CN202709820U - Static combined cooling pipe structure - Google Patents
Static combined cooling pipe structure Download PDFInfo
- Publication number
- CN202709820U CN202709820U CN 201220280251 CN201220280251U CN202709820U CN 202709820 U CN202709820 U CN 202709820U CN 201220280251 CN201220280251 CN 201220280251 CN 201220280251 U CN201220280251 U CN 201220280251U CN 202709820 U CN202709820 U CN 202709820U
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- bobbin
- cooling
- pipe structure
- mixing pipe
- static mixing
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Abstract
The utility model discloses a static combined cooling pipe structure, which comprises a tubular pipe, an outer cavity sealing plate and a turbolator, wherein the tubular pipe comprises an inner tubular pipe, an outer tubular pipe and ribs for connecting the inner tubular pipe and the outer tubular pipe; two ends of the inner tubular pipe are a hot fluid inlet end and a hot fluid outlet end; two ends of the outer tubular pipe are provided with a cooling carrier inlet and a cooling carrier outlet; the outer cavity sealing plate is arranged at the outlet end, used for sealing an outer cavity and provided with a hot fluid outlet which is communicated with an inner cavity; the turbolator comprises a cover body, a connecting plate and a turbulence plate group arranged in the inner cavity, wherein the cover body is used for sealing the outer cavity and is provided with a hot fluid inlet communicated with the inner cavity, and the turbulence plate group is movably connected to the cover body through the connecting plate. The static combined cooling pipe structure disclosed by the utility model ensures that the hot fluid can be rapidly and uniformly cooled and the heat exchange effect is good.
Description
Technical field
The utility model relates to a kind of rapid homogeneous cooling apparatus of fluid, refers in particular to a kind of static mixing pipe structure for cooling.
Background technology
In modern industry is produced, a lot of arts demands relate to fluid and cool off fast, in existing cooling technology, be mostly to adopt air-cooled or fluid cooling (such as water-cooled), because this dual mode also is most economical applicable, the structure of the most frequently used cooling system is just like interior exocoel device, exocoel passes into fresh coolant carrier, and inner chamber is by needing the hot fluid of cooling, and the defective of this mode is that cooling is insufficient, efficient is low, and the cooling velocity of medium inside is inconsistent.The hot fluid at position may not contact with the cooling chamber wall in by the process of cooling system in the inner chamber, and this part hot fluid just is not cooled like this, and heat energy passes to again chilled hot fluid, thereby causes cooling effect to reduce.The viscosity temperature influence of part decentralized medium is larger, so just may cause fouling at cavity inner wall, has further weakened its radiating effect.
The utility model content
The purpose of this utility model is to provide a kind of cooling even, the static mixing pipe structure for cooling that heat exchange effect is good.
For achieving the above object, the utility model is by the following technical solutions:
A kind of static mixing pipe structure for cooling, comprise bobbin, exocoel diaphragm seal and turbulator, described bobbin is the double-layer circular structure, and it comprises inner bobbin, outer bobbin and rib, described inner bobbin is set in the described outer bobbin, and inside and outside bobbin links to each other by described rib; The tube wall of described outer bobbin is provided with import and the outlet of coolant carrier; Described exocoel diaphragm seal places an end of described bobbin; Described turbulator sealing is arranged at the other end of described bobbin, and part is arranged in described inner bobbin cavity.
Above-mentioned inner bobbin, outer bobbin and rib are one-body molded.
The outer surface of above-mentioned inner bobbin is provided with perpendicular muscle.
Above-mentioned turbulator comprises lid, brace and places the turbulent sheet group of inner bobbin cavity, and described turbulent sheet group is movably connected on the described lid by described brace, and described lid links to each other with described bobbin sealing.
Above-mentioned turbulent sheet group is comprised of one group of interconnective turbulent sheet, and described lid seals the cavity between described inner bobbin and outer bobbin.
The import and export of above-mentioned coolant carrier is positioned at the two ends of outer bobbin.
Above-mentioned rib is no more than described coolant carrier import and export along the axial distance of barrel along the axial length of barrel.
Above-mentioned rib is the 3-12 root, circumferentially evenly distributes along described bobbin.
Above-mentioned turbulent sheet is spiral sheet or arc sheet.
After adopting technique scheme, the utility model is compared with existing background technology, has following advantage:
1. inner bobbin, outer bobbin connect by rib, and intensity is reliable, and simultaneously rib adopts the good conductor of heat, has increased area of dissipation, have namely increased the contact area with coolant carrier, more are conducive to the quick cooling of hot fluid.
2. turbulent sheet constantly rotation in inner bobbin under the percussion of hot fluid makes the hot fluid each several part can both touch the inner core tube wall, thereby reaches the purpose of Quick uniform cooling, so that cooling effectiveness promotes greatly, can be used in the automated production.
3. turbulent sheet is spiral sheet or arc sheet, makes the interior fluid of inner bobbin along with the rotating screw of turbulent sheet advances, and makes fluid more contact the inner tube wall end, and heat is passed, and promotes cooling effectiveness.
Description of drawings
Fig. 1 is schematic appearance of the present utility model;
Fig. 2 is decomposing schematic representation of the present utility model;
Fig. 3 is generalized section of the present utility model;
Fig. 4 is the A-A section enlarged diagram of Fig. 3;
Fig. 5 is the structural representation of the utility model turbulator;
Fig. 6 is sectional block diagram of the present utility model;
Fig. 7 is the structural representation of another embodiment of bobbin.
The primary clustering symbol description:
100: bobbin, 110: inner bobbin, 120: outer bobbin, 121: import, 122: outlet, 130: rib, 200: exocoel diaphragm seal, 210: hot fluid outlet, 300: turbulator, 310: lid, 311: hot fluid entrance, 320: brace, 330: turbulent sheet, 400: exocoel, 500: inner chamber.
The specific embodiment
In order to make the purpose of this utility model, technical scheme and advantage clearer, below in conjunction with drawings and Examples, the utility model is further elaborated.Should be appreciated that specific embodiment described herein only in order to explaining the utility model, and be not used in restriction the utility model.
See also Fig. 1, shown in Figure 2, this is novel to disclose a kind of static mixing pipe structure for cooling, comprises bobbin 100, exocoel diaphragm seal 200 and turbulator 300, wherein:
Cooperate shown in Fig. 3,4,6, bobbin 100 be the double-layer circular structure, comprises inner bobbin 110, outer bobbin 120 and connects the rib 130 of inside and outside bobbin 120, and rib 130 be the 3-12 root, and the present embodiment is 4, along circumferentially even distributions of bobbin 100.
Shown in Fig. 3,4, inner bobbin 110 two ends are respectively arrival end and the port of export of hot fluid, cavity between the inside and outside bobbin is exocoel 400, the cavity of inner bobbin 110 is inner chamber 500, outer bobbin 120 two ends are provided with coolant carrier import 121 and export 122, be used for the turnover of coolant carrier, in the present embodiment, coolant carrier import 121 and export that the length along the barrel direction is 200mm～3000mm between 122.Rib 130 is no more than the coolant carrier import and export along the axial distance of barrel along the axial length of barrel, so that the coolant carrier that import 121 is injected can fully enter exocoel 400, and can flow out through exporting 122.The material of inner cylinder 110 is the good conductor of heat, is conducive to the rapid transmission of heat.
As shown in Figure 5, turbulator 300 comprises lid 310, brace 320 and places the turbulent sheet group of inner chamber 500.Turbulent flow sheet group is comprised of interconnective turbulent sheet 330, lid 310 cross sections are " worker " font, lid 310 is provided with the hot fluid entrance 311 that is communicated with inner chamber 500, turbulent flow sheet group is movably connected on the lid 310 by brace 320, turbulent flow sheet 330 is spiral sheet or arc sheet, turbulator 300 is installed in the port of export, lid 310 sealing exocoels 400, and turbulent sheet 330 places inner bobbin 110.
Connection sealed air-tight between interior exocoel bobbin 110,120, exocoel diaphragm seal 200 and the turbulator 300 can be realized by modes such as welding, meltings.
In the process of using, hot fluid enters inner bobbin 110 from the hot fluid entrance 311 on the lid 310, coolant carrier injects from the import 121 of outer bobbin 120 simultaneously, the injection of hot fluid is overturn the spiral sheet of inner bobbin 110 or the turbulent sheet 330 of arc sheet at inner chamber 500 under the percussion of hot fluid, hot fluid rotates under the effect of turbulent sheet 330 and advances, make hot fluid more contact inner bobbin 110 wall ends, heat is passed out to the coolant carrier in the exocoel 400.Coolant carrier enters the exocoel 400 from import 121 and flows, and guarantees the continuous supply of coolant carrier.Turbulent flow sheet 330 drives the hot fluid each several part and can both touch on the tube wall of inner bobbin 110, thereby reaches the purpose of Quick uniform cooling, so that cooling effectiveness promotes greatly, can be used in the automated production.
Hot fluid finally flows out from the outlet 122 of outer bobbin 120, and most of heat of the hot fluid during outflow has passed to coolant carrier in the process that inner bobbin 110 flows, play the effect of cooling down.
With reference to shown in Figure 7, on the outer surface of inner bobbin 110, namely on the inwall of exocoel 400, be provided with perpendicular muscle 111, the increase of perpendicular muscle 111, purpose is the area of dissipation that increases inwall, strengthens its radiating effect.
The above; it only is the better specific embodiment of the utility model; but protection domain of the present utility model is not limited to this; anyly be familiar with those skilled in the art in the technical scope that the utility model discloses; the variation that can expect easily or replacement all should be encompassed within the protection domain of the present utility model.Therefore, protection domain of the present utility model should be as the criterion with the protection domain of claim.
Claims (9)
1. static mixing pipe structure for cooling, comprise bobbin, exocoel diaphragm seal and turbulator, it is characterized in that: described bobbin is the double-layer circular structure, it comprises inner bobbin, outer bobbin and rib, described inner bobbin is set in the described outer bobbin, and inside and outside bobbin links to each other by described rib; The tube wall of described outer bobbin is provided with import and the outlet of coolant carrier; Described exocoel diaphragm seal places an end of described bobbin; Described turbulator sealing is arranged at the other end of described bobbin, and part is arranged in described inner bobbin cavity.
2. a kind of static mixing pipe structure for cooling as claimed in claim 1, it is characterized in that: described inner bobbin, outer bobbin and rib are one-body molded.
3. a kind of static mixing pipe structure for cooling as claimed in claim 1 or 2, it is characterized in that: the outer surface of described inner bobbin is provided with perpendicular muscle.
4. a kind of static mixing pipe structure for cooling as claimed in claim 3, it is characterized in that: described turbulator comprises lid, brace and places the turbulent sheet group of inner bobbin cavity, described turbulent sheet group is movably connected on the described lid by described brace, and described lid links to each other with described bobbin sealing.
5. a kind of static mixing pipe structure for cooling as claimed in claim 1 or 2, it is characterized in that: described turbulent sheet group is comprised of one group of interconnective turbulent sheet, and described lid seals the cavity between described inner bobbin and outer bobbin.
6. a kind of static mixing pipe structure for cooling as claimed in claim 3, it is characterized in that: the import and export of described coolant carrier is positioned at the two ends of outer bobbin.
7. a kind of static mixing pipe structure for cooling as claimed in claim 6, it is characterized in that: described rib is no more than described coolant carrier import and export along the axial distance of barrel along the axial length of barrel.
8. a kind of static mixing pipe structure for cooling as claimed in claim 2, it is characterized in that: described rib is the 3-12 root, circumferentially evenly distributes along described bobbin.
9. a kind of static mixing pipe structure for cooling as claimed in claim 4, it is characterized in that: described turbulent sheet is spiral sheet or arc sheet.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220280251 CN202709820U (en) | 2012-06-14 | 2012-06-14 | Static combined cooling pipe structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220280251 CN202709820U (en) | 2012-06-14 | 2012-06-14 | Static combined cooling pipe structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202709820U true CN202709820U (en) | 2013-01-30 |
Family
ID=47590111
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220280251 Expired - Lifetime CN202709820U (en) | 2012-06-14 | 2012-06-14 | Static combined cooling pipe structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202709820U (en) |
-
2012
- 2012-06-14 CN CN 201220280251 patent/CN202709820U/en not_active Expired - Lifetime
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C53 | Correction of patent of invention or patent application | ||
| CB03 | Change of inventor or designer information |
Inventor after: Liu Xiaobao Inventor after: Yan Yongjun Inventor before: Zhu Liren Inventor before: Yan Yongjun |
|
| COR | Change of bibliographic data |
Free format text: CORRECT: INVENTOR; FROM: ZHU LIREN YAN YONGJUN TO: LIU XIAOBAO YAN YONGJUN |
|
| CX01 | Expiry of patent term |
Granted publication date: 20130130 |
|
| CX01 | Expiry of patent term |