WO2024036611A1 - Gecko-claw-imitating composite thermal interface material and preparation method therefor - Google Patents

Gecko-claw-imitating composite thermal interface material and preparation method therefor Download PDF

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WO2024036611A1
WO2024036611A1 PCT/CN2022/113646 CN2022113646W WO2024036611A1 WO 2024036611 A1 WO2024036611 A1 WO 2024036611A1 CN 2022113646 W CN2022113646 W CN 2022113646W WO 2024036611 A1 WO2024036611 A1 WO 2024036611A1
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preparation
thermal interface
interface material
micron
polymer
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Chinese (zh)
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叶振强
曾小亮
么依民
许建斌
孙蓉
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中国科学院深圳先进技术研究院
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    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K3/00Use of inorganic substances as compounding ingredients
    • C08K3/02Elements
    • C08K3/04Carbon
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F21/00Constructions of heat-exchange apparatus characterised by the selection of particular materials
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L23/00Details of semiconductor or other solid state devices
    • H01L23/34Arrangements for cooling, heating, ventilating or temperature compensation ; Temperature sensing arrangements
    • H01L23/36Selection of materials, or shaping, to facilitate cooling or heating, e.g. heatsinks
    • H01L23/373Cooling facilitated by selection of materials for the device or materials for thermal expansion adaptation, e.g. carbon

