CN2168101Y - Vortex disk structure - Google Patents
Vortex disk structure Download PDFInfo
- Publication number
- CN2168101Y CN2168101Y CN 93219175 CN93219175U CN2168101Y CN 2168101 Y CN2168101 Y CN 2168101Y CN 93219175 CN93219175 CN 93219175 CN 93219175 U CN93219175 U CN 93219175U CN 2168101 Y CN2168101 Y CN 2168101Y
- Authority
- CN
- China
- Prior art keywords
- groove
- vortex
- scroll
- flow
- movable orbiting
- 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
Images
Landscapes
- Rotary Pumps (AREA)
Abstract
The utility model provides a new vortex disk structure in the technical field of vortex compressors. The central parts of a traditional vortex disk and a fixed vortex disk are respectively processed with grooves to quickly increase the area of a through flow passage from a compression chamber to a central air exhausting chamber at the beginning of air exhaust and reduce the flow loss resulted by too much small flow area. Simultaneously, air exhausting flow passages are partially changed to reduce the flow loss because the vortex wall of the movable vortex disk moves at the front of an air exhausting port and disturbs a flow field. Thereby, the efficiency of vortex compressors is improved.
Description
The utility model belongs to the scroll compressor technical field.
In scroll compressor, when traditional scroll structure is communicated with at its exhaust starting stage, compression chamber and center cavity, the dynamic and static scroll laws of motion that are meshing with each other have determined by compression chamber very for a short time to the circulation area of central row air cavity, and circulation area increases slowly, and element volume reduces soon.Therefore, fluid is subjected to serious throttling inhibition when flowing through this passage, and flow velocity increases and forms strong vortex in the vortex ring tip region, has caused serious flow losses.In addition, movable orbiting scroll vortex wall tip part keeps off before vent ports, and interference flowing field distributes, and has also increased loss.
The purpose of this utility model is by reducing flow losses in the scroll center region of scroll compressor machined grooves, thereby improves the efficient of scroll compressor.
The utility model is achieved in that in quiet whirlpool dish and movable orbiting scroll center region difference machined grooves, the Flow area that is communicated with from compression chamber to the central row air cavity when beginning with quick increase exhaust, the flow losses that minimizing causes because of Flow area is too small, the simultaneously local grate flow channel that changes reduces the flow losses that the interference because of the mobile stream field of movable orbiting scroll vortex wall before vent ports causes.The design fibrous root of groove is determined according to the working procedure of scroll compressor.The projection that groove location is quiet when movable orbiting scroll goes to the exhaust angle in engagement process, that moving vortex circle molded lines (the outer molded lines that comprises corresponding vortex ring) is surrounded center cavity zone on bottom surface separately rings in the zone, and groove will have certain depth.
Fig. 1 is the plan view of quiet whirlpool dish 1.
Fig. 2 is the sectional view of quiet whirlpool dish 1.
Fig. 3 is the plan view of movable orbiting scroll 2.
Fig. 4 is the sectional view of movable orbiting scroll 2.
Fig. 5 is that compression ends, be about to begin exhaust instantaneous, be movable orbiting scroll 2 when in engagement process, going to position, exhaust angle, quiet, movable orbiting scroll position schematic transverse sectional view.
Fig. 6 is the axial sectional view of Fig. 5.
Fig. 7 is dish 2 relative Fig. 5 positions in whirlpool when turning over an angle slightly again, quiet, the movable orbiting scroll position of the work that is meshed and the transverse sectional view that flows and illustrate.
Fig. 8 is the axial sectional view of Fig. 7.
Fig. 9 is the vortex wall tip part retaining of movable orbiting scroll 2 before vent ports the time, the transverse sectional view of the relative position of quiet whirlpool dish 1 and movable orbiting scroll 2 and the signal of flowing.
Figure 10 is the axial sectional view of Fig. 9.
Figure 11 simplifies the groove schematic representation.
By machined grooves, making flows improves.At movable orbiting scroll when position, exhaust angle turns over an angle more slightly, from accompanying drawing 7, accompanying drawing 8 as can be seen, after improving structure, connected surface increases rapidly, and flowing has also increased the passage shown in the arrow in the accompanying drawing 8 crawlway shown in the arrow in accompanying drawing 7, when the vortex wall tip part of movable orbiting scroll 2 keeps off in vent ports, from accompanying drawing 9, accompanying drawing 10 as can be seen, increased and passed through flowing of groove, can extenuate of the influence of moving spirotheca end flowing.
Groove on quiet, the movable orbiting scroll also can be processed as other shape, and the groove of quiet movable orbiting scroll can be different, but they all must as preceding definite zone in.
In scroll compressor, adopt the utility model can reduce discharge flow resistance, thereby improve compressor efficiency.Simultaneously, can extenuate, further reduce the moment of torsion in the past exhaust process, strengthen the stationarity of compressor operation, thereby reduce the electromagnetic noise of motor and the air pocket noise that air-flow causes because of flow resistance causes excessive overcompression.
Claims (4)
1, a kind of structure of scroll is characterized in that: in the center region machined grooves (3) of quiet whirlpool dish (1), in the center region machined grooves (4) of movable orbiting scroll (2).
2, scroll as claimed in claim 1 is characterized in that: when position movable orbiting scroll in engagement process of groove (3) and groove (4) went to the exhaust angle, the center cavity zone quiet, that the moving vortex circle molded lines is surrounded was in the view field on the bottom surface separately.
3, scroll as claimed in claim 1 is characterized in that: groove (3) and groove (4) can be designed to involute shape, also can be designed to cylindrical or other shape, and the groove (4) of groove (3) can be designed in same shape.
4, scroll as claimed in claim 1 is characterized in that: the degree of depth of groove (3) and groove (4) is 1 millimeter to 3 millimeters.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 93219175 CN2168101Y (en) | 1993-07-16 | 1993-07-16 | Vortex disk structure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 93219175 CN2168101Y (en) | 1993-07-16 | 1993-07-16 | Vortex disk structure |
Publications (1)
Publication Number | Publication Date |
---|---|
CN2168101Y true CN2168101Y (en) | 1994-06-08 |
Family
ID=33798629
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 93219175 Expired - Fee Related CN2168101Y (en) | 1993-07-16 | 1993-07-16 | Vortex disk structure |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN2168101Y (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN100378334C (en) * | 2003-11-10 | 2008-04-02 | 日立家用电器公司 | Scroll compressor |
-
1993
- 1993-07-16 CN CN 93219175 patent/CN2168101Y/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN100378334C (en) * | 2003-11-10 | 2008-04-02 | 日立家用电器公司 | Scroll compressor |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN2168101Y (en) | Vortex disk structure | |
CN110566285B (en) | Compact centripetal turbine guider | |
JPS58135396A (en) | Movable-blade compressor | |
EP1534957B1 (en) | Screw compressor discharge flow guide | |
CN2054100U (en) | Involute impeller for rotary fluid machines | |
CN214273971U (en) | Centrifugal compressor and volute thereof | |
CN207064317U (en) | Slow-speed of revolution centrifugal pump | |
CN208886871U (en) | A kind of range hood with collector | |
CN211422999U (en) | Mixed flow type impeller | |
CN1952407A (en) | Centrifugal pump having extrusion chamber with subchannel | |
CN2811610Y (en) | Vortex compressor with reverse rotation preventing device for air conditioner | |
CN2874070Y (en) | Double blade compressor with direct flow air suction valve | |
CN115773276A (en) | High-speed impeller and hydrogen circulating pump | |
CN113094833A (en) | Method for designing diffuser with dovetail leading edge and integrated radial and axial blades | |
CN112628205A (en) | Centrifugal fan collector of double-arc molded line | |
CN100354523C (en) | Vortex rotary compressor | |
CN2457370Y (en) | Multiple stage centrifugal pump | |
CN217029398U (en) | Centrifugal impeller and centrifugal compressor with same | |
JPH0610892A (en) | Axial flow blower and air conditioner using this blower | |
CN214196763U (en) | Fan wheel subassembly, fan subassembly and fan | |
CN213205971U (en) | Rotary vane compressor | |
JPH0972222A (en) | Axial-flow compressor | |
CN209743263U (en) | Fluid jet vacuum generator | |
CN208431164U (en) | A kind of helical-lobe compressor from off-load sliding valve structure | |
CN1644930A (en) | Anti-surge ring of axial fan |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C19 | Lapse of patent right due to non-payment of the annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |