CN109640593B - A micro-rib array heat dissipation device and method equipped with a synthetic jet exciter - Google Patents
A micro-rib array heat dissipation device and method equipped with a synthetic jet exciter Download PDFInfo
- Publication number
- CN109640593B CN109640593B CN201811638293.0A CN201811638293A CN109640593B CN 109640593 B CN109640593 B CN 109640593B CN 201811638293 A CN201811638293 A CN 201811638293A CN 109640593 B CN109640593 B CN 109640593B
- Authority
- CN
- China
- Prior art keywords
- micro
- synthetic jet
- heat sink
- rib array
- heat
- 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.)
- Active
Links
- 230000017525 heat dissipation Effects 0.000 title claims abstract description 28
- 238000000034 method Methods 0.000 title claims abstract description 11
- 239000012530 fluid Substances 0.000 claims abstract description 14
- 230000000694 effects Effects 0.000 claims abstract description 13
- 239000000758 substrate Substances 0.000 claims description 24
- 238000012546 transfer Methods 0.000 claims description 13
- 230000008859 change Effects 0.000 claims description 8
- 238000010438 heat treatment Methods 0.000 claims description 8
- 238000011144 upstream manufacturing Methods 0.000 claims description 7
- 230000003993 interaction Effects 0.000 claims description 3
- 239000011148 porous material Substances 0.000 claims description 2
- 230000001105 regulatory effect Effects 0.000 claims 3
- 230000002708 enhancing effect Effects 0.000 abstract description 2
- 238000005516 engineering process Methods 0.000 description 7
- 238000010586 diagram Methods 0.000 description 4
- 230000004907 flux Effects 0.000 description 4
- 229910003460 diamond Inorganic materials 0.000 description 2
- 239000010432 diamond Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010892 electric spark Methods 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000004088 simulation Methods 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K7/00—Constructional details common to different types of electric apparatus
- H05K7/20—Modifications to facilitate cooling, ventilating, or heating
- H05K7/20218—Modifications to facilitate cooling, ventilating, or heating using a liquid coolant without phase change in electronic enclosures
Landscapes
- Engineering & Computer Science (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Cooling Or The Like Of Semiconductors Or Solid State Devices (AREA)
- Cooling Or The Like Of Electrical Apparatus (AREA)
Abstract
本发明公开了一种配备合成射流激励器的微肋阵散热装置及方法,该装置通过在微肋阵热沉顶部安装合成射流激励器并在微肋阵热沉顶部盖板上布置微孔,使得合成射流激励器在工作时,能够通过微孔周期性地吸入、喷出流体,形成合成射流。合成射流激励器产生的合成射流能够改善微肋阵内的流动环境,最终实现强化微肋阵热沉散热性能的效果。这种热沉结构的优点在于结构紧凑,强化散热效果好,对微肋阵热沉前后的压力降影响较小,并且可通过调节合成射流激励器的输入参数,实时调控热沉散热强度,为现代化高性能电子器件的散热问题以及温度控制提供一条新的路径。
The invention discloses a micro-rib array heat dissipation device and method equipped with a synthetic jet exciter. The device adopts a synthetic jet exciter on the top of a micro-rib array heat sink and arranges micro-holes on the top cover of the micro-rib array heat sink. When the synthetic jet exciter is working, the fluid can be periodically inhaled and ejected through the micro-holes to form a synthetic jet. The synthetic jet generated by the synthetic jet exciter can improve the flow environment in the micro-fin array, and finally achieve the effect of enhancing the heat dissipation performance of the micro-fin array heat sink. The advantages of this heat sink structure are that it is compact in structure, has good heat dissipation effect, and has little effect on the pressure drop before and after the micro-rib array heat sink. Thermal issues and temperature control in modern high-performance electronics offer a new avenue.
Description
技术领域technical field
本发明属于高热流密度的散热领域,具体涉及一种配备合成射流激励器的微肋阵散热装置及方法。The invention belongs to the field of heat dissipation with high heat flux density, and in particular relates to a micro-rib array heat dissipation device and method equipped with a synthetic jet exciter.
