ROTARY COMPRESSOR
20180195512 ยท 2018-07-12
Assignee
Inventors
Cpc classification
F04C29/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04C2240/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04C29/0085
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04C2240/40
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04C29/068
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04C29/065
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04C23/008
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
A rotary compressor (100) includes a casing (1), an electric motor (2) and a compression mechanism (3), in which the electric motor (2) includes a stator core (21) and a rotor core (22), the compression mechanism (3) includes an air cylinder assembly (31) and a main bearing (32) connected to a side end face of the cylinder assembly (31) adjacent to the electric motor (2), the largest distance between a side end face of the stator core (21) adjacent to the first end wall (111) and the first end wall (111) is denoted by Dst, the smallest distance between a side end face of the rotor core (22) adjacent to the first end wall (111) and a side end face of a flange portion (321) of the main bearing (32) at one side adjacent to the first end wall (111) is denoted by Drt, in which Dst and Drt satisfy a relationship: 0.335?Dst/Drt?0.838.
Claims
1. A rotary compressor comprising: a casing, two ends of the casing in an axial direction having a first end wall and a second end wall respectively; an electric motor disposed in the casing and comprising a stator core and a rotor core, wherein in the axial direction of the casing, the largest distance between a side end face of the stator core adjacent to the first end wall and the first end wall is denoted by Dst; a compression mechanism disposed in the casing and located at one side of the electric motor far away from the first end wall, the compression mechanism comprising an air cylinder assembly and a main bearing, the main bearing being connected to a side end face of the cylinder assembly adjacent to the electric motor, wherein in the axial direction of the casing, the smallest distance between a side end face of the rotor core adjacent to the first end wall and a side end face of a flange portion of the main bearing adjacent to the first end wall is denoted by Drt; wherein, Dst and Drt satisfy a relationship: 0.335?Dst/Drt?0.838.
2. The rotary compressor according to claim 1, wherein Dst and Drt further satisfy a relationship: 0.568?Dst/Drt?0.680.
3. The rotary compressor according to claim 1, wherein an air hole is formed on and throughout the rotor core and a central axis of the air hole is parallel to a rotation axis of the rotor core.
4. The rotary compressor according to claim 3, wherein the air holes are axisymmetrically distributed about a first diameter of the rotor core and a width D of the air hole in a first diameter direction satisfies a relationship: 0.204 mm?D?0.480 mm.
5. The rotary compressor according to claim 4, wherein D further satisfies a relationship: 0.404 mm?D?0.460 mm.
6. The rotary compressor according to claim 3, wherein a contour of a cross section of the air hole is a curve or a combination of a curve and a straight line.
7. The rotary compressor according to claim 3, wherein in a rotation axis direction of the rotor core, the cross section of the air hole has the same shape and dimension.
8. The rotary compressor according to claim 3, wherein a plurality of air holes are provided and evenly spaced apart from one another along a circumferential direction of the rotor core.
9. The rotary compressor according to claim 8, wherein each air hole has the same shape and dimension.
10. The rotary compressor according to claim 1, wherein the rotor core is rotatably disposed inside the stator core.
11. The rotary compressor according to claim 4, wherein a contour of a cross section of the air hole is a curve or a combination of a curve and a straight line.
12. The rotary compressor according to claim 5, wherein a contour of a cross section of the air hole is a curve or a combination of a curve and a straight line.
13. The rotary compressor according to claim 4, wherein in a rotation axis direction of the rotor core, the cross section of the air hole has the same shape and dimension.
14. The rotary compressor according to claim 5, wherein in a rotation axis direction of the rotor core, the cross section of the air hole has the same shape and dimension.
15. The rotary compressor according to claim 6, wherein in a rotation axis direction of the rotor core, the cross section of the air hole has the same shape and dimension.
16. The rotary compressor according to claim 4, wherein a plurality of air holes are provided and evenly spaced apart from one another along a circumferential direction of the rotor core.
17. The rotary compressor according to claim 5, wherein a plurality of air holes are provided and evenly spaced apart from one another along a circumferential direction of the rotor core.
