CN115060099A - Micro-nano multi-scale structure steam chamber and manufacturing method thereof - Google Patents
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- 238000004519 manufacturing process Methods 0.000 title claims abstract description 24
- 238000001704 evaporation Methods 0.000 claims abstract description 68
- 238000009833 condensation Methods 0.000 claims abstract description 64
- 230000005494 condensation Effects 0.000 claims abstract description 64
- 230000008020 evaporation Effects 0.000 claims abstract description 63
- 239000002086 nanomaterial Substances 0.000 claims abstract description 51
- 238000012546 transfer Methods 0.000 claims abstract description 35
- 238000000034 method Methods 0.000 claims description 17
- 238000009835 boiling Methods 0.000 claims description 11
- 239000000463 material Substances 0.000 claims description 9
- 229910000838 Al alloy Inorganic materials 0.000 claims description 7
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 claims description 5
- 229910000861 Mg alloy Inorganic materials 0.000 claims description 4
- 239000002073 nanorod Substances 0.000 claims description 4
- 238000003486 chemical etching Methods 0.000 claims description 3
- 238000010329 laser etching Methods 0.000 claims description 3
- 238000003801 milling Methods 0.000 claims description 3
- 238000005096 rolling process Methods 0.000 claims description 3
- 238000010892 electric spark Methods 0.000 claims 1
- 238000004049 embossing Methods 0.000 claims 1
- 230000005486 microgravity Effects 0.000 abstract description 6
- 239000000956 alloy Substances 0.000 description 9
- 239000007788 liquid Substances 0.000 description 7
- 229910000553 6063 aluminium alloy Inorganic materials 0.000 description 6
- 238000001027 hydrothermal synthesis Methods 0.000 description 4
- 238000003672 processing method Methods 0.000 description 4
- 238000010992 reflux Methods 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
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- 230000000694 effects Effects 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 230000017525 heat dissipation Effects 0.000 description 2
- 230000002209 hydrophobic effect Effects 0.000 description 2
- 238000004377 microelectronic Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
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- 229910021529 ammonia Inorganic materials 0.000 description 1
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D15/00—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
- F28D15/02—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
- F28D15/04—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes with tubes having a capillary structure
- F28D15/046—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes with tubes having a capillary structure characterised by the material or the construction of the capillary structure
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F21/00—Constructions of heat-exchange apparatus characterised by the selection of particular materials
- F28F21/08—Constructions of heat-exchange apparatus characterised by the selection of particular materials of metal
- F28F21/081—Heat exchange elements made from metals or metal alloys
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F21/00—Constructions of heat-exchange apparatus characterised by the selection of particular materials
- F28F21/08—Constructions of heat-exchange apparatus characterised by the selection of particular materials of metal
- F28F21/081—Heat exchange elements made from metals or metal alloys
- F28F21/084—Heat exchange elements made from metals or metal alloys from aluminium or aluminium alloys
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Abstract
本发明提供一种微纳多尺度结构蒸汽腔及其制造方法,微纳多尺度结构蒸汽腔包括蒸发端、冷凝端和位于所述蒸发端与所述冷凝端之间的多个支承柱,且所述支承柱的两端分别与所述蒸发端和所述冷凝端连接,所述蒸发端和所述冷凝端组成蒸汽腔,所述蒸汽腔内填充有传热工质;其中,所述蒸发端与所述冷凝端靠近的一侧表面具有超亲水微纳多尺度结构,所述冷凝端与所述蒸发端靠近的一侧表面具有超亲水纳米结构。本发明提供的微纳多尺度结构蒸汽腔的冷凝端表面具有超亲水纳米结构,在微重力环境下能够依靠超亲水纳米结构强大的毛细芯吸作用实现冷凝后的传热工质高效回流,且多支承柱设计方案能够在高压环境下提供可靠的承载力。
The present invention provides a micro-nano multi-scale structure steam chamber and a manufacturing method thereof. The micro-nano multi-scale structure steam chamber comprises an evaporation end, a condensation end and a plurality of support columns located between the evaporation end and the condensation end, and Two ends of the support column are respectively connected with the evaporation end and the condensation end, the evaporation end and the condensation end form a steam cavity, and the steam cavity is filled with a heat transfer medium; wherein, the evaporation end and the condensation end The surface of the side of the end close to the condensation end has a super-hydrophilic micro-nano multi-scale structure, and the surface of the side of the condensation end close to the evaporation end has a super-hydrophilic nanostructure. The surface of the condensation end of the micro-nano multi-scale structure steam cavity provided by the invention has a super-hydrophilic nano-structure, and in a microgravity environment, the condensed heat transfer working medium can be efficiently refluxed by relying on the strong capillary wicking action of the super-hydrophilic nano-structure , and the multi-support column design scheme can provide reliable bearing capacity under high pressure environment.
Description
技术领域technical field
本发明涉及传热技术领域,具体而言,涉及一种微纳多尺度结构蒸汽腔及其制造方法。The invention relates to the technical field of heat transfer, in particular to a micro-nano multi-scale structure steam cavity and a manufacturing method thereof.
背景技术Background technique
随着微电子设备、雷达、激光武器和核动力装置等高端装备的不断向高集成度、高功率方向发展,装备功率从目前的千瓦级逐步向万瓦级发展,且未来甚至可达到兆瓦级。如果其功率热源产生的瞬时高密度热流不能被及时排散,则极易造成设备故障或失效。蒸汽腔能够利用蒸发/沸腾、冷凝双相变提供的巨大潜热来实现高热流密度的有效疏散,目前蒸汽腔已被应用至芯片散热、集成微电子设备等领域。With the continuous development of high-end equipment such as microelectronic equipment, radar, laser weapons and nuclear power plants towards high integration and high power, the power of equipment has gradually developed from the current kilowatt level to 10,000 watts, and may even reach megawatts in the future class. If the instantaneous high-density heat flow generated by its power heat source cannot be dissipated in time, it will easily cause equipment failure or failure. The vapor chamber can utilize the huge latent heat provided by the dual phase transition of evaporation/boiling and condensation to achieve effective evacuation of high heat flux density. At present, the vapor chamber has been applied to the fields of chip heat dissipation and integrated microelectronic devices.
随着我国航天宇航技术的不断发展,空间星载电子元器件、天基武器也同样面临着严峻的散热难题。现有技术中的蒸汽腔大多依靠蒸发端的亲水特性提高沸腾传热极限,依靠冷凝端的疏水特性促进液滴冷凝后再依靠重力作用滴落实现传热增强,且现有技术中的蒸汽腔不需要考虑腔内较高的蒸汽压,其支撑结构相对简单。但是,空间中微重力环境和极冷极热现象,使得疏水性冷凝面无法实现有效的工质回流,且腔内的高压环境需要可靠的支撑结构。With the continuous development of my country's aerospace technology, space-borne electronic components and space-based weapons are also facing severe heat dissipation problems. Most of the steam chambers in the prior art rely on the hydrophilic properties of the evaporating end to improve the limit of boiling heat transfer, and rely on the hydrophobic properties of the condensation end to promote the condensation of droplets and then rely on gravity to drop to achieve enhanced heat transfer. The higher vapor pressure in the cavity needs to be considered, and its support structure is relatively simple. However, due to the microgravity environment and extremely cold and extremely hot phenomena in the space, the hydrophobic condensing surface cannot achieve effective working fluid backflow, and the high-pressure environment in the cavity requires a reliable support structure.
发明内容SUMMARY OF THE INVENTION
本发明解决的问题是提供一种能够应用于空间装置散热,且能够提供可靠支撑的蒸汽腔。The problem to be solved by the present invention is to provide a steam chamber that can be applied to a space device to dissipate heat and can provide reliable support.
为解决上述问题中的至少一方面,本发明提供一种微纳多尺度结构蒸汽腔,包括蒸发端、冷凝端和位于所述蒸发端与所述冷凝端之间的多个支承柱,且所述支承柱的两端分别与所述蒸发端和所述冷凝端连接,所述蒸发端和所述冷凝端组成蒸汽腔,所述蒸汽腔内填充有传热工质;其中,所述蒸发端与所述冷凝端靠近的一侧表面具有超亲水微纳多尺度结构,所述冷凝端与所述蒸发端靠近的一侧表面具有超亲水纳米结构。In order to solve at least one aspect of the above problems, the present invention provides a micro-nano multi-scale structure steam chamber, comprising an evaporation end, a condensation end and a plurality of support columns located between the evaporation end and the condensation end, and the Two ends of the support column are respectively connected with the evaporation end and the condensation end, the evaporation end and the condensation end form a steam chamber, and the steam chamber is filled with a heat transfer medium; wherein, the evaporation end The surface of the side close to the condensation end has a super-hydrophilic micro-nano multi-scale structure, and the surface of the side of the condensation end close to the evaporation end has a super-hydrophilic nanostructure.
优选地,所述超亲水微纳多尺度结构包括微结构和位于所述微结构表面的超亲水纳米结构;其中,所述微结构包括微通道、微柱和微孔,所述微结构的尺寸为几十微米至几毫米,所述超亲水纳米结构包括纳米柱、纳米孔和纳米棒,所述超亲水纳米结构的尺寸为几至几百纳米。Preferably, the super-hydrophilic micro-nano multi-scale structure includes a micro-structure and a super-hydrophilic nano-structure located on the surface of the micro-structure; wherein the micro-structure includes micro-channels, micro-pillars and micro-pores, and the micro-structure The size of the superhydrophilic nanostructure is from several tens of micrometers to several millimeters, and the superhydrophilic nanostructure includes nanopillars, nanopores and nanorods, and the size of the superhydrophilic nanostructure is several to several hundreds of nanometers.
优选地,所述微结构为金字塔阵列微结构,所述金字塔阵列微结构的特征尺寸为100μm,周期为1mm。Preferably, the microstructure is a pyramid array microstructure, and the feature size of the pyramid array microstructure is 100 μm and the period is 1 mm.
优选地,所述支承柱表面具有超亲水纳米结构。Preferably, the surface of the support column has superhydrophilic nanostructures.
优选地,所述蒸汽腔的面积为100cm2~1m2,所述支承柱的边长或直径为2.5-3.5mm,两个所述支承柱之间的间距为6-10mm,所述蒸发端和所述冷凝端的厚度为1-2mm,所述蒸发端与所述冷凝端的距离为0.5-2.5mm,且所述蒸汽腔的总体厚度小于或等于5mm。Preferably, the area of the steam chamber is 100cm 2 to 1m 2 , the side length or diameter of the support column is 2.5-3.5mm, the distance between the two support columns is 6-10mm, and the evaporation end And the thickness of the condensation end is 1-2mm, the distance between the evaporation end and the condensation end is 0.5-2.5mm, and the overall thickness of the steam chamber is less than or equal to 5mm.
优选地,所述传热工质为液氨。Preferably, the heat transfer working medium is liquid ammonia.
优选地,所述蒸发端、所述冷凝端和所述支承柱的材质包括铝合金或镁合金。Preferably, the materials of the evaporation end, the condensation end and the support column include aluminum alloy or magnesium alloy.
本发明通过在蒸发端和冷凝端之间设置多个支承柱,支承柱的两端分别与蒸发端和冷凝端连接,增强蒸汽腔在空间环境中高压承载的能力;对于微重力的空间环境,蒸发端表面具有超亲水微纳多尺度结构,其中微纳多尺度结构能够提高更多气泡活性成核位点,而超亲水性则能够实现受热干涸区液体的快速补充,另外还可提供液体输送通道,从而实现传热系数和沸腾传热极限的协同增强,在蒸发端受热蒸发后的传热工质被输送至冷凝端,由于冷凝端表面具有超亲水纳米结构,使被蒸发的传热工质在超亲水纳米结构上冷凝,并能够依靠超亲水纳米结构强大的毛细芯吸作用实现冷凝后的传热工质高效回流的目的,因此能够在微重力的空间环境下实现高效传热;本发明提供的微纳多尺度结构蒸汽腔能够保证蒸汽腔在微重力和存在极冷极热现象的空间环境中实现有效的工质回流,且能够在高压环境下提供可靠的承载力。In the present invention, a plurality of support columns are arranged between the evaporation end and the condensation end, and the two ends of the support columns are respectively connected with the evaporation end and the condensation end, so as to enhance the high-pressure bearing capacity of the steam chamber in the space environment; for the microgravity space environment, The surface of the evaporation end has a super-hydrophilic micro-nano multi-scale structure, in which the micro-nano multi-scale structure can increase more active nucleation sites for bubbles, while the super-hydrophilicity can realize the rapid replenishment of the liquid in the heat-drying area, and can also provide Liquid transport channel, so as to achieve synergistic enhancement of heat transfer coefficient and boiling heat transfer limit. The heat transfer working medium after being heated and evaporated at the evaporation end is transported to the condensation end. Because the surface of the condensation end has super hydrophilic nanostructures, the evaporated The heat transfer working medium is condensed on the superhydrophilic nanostructure, and can rely on the strong capillary wicking effect of the superhydrophilic nanostructure to achieve the purpose of efficient reflux of the condensed heat transfer working medium, so it can be realized in a microgravity space environment. Efficient heat transfer; the micro-nano multi-scale structure steam chamber provided by the present invention can ensure that the steam chamber can achieve effective working fluid backflow in microgravity and a space environment with extremely cold and extremely hot phenomena, and can provide reliable bearing in a high-pressure environment force.
本发明的另一实施例提供一种上述的微纳多尺度结构蒸汽腔的制造方法,通过微结构制造方法在沸腾传热材料表面制得微结构,再通过超亲水纳米结构制造方法在所述微结构基础上制得超亲水纳米结构,得到蒸发端,所述蒸发端表面具有超亲水微纳多尺度结构;通过所述超亲水纳米结构制造方法直接在沸腾传热材料表面制得超亲水纳米结构,得到冷凝端,所述冷凝端表面具有超亲水纳米结构。Another embodiment of the present invention provides a method for fabricating the above-mentioned micro-nano multi-scale structure steam cavity. The micro-structure is fabricated on the surface of the boiling heat transfer material by the micro-structure fabrication method, and then the super-hydrophilic nano-structure fabrication method is used in the above-mentioned fabrication method. On the basis of the microstructure described above, a superhydrophilic nanostructure is obtained, and an evaporation end is obtained, and the surface of the evaporation end has a superhydrophilic micro-nano multiscale structure; the superhydrophilic nanostructure is directly prepared on the surface of the boiling heat transfer material by the superhydrophilic nanostructure manufacturing method. A superhydrophilic nanostructure is obtained, and a condensation end is obtained, and the surface of the condensation end has a superhydrophilic nanostructure.
优选地,所述微结构制造方法包括微压印、滚压、微铣削或微细电火花。Preferably, the microstructure fabrication method includes micro-imprinting, rolling, micro-milling or micro-electric sparking.
优选地,所述超亲水纳米结构制造方法包括激光刻蚀、化学腐蚀或电化学处理。Preferably, the superhydrophilic nanostructure fabrication method includes laser etching, chemical etching or electrochemical treatment.
本发明提供的微纳多尺度结构蒸汽腔的制造方法与现有技术相比具有的有益效果,与微纳多尺度结构蒸汽腔相同,在此不再赘述。Compared with the prior art, the manufacturing method of the micro-nano multi-scale structure steam cavity provided by the present invention has the same beneficial effects as the micro-nano multi-scale structure steam cavity, which will not be repeated here.
附图说明Description of drawings
图1为本发明实施例中微纳多尺度结构蒸汽腔的结构示意图;FIG. 1 is a schematic structural diagram of a micro-nano multi-scale structure steam chamber in an embodiment of the present invention;
图2为本发明实施例中不同蒸汽腔结构的润湿性分析图;Fig. 2 is the wettability analysis diagram of different steam chamber structures in the embodiment of the present invention;
图3为本发明实施例中蒸汽腔承载分析图。FIG. 3 is an analysis diagram of the steam chamber load in the embodiment of the present invention.
附图标记说明:Description of reference numbers:
1、蒸发端;2、冷凝端;3、支承柱;4、传热工质。1. Evaporating end; 2. Condensing end; 3. Supporting column; 4. Heat transfer medium.
具体实施方式Detailed ways
为使本发明的上述目的、特征和优点能够更为明显易懂,下面对本发明的具体实施例做详细的说明。In order to make the above objects, features and advantages of the present invention more clearly understood, specific embodiments of the present invention will be described in detail below.
需要说明的是,在不冲突的情况下,本发明中的实施例中的特征可以相互组合。术语“包含”、“包括”、“含有”、“具有”的含义是非限制性的,即可加入不影响结果的其它步骤和其它成分。以上术语涵盖术语“由……组成”和“基本上由……组成”。如无特殊说明的,材料、设备、试剂均为市售。另外,需要说明的是,图中空心箭头所示方向为热蒸汽路径,实心箭头所示方形为传热工质回流路径。It should be noted that the features in the embodiments of the present invention may be combined with each other without conflict. The meanings of the terms "comprising", "including", "containing", "having" are non-limiting, that is, other steps and other ingredients may be added that do not affect the result. The above terms cover the terms "consisting of" and "consisting essentially of". Unless otherwise specified, materials, equipment and reagents are all commercially available. In addition, it should be noted that the direction indicated by the hollow arrow in the figure is the hot steam path, and the square indicated by the solid arrow is the heat transfer working medium return path.
本发明实施例提供一种微纳多尺度结构蒸汽腔,包括蒸发端1、冷凝端2和位于所述蒸发端1与所述冷凝端2之间的多个支承柱3,且所述支承柱3的两端分别与所述蒸发端1和所述冷凝端2连接,所述蒸发端1和所述冷凝端2组成蒸汽腔,所述蒸汽腔内填充有传热工质4;其中,所述蒸发端1与所述冷凝端2靠近的一侧表面具有超亲水微纳多尺度结构,所述冷凝端2与所述蒸发端1靠近的一侧表面具有超亲水纳米结构。The embodiment of the present invention provides a micro-nano multi-scale structure steam chamber, including an evaporation end 1, a
其中,所述蒸发端1表面的所述超亲水微纳多尺度结构包括微结构和位于所述微结构表面的超亲水纳米结构;其中,所述微结构包括微通道、微柱和微孔,所述微结构的尺寸为几十微米至几毫米,例如10微米至10毫米,所述超亲水纳米结构包括纳米柱、纳米孔和纳米棒,所述超亲水纳米结构的尺寸为几至几百纳米,例如1纳米至1000纳米。Wherein, the super-hydrophilic micro-nano multi-scale structure on the surface of the evaporation end 1 includes a microstructure and a super-hydrophilic nanostructure on the surface of the microstructure; wherein, the microstructure includes microchannels, micropillars and microstructures Pores, the size of the microstructures is tens of micrometers to several millimeters, such as 10 micrometers to 10 millimeters, the superhydrophilic nanostructures include nanopillars, nanopores and nanorods, and the size of the superhydrophilic nanostructures is A few to several hundred nanometers, such as 1 nanometer to 1000 nanometers.
示例性地,所述微结构为金字塔阵列微结构,所述金字塔阵列微结构的特征尺寸为100μm,周期为1mm。Exemplarily, the microstructure is a pyramid array microstructure, and the feature size of the pyramid array microstructure is 100 μm and the period is 1 mm.
所述超亲水微纳多尺度结构中的微纳多尺度结构能够为更多气泡提供活性成核位点,由于其具有超亲水性,从而能够实现受热干涸区域液体的快速补充,另外,所述超亲水微纳多尺度结构中的微结构还能够提供液体输送通道,当所述蒸发端1受热时,尤其是在高热流密度下,能够通过所述蒸发端1表面的超亲水微纳多尺度结构实现传热系数和沸腾传热极限的协同增强。The micro-nano multi-scale structure in the super-hydrophilic micro-nano multi-scale structure can provide active nucleation sites for more bubbles, and because of its super-hydrophilicity, it can realize rapid replenishment of liquid in the heat-dried area. In addition, The microstructure in the superhydrophilic micro-nano multiscale structure can also provide a liquid transport channel, when the evaporation end 1 is heated, especially under high heat flux density, it can pass through the superhydrophilic surface of the evaporation end 1. The micro-nano multi-scale structure achieves synergistic enhancement of heat transfer coefficient and boiling heat transfer limit.
所述冷凝端2表面的所述超亲水纳米结构包括纳米柱、纳米孔和纳米棒,所述超亲水纳米结构的尺寸为几至几百纳米,例如1纳米至1000纳米。The superhydrophilic nanostructures on the surface of the
所述蒸发端1与所述冷凝端2靠近的一侧表面具有超亲水微纳多尺度结构,所述冷凝端2与所述蒸发端1靠近的一侧表面具有超亲水纳米结构;即,所述蒸发端1的所述超亲水微纳多尺度结构与所述冷凝端2表面的所述超亲水纳米结构均位于所述蒸汽腔内部。The surface of the side close to the evaporation end 1 and the
另外,所述支承柱3表面具有超亲水纳米结构。通过在所述支承柱3表面设置超亲水纳米结构能够提高冷凝回流的效率,传热工质4在所述冷凝端2具有超亲水纳米结构的表面上冷凝后,能够通过所述支承柱3上的超亲水纳米结构快速回流至所述蒸发端1表面。In addition, the surface of the support column 3 has a super-hydrophilic nanostructure. By arranging superhydrophilic nanostructures on the surface of the support column 3, the efficiency of condensation and reflux can be improved. The superhydrophilic nanostructures on 3 quickly reflow to the surface of the evaporation end 1.
具体地,所述蒸汽腔的面积为100cm2~1m2,所述支承柱3的边长或直径为2.5-3.5mm,两个所述支承柱3之间的间距为6-10mm,所述蒸发端1和所述冷凝端2的厚度为1-2mm,所述蒸发端1与所述冷凝端2的距离为0.5-2.5mm,且所述蒸汽腔的总体厚度小于或等于5mm。为了能够应用于空间环境中,所述蒸汽腔具有较大的面积,面积为100cm2~1m2;由于传热工质4在高热流密度下能够产生蒸汽压,当传热工质4为液氨时,蒸汽压最高可达到5.6MPa,所述支承柱3可以为方柱形或者圆柱形,其边长或直径为2.5-3.5mm,且两个所述支承柱3之间的间距为6-10mm,从而能够为所述蒸汽腔提供足够的承载力,避免所述蒸汽腔高压形变失效。Specifically, the area of the steam chamber is 100cm 2 to 1m 2 , the side length or diameter of the support column 3 is 2.5-3.5mm, and the distance between the two support columns 3 is 6-10mm. The thickness of the evaporation end 1 and the
所述蒸汽腔中的传热工质4优选为液氨,液氨与所述蒸汽腔的相容性好,相变潜热大,且蒸汽密度低。The heat transfer working medium 4 in the steam chamber is preferably liquid ammonia, which has good compatibility with the steam chamber, large latent heat of phase change, and low steam density.
由于本发明实施例提供的蒸汽腔应用于空间环境,因此所述蒸发端1、所述冷凝端2和所述支承柱3均采用低密度轻量化材料,如铝合金或镁合金。Since the steam chamber provided in the embodiment of the present invention is applied to a space environment, the evaporation end 1 , the
当蒸汽腔工作时,蒸发端1受热,传热工质4被蒸发生成热蒸汽,由于蒸发端1表面具有超亲水微纳多尺度结构,能够实现传热系数和沸腾传热极限的协同增强,且能够实现受热干涸区域液体的快速补充,热蒸汽蒸发至冷凝端2后,通过冷凝端2的冷凝再次转换为液态的传热工质4,并通过冷凝端2表面的超亲水纳米结构具有的强大的毛细芯吸作用实现冷凝后的传热工质4高效回流,且支承柱3表面的超亲水纳米结构能够进一步提高传热工质4的回流效率,从而实现在微重力的空间环境下能够稳定运行,支承柱3则保证了蒸汽腔在工作时具有良好的承载能力。When the steam chamber is working, the evaporation end 1 is heated, and the heat transfer working medium 4 is evaporated to generate hot steam. Since the surface of the evaporation end 1 has a super-hydrophilic micro-nano multi-scale structure, the synergistic enhancement of the heat transfer coefficient and the boiling heat transfer limit can be achieved. , and can realize the rapid replenishment of the liquid in the heated and dry area. After the hot steam evaporates to the
本发明的另一实施例提供一种上述的微纳多尺度结构蒸汽腔的制造方法,通过微结构制造方法在沸腾传热材料表面制得微结构,再通过超亲水纳米结构制造方法在所述微结构基础上制得超亲水纳米结构,得到蒸发端1,所述蒸发端1表面具有超亲水微纳多尺度结构;通过所述超亲水纳米结构制造方法直接在沸腾传热材料表面制得超亲水纳米结构,得到冷凝端2,所述冷凝端2表面具有超亲水纳米结构。Another embodiment of the present invention provides a method for fabricating the above-mentioned micro-nano multi-scale structure steam cavity. The micro-structure is fabricated on the surface of the boiling heat transfer material by the micro-structure fabrication method, and then the super-hydrophilic nano-structure fabrication method is used in the above-mentioned fabrication method. On the basis of the microstructure, a superhydrophilic nanostructure is obtained to obtain an evaporation end 1, and the surface of the evaporation end 1 has a superhydrophilic micro-nano multiscale structure; the superhydrophilic nanostructure manufacturing method is directly used in the boiling heat transfer material. A superhydrophilic nanostructure is prepared on the surface, and a
其中,所述微结构制造方法包括微压印、滚压、微铣削或微细电火花,所述超亲水纳米结构制造方法包括激光刻蚀、化学腐蚀或电化学处理。Wherein, the microstructure manufacturing method includes micro-imprinting, rolling, micro-milling or micro-electric sparking, and the super-hydrophilic nanostructure manufacturing method includes laser etching, chemical etching or electrochemical treatment.
示例性地,先采用微压印方法在铝合金材料表面制得微结构,微压印参数为:压印温度350℃,成形压力156MPa,压印速度0.005mm/s,保压时间300s,再通过高压水热法对具有微结构的铝合金材料进行处理,高压水热法的参数为:温度200℃,压力1.56MPa,处理时间120min,得到蒸发端1,蒸发端1的表面具有超亲水微纳多尺度结构;直接采用纳秒脉冲激光加工方法在铝合金材料表面制得超亲水纳米结构,得到冷凝端2,其中,纳米脉冲激光加工方法参数为:激光功率80W,扫描速度100mm/s,脉冲频率10kHz,填充间距50μm。Exemplarily, a micro-imprinting method is used to obtain a microstructure on the surface of an aluminum alloy material. The micro-imprinting parameters are: an imprinting temperature of 350° C., a forming pressure of 156 MPa, an imprinting speed of 0.005 mm/s, a pressure holding time of 300 s, and then a pressure of 156 MPa. The aluminum alloy material with microstructure is processed by high-pressure hydrothermal method. The parameters of high-pressure hydrothermal method are: temperature 200℃, pressure 1.56MPa, treatment time 120min, and the evaporation end 1 is obtained, and the surface of the evaporation end 1 has super hydrophilic properties. Micro-nano multi-scale structure; the super-hydrophilic nanostructure is directly obtained on the surface of the aluminum alloy material by the nanosecond pulse laser processing method, and the
下面结合具体实施例,进一步阐述本发明。应理解,这些实施例仅用于说明本发明而不用于限制本发明的范围。下列实施例中未注明具体条件的实验方法,通常按照制造厂商所建议的条件。The present invention will be further described below in conjunction with specific embodiments. It should be understood that these examples are only used to illustrate the present invention and not to limit the scope of the present invention. In the following examples, the experimental methods without specific conditions are generally in accordance with the conditions suggested by the manufacturer.
实施例Example
1.1、先采用微压印方法在6063铝合金材料表面制得微结构,微压印参数为:压印温度350℃,成形压力156MPa,压印速度0.005mm/s,保压时间300s,再通过高压水热法对具有微结构的6063铝合金材料进行处理,高压水热法的参数为:温度200℃,压力1.56MPa,处理时间120min,得到蒸发端,蒸发端的表面具有超亲水微纳多尺度结构;1.1. First, the microstructure was obtained on the surface of 6063 aluminum alloy material by micro-imprinting method. The micro-imprinting parameters were: imprinting temperature 350℃, forming pressure 156MPa, imprinting speed 0.005mm/s, holding time 300s, and then passed The 6063 aluminum alloy material with microstructure is treated by high pressure hydrothermal method. The parameters of high pressure hydrothermal method are: temperature 200℃, pressure 1.56MPa, treatment time 120min, and the evaporation end is obtained, and the surface of the evaporation end has super-hydrophilic micro-nano poly scale structure;
1.2、直接采用纳秒脉冲激光加工方法在6063铝合金材料表面制得超亲水纳米结构,得到冷凝端,其中,纳米脉冲激光加工方法参数为:激光功率80W,扫描速度100mm/s,脉冲频率10kHz,填充间距50μm;1.2. The super-hydrophilic nanostructure is directly obtained on the surface of 6063 aluminum alloy material by nanosecond pulse laser processing method, and the condensation end is obtained. The parameters of nano pulse laser processing method are: laser power 80W, scanning speed 100mm/s, pulse frequency 10kHz, fill spacing 50μm;
1.3、将蒸发端和冷凝端组装成蒸汽腔,在蒸汽腔中采用多个支承柱连接蒸发端和冷凝端,制得面积为100cm2的蒸汽腔,蒸汽腔的高度为1.5mm,其中,蒸发端和冷凝端的厚度均为1.6mm,支承柱为圆柱形,直径为3mm,两个支承柱之间的间距为7mm,蒸发端上的微结构为金字塔阵列微结构,特征尺寸为100μm,周期为1mm。1.3. Assemble the evaporating end and the condensing end into a steam chamber, and use a plurality of supporting columns to connect the evaporating end and the condensing end in the steam chamber to obtain a steam chamber with an area of 100 cm 2 , and the height of the steam chamber is 1.5 mm, wherein the evaporation The thickness of the end and the condensation end are both 1.6mm, the support column is cylindrical with a diameter of 3mm, the spacing between the two support columns is 7mm, the microstructure on the evaporation end is a pyramid array microstructure, the feature size is 100μm, and the period is 1mm.
实验例1Experimental example 1
分别对在初始6063铝合金材料、实施例中的蒸发端和实施例中的冷凝端表面滴加5μL的纯水,测量水的接触角,对润湿性进行测试。结果如图2所示:5 μL of pure water was dropped on the surface of the initial 6063 aluminum alloy material, the evaporation end in the example, and the condensation end in the example, respectively, to measure the contact angle of water, and to test the wettability. The result is shown in Figure 2:
图2中(a)为6063铝合金材料表面的润湿性结果,图2中(b)为实施例中蒸发端表面的润湿性结果,图2中(c)为实施例中冷凝端表面的润湿性结果,可以看出,在6063铝合金材料表面的水具有一定接触角,而在实施例中蒸发端和冷凝端的纯水则能够完全铺平,接触角为0,说明本发明实施例制得的蒸发端和冷凝端具有超亲水性。Fig. 2(a) is the wettability result of the surface of the 6063 aluminum alloy material, Fig. 2(b) is the wettability result of the evaporation end surface in the embodiment, and Fig. 2(c) is the condensation end surface in the embodiment It can be seen that the water on the surface of the 6063 aluminum alloy material has a certain contact angle, while in the example, the pure water at the evaporation end and the condensation end can be completely flattened, and the contact angle is 0, indicating the implementation of the present invention. The evaporating end and the condensing end prepared in this example are superhydrophilic.
实验例2Experimental example 2
对实施例中蒸汽腔的应力进行模拟分析,由于蒸汽腔承压模型为轴对称模型,所以对实施例中蒸汽腔的1/4模型进行数值模拟验证,设置腔内的压力为5.6MPa。结果如图3所示:The stress of the steam chamber in the embodiment is simulated and analyzed. Since the pressure bearing model of the steam chamber is an axisymmetric model, the 1/4 model of the steam chamber in the embodiment is numerically simulated and verified, and the pressure in the chamber is set to 5.6MPa. The result is shown in Figure 3:
其中图3中(a)为蒸汽腔整体Mises应力分布情况,图3中(b)为蒸发端的微结构以及支承柱局部Mises应力分布情况,其中蒸汽腔的整体最大Mises应力为52.9MPa,微结构剂支承柱局部的最大Mises应力为62.1MPa,均小于铝合金和镁合金等材料的屈服强度,能够满足空间环境的承载需要,保证在腔内压力为5.6MPa时,蒸汽腔的任何位置均不存在塑性变形。Among them, Figure 3(a) is the overall Mises stress distribution of the steam chamber, and Figure 3(b) is the microstructure of the evaporation end and the local Mises stress distribution of the support column. The overall maximum Mises stress of the steam chamber is 52.9MPa, and the microstructure The local maximum Mises stress of the agent support column is 62.1 MPa, which is smaller than the yield strength of aluminum alloy and magnesium alloy and other materials, which can meet the bearing requirements of the space environment, and ensure that when the pressure in the cavity is 5.6 MPa, any position of the steam chamber will not be damaged. There is plastic deformation.
虽然本公开披露如上,但本公开的保护范围并非仅限于此。本领域技术人员在不脱离本公开的精神和范围的前提下,可进行各种变更与修改,这些变更与修改均将落入本发明的保护范围。Although the present disclosure is disclosed above, the scope of protection of the present disclosure is not limited thereto. Those skilled in the art can make various changes and modifications without departing from the spirit and scope of the present disclosure, and these changes and modifications will fall within the protection scope of the present invention.
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