背景技术Background technique
在电子产品小型化、高性能化的发展趋势下,电子产品的热流密度呈现出迅速增长的趋势,这对电子产品的热设计提出了极高的要求,一些传统的被动式散热技术,已经无法满足极高热流密度情形下的散热需要,而新一代配备现代高效驱动、扰动技术的主动式强化散热技术,由于其具有极好的散热性能,并且具备可控性强等显著优点,已成为电子散热技术领域的研究重点。但目前现有的散热装置一般结构比较复杂,散热效果也不尽如人意。Under the development trend of miniaturization and high performance of electronic products, the heat flux density of electronic products shows a trend of rapid growth, which puts forward extremely high requirements for the thermal design of electronic products. Some traditional passive cooling technologies can no longer meet the requirements. The need for heat dissipation in the case of extremely high heat flux density, and the new generation of active enhanced heat dissipation technology equipped with modern high-efficiency drive and disturbance technology, due to its excellent heat dissipation performance and strong controllability and other significant advantages, has become an electronic heat dissipation technology. Research focus in the field of technology. However, the current existing heat dissipation devices generally have complex structures, and the heat dissipation effect is not satisfactory.
发明内容SUMMARY OF THE INVENTION
为了解决现代高性能电子产品的高热流密度问题,弥补传统被动式散热技术的不足,本发明提供了一种配备合成射流激励器的微肋阵散热装置及方法。In order to solve the problem of high heat flux density of modern high-performance electronic products and make up for the deficiency of traditional passive heat dissipation technology, the present invention provides a micro-rib array heat dissipation device and method equipped with a synthetic jet exciter.
一种配备合成射流激励器的微肋阵散热装置,包括热沉基板、微肋阵结构、顶部盖板、合成射流激励器;所述的热沉基板与电子器件的发热部分直接或者间接相连;所述的微肋阵结构位于热沉基板上方;所述的顶部盖板位于微肋阵结构上方,顶部盖板与热沉基板之间通有流体;所述的合成射流激励器为底部敞口结构,位于顶部盖板上方与顶部盖板装配形成合成射流腔体,所述的顶部盖板上开设有微孔阵列。A micro-rib array heat dissipation device equipped with a synthetic jet exciter, comprising a heat sink substrate, a micro-rib array structure, a top cover, and a synthetic jet exciter; the heat sink substrate is directly or indirectly connected with a heating part of an electronic device; The micro-rib array structure is located above the heat sink substrate; the top cover plate is located above the micro-rib array structure, and fluid is communicated between the top cover plate and the heat sink substrate; the synthetic jet exciter is open at the bottom The structure is located above the top cover plate and assembled with the top cover plate to form a synthetic jet cavity, and the top cover plate is provided with a micropore array.
上述技术方案中,所述的微肋阵结构的排列方式可以采用顺排、叉排、组合排列或无序排列,微肋阵结构中各肋片的横截面形状可以为矩形、圆形、三角形、或菱形等,横截面尺寸随肋片高度发生变化。In the above technical scheme, the arrangement of the micro-rib array structure can be in order, fork, combined or disordered, and the cross-sectional shape of each rib in the micro-rib array structure can be rectangular, circular, triangular. , or rhombus, etc., the cross-sectional size changes with the height of the rib.
所述的微孔阵列的排列方式通常与微肋阵结构一致,各微孔的横截面形状为矩形、圆形、三角形、或菱形等,微孔的大小随孔深发生变化,形成锥形孔。The arrangement of the micro-hole array is usually consistent with the micro-rib array structure, the cross-sectional shape of each micro-hole is rectangle, circle, triangle, or diamond, etc., and the size of the micro-hole changes with the depth of the hole, forming a conical hole. .
所述的合成射流腔体可以为长方体、圆柱体、或其他任意形状。The synthetic jet cavity can be a cuboid, a cylinder, or any other shape.
所述的合成射流激励器的驱动方式可以是火花、压电、等离子体驱动等。The driving manner of the synthetic jet exciter may be spark, piezoelectric, plasma driving, and the like.