18. The rotary compressor according to claim 6, wherein a plurality of air holes are provided and evenly spaced apart from one another along a circumferential direction of the rotor core.
19. The rotary compressor according to claim 7, wherein a plurality of air holes are provided and evenly spaced apart from one another along a circumferential direction of the rotor core.
20. The rotary compressor according to claim 2, wherein the rotor core is rotatably disposed inside the stator core.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0016]
[0017]
[0018]
[0019]
[0020]
[0021]
REFERENCE NUMERALS
[0022] casing 1; first casing 11; first end wall 111; middle casing 12; second casing 13; second end wall 131;
[0023] electric motor 2; stator core 21; rotor core 22; air hole 221;
[0024] compression mechanism 3; air cylinder assembly 31; main bearing 32; flange portion 321;
[0025] crankshaft 4.
DETAILED DESCRIPTION
[0026] Reference will be made in detail to embodiments of the present disclosure. The same or similar elements and the elements having same or similar functions are denoted by like reference numerals throughout the descriptions. The embodiments described herein with reference to drawings are explanatory, illustrative, and used to generally understand the present disclosure. The embodiments shall not be construed to limit the present disclosure.
[0027] Various embodiments and examples are provided in the following description to implement different structures of the present disclosure. In order to simplify the present disclosure, certain elements and settings will be described. However, these elements and settings are only by way of example and are not intended to limit the present disclosure. In addition, reference numerals may be repeated in different examples in the present disclosure. This repeating is for the purpose of simplification and clarity and does not refer to relations between different embodiments and/or settings. Furthermore, examples of different processes and materials are provided in the present disclosure. However, it would be appreciated by those skilled in the art that other processes and/or materials may be also applied.
[0028] A rotary compressor 100 according to embodiments of the present disclosure will be described with reference to
[0029] Referring to
[0030] In which, two ends of the casing 1 in an axial direction have a first end wall 111 and a second end wall 131 respectively. For example in an embodiment shown in
[0031] Referring to
[0032] Further, any one of the first casing 11 and the second casing 13 may be integrated with the middle casing 12. Referring to
[0033] Specifically, the electric motor 2 is disposed in the casing 1 and includes a stator core 21 and a rotor core 22. In the axial direction of the casing 1 (for example, an up-down direction shown in
[0034] Further, the compression mechanism 3 is disposed in the casing 1 and is located at one side of the electric motor 2 far away from the first end wall 111. For example, in the embodiment shown in
[0035] Specifically, referring to
[0036] In which, Dst and Drt satisfy a relationship: 0.335?Dst/Drt?0.838. Referring to
[0037] It can be seen, by setting the ratio of Dst/Drt of the rotary compressor 100 as: 0.335?Dst/Drt?0.838, the working noise of the rotary compressor 100 may be reduced effectively.
[0038] In should be noted that, both the electric motor 2 and the compression mechanism 3 may be disposed coaxially with the casing 1, that is to say, a central axis of the crankshaft 4 and a central axis of the casing 1 are coincident, thereby a rotation axis of the rotor core 22 being coincident with the central axis of the casing 1, which means that both a central axis of the main bearing 32 and a central axis of the air cylinder assembly 31 are coincident with the central axis of the casing 1, thus the structure of the rotary compressor 100 being simple and reasonable, and the assembly of the rotary compressor 100 being convenient.
[0039] By configuring the value of Dst/Drt of the rotary compressor 100 according to embodiments of the present disclosure within a reasonable scope, the noise may be effectively reduced when the rotary compressor 100 is working, thereby the rotary compressor 100 having a simple and reasonable structure, easy assembly, low noise and the like advantages.
[0040] Preferably, Dst and Drt further satisfy a relationship: 0.568?Dst/Drt?0.680. For example, when Dst/Drt is equal to 0.58, 0.6 or 0.65, the working noise of the rotary compressor 100 is close to the minimum. It can be seen, by configuring the ratio of Dst/Drt of the rotary compressor 100 as: 0.568?Dst/Drt?0.680, the working noise of the rotary compressor 100 may be further reduced.
