CN101806304A - Rotary compressor with axial thrust of crankshaft - Google Patents
Rotary compressor with axial thrust of crankshaft Download PDFInfo
- Publication number
- CN101806304A CN101806304A CN200910244340A CN200910244340A CN101806304A CN 101806304 A CN101806304 A CN 101806304A CN 200910244340 A CN200910244340 A CN 200910244340A CN 200910244340 A CN200910244340 A CN 200910244340A CN 101806304 A CN101806304 A CN 101806304A
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- China
- Prior art keywords
- lower flange
- rotary compressor
- crankshaft
- supporting spring
- eccentric crankshaft
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Abstract
The invention relates to the technical field of refrigeration compressors, in particular to a rotary compressor with the axial thrust of a crankshaft. A supporting spring is arranged on the lower end face of a lower flange of the rotary compressor and supports the tail end face of the eccentric crankshaft; the gravity generated by bearing the eccentric crankshaft and a motor rotor arranged at the upper end of the eccentric crankshaft through the eccentric crankshaft is mostly borne by the supporting spring; and in the working process, the current situation that a contact surface of a lower thrust surface and the lower flange bears most gravity is avoided, the friction and wear of the lower thrust surface and the lower flange are reduced, the eccentric crankshaft is prevented from being loosened in an air cylinder, the compressor works more stably, the noise is reduced, the reliability is strengthened, the energy efficiency is effectively improved, and the service life of the compressor is effectively prolonged.
Description
Technical field
The present invention relates to technical field of refrigeration compressors, relate in particular to a kind of rotary compressor with axial thrust of crankshaft.
Background technique
Compressor is that compression refrigerant makes it participate in the circuit nucleus equipment in refrigerator, the air-conditioning system, rotary compressor is a kind of compressor commonly used, the structure of existing rotary compressor is as shown in Figure 1: include upper flange 1, lower flange 2, cylinder 3, eccentric crankshaft 4, upper flange 1, lower flange 2 lids are located at the two ends of cylinder 3, eccentric crankshaft 4 wore upper flange 1, lower flange 2, and the eccentric part 44 of eccentric crankshaft 4 and the upper and lower thrust surface of eccentric part 44 41,42 are arranged between the upper and lower flange 1,2.In existing compressor, on the eccentric crankshaft 4, following thrust surface 41,42 contact respectively near last, lower flange 1,2 end face, be used to reduce eccentric crankshaft 4 and upper flange 1, thereby long-pending the reducing of the direct contact surface between the lower flange 2 rubs, but because eccentric crankshaft 4 carrying self and the weight that is arranged on eccentric crankshaft 4 upper end rotors 8, the gravity major part that is produced is all born by the following thrust surface 42 and the contacting point of lower flange 2, therefore in the course of the work, following thrust surface 42 is more serious with the abrasion condition of the surface of contact of lower flange 2, cause friction to increase after the wearing and tearing, eccentric crankshaft 4 is loosening in cylinder 3, thereby makes the compressor operating instability, noise increases, poor reliability, efficiency reduces, shorten the life-span of compressor.
Summary of the invention
Of the present invention is big at the following thrust surface of the eccentric crankshaft of present rotary compressor and lower flange fretting wear and problem that produce, and a kind of exhaust device of rotary compressor that overcomes the above problems is provided.
For reaching above purpose, adopt following technological scheme:
A kind of rotary compressor with axial thrust of crankshaft, described rotary compressor includes upper flange, lower flange, cylinder, eccentric crankshaft, upper flange, lower flange lid are located at the two ends of cylinder, eccentric crankshaft wore upper flange, lower flange, and the upper and lower thrust surface of the eccentric part of eccentric crankshaft is arranged between the upper and lower flange; The lower end surface of described lower flange is provided with supporting spring, and described supporting spring is held the breech face of eccentric crankshaft.
The gap, upper-end surface of wherein said thrust surface down and lower flange is provided with.
Wherein said supporting spring and lower flange design for one.
Be provided with a wear plate between the breech face of wherein said supporting spring and eccentric crankshaft.
Wherein said supporting spring and lower flange design for split.
Wherein said lower flange lower end surface is provided with groove, and supporting spring is arranged in the groove.
Wherein said supporting spring and lower flange are bolted to connection.
The gap, upper-end surface of wherein said thrust surface down and lower flange is D, and the span of D is: 0.2≤D≤1.0mm.
Wherein said rotary compressor is single cylinder rotary compressor or duplex-cylinder rotary compressor.
Beneficial effect of the present invention is: the lower end surface of rotary compressor lower flange of the present invention is provided with supporting spring, and supporting spring is held the breech face of eccentric crankshaft; Eccentric crankshaft carrying self and the gravity major part that weight produced that is arranged on eccentric crankshaft upper end rotor are born by supporting spring, in the course of the work, avoid the surface of contact of thrust surface and lower flange under the prior art to bear the present situation of main gravity, reduced the friction of time thrust surface and lower flange, reduce both wearing and tearing, avoid eccentric crankshaft loosening in cylinder, compressor operating is stable more, noise reduces, reliability strengthens, efficiency is effectively promoted, and prolongs the working life of compressor.
Description of drawings
Fig. 1 is a prior art rotary compressor structural representation;
Fig. 2 is the embodiment of the invention 1 structural representation;
Fig. 3 is the embodiment of the invention 2 structural representations;
Fig. 4 is the embodiment of the invention 3 structural representations;
Fig. 5 is the embodiment of the invention 4 structural representations.
Embodiment
Below in conjunction with accompanying drawing the present invention is further specified:
Embodiment 1, as shown in Figure 2: a kind of rotary compressor with axial thrust of crankshaft, rotary compressor is single cylinder rotary compressor or duplex-cylinder rotary compressor, as present embodiment is the single cylinder rotary compressor, rotary compressor includes upper flange 1, lower flange 2, cylinder 3, eccentric crankshaft 4, upper flange 1, lower flange 2 lids are located at the two ends of cylinder 3, eccentric crankshaft 4 wore upper flange 1, lower flange 2, on the eccentric part 44 of eccentric crankshaft 4 and the eccentric part 44, following thrust surface 41,42 are arranged on, lower flange 1, between 2, the upper end outside cylinder 3 of eccentric crankshaft 4 is provided with rotor 8, the lower end surface 21 of lower flange 2 is provided with supporting spring 5, and supporting spring 5 is held the breech face 43 of eccentric crankshaft 4; In the present embodiment, supporting spring 5 and the design of lower flange 2 one, step-like convex ring plate is arranged in axis hole 23 lower ends of lower flange 2, and the convex ring plate forms supporting spring 5, and supporting spring 5 is held the breech face 43 of eccentric crankshaft 4; The gravity that rotary compressor eccentric crankshaft 4 under this configuration state and rotor 8 are produced all has supporting spring 5 to bear.
The above embodiment, it is the preferred embodiments of type of the present invention, be not to limit the scope of the present invention,, all should be included in the patent claim of the present invention so all equivalences of doing according to the described structure of the present patent application claim, feature and principle change or modify.
Claims (9)
1. rotary compressor with axial thrust of crankshaft, described rotary compressor includes upper flange (1), lower flange (2), cylinder (3), eccentric crankshaft (4), upper flange (1), lower flange (2) lid are located at the two ends of cylinder (3), eccentric crankshaft (4) wore upper flange (1), lower flange (2), and the upper and lower thrust surface of the eccentric part of eccentric crankshaft (4) (41,42) is arranged between the upper and lower flange (1,2); It is characterized in that the lower end surface (21) of described lower flange (2) is provided with supporting spring (5), described supporting spring (5) is held the breech face (43) of eccentric crankshaft (4).
2. the rotary compressor with axial thrust of crankshaft according to claim 1 is characterized in that, described thrust surface (42) down is provided with the gap, upper-end surface (22) of lower flange (2).
3. the rotary compressor with axial thrust of crankshaft according to claim 1 is characterized in that, described supporting spring (5) designs for one with lower flange (2).
4. the rotary compressor with axial thrust of crankshaft according to claim 3 is characterized in that, is provided with a wear plate (6) between the breech face (43) of described supporting spring (5) and eccentric crankshaft (4).
5. the rotary compressor with axial thrust of crankshaft according to claim 1 is characterized in that, described supporting spring (5) designs for split with lower flange (2).
6. the rotary compressor with axial thrust of crankshaft according to claim 5 is characterized in that, described lower flange (2) lower end surface (21) is provided with groove (211), and supporting spring (5) is arranged in the groove (211).
7. the rotary compressor with axial thrust of crankshaft according to claim 5 is characterized in that, described supporting spring (5) is fixedlyed connected by bolt (7) with lower flange (2).
8. the rotary compressor with axial thrust of crankshaft according to claim 2 is characterized in that, described thrust surface (42) down is D with the gap, upper-end surface (22) of lower flange (2), and the span of D is: 0.2 mm≤D≤1.0mm.
9. have the rotary compressor of axial thrust of crankshaft according to described any one of claim 1-8, it is characterized in that, described rotary compressor is single cylinder rotary compressor or duplex-cylinder rotary compressor.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2009102443408A CN101806304B (en) | 2009-12-31 | 2009-12-31 | Rotary compressor with axial thrust of crankshaft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2009102443408A CN101806304B (en) | 2009-12-31 | 2009-12-31 | Rotary compressor with axial thrust of crankshaft |
Publications (2)
Publication Number | Publication Date |
---|---|
CN101806304A true CN101806304A (en) | 2010-08-18 |
CN101806304B CN101806304B (en) | 2012-07-25 |
Family
ID=42608220
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2009102443408A Ceased CN101806304B (en) | 2009-12-31 | 2009-12-31 | Rotary compressor with axial thrust of crankshaft |
Country Status (1)
Country | Link |
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CN (1) | CN101806304B (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104653459A (en) * | 2014-12-12 | 2015-05-27 | 广东美芝制冷设备有限公司 | Compressor |
CN104728112A (en) * | 2013-12-20 | 2015-06-24 | 珠海格力节能环保制冷技术研究中心有限公司 | Cylinder and compressor |
CN106089718A (en) * | 2016-07-28 | 2016-11-09 | 珠海格力节能环保制冷技术研究中心有限公司 | A kind of compressor pump and compressor |
CN106368951A (en) * | 2016-10-18 | 2017-02-01 | 珠海格力节能环保制冷技术研究中心有限公司 | Rotary compressor |
CN108547769A (en) * | 2018-07-18 | 2018-09-18 | 珠海格力节能环保制冷技术研究中心有限公司 | The pump housing and compressor |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN2284310Y (en) * | 1996-06-21 | 1998-06-17 | 林长春 | Steering ball joint |
CN201090418Y (en) * | 2007-09-17 | 2008-07-23 | 马宝忠 | Hydraulic pressure-driven gear oil well pump |
CN201636009U (en) * | 2009-12-31 | 2010-11-17 | 珠海格力电器股份有限公司 | Rotary compressor with crankshaft axial thrust |
-
2009
- 2009-12-31 CN CN2009102443408A patent/CN101806304B/en not_active Ceased
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104728112A (en) * | 2013-12-20 | 2015-06-24 | 珠海格力节能环保制冷技术研究中心有限公司 | Cylinder and compressor |
CN104728112B (en) * | 2013-12-20 | 2017-05-31 | 珠海格力节能环保制冷技术研究中心有限公司 | Cylinder and compressor |
CN104653459A (en) * | 2014-12-12 | 2015-05-27 | 广东美芝制冷设备有限公司 | Compressor |
CN106089718A (en) * | 2016-07-28 | 2016-11-09 | 珠海格力节能环保制冷技术研究中心有限公司 | A kind of compressor pump and compressor |
CN106368951A (en) * | 2016-10-18 | 2017-02-01 | 珠海格力节能环保制冷技术研究中心有限公司 | Rotary compressor |
WO2018072497A1 (en) * | 2016-10-18 | 2018-04-26 | 珠海格力节能环保制冷技术研究中心有限公司 | Rotary compressor |
CN108547769A (en) * | 2018-07-18 | 2018-09-18 | 珠海格力节能环保制冷技术研究中心有限公司 | The pump housing and compressor |
CN108547769B (en) * | 2018-07-18 | 2023-08-25 | 珠海格力节能环保制冷技术研究中心有限公司 | Pump body and compressor |
Also Published As
Publication number | Publication date |
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CN101806304B (en) | 2012-07-25 |
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Decision date of declaring invalidation: 20150304 Decision number of declaring invalidation: 25317 Granted publication date: 20120725 |