CN204941932U - A kind of oil-free vortex air compressor - Google Patents
A kind of oil-free vortex air compressor Download PDFInfo
- Publication number
- CN204941932U CN204941932U CN201520682016.5U CN201520682016U CN204941932U CN 204941932 U CN204941932 U CN 204941932U CN 201520682016 U CN201520682016 U CN 201520682016U CN 204941932 U CN204941932 U CN 204941932U
- Authority
- CN
- China
- Prior art keywords
- bearing
- orbiter
- frame
- thrust
- locating tab
- 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
Landscapes
- Rotary Pumps (AREA)
Abstract
The utility model relates to a kind of oil-free vortex air compressor, and comprise fixed scroll, orbiter, bent axle, frame, main equilibrium block, belt pulley, intakeport and relief opening, described orbiter engages the compression chamber forming air with fixed scroll; Bent axle is arranged in frame with main bearing and supplementary bearing, a Roller Disc structure is provided with between orbiter and frame, this Roller Disc structure includes the fixed base being arranged on frame, fixed base is provided with a radial bearing and a thrust-bearing, described fixed base is provided with a mounting hole, radial bearing is fixed in mounting hole, is arranged on the eccentric shaft of bent axle one end; Described thrust-bearing is fixed on fixed base side, is adjacent in frame side; Described radial bearing and thrust-bearing are concentric shafts, thrust block ring is enclosed within outside radial bearing, when orbiter and fixed scroll are relatively rotated, orbiter drives eccentric rotary by radial bearing on eccentric shaft, and by thrust-bearing position rotating, make between orbiter and fixed scroll, to keep good phase difference.The utility model has that structure is simple, cost is low and the feature such as rotating property is stable.
Description
Technical field
The utility model relates to a kind of air compressor, is specifically related in a kind of oil-free vortex air compressor.
Background technique
Scroll air compressor is high with its efficiency, noise is low, volume is little, be conducive to the advantages such as energy-conservation and protection of the environment and be widely used in the industries such as industry, agricultural, communications and transportation needing compressed-air actuated occasion.Scroll air compressor mainly runs the dish engagement of part whirlpool, and do not produce wearing and tearing, thus the life-span is longer than piston type, screw compressor, is pneumatic machinery ideal power source.In scroll air compressor, main operation part whirlpool dish is divided into orbiter and fixed scroll, vortex sheet is established in orbiter and fixed scroll, usually, be bonded to each other by orbiter and fixed scroll and form compression chamber, when orbiter does translation by bent axle drive along certain circular path, orbiter vortex sheet moves relative to fixed scroll vortex sheet, namely the compression chamber formed by both moves and changes its volume, thus suck, compression, discharge, complete compressed-air actuated process, but orbiter and fixed scroll rely on and bent axle arranges two bearings fix, when high speed rotating, cooperation between orbiter and fixed scroll is affected displacement, frictional force is each other caused to increase, affect orbiter rotational stability.
Tradition oil spout air eddy compressor, compression chamber needs oil spout to carry out lubrication and cooling, and each bearing portion also needs the lubrication and cooling of lubricant oil, and lubricant oil discharges exhaust outlet of compressor together with pressurized gas.Lubricant oil in pressurized air needs to adopt the means be separated and filter it to be separated from pressurized air, such system just must consider separation and the cooling of oil, several grades of process must be adopted just to reach the requirement of pressurized air oil-containing before use pressurized air.The design of oil spout air eddy compressor assembly is complicated, and low oil-containing pressurized air needs to expend more cost, and lubricant oil can cause the destruction of environment.
Model utility content
The purpose of this utility model is, having above-mentioned deficiency, providing a kind of oil-free vortex air compressor to solve existing air eddy compressor.
The purpose of this utility model can be achieved through the following technical solutions:
A kind of oil-free vortex air compressor, comprise fixed scroll, orbiter, bent axle, frame, main equilibrium block, belt pulley, intakeport and relief opening, described orbiter engages the compression chamber forming air with fixed scroll; Bent axle is arranged in frame with main bearing and supplementary bearing, a Roller Disc structure is provided with between orbiter and frame, this Roller Disc structure includes the fixed base being arranged on frame, fixed base is provided with a radial bearing and a thrust-bearing, described fixed base is provided with a mounting hole, radial bearing is fixed in mounting hole, is arranged on the eccentric shaft of bent axle one end; Described thrust-bearing is fixed on fixed base side, is adjacent in frame side; Described radial bearing and thrust-bearing are concentric shafts, thrust block ring is enclosed within outside radial bearing, when orbiter and fixed scroll are relatively rotated, orbiter drives eccentric rotary by radial bearing on eccentric shaft, and by thrust-bearing position rotating, make between orbiter and fixed scroll, to keep good phase difference.
The purpose of this utility model can also be achieved through the following technical solutions:
Further, the fixed base of described Roller Disc structure is a ring part, the endoporus of this ring part is the mounting hole of fixed base, ring part side is provided with the annular mounting groove with mounting hole concentric, described radial bearing is arranged on the endoporus position of ring part, and thrust-bearing is arranged in annular mounting groove.
Further, described thrust-bearing includes the multiple steel balls being located at annular mounting groove, steel ball is provided with annular locating tab and lower annular locating tab on one, on this, annular locating tab and the equal annular spread of lower annular locating tab have the positioning through hole of fixing steel ball, and described steel ball is located at position between annular locating tab and positioning through hole corresponding to lower annular locating tab.
Further, described upper annular locating tab is screwed on fixed base, and lower annular locating tab is screwed in frame.
Further, the Smooth annular egative film of hard, wear-resistant is also provided with inside described upper annular locating tab, this Smooth annular egative film is located at bottom the annular mounting groove of fixed base, also be provided with the lower smooth annular egative film of hard, wear-resistant inside lower annular locating tab, this lower annular locating tab is located at bottom circular mounting hole that frame is established.
Further, described bent axle is provided with a fan, and this fan is the blade be arranged on bent axle, and this blade rotates with the rotation of bent axle, and fan is positioned at Roller Disc structure side, acts on Roller Disc inside configuration quick heat radiating.
Further, described Roller Disc structure is made by high tensile steel material, and heat treatment hardness value is at more than HRC50.
The beneficial effects of the utility model:
1, the orbiter in the utility model is rotationally connected by Roller Disc respective outer side edges, drives the crank rotation of orbiter in frame by radial bearing and thrust-bearing.Thus, the phase angle of orbiter and fixed scroll can be kept, reduce friction, have that structure is simple, cost is low and the feature such as rotating property is stable.
2, Roller Disc structure of the present utility model includes fixed base, radial bearing and thrust-bearing, and its structure is simple, and quick and easy for installation, compressor arrangement is compact, therefore, can effectively reduce fabricating cost of the present utility model.
3, thrust-bearing of the present utility model includes the multiple steel balls being located at annular mounting groove, steel ball is provided with annular locating tab and lower annular locating tab on one, on this, annular locating tab and the equal annular spread of lower annular locating tab have the positioning through hole of fixing steel ball, and described steel ball is located at position between annular locating tab and positioning through hole corresponding to lower annular locating tab.Described upper annular locating tab is screwed on fixed base, and lower annular locating tab is screwed in frame.The Smooth annular egative film of hard, wear-resistant is also provided with inside described upper annular locating tab, this Smooth annular egative film is located at bottom the annular mounting groove of fixed base, also be provided with the lower smooth annular egative film of hard, wear-resistant inside lower annular locating tab, this lower annular locating tab is located at bottom circular mounting hole that frame is established.Thus, in use, thrust-bearing better makes orbiter rotate in frame, ensures the phase difference between it simultaneously, makes its rotating property more stable.
4, the cooling fan that is provided with in operation process of the present utility model cools compression chamber and bearing movable position, and main bearing and supplementary bearing adopt seal gease lubrication deep groove ball bearing, adopt and regularly inject and change lubricating grease in Roller Disc structure.Effectively can improve using effect thus, so that reach effect of energy-conserving and environment-protective.
Accompanying drawing explanation
Fig. 1 is the utility model compressor overall schematic.
Fig. 2 is the structural representation of the utility model Roller Disc structure.
Fig. 3 is the scheme of installation of Fig. 2.
Fig. 4 is the structural representation of the utility model Roller Disc structure installment in frame.
Fig. 5 is the scheme of installation of Fig. 4.
Embodiment
Below in conjunction with accompanying drawing, the utility model is described in further detail.
Referring to figs. 1 through a kind of oil-free vortex air compressor shown in Fig. 5, comprise fixed scroll 1, orbiter 2, bent axle 4, frame 5, main equilibrium block 6, belt pulley 9, intakeport and relief opening, described orbiter 2 engages with fixed scroll 1 compression chamber forming air; Bent axle 4 is arranged in frame 5 with main bearing 18 and supplementary bearing 17, a Roller Disc structure 3 is provided with between orbiter 2 and frame 5, this Roller Disc structure 3 includes the fixed base 31 being arranged on frame 5, fixed base 31 is provided with radial bearing 32 and a thrust-bearing 33, described fixed base 31 is provided with a mounting hole 312, radial bearing 32 is fixed in mounting hole 312, is arranged on the eccentric shaft 34 of bent axle 4 one end; Described thrust-bearing 33 is fixed on fixed base 31 side, is adjacent in frame 5 side; Described radial bearing 32 and thrust-bearing 33 are concentric shafts, thrust-bearing 33 ring set is outside radial bearing 32, when orbiter 2 and fixed scroll 1 are relatively rotated, orbiter 2 drives eccentric rotary by radial bearing 32 on eccentric shaft 34, and by thrust-bearing 33 position rotating, make to keep good phase difference between orbiter 2 and fixed scroll 1.
Concrete, the fixed base 31 of described Roller Disc structure 3 is a ring part, the endoporus of this ring part is the mounting hole 312 of fixed base 31, ring part side is provided with the annular mounting groove 311 with mounting hole 312 concentric, described radial bearing 32 is arranged on the endoporus position of ring part, and thrust-bearing 33 is arranged in annular mounting groove 311.
Described thrust-bearing 33 includes the multiple steel ball 3-3 being located at annular mounting groove 311, steel ball 3-3 is provided with annular locating tab 3-2 and lower annular locating tab 3-4 on, on this, annular locating tab 3-2 and the equal annular spread of lower annular locating tab 3-4 have the positioning through hole 3-41 of fixing steel ball 3-3, and described steel ball 3-3 is located at position between positioning through hole 3-41 corresponding to annular locating tab 3-2 and lower annular locating tab 3-4.Described upper annular locating tab 3-2 is fixed on fixed base 31 by screw 3-6, and be also provided with the Smooth annular egative film 3-1 of hard, wear-resistant inside upper annular locating tab 3-2, Smooth annular egative film 3-1 is located at bottom the annular mounting groove 311 of fixed base 31.Described lower annular locating tab 3-4 is fixed in frame 5 by screw 3-6.Also be provided with the lower smooth annular egative film 3-5 of hard, wear-resistant inside lower annular locating tab 3-4, this lower annular locating tab 3-4 is located at bottom circular mounting hole 51 that frame 5 is established.
In order to increase working life and the effect of compressor, described bent axle 4 is provided with the fan 7 for dispelling the heat, this fan 7 is for being arranged on the blade on bent axle, this blade rotates with the rotation of bent axle 4, fan 7 arranges a fan guard 8, this fan 7 is positioned at Roller Disc structure 3 side, the inner quick heat radiating of effect Roller Disc structure 3.Described Roller Disc structure 3 is made by high tensile steel material, and heat treatment hardness value is at more than HRC50.Specifically, each parts such as described fixed base 31, upper annular locating tab 3-2, lower annular locating tab 3-4, screw 3-6, Smooth annular egative film 3-1, smooth annular egative film 3-5 and lower annular locating tab 3-4 are made by high tensile steel material, and the heat treatment hardness value of each parts is at more than HRC50.
When the utility model uses, when the eccentric shaft 34 of bent axle 4 one end drives the hub rotation of orbiter 2, the steel ball 3-3 of described Roller Disc structure 3 does circumferentially translation in Roller Disc structure 3 inside, is provided with seal ring between the orbiter 2 outside Roller Disc structure and frame 4.
In the utility model, Roller Disc structure 3 is arranged between frame 5 and orbiter 2, and Roller Disc structure 3 comprises and is installed on upper annular locating tab 3-2 on orbiter 2 and Smooth annular egative film 3-1, is installed on lower annular locating tab 3-4 in frame 5 and smooth annular egative film 3-5 and the steel ball 3-3 between fixed base 31 and frame 5.Orbiter 2 is when circling, and orbiter 2 is close to frame 5 under the effect of compression chamber axial gas power, and Roller Disc structure 3 is as axially support bearing axially support orbiter 2.Steel ball 3-3 is positioned over the annular locating tab 3-2 on fixed base 31 and between the positioning through hole 3-41 of the lower annular locating tab 3-4 in frame 5, because specifically design makes orbiter 2 remain constant relative to the phase difference of frame 5, also just ensure that orbiter 2 is constant relative to the phase difference of fixed scroll 1.