[0041] In some embodiments of the present disclosure, referring to
[0042] Further, a central axis of the air hole 221 is parallel to the rotation axis of the rotor core 22, for example, in the embodiment shown in
[0043] In some embodiments of the present disclosure, the air holes 221 are axisymmetrically distributed about a first diameter of the rotor core 22, a width D of the air hole 221 in the first diameter direction satisfies: 0.204 mm?D?0.480 mm. For example, in an embodiment shown in
[0044] It can be seen, by configuring the value of D of the air hole 221 of the rotary compressor 100 as: 0.204 mm?D?0.480 mm, the working noise of the rotary compressor 100 may be reduced effectively.
[0045] Preferably, D further satisfies a relationship: 0.404 mm?D?0.460 mm, fox example when D is equal to 0.41 mm, 0.43 mm or 0.45 mm, the working noise of the rotary compressor 100 is close to the minimum. It can be seen, by configuring the value of D of the air hole 221 of the rotary compressor 100 as: 0.404 mm?D?0.460 mm, the working noise of the rotary compressor 100 may be further reduced.
[0046] In some embodiments of the present disclosure, a contour of a cross section of the air hole 221 may be a curve or a combination of a curve and a straight line. For example, the cross section of the air hole 221 may be configured in the shape of a hollow curve (as shown in
[0047] In some embodiments of the present disclosure, in the rotation axis direction of the rotor core 22 (for example the up-down direction as shown in
[0048] In some embodiments of the present disclosure, referring to
[0049] Further, referring to
[0050] In some embodiments of the present disclosure, referring to
[0051] In addition, the other components, working principles and operation manners of the rotary compressor according to embodiments of the present disclosure are known to those skilled in the art, which will not be described herein. In the specification, it is to be understood that terms such as central, longitudinal, lateral, length, width, thickness, upper, lower, front, rear, left, right, vertical, horizontal, top, bottom, inner, outer, clockwise, and counterclockwise should be construed to refer to the orientation as then described or as shown in the drawings under discussion. These relative terms are for convenience of description and do not require that the present invention be constructed or operated in a particular orientation.
[0052] In addition, terms such as first and second are used herein for purposes of description and are not intended to indicate or imply relative importance or significance or to imply the number of indicated technical features. Thus, the feature defined with first and second may comprise one or more of this feature. In the description of the present invention, a plurality of means two or more than two, unless specified otherwise.
[0053] In the present invention, unless specified or limited otherwise, the terms mounted, connected, coupled, fixed and the like are used broadly, and may be, for example, fixed connections, detachable connections, or integral connections; may also be mechanical or electrical connections; may also be direct connections or indirect connections via intervening structures; may also be inner communications of two elements, which can be understood by those skilled in the art according to specific situations.
[0054] In the present invention, unless specified or limited otherwise, a structure in which a first feature is on or below a second feature may include an embodiment in which the first feature is in direct contact with the second feature, and may also include an embodiment in which the first feature and the second feature are not in direct contact with each other, but are contacted via an additional feature formed therebetween. Furthermore, a first feature on, above, or on top of a second feature may include an embodiment in which the first feature is right or obliquely on, above, or on top of the second feature, or just means that the first feature is at a height higher than that of the second feature; while a first feature below, under, or on bottom of a second feature may include an embodiment in which the first feature is right or obliquely below, under, or on bottom of the second feature, or just means that the first feature is at a height lower than that of the second feature.
[0055] Reference throughout this specification to an embodiment, some embodiments, one embodiment, another example, an example, a specific example, or some examples, means that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the present disclosure. Thus, the appearances of the phrases such as in some embodiments, in one embodiment, in an embodiment, in another example, in an example, in a specific example, or in some examples, in various places throughout this specification are not necessarily referring to the same embodiment or example of the present disclosure. Furthermore, the particular features, structures, materials, or characteristics may be combined in any suitable manner in one or more embodiments or examples.
[0056] Although explanatory embodiments have been shown and described, it would be appreciated by those skilled in the art that the above embodiments cannot be construed to limit the present disclosure, and changes, alternatives, and modifications can be made in the embodiments without departing from spirit, principles and scope of the present disclosure.