CN1471159A - Microjet array cooling heat sink - Google Patents
Microjet array cooling heat sink Download PDFInfo
- Publication number
- CN1471159A CN1471159A CNA031466486A CN03146648A CN1471159A CN 1471159 A CN1471159 A CN 1471159A CN A031466486 A CNA031466486 A CN A031466486A CN 03146648 A CN03146648 A CN 03146648A CN 1471159 A CN1471159 A CN 1471159A
- Authority
- CN
- China
- Prior art keywords
- jet
- inlet
- sheet
- fluid
- heat sink
- 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.)
- Granted
Links
- 238000001816 cooling Methods 0.000 title claims description 36
- 239000012530 fluid Substances 0.000 claims abstract description 43
- 239000007788 liquid Substances 0.000 claims description 19
- 230000004907 flux Effects 0.000 abstract description 6
- 239000000706 filtrate Substances 0.000 abstract 2
- 239000004065 semiconductor Substances 0.000 description 12
- 238000010586 diagram Methods 0.000 description 6
- 238000005516 engineering process Methods 0.000 description 5
- 238000007789 sealing Methods 0.000 description 4
- 230000004888 barrier function Effects 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 238000004020 luminiscence type Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000004377 microelectronic Methods 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 238000003491 array Methods 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000001311 chemical methods and process Methods 0.000 description 1
- 239000002826 coolant Substances 0.000 description 1
- 239000012809 cooling fluid Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 238000007323 disproportionation reaction Methods 0.000 description 1
- 230000005684 electric field Effects 0.000 description 1
- 238000005538 encapsulation Methods 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 230000003116 impacting effect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 229910052709 silver Inorganic materials 0.000 description 1
- 239000004332 silver Substances 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Landscapes
- Cooling Or The Like Of Semiconductors Or Solid State Devices (AREA)
- Cooling Or The Like Of Electrical Apparatus (AREA)
Abstract
The invention comprises the flow pass slice, jet inlet cavity slice, ejector nozzle slice, jet outlet slice and heat transfer slice. There are fluid inlet and fluid outlet in the flow pass slice, and there are jet inlet cavity, fluid inlet and outlet orifice in jet inlet cavity slice. The ejector nozzle slice comprises the ejector nozzle, the feed fluid diversion channel and the filtrate diversion channel. The ejector nozzle is connected to the jet inlet cavity and jet outlet cavity on the jet outlet slice. The feed fluid diversion channel is connected to the fluid inlet orifice and the jet inlet cavity. The filtrate diversion channel is connected to the fluid outlet orifice and the jet outlet cavity. The invention realizes heat transfer with high heat flux, possessing very high heat transfer rate so as to lower temperature on heat exchange surface of electron device effectively as well as raise evenness of temperature distribution.
Description
Technical field
The invention belongs to microelectronics technology, relate to a kind of cooling device.
Background technology:
Along with the continuous development of industrial technology, various electronic products direction little, in light weight towards volume invariably, high heat flux develops.Therefore, for the electronic equipment of a new generation, the design limit of traditional cooler and manufacturing technology can't meet the requirements.The development of micro-cooler comes from the heat dissipation problem that solves high speed integrated circuit, at present to the various high heat flux field development that weight limits and volume restrictions are arranged, as aerospace industry, electronic devices and components cooling, high power semiconductor lasers cooling, chemical-process heat transfer etc.Its main purpose is in order to reduce electronic equipment because of the overheated probability that breaks down and damage, and improves the performance and the reliability of electronic equipment simultaneously.
The micro-cooler of actively setting about studying and using both at home and abroad comprises at present: micro-heat exchanger, little refrigerator, micro-channel heat sink, the equal backing of micro heat pipe and integrated micro-cooler etc.Wherein micro-channel heat sink has been proved to be one of type of cooling of the best and tool application potential of heat transfer property.