As shown in Figure 1, Roller Disc structure 3 is installed between frame 5 and orbiter 2, Smooth egative film 3-1 and upper annular locating tab 3-2 is consolidated on orbiter 2 by set screw 3-6, and lower annular locating tab 3-4 and lower smooth egative film 3-5 is consolidated in frame 5 by set screw 3-6.Lubricant grease is injected, with lubricated balls disc structure in the cavity 50 of Roller Disc structure 3.Orbiter 2 does circumferentially translation under the driving of the eccentric part of bent axle 4, orbiter 2 wheel hub is at Roller Disc structure 3 internal motion, orbiter 2 is close to frame 5 under the effect of compression chamber gas axial pressure, and Roller Disc structure 3 axially support orbiter 2 is to keep axial position constant all the time.When orbiter 2 makes circular translational, needing to ensure itself and frame 5 phase difference, constant all the time (fixed scroll 1 relative frame 5 phase difference is constant all the time, this ensures that there orbiter 2 to become in portion all the time with fixed scroll 1 phase difference), steel ball 3-3 limits the phase difference of Smooth egative film 3-1 and lower annular locating tab 3-4 in Roller Disc structure 3, this ensures that theres orbiter 2 constant all the time with the phase difference of frame 5.
The lubrication of Roller Disc structure 3 of the present utility model is close in Roller Disc structural cavities 50 regularly to inject and change lubricant grease and ensures, Roller Disc structure 3 inside cools by fan 7, fan 7 is fixed on bent axle 4, and when revolution running done by bent axle 4, fan 7 is running just.Roller Disc structure 3 (axially support bearing and phase place holding structure) of the present utility model has simple novelty, feature with low cost.
Claims (7)
1. an oil-free vortex air compressor, comprise fixed scroll (1), orbiter (2), bent axle (4), frame (5), main equilibrium block (6), belt pulley (9), intakeport and relief opening, described orbiter (2) engages with fixed scroll (1) compression chamber forming air, bent axle (4) is arranged in frame (5) with main bearing (18) and supplementary bearing (17), it is characterized in that: between orbiter (2) and frame (5), be provided with a Roller Disc structure (3), this Roller Disc structure (3) includes the fixed base (31) being arranged on frame (5), fixed base (31) is provided with a radial bearing (32) and a thrust-bearing (33), described fixed base (31) is provided with a mounting hole (312), radial bearing (32) is fixed in mounting hole (312), be arranged on the eccentric shaft (34) of bent axle (4) one end, described thrust-bearing (33) is fixed on fixed base (31) side, is adjacent in frame (5) side, described radial bearing (32) and thrust-bearing (33) are concentric shafts, thrust-bearing (33) ring set is in radial bearing (32) outside, when orbiter (2) and fixed scroll (1) are relatively rotated, orbiter (2) drives eccentric rotary by the upper radial bearing (32) of eccentric shaft (34), and by thrust-bearing (33) position rotating, make to keep good phase difference between orbiter (2) and fixed scroll (1).
2. a kind of oil-free vortex air compressor according to claim 1, it is characterized in that: the fixed base (31) of described Roller Disc structure (3) is a ring part, the endoporus of this ring part is the mounting hole (312) of fixed base (31), ring part side is provided with the annular mounting groove (311) with mounting hole (312) concentric, described radial bearing (32) is arranged on the endoporus position of ring part, and thrust-bearing (33) is arranged in annular mounting groove (311).
3. a kind of oil-free vortex air compressor according to claim 1 or 2, it is characterized in that: described thrust-bearing (33) includes the multiple steel balls (3-3) being located at annular mounting groove (311), steel ball (3-3) is provided with annular locating tab on (3-2) and lower annular locating tab (3-4), on this, annular locating tab (3-2) and the equal annular spread of lower annular locating tab (3-4) have the positioning through hole (3-41) of fixing steel ball (3-3), described steel ball (3-3) is located at position between positioning through hole (3-41) corresponding to annular locating tab (3-2) and lower annular locating tab (3-4).
