CN109149325B - A Hybrid Structure Microchannel Heat Sink - Google Patents
A Hybrid Structure Microchannel Heat Sink Download PDFInfo
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- CN109149325B CN109149325B CN201811106670.6A CN201811106670A CN109149325B CN 109149325 B CN109149325 B CN 109149325B CN 201811106670 A CN201811106670 A CN 201811106670A CN 109149325 B CN109149325 B CN 109149325B
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- 230000017525 heat dissipation Effects 0.000 claims abstract description 11
- 239000000758 substrate Substances 0.000 claims abstract description 9
- 238000005530 etching Methods 0.000 claims abstract description 3
- 239000000463 material Substances 0.000 claims description 10
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 5
- 229910052710 silicon Inorganic materials 0.000 claims description 5
- 239000010703 silicon Substances 0.000 claims description 5
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 3
- 229910052802 copper Inorganic materials 0.000 claims description 3
- 239000010949 copper Substances 0.000 claims description 3
- 239000002210 silicon-based material Substances 0.000 claims description 2
- 238000000034 method Methods 0.000 abstract description 5
- 239000000110 cooling liquid Substances 0.000 abstract description 3
- 239000002826 coolant Substances 0.000 description 16
- 238000001816 cooling Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 5
- 230000004907 flux Effects 0.000 description 5
- 239000007788 liquid Substances 0.000 description 4
- 230000002708 enhancing effect Effects 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 238000004064 recycling Methods 0.000 description 2
- 238000004088 simulation Methods 0.000 description 2
- 230000008646 thermal stress Effects 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 238000009828 non-uniform distribution Methods 0.000 description 1
- 239000002861 polymer material Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01S—DEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
- H01S3/00—Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
- H01S3/02—Constructional details
- H01S3/04—Arrangements for thermal management
- H01S3/0407—Liquid cooling, e.g. by water
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01S—DEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
- H01S5/00—Semiconductor lasers
- H01S5/02—Structural details or components not essential to laser action
- H01S5/024—Arrangements for thermal management
- H01S5/02407—Active cooling, e.g. the laser temperature is controlled by a thermo-electric cooler or water cooling
- H01S5/02423—Liquid cooling, e.g. a liquid cools a mount of the laser
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- Optics & Photonics (AREA)
- Engineering & Computer Science (AREA)
- Plasma & Fusion (AREA)
- Condensed Matter Physics & Semiconductors (AREA)
- General Physics & Mathematics (AREA)
- Cooling Or The Like Of Semiconductors Or Solid State Devices (AREA)
- Cooling Or The Like Of Electrical Apparatus (AREA)
Abstract
本发明公开了一种混合结构微通道热沉,包括密封连接的热沉模块和盖板,盖板位于热沉模块的上方,盖板上设置有若干个间隔设置的进口和出口,热沉模块包括基底以及通过刻蚀或机械加工方式在所述基底上得到的微通道散热结构,所述微通道散热结构包括若干个平行设置的肋片,所述肋片之间构成微通道,微通道与进口和出口垂直设置,肋片上开设有二次流道,进口和出口之间设有矩形肋片;进口下方的基底上设置有与进口相对应的大肋片,大肋片的长度等于进口的宽度。本发明的歧管式、二次流道和矩形肋片组成的混合结构热沉缩短了冷却液在微通道中的流动距离,增大了流动空间,并增强了流动过程中的扰动,从而可同时增强换热和降低压损,并进一步提高了芯片温度的均匀性。
The invention discloses a microchannel heat sink with a mixed structure, which comprises a heat sink module and a cover plate sealed and connected, the cover plate is located above the heat sink module, and several inlets and outlets arranged at intervals are provided on the cover plate It includes a substrate and a microchannel heat dissipation structure obtained on the substrate by etching or mechanical processing. The microchannel heat dissipation structure includes several parallel fins, and microchannels are formed between the fins. The microchannels and The inlet and outlet are arranged vertically, the fins are provided with a secondary flow channel, and a rectangular fin is arranged between the inlet and the outlet; a large fin corresponding to the inlet is arranged on the base below the inlet, and the length of the large fin is equal to that of the inlet. width. The mixed structure heat sink composed of manifold type, secondary flow channel and rectangular fins of the present invention shortens the flow distance of the cooling liquid in the microchannel, increases the flow space, and enhances the disturbance in the flow process, so that it can At the same time, it enhances heat transfer and reduces pressure loss, and further improves the uniformity of chip temperature.
Description
技术领域technical field
本发明涉及热沉的技术领域,特别是涉及一种混合结构微通道热沉。The invention relates to the technical field of heat sinks, in particular to a microchannel heat sink with a mixed structure.
背景技术Background technique
随着科学技术的进步,芯片的运算速度越来越快,集成度越来越高,因此单位面积上产生的热量越来越多,如果不能及时把热量带走的话,芯片的可靠性会降低,性能会下降,寿命也会缩短。With the advancement of science and technology, the computing speed of the chip is getting faster and higher, and the integration is getting higher and higher, so more and more heat is generated per unit area. If the heat cannot be taken away in time, the reliability of the chip will be reduced. , the performance will decrease and the life will be shortened.
解决这个问题的方法之一是通过热沉结构将热量带走,包括风冷和液冷。风冷适用于热流密度小于10W/cm2的情况,对于高热流密度散热要求,需要引入液体进行冷却。1981年,美国的两位学者提出了微通道液冷的概念,他们用50μm宽320μm高的微通道阵列热沉,实现了790W/cm2的高热流密度散热要求,但是所需的压损高达216kPa,很难获得实际应用。One of the ways to solve this problem is to take the heat away through the heat sink structure, including air cooling and liquid cooling. Air cooling is suitable for situations where the heat flux density is less than 10W/cm 2 , and for high heat flux dissipation requirements, it is necessary to introduce liquid for cooling. In 1981, two scholars in the United States proposed the concept of microchannel liquid cooling. They used a microchannel array heat sink with a width of 50 μm and a height of 320 μm to achieve a high heat flux dissipation requirement of 790W/ cm2 , but the required pressure loss was as high as 216kPa, it is difficult to obtain practical application.
为此,大量学者对微通道热沉的结构进行了改进和优化,但是目前的微通道热沉存在的问题是:1.如果想要达到较大的热流密度q,需要付出的压损ΔP会很大;2.合理的压损ΔP,所能散出的热流密度q又非常有限;3.微通道热沉散热带来芯片温度的不均匀性,从而带来热应力,对芯片的可靠性、性能、寿命均带来不利影响。For this reason, a large number of scholars have improved and optimized the structure of micro-channel heat sinks, but the existing problems of micro-channel heat sinks are: 1. If you want to achieve a larger heat flux q, the pressure loss ΔP that needs to be paid will be larger Very large; 2. Reasonable pressure loss ΔP, the heat flux q that can be dissipated is very limited; 3. The heat dissipation of the micro-channel heat sink brings the unevenness of the chip temperature, which brings thermal stress, which affects the reliability of the chip , performance, and life are adversely affected.
发明内容Contents of the invention
本发明的目的是提供一种混合结构微通道热沉,以解决上述现有技术存在的问题,一方面可以降低压损和泵功,另一方面,可以降低芯片表面的最高温度并提高芯片表面温度的均匀性,进而提高芯片的可靠性、性能和寿命。The purpose of the present invention is to provide a microchannel heat sink with a hybrid structure to solve the problems of the above-mentioned prior art. On the one hand, it can reduce the pressure loss and pump work, on the other hand, it can reduce the maximum temperature of the chip surface and improve Uniformity of temperature, which in turn improves chip reliability, performance and lifetime.
为实现上述目的,本发明提供了如下方案:To achieve the above object, the present invention provides the following scheme:
本发明提供了一种混合结构微通道热沉,包括密封连接的热沉模块和盖板,所述盖板位于所述热沉模块的上方,所述盖板上设置有若干个间隔设置的进口和出口,所述热沉模块包括基底以及通过刻蚀或机械加工方式在所述基底上得到的微通道散热结构,所述微通道散热结构包括若干个平行设置的肋片,所述肋片之间构成微通道,所述微通道与所述进口和所述出口垂直设置,所述肋片上开设有二次流道,所述进口和所述出口之间的所述微通道内设有矩形肋片;所述进口下方的所述基底上设置有与所述进口相对应的大肋片,所述大肋片的长度等于所述进口的宽度。The invention provides a microchannel heat sink with a hybrid structure, which includes a heat sink module and a cover plate that are sealed and connected, the cover plate is located above the heat sink module, and several inlets arranged at intervals are arranged on the cover plate and an outlet, the heat sink module includes a substrate and a micro-channel heat dissipation structure obtained on the substrate by etching or machining, the micro-channel heat dissipation structure includes several parallel fins, one of the fins The microchannel is formed between the inlet and the outlet, the microchannel is vertically arranged with the inlet and the outlet, and a secondary flow channel is opened on the rib, and a rectangular rib is arranged in the microchannel between the inlet and the outlet. sheet; the base below the inlet is provided with a large rib corresponding to the inlet, and the length of the large rib is equal to the width of the inlet.
优选的,所述矩形肋片为若干个且均布于所述微通道出口处。Preferably, there are several rectangular fins uniformly distributed at the outlet of the microchannel.
优选的,每一竖列所述矩形肋片竖向对齐且为一组,所述矩形肋片设置为一至八组的任意数量。Preferably, the rectangular ribs in each vertical row are vertically aligned and form a group, and the rectangular ribs are arranged in any number from one to eight groups.
优选的,所述矩形肋片替换为平行四边形、菱形、三角形和翼形肋片中的一种。Preferably, the rectangular ribs are replaced with one of parallelogram, rhombus, triangle and wing-shaped ribs.
优选的,所述肋片被所述二次流道分割为若干个梯形肋片或平行四边形肋片,所述梯形肋片的形状为等腰梯形。Preferably, the fins are divided into several trapezoidal fins or parallelogram fins by the secondary flow channel, and the shape of the trapezoidal fins is an isosceles trapezoid.
优选的,所述热沉模块为高导热材料。Preferably, the heat sink module is made of high thermal conductivity material.
优选的,所述高导热材料为铜或者硅材料。Preferably, the high thermal conductivity material is copper or silicon.
优选的,所述进口宽度为所述出口宽度的两倍。Preferably, the width of the inlet is twice the width of the outlet.
优选的,所述基底替换为芯片背面的硅板。Preferably, the substrate is replaced by a silicon plate on the back of the chip.
本发明相对于现有技术取得了以下技术效果:Compared with the prior art, the present invention has achieved the following technical effects:
本发明的歧管式、二次流道和矩形肋片组成的混合结构热沉可通过歧管结构缩短冷却液在微通道中的流动距离,通过二次流道增强流体的掺混,并增大流动空间,通过矩形肋片使得更多流体流入二次流道,从而可同时增强换热和降低压损,并提高芯片的温度均匀性。The mixed structure heat sink composed of manifold type, secondary flow channel and rectangular fins of the present invention can shorten the flow distance of cooling liquid in the microchannel through the manifold structure, enhance the mixing of fluid through the secondary flow channel, and increase the The large flow space allows more fluid to flow into the secondary channel through the rectangular fins, thereby enhancing heat transfer and reducing pressure loss at the same time, and improving the temperature uniformity of the chip.
附图说明Description of drawings
为了更清楚地说明本发明实施例或现有技术中的技术方案,下面将对实施例中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图仅仅是本发明的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图。In order to more clearly illustrate the technical solutions in the embodiments of the present invention or the prior art, the following will briefly introduce the accompanying drawings required in the embodiments. Obviously, the accompanying drawings in the following description are only some of the present invention. Embodiments, for those of ordinary skill in the art, other drawings can also be obtained based on these drawings without any creative effort.
图1为本发明混合结构微通道热沉的歧管式结构的原理示意图(未画出二次流道和矩形肋片结构);Fig. 1 is the schematic diagram of the principle of the manifold structure of the hybrid structure microchannel heat sink of the present invention (the secondary runner and the rectangular fin structure are not drawn);
图2为本发明混合结构微通道热沉的热沉模块的结构示意图;Fig. 2 is the structural representation of the heat sink module of the hybrid structure microchannel heat sink of the present invention;
图3为本发明混合结构微通道热沉盖板的结构示意图;Fig. 3 is the structure schematic diagram of the hybrid structure microchannel heat sink cover plate of the present invention;
图4为本发明带三角形肋片的混合结构微通道热沉的结构示意图;Fig. 4 is the structural representation of the mixed structure microchannel heat sink with triangular fins of the present invention;
图5为本发明混合结构微通道热沉的结构示意图一;Fig. 5 is a structural schematic diagram 1 of the hybrid structure microchannel heat sink of the present invention;
图6为本发明混合结构微通道热沉的结构示意图二;Fig. 6 is the structural schematic diagram II of the hybrid structure microchannel heat sink of the present invention;
图7为本发明混合结构微通道热沉的结构示意图三;Fig. 7 is the structural schematic diagram III of the hybrid structure microchannel heat sink of the present invention;
其中:1-基底,2-盖板,3-进口,4-出口,5-微通道,6-梯形肋片,7-矩形肋片,8-三角形肋片,9-大梯形肋片,10-二次流道。Among them: 1-base, 2-cover plate, 3-inlet, 4-outlet, 5-microchannel, 6-trapezoidal fin, 7-rectangular fin, 8-triangular fin, 9-large trapezoidal fin, 10 -Secondary runner.
具体实施方式Detailed ways
下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有付出创造性劳动的前提下所获得的所有其他实施例,都属于本发明保护的范围。The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
本发明的目的是提供一种混合结构微通道热沉,以解决现有技术存在的问题,可以同时增强换热和降低压损,并使芯片表面温度的均匀性得以提高,进而提高芯片的可靠性、性能和寿命。The purpose of the present invention is to provide a micro-channel heat sink with a hybrid structure to solve the problems existing in the prior art, which can simultaneously enhance heat transfer and reduce pressure loss, and improve the uniformity of chip surface temperature, thereby improving the reliability of the chip performance, performance and longevity.
为使本发明的上述目的、特征和优点能够更加明显易懂,下面结合附图和具体实施方式对本发明作进一步详细的说明。In order to make the above objects, features and advantages of the present invention more comprehensible, the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.
如图1至图7所示:本实施例提供了一种混合结构微通道热沉,密封连接的热沉模块和盖板2,盖板2位于热沉模块的上方,盖板2上设置有若干个间隔设置的进口3和出口4,热沉模块包括基底1和刻蚀或机械加工在基底上的微通道散热结构。热沉模块为高导热材料,高导热材料优选为铜或者硅材料,高导热材料还可以为铝或其他高导热金属合金等导热系数高的材料,便于散热。盖板2为低导热材料,优选为聚合物材料,便于加工和成型。As shown in Figures 1 to 7: this embodiment provides a microchannel heat sink with a hybrid structure, the heat sink module and the cover plate 2 are sealed and connected, the cover plate 2 is located above the heat sink module, and the cover plate 2 is provided with Several inlets 3 and outlets 4 are provided at intervals, and the heat sink module includes a base 1 and a microchannel heat dissipation structure etched or machined on the base. The heat sink module is made of high thermal conductivity material. The high thermal conductivity material is preferably copper or silicon material. The high thermal conductivity material can also be aluminum or other high thermal conductivity metal alloys and other materials with high thermal conductivity to facilitate heat dissipation. The cover plate 2 is made of low thermal conductivity material, preferably a polymer material, which is convenient for processing and molding.
盖板2位于基底1的上方,盖板2上设置有若干个间隔设置的进口3和出口4,本实施例中的进口3宽度为出口4宽度的两倍。本实施例中的混合结构微通道热沉作为其中一个单元,其盖板2上设置有一个进口3,两个出口4,还可以为一个出口4,两个进口3。微通道5内用于流通冷却介质。其中,冷却介质可以为水、HFE-7100、氟利昂等液体,还可以为空气或氮气等气体介质。在盖板2的一端上设置有冷却介质的导入孔和导出孔,便于对冷却介质的更换或者循环利用。The cover plate 2 is located above the base 1. Several inlets 3 and outlets 4 are provided on the cover 2 at intervals. In this embodiment, the width of the inlet 3 is twice the width of the outlet 4 . The mixed structure microchannel heat sink in this embodiment is used as one of the units, and its cover plate 2 is provided with one inlet 3 and two outlets 4 , or one outlet 4 and two inlets 3 . The microchannel 5 is used for circulating cooling medium. Wherein, the cooling medium can be water, HFE-7100, Freon and other liquids, and can also be gaseous medium such as air or nitrogen. One end of the cover plate 2 is provided with an inlet hole and an outlet hole for the cooling medium, which facilitates replacement or recycling of the cooling medium.
基底1上设置有若干个平行设置的肋片,肋片之间构成微通道5,本实施例中的微通道5与进口3和出口4垂直设置,其中,微通道5与进口3和出口4还可以相交设置,其夹角不限制于90°,可以为任意角。其中,进口3和出口4相邻设计,可以减少冷却介质的在微通道5中的流动距离和压损。The substrate 1 is provided with several ribs arranged in parallel, and the microchannel 5 is formed between the ribs. The microchannel 5 in this embodiment is vertically arranged with the inlet 3 and the outlet 4, wherein the microchannel 5 is connected with the inlet 3 and the outlet 4 It can also be arranged to intersect, and the included angle is not limited to 90°, and can be any angle. Wherein, the inlet 3 and the outlet 4 are adjacently designed, which can reduce the flow distance and pressure loss of the cooling medium in the microchannel 5 .
进口3下方的基底1上设置有与梯形肋片6相匹配的大梯形肋片9,大梯形肋片9的长底边的长度等于进口3的宽度。肋片上开设有二次流道10,肋片被二次流道10分割为若干个梯形肋片6或平行四边形肋片。其中,梯形肋片6的形状优选为等腰梯形。相邻梯形肋片6之间的间隙形成的二次流道10可以增强冷却介质流动过程中的扰动,从而增强换热,且二次流道10增大了流动空间,在一定程度上也可以降低压损。The base 1 below the inlet 3 is provided with a large trapezoidal rib 9 matching the trapezoidal rib 6 , and the length of the long base of the large trapezoidal rib 9 is equal to the width of the inlet 3 . A secondary flow channel 10 is opened on the fin, and the fin is divided into several trapezoidal fins 6 or parallelogram fins by the secondary flow channel 10 . Wherein, the shape of the trapezoidal ribs 6 is preferably an isosceles trapezoid. The secondary flow channel 10 formed by the gap between adjacent trapezoidal fins 6 can enhance the turbulence in the flow process of the cooling medium, thereby enhancing heat exchange, and the secondary flow channel 10 increases the flow space, and to a certain extent can also Reduce pressure loss.
进口3和出口4之间的微通道5内设有矩形肋片7。本实施例的混合结构微通道热沉的矩形肋片7均布于微通道5内部的两端。矩形肋片7可以替换为平行四边形肋片、菱形肋片、三角形肋片8和翼形肋片中的一种。其中,矩形肋片7可以在进口3两侧均匀排布,也可以在进口3两侧非均匀排布,使得更多的冷却介质流入流道中进一步增强换热。本实施例中均匀排布的矩形肋片7设置的是八组,可以使得更多的冷却介质流入微通道5中,进一步增强换热。矩形肋片7也可以在进口3两侧处非均匀排布,非均匀排布时,可根据梯形肋片6的数量设置任意组数,用于提高热源的温度均匀性,并降低热应力。Rectangular ribs 7 are arranged in the microchannel 5 between the inlet 3 and the outlet 4 . The rectangular fins 7 of the mixed-structure microchannel heat sink in this embodiment are evenly distributed at both ends of the microchannel 5 . The rectangular fins 7 can be replaced by one of parallelogram fins, rhombus fins, triangular fins 8 and wing-shaped fins. Wherein, the rectangular fins 7 can be evenly arranged on both sides of the inlet 3, or can be arranged non-uniformly on both sides of the inlet 3, so that more cooling medium flows into the flow channel to further enhance heat exchange. In this embodiment, there are eight sets of uniformly arranged rectangular fins 7, which can allow more cooling medium to flow into the microchannel 5, further enhancing heat exchange. Rectangular fins 7 can also be arranged non-uniformly on both sides of the inlet 3. When non-uniformly arranged, any number of groups can be set according to the number of trapezoidal fins 6 to improve the temperature uniformity of the heat source and reduce thermal stress.
矩形肋片7为若干个且均布于微通道5出口4处。矩形肋片7也可以图2中设置成非均匀分布的。每一竖列矩形肋片7竖向对齐且为一组,矩形肋片7优选设置为三组、五组或者八组,还可以是根据微通道5的长度和散热需求设置(超过八组)的任意组数。There are several rectangular fins 7 uniformly distributed at the exit 4 of the microchannel 5 . The rectangular ribs 7 can also be arranged in a non-uniform distribution as shown in FIG. 2 . Each vertical rectangular fin 7 is vertically aligned and is one group, and the rectangular fins 7 are preferably arranged in three groups, five groups or eight groups, and can also be arranged according to the length of the microchannel 5 and heat dissipation requirements (more than eight groups) any number of groups.
对三种矩形肋片7结构组数不同的热沉进行了数值仿真,发现3种热沉结构的芯片(热源)最高温度Tmax基本一致,但三号结构的压损ΔP=16388Pa,仅为一号结构30782Pa的53.2%,即把压降降低了46.8%,但并未增加芯片(热源)的最高温度,也即未增加热沉的总热阻。因此在使用过程中可以根据使用环境选择合适的矩形肋片7组数来满足散热需求。Numerical simulations were carried out on three types of heat sinks with different numbers of rectangular fin 7 structures, and it was found that the maximum temperature T max of the chip (heat source) of the three heat sink structures was basically the same, but the pressure loss ΔP of the structure No. 3 was 16388Pa, which was only The 53.2% of the No. 1 structure 30782Pa reduces the pressure drop by 46.8%, but does not increase the maximum temperature of the chip (heat source), that is, does not increase the total thermal resistance of the heat sink. Therefore, during use, an appropriate number of 7 sets of rectangular fins can be selected according to the use environment to meet heat dissipation requirements.
表1三种矩形肋片组数不同的热沉结构仿真数据表Table 1 Simulation data table of three heat sink structures with different numbers of rectangular fin groups
本实施例的混合结构微通道热沉可以是贴合式的,也可以是嵌入式。贴合式是指在高导热材料上加工得到混合结构的微通道5,再使用高导热胶将热沉模块的基底1与芯片背面粘贴在一起。嵌入式是指直接在芯片背面的硅板上刻蚀出微通道5和二次流道10,再将盖板2与其密封贴合,芯片背面的硅板直接作为了热沉模块的基底1,再通过冷却介质的流动对芯片进行直接的冷却。The mixed-structure microchannel heat sink in this embodiment can be adhering or embedded. The bonding type refers to processing the microchannel 5 with a mixed structure on a high thermal conductivity material, and then using a high thermal conductivity adhesive to paste the base 1 of the heat sink module and the back of the chip together. Embedded means that the microchannel 5 and the secondary flow channel 10 are directly etched on the silicon plate on the back of the chip, and then the cover plate 2 is sealed and bonded to it. The silicon plate on the back of the chip is directly used as the base 1 of the heat sink module. Then the chip is directly cooled by the flow of the cooling medium.
本实施例的工作过程及原理如下:The working process and principle of the present embodiment are as follows:
冷却介质由盖板2中导入口导入至盖板2中的进口3,进而流至盖板2下方的微通道5中,冷却介质再通过由梯形肋片6和矩形肋片7形成的流道向两侧出口流动,直至由盖板2两端的出口4流出,进而流至导出口,进行冷却介质的更换或者循环使用。其中,盖板2在进口3相邻的两侧各设置一出口4的流道结构缩短了冷却介质在流道中的流动距离,从而大幅减小压损;将原有的长直肋片切割为一个个成排排列的梯形肋片6或者平行四边形肋片,梯形肋片6或者平行四边形肋片之间形成了二次流道10,主流区域的冷却介质可以流入这些二次流道10,从而增强了冷却液体的扰动,增强换热;再在出口4的附近加入矩形肋片7,可以减缓冷却介质的流速,使得更多的冷却介质流入二次流道10中从而进一步增强换热。The cooling medium is introduced from the inlet in the cover plate 2 to the inlet 3 in the cover plate 2, and then flows into the microchannel 5 under the cover plate 2, and then the cooling medium passes through the flow channel formed by the trapezoidal fins 6 and the rectangular fins 7 It flows toward the outlets on both sides until it flows out from the outlets 4 at both ends of the cover plate 2, and then flows to the outlet for replacement or recycling of the cooling medium. Among them, the flow channel structure of the cover plate 2 with an outlet 4 on both sides adjacent to the inlet 3 shortens the flow distance of the cooling medium in the flow channel, thereby greatly reducing the pressure loss; the original long straight fins are cut into The trapezoidal fins 6 or parallelogram fins are arranged in rows one by one, and secondary flow channels 10 are formed between the trapezoidal fins 6 or parallelogram fins, and the cooling medium in the main flow area can flow into these secondary flow channels 10, thereby The turbulence of the cooling liquid is enhanced, and the heat exchange is enhanced; adding rectangular fins 7 near the outlet 4 can slow down the flow velocity of the cooling medium, so that more cooling medium flows into the secondary flow channel 10 to further enhance the heat exchange.
本说明书中应用了具体个例对本发明的原理及实施方式进行了阐述,以上实施例的说明只是用于帮助理解本发明的方法及其核心思想;同时,对于本领域的一般技术人员,依据本发明的思想,在具体实施方式及应用范围上均会有改变之处。综上所述,本说明书内容不应理解为对本发明的限制。In this description, specific examples are used to illustrate the principle and implementation of the present invention. The description of the above embodiments is only used to help understand the method and core idea of the present invention; meanwhile, for those of ordinary skill in the art, according to this The idea of the invention will have changes in the specific implementation and scope of application. In summary, the contents of this specification should not be construed as limiting the present invention.
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CN110572990A (en) * | 2019-09-12 | 2019-12-13 | 北京交通大学 | An impingement cooling corrugated surface composite enhanced heat dissipation device |
CN110707059B (en) * | 2019-09-26 | 2020-12-22 | 上海交通大学 | Multi-dimensional mesh-shaped mixed micro-channel fluid radiator |
CN110662403A (en) * | 2019-10-15 | 2020-01-07 | 北京交通大学 | Jet cooling device for array turbulence column |
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 |
CN115377027B (en) * | 2021-05-20 | 2024-11-26 | 中国科学院理化技术研究所 | A hybrid structure heat sink |
CN113629484B (en) * | 2021-07-01 | 2022-09-16 | 佛山华智新材料有限公司 | Porous heat sink and manufacturing method thereof |
CN113543600A (en) * | 2021-07-21 | 2021-10-22 | 中国石油大学(华东) | An incompletely filled staggered microchannel heat exchanger |
CN113613440A (en) * | 2021-08-17 | 2021-11-05 | 珠海格莱克科技有限公司 | Enhanced heat dissipation device using array heat dissipation fins |
CN115014107B (en) * | 2022-05-26 | 2023-04-07 | 西安交通大学 | Double-effect enhanced heat exchange micro-channel heat sink with airfoil flow distribution ribs |
CN115551303A (en) * | 2022-09-28 | 2022-12-30 | 华中科技大学 | Rib matrix microchannel heat sink with top gap |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN203036603U (en) * | 2013-02-07 | 2013-07-03 | 东北林业大学 | Radiator for light-emitting diode (LED) lighting device |
CN203785330U (en) * | 2013-03-22 | 2014-08-20 | 三菱电机株式会社 | Plate heat exchanger and refrigeration circulation device with plate heat exchanger |
CN206365202U (en) * | 2016-12-12 | 2017-07-28 | 中国航空工业集团公司西安航空计算技术研究所 | A kind of new high power electronic device air cooling equipment |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SG10201408026VA (en) * | 2009-12-02 | 2015-01-29 | Univ Singapore | An enhanced heat sink |
CN102620590B (en) * | 2012-03-30 | 2014-02-12 | 中国科学院工程热物理研究所 | A microchannel heat sink and a performance testing device for the microchannel heat sink |
CN202855726U (en) * | 2012-09-21 | 2013-04-03 | 上海大学 | Prism array microchannel heat radiator three-dimensional stacked package |
CN204012181U (en) * | 2014-07-04 | 2014-12-10 | 成都三鼎日新激光科技有限公司 | Microchannel cooling heat sink in a kind of |
CN104658992A (en) * | 2015-02-13 | 2015-05-27 | 西安电子科技大学 | Novel micro heat sink provided with pin-fin array |
CN106601703B (en) * | 2016-10-27 | 2019-08-02 | 湖北工程学院 | Using the micro-channel heat sink of secondary back refrigerating mode |
CN107731767A (en) * | 2017-10-09 | 2018-02-23 | 上海工程技术大学 | A kind of microchannel heat sink with horizontal direction and vertical direction turbulence structure |
-
2018
- 2018-09-21 CN CN201811106670.6A patent/CN109149325B/en active Active
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN203036603U (en) * | 2013-02-07 | 2013-07-03 | 东北林业大学 | Radiator for light-emitting diode (LED) lighting device |
CN203785330U (en) * | 2013-03-22 | 2014-08-20 | 三菱电机株式会社 | Plate heat exchanger and refrigeration circulation device with plate heat exchanger |
CN206365202U (en) * | 2016-12-12 | 2017-07-28 | 中国航空工业集团公司西安航空计算技术研究所 | A kind of new high power electronic device air cooling equipment |
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