应用上述的装置进行散热的方法,如下:将热沉基板与电子器件的发热部分直接或间接相连,在顶部盖板与热沉基板之间通入流体,热沉基板通过热传导接收来自电子器件发热部分的热量,并传递至微肋阵结构;微肋阵结构通过对流换热效应将热量传递给上游来流,启动合成射流激励器进入主动模式;在主动模式下,无需改变来流条件,通过调节合成射流激励器的输入参数,可实时对微肋阵热沉的散热性能进行调控,具体为调节合成射流激励器的输入参数使得合成射流腔体内的压力呈现周期性升降,这种压力变化使得合成射流激励器周期性地通过顶部盖板上的微孔阵列吸入、喷出流体,形成合成射流;合成射流与来自上游的流体之间产生相互作用,改善流动结构并提高微肋阵结构表面与热沉基板上表面的对流换热效果,从而实现散热性能的强化。The method of applying the above-mentioned device for heat dissipation is as follows: the heat sink substrate is directly or indirectly connected to the heating part of the electronic device, a fluid is passed between the top cover plate and the heat sink substrate, and the heat sink substrate receives heat from the electronic device through thermal conduction. Part of the heat is transferred to the micro-rib array structure; the micro-rib array structure transfers the heat to the upstream flow through the convective heat transfer effect, and the synthetic jet exciter is activated to enter the active mode; in the active mode, there is no need to change the incoming flow conditions. Adjusting the input parameters of the synthetic jet exciter can control the heat dissipation performance of the micro-rib array heat sink in real time. Specifically, adjusting the input parameters of the synthetic jet exciter makes the pressure in the synthetic jet cavity rise and fall periodically. This pressure change makes The synthetic jet exciter periodically sucks and ejects fluid through the micro-hole array on the top cover to form a synthetic jet; the interaction between the synthetic jet and the fluid from the upstream improves the flow structure and enhances the surface of the micro-rib array structure. The convection heat transfer effect on the upper surface of the heat sink substrate, thereby enhancing the heat dissipation performance.
本发明的有益效果在于:第一,采用合成射流激励器作为扰动装置,结构紧凑,扰流效果好;第二,无需改变来流条件,仅需通过调节合成射流激励器的工作参数即可实时对热沉结构的散热性能进行调节,凸显了配备合成射流激励器的热沉结构可控性强的特点;第三,采用微肋阵结构作为基础热沉结构,散热效果好,易于加工。The beneficial effects of the present invention are as follows: first, the synthetic jet exciter is used as the disturbance device, which has a compact structure and a good effect of disturbing the flow; second, it does not need to change the incoming flow conditions, and only needs to adjust the working parameters of the synthetic jet exciter. Adjusting the heat dissipation performance of the heat sink structure highlights the strong controllability of the heat sink structure equipped with the synthetic jet exciter; thirdly, the micro-rib array structure is used as the basic heat sink structure, which has good heat dissipation effect and is easy to process.
附图说明Description of drawings
图1是配备合成射流激励器的微肋阵散热装置的结构示意图;Fig. 1 is the structural schematic diagram of the micro-rib array heat sink equipped with synthetic jet exciter;
图2是合成射流激励器结构三视图;Fig. 2 is three views of the structure of the synthetic jet exciter;
图3是微肋阵热沉结构示意图;Figure 3 is a schematic diagram of the structure of the micro-rib array heat sink;
图4是微肋阵热沉顶部盖板结构示意图;Figure 4 is a schematic diagram of the structure of the top cover plate of the micro-rib array heat sink;
图5是合成射流激励器腔体结构说明图;FIG. 5 is an explanatory diagram of the cavity structure of the synthetic jet exciter;
附图标记说明:1.热沉基板;2.微肋阵结构;3.顶部盖板;4.合成射流激励器;5.微孔阵列;6.合成射流腔体。Description of reference numerals: 1. Heat sink substrate; 2. Micro-rib array structure; 3. Top cover plate; 4. Synthetic jet actuator; 5. Microwell array; 6. Synthetic jet cavity.
具体实施方式Detailed ways
下面结合附图和实施例对本发明作进一步的说明。The present invention will be further described below with reference to the accompanying drawings and embodiments.
如图1所示,一种配备合成射流激励器的微肋阵散热装置,它包括热沉基板1、微肋阵结构2、顶部盖板3、合成射流激励器4;热沉基板1直接或间接与热源相连;微肋阵结构2位于热沉基板1上方;顶部盖板3位于微肋阵结构2上方;合成射流激励器4底部为敞口结构,位于顶部盖板3上方与顶部盖板3装配形成合成射流腔体6。As shown in Figure 1, a micro-rib array heat dissipation device equipped with a synthetic jet exciter includes a
如图3所示,所述的热沉基板1与电子器件的发热部分直接或通过热管等装置间接相连,从而通过热传导接收来自电子器件发热部分的热量,并传递至微肋阵结构2。As shown in FIG. 3 , the
如图3所示,所述的微肋阵结构2可设计为顺排、叉排、组合排列、无序排列等多种排列方式,微肋阵结构中各肋片的横截面形状可设计为矩形、圆形、三角形、菱形等多种形状,肋片的横截面尺寸可随肋片高度发生变化;在顶部盖板与热沉基板之间通有流体,微肋阵接收来自于热沉基板1的热量,并通过对流换热效应将热量传递给来自于上游的低温流体。As shown in FIG. 3 , the
如图4所示,所述的顶部盖板3,其表面布置有微孔阵列5,微孔阵列可设计为顺排、叉排、组合排列、无序排列等多种排列方式,微孔的横截面形状可设计为矩形、圆形、三角形、菱形等多种形状,微孔的大小可随孔深发生变化,形成锥形孔。As shown in FIG. 4 , the
如图2、5所示,所述的合成射流激励器4,其敞口部分与顶部盖板3装配之后形成合成射流腔体6;合成射流激励器4的合成射流腔体6可设计为长方体、圆柱体、异形体等多种形状;合成射流激励器4可使用电火花、压电、等离子体等多种方式进行驱动,只要能调节合成射流腔体内压力即可。As shown in Figures 2 and 5, the synthetic jet exciter 4, its open part is assembled with the
上述配备合成射流激励器的微肋阵散热装置的工作方法为:热沉基板1与电子器件的发热部分直接或通过热管等装置间接相连,从而通过热传导接收来自电子器件发热部分的热量,并传递至微肋阵结构2;微肋阵结构2接收来自于热沉基板1的热量,并通过对流换热效应将热量传递给来自于上游的低温流体;启动合成射流激励器进入主动模式;在主动模式下,无需改变来流条件,仅通过调节合成射流激励器的输入参数,即可实时对微肋阵热沉的散热性能进行调控,具体为合成射流激励器腔体6内的压力会随着激励器输入参数的变化相应地变化,这种压力变化使得合成射流激励器4能够周期性地通过顶部盖板3上的微孔吸入、喷出流体,形成合成射流;合成射流与来自上游的流体之间产生相互作用,改善了微肋阵热沉内部的流动结构,提高了微肋阵表面与热沉基板上表面的对流换热效果,从而实现散热性能的强化。The working method of the above-mentioned micro-rib array heat sink equipped with a synthetic jet exciter is as follows: the
采用本发明的装置与传统的微肋阵散热装置相比,在微孔峰值速度为3m/s的条件下,全局平均对流换热系数可提高80%以上,而压降增长量仅为30%。通过仿真分析可知,在合成射流激励器的影响下,一方面,微肋阵散热装置内部前排微肋片与后排微肋片之间流动滞止区域内的整体动量水平有了明显的提高;另一方面,合成射流对微肋片下游表面的流动分离现象具有明显的抑制作用,在这两种作用的综合影响下,流动滞止区与主流区之间的动量交换更为频繁,对流换热更为充分,并且由于合成射流微孔位置布置在流动滞止区域内,合成射流对主流的影响有限,从而使得整体压降损失的增长量较小。此外,与传统的连续式或者间歇式射流强化技术相比,合成射流具有结构紧凑、调控方便、维护简单等诸多优势,这使得合成射流在微结构散热领域具有十分突出的优越性与广阔的应用前景。Compared with the traditional micro-rib array heat dissipation device, the device of the present invention can increase the global average convective heat transfer coefficient by more than 80% under the condition that the peak velocity of the micro-pore is 3m/s, while the increase of the pressure drop is only 30%. . Through the simulation analysis, it can be seen that under the influence of the synthetic jet exciter, on the one hand, the overall momentum level in the flow stagnation area between the front row of micro-fins and the rear row of micro-fins inside the micro-fin array heat sink has been significantly improved. On the other hand, the synthetic jet has an obvious inhibitory effect on the flow separation phenomenon on the downstream surface of the micro-fins. Under the combined influence of these two effects, the momentum exchange between the flow stagnation area and the main flow area is more frequent, and the convection The heat exchange is more sufficient, and the synthetic jet has a limited influence on the main flow due to the arrangement of the micropores of the synthetic jet in the flow stagnation area, so that the increase in the overall pressure drop loss is small. In addition, compared with the traditional continuous or intermittent jet enhancement technology, the synthetic jet has many advantages such as compact structure, convenient control, and simple maintenance, which makes the synthetic jet have outstanding advantages and broad applications in the field of microstructure heat dissipation. prospect.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811638293.0A CN109640593B (en) | 2018-12-29 | 2018-12-29 | A micro-rib array heat dissipation device and method equipped with a synthetic jet exciter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811638293.0A CN109640593B (en) | 2018-12-29 | 2018-12-29 | A micro-rib array heat dissipation device and method equipped with a synthetic jet exciter |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109640593A CN109640593A (en) | 2019-04-16 |
| CN109640593B true CN109640593B (en) | 2020-12-08 |
Family
ID=66055005
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811638293.0A Active CN109640593B (en) | 2018-12-29 | 2018-12-29 | A micro-rib array heat dissipation device and method equipped with a synthetic jet exciter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109640593B (en) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111970897B (en) * | 2020-08-06 | 2022-06-21 | 中国电子科技集团公司第三十八研究所 | Heat exchange radiator is reinforceed to semi-enclosed island type rib pole side hole vortex |
| CN113289529B (en) * | 2021-05-10 | 2022-07-12 | 浙江大学 | Microfluid mixer based on piezoelectric type synthetic jet technology and mixing method thereof |
