CN1233038C - Microjet array cooling heat sink - Google Patents
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Abstract
Description
技术领域technical field
本发明属于微电子技术领域,涉及一种冷却装置。The invention belongs to the technical field of microelectronics and relates to a cooling device.
背景技术:Background technique:
随着工业技术的不断发展,各种电子产品无不朝着体积小、重量轻、高热流通量的方向发展。因此,对新一代的电子设备而言,传统的冷却器的设计极限与制作技术已无法合乎要求。微冷却器的发展源于解决高速集成电路的散热问题,目前已向各种有重量限制与体积限制的高热流通量领域发展,如航天工业、电子元器件冷却、大功率半导体激光器冷却、化工流程传热等。其主要目的是为了要降低电子设备因过热而发生故障损坏的机率,并同时提高电子设备的性能及可靠性。With the continuous development of industrial technology, all kinds of electronic products are developing in the direction of small size, light weight and high heat flux. Therefore, for the new generation of electronic equipment, the design limit and manufacturing technology of the traditional cooler can no longer meet the requirements. The development of micro-coolers stems from solving the heat dissipation problem of high-speed integrated circuits. At present, it has developed into various high heat flux fields with weight restrictions and volume restrictions, such as aerospace industry, cooling of electronic components, cooling of high-power semiconductor lasers, chemical process heat transfer etc. Its main purpose is to reduce the probability of failure and damage of electronic equipment due to overheating, and at the same time improve the performance and reliability of electronic equipment.
目前国内外正在积极着手研究和已经应用的微冷却器包括:微热交换器、微冷冻机、微通道热沉、微热管均热片及整合式微冷却器等。其中微通道热沉已经被证实是传热性能最佳且最具应用潜力的冷却方式之一。At present, micro-coolers that are being actively researched and applied at home and abroad include: micro-heat exchangers, micro-refrigerators, micro-channel heat sinks, micro-heat pipe heat spreaders, and integrated micro-coolers. Among them, the microchannel heat sink has been proved to be one of the cooling methods with the best heat transfer performance and the most application potential.
目前普遍公认的两种有代表性的微通道冷却热沉是:传统微通道型(Traditional Microchannel Type,TMC)和岐管微通道型(ManifoldMicrochannel Type,MMC)。TMC热沉的特点是入口和出口分别位于被冷却元器件的两端。虽然TMC热沉具有高的冷却能力,但两个设计上的局限限制了它的广泛应用。其一,是由于小尺寸所产生的较大压力降;其二,是热源入口、出口间巨大的温度变化。而MMC热沉具有多条入口、出口通道,以一定间隔交替分布在通道长度方向上。在一个固定的流率下,依据岐管通道的入口/出口数量,流动阻力被相应减小,温度变化幅度被相应减小,总的传热热阻也被相应地减小。因此,与TMC热沉相比,MMC热沉具有很大的优越性。然而,无论是TMC热沉还是MMC热沉,其冷却机理均为通道内流体受迫对流换热。其结果是通道入口处流体温度低、冷却效果好,而出口处流体温度高、冷却效果相对较差,由此导致换热表面温度分布不均。而这一局部区域的温度分布(特别是最高温度)是影响被冷却器件工作特性的关键,也是评价微通道热沉性能优劣的重要指标。Two representative microchannel cooling heat sinks generally recognized at present are: traditional microchannel type (Traditional Microchannel Type, TMC) and manifold microchannel type (Manifold Microchannel Type, MMC). The characteristic of TMC heat sink is that the inlet and outlet are respectively located at both ends of the cooled component. Although the TMC heat sink has high cooling capacity, two design limitations limit its wide application. One is the large pressure drop due to the small size; the other is the huge temperature change between the inlet and outlet of the heat source. The MMC heat sink has multiple inlet and outlet channels, which are alternately distributed in the channel length direction at a certain interval. At a fixed flow rate, according to the number of inlets/outlets of the manifold channel, the flow resistance is correspondingly reduced, the range of temperature variation is correspondingly reduced, and the total heat transfer resistance is also correspondingly reduced. Therefore, compared with TMC heat sinks, MMC heat sinks have great advantages. However, whether it is a TMC heat sink or an MMC heat sink, the cooling mechanism is the forced convection heat transfer of the fluid in the channel. The result is that the fluid temperature at the inlet of the channel is low and the cooling effect is good, while the fluid temperature at the outlet is high and the cooling effect is relatively poor, resulting in uneven temperature distribution of the heat exchange surface. The temperature distribution (especially the highest temperature) in this local area is the key to affect the working characteristics of the cooled device, and it is also an important index to evaluate the performance of the microchannel heat sink.
发明内容:Invention content:
本发明的目的在于提供一种冷却热沉,来克服上述两种微通道冷却热沉的缺点。The object of the present invention is to provide a cooling heat sink to overcome the above-mentioned shortcomings of the two microchannel cooling heat sinks.
一种微射流阵列冷却热沉,其特征在于,如图1所示,包括有依次重叠封装在一起的过流片1,射流入口腔片2,射流喷嘴片3,射流出口腔片4,传热片5;过流片1上开有与外部管路连接的进液口6和出液口7;射流入口腔片2上设有射流入口腔8,在与过流片1上的进液口6和出液口7相对应的位置分别开有进液孔9和出液孔10,射流入口腔8与进液孔9和出液孔10在射流入口腔片上2互相不连通;射流出口腔片4上在与射流入口腔片2的射流入口腔8相对应的位置设有射流出口腔14;射流喷嘴片3上设有与射流入口腔8和设置在射流出口腔片4上的射流出口腔14相通的由孔阵列组成的射流喷嘴11,连通进液孔9和射流入口腔8的进液导流通道12,连通出液孔10和射流出口腔14的出液导流通道13。A kind of cooling heat sink of micro-jet array, it is characterized in that, as shown in Figure 1, comprises flow-through
如图8所示,本发明的射流出口腔片4上在与过流片1上的进液口6和出液口7相对应的位置开有进液孔9和出液孔10,传热片5上在与过流片1上的进液口6和出液口7相对应的位置分别开有进液口6和出液口7。As shown in Figure 8, on the
如图4所示,本发明在射流出口腔片4上采用了开有微通道17的射流出口腔14,微通道17的数量及位置与射流喷嘴11中的孔相对应。As shown in FIG. 4 , the present invention adopts a
本发明提出的微射流阵列冷却热沉基于射流冲击换热理论。射流冲击冷却时,流体法向冲击传热表面,形成很薄的速度和温度边界层,因而具有很高的传热率。同时,采用合理的微射流阵列布置方式,可以极大地提高被冷却表面温度分布的均匀性。因此,微射流阵列冷却热沉是减小电子器件换热表面最高温度、降低温度变化的有效方法。The micro-jet array cooling heat sink proposed by the present invention is based on the theory of jet impingement heat transfer. During jet impingement cooling, the fluid normal impacts the heat transfer surface, forming a very thin velocity and temperature boundary layer, so it has a high heat transfer rate. At the same time, the uniformity of the temperature distribution of the cooled surface can be greatly improved by adopting a reasonable arrangement of micro-jet arrays. Therefore, the micro-fluidic array cooling heat sink is an effective method to reduce the maximum temperature of the heat exchange surface of electronic devices and reduce the temperature change.
如图2所示,将热沉片组合封装后形成微射流阵列冷却热沉15。在热沉内部可形成封闭的流体循环,流体流经顺序为:进液口6、进液孔9、进液导流通道12、射流入口腔8、射流喷嘴11、射流出口腔14、出液导流通道13、出液孔10、出液口7,流体通过射流喷嘴11以较高的速度、垂直喷射在传热片5上,实现了高热流通量传热。As shown in FIG. 2 , the
换热工质可分别选用空气、水、制冷剂等。根据所用工质以及器件最佳工作温度范围,在传热表面上将形成单相流体射流冲击换热、射流冲击相变换热来实现冷却技术要求。The heat exchange medium can be air, water, refrigerant and so on. According to the working fluid used and the optimum operating temperature range of the device, a single-phase fluid jet impingement heat exchange and jet impingement phase exchange heat will be formed on the heat transfer surface to meet the cooling technical requirements.
热沉片可选用无氧铜、硅片、银等材料,总体几何形状尺寸可根据被冷却器件尺寸及总体封装要求确定。The heat sink can be made of oxygen-free copper, silicon wafer, silver and other materials, and the overall geometric shape and size can be determined according to the size of the cooled device and the overall packaging requirements.
射流冲击冷却是一种强烈的对流换热方式,特别是在微细尺度条件下,射流冲击换热具有极高的换热速率。本发明充分利用了微射流冲击换热系数极高这一特点,利用微射流阵列热沉来冷却微电子器件,同时在某些情况下可以实现射流冲击相变换热,利用流体发生相变时的潜热来实现更高的热流密度。Jet impingement cooling is a strong convective heat transfer method, especially in micro-scale conditions, jet impingement heat transfer has a very high heat transfer rate. The present invention makes full use of the characteristic of extremely high micro-jet impact heat transfer coefficient, and uses the micro-jet array heat sink to cool microelectronic devices. latent heat to achieve higher heat flux.
附图说明:Description of drawings:
图1:本发明的具有圆孔阵列射流喷嘴的结构示意图;Fig. 1: the structure schematic diagram of jet nozzle with circular hole array of the present invention;
图中:1、过流片,2、射流入口腔片,3、射流喷嘴片,4、射流出口腔片,5、传热片,6、进液口,7、出液口,8、射流入口腔,9、进液孔,10、出液孔,11、射流喷嘴,12、进液导流通道,13、出液导流通道,14、射流出口腔;In the figure: 1. flow-through sheet, 2. injection-into-mouth sheet, 3. jet-flow nozzle sheet, 4. jet-outlet-mouth sheet, 5. heat-transfer sheet, 6. liquid inlet, 7. liquid outlet, 8. injection Inflow mouth, 9, liquid inlet hole, 10, liquid outlet hole, 11, jet nozzle, 12, liquid inlet diversion channel, 13, liquid outlet diversion channel, 14, jet flow out of oral cavity;
图2:具有图1所示结构的本发明示意图;Fig. 2: the schematic diagram of the present invention having the structure shown in Fig. 1;
图中:15、冷却热沉;In the figure: 15, cooling heat sink;
图3:本发明冷却半导体激光条的示意图;Fig. 3: the schematic diagram of cooling semiconductor laser bar of the present invention;
图中:16、半导体激光条;In the figure: 16, semiconductor laser bar;
图4:本发明的具有圆孔阵列射流喷嘴和微通道的结构示意图;Fig. 4: the structure schematic diagram that has circular hole array jet nozzle and microchannel of the present invention;
图中:17、微通道;In the figure: 17, micro channel;
图5:本发明的具有长方孔阵列射流喷嘴的结构示意图;Fig. 5: the structural representation of jet nozzle with rectangular hole array of the present invention;
图6:具有图5所示结构的本发明示意图;Figure 6: a schematic diagram of the present invention having the structure shown in Figure 5;
图7:本发明冷却大功率半导体激光器阵列的示意图;Fig. 7: the schematic diagram of cooling high-power semiconductor laser array of the present invention;
图中:18、电源正极,19、绝缘层,20、光线,21、入口管,22、出口管,23、密封圈;In the figure: 18, positive pole of power supply, 19, insulating layer, 20, light, 21, inlet pipe, 22, outlet pipe, 23, sealing ring;
图8:射流出口腔片上具有进、出液孔和传热片上具有进、出液口的冷却热沉结构示意图。Figure 8: Schematic diagram of the structure of the cooling heat sink with liquid inlet and outlet holes on the jet outlet and liquid inlet and outlet on the heat transfer sheet.
具体实施方式Detailed ways
实施例1:Example 1:
如图3所示,用微射流阵列热沉冷却半导体激光条16,一种典型半导体激光条16的长度、宽度、厚度的尺寸为10000×1000×115微米3,其中有数个均匀排列的激光发射器,微射流阵列热沉15由图1所示的过流片1、射流入口腔片2、射流喷嘴片3、射流出口腔片4、传热片5依次焊接而成,每片均为长方形,宽度与半导体激光条16的长度相同,半导体激光条16固定在传热片5上,射流喷嘴11由一排直径为70微米的圆孔组成,圆孔的深度为射流喷嘴片3的厚度,为300微米,圆孔的数量和位置与激光条中激光发射器的数量和位置相对应,射流出口腔片4的厚度为200微米,过流片1、射流入口腔片2、传热片5厚度均为300微米。在微射流阵列热沉内部可形成封闭的流体循环,流体流经顺序为:进液口6、进液孔9、进液导流通道12、射流入口腔8、射流喷嘴11、射流出口腔14、出液导流通道13、出液孔10、出液口7。流体通过射流喷嘴11以较高的速度、垂直喷射在传热片5上,将激光发射器产生并传到传热片5上的热量带走,实现了高热流通量传热。As shown in Figure 3, the
实施例2:Example 2:
如图4所示,在射流出口腔片4上的射流出口腔14开有微通道17,微通道17的数量及位置与射流喷嘴11中的圆孔相对应,微通道17的宽度为300-500微米,各片加工完成后,依次焊接在一起,形成微射流冷却热沉,流体在热沉内部流经顺序为:进液口6、进液孔9、进液导流通道12、射流入口腔8、射流喷嘴11、微通道17、射流出口腔14、出液导流通道13、出液孔10、出液口7;当流体进入到射流入口腔8后,首先通过射流喷嘴11以较高的速度、垂直喷射在传热片5上,实现了高热流通量传热,然后流体经微通道17流动到射流出口腔14,实现了与传热面换热,充分利用了射流冲击换热与通道内受迫对流换热组合的冷却方式。As shown in Figure 4, the
实施例3:Example 3:
如图5所示,采用两块厚度为200微米的射流喷嘴片3,射流喷嘴11由一排均匀排列的宽度为40微米、长度为500微米的长方孔组成,射流出口腔片4的厚度为200微米,过流片1、射流入口腔片2、传热片5的厚度均为300微米,如图6所示为具有图5结构的热沉示意图。流体在热沉内部流经顺序为:进液口6、进液孔9、进液导流通道12、射流入口腔8、射流喷嘴11、射流出口腔14、出液导流通道13、出液孔10、出液口7。流体通过射流喷嘴11的长方孔以平面射流方式垂直、高速喷射在传热片5上,实现了对于某些具有狭长的发热区域器件的冷却。As shown in Figure 5, two
实施例4:Example 4:
如图7所示,采用本发明冷却大功率半导体激光器阵列,该阵列由M个发光单元组成,在本实施例中M=4,每个发光单元间涂有绝缘层19;每个发光单元包括:电源正极18、冷却热沉15、及置于它们之间的半导体激光条16和绝缘层19,冷却热沉15同时作为电源负极,半导体激光条16在电场的作用下发出光线20。流体经入口管21分别进入每个冷却热沉15,经出口管22流出;入口管21、出口管22与冷却热沉15之间有橡胶密封圈23密封。As shown in Figure 7, adopt cooling high-power semiconductor laser array of the present invention, this array is made up of M light-emitting units, in the present embodiment M=4, is coated with insulating layer 19 between each light-emitting unit; Each light-emitting unit comprises 1. Power supply positive pole 18, cooling
在本实施例中,最上方的冷却热沉15与图1所示结构相同,即射流出口腔片4、传热片5上无进、出液孔,下方的冷却热沉15的射流出口腔片4、传热片5上分别加工有进、出液孔和进、出液口,如图8所示,这样,冷却流体可以经过同一根入口管分别进入每个热沉,并经同一出口管流出,实现了对大功率半导体激光器阵列的冷却。In this embodiment, the uppermost
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN100461995C (en) * | 2006-11-24 | 2009-02-11 | 北京工业大学 | Array Jet Micro Heat Exchanger |
| US9615482B2 (en) | 2009-12-11 | 2017-04-04 | General Electric Company | Shaped heat sinks to optimize flow |
| US9478479B2 (en) * | 2010-10-26 | 2016-10-25 | General Electric Company | Thermal management system and method |
| 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 |
| 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 |
| 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 |
| 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 |
| 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 |
| GB201808726D0 (en) * | 2018-05-29 | 2018-07-11 | J A Kemp | Jet impingement cooling apparatus and method |
| CN108712852B (en) * | 2018-07-12 | 2019-07-30 | 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 | A heat sink device |
| CN111386011B (en) * | 2020-01-09 | 2021-04-27 | 西安交通大学 | A lateral flow impingement microchannel cold plate and electronic equipment |
| CN111148409B (en) * | 2020-01-09 | 2020-12-15 | 西安交通大学 | A jet microchannel cold plate |
| 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 |
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