4. a kind of oil-free vortex air compressor according to claim 3, it is characterized in that: described upper annular locating tab (3-2) is screwed on fixed base (31), lower annular locating tab (3-4) is screwed in frame (5).
5. a kind of oil-free vortex air compressor according to claim 3, it is characterized in that: described upper annular locating tab (3-2) inner side is also provided with Smooth annular egative film (3-1) of hard, wear-resistant, this Smooth annular egative film (3-1) is located at annular mounting groove (311) bottom of fixed base (31), lower annular locating tab (3-4) inner side is also provided with the lower smooth annular egative film (3-5) of hard, wear-resistant, and this lower annular locating tab (3-4) is located at circular mounting hole (51) bottom that frame (5) is established.
6. a kind of oil-free vortex air compressor according to claim 1, it is characterized in that: described bent axle (4) is provided with a fan (7), this fan (7) is for being arranged on the blade on bent axle, this blade rotates with the rotation of bent axle (4), fan (7) is positioned at Roller Disc structure (3) side, acts on Roller Disc structure (3) inner quick heat radiating.
7. a kind of oil-free vortex air compressor according to claim 1, is characterized in that: described Roller Disc structure (3) is made by high tensile steel material, and heat treatment hardness value is at more than HRC50.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520682016.5U CN204941932U (en) | 2015-09-02 | 2015-09-02 | A kind of oil-free vortex air compressor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520682016.5U CN204941932U (en) | 2015-09-02 | 2015-09-02 | A kind of oil-free vortex air compressor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204941932U true CN204941932U (en) | 2016-01-06 |
Family
ID=55009370
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520682016.5U Expired - Fee Related CN204941932U (en) | 2015-09-02 | 2015-09-02 | A kind of oil-free vortex air compressor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204941932U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105041646A (en) * | 2015-09-02 | 2015-11-11 | 广州广涡压缩机有限公司 | Oil-free scroll air compressor |
-
2015
- 2015-09-02 CN CN201520682016.5U patent/CN204941932U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105041646A (en) * | 2015-09-02 | 2015-11-11 | 广州广涡压缩机有限公司 | Oil-free scroll air compressor |
| CN105041646B (en) * | 2015-09-02 | 2018-05-15 | 广州广涡压缩机有限公司 | A kind of oil-free vortex air compressor |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| WO2013093479A3 (en) | Centrifugal refrigerant vapour compressors | |
| CN101245856B (en) | Bearing sealing device | |
| CN106050726B (en) | Compressor | |
| DE60216474D1 (en) | TOUCH-FREE SEAL FOR LARGE AXLE SPRING APPLICATIONS | |
| CN105526164A (en) | Vehicle-mounted direct current direct-connected-type oil-free vortex air compressor | |
| AU2017204145A1 (en) | Pump or rotary compressor | |
| CN104500394A (en) | Oil-free lubricatoin scroll compressor | |
| CN104895807A (en) | Centrifugal compressor | |
| US7189052B2 (en) | Centrifugal compressor having rotatable compressor case insert | |
| CN201330705Y (en) | Mechanical seal structure of Roots vacuum pump | |
| CN204941932U (en) | A kind of oil-free vortex air compressor | |
| CN105041646A (en) | Oil-free scroll air compressor | |
| US9765791B2 (en) | Turbo compressor | |
| CN204386881U (en) | A kind of non-lubricated vortex compressor | |
| CN202065468U (en) | Corrugated slot sealing ring structure | |
| CN108350869A (en) | Fluid machinery | |
| JP6167319B2 (en) | Shaft seal structure of rotary pump | |
| CN203500482U (en) | External ultra-thin labyrinth seal with positioning device | |
| CN106122014B (en) | A kind of liquid rotary compressor | |
| CN205600507U (en) | Pneumatic oil film static pressure bistrique | |
| KR20190056724A (en) | Oil retrieval device | |
| CN105849411B (en) | Convolute-hydrodynamic mechanics | |
| CN209026205U (en) | A kind of oil sealing arrangement of the gas turbine with flag-shaped slot rotating ring | |
| CN104047850B (en) | Oil spout scroll air compressor | |
| CN103362801B (en) | A kind of scroll compressor |
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 |
Granted publication date: 20160106 Termination date: 20190902 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |