inner diameter D3 smaller than the inner diameter D1.

The first housing portion 31 is formed at a position corresponding to the axial center portion of the stator core 10. The second housing portion 32 is formed on each of the axial sides of the first housing portion 31. The third housing portion 33 is formed on each of the axial sides of the second housing portion 32.

The inner peripheral surface 31a of the first housing portion 31 is radially separated from the outer peripheral surface 11b of the stator core 10. The inner peripheral surface 32a of the second housing portion 32 radially abuts against the outer peripheral surface 11b of the stator core 10. The inner peripheral surface 33a of the third housing portion 33 does not radially face the outer peripheral surface 11b of the stator core 10.

The first housing portion 31 is obtained by forming a recess 35 in the inner peripheral surface of the housing 3. The recess 35 is formed by, for example, cutting a cylindrical case having a constant thickness from the inner peripheral side. Instead of the cutting, the later-described pipe expanding process (fig. 8(a) and (B)) may be used. The recess 35 has a depth d in the radial direction centered on the axis C1. The depth d is constant in the axial direction, but may not be constant.

Here, the outer peripheral surface 36 of the case 3 is a cylindrical surface. However, when the recess 35 is formed by pipe expanding, the first housing portion 31 has a shape in which the outer peripheral surface 36 bulges outward in the radial direction (see fig. 8B).

The stator core 10 includes a first core portion 101 radially opposed to the first housing portion 31 and a second core portion 102 abutting against the second housing portion 32 in the axial direction. The first core 101 is located at an axial center portion of the stator core 10, and the second cores 102 are located on both axial sides of the first core 101, respectively. The first core portion 101 and the second core portion 102 are formed of laminated steel sheets having the same shape, and have the same outer diameter.

As described above, the stator core 10 is fitted to the housing 3 by shrink fitting or press fitting. Specifically, the second core portion 102 of the stator core 10 is fitted inside the second housing portion 32 of the housing 3. The first core portion 101 of the stator core 10 faces the first housing portion 31 of the housing 3, but does not abut. Therefore, the first core portion 101 is not subjected to the compressive stress from the case 3, thereby suppressing the change in magnetic characteristics due to the compressive stress and reducing the iron loss.

< method for manufacturing Motor >

Next, a method for manufacturing the motor 100 will be described. Fig. 7 is a flowchart showing a manufacturing process of the motor 100. First, a plurality of laminated elements are stacked in the axial direction and integrally fixed by the caulking portions 17 to form the split core 8 shown in fig. 3 (step S101). Next, the insulator 20 and the insulating film 25 (fig. 3) as insulating portions are attached to the split core 8, and the coil 15 is wound around the tooth 12 via the insulating portions (step S102). Then, the plurality of split cores 8 are joined by welding or the like to form the stator core 10 (step S103). Thereby, the stator 1 is formed.

On the other hand, a recess 35 is formed in advance in the housing 3 to which the stator 1 is attached. As described above, the concave portion 35 is formed by cutting the inner peripheral surface of the cylindrical housing 3. However, the pipe expanding process may be used without being limited to the cutting process.

Fig. 8(a) and (B) are schematic views for explaining the pipe expanding process. In the pipe expanding process, as shown in fig. 8(a), the disk-shaped tool 7 is fitted inside the portion of the housing 3 where the recess 35 is formed. Then, as shown in fig. 8(B), the tool 7 is heated and expanded. Thereby, the outer peripheral end 71 of the tool 7 presses the housing 3 radially outward, and the housing 3 is plastically deformed radially outward. Thereafter, the tool 7 is air-cooled and pulled out of the housing 3. Thereby, the recess 35 is formed in the housing 3.

The stator 1 is fixed by shrink fitting to the housing 3 formed with the recess 35 formed in this way (step S104). Fig. 9(a) and (B) are schematic diagrams for explaining the hot charging step. In the shrink-fitting step, as shown in fig. 9(a), the housing 3 is heated and thermally expanded so that the inner diameter D0 of the housing 3 is larger than the outer diameter DS of the stator core 10. In this state, the stator 1 is inserted into the inside of the housing 3.

After that, by cooling the housing 3, the inner diameter of the housing 3 is contracted as shown in fig. 9 (B). Thereby, the outer peripheral surface 11b of the stator core 10 is fitted to the inner peripheral surface of the housing 3.

Fig. 10 is a view showing the stator 1 and the housing 3 after the shrink fitting. Since the second housing portion 32 abuts the stator core 10, the inner diameter D2 of the second housing portion 32 is the same as the outer diameter DS of the stator core 10. In contrast, since the third housing portion 33 does not abut on the stator core 10, the inner diameter D3 of the third housing portion 33 may be equal to or smaller than the outer diameter DS of the stator core 10.

Therefore, as shown in fig. 10, inner diameter D3 of third case portion 33 is equal to or smaller than inner diameter D2 of second case portion 32 (D2 ≧ D3), and more preferably smaller than inner diameter D2(D2> D3). Thus, the third housing portion 33 effectively functions as a coming-off prevention portion that prevents the stator 1 from coming off the housing 3 in the axial direction.

Further, without being limited to the configuration shown in fig. 10, if the inner diameter D3 of the third housing part 33 is smaller than the inner diameter D1 of the first housing part 31 (D1> D3), a certain retaining effect of the stator 1 can be expected.

Here, the case where the stator core 10 and the housing 3 are fitted by shrink fitting has been described, but press fitting may be used instead of shrink fitting, for example.

As shown in fig. 11, the fitting portion of the stator core 10 and the housing 3 is preferably fixed by hot caulking. Here, heat and force P are applied from the outer peripheral surface 36 to the second housing portion 32 of the housing 3 at a portion corresponding to the recess 18 of the stator core 10. Thereby, a part of the case 3 is deformed radially inward to form a caulking portion 34, and the caulking portion 34 is engaged with the concave portion 18 of the stator core 10.

The caulking portion 34 of the case 3 is engaged with the recess 18 of the stator core 10, thereby preventing the positional deviation between the case 3 and the stator 1 in the circumferential direction. It is preferable that all the positions corresponding to the recesses 18 be heat-staked, but it may be performed at least at one location in the circumferential direction of the stator core 10.

On the other hand, the rotor core 50 is formed by laminating a plurality of laminated elements in the axial direction, and the permanent magnets 55 are inserted into the magnet insertion holes 51, thereby forming the rotor 5. The rotor 5 is attached to the inside of the stator 1 fixed to the housing 3 (step S105 in fig. 7). Thereafter, the case 3 is sealed (step S106). Thereby, the motor 100 including the stator 1, the rotor 5, and the housing 3 is completed.

< action >

Next, the operation of the motor 100 according to embodiment 1 will be described. The energy consumed in a core such as a stator core when the magnetic flux changes in the core is referred to as an iron loss. Since the variation of the magnetic flux is small in the rotor core 50, most of the iron loss in the motor 100 is the iron loss in the stator core 10. The core loss is expressed by the sum of the hysteresis loss and the eddy current loss. Hysteresis loss is proportional to the frequency of the flux change and eddy current loss is proportional to the square of the frequency.

In the motor 100 using the permanent magnet 55, the proportion of the iron loss in the total loss is larger than that in a motor not using a permanent magnet, such as an induction motor. That is, when the magnetic flux generated in the permanent magnet 55 flows through the stator core 10, iron loss corresponding to the change in the magnetic flux is generated.

When a current is caused to flow through the coil 15, a high-frequency magnetic flux component is generated due to the overlap of the magnetic flux generated by the permanent magnet 55 and the magnetic flux generated by the current flowing through the coil 15. As described above, since the hysteresis loss is proportional to the frequency of the change in magnetic flux and the eddy current loss is proportional to the square of the frequency, the iron loss increases as the magnetic flux becomes higher.

Fig. 12 is a longitudinal sectional view showing a motor of a comparative example of the motor 100 according to embodiment 1. In the motor of the comparative example, the housing 3H of the comparative example does not have the recess 35 (fig. 5) described in embodiment 1, and the inner diameter D4 is constant in the axial direction. Therefore, the entire outer peripheral surface 11b of the stator core 10 abuts against the housing 3H.

Since stator core 10 is fitted to housing 3H by shrink fitting or press fitting, it receives a compressive stress from housing 3H. The product of the contact area between the stator core 10 and the housing 3H and the average stress acting on the area is defined as the heat load. The thermal load is an index of the fixing force of the stator core 10 to the housing 3H.

When a core material such as an electromagnetic steel sheet constituting the stator core 10 is subjected to a compressive stress, magnetic characteristics change, and iron loss increases. In the motor of the comparative example shown in fig. 12, since the entire outer peripheral surface 11b of the stator core 10 is fitted into the housing 3H, iron loss increases in the entire stator core 10, and as a result, motor efficiency decreases.

In contrast, in motor 100 according to embodiment 1, first core portion 101 of stator core 10 does not abut against housing 3 and is not subjected to compressive stress, as shown in fig. 6, and therefore, an increase in iron loss in first core portion 101 is hardly generated. Therefore, the motor efficiency can be improved as compared with the motor of the comparative example.

Here, the effect of reducing the iron loss in embodiment 1 will be described with specific numerical values. The core loss per unit volume of the stator core 10 of the motor of the comparative example before hot-fitting and press-fitting was set to 1. Further, it is assumed that the iron loss in the stator core 10 increases to 2 by shrink fitting or press fitting.

In the motor 100 of embodiment 1, it is assumed that the first core portion 101 occupies 50% of the axial length of the stator core 10. In this case, the contact area between the stator core 10 and the housing 3 is half of that in the comparative example. When the thermal load is set to be the same as the comparative example, a compressive stress 2 times as large as that of the comparative example acts on the second core portion 102.

Since the first core portion 101 is not subjected to compressive stress from the case 3, the core loss per unit volume in the first core portion 101 can be considered to be 1. On the other hand, the second core portion 102 receives a compressive stress from the case 3, the magnitude of which is 2 times that of the comparative example.

Fig. 13 is a graph showing a relationship between the compressive stress received by the stator core 10 and the rate of increase in iron loss per unit volume in the stator core 10. The iron loss increase rate is a relative value of the iron loss with the iron loss at the compressive stress of 0 as a reference (i.e., 1). As described above, the core loss per unit volume in the stator core 10 of the comparative example is 2.

As shown in fig. 13, as the compressive stress increases, the iron loss also increases, but the rate of increase in the iron loss gradually saturates. Therefore, in the second core portion 102 of embodiment 1 in which the compressive stress is large, saturation of the core loss occurs. As a result, the iron loss per unit volume in the second core portion 102 becomes a value smaller than 2 times that of the comparative example.

When the core loss per unit volume in the second core portion 102 is assumed to be 2.4, which is 1.2 times that of the comparative example, the average value of the core losses per unit volume of the stator cores 10 that occupy 50% of each of the first and second core portions 101 and 102 is (2.4 × 0.5) + (1 × 0.5) ═ 1.7. This value is smaller than the iron loss per unit volume (═ 2) of the stator core 10 of the comparative example. That is, it is understood that the motor 100 according to embodiment 1 can obtain an effect of reducing the iron loss.

Fig. 14 is a graph showing a relationship between the breakout load and the rate of increase in iron loss per unit volume in the stator core 10. The disengagement load is a load required to pull the stator 1 out of the housing 3 in the axial direction. Fig. 15 is a graph showing a relationship between the hot-load and the rate of increase in iron loss per unit volume in the stator core 10. In each of the graphs, the iron loss increase rate is a relative value of the iron loss with the iron loss at the load of 0 as a reference (i.e., 1).

As is clear from fig. 14 and 15, the iron loss shows the same tendency with respect to the detachment load and the hot-load. In the stator core 10 of embodiment 1, since stress is concentrated on the second core portion 102, saturation of the core loss occurs under a detachment load and a thermal loading load smaller than those of the stator core 10 of the comparative example. The increase in core loss is small relative to the increase in breakout load and hot-load.

Therefore, according to embodiment 1, it is possible to firmly fix the stator core 10 to the housing 3 and suppress an increase in the iron loss. In other words, the iron loss in the stator core 10 can be reduced by utilizing saturation of the iron loss accompanying the concentration of stress to the second core portion 102.

In motor 100 according to embodiment 1, both axial ends of stator core 10 are fitted to housing 3. Therefore, the stator 1 can be supported in a stable state, and vibration and noise can be suppressed.

The stator core 10 is formed of a laminated body of laminated steel plates, but is easily deformed in the lamination direction, i.e., the axial direction, due to the expansion and contraction of the lamination gap. By fitting both axial ends of the stator core 10 into the housing 3, deformation of the stator core 10 in the axial direction can be suppressed, and vibration and noise can be suppressed.

Further, since the magnetic flux from the rotor 5 easily flows into the first core portion 101 at the axial center portion of the stator core 10, the magnetic flux density is higher than that of the second core portions 102 at the axial end portions. Since the first core 101 faces the first housing 31 of the housing 3, it is not subjected to a compressive stress, and therefore, the effect of reducing the iron loss can be enhanced.

Further, as described above, since the compressive stress is concentrated on the second core portion 102, the close contact between the case 3 and the second core portion 102 can be improved. This can improve the fixing force when fixing the housing 3 and the stator core 10 by hot caulking (fig. 11) or arc welding (fig. 17). Alternatively, the stator core 10 can be fitted to the housing 3 with a smaller thermal load by caulking or arc welding, and the effect of reducing the iron loss can be further improved.

Further, since the stator core 10 is formed of the plurality of split cores 8, the coils 15 are easily wound around the teeth 12 at high density, and on the other hand, it is difficult to improve the roundness of the stator core 10. In embodiment 1, since the second core portion 102 of the stator core 10 is subjected to a high compressive stress, the stator core 10 is firmly fastened. Thereby, the adjacent divided cores 8 are firmly pressed against each other and positioned at the correct relative positions. As a result, the roundness of the stator core 10 can be improved.

< effects of the embodiment >

As described above, in embodiment 1, the housing 3 includes the first housing portion 31 facing the stator core 10 in the radial direction, the second housing portion 32 abutting the stator core 10 in the radial direction, and the third housing portion 33 protruding from the stator core 10 in the axial direction, and the inner diameters D1, D2, and D3 of the housing portions 31, 32, and 33 satisfy D1> D2 and D1> D3. Therefore, the stator core 10 can be firmly fixed to the housing 3 by the abutment of the second housing portion 32 with the stator core 10. In addition, since the stator core 10 does not receive a compressive stress from the first housing portion 31, it is possible to reduce iron loss in the stator core 10 and improve motor efficiency. In addition, the third housing portion 33 can suppress the stator core 10 from being detached from the housing 3.

Further, the inner diameters D2, D3 of the second case portion 32 and the third case portion 33 satisfy D2 ≧ D3, whereby the stator core 10 can be effectively prevented from coming off the case 3.

Further, since the first case portion 31 of the case 3 has the recess 35 on the side facing the stator core 10, the case 3 satisfying D1> D2 can be formed by a simple process such as cutting.

Further, since the stator core 10 and the case 3 are fixed to each other by heat caulking (caulking portion 34), the fixing strength of the stator core 10 and the case 3 can be improved.

Further, by the structure in which the stator core 10 is fastened by the second housing portion 32 of the housing 3, a high degree of roundness can be obtained even in the case of the stator core 10 configured by the plurality of split cores 8.

Further, since the first housing portion 31 of the housing 3 is formed at a position corresponding to the axial center portion of the stator core 10 where the magnetic flux from the rotor 5 flows at the maximum, the effect of reducing the iron loss can be enhanced.

Further, since the second housing portion 32 of the housing 3 abuts against the axial end portion of the stator core 10, it is possible to suppress deformation of the stator core 10 and reduce vibration and noise.

Modification examples.

Fig. 16 is a vertical cross-sectional view showing a stator core 10 and a housing 3A according to a modification of embodiment 1. In embodiment 1 described above, the depth d of the recess 35 (fig. 6) of the first housing portion 31 is constant in the axial direction. In contrast, the depth d of the recess 37 of the first housing portion 31 of the modified example changes in the axial direction.

More specifically, the depth d of the recess 37 is maximized at the axial center. However, the position where the depth d of the recess 37 is maximized is not limited to the axial center, and may be, for example, an axial end. The concave portion 37 can be formed by the cutting or pipe expanding process described in embodiment 1.

In this modification as well, the first housing portion 31 of the housing 3A has the recess 37 and does not abut against the stator core 10. Therefore, the compressive stress does not act on the first core portion 101 of the stator core 10, and the iron loss in the stator core 10 can be reduced.

Embodiment 2.

Fig. 17 is a cross-sectional view showing stator core 10 and housing 3B according to embodiment 2. In embodiment 1 described above, as shown in fig. 11, the fitting portion between the stator core 10 and the housing 3 is fixed by heat caulking. In embodiment 2, the fitting portion between the stator core 10 and the housing 3B is fixed by arc spot welding.

As described in embodiment 1, the stator core 10 is configured by the plurality of split cores 8. The arc spot welding is performed at a position where the divided surface portion 16 of the divided core 8 and the inner peripheral surface 32a of the second case portion 32 of the case 3B intersect. Thereby, the welded portion W is formed at the position where the divided surface portion 16 intersects the inner peripheral surface 32a of the case 3B.

As described in embodiment 1, since the stator core 10 is firmly fastened by the second housing portion 32, the fixing strength of the arc spot welding of the stator core 10 and the housing 3B can be improved.

The motor of embodiment 2 is configured in the same manner as the motor 100 of embodiment 1, except for the above-described points.

In embodiment 2, since the stator core 10 and the housing 3B are fixed to each other by arc spot welding, the fixing strength of the stator core 10 and the housing 3B can be improved.

Embodiment 3.

Fig. 18 is a longitudinal sectional view showing stator core 10 and housing 3C according to embodiment 3. In embodiment 1 described above, the first housing portion 31 of the housing 3 is formed at a position corresponding to the axial center portion of the stator core 10, and the second housing portion 32 is formed at a position corresponding to the axial both end portions of the stator core 10.

The housing 3C of embodiment 3 has second housing portions 32 at positions corresponding to the axial center portion and the axial both end portions of the stator core 10. In other words, the housing 3C abuts against the axial center portion and the axial both end portions of the stator core 10.

The housing 3C has the first housing portion 31 on both axial sides of the second housing portion 32 in the axial center portion. The first housing portion 31 is obtained by forming a recess 35 in the inner periphery of the housing 3C. Instead of the recess 35, a recess 37 shown in fig. 16 may be formed.

The stator core 10 has a first core portion 101 radially opposed to the first housing portion 31 and a second core portion 102 contacting the second housing portion 32. The second core portions 102 are located at the axial center and both axial ends of the stator core 10, and the first core portions 101 are located at the axial center and on both axial sides of the second core portions 102.

That is, in embodiment 3, the axial center portion and the axial both end portions of the stator core 10 are fitted to the housing 3C. The fitting portion between the stator core 10 and the housing 3C may be fixed by hot caulking as shown in fig. 11 or may be fixed by arc spot welding as shown in fig. 17.

The motor of embodiment 3 is configured in the same manner as the motor 100 of embodiment 1, except for the above-described points.

In embodiment 3, the axial center portion and the axial both end portions of the stator core 10 are fitted to the housing 3. Therefore, the stator core 10 can be firmly fixed to the housing 3, deformation of the stator core 10 can be suppressed, and vibration and noise can be reduced. In addition, since the first housing portion 31 does not receive a compressive stress from the stator core 10, the iron loss in the stator core 10 can be reduced.

Embodiment 4.

Fig. 19 is a vertical sectional view showing stator core 10 and housing 3D according to embodiment 4. In embodiment 1 described above, the first housing portion 31 of the housing 3 is formed at a position corresponding to the axial center portion of the stator core 10, and the second housing portion 32 is formed at a position corresponding to the axial both end portions of the stator core 10.

The housing 3D according to embodiment 4 includes a second housing portion 32 at a position corresponding to the axial center portion of the stator core 10. In other words, the housing 3 abuts against the axial center portion of the stator core 10.

The housing 3D has the first housing portion 31 on both sides in the axial direction of the second housing portion 32. The first housing portion 31 is obtained by forming a recess 35 on the inner periphery of the housing 3. Instead of the recess 35, a recess 37 shown in fig. 16 may be formed.

The stator core 10 has a first core portion 101 radially opposed to the first housing portion 31 and a second core portion 102 contacting the second housing portion 32. The second core portions 102 are respectively located at the axial center portions of the stator cores 10, and the first core portions 101 are respectively located at both axial sides of the second core portions 102.

That is, in embodiment 4, the axial center portion of the stator core 10 is fitted to the housing 3D. The fitting portion between the stator core 10 and the housing 3D may be fixed by hot caulking as shown in fig. 11 or may be fixed by arc spot welding as shown in fig. 17.

The motor of embodiment 4 is configured in the same manner as the motor 100 of embodiment 1, except for the above-described points.

In embodiment 4, since the axial center portion of the stator core 10 is fitted to the housing 3D, stress can be concentrated on the axial center portion of the stator core 10, and the stator core 10 can be firmly fixed to the housing 3. In addition, since the first housing portion 31 does not receive a compressive stress from the stator core 10, the iron loss in the stator core 10 can be reduced.

Embodiment 5.

Fig. 20 is a vertical sectional view showing stator core 10 and case 3E according to embodiment 5. In embodiment 5, as in embodiment 1, the first housing portion 31 of the housing 3E is formed at a position corresponding to the axial center portion of the stator core 10, and the second housing portions 32 are formed at positions corresponding to the axial end portions of the stator core 10. The first housing portion 31 is obtained by forming a recess 35 in the inner peripheral surface of the housing 3E. Instead of the recess 35, a recess 37 shown in fig. 16 may be formed.

The stator core 10 has a first core portion 101 radially opposed to the first housing portion 31 and a second core portion 102 contacting the second housing portion 32. The first core portion 101 is located at an axial center portion of the stator core 10, and the second core portions 102 are located at axial both end portions of the stator core 10, respectively.

The first housing portion 31 has a length L1 in the axial direction. The two second housing parts 32 each have a length L2 in the axial direction. The length L1 of the first case 31 is longer than the total length L2 × 2 of the length L2 of the second case 32. Namely, L1> L2 × 2 holds. In other words, the area of the inner peripheral surface 31a of the first housing portion 31 is larger than the total of the areas of the inner peripheral surfaces 32a of the second housing portion 32.

The above-described length L1 is also the length in the axial direction of the first core portion 101. The above-described length L2 is also the length in the axial direction of the second core portion 102. Therefore, the length L1 of the first core part 101 is longer than the total L2 × 2 of the length L2 of the second core part 102, and the area of the outer peripheral surface of the first core part 101 is larger than the total area of the outer peripheral surfaces of the second core part 102.

In this way, the area of the inner peripheral surface 31a of the first housing portion 31, that is, the area of the surface of the housing 3E that does not abut against the stator core 10 is large, and therefore the effect of reducing the iron loss can be improved. Further, since the area of the inner peripheral surface 32a of the second case portion 32, that is, the area of the surface of the case 3E that contacts the stator core 10 is small, the compressive stress can be concentrated, and the stator core 10 can be firmly fixed to the case 3E.

The motor according to embodiment 5 is configured in the same manner as the motor 100 according to embodiment 1, except for the above-described points.

In embodiment 5, the area of the inner peripheral surface 31a of the first housing part 31 is larger than the area of the inner peripheral surface 32a of the second housing part 32, so that the effect of reducing the iron loss can be enhanced. In addition, the stator core 10 can be firmly fixed to the housing 3E by concentration of the compressive stress.

The case portions 31 and 32 of the case 3E may be arranged as described in embodiment 3 (fig. 18) and embodiment 4 (fig. 19). In this case, the total area of the surfaces of the stator core 10 facing the housing 3 may be larger than the total area of the surfaces in contact with the housing 3. The fitting portion between the stator core 10 and the housing 3E may be fixed by heat caulking or arc spot welding.

Embodiment 6.

Fig. 21(a) is a front view showing an inner peripheral surface of a housing 3F of embodiment 6. In embodiment 1 described above, the first case portion 31 of the case 3 is formed with the recess 35 (fig. 6). In contrast, in embodiment 6, a plurality of grooves 38 are formed in the inner peripheral surface of the housing 3F. Here, the groove portion 38 is formed in a lattice shape extending in the axial direction and the circumferential direction, but is not limited to this pattern.

The groove 38 of the case 3F does not abut on the outer peripheral surface of the stator core 10. That is, the stator core 10 is not subjected to compressive stress from the groove portion 38 of the housing 3F. Therefore, an effect of reducing the iron loss in the stator core 10 can be obtained.

In embodiment 6, the groove 38 in the inner peripheral surface of the housing 3F serves as the first housing part 31, and the portion other than the groove 38 serves as the second housing part 32. The third housing portion 33 (fig. 6) is as described in embodiment 1.

The motor of embodiment 6 is configured in the same manner as the motor 100 of embodiment 1, except for the above-described points.

Instead of forming the groove 38 in the inner peripheral surface of the housing 3F, the surface roughness of the inner peripheral surface of the housing 3F may be increased to form a concave-convex portion. Since the concave portion of the uneven portion does not abut on the outer peripheral surface of the stator core 10, an effect of reducing the iron loss can be obtained. Fig. 21(B) is a diagram showing an example of the surface roughness of the concave-convex portion.

In this case, the average roughness Ra of the inner peripheral surface of the case 3F before the shrink-fitting process (step S103 shown in fig. 7) is made larger than the interference in the shrink-fitting process. The interference is a value obtained by subtracting the inner diameter of the housing 3F before the stator core 10 is fixed from the outer diameter DS (fig. 9) of the stator core 10.

Thus, after stator core 10 is fixed to case 3F by shrink fitting, the uneven portions on the inner circumferential surface of case 3F remain without being crushed. Therefore, a portion that does not receive compressive stress from the case 3F can be provided on the outer peripheral surface of the stator core 10, and the iron loss can be reduced.

In embodiment 6, by providing the groove portion 38 or the uneven portion on the inner peripheral surface of the case 3F, it is possible to dispersedly provide a portion that does not receive the compressive stress from the case 3F on the outer peripheral surface of the stator core 10. Therefore, it is possible to reduce the iron loss in the stator core 10 and firmly fix the stator core 10 to the case 3E.

The groove 38 or the concave-convex portion described in embodiment 6 may be provided on the inner peripheral surface 32a of the second case portion 32 described in embodiments 1, 3, and 4. As described in embodiment 5, the total area of the surfaces of the case 3F facing the stator core 10 may be larger than the total area of the surfaces in contact with the case 3F. The fitting portion of the stator core 10 and the housing 3F may be fixed by heat caulking or arc spot welding.

Modification examples.

Fig. 22 is a cross-sectional view showing another configuration example of the stator core 10 according to embodiments 1 to 6 together with the housing 3. The stator core 10 (fig. 2) described in each of the above embodiments is configured by a plurality of split cores 8. The stator core 10A shown in fig. 22 is configured by a plurality of coupling cores 9 coupled to each other at the outer periphery of the yoke 11.

The connecting core 9 is arranged according to the teeth 12. The yoke 11 is formed with a split surface portion 91 that serves as a boundary between adjacent coupling cores 9. The split surface portion 91 extends radially outward from the inner peripheral surface of the yoke 11, but does not reach the outer peripheral surface 11b of the yoke 11. A thin portion 92 is formed between the end of the dividing surface 91 and the outer peripheral surface 11b of the yoke 11.

Therefore, the strip-shaped body in which the plurality of connecting cores 9 are connected in a row can be rolled into a ring shape while deforming the thin portions 92. The two coupling cores 9 located at the end portions of the strip are joined to each other by a weld W.

The plurality of coupled cores 9 of the stator core 10A are coupled by the thin-walled portion 92, but it is difficult to improve the roundness compared with a stator core integrally formed in a ring shape. In each of the above embodiments, since the compressive stress from the case 3 is concentrated on the second core portion 102 of the stator core 10 and the stator core 10 is firmly fastened, the improvement of the roundness is easy.

The stator core is not limited to the member constituted by the split core 8 (fig. 2) or the coupling core 9 (fig. 22), and may be integrally formed in a ring shape.

< Structure of compressor >

Next, a compressor 500 to which the motor of each embodiment can be applied will be described. Fig. 23 is a longitudinal sectional view showing the compressor 500. The compressor 500 is a rotary compressor, and is used, for example, in the air conditioner 400 (fig. 24). The compressor 500 includes a compression mechanism 501, a motor 100 for driving the compression mechanism 501, a shaft 56 for connecting the compression mechanism 501 and the motor 100, and a hermetic container 507 for storing them. Here, the axial direction of the shaft 56 is the vertical direction, and the electric motor 100 is disposed above the compression mechanism 501.

The closed casing 507 is a steel plate-made casing, and has a cylindrical casing 3, a casing upper portion covering the upper side of the casing 3, and a casing bottom portion covering the lower side of the casing 3. Stator 1 of motor 100 is assembled inside the casing of hermetic container 507 by shrink fitting, press fitting, welding, or the like.

A discharge pipe 512 for discharging the refrigerant to the outside and a terminal 511 for supplying electric power to the motor 100 are provided in the upper part of the sealed container 507. Further, an accumulator 510 for storing refrigerant gas is attached to the outside of the closed casing 507. Refrigerating machine oil for lubricating the bearing portion of the compression mechanism 501 is stored in the bottom of the closed casing 507.

The compression mechanism 501 includes: a cylinder block 502 having a cylinder chamber 503, a rolling piston 504 fixed to the shaft 56, a vane that divides the interior of the cylinder chamber 503 into a suction side and a compression side, and an upper frame 505 and a lower frame 506 that close both axial end portions of the cylinder chamber 503.

Each of the upper frame 505 and the lower frame 506 has a bearing portion that rotatably supports the shaft 56. An upper discharge muffler 508 and a lower discharge muffler 509 are attached to the upper frame 505 and the lower frame 506, respectively.

The cylinder 502 is provided with a cylindrical cylinder chamber 503 centered on an axis C1. The eccentric shaft portion 56a of the shaft 56 is located inside the cylinder chamber 503. The eccentric shaft portion 56a has a center eccentric with respect to the axis C1. Rolling piston 504 is fitted to the outer periphery of eccentric shaft portion 56 a. When the motor 100 rotates, the eccentric shaft 56a and the rolling piston 504 eccentrically rotate in the cylinder chamber 503.

A suction port 515 for sucking the refrigerant gas into the cylinder chamber 503 is formed in the cylinder block 502. A suction pipe 513 is attached to the closed casing 507 and communicates with a suction port 515, and refrigerant gas is supplied from the accumulator 510 to the cylinder chamber 503 through the suction pipe 513.

The low-pressure refrigerant gas and the liquid refrigerant are mixed and supplied from the refrigerant circuit of the air conditioner 400 (fig. 24) to the compressor 500, but when the liquid refrigerant flows into the compression mechanism 501 and is compressed, the liquid refrigerant becomes a cause of a failure of the compression mechanism 501. Therefore, the liquid refrigerant is separated from the refrigerant gas in the accumulator 510, and only the refrigerant gas is supplied to the compression mechanism 501.

As the refrigerant, for example, R410A, R407C, R22, or the like can be used, but from the viewpoint of preventing global warming, a refrigerant having a low GWP (global warming potential) is preferably used.

The operation of the compressor 500 is as follows. When a current is supplied from the terminal 511 to the coil 15 of the stator 1, an attractive force and a repulsive force are generated between the stator 1 and the rotor 5 by a rotating magnetic field generated by the current and a magnetic field of the permanent magnet 55 of the rotor 5, and the rotor 5 rotates. Along with this, the shaft 56 fixed to the rotor 5 also rotates.

The low-pressure refrigerant gas is sucked from the accumulator 510 into the cylinder chamber 503 of the compression mechanism 501 through the suction port 515. In cylinder chamber 503, eccentric shaft portion 56a of shaft 56 and rolling piston 504 attached to eccentric shaft portion 56a rotate eccentrically, and the refrigerant is compressed in cylinder chamber 503.

The refrigerant compressed in the cylinder chamber 503 is discharged into the hermetic container 507 through a discharge port and discharge mufflers 508 and 509, which are not shown. The refrigerant discharged into sealed container 507 passes through holes 57 and 58 of rotor core 50, etc., rises in sealed container 507, is discharged from discharge pipe 512, and is sent to the refrigerant circuit of air conditioner 400 (fig. 24).

Since the compressor 500 can be applied to the motors described in embodiments 1 to 5 and the modifications, vibration and noise of the compressor 500 can be suppressed.

< air conditioner >

Next, an air conditioner 400 including the compressor 500 shown in fig. 23 will be described. Fig. 24 is a diagram showing an air conditioner 400. The air conditioner 400 includes the compressor 500 of embodiment 1, a four-way valve 401 as a switching valve, a condenser 402 for condensing the refrigerant, a pressure reducer 403 for reducing the pressure of the refrigerant, an evaporator 404 for evaporating the refrigerant, and a refrigerant pipe 410 connecting these components.

The compressor 500, the four-way valve 401, the condenser 402, the pressure reducing device 403, and the evaporator 404 are connected by a refrigerant pipe 410 to constitute a refrigerant circuit. The compressor 500 includes an outdoor fan 405 facing the condenser 402 and an indoor fan 406 facing the evaporator 404.

The air conditioner 400 operates as follows. The compressor 500 compresses a sucked refrigerant and sends the compressed refrigerant as a high-temperature and high-pressure refrigerant gas. Four-way valve 401 switches the flow direction of the refrigerant, and during the cooling operation, as shown in fig. 24, the refrigerant sent from compressor 500 flows to condenser 402.

The condenser 402 performs heat exchange between the refrigerant sent from the compressor 500 and the outdoor air blown by the outdoor air-sending device 405, condenses the refrigerant, and sends out the condensed refrigerant as a liquid refrigerant. The pressure reducing device 403 expands the liquid refrigerant sent from the condenser 402 and sends the expanded liquid refrigerant as a low-temperature low-pressure liquid refrigerant.

The evaporator 404 performs heat exchange between the low-temperature low-pressure liquid refrigerant sent from the pressure reducing device 403 and the indoor air, evaporates (vaporizes) the refrigerant, and sends out the refrigerant as a refrigerant gas. The air deprived of heat in the evaporator 404 is supplied to the room as the space to be air-conditioned by the indoor air-sending device 406.

In the heating operation, four-way valve 401 sends the refrigerant sent from compressor 500 to evaporator 404. In this case, the evaporator 404 functions as a condenser, and the condenser 402 functions as an evaporator.

Since the compressor 500 can suppress vibration and noise as described above, the quietness of the air conditioner 400 can be improved.

While the preferred embodiments of the present invention have been described above in detail, the present invention is not limited to the above embodiments, and various improvements and modifications can be made without departing from the scope of the present invention.

Description of reference numerals

1 stator, 3A, 3B, 3C, 3D, 3E, 3F, 3H case, 5 rotor, 7 tool, 8 divided core, 9 connected core, 10A stator core, 11 yoke, 12 teeth, 13 slots, 14 laminated steel plate, 15 coils, 16 divided face, 17 riveted part, 18 recess, 19 holes, 20 insulator, 25 insulating film, 31 first case, 32 second case, 33 third case, 34 riveted part, 35, 37 recess, 38 slots, 50 rotor core, 51 magnet insertion hole, 55 permanent magnet, 56 shaft, 100 motor, 101 first core, 102 second core, 400 air conditioner, four-way valve 401, 402 condenser, 403 decompressor, 404 evaporator, 405 outdoor blower, 406 indoor blower, 410 refrigerant piping, 500, 501 compression mechanism part, 507 closed container.

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