CN101113734B - Rotor type compressor - Google Patents
Rotor type compressor Download PDFInfo
- Publication number
- CN101113734B CN101113734B CN2006101037028A CN200610103702A CN101113734B CN 101113734 B CN101113734 B CN 101113734B CN 2006101037028 A CN2006101037028 A CN 2006101037028A CN 200610103702 A CN200610103702 A CN 200610103702A CN 101113734 B CN101113734 B CN 101113734B
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- CN
- China
- Prior art keywords
- separating device
- rotor
- cylinder
- stator
- low pressure
- 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
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- Applications Or Details Of Rotary Compressors (AREA)
- Rotary Pumps (AREA)
Abstract
A rotor compressor, when the compressor has a single cylinder, comprises a cylinder body stator. A front end cap and a rear end cap are arranged on the front end face and the rear end face of the cylinder body stator. An eccentricity rotor that has a moving ring is arranged in the cylinder and does rotary motion around a central shaft, forming a crescent empty cavity. The crescent empty cavity isseparated into a high-pressure cavity and a low-pressure cavity by a separating device of a high-pressure cavity and a low-pressure cavity. A rotary shaft of the separating device is integrated with a stop dog. The rotary shaft of the stop dog is hidden in a shaft hole of radial cut opening of a stator inner cavity. The separating device is restrictively driven by a fixed cylinder of the moving ring on the rotor through a connector and does fan-shaped swing around the center of the open shaft hole to realize input and output liquid.
Description
Technical field:
The present invention relates to the energy conversion device that a kind of mechanical energy changes the pressure ability into, particularly a kind of rotor-type compressor.
Background technique:
Although existing rotor-type compressor has the incomparable advantage of other kind compressors; But owing to existing the processing technology complicacy, sealing insecure shortcoming; Especially the reliability of mechanical structure and sealing greatly reduces when volume strengthens, and therefore is difficult to improve swept volume.Cause the main cause of above-mentioned shortcoming to be that the separation block the sphere of activities of activity of separates chamber and low pressure chamber is little, reliability is relatively poor, when realizing increasing swept volume, processing technology is difficult to realize more.
Goal of the invention:
The object of the present invention is to provide rotor-type compressor, it can realize sealing more reliably between hyperbaric chamber and low pressure chamber, and can under the prerequisite of equal volume, weight, significantly increase swept volume.
Technological scheme:
To achieve these goals, the invention provides rotor-type compressor, when it is the single cylinder structure, comprise a cylinder body stator; Be assemblied in the front and rear cover on the cylinder body stator front/rear end; One is configured in the eccentric rotor that has rotating ring that cylinder interior rotates around central shaft, forms the crescent shape cavity; The separating device of one hyperbaric chamber and low pressure chamber is divided into hyperbaric chamber and low pressure chamber with the crescent shape cavity; The rotatingshaft and the block of separating device are integrated; The rotatingshaft of block is contained in the axis hole of the radially deep opening of bore of stator; Separating device has restrictedly through link under the drive of the stationary cylinder of epitrochanterian rotating ring; Separating device is that fan-shaped swing is done in the center of circle with the axis hole of opening, is accomplished the suction and the discharge of convection cell; The rotatingshaft of separating device is removed with the end face of end cap and is kept having no association outside the necessary axial fit clearance;
The suction port and the exhaust port of fluid are set in the front and back of the circumferencial direction of above-mentioned separating device; Suction port and exhaust port can be arranged on the stator, also can be arranged on the end cap.
According to one aspect of the invention, the block shaft of separating device, block can adopt any way to be fastenedly connected, and the hole in the cylindrical body center of circle is used for connector member, make the separating device of separates chamber and low pressure chamber and rotating ring remain coupled condition.
According to another aspect of the present invention, the link that connects separating device should be swung in the scalloped recess of cylindrical body both ends of the surface, and the opening of scalloped recess realizes being divided into prerequisite to guarantee hyperbaric chamber and low pressure chamber.
Another aspect of the present invention, described rotor-type compressor can be the multi-cylinder structures; In the multi-cylinder structure, realize that dynamic balancing is just passable as long as guarantee arranging of rotor.
Beneficial effect:
Because the separating device that the present invention adopted makes the volumetric efficiency of rotor-type compressor be greatly improved, structure is simpler, and manufacturability is more superior, and the condition of mechanical motion is especially reasonable, can further realize low noise, shockproof.
