CN101113734B - Rotor type compressor - Google Patents

Rotor type compressor Download PDF

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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
Authority
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
Application number
CN2006101037028A
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Chinese (zh)
Other versions
CN101113734A (en
Inventor
云晓璎
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN2006101037028A priority Critical patent/CN101113734B/en
Priority to EP07785169.9A priority patent/EP2050964B1/en
Priority to CN2007800274989A priority patent/CN101490421B/en
Priority to PCT/CN2007/002254 priority patent/WO2008014688A1/en
Priority to US12/374,479 priority patent/US8075292B2/en
Publication of CN101113734A publication Critical patent/CN101113734A/en
Application granted granted Critical
Publication of CN101113734B publication Critical patent/CN101113734B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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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

Rotor-type compressor
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.
CN2006101037028A 2006-07-26 2006-07-26 Rotor type compressor Expired - Fee Related CN101113734B (en)

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)

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CN (2) CN101113734B (en)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (3)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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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Granted publication date: 20120502

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