At present universally recognized two kinds of representational microchannel cooling heat sinks are: traditional microchannel type (Traditional Microchannel Type, TMC) and menifold microchannel type (ManifoldMicrochannel Type, MMC).The characteristics that TMC is heat sink are two ends that entrance and exit lays respectively at the components and parts that are cooled.Though TMC is heat sink to have a high cooling capacity, the limitation in two designs has limited its extensive use.One is because the big pressure that small size produced falls; Its two, be huge variations in temperature between thermal source inlet, outlet.Have many inlets, an exit passageway and MMC is heat sink, be alternately distributed on channel-length direction at certain intervals.Under a fixing flow rate, according to the inlet/outlet quantity of menifold passage, flow resistance is reduced by corresponding, and range of temperature is reduced by corresponding, and total heat transfer resistance is also correspondingly reduced.Therefore, compare with TMC is heat sink, the heat sink tool of MMC has an enormous advantage.Yet, no matter be that TMC is heat sink or MMC is heat sink, its coolant mechanism is the inner fluid passage forced convection heat transfer.Low, the good cooling results of feeder connection place fluid temperature (F.T.) consequently, and exit fluid temperature (F.T.) height, cooling effect are relatively poor relatively, cause the heat exchange surface temperature distributing disproportionation thus.And the Temperature Distribution of this regional area (particularly maximum temperature) is the key that influences the device operating characteristic that is cooled, and also is the important indicator of estimating micro-channel heat sink performance quality.
Summary of the invention:
The object of the present invention is to provide a kind of cooling heat sink, overcome the shortcoming of above-mentioned two kinds of microchannel cooling heat sinks.
A kind of microjet array cooling heat sink is characterized in that, as shown in Figure 1, includes the flow 1 excessively that is packaged together successively, jet inlet chamber sheet 2, jet nozzle sheet 3, jet exit plate 4, heat transfer sheet 5; Cross and have inlet 6 and the liquid outlet 7 that is connected with exterior line in the flow 1; Jet inlet chamber sheet 2 is provided with jet inlet chamber 8, is having inlet opening 9 and fluid hole 10 with inlet 6 and the liquid outlet 7 corresponding positions crossed in the flow 1; Jet nozzle sheet 3 is provided with jet inlet chamber 8 and is arranged on the jet nozzle 11 that the jet exit chamber 14 on the jet exit chamber sheet 4 communicates, the feed liquor flow-guiding channel 12 that is communicated with inlet opening 9 and jet inlet chamber 8, the fluid flow-guiding channel 13 in connection fluid hole 10 and jet exit chamber 14; Be provided with jet exit chamber 14 in 8 corresponding positions, jet inlet chamber on the jet exit chamber sheet 4 with jet inlet chamber sheet 2.
As shown in Figure 8, have inlet opening 9 and fluid hole 10 with inlet 6 and the liquid outlet 7 corresponding positions crossed in the flow 1 on the jet exit of the present invention chamber sheet 4, having inlet 6 and liquid outlet 7 with inlet 6 and the liquid outlet 7 corresponding positions crossed in the flow 1 on the heat transfer sheet 5.
The present invention has adopted the jet nozzle of being made up of the hole array 11.
As shown in Figure 4, the present invention has adopted the jet exit chamber 14 that has microchannel 17 on jet exit chamber sheet 4, and the quantity of microchannel 17 and position are corresponding with the hole in the jet nozzle 11.
The microjet array cooling heat sink that the present invention proposes is based on the jet impulse heat transfer theory.During the jet impulse cooling, flow process forms very thin speed and temperature boundary layer, thereby has the very high coefficient of overall heat transmission to impacting heating surface.Simultaneously, adopt rational microjet arranged in arrays mode, can greatly improve the uniformity of the surface temperature distribution that is cooled.Therefore, microjet array cooling heat sink is the effective ways that reduce electronic device heat exchange surface maximum temperature, reduce variations in temperature.
As shown in Figure 2, microjet array cooling heat sink 15 will be formed after the heat sink assembled package.Can form the circulation of fluid of sealing in heat sink inside, fluid is flowed through and is in proper order: inlet 6, inlet opening 9, feed liquor flow-guiding channel 12, jet inlet chamber 8, jet nozzle 11, jet exit chamber 14, fluid flow-guiding channel 13, fluid hole 10, liquid outlet 7, fluid with higher speed, vertically be injected on the heat transfer sheet 5, has realized that high heat flux conducts heat by jet nozzle 11.
Heat-exchange working medium can be selected air, water, cold-producing medium etc. respectively for use.According to used working medium and device optimum working temperature scope, on heating surface, will form the heat exchange of monophasic fluid jet impulse, the jet impulse phase-change heat-exchange is realized the cooling technology requirement.
Can select materials such as oxygen-free copper, silicon chip, silver for use for heat sink, the global geometric shape size can require to determine according to be cooled device size and overall encapsulation.
The jet impulse cooling is a kind of strong heat convection mode, and particularly under the micro-scale condition, the jet impulse heat exchange has high heat exchange rate.The present invention has made full use of high these characteristics of microjet impingement heat transfer coefficient, utilize the heat sink microelectronic component that cools off of microjet array, simultaneously can realize the jet impulse phase-change heat-exchange in some cases, the latent heat when utilizing fluid to undergo phase transition is realized higher density of heat flow rate.
Description of drawings:
Fig. 1: the structural representation with array of circular apertures jet nozzle of the present invention;
Among the figure: 1, cross flow, 2, jet inlet chamber sheet, 3, the jet nozzle sheet, 4, jet exit chamber sheet, 5, heat transfer sheet, 6, inlet, 7, liquid outlet, 8, jet inlet chamber, 9, inlet opening, 10, fluid hole, 11, jet nozzle, 12, feed liquor flow-guiding channel, 13, the fluid flow-guiding channel, 14, the jet exit chamber;
Fig. 2: schematic diagram of the present invention with structure shown in Figure 1;
Among the figure: 15, cooling heat sink;
Fig. 3: the present invention cools off the schematic diagram of semiconductor laser bar;
Among the figure: 16, semiconductor laser bar;
Fig. 4: the structural representation with array of circular apertures jet nozzle and microchannel of the present invention;
Among the figure: 17, microchannel;
Fig. 5: of the present invention have an oblong aperture array jetting structure of nozzle schematic diagram;
Fig. 6: schematic diagram of the present invention with structure shown in Figure 5;
Fig. 7: the present invention cools off the schematic diagram of large power semiconductor laser array;
Among the figure: 18, positive source, 19, insulating barrier, 20, light, 21, inlet tube, 22, outlet, 23, sealing ring;
Fig. 8: have the cooling heat sink structural representation that has liquid inlet and outlet on liquid inlet and outlet hole and the heat transfer sheet on the sheet of jet exit chamber.
Embodiment
Embodiment 1:
As shown in Figure 3, with the heat sink cooling semiconductor laser bar 16 of microjet array, a kind of length of typical semiconductor laser strip 16, width, thickness are of a size of 10000 * 1000 * 115 microns
3Several evenly distributed generating lasers are wherein arranged, the microjet array is heat sink 15 crosses flow 1 by shown in Figure 1, jet inlet chamber sheet 2, jet nozzle sheet 3, jet exit chamber sheet 4, heat transfer sheet 5 is welded successively, every is rectangle, width is identical with the length of semiconductor laser bar 16, semiconductor laser bar 16 is fixed on the heat transfer sheet 5, jet nozzle 11 is that 70 microns circular hole is formed by row's diameter, the degree of depth of circular hole is the thickness of jet nozzle sheet 3, it is 300 microns, the quantity of circular hole is corresponding with the quantity and the position of generating laser in the laser strip with the position, the thickness of jet exit chamber sheet 4 is 200 microns, crosses flow 1, jet inlet chamber sheet 2, heat transfer sheet 5 thickness are 300 microns.Can form the circulation of fluid of sealing in the heat sink inside of microjet array, fluid is flowed through and is in proper order: inlet 6, inlet opening 9, feed liquor flow-guiding channel 12, jet inlet chamber 8, jet nozzle 11, jet exit chamber 14, fluid flow-guiding channel 13, fluid hole 10, liquid outlet 7.With higher speed, vertically be injected on the heat transfer sheet 5, take away by the heat that generating laser is produced and passes on the heat transfer sheet 5 by jet nozzle 11 for fluid, realized that high heat flux conducts heat.
Embodiment 2:
As shown in Figure 4, jet exit chamber 14 on jet exit chamber sheet 4 has microchannel 17, the quantity of microchannel 17 and position are corresponding with the circular hole in the jet nozzle 11, the width of microchannel 17 is the 300-500 micron, after each sheet machines, weld together successively, form the microjet cooling heat sink, fluid is flowed through in heat sink inside and is in proper order: inlet 6, inlet opening 9, feed liquor flow-guiding channel 12, jet inlet chamber 8, jet nozzle 11, microchannel 17, jet exit chamber 14, fluid flow-guiding channel 13, fluid hole 10, liquid outlet 7; After fluid enters into jet inlet chamber 8, at first by jet nozzle 11 with higher speed, vertically be injected on the heat transfer sheet 5, realized that high heat flux conducts heat, fluid 17 flow to jet exit chamber 14 through the microchannel then, realized and the heat-transfer area heat exchange, made full use of the type of cooling of forced convection heat transfer combination in jet impulse heat exchange and the passage.
Embodiment 3:
As shown in Figure 5, adopting two thickness is 200 microns jet nozzle sheet 3, jet nozzle 11 is that 40 microns, length are that 500 microns oblong aperture is formed by the evenly distributed width of a row, the thickness of jet exit chamber sheet 4 is 200 microns, the thickness of crossing flow 1, jet inlet chamber sheet 2, heat transfer sheet 5 is 300 microns, is illustrated in figure 6 as the heat sink schematic diagram with Fig. 5 structure.Fluid is flowed through in heat sink inside and is in proper order: inlet 6, inlet opening 9, feed liquor flow-guiding channel 12, jet inlet chamber 8, jet nozzle 11, jet exit chamber 14, fluid flow-guiding channel 13, fluid hole 10, liquid outlet 7.The oblong aperture of fluid by jet nozzle 11 is vertical in the plane jet mode, high velocity jet on heat transfer sheet 5, realized having the cooling of long and narrow heating region device for some.
Embodiment 4:
As shown in Figure 7, adopt the present invention to cool off large power semiconductor laser array, this array is made up of M luminescence unit, and M=4 scribbles insulating barrier 19 between each luminescence unit in the present embodiment; Each luminescence unit comprises: positive source 18, cooling heat sink 15 and place semiconductor laser bar 16 and insulating barrier 19 between them, and cooling heat sink 15 is simultaneously as power cathode, and semiconductor laser bar 16 emits beam 20 under effect of electric field.Fluid enters each cooling heat sink 15 respectively through inlet tube 21, flows out through outlet 22; Rubber seal 23 sealings are arranged between inlet tube 21, outlet 22 and the cooling heat sink 15.
In the present embodiment, the cooling heat sink 15 of the top is identical with structure shown in Figure 1, it is no liquid inlet and outlet hole on jet exit chamber sheet 4, the heat transfer sheet 5, be processed with liquid inlet and outlet hole and liquid inlet and outlet respectively on the jet exit chamber sheet 4 of the cooling heat sink 15 of below, the heat transfer sheet 5, as shown in Figure 8, like this, cooling fluid can enter that each is heat sink through same root entry pipe respectively, and, realized cooling to large power semiconductor laser array through same outlet outflow.
Claims (4)
1, a kind of microjet array cooling heat sink is characterized in that, includes the flow (1) excessively that is packaged together successively, jet inlet chamber sheet (2), jet nozzle sheet (3), jet exit plate (4), heat transfer sheet (5); Cross and have inlet (6) and the liquid outlet (7) that is connected with exterior line in the flow (1); Jet inlet chamber sheet (2) is provided with jet inlet chamber (8), is having inlet opening (9) and fluid hole (10) with inlet (6) and the corresponding position of liquid outlet (7) crossed in the flow (1); Jet nozzle sheet (3) is provided with jet inlet chamber (8) and is arranged on the jet nozzle (11) that the jet exit chamber (14) on the jet exit chamber sheet (4) communicates, the feed liquor flow-guiding channel (12) that is communicated with inlet opening (9) and jet inlet chamber (8), the fluid flow-guiding channel (13) of connection fluid hole (10) and jet exit chamber (14); Jet exit chamber sheet (4) is gone up and is provided with jet exit chamber (14) in the corresponding position, jet inlet chamber (8) with jet inlet chamber sheet (2).
2, a kind of microjet array cooling heat sink according to claim 1, it is characterized in that described jet exit chamber sheet (4) is having inlet opening (9) and fluid hole (10) with inlet (6) and the corresponding position of liquid outlet (7) crossed in the flow (1); Described heat transfer sheet (5) is having inlet opening (6) and fluid hole (7) with inlet (6) and the corresponding position of liquid outlet (7) crossed in the flow (1).
3, a kind of microjet array cooling heat sink according to claim 1 and 2 is characterized in that, has adopted the jet nozzle of being made up of the hole array (11).
4, a kind of microjet array cooling heat sink according to claim 3, it is characterized in that, adopted the jet exit chamber (14) that has microchannel (17) on jet exit chamber sheet (4), the quantity of microchannel (17) and position are corresponding with the hole in the jet nozzle (11).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 03146648 CN1233038C (en) | 2003-07-11 | 2003-07-11 | Microjet array cooling heat sink |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 03146648 CN1233038C (en) | 2003-07-11 | 2003-07-11 | Microjet array cooling heat sink |
Publications (2)
Publication Number | Publication Date |
---|---|
CN1471159A true CN1471159A (en) | 2004-01-28 |
CN1233038C CN1233038C (en) | 2005-12-21 |
Family
ID=34156095
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 03146648 Expired - Fee Related CN1233038C (en) | 2003-07-11 | 2003-07-11 | Microjet array cooling heat sink |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN1233038C (en) |
Cited By (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN100461995C (en) * | 2006-11-24 | 2009-02-11 | 北京工业大学 | Array jetting micro heat exchanger |
CN101883483B (en) * | 2009-05-06 | 2012-03-21 | 中国科学院半导体研究所 | Three-plate mini-type heat radiator |
CN102456645A (en) * | 2010-10-26 | 2012-05-16 | 通用电气公司 | Thermal management system and method |
CN104112725A (en) * | 2014-08-04 | 2014-10-22 | 华进半导体封装先导技术研发中心有限公司 | Heat radiation structure used for BGA (Ball Grid Array) package of high-power chip |
US8912643B2 (en) | 2012-12-10 | 2014-12-16 | General Electric Company | Electronic device cooling with microjet impingement and method of assembly |
CN105451523A (en) * | 2015-12-28 | 2016-03-30 | 联想(北京)有限公司 | Heat radiator and electronic device |
CN104112725B (en) * | 2014-08-04 | 2017-01-04 | 华进半导体封装先导技术研发中心有限公司 | Radiator structure for high-power chip BGA package |
CN106440894A (en) * | 2016-10-07 | 2017-02-22 | 南京艾科美热能科技有限公司 | Heat equalizing plate with cavity internally having continuous jetting cooling function and method of heat equalizing plate |
US9615482B2 (en) | 2009-12-11 | 2017-04-04 | General Electric Company | Shaped heat sinks to optimize flow |
CN108712852A (en) * | 2018-07-12 | 2018-10-26 | 厦门大学 | A kind of microchannel heat sink of gas-liquid two-phase mixing jetting |
CN109195406A (en) * | 2018-08-28 | 2019-01-11 | 中国科学院理化技术研究所 | Heat sink device |
CN109216291A (en) * | 2017-06-29 | 2019-01-15 | 比亚迪股份有限公司 | Radiator for power module and the vehicle with it |
US10274263B2 (en) | 2009-04-09 | 2019-04-30 | General Electric Company | Method and apparatus for improved cooling of a heat sink using a synthetic jet |
CN111148409A (en) * | 2020-01-09 | 2020-05-12 | 西安交通大学 | Jet flow micro-channel cold plate |
CN111386011A (en) * | 2020-01-09 | 2020-07-07 | 西安交通大学 | Side flow impact micro-channel cold plate and electronic equipment |
CN112352291A (en) * | 2018-05-29 | 2021-02-09 | 牛津大学创新有限公司 | Jet impingement cooling apparatus and method |
CN114279597A (en) * | 2021-12-28 | 2022-04-05 | 中国科学院长春光学精密机械与物理研究所 | High-precision low-power radiant heat flow meter capable of being used for radiant heat flow tracing calibration |
-
2003
- 2003-07-11 CN CN 03146648 patent/CN1233038C/en not_active Expired - Fee Related
Cited By (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN100461995C (en) * | 2006-11-24 | 2009-02-11 | 北京工业大学 | Array jetting micro heat exchanger |
US10274264B2 (en) | 2009-04-09 | 2019-04-30 | General Electric Company | Method and apparatus for improved cooling of a heat sink using a synthetic jet |
US10274263B2 (en) | 2009-04-09 | 2019-04-30 | General Electric Company | Method and apparatus for improved cooling of a heat sink using a synthetic jet |
US9854704B2 (en) | 2009-04-09 | 2017-12-26 | General Electric Company | Shaped heat sinks to optimize flow |
CN101883483B (en) * | 2009-05-06 | 2012-03-21 | 中国科学院半导体研究所 | Three-plate mini-type heat radiator |
US9615482B2 (en) | 2009-12-11 | 2017-04-04 | General Electric Company | Shaped heat sinks to optimize flow |
CN102456645A (en) * | 2010-10-26 | 2012-05-16 | 通用电气公司 | Thermal management system and method |
US9478479B2 (en) | 2010-10-26 | 2016-10-25 | General Electric Company | Thermal management system and method |
US8912643B2 (en) | 2012-12-10 | 2014-12-16 | General Electric Company | Electronic device cooling with microjet impingement and method of assembly |
CN104112725B (en) * | 2014-08-04 | 2017-01-04 | 华进半导体封装先导技术研发中心有限公司 | Radiator structure for high-power chip BGA package |
CN104112725A (en) * | 2014-08-04 | 2014-10-22 | 华进半导体封装先导技术研发中心有限公司 | Heat radiation structure used for BGA (Ball Grid Array) package of high-power chip |
US9823716B2 (en) | 2015-12-28 | 2017-11-21 | Lenovo (Beijing) Limited | Heat dissipation apparatus and electronic device |
CN105451523A (en) * | 2015-12-28 | 2016-03-30 | 联想(北京)有限公司 | Heat radiator and electronic device |
CN106440894A (en) * | 2016-10-07 | 2017-02-22 | 南京艾科美热能科技有限公司 | Heat equalizing plate with cavity internally having continuous jetting cooling function and method of heat equalizing plate |
CN106440894B (en) * | 2016-10-07 | 2019-01-11 | 南京艾科美热能科技有限公司 | A kind of intracavitary soaking plate and its method with continuous spray cooling function |
CN109216291A (en) * | 2017-06-29 | 2019-01-15 | 比亚迪股份有限公司 | Radiator for power module and the vehicle with it |
CN109216291B (en) * | 2017-06-29 | 2022-06-21 | 比亚迪半导体股份有限公司 | Radiator for power module and vehicle with radiator |
CN112352291B (en) * | 2018-05-29 | 2024-02-13 | 牛津大学创新有限公司 | Jet impingement cooling apparatus and method |
CN112352291A (en) * | 2018-05-29 | 2021-02-09 | 牛津大学创新有限公司 | Jet impingement cooling apparatus and method |
CN108712852A (en) * | 2018-07-12 | 2018-10-26 | 厦门大学 | A kind of microchannel heat sink of gas-liquid two-phase mixing jetting |
CN109195406B (en) * | 2018-08-28 | 2020-04-10 | 中国科学院理化技术研究所 | Heat sink device |
CN109195406A (en) * | 2018-08-28 | 2019-01-11 | 中国科学院理化技术研究所 | Heat sink device |
CN111386011A (en) * | 2020-01-09 | 2020-07-07 | 西安交通大学 | Side flow impact micro-channel cold plate and electronic equipment |
CN111148409B (en) * | 2020-01-09 | 2020-12-15 | 西安交通大学 | Jet flow micro-channel cold plate |
CN111148409A (en) * | 2020-01-09 | 2020-05-12 | 西安交通大学 | Jet flow micro-channel cold plate |
CN111386011B (en) * | 2020-01-09 | 2021-04-27 | 西安交通大学 | Side flow impact micro-channel cold plate and electronic equipment |
CN114279597A (en) * | 2021-12-28 | 2022-04-05 | 中国科学院长春光学精密机械与物理研究所 | High-precision low-power radiant heat flow meter capable of being used for radiant heat flow tracing calibration |
Also Published As
Publication number | Publication date |
---|---|
CN1233038C (en) | 2005-12-21 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN1233038C (en) | Microjet array cooling heat sink | |
Jörg et al. | Direct single impinging jet cooling of a MOSFET power electronic module | |
US8391008B2 (en) | Power electronics modules and power electronics module assemblies | |
CN203242614U (en) | Microfluidic-channel heat dissipation device used for an electronic component and electronic device | |
CN110164835A (en) | A kind of manifold-type labyrinth microchannel minitype radiator | |
CN104167399B (en) | The complicated microchannel micro heat exchanger of dislocation | |
US20120063085A1 (en) | Jet Impingement Heat Exchanger Apparatuses and Power Electronics Modules | |
JP6050617B2 (en) | Cooling device for power supply module and related method | |
US7992625B1 (en) | Fluid-operated heat transfer device | |
CN103188912A (en) | Lotus-type regular porous metal microchannel heat sink using liquid metal working medium | |
CN101854027A (en) | Liquid refrigerator for semiconductor laser | |
CN101640372B (en) | Novel single bar liquid refrigeration laser and manufacturing method thereof | |
CN209896047U (en) | Manifold type micro-channel micro radiator with complex structure | |
CN101635432B (en) | Liquid refrigerating chip for semiconductor laser and preparation method thereof | |
CN109979901A (en) | Two-side water cooling device for power electronic semiconductor | |
CN2632857Y (en) | Microject array cooled heat deposition | |
TWI726806B (en) | Water-cooling heat dissipation device and manufacturing method thereof | |
CN102620592B (en) | Preparation method for liquid refrigerator applied to semiconductor laser and refrigerating device for semiconductor laser | |
CN100486410C (en) | Fluid cross pin-rib array minisize heat exchanger | |
CN108712848B (en) | A kind of embedded jet strengthened heat-exchange radiator of rib wall punching | |
CN116190333A (en) | Cross flow-jet flow heat radiating device | |
CN116234266A (en) | Radiating assembly and electronic equipment | |
CN114551379A (en) | Chip radiator with high-efficient heat dispersion | |
CN202602082U (en) | Liquid cooling device for semiconductor laser | |
CN114828598A (en) | Liquid cooling radiator, electric drive controller and car |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
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 | ||
C17 | Cessation of patent right | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20051221 |