The drawing explanation:
Fig. 1 is a first embodiment of the present invention cross-section profile;
Realize the preferred embodiments of the present invention:
As shown in Figure 1, the rotor-type compressor of first embodiment of the invention comprises a cylinder block stator 1 and the eccentric rotor 3 that rotates around the axle center that has rotating ring 4, and rotor 3 is by key 5 circumferencial direction location on axle 2; Rotor 3 in motion as shown in the figure by block shaft 10, the block 11 of separating device; To be fixed on through link 7 that cylindrical body 6 links together on the rotating ring 4; Airtight crescent shape cavity is separated into hyperbaric chamber and low pressure chamber; Suck fluid by low pressure chamber suction port 12, will discharge fluid through the exhaust port 9 of hyperbaric chamber through the check valve 8 of any structure thereafter.
In conjunction with Fig. 1, provide each toponym of the present invention:
1. cylinder body stator;
The axle;
3. rotor;
4. rotating ring;
5. key;
6. cylindrical body;
7. link;
8. check valve;
9. exhaust port;
10. block shaft;
11. block;
12. suction port;
More than combine accompanying drawing and embodiment to describe the present invention; But those skilled in the art is to be understood that; The foregoing description only is an exemplary and nonrestrictive, under the condition that does not deviate from spirit and scope of the invention, can make all improvement to the foregoing description.For example: the shape of block and bearing are selected and can be adjusted according to practical application.
Claims (3)
1. a rotor-type compressor when it is the single cylinder structure, comprises a cylinder body stator; Be assemblied in the front and rear cover on the cylinder body stator front/rear end; One is configured in the eccentric rotor that has rotating ring that cylinder interior rotates around central shaft, forms the crescent shape cavity; The separating device of one hyperbaric chamber and low pressure chamber is divided into hyperbaric chamber and low pressure chamber with the crescent shape cavity; The rotatingshaft and the block of separating device are integrated; The rotatingshaft of block is contained in the axis hole of the radially deep opening of bore of stator; Separating device has restrictedly through link, under the drive of the stationary cylinder of epitrochanterian rotating ring; Axis hole with opening is that fan-shaped swing is done in the center of circle, is accomplished the suction and the discharge of convection cell; The rotatingshaft of separating device is removed with the end face of end cap and is kept having no association outside the necessary axial fit clearance; Block shaft, the block of separating device are fastenedly connected, and the hole in the cylindrical body center of circle is used for connector member, make the separating device of separates chamber and low pressure chamber and rotating ring remain coupled condition; The link that connects separating device should be swung in the scalloped recess of cylindrical body both ends of the surface, and the opening of scalloped recess realizes being divided into prerequisite to guarantee hyperbaric chamber and low pressure chamber.
2. rotor compressor as claimed in claim 1 is provided with the suction port and the exhaust port of fluid in the front and back of the circumferencial direction of above-mentioned separating device; Suction port and exhaust port can be arranged on the stator, also can be arranged on the end cap.
3. rotor compressor as claimed in claim 1 can be the multi-cylinder structure; In the multi-cylinder structure, the realization dynamic balancing of arranging of rotor.
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2006101037028A CN101113734B (en) | 2006-07-26 | 2006-07-26 | Rotor type compressor |
EP07785169.9A EP2050964B1 (en) | 2006-07-26 | 2007-07-25 | A rotary piston compressor |
CN2007800274989A CN101490421B (en) | 2006-07-26 | 2007-07-25 | Rotor compressor |
PCT/CN2007/002254 WO2008014688A1 (en) | 2006-07-26 | 2007-07-25 | A rotary piston compressor |
US12/374,479 US8075292B2 (en) | 2006-07-26 | 2007-07-25 | Eccentric rotor compressor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2006101037028A CN101113734B (en) | 2006-07-26 | 2006-07-26 | Rotor type compressor |
Publications (2)
Publication Number | Publication Date |
---|---|
CN101113734A CN101113734A (en) | 2008-01-30 |
CN101113734B true CN101113734B (en) | 2012-05-02 |
Family
ID=39022227
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2006101037028A Expired - Fee Related CN101113734B (en) | 2006-07-26 | 2006-07-26 | Rotor type compressor |
CN2007800274989A Expired - Fee Related CN101490421B (en) | 2006-07-26 | 2007-07-25 | Rotor compressor |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2007800274989A Expired - Fee Related CN101490421B (en) | 2006-07-26 | 2007-07-25 | Rotor compressor |
Country Status (1)
Country | Link |
---|---|
CN (2) | CN101113734B (en) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101864991A (en) * | 2010-06-10 | 2010-10-20 | 姚镇 | Star rotary fluid motor or engine and compressor and pump |
CN102678182B (en) * | 2011-03-17 | 2013-12-18 | 北京星旋世纪科技有限公司 | Star-spinning type rotation device with double sun wheels, engine and fluid machine |
CN102678289B (en) * | 2011-03-17 | 2014-02-12 | 北京星旋世纪科技有限公司 | Spiraster-type rotation device, engine, pneumatic motor, and compressor |
CN102230446A (en) * | 2011-05-06 | 2011-11-02 | 曾梓 | Hydraulic power machine |
CN102808654B (en) * | 2011-05-31 | 2014-04-30 | 北京星旋世纪科技有限公司 | Rotating valve mechanism and planetary rotating device using same |
CN103967787B (en) | 2013-01-25 | 2016-02-17 | 北京星旋世纪科技有限公司 | Slewing gear and apply its rotor-type compressor and fluid motor |
CN104100299B (en) * | 2013-04-12 | 2016-05-25 | 北京星旋世纪科技有限公司 | Tumbler and apply its fluid motor, engine, compressor and pump |
WO2015131633A1 (en) * | 2014-03-06 | 2015-09-11 | 艾默生环境优化技术(苏州)有限公司 | Rolling rotor type compression mechanism and compressor comprising mechanism |
CN106014989A (en) * | 2016-07-03 | 2016-10-12 | 南通广兴气动设备有限公司 | Spinning vacuum pump |
CN106015003A (en) * | 2016-07-03 | 2016-10-12 | 南通广兴气动设备有限公司 | Spinning high pressure air pump |
CN105667749A (en) * | 2016-03-18 | 2016-06-15 | 曾梓 | Bionic propeller |
CN106050652A (en) * | 2016-07-27 | 2016-10-26 | 王鼎兴 | Disc pump with elastic return rods |
CN108087251A (en) * | 2017-12-26 | 2018-05-29 | 宁波新邦工具有限公司 | A kind of rotator type compressed air generating means |
CN109654020A (en) * | 2018-12-13 | 2019-04-19 | 宁波甬微集团有限公司 | A kind of compressor assembly and preparation method thereof |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1204010A (en) * | 1998-05-08 | 1999-01-06 | 云晓璎 | Rotor pump |
CN1482362A (en) * | 2003-02-12 | 2004-03-17 | Rotary pump | |
CN1707110A (en) * | 2004-06-11 | 2005-12-14 | 云晓璎 | Rotor pump |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SU1779786A1 (en) * | 1989-08-25 | 1992-12-07 | Izmalkov German | Rotary pump |
DE4010755C2 (en) * | 1990-04-04 | 1998-11-05 | Pierburg Ag | Vane cell or swivel vane vacuum pump |
RU2103553C1 (en) * | 1994-08-31 | 1998-01-27 | Научно-производственное управление акционерного общества "Оренбургнефть" | Pump |
CN1078680C (en) * | 1999-01-26 | 2002-01-30 | 付云树 | Compressor with hinged arc blades and rolling rotor |
-
2006
- 2006-07-26 CN CN2006101037028A patent/CN101113734B/en not_active Expired - Fee Related
-
2007
- 2007-07-25 CN CN2007800274989A patent/CN101490421B/en not_active Expired - Fee Related
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1204010A (en) * | 1998-05-08 | 1999-01-06 | 云晓璎 | Rotor pump |
CN1482362A (en) * | 2003-02-12 | 2004-03-17 | Rotary pump | |
CN1707110A (en) * | 2004-06-11 | 2005-12-14 | 云晓璎 | Rotor pump |
Non-Patent Citations (1)
Title |
---|
CN 1204010 A,全文. |
Also Published As
Publication number | Publication date |
---|---|
CN101490421A (en) | 2009-07-22 |
CN101113734A (en) | 2008-01-30 |
CN101490421B (en) | 2011-03-23 |
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Legal Events
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C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120502 Termination date: 20140726 |
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EXPY | Termination of patent right or utility model |