| CN113873842B (en) * | 2021-09-28 | 2022-06-07 | 北京大学 | Heat dissipation device and heat dissipation regulation and control method |
| CN114334858B (en) * | 2021-12-27 | 2022-11-01 | 哈尔滨工业大学 | Electric-drive self-circulation flexible heat dissipation device integrated with micro-rib channel and manufacturing method thereof |
| CN115551303A (en) * | 2022-09-28 | 2022-12-30 | 华中科技大学 | Rib matrix microchannel heat sink with top gap |
| CN117832184B (en) * | 2024-01-08 | 2025-05-23 | 安徽理工大学 | Double-layer micro-channel jet flow cooling heat sink device |
| CN120527321B (en) * | 2025-07-25 | 2025-10-03 | 浪潮计算机科技有限公司 | Microchannel heat exchanger |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7597135B2 (en) * | 2006-05-23 | 2009-10-06 | Coolit Systems Inc. | Impingement cooled heat sink with low pressure drop |
| US7511957B2 (en) * | 2006-05-25 | 2009-03-31 | International Business Machines Corporation | Methods for fabricating a cooled electronic module employing a thermally conductive return manifold structure sealed to the periphery of a surface to be cooled |
| US8944151B2 (en) * | 2008-05-28 | 2015-02-03 | International Business Machines Corporation | Method and apparatus for chip cooling |
| CN102271485B (en) * | 2011-05-12 | 2015-09-23 | 南京理工大学 | Array jetting, boiling cooling exchange method based on combination under high heat flux condition |
| CN203708731U (en) * | 2013-11-19 | 2014-07-09 | 中国计量学院 | Intermittent impact jet fractal fin cooling device |
| US10265812B2 (en) * | 2015-08-12 | 2019-04-23 | International Business Machines Corporation | Liquid-cooled, composite heat sink assemblies |
-
2018
- 2018-12-29 CN CN201811638293.0A patent/CN109640593B/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN109640593A (en) | 2019-04-16 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN109640593B (en) | A micro-rib array heat dissipation device and method equipped with a synthetic jet exciter | |
| CN107223004B (en) | A device and method for microchannel surface spray cooling to enhance heat transfer | |
| CN112201635B (en) | A kind of synergistically driven high heat flux density chip phase change cooling device and method | |
| CN103415190A (en) | Abnormal channel array jet flow impact cold plate | |
| CN104658992A (en) | Novel micro heat sink provided with pin-fin array | |
| CN109386399B (en) | A structure with a circuitous inner flow channel and a manufacturing method thereof | |
| CN110381700B (en) | A spray cavity and steam cavity integrated phase change cooling device and system | |
| CN103075202A (en) | Impingement cooling structure with grid turbulence effect in turbine blade | |
| CN109618481B (en) | Plasma Synthetic Jet Exciter at Low Reynolds Number | |
| CN110319456A (en) | A kind of solid-rocket scramjet engine using multistage combustion enhancement device | |
| CN104154512B (en) | Heat dissipation device of LED lamp based on synthesis dual-jet driver | |
| CN104648674A (en) | Low-resistance fan-aided ejecting air feeding device | |
| CN204992243U (en) | Cooling of 3D printing technique preparation is heat sink | |
| CN103826422A (en) | Microchannel cooling device | |
| TW200900592A (en) | Jets device | |
| CN108598049A (en) | A kind of electronic component radiator | |
| CN107054673A (en) | It is a kind of to synthesize dual-jet driver and hypersonic flow flowing control method from maintenance | |
| CN120308331B (en) | Intelligent flow control method and system for air suction type high-speed aircraft | |
| CN103824825B (en) | Micro-channel phase change heat exchange device | |
| CN110381701B (en) | A spray cooling device combining steam cavity and composite microstructure | |
| CN202747837U (en) | Steam heater | |
| CN109462964A (en) | Boiling heat transfer structure | |
| CN202841823U (en) | Pulse jet fin cooling unit | |
| CN207969271U (en) | Integrated VR glasses radiator based on piezoelectric type synthesizing jet-flow and heat pipe | |
| CN206171797U (en) | Spark type synthetic jet energizer based on solenoid valve |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |