CN216642554U - Rotor assembly, air supply device and dust collector - Google Patents
Rotor assembly, air supply device and dust collector Download PDFInfo
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- CN216642554U CN216642554U CN202122793523.4U CN202122793523U CN216642554U CN 216642554 U CN216642554 U CN 216642554U CN 202122793523 U CN202122793523 U CN 202122793523U CN 216642554 U CN216642554 U CN 216642554U
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- outer diameter
- diameter portion
- impeller
- rotor assembly
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Abstract
The utility model provides a rotor assembly, an air supply device and a dust collector. The rotor assembly has: a shaft disposed along a central axis extending in the vertical direction; an impeller rotatable about the central axis; a rotor core; an upper bearing; and a lower bearing disposed below the upper bearing, the impeller, the rotor core, the upper bearing, and the lower bearing being fixed to the shaft, the shaft having a first outer diameter portion, a second outer diameter portion, a third outer diameter portion, and a fourth outer diameter portion, an outer diameter of the second outer diameter portion being larger than an outer diameter of the first outer diameter portion, an outer diameter of the third outer diameter portion being smaller than an outer diameter of the second outer diameter portion, and an outer diameter of the fourth outer diameter portion being smaller than an outer diameter of the third outer diameter portion.
Description
Technical Field
The utility model relates to a rotor assembly, an air supply device and a dust collector.
Background
Conventionally, there is known an electric blower including a motor, an impeller fixed to a rotating shaft of the motor and generating an air flow, and the like. (patent document 1)
Documents of the prior art
Patent document
Patent document 1: japanese patent laid-open publication No. 2011-157867
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved by the utility model
The motor shaft of the electric blower needs to be fixed to an impeller, a bearing, a rotor core, and the like to constitute a so-called rotor assembly. In this case, the workability of assembling the rotor assembly is improved, and the rotor assembly is reduced in size.
The utility model provides a rotor assembly capable of improving assembling workability and inhibiting size from increasing.
Technical scheme for solving technical problems
The rotor assembly of the exemplary embodiment of the present invention has: a shaft disposed along a central axis extending in the vertical direction; an impeller rotatable about the central axis; a rotor core; an upper bearing; and a lower bearing disposed below the upper bearing, the impeller, the rotor core, the upper bearing, and the lower bearing being fixed to the shaft, the shaft has a first outer diameter portion, a second outer diameter portion, a third outer diameter portion, and a fourth outer diameter portion, the impeller and the upper bearing are fixed to the first outer diameter portion, the second outer diameter portion is disposed below the first outer diameter portion, a rotor core is fixed to the third outer diameter portion, and the third outer diameter portion is disposed below the second outer diameter portion, the lower bearing is fixed to the fourth outer diameter portion, and the fourth outer diameter portion is disposed below the third outer diameter portion, the second outer diameter portion has an outer diameter larger than that of the first outer diameter portion, the third outer diameter portion has an outer diameter smaller than that of the second outer diameter portion, and the fourth outer diameter portion has an outer diameter smaller than that of the third outer diameter portion.
The third outer diameter portion may have an outer diameter larger than that of the first outer diameter portion.
A lower end portion of the first outer diameter portion and an upper end portion of the second outer diameter portion may be connected by a first connection portion that expands in a direction away from the central axis, and at least a part of a lower surface of the upper bearing may be in contact with an upper surface of the first connection portion in an axial direction.
A lower end portion of the second outer diameter portion and an upper end portion of the third outer diameter portion may be connected by a second connecting portion expanding in a direction away from the central axis, and at least a part of an upper surface of the rotor core may be in contact with a lower surface of the second connecting portion in the axial direction.
A lower end of the third outer diameter portion and an upper end of the fourth outer diameter portion may be connected by a third connecting portion that expands in a direction away from the central axis, and at least a part of an upper surface of the lower bearing may be in contact with a lower surface of the third connecting portion in the axial direction.
The center of gravity of the shaft, the impeller, and the rotor core may be disposed on the central axis, and the center of gravity may be disposed axially between an upper end of the second outer diameter portion and a lower end of the second outer diameter portion.
The axial length of the first outer diameter portion may be longer than the axial length of the second outer diameter portion, the axial length of the third outer diameter portion may be longer than the axial length of the second outer diameter portion, and the axial length of the fourth outer diameter portion may be shorter than the axial length of the second outer diameter portion.
The sum of the axial length of the third outer diameter portion and the axial length of the fourth outer diameter portion may be longer than the axial length of the first outer diameter portion.
An air blowing device according to an exemplary embodiment of the present invention includes: the above-described rotor assembly; a motor capable of rotating the rotor assembly about the central axis; and a housing enclosing a radially outer side of the rotor assembly.
The dust collector of the exemplary embodiment of the utility model is provided with the air supply device.
Effect of the utility model
In an exemplary embodiment of the present invention, a rotor assembly capable of improving assembly workability and suppressing an increase in size can be provided.
Drawings
Fig. 1 is a perspective view of a vacuum cleaner of the present embodiment.
Fig. 2 is a perspective view of the air blowing device.
Fig. 3 is a longitudinal sectional view of the blower device shown in fig. 2.
Fig. 4 is a cross-sectional view of the impeller.
Fig. 5 is an enlarged view of the dotted line region shown in fig. 4.
Fig. 6 is an enlarged view of the periphery of the impeller shown in fig. 3 in a longitudinal sectional view.
Fig. 7 is an enlarged view of the shaft periphery of the longitudinal sectional view shown in fig. 3.
Fig. 8 is an enlarged view of the periphery of the rotor core in the longitudinal sectional view shown in fig. 3.
Fig. 9 is an enlarged view of the peripheries of the upper and lower housings of the longitudinal sectional view shown in fig. 3.
Fig. 10 is a top perspective view of the upper housing.
Fig. 11 is a bottom perspective view of the upper housing.
Fig. 12 is a top perspective view of the lower housing.
Fig. 13 is an enlarged cross-sectional view of a modification of the impeller.
Fig. 14 is a vertical cross-sectional view showing the periphery of a modified example of the impeller.
(symbol description)
J center axis
R direction of rotation
One side of C1 circumference
The other circumferential side of C2
One side of DL1 in the longitudinal direction
The other side of DL2 in the longitudinal direction
One side in the short side direction of DS1
The other side in the short side direction of DS2
CM center of gravity
M1 axial midpoint
M2 radial midpoint
N normal
S fixing component
Width in the circumferential direction of W1
Width in the circumferential direction of W2
1 blowing device
10 Motor
11 rotor
12 shaft
13 rotor core
14 stator
15 stator core
16 insulator
17 coil
18 base plate
19 substrate cover
20 upper shell
21 upper bearing holding part
22 upper connecting part
23 upper projection
24 first wall part
241 communication part
25 second wall part
251 radially inner side surface
26 fixed blade
27 column part
271 convex part
28 fixing recess
30 lower shell
31 lower bearing holding part
32 lower connecting part
321 radial outer side
33 first lower wall part
331 inclined plane
34 second lower wall part
35 fixed hole
351 inner side surface
40 upper bearing
41 lower surface
50 lower bearing
51 upper surface of
52 lower surface
53 lower bushing
60 impeller
61 upper base
611 lower surface
612 radially outer end
613 radially inner end
62 first projection
621 side surface
622 side
623 one side end in the long side direction
624 on the other side end in the longitudinal direction
63 second projection
631 side surface
632 side surface
633 one side end in the longitudinal direction
634 the other side end in the longitudinal direction
635 convex part
636 lower end
64 upper extension part
641 lower surface
65 air inlet
66 lower base
661 upper surface of
662 lower surface
663 radially inner side
664 upper protruding part
665 lower surface
666 lower protruding part
667 upper surface
668 enlarged part
67 blade
671 side surface
672 side surface
674 at the other end in the longitudinal direction
68 bushing
681 tube part
682 upper surface
683 lower surface
684 protruding part
685 upper surface
686 lower surface
687 radial outer side surface
6870 processing noodles
688 connecting part
70 outer casing
71 impeller cover
711 air inlet
72 diffuser
73 top surface part
74 inner wall portion
75 outer wall part
76 fixed blade
80 vacuum cleaner
Detailed Description
Hereinafter, exemplary embodiments of the present invention will be described in detail with reference to the accompanying drawings. In the present specification, in the air blowing device 1, a direction parallel to the central axis J of the air blowing device 1 is referred to as an "axial direction", a direction perpendicular to the central axis J of the air blowing device 1 is referred to as a "radial direction", and a direction along an arc centered on the central axis J of the air blowing device 1 is referred to as a "circumferential direction". In the present specification, the blower 1 is configured such that the axial direction is the vertical direction and the side on which the impeller 60 is disposed with respect to the stator 14 is the upper side. The vertical direction is merely an explanatory direction, and the positional relationship and the direction in the use state of the air blowing device 1 are not limited. Further, "upstream" and "downstream" show upstream and downstream, respectively, of the airflow generated when the impeller 60 is rotated.
Further, in the air blowing device 1, the impeller 60 rotates in the circumferential direction around the central axis J. In the present description, in the rotation direction R of the impeller 60, the forward direction of rotation is referred to as "forward direction of rotation" or "the other side in the circumferential direction", and the forward direction of rotation is referred to as "backward direction of rotation" or "one side in the circumferential direction". In other words, when a certain point on the impeller 60 is set as a reference, a side where the certain point arrives after a predetermined time has elapsed is set as a front side in the rotation direction R or the other side in the circumferential direction, and a side which has already passed is set as a rear side in the rotation direction R or the one side in the circumferential direction. In the present specification, the shape and size of each part may be different from the actual structure in order to facilitate understanding of the structure of each part, and a specific part may be omitted from the drawings.
< vacuum cleaner >
Fig. 1 is a perspective view of a vacuum cleaner 80 according to the present embodiment. As shown in fig. 1, the vacuum cleaner 80 of the present embodiment is a so-called stick type electric vacuum cleaner, and includes a housing 81, and an air passage (not shown) in which the blower device 1 is disposed is formed in the housing 81. The housing 81 is provided with an intake section 82 and an exhaust section 83. A cylindrical suction tube 84 is connected to the air inlet 82. The vacuum cleaner 80 is not limited to a stick type, and may be a so-called robot type, canister type, or hand-held type electric vacuum cleaner. That is, the vacuum cleaner 80 includes the blower 1. Thus, in the blower 1 attached to the vacuum cleaner 80, the strength of the impeller 60 can be increased, and a decrease in blowing efficiency can be suppressed.
Fig. 2 is a perspective view of the blower 1. Fig. 3 is a longitudinal sectional view of the blower 1 shown in fig. 2. Fig. 3 shows a longitudinal section of the air blower 1 cut in a section passing through the central axis J. As shown in fig. 2 to 3, the blower 1 includes a motor 10, an upper casing 20, a lower casing 30, an upper bearing 40, a lower bearing 50, an impeller 60, and a casing 70.
The motor 10 has a rotor 11, a stator 14, an upper housing 20, a lower housing 30, an upper bearing 40, and a lower bearing 50. The rotor 11 has a shaft 12 rotatable about a central axis J extending in the up-down direction. A rotor core 13 is fixed to a radially outer peripheral surface of the shaft 12. The rotor core 13 is a ring-shaped magnet. The rotor core 13 may be fixed directly to the radially outer peripheral surface of the shaft 12, or may be fixed via another member.
The stator 14 is disposed radially opposite the rotor 11. The stator 14 includes a stator core 15, an insulator 16, and a coil 17. The stator core 15 has: an annular core back 151; and a plurality of teeth 152 extending radially inward from the core back 151 and arranged in the circumferential direction. At least a portion of the teeth 152 are covered by the insulator 16. Each tooth 152 is wound with a conductive wire through an insulator 16 to form a coil 17. The radially inner side surface of the tooth 152 is radially opposed to the radially outer side surface of the rotor core 13.
The upper bearing 40 and the lower bearing 50 support the shaft 12 to be rotatable about the center axis J. The upper bearing 40 is disposed above the stator 14, and the lower bearing 50 is disposed below the stator 14. The upper bearing 40 and the lower bearing 50 are ball bearings. The upper bearing and the lower bearing may be other bearings such as a slide bearing. Further, both the upper bearing and the lower bearing may be disposed above or below the stator.
At least a part of the upper housing 20 is disposed above the stator 14. The upper housing 20 has an upper bearing holding portion 21, an upper connecting portion 22, and an upper protruding portion 23. The upper bearing holding portion 21 is a cylindrical portion extending in the axial direction. The upper bearing holding portion 21 supports the upper bearing 40 above the stator 14. The upper connecting portion 22 extends from the upper bearing holding portion 21 in a direction away from the central axis J. In the present embodiment, the upper connecting portion 22 is a plurality of ribs extending radially outward and downward from the center axis J and arranged in the circumferential direction. However, the upper connecting portion may be a plate-shaped portion extending in a direction intersecting the central axis J. The upper protruding portion 23 extends downward from the upper connecting portion 22.
At least a part of the lower case 30 is disposed below the stator 14. The lower housing 30 has a lower bearing holding portion 31 and a lower connecting portion 32. The lower bearing holding portion 31 is a cylindrical portion extending in the axial direction. The lower bearing holding portion 31 supports the lower bearing 50 below the stator 14. The lower connecting portion 32 extends from the lower bearing holding portion 31 in a direction away from the center axis J. In the present embodiment, the lower connecting portion 32 has a plurality of ribs extending radially outward from the lower bearing holding portion 31 and arranged in the circumferential direction. However, the lower connecting portion may be a plate-shaped portion extending in a direction intersecting the central axis J.
The motor 10 has a base plate 18. The substrate 18 is disposed below the lower case 30. The lower casing 30 is surrounded radially outside and below by the substrate cover 19. The substrate cover 19 is fixed to the lower case 30.
The impeller 60 is fixed to the upper end of the shaft 12. Impeller 60 has an upper base 61, a lower base 66, and a plurality of blades 67. The upper base portion 61 expands in a direction intersecting a central axis J extending in the up-down direction. An air inlet 65 penetrating in the axial direction is disposed in the center of the upper base portion 61. The lower base portion 66 is disposed below the upper base portion 61 and extends in a direction intersecting the central axis J. The lower base 66 is fixed to the upper end of the shaft 12 via a bushing 68. The bushing 68 has a cylindrical shape extending in the axial direction. A plurality of blades 67 connect the upper base 61 and the lower base 66 and are arranged in the circumferential direction.
The housing 70 has an impeller cup 71 and a diffuser 72. The impeller cup 71 covers at least a portion radially outside and above the impeller 60. An intake port 711 penetrating in the axial direction is disposed at the center of the impeller cover 71. The housing 70 may be formed of only a single impeller cup, or may include another member having a structure different from that of the present embodiment.
The diffuser 72 includes a top surface portion 73, an inner wall portion 74, an outer wall portion 75, and a stationary blade 76. The top surface portion 73 is a portion that expands in a direction intersecting the center axis J. The radially inner edge of the top surface portion 73 is fixed to the upper bearing holding portion 21. The inner wall portion 74 extends downward from the radially outer edge of the top surface portion 73. The outer wall portion 75 is a cylindrical portion disposed radially outward of the inner wall portion 74 and extending in the axial direction. The fixed vane 76 connects the inner wall portion 74 and the outer wall portion 75. A flow path is arranged between the inner wall 74 and the outer wall 75 in the radial direction.
When the impeller 60 rotates, the gas sucked in from the inlet 711 is introduced into the impeller 60 through the inlet 65, passes through the radially inner side of the impeller cover 71, and flows downward between the inner wall 74 and the outer wall 75 in the radial direction. Further, a part of the gas passes through between the inner wall portions 74 arranged in the circumferential direction, is guided radially inward of the inner wall portions 74, and flows downward around the rotor 11 and the stator 14. This enables the rotor 11 and the stator 14 to be cooled.
Fig. 4 is a cross-sectional view of the impeller 60. More specifically, fig. 4 shows a pattern of the impeller 60 as viewed from below along a section X-X shown in fig. 3. Fig. 5 is an enlarged view showing a dotted line region of fig. 4. The impeller 60 will be described below mainly with reference to fig. 4 and 5.
As shown in fig. 4 and 5, the blade 67 extends toward one longitudinal side DL 1. The longitudinal direction side DL1 is directed radially outward and toward the circumferential direction side C1. The direction radially inward along the direction in which the vane 67 extends and toward the other circumferential side C2 is referred to as the other longitudinal side DL 2. The direction substantially perpendicular to the longitudinal direction is referred to as the short-side direction. In the short-side direction, the direction toward the one circumferential side C1 is referred to as a short-side direction one side DS1, and the direction toward the other circumferential side C2 is referred to as a short-side direction other side DS 2.
The upper base 61 has a first projection 62 and a second projection 63. The first protruding portion 62 protrudes downward from the lower surface 611 of the upper base portion 61. The first projection 62 contacts a side surface 672 of the other circumferential side C2 of the vane 67. This enables the first protrusion 62 to support and support the side surface 672 of the other circumferential side C2 of the vane 67, thereby improving the strength of the impeller 60. In the present embodiment, the lower base 66 and the blade 67 are molded as an integral member. However, the upper base portion and the blade may be formed as a single piece, and the lower base portion 66 may have a first protruding portion and a second protruding portion.
The second protruding portion 63 protrudes downward from the lower surface 611 of the upper base portion 61. The second projection 63 contacts a side surface 671 of the circumferential side C1 of the blade 67. More specifically, the side surface 632 of the other circumferential side C2 of the second protrusion 63 contacts the side surface 671 of the one circumferential side C1 of the vane 67. This enables the side surface 671 of the circumferential side C1 of the blade 67 to be supported by the second protrusion 63, thereby improving the strength of the impeller 60. In the present embodiment, since the side surfaces of the vane 67 on both sides in the circumferential direction are supported by the first projecting portion 62 and the second projecting portion 63, the strength of the impeller 60 is further improved. In the present embodiment, the first projection 62 and the second projection 63 are welded to the blade 67. Therefore, the strength of the impeller 60 is further improved.
The longitudinal-direction one-side end 623 of the first projecting portion 62 is disposed closer to the longitudinal-direction one side DL1 than the longitudinal-direction one-side end 633 of the second projecting portion 63. This can suppress narrowing of the flow path in the impeller 60, and thus can suppress reduction in the air blowing efficiency of the impeller 60. In other words, the longitudinal length of the second projecting portion 63 can be shortened as compared with a case where the longitudinal position of the longitudinal side end 633 of the second projecting portion 63 is substantially the same as the longitudinal position of the longitudinal side end 623 of the first projecting portion 62. Therefore, the flow passage in the impeller 60 can be suppressed from being narrowed because the second protruding portion 63 is long in the longitudinal direction.
When the impeller 60 rotates in the rotation direction R, the side surface 672 of the other circumferential side C2 of the vane 67, on which stress is more likely to concentrate, is supported by the first projecting portion 62 that is long in the longitudinal direction, and the flow passage in the impeller 60 can be suppressed from being narrowed by the second projecting portion 63. Therefore, the strength of the impeller 60 can be increased while suppressing a decrease in air blowing efficiency. The rotational direction R is the same direction as the other circumferential side C2.
Further, when assembling the blade 67 and the upper base portion 61, the blade 67 needs to be arranged between the first protruding portion 62 and the second protruding portion 63 in the circumferential direction. At this time, if the longitudinal position of the longitudinal side end 633 of the second projecting portion 63 is substantially the same as the longitudinal position of the longitudinal side end 623 of the first projecting portion 62, the workability of the step of inserting the blade 67 between the first projecting portion 62 and the second projecting portion 63 in the circumferential direction may be deteriorated. However, in the present embodiment, the length of the second protruding portion 63 in the longitudinal direction is shortened, thereby suppressing the deterioration of the workability of the above-described steps.
The blower 1 includes: the above-mentioned impeller 60; a motor 10 capable of rotating the impeller 60 about the center axis J; and a casing 70 surrounding a radially outer side of the impeller 60. This improves the strength of the impeller 60 attached to the blower 1, and reduces the reduction in blowing efficiency.
The first projection 62 is arranged along the side 672 of the other circumferential side C2 of the vane 67. That is, the side surface 621 of the circumferential one side C1 of the first protrusion 62 is arranged along the side surface 672 of the circumferential other side C2 of the vane 67. This enables the first protruding portion 62 to support the blade 67 more firmly.
The width of the first protruding portion 62 in the short side direction is substantially constant in the long side direction. Therefore, the side surface 622 of the other circumferential side C2 of the first protrusion 62 is arranged along the side surface 672 of the other circumferential side C2 of the vane 67.
The second protruding portion 63 has a convex portion 635. The convex portion 635 is a portion that protrudes toward the circumferential side C1 at the side face 631 of the circumferential side C1 of the second protruding portion 63. That is, the side face 631 of the circumferential side C1 of the second projecting portion 63 projects toward the circumferential side C1. This can widen the width of the second protruding portion 63 in the short-side direction, and thus the strength of the second protruding portion 63 is improved. Therefore, the rigidity of the impeller 60 is improved.
The width W1 in the short direction at the other longitudinal side end 674 of the blade 67 is narrower than the width W2 in the short direction at the longitudinal center portion of the blade 67. The short-side direction is a direction orthogonal to the long-side direction. This facilitates insertion of the other longitudinal side end 674 of the blade 67 between the first projection 62 and the second projection 63 in the circumferential direction. Therefore, workability of assembling the impeller 60 is improved.
The other longitudinal side end 624 of the first projecting portion 62, the other longitudinal side end 674 of the vane 67, and the other longitudinal side end 634 of the second projecting portion 63 are arranged substantially on a straight line in a direction intersecting the center axis J. Thus, the other longitudinal side end 674 of the blade 67 can be supported by both the other longitudinal side end 624 of the first projecting portion 62 and the other longitudinal side end 634 of the second projecting portion 63, and the strength of the impeller 60 can be further improved. In addition, when the width W1 in the short-side direction of the other longitudinal-direction side end 674 of the blade 67 is narrow, the effect of improving the strength of the impeller 60 by supporting the other longitudinal-direction side end 674 of the blade 67 from both sides in the circumferential direction is more significant.
Referring to fig. 3 to 5, the upper base portion 61 has an upper extending portion 64 extending radially inward and upward. That is, the upper extending portion 64 is a portion of the upper base portion 61 that is radially inward of the radial middle between the radially outer end 612 and the radially inner end 613 of the lower surface 611. The upper extension 64 has an air inlet 65 penetrating in the axial direction.
The second protrusion 63 is disposed on the lower surface 641 of the upper extension 64. Therefore, the length of the second protruding portion 63 in the longitudinal direction is equal to or less than half the length of the blade 67 in the longitudinal direction. The lower end 636 of the second protruding portion 63 is arranged above the radially outer end 612 of the lower surface 611 of the upper base portion 61. This can suppress narrowing of the flow path at the radially outer end 612 of the lower surface 611 of the upper base 61, which is a region where the pressure inside the impeller 60 tends to increase, and can suppress a decrease in the air blowing efficiency of the impeller 60. In other words, it is possible to suppress a decrease in the blowing efficiency of the impeller 60 while firmly fixing the blades 67 and the upper base 61. In particular, in the upper extending portion 64, the upper base portion 61 is bent upward, and therefore the blade 67 and the upper base portion 61 tend to be less likely to be welded. However, in the present embodiment, by forming the second protruding portion 63 in the upper extending portion 64, the blade 67 and the upper base portion 61 can be firmly welded while suppressing the influence on the air blowing efficiency of the impeller 60.
Fig. 6 is an enlarged view of the periphery of the impeller 60 in the longitudinal sectional view shown in fig. 3. As shown in fig. 6, the impeller 60 has a lower base 66, a plurality of blades 67, and a bushing 68. The lower base portion 66 expands in a direction intersecting with a central axis J extending in the up-down direction. The plurality of blades 67 are arranged in the circumferential direction on the upper surface 661 of the lower base 66. The bushing 68 is disposed near the center of the lower base 66.
The bush 68 has a cylindrical portion 681 and a protruding portion 684. The cylinder portion 681 has a cylindrical shape extending in the axial direction. The protruding portion 684 protrudes radially outward from the radially outer surface 6811 of the cylinder portion 681. The lower base 66 is fixed to the shaft 12 via a bushing 68. The radially outer side of the shaft 12 is fixed to the radially inner side of the bushing 68. The radially outer side of the bushing 68 is fixed to the radially inner side 663 of the lower base 66.
The lower base 66 has a lower protrusion 666. The lower protruding portion 666 protrudes radially inward from the radially inner side face 663 of the lower base 66. In the present embodiment, the lower base 66 has an upper protrusion 664 disposed above the lower protrusion 666. The upper protruding portion 664 protrudes radially inward from the radially inner surface 663 of the lower base portion 66.
At least a portion of a lower surface 686 of the projection 684 is in axial contact with an upper surface 667 of the lower projection 666. This can firmly fix the lower base 66 and the bush 68. When the impeller 60 rotates, the gas is discharged radially outward and downward by the impeller 60, and therefore an upward force acts on the impeller 60 as a reaction force thereof. At this time, by bringing an upper surface 667 of the lower protrusion 666, which is a part of the lower base 66, into contact with a lower surface 686 of the protrusion 684 in the axial direction, upward movement of the lower base 66 can be suppressed.
The blower 1 includes: the above-mentioned impeller 60; a motor 10 capable of rotating the impeller 60 about the center axis J; and a casing 70 surrounding a radially outer side of the impeller 60. This enables the lower base 66 and the bush 68 to be firmly fixed to the impeller 60 attached to the blower 1.
The vacuum cleaner 80 has the blower 1. This can improve the strength of the impeller 60 in the vacuum cleaner 80 to which the blower 1 is attached.
At least a portion of the upper surface 685 of the projection 684 is in axial contact with the lower surface 665 of the upper projection 664. This can firmly fix the lower base 66 and the bush 68. In the impeller 60, the lower surface 665 of the upper protruding portion 664 and the upper surface 667 of the lower protruding portion 666 are in contact with the upper surface 685 and the lower surface 686 of the protruding portion 684 in the axial direction, respectively, and therefore, the lower base 66 and the liner 68 can be further firmly fixed.
At least a portion of the radially outer side surface 687 of the protruding portion 684 is knurled. That is, the radially outer surface 687 of the protruding portion 684 has a machined surface 6870 that has been knurled. In the present embodiment, the processing surface 6870 includes: a plurality of protrusions arranged in a circumferential direction, the protrusions having a longitudinal direction in an axial direction and protruding outward in a radial direction; and a recessed portion disposed between the convex portions in the circumferential direction and recessed radially inward of radially outer side surfaces of the convex portions.
The machined surface 6870 radially contacts the radially inner side surface 663 of the lower base 66. This can firmly fix the lower base 66 and the bush 68. In the present embodiment, the radially inner surface 663 of the lower base 66 below the upper protruding portion 664 and above the lower protruding portion 666 is in contact with the machined surface 6870 in the radial direction. However, the radially outer surface of the tube portion 681 may have a machined surface that is knurled, and at least one of the upper protruding portion and the lower protruding portion may be in contact with the machined surface in the radial direction.
The upper surface 685 of the protrusion 684 and the radially outer side surface 687 of the protrusion 684 are connected via a connection 688. The connecting portion 688 is a portion extending radially outward and downward. That is, the protrusion 684 has a connecting portion 688 that connects the upper surface 685 and the radially outer side surface 687 of the protrusion 684 and extends radially outward and downward.
The radially inner end of the upper surface 682 of the cylinder 681 and the upper surface 661 of the lower base 66 are substantially flush. This can suppress the length of the lower base 66 in the axial direction from becoming longer. That is, the length of the lower base 66 in the axial direction can be made shorter than in the case where the upper end of the tube 681 protrudes above the upper surface of the lower base 66.
The upper surface 661 of the lower base 66 has an enlarged portion 668. Enlarged portion 668 extends downward as it goes radially outward. The radially inner end of enlarged portion 668 is disposed radially inward of radially outer side surface 687 of protrusion 684. The radially outer end of enlarged portion 668 is disposed radially outward and downward of radially outward surface 687 of protrusion 684.
At least a part of the enlarged portion 668 intersects with a normal line N directed radially outward and upward from the connection portion 688. Thus, the distance between the expanded portion 668 and the connecting region between the upper surface 685 of the protruding portion 684 and the radially outer surface 687 can be made longer than in the case where the upper surface of the protruding portion is connected perpendicularly to the radially outer surface. Therefore, in the region where the enlarged portion 668 intersects the normal line N, the thickness of the lower base 66 in the normal line N direction increases, and the strength of the lower base 66 improves. In the present embodiment, the enlarged portion 668 and the connecting portion 688 extend substantially parallel to each other radially outward and downward. This makes it possible to keep the thickness of the lower base 66 substantially constant in the normal N direction in this region, and thus to improve the strength of the lower base 66 over the entire region.
The lower surface 683 of the barrel 681 is in a plane with the lower surface 662 of the lower base 66. This can suppress the impeller 60 from becoming long in the axial direction.
Fig. 7 is an enlarged view of the periphery of the shaft 12 in the longitudinal sectional view shown in fig. 3. Fig. 8 is an enlarged view of the periphery of the rotor core 13 in the longitudinal sectional view shown in fig. 3. Referring to fig. 3, 7, and 8, the motor 10 has a rotor assembly 100.
The rotor assembly 100 has a shaft 12, an impeller 60, a rotor core 13, an upper bearing 40 and a lower bearing 50. The shaft 12 is disposed along a central axis J extending in the vertical direction. The impeller 60 is fixed to the shaft 12 and is rotatable about the central axis J. The rotor core 13 is fixed to the shaft 12. The upper bearing 40 and the lower bearing 50 are fixed to the shaft 12. The lower bearing 50 is disposed below the upper bearing 40.
The shaft 12 has a first outer diameter portion 121, a second outer diameter portion 122, a third outer diameter portion 123, and a fourth outer diameter portion 124. The outer diameter of first outer diameter portion 121 is first outer diameter d 1. The impeller 60 and the upper bearing 40 are fixed to the first outer diameter portion 121. The second outer diameter portion 122 is disposed below the first outer diameter portion 121. The outer diameter of the second outer diameter portion 122 is the second outer diameter d2, which is larger than the first outer diameter d 1. The third outer diameter portion 123 is disposed below the second outer diameter portion 122. The third outer diameter part 123 has a third outer diameter d3 smaller than the second outer diameter d 2. The rotor core 13 is fixed to the third outer diameter portion 123. The fourth outer diameter portion 124 is disposed below the third outer diameter portion 123. The outer diameter of the fourth outer diameter portion 124 is the fourth outer diameter d4, which is smaller than the third outer diameter d 3. The lower bearing 50 is fixed to the fourth outer diameter portion 124. In the present embodiment, the third outer diameter d3 is larger than the first outer diameter d 1. That is, the third outer diameter portion 123 is thicker than the first outer diameter portion 121.
The lower end of the first outer diameter portion 121 and the upper end of the second outer diameter portion 122 are connected via a first connection portion 125 expanding in a direction away from the central axis J. The lower end of the second outer diameter portion 122 and the upper end of the third outer diameter portion 123 are connected via a second connecting portion 126 expanding in a direction away from the central axis J. A lower end of the third outer diameter portion 123 and an upper end of the fourth outer diameter portion 124 are connected via a third connecting portion 127 expanding in a direction away from the central axis J. In the present embodiment, the first connection portion 125, the second connection portion 126, and the third connection portion 127 are constituted by planes extending in the radial direction.
At least a portion of the lower surface 41 of the upper bearing 40 is in contact with the upper surface of the first connection portion 125 in the axial direction. Thereby, the upper bearing 40 and the shaft 12 are positioned. Further, for example, the upper bearing 40 can be pressed until the lower surface 41 of the upper bearing 40 comes into contact with the upper surface of the first connection portion 125 to easily position the upper bearing 40 and the shaft 12, and therefore, the assembling workability of the rotor assembly 100 is improved.
At least a part of the upper surface 131 of the rotor core 13 is in contact with the lower surface of the second connecting portion 126 in the axial direction. Thereby, the rotor core 13 and the shaft 12 are positioned. Further, for example, the rotor core 13 and the shaft 12 can be easily positioned by press-fitting the rotor core 13 until the upper surface 131 of the rotor core 13 comes into contact with the lower surface of the second connecting portion 126, and therefore, the assembling workability of the rotor assembly 100 is improved.
At least a portion of the upper surface 51 of the lower bearing 50 is in contact with the lower surface of the third connecting portion 127 in the axial direction. Thereby, the lower bearing 50 and the shaft 12 are positioned. Further, for example, the lower bearing 50 and the shaft 12 can be easily positioned by press-fitting the lower bearing 50 until the upper surface 51 of the lower bearing 50 comes into contact with the lower surface of the third connecting portion 127, and therefore, the assembling workability of the rotor assembly 100 is improved.
The center of gravity CM of the shaft 12, the impeller 60, and the rotor core 13 is disposed at the second outer diameter portion 122. More specifically, the center of gravity CM is disposed on the central axis J, and the center of gravity CM is disposed between the upper end of the second outer diameter portion 122 and the lower end of the second outer diameter portion 122 in the axial direction. This enables the rotor assembly 100 to support the center of gravity CM from both axial sides by the upper bearing 40 and the lower bearing 50.
Further, by providing the rotor assembly 100 with the above-described configuration, it is possible to suppress an increase in the size of the rotor assembly 100 in the radial direction. That is, since a force acts between the rotor core and the stator in the motor, when a normal rotor assembly is configured, the axial positions of the centers of gravity of the shaft, the impeller, and the rotor core are often disposed between the upper end and the lower end of the rotor core in the axial direction. However, in this case, the outer diameter of the region to which the rotor core is fixed is larger than the outer diameter of the other region of the shaft, and the outer diameter of the rotor core becomes large, resulting in an increase in the radial dimension of the rotor assembly. On the other hand, in the rotor assembly 100, the second outer diameter d2 is larger than the third outer diameter d3 of the third outer diameter portion 123 to which the rotor core 13 is fixed, whereby the third outer diameter d3 can be made relatively small. Therefore, the radial dimension of the rotor assembly 100 can be suppressed from increasing. The center of gravity CM of the shaft 12, the impeller 60, and the rotor core 13 is a rotating body rotatably supported by a bearing. That is, when the rotor assembly includes the spacer, the center of gravity of the shaft, the impeller, the rotor core, and the spacer may be disposed on the second outer diameter portion.
The air supply device 1 is provided with; the above rotor assembly 100; a stator 14 disposed to face the rotor core 13 in the radial direction; and a casing 70 surrounding a radially outer side of the impeller 60. This can suppress an increase in the radial dimension of the rotor assembly 100 mounted to the blower 1.
The vacuum cleaner 80 has the blower 1. This can suppress an increase in the radial dimension of the rotor assembly 100 attached to the vacuum cleaner 80.
The axial length L1 of the first outer diameter portion 121 is longer than the axial length L2 of the second outer diameter portion 122. The axial length L3 of the third outer diameter portion 123 is longer than the axial length L2 of the second outer diameter portion 122. Axial length L4 of fourth outer diameter portion 124 is shorter than axial length L2 of second outer diameter portion 122. Thereby, the rotation of the rotor assembly 100 is stabilized. That is, by making the axial length L3 of the third outer diameter portion 123 longer than the axial length L2 of the second outer diameter portion 122, the center of gravity CM can be disposed as low as possible. Therefore, the center of gravity CM can be located as close to the rotor core 13 as possible in the axial direction, and therefore the center of gravity CM can be located close to the region where a force acts between the rotor core 13 and the stator 14, and the rotation of the rotor assembly 100 is stabilized.
The axial length from the upper end of the third outer diameter portion 123 to the lower end of the fourth outer diameter portion 124 is longer than the axial length L1 of the first outer diameter portion 121. That is, the sum of the axial length L3 and the axial length L4 is longer than the axial length L1. Thereby, the center of gravity CM is close to the rotor core 13 in the axial direction, and thus the rotation of the rotor assembly 100 is stabilized.
The center of gravity CM is disposed below the axial midpoint M1 of the second outer diameter portion 122. Thereby, the center of gravity CM is close to the rotor core 13 in the axial direction, and thus the rotation of the rotor assembly 100 is stabilized.
As shown in fig. 8, a radial midpoint M2 between the radially inner end 133 of the rotor core 13 and the radially outer end 134 of the rotor core 13 is disposed radially outward of the radially outer end of the second outer diameter portion 122. This can reduce the thickness of the second outer diameter portion 122, and thus can suppress an increase in weight of the rotor assembly 100. Moreover, by suppressing the thickness of the second outer diameter portion 122, the center of gravity CM is made close to the rotor core 13 in the axial direction, and therefore, the rotation of the rotor assembly 100 is stabilized.
A radially inner edge 132 in the upper surface 131 of the rotor core 13 extends downward as approaching the central axis J. This can reduce the contact area between the upper surface 131 of the rotor core 13 and the lower surface of the second connection portion 126. Therefore, leakage of the magnetic flux of the rotor core portion 13 to the second outer diameter portion 122 can be suppressed. Also, the positioning accuracy of the rotor core 13 and the shaft 12 is improved.
Fig. 9 is an enlarged view of the periphery of the upper and lower housings 20 and 30 of the longitudinal sectional view shown in fig. 3. Fig. 10 is a top perspective view of the upper housing 20. Fig. 11 is a bottom perspective view of the upper housing 20. Fig. 12 is a top perspective view of the lower housing 30.
As shown in fig. 9 to 11, the upper housing 20 includes an upper bearing holding portion 21, an upper connecting portion 22, and an upper protruding portion 23. The upper bearing holding portion 21 is a cylindrical portion extending in the axial direction. The upper connecting portion 22 extends radially outward from the upper bearing holding portion 21. The upper protruding portion 23 protrudes downward from the upper connecting portion 22.
In the present embodiment, the upper protruding portion 23 has a first wall portion 24 and a second wall portion 25. The first wall portion 24 is a wall-shaped portion extending downward from the radially outer end of the upper connecting portion 22. A part of the radially outer side surface of the first wall portion 24 is fixed to the inner wall portion 74. A communication portion 241 penetrating in the radial direction is arranged above the first wall portion 24. In the present embodiment, the communication portion 241 is a cutout in which a portion of the first wall portion 24 is cut off between the upper connection portions 22 in the circumferential direction and communicates in the radial direction. A part of the gas flowing downward from the vicinity of the inner wall portion 74 by the impeller 60 passes through the communication portion 241 and collides with the rotor 11 and the stator 14. This enables the rotor 11 and the stator 14 to be cooled.
The second outer wall portion 25 is a cylindrical portion disposed radially outward of the first wall portion 24 and extending in the axial direction. The first wall portion 24 and the second wall portion 25 are connected by a fixed vane 26. At least a portion of the second wall portion 25 is fixed to the impeller cup 71. In the present embodiment, at least a part of the second wall portion 25 is fixed to the outer wall portion 75. Thereby, a flow path of gas is arranged between the first wall portion 24 and the second wall portion 25. Therefore, the gas flowing downward in the radial direction between the inner wall 74 and the outer wall 75 flows downward in the flow path disposed in the radial direction between the first wall 24 and the second wall 25, and is discharged from the lower end of the upper casing 20 to the external space of the air blower 1.
The upper protruding portion 23 has a plurality of columnar portions 27. The columnar portion 27 is a columnar portion that connects parts of the first wall portion 24 and the second wall portion 25 and extends downward. The width in the radial direction of the columnar portion 27 is wider than the width in the radial direction of the first wall portion 24 and the width in the radial direction of the second wall portion 25. The rigidity of the upper case 20 is improved by providing the columnar portion 27 in the upper protruding portion 23. In particular, the rigidity in the vicinity of the columnar portion 27 is improved.
A projection 271 projecting downward is formed radially outward of the columnar portion 27. In other words, a part of the second wall portion 25 protrudes downward as the protrusion 271. The projection 271 contacts at least a portion of the lower case 30. In more detail, the radially inner side surface 251 of the second wall portion 25 contacts the lower casing 30. That is, at least a portion of the upper housing 20 contacts at least a portion of the lower housing 30 in a direction crossing the central axis J. This enables the upper and lower housings 20 and 30 to be positioned with high accuracy. That is, the upper and lower housings 20 and 30 can be positioned with high accuracy in the direction intersecting the center axis J. Therefore, the coaxiality of the upper bearing 40 fixed to the upper housing 20 and the lower bearing 50 fixed to the lower housing 30 is improved. Therefore, the rotational accuracy of the motor 10 is improved.
In the present embodiment, at least a part of the upper protruding portion 23 contacts at least a part of the lower housing 30 in a direction intersecting the center axis J. Thus, the upper case 20 and the lower case 30 can be positioned with high accuracy by forming the upper protruding portion 23 of an arbitrary shape in the upper case 20 and bringing a portion of the upper protruding portion 23 having an appropriate shape into contact with at least a part of the lower case 30.
The upper case 20 has a fixing recess 28 recessed upward. More specifically, the fixing recess 28 is configured as a recess recessed upward from the lower surface of the columnar portion 27 that is a part of the upper case 20. A fixing member S is inserted into the fixing recess 28. By disposing the fixing recess 28 in the columnar portion 27 having high rigidity, a decrease in rigidity of the upper case 20 can be suppressed. Further, the upper housing 20 and the lower housing 30 can be positioned with high accuracy by fixing the upper housing 20 and the lower housing 30 using the fixing member S using a portion having high rigidity.
The lower housing 30 has a lower bearing holding portion 31 and a lower connecting portion 32. The lower bearing holding portion 31 is a cylindrical portion extending in the axial direction. A lower bush 53 is disposed radially inward of the lower bearing holding portion 31. The lower bearing 50 is supported by a radially inner side surface of the lower bushing 53. In the present embodiment, the lower connecting portions 32 are ribs extending in the radial direction and arranged in the circumferential direction. However, the lower connecting portion 32 may be a plate-shaped portion that spreads in a direction intersecting the central axis J.
The lower case 30 has a first lower wall portion 33 and a second lower wall portion 34. The first lower wall portion 33 is a portion connecting the radially outer ends of the circumferentially adjacent lower connecting portions 32. The upper surface of the first lower wall 33 has an inclined surface 331 inclined radially outward and downward. Accordingly, the gas flowing downward in the flow path disposed between the first wall portion 24 and the second wall portion 25 is smoothly guided radially outward and downward via the inclined surface 331, and thus the air blowing efficiency of the air blower 1 is improved.
The second lower wall 34 extends downward from the lower end of the first lower wall 33. At least a portion of the second lower wall portion 34 is connected to a radially outer end portion of the lower connecting portion 32. The rigidity of the radially outer end portion of the lower casing 30 is increased by the arrangement of the second lower wall portion 34.
The lower case 30 has a fixing hole 35 penetrating in the axial direction. More specifically, the fixing hole 35 is disposed at a radially outer end portion of the lower connecting portion 32. A fixing member S is inserted into the fixing hole 35. That is, the fixing member S is inserted into the fixing recess 28 through the fixing hole 35. Therefore, the upper and lower housings 20 and 30 are fixed by the fixing member S extending in the axial direction. In the present embodiment, the fixing member S is a screw. However, the fixing member S may be a member other than a screw. This enables the upper case 20 and the lower case 30 to be fixed in a state of being positioned with high accuracy.
As shown in fig. 9, at least a part of the inner surface 351 of the lower case 30 constituting the fixing hole 35 faces the outer surface of the fixing member S with a gap therebetween. That is, at least a portion of the inner surface 351 of the lower case 30 constituting the fixing hole 35 does not contact the outer surface of the fixing member S. This enables the upper and lower housings 20 and 30 to be positioned with high accuracy. That is, for example, when the inner diameter of the inner surface 351 of the lower case 30 constituting the fixing hole 35 is substantially the same as the outer diameter of the fixing member, the positions of the upper case 20 and the lower case 30 in the radial direction of the members are determined by the arrangement of the fixing member when it is inserted into the fixing hole. However, in the present structure, there is a gap between the inner surface 351 and the radially outer surface of the fixing member S. Therefore, the radial positions of the radial inner surface 251 of the upper casing 20 and the radial outer surface 321 of the lower casing 30 can be fixed by the fixing member S. Therefore, the upper and lower housings 20 and 30 can be positioned with high accuracy.
In the present embodiment, the radially inner surface 251 of the upper protruding portion 23 is in contact with the radially outer surface 321 of the lower connecting portion 32 in the radial direction. This allows the upper and lower housings 20 and 30 to be provided with a simple structure, and allows the upper and lower housings 20 and 30 to be positioned with high accuracy. Since the upper case 20 and the lower case 30 can be fixed without forming a portion protruding upward on the lower case 30, the structure of the lower case 30 can be particularly simplified.
The fixing member S is disposed in the vicinity of a region where the radially inner surface 251 of the upper casing 20 and the radially outer surface 321 of the lower casing 30 are in contact with each other. This can further improve the positioning accuracy of the upper and lower cases 20 and 30.
At least a portion of the upper protrusion 23 is in contact with at least a portion of the lower housing 30 in the axial direction. Thereby, the upper casing 20 and the lower casing 30 can be fixed in the axial direction. In particular, when at least a part of the inner surface 351 constituting the fixing hole 35 faces the outer surface of the fixing member S with a gap therebetween, the lower housing 30 is pressed against the upper housing 20 in the axial direction by the above-described structure while fixing the two, whereby the two can be firmly fixed.
At least a part of the upper protruding portion 23 and at least a part of the lower housing 30 are arranged axially between the upper surface 51 and the lower surface 52 of the lower bearing 50 in a region where they contact in a direction intersecting the central axis J. More specifically, at least a portion of a region where the radially inner side surface 251 of the second wall portion 25 and the radially outer side surface 321 of the lower connecting portion 32 contact in the radial direction is arranged in the axial direction between the upper surface 51 of the lower bearing 50 and the lower surface 52 of the lower bearing 50. Thereby, the fixing area of the upper housing 20 and the lower housing 30 is closer to the lower bearing 50, and thus the rotational accuracy of the rotor 11 is improved.
The blower 1 includes: the above-mentioned motor 10; an impeller 60 disposed above the upper bearing 40 and fixed to the shaft 12; and a casing 70 surrounding a radially outer side of the impeller 60. This improves the rotational accuracy of the motor 10 mounted on the blower 1. The vacuum cleaner 80 includes the blower 1. This enables a vacuum cleaner having the motor 10 with high rotation accuracy to be realized.
Fig. 13 is an enlarged cross-sectional view of a modification of the impeller. That is, fig. 13 is an enlarged view showing the same region as fig. 5 in a modification of the impeller. In fig. 13, the first projection 62A is different in structure from the first projection 62, and is otherwise the same as the impeller 60. Therefore, in the modification of the impeller shown in fig. 13, the same parts as those of the impeller 60 shown in fig. 5 are denoted by the same reference numerals, and the description thereof is omitted. Hereinafter, only the difference between the impeller shown in fig. 13 and the impeller 60 shown in fig. 5 will be described.
In the modification of the impeller shown in fig. 13, a plurality of first protrusions 62A are arranged in the longitudinal direction. This can shorten the total length of all the first protruding portions 62A in the longitudinal direction as compared with the first protruding portions 62 of the impeller 60, and thus can reduce the weight of the impeller 60. Further, since the side surface 621A of the first projecting portion 62A on the one circumferential side C1 and the side surface 672 of the second circumferential side C2 of the blade 67 are partially in contact with each other, the contact area between the blade 67 and the first projecting portion 62A can be narrowed, and therefore, workability in assembling both can be improved.
The width in the circumferential direction between the side surface 621A of the first protrusion 62A on the one circumferential side C1 and the side surface 622A of the second circumferential side C2 is substantially constant in each first protrusion 62A. This enables the strength of welding to be as uniform as possible in the longitudinal direction when the first protruding portion 62A and the blade 67 are welded.
In the present embodiment, the number of first protruding portions 62A that contact a certain blade 67 is three. The number of first projections 62A may be other numbers. One longitudinal side end 623A of the first protrusion 62A disposed on the one longitudinal side DL1 is disposed closer to the other longitudinal side DL2 than the one longitudinal side end of the blade 67. The other longitudinal side end 624A of the first protrusion 62A disposed on the other longitudinal side DL2 is disposed at the same position as the other longitudinal side end 674 of the blade 67 in the longitudinal direction.
Fig. 14 is a vertical cross-sectional view showing the periphery of a modified example of the impeller. Fig. 14 shows a region corresponding to the cross-sectional view shown in fig. 6 in a modification of the impeller. Hereinafter, only the difference from the impeller 60 will be described with respect to a modification of the impeller.
In the modification of the impeller shown in fig. 14, the shape of the lower base 66A is different from the shape of the lower base 66. In fig. 14, the radially inner end portion of the lower base portion 66A is cup-shaped. That is, the upper side of the upper projection 664A extends further radially inward to form a plate-like portion covering the upper surface 128 of the shaft 12. Likewise, a radially inner end portion in the upper surface 661A of the lower base portion 66A covers the upper surface of the cylinder portion 681. This further increases the rigidity of the lower base portion 66A. Further, the upper surface 661A of the lower base portion 66A can be extended further upward and radially inward than the shape of the lower base portion 66. Therefore, the airflow sucked by the blade 67 can be guided further smoothly downward and radially outward. Therefore, the generation of turbulence in the upper surface 661A of the lower base 66A can be suppressed.
The present invention has been described above, but various modifications and combinations of the embodiments are possible within the scope of the present invention.
Industrial applicability of the utility model
The present invention can be used for an impeller, a blower, and a vacuum cleaner.
Claims (10)
1. A rotor assembly having:
a shaft disposed along a central axis extending in the vertical direction;
an impeller rotatable about the central axis;
a rotor core;
an upper bearing; and
a lower bearing disposed below the upper bearing,
the impeller, the rotor core, the upper bearing, and the lower bearing are fixed to the shaft,
it is characterized in that the method is characterized in that,
the shaft has a first outer diameter portion, a second outer diameter portion, a third outer diameter portion, and a fourth outer diameter portion,
the impeller and the upper bearing are fixed on the first outer diameter part,
the second outer diameter portion is disposed below the first outer diameter portion,
a rotor core is fixed to the third outer diameter portion, and the third outer diameter portion is disposed below the second outer diameter portion,
the lower bearing is fixed to the fourth outer diameter portion, and the fourth outer diameter portion is disposed below the third outer diameter portion,
the second outer diameter portion has an outer diameter larger than that of the first outer diameter portion,
the third outer diameter portion has an outer diameter smaller than an outer diameter of the second outer diameter portion,
the fourth outer diameter portion has an outer diameter smaller than an outer diameter of the third outer diameter portion.
2. A rotor assembly as set forth in claim 1,
the third outer diameter portion has an outer diameter larger than that of the first outer diameter portion.
3. A rotor assembly as set forth in claim 1,
a lower end portion of the first outer diameter portion and an upper end portion of the second outer diameter portion are connected by a first connecting portion expanding in a direction away from the central axis,
at least a portion of a lower surface of the upper bearing is in contact with an upper surface of the first connecting portion in an axial direction.
4. A rotor assembly as set forth in claim 1,
a lower end portion of the second outer diameter portion and an upper end portion of the third outer diameter portion are connected by a second connecting portion expanding in a direction away from the central axis,
at least a part of an upper surface of the rotor core is in contact with a lower surface of the second connecting portion in an axial direction.
5. A rotor assembly as set forth in claim 1,
a lower end portion of the third outer diameter portion and an upper end portion of the fourth outer diameter portion are connected by a third connecting portion expanding in a direction away from the central axis,
at least a portion of an upper surface of the lower bearing is in contact with a lower surface of the third connecting portion in the axial direction.
6. A rotor assembly as set forth in claim 1,
the centers of gravity of the shaft, the impeller, and the rotor core are arranged on the central axis,
the center of gravity is disposed axially between an upper end of the second outer diameter portion and a lower end of the second outer diameter portion.
7. A rotor assembly as set forth in claim 1,
the axial length of the first outer diameter portion is longer than the axial length of the second outer diameter portion,
the axial length of the third outer diameter portion is longer than the axial length of the second outer diameter portion,
the axial length of the fourth outer diameter portion is shorter than the axial length of the second outer diameter portion.
8. A rotor assembly as set forth in claim 1,
the sum of the axial length of the third outer diameter portion and the axial length of the fourth outer diameter portion is longer than the axial length of the first outer diameter portion.
9. An air supply device is characterized by comprising:
a rotor assembly as defined in any one of claims 1 to 8;
a motor capable of rotating the rotor assembly about the central axis; and
a housing enclosing a radially outer side of the rotor assembly.
10. A vacuum cleaner comprising the blower device according to claim 9.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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JP2020-190566 | 2020-11-16 | ||
JP2020190566A JP2022079382A (en) | 2020-11-16 | 2020-11-16 | Impeller, blower, and cleaner |
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CN216642554U true CN216642554U (en) | 2022-05-31 |
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ID=81707597
Family Applications (4)
Application Number | Title | Priority Date | Filing Date |
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CN202122792645.1U Active CN216649375U (en) | 2020-11-16 | 2021-11-15 | Motor, air supply device and dust collector |
CN202122784398.0U Active CN216642553U (en) | 2020-11-16 | 2021-11-15 | Impeller, air supply device and dust collector |
CN202122793523.4U Active CN216642554U (en) | 2020-11-16 | 2021-11-15 | Rotor assembly, air supply device and dust collector |
CN202122783847.XU Active CN216642552U (en) | 2020-11-16 | 2021-11-15 | Impeller, air supply device and dust collector |
Family Applications Before (2)
Application Number | Title | Priority Date | Filing Date |
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CN202122792645.1U Active CN216649375U (en) | 2020-11-16 | 2021-11-15 | Motor, air supply device and dust collector |
CN202122784398.0U Active CN216642553U (en) | 2020-11-16 | 2021-11-15 | Impeller, air supply device and dust collector |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
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CN202122783847.XU Active CN216642552U (en) | 2020-11-16 | 2021-11-15 | Impeller, air supply device and dust collector |
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JP (1) | JP2022079382A (en) |
CN (4) | CN216649375U (en) |
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2020
- 2020-11-16 JP JP2020190566A patent/JP2022079382A/en active Pending
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2021
- 2021-11-15 CN CN202122792645.1U patent/CN216649375U/en active Active
- 2021-11-15 CN CN202122784398.0U patent/CN216642553U/en active Active
- 2021-11-15 CN CN202122793523.4U patent/CN216642554U/en active Active
- 2021-11-15 CN CN202122783847.XU patent/CN216642552U/en active Active
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JP2022079382A (en) | 2022-05-26 |
CN216649375U (en) | 2022-05-31 |
CN216642553U (en) | 2022-05-31 |
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