CN203871938U - Motor rotor of rotary compressor - Google Patents
Motor rotor of rotary compressor Download PDFInfo
- Publication number
- CN203871938U CN203871938U CN201320849547.XU CN201320849547U CN203871938U CN 203871938 U CN203871938 U CN 203871938U CN 201320849547 U CN201320849547 U CN 201320849547U CN 203871938 U CN203871938 U CN 203871938U
- Authority
- CN
- China
- Prior art keywords
- rotor
- rotor section
- diameter
- section
- diameter rotor
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 229910000976 Electrical steel Inorganic materials 0.000 claims description 12
- 238000010030 laminating Methods 0.000 claims description 6
- 238000000034 method Methods 0.000 description 7
- 238000010586 diagram Methods 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- 238000007514 turning Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000004512 die casting Methods 0.000 description 2
- 230000007613 environmental effect Effects 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000011112 process operation Methods 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
Landscapes
- Iron Core Of Rotating Electric Machines (AREA)
- Manufacture Of Motors, Generators (AREA)
Abstract
The utility model discloses a motor rotor of a rotary compressor, which consists of a large-diameter rotor section and a small-diameter rotor section which are arranged along the axial direction, and the small-diameter rotor section is laminated on the large-diameter rotor section with the same axle center to form the whole motor rotor; the thickness ratio of the small-diameter rotor section to the large-diameter rotor section in the axial direction is 1: 4, make minor diameter rotor section and the major diameter rotor section of superpose in the downside form a circular shape step, make the unilateral clearance distance between minor diameter rotor section excircle and the interior circle of its complex stator be greater than the unilateral clearance that major diameter rotor section formed, like this, after the bent axle after the electric motor rotor hot jacket, can effectually avoid the bent axle to change the influence on electric motor rotor upper portion in the deflection of axial direction, reserve the step and satisfy electric motor rotor's hot jacket deformation needs, can make electric motor rotor directly assemble in electric motor stator, save current rotor excircle lathe work.
Description
[technical field]
The utility model relates to rotary compressor, relates in particular to the rotor of rotary compressor.
[background technology]
The rotor of rotary compressor, because of die casting, heat treatment, hot jacket heating and extruding, easily produces rotor punching local deformation, has affected rotor outer circle circularity, is assemblied in compressor and easily causes axiality, rotor to sweep the bad problems of motor such as hall, electromagnetism sound afterwards.Therefore, in order to improve the overall performance of compressor electric motor, the rotor core of many compressors is after on mould, die casting has laminated, as depicted in figs. 1 and 2, generally adopt the L section cylindrical to rotor core top on lathe to carry out the turning processing of taper theta angle, monolateral clearance distance between L section cylindrical and the stator inner circle on guarantee rotor core top is not less than 0.5mm, and whole making assembling process operation is many, and in cleaning, iron filings are many and more difficult; But in the course of processing, owing to can not effectively ensureing that the machining center of rotor outer circle and rotor center align, but in assembling process, the spindle central of motor is concentric with stator inner circle center, non-uniform air-gap when this just must cause work between rotor outer circle and stator inner circle, make the size of gaps in rotor operation process and between stator inner circle have variation, strengthen vibration and the unilateral magnetic force of motor in compressor rotation process, and the electric current producing on motor stator is caused to larger impact.
[utility model content]
It is a kind of simple in structure, easy to process that the utility model provides, and assembling is reliable, can save the rotor of the rotary compressor of rotor turning processing.
In order to realize above-mentioned utility model object, the technical solution adopted in the utility model is:
The rotor of rotary compressor, this rotor is made up of the large-diameter rotor section in axial direction arranging and minor diameter rotor section, minor diameter rotor section and large-diameter rotor section are in axial direction setting up and down, and laminating of minor diameter rotor section concentric forms whole rotor in large-diameter rotor section; Described minor diameter rotor section and large-diameter rotor section Thickness Ratio are in the axial direction 1:4; Described minor diameter rotor section and the large-diameter rotor section that is superimposed on downside form the step of a circle.
Preferably, the direct concentric of multiple major diameter silicon steel sheets that described large-diameter rotor section is stamped to form by major diameter diel is overrided to form.
Preferably, the direct concentric of multiple minor diameter silicon steel sheets that described minor diameter rotor section is stamped to form by minor diameter diel is overrided to form.
Preferably, the monolateral clearance distance between the stator inner circle that the large-diameter rotor section cylindrical of described rotor is mated is not less than 0.5mm.
Preferably, the monolateral clearance distance between the stator inner circle that the minor diameter rotor section cylindrical of described rotor is mated is not less than 0.7mm.
The beneficial effects of the utility model are:
Rotary compressor motor rotor of the present utility model adopts the structure of two section type, is made up of the large and small diameter rotor section in axial direction arranging, and laminating of minor diameter rotor section concentric forms whole rotor in large-diameter rotor section, because the silicon steel sheet diameter of minor diameter rotor section is less than the silicon steel sheet diameter of large-diameter rotor section, and the Thickness Ratio of minor diameter rotor section and large-diameter rotor section is 1:4 in the axial direction, make minor diameter rotor section and the large-diameter rotor section that is superimposed on downside form the step of a circle, make the monolateral clearance distance between stator inner circle that minor diameter rotor section cylindrical is mated be greater than the monolateral gap that large-diameter rotor section forms, like this, when after bent axle after rotor hot jacket, can effectively avoid bent axle in the axial direction amount of deflection change the impact on rotor top, reserved step meets the hot jacket distortion needs of rotor, can make rotor directly be assemblied in motor stator, save existing rotor outer circle turning manufacturing procedure, save processing cost, assembly technology is effectively improved simultaneously, save the rotor machining time, assembling process environmental protection and improved production efficiency.
[brief description of the drawings]
Fig. 1 is the main TV structure enlarged diagram of prior art rotor;
Fig. 2 is the plan structure enlarged diagram after prior art rotor and stator assembling;
Fig. 3 is the main TV structure enlarged diagram of rotor of the present utility model;
Fig. 4 is the plan structure enlarged diagram after rotor of the present utility model and stator assembling;
Fig. 5 is that the utility model rotor is installed on and in compressor, uses state cutaway view.
[embodiment]
The rotor of rotary compressor, as shown in Figures 3 to 5, this rotor is made up of the large-diameter rotor section 1 in axial direction arranging and minor diameter rotor section 2, minor diameter rotor section 2 is in axial direction setting up and down with large-diameter rotor section 1, and laminating of minor diameter rotor section 2 concentrics forms whole rotor in large-diameter rotor section 1; Minor diameter rotor section 2 is 1:4 with large-diameter rotor section 1 Thickness Ratio in the axial direction; Minor diameter rotor section 2 and the large-diameter rotor section 1 that is superimposed on downside form the step 3 of a circle.
Wherein, the direct concentric of multiple major diameter silicon steel sheets that large-diameter rotor section 1 is stamped to form by major diameter diel is overrided to form, and the direct concentric of multiple minor diameter silicon steel sheets that minor diameter rotor section 2 is stamped to form by minor diameter diel is overrided to form.
As shown in Figure 4, after rotor and stator assembling, monolateral clearance distance between stator 4 inner circles that large-diameter rotor section 1 cylindrical of rotor is mated is not less than 0.5mm, and the monolateral clearance distance between stator 4 inner circles that minor diameter rotor section 2 cylindricals of rotor are mated is not less than 0.7mm.
The rotor method for processing and assembling of this rotary compressor, comprises the following steps:
1), the direct concentric of multiple major diameter silicon steel sheets that is stamped to form by major diameter diel laminates and forms large-diameter rotor section 1, the monolateral clearance distance between stator 4 inner circles that large-diameter rotor section 1 cylindrical is mated is not less than 0.5mm;
2), the direct concentric of multiple minor diameter silicon steel sheets that is stamped to form by minor diameter diel laminates and forms minor diameter rotor section 2, the monolateral clearance distance between the stator inner circle that minor diameter rotor section 2 cylindricals are mated is not less than 0.7mm;
3), select minor diameter rotor section 2 and large-diameter rotor section 1 Thickness Ratio 1:4 in the axial direction;
4), in axial direction setting up and down laminating of minor diameter rotor section 2 concentrics formed to whole rotor in large-diameter rotor section 1, minor diameter rotor section 2 and the large-diameter rotor section 1 that is superimposed on downside form the step 3 of a circle;
5), the bent axle 5 concentric hot jackets assemblings of the minor diameter rotor section 2 after stack and large-diameter rotor section 1 and motor up and down;
6), hot jacket the rotor of bent axle 5 be directly assemblied in the stator 4 of compressor, complete the assembling of rotor.
Rotor of the present utility model adopts the structure of two section type, is made up of the large and small diameter rotor section in axial direction arranging, and laminating of minor diameter rotor section 2 concentrics forms whole rotor in large-diameter rotor section 1, because the silicon steel sheet diameter of minor diameter rotor section 2 is less than the silicon steel sheet diameter of large-diameter rotor section 1, and minor diameter rotor section 2 is 1:4 with the Thickness Ratio of large-diameter rotor section 1 in the axial direction, make minor diameter rotor section 2 and the large-diameter rotor section 1 that is superimposed on downside form the step 3 of a circle, make the monolateral clearance distance between stator 4 inner circles that minor diameter rotor section 2 cylindricals are mated be greater than the monolateral gap that large-diameter rotor section 1 forms, like this, when after bent axle 5 after rotor hot jacket, can effectively avoid bent axle 5 in the axial direction amount of deflection change the impact on rotor top, reserved step 3 meets the hot jacket distortion needs of rotor, can make rotor directly be assemblied in motor stator 4, save existing rotor outer circle turning manufacturing procedure, save processing cost, assembly technology is effectively improved simultaneously, save the rotor machining time, assembling process environmental protection and improved production efficiency.
The above embodiment just, for preferred embodiment of the present utility model, not limits practical range of the present utility model with this, and the equivalence that all shapes according to the utility model, structure and principle are done changes, and all should be covered by protection range of the present utility model.
Claims (5)
1. the rotor of rotary compressor, is characterized in that:
This rotor is made up of the large-diameter rotor section in axial direction arranging and minor diameter rotor section, minor diameter rotor section and large-diameter rotor section are in axial direction setting up and down, and laminating of minor diameter rotor section concentric forms whole rotor in large-diameter rotor section;
Described minor diameter rotor section and large-diameter rotor section Thickness Ratio are in the axial direction 1:4;
Described minor diameter rotor section and the large-diameter rotor section that is superimposed on downside form the step of a circle.
2. the rotor of rotary compressor according to claim 1, is characterized in that, the direct concentric of multiple major diameter silicon steel sheets that described large-diameter rotor section is stamped to form by major diameter diel is overrided to form.
3. the rotor of rotary compressor according to claim 1, is characterized in that, the direct concentric of multiple minor diameter silicon steel sheets that described minor diameter rotor section is stamped to form by minor diameter diel is overrided to form.
4. according to the rotor of the rotary compressor described in claim 1 or 2 or 3, it is characterized in that, the monolateral clearance distance between the stator inner circle that the large-diameter rotor section cylindrical of described rotor is mated is not less than 0.5mm.
5. according to the rotor of the rotary compressor described in claim 1 or 2 or 3, it is characterized in that, the monolateral clearance distance between the stator inner circle that the minor diameter rotor section cylindrical of described rotor is mated is not less than 0.7mm.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201320849547.XU CN203871938U (en) | 2013-12-20 | 2013-12-20 | Motor rotor of rotary compressor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201320849547.XU CN203871938U (en) | 2013-12-20 | 2013-12-20 | Motor rotor of rotary compressor |
Publications (1)
Publication Number | Publication Date |
---|---|
CN203871938U true CN203871938U (en) | 2014-10-08 |
Family
ID=51652860
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201320849547.XU Expired - Fee Related CN203871938U (en) | 2013-12-20 | 2013-12-20 | Motor rotor of rotary compressor |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN203871938U (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103840584A (en) * | 2013-12-20 | 2014-06-04 | 珠海凌达压缩机有限公司 | Motor rotor of rotary compressor and processing and assembling method thereof |
CN105356635A (en) * | 2015-11-02 | 2016-02-24 | 常州大学 | Rotor silicon steel sheet pile structure with low eddy current loss and device for closely fitting structure and shaft |
CN112968536A (en) * | 2019-12-12 | 2021-06-15 | 上海海立电器有限公司 | Motor core and compressor |
-
2013
- 2013-12-20 CN CN201320849547.XU patent/CN203871938U/en not_active Expired - Fee Related
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103840584A (en) * | 2013-12-20 | 2014-06-04 | 珠海凌达压缩机有限公司 | Motor rotor of rotary compressor and processing and assembling method thereof |
CN105356635A (en) * | 2015-11-02 | 2016-02-24 | 常州大学 | Rotor silicon steel sheet pile structure with low eddy current loss and device for closely fitting structure and shaft |
CN112968536A (en) * | 2019-12-12 | 2021-06-15 | 上海海立电器有限公司 | Motor core and compressor |
CN112968536B (en) * | 2019-12-12 | 2023-06-30 | 上海海立电器有限公司 | Motor stator core and compressor |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20141008 |