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  • the invention relates to the technical field of manufacturing non-metallic functional materials for electronic components, and in particular to a composite thermal interface material imitating gecko claws and a preparation method thereof.
  • thermal interface materials have emerged.
  • polymer-based thermal interface material which accounts for nearly 90% of all thermal interface material products [1] .
  • Polymer-based thermal interface materials are composed of polymer matrix and high thermal conductivity fillers (such as metals [2] , ceramics [3] , carbon-based materials [4] , etc.).
  • Thermal conductive fillers such as graphene, boron nitride, aluminum powder, etc., although have high thermal conductivity, are relatively hard and are not conducive to bonding with the device interface.
  • the filler content has to be increased. This will inevitably affect the mechanical properties of the thermal interface material, and further affect the contact between the thermal interface material itself and the device interface. Thermal interface materials with poor mechanical properties will not only not reduce the interface thermal resistance, but also introduce additional interface thermal resistance. Therefore, it is crucial to develop methods to reduce the interface thermal resistance of thermal interface materials.
  • the method of reducing interface thermal resistance can be based on both a physical and chemical perspective. Chemical methods use chemical reactions to reduce interface thermal resistance, and the conditions for implementation are relatively harsh. The physical method improves interface contact by optimizing the surface structure, and the use conditions are simpler. Prasher [5] studied the effect of surface roughness on interface contact thermal resistance. Several groups of copper substrates with different roughness were used as contact surfaces, and thermal conductive silicone grease and phase change composite materials were used as thermal interface materials to measure the interface heat of different combinations. It is found that as the roughness increases, the contact area between the device and the thermal interface material increases, thereby reducing the contact thermal resistance. The method used is relatively simple and is suitable for device interfaces that have a certain roughness.
  • the roughness of the thermal interface material needs to match the roughness of the device interface to be effective.
  • the biological world can always bring inspiration.
  • the gecko has become the darling of the bionics community because of its ability to fly over walls and fly over walls [6] .
  • gecko feet have dense, high-aspect-ratio, arrays of micron-sized bristles.
  • the bristles are made of flexible material and have numerous nano-sized hairs at their ends.
  • this micro-nano multi-level structure increases the contact area between the interfaces in a disguised manner, doubling the van der Waals force on the contact surface, thus forming a strong adhesion force [6] .
  • the imitation gecko claw structure can effectively enhance the interaction of the contact surface, but it is rarely applied to thermal interface materials.
  • the main reason is that the current research on imitation gecko claws mainly focuses on adhesive materials, and some problems need to be overcome when transferring to thermally conductive materials.
  • Thermal interface materials are usually composite materials composed of highly thermally conductive fillers and matrices. The materials are uneven and it is more difficult to prepare micron double-layer structures.
  • carbon nanotubes are prepared by chemical vapor deposition, they cannot grow directly on the surface of the thermal interface material. Even if the micron-scale array structure is first etched on the surface of the thermal interface material, it is difficult to transfer the carbon nanotube array to the micron-scale structure.
  • the present invention provides a composite thermal interface material imitating a gecko claw and a preparation method thereof, which reduces the thermal contact resistance between the thermal interface material itself and the device interface.
  • the present invention provides a method for preparing a composite thermal interface material imitating gecko claws, which includes the following steps:
  • the density of the carbon nanotubes implanted is 30 to 100 mg/cm 2 .
  • the micron-scale array structure includes a plurality of micron-scale columnar holes; the hole depth H of the columnar holes is 20 microns to 40 microns, and the hole diameter D of the columnar holes is 20 to 30 microns, and the center distance L between adjacent holes of the plurality of micron-sized columnar holes is 40 to 90 microns.
  • the template with a micron-scale array structure on its surface is a silicon substrate
  • the micron-scale array structure is etched by photolithography technology
  • it also includes pre-treatment of coating the template with a hydrophobic film
  • the hydrophobic film is a polytetrafluoroethylene film, and the thickness is preferably 100 to 200 nanometers;
  • the polytetrafluoroethylene film is plated on the surface of the template using plasma enhanced chemical vapor deposition (PECVD).
  • PECVD plasma enhanced chemical vapor deposition
  • the components of the polymer-based thermal interface material prepolymer include a polymer matrix and fillers
  • the polymer matrix is not particularly limited. Specific examples include epoxy resin, polybutadiene, polyurethane, acrylic resin, polydimethylsiloxane, etc., and is preferably a flexible polymer. Polymers such as polydimethylsiloxane (PDMS);
  • the polymer matrix includes a monomer and a cross-linking agent; the monomer is preferably a vinyl-terminated silicone oil, and the cross-linking agent is preferably a side chain hydrogen-containing silicone oil; the vinyl-terminated silicone oil
  • the mass ratio of the base silicone oil and the side chain hydrogen-containing silicone oil is preferably 1: (0.4 ⁇ 0.8);
  • the type of filler is not particularly limited. Specific examples include aluminum powder, alumina powder, boron nitride, silver powder, graphene, carbon fiber, etc., preferably aluminum powder; There is no special restriction on the amount.
  • Aluminum powder is used as a filler, and its mass fraction accounts for 80wt% to 92wt% of the polymer-based thermal interface material prepolymer.
  • Carbon fiber or graphene is used as a filler, and its mass fraction accounts for 80wt% to 92wt% of the polymer-based thermal interface material prepolymer. 20wt% ⁇ 40wt% of the base thermal interface material prepolymer.
  • the filler is proportioned according to a mass ratio of particle size 1 to 6 microns: particle size 10 to 20 microns (2/8 to 3/7): 1;
  • step (1) the specific steps for preparing the polymer-based thermal interface material prepolymer are: after mixing each component of the polymer-based thermal interface material prepolymer evenly, apply it on the surface with micron On the template of the hierarchical array structure, pre-cure at 100°C to 150°C for 10 to 20 minutes, and then demould; in the technical solution of the present invention, the surface of the polymer-based thermal interface material prepolymer obtained through the above steps has a micron-scale array structure and viscosity.
  • the outer diameter of the carbon nanotube is 5 to 15 nanometers, and the length is 0.5 to 2 microns;
  • the carbon nanotubes undergo hydroxylation treatment.
  • step (2) the voltage of the electrostatic flocking is 20-100kV;
  • the flocking time of the electrostatic flocking is 20 to 60 seconds.
  • the curing temperature is 100-150°C
  • the curing time is 1.5 to 2.5 hours.
  • the present invention provides a gecko claw-like composite thermal interface material obtained by the above preparation method.
  • the invention provides a composite thermal interface material imitating a gecko claw and a preparation method thereof.
  • the invention first uses a template with a micron-scale array structure on the surface to pour a micron-scale array on the surface of the polymer-based thermal interface material prepolymer, and then uses electrostatic flocking technology to implant the carbon nanotube array onto the micron-scale array structure.
  • This structure can effectively increase the interface contact area, enhance the interface adsorption force, thereby reducing the interface contact thermal resistance.
  • the present invention uses electrostatic flocking to introduce carbon nanotube arrays. Compared with directly growing carbon nanotubes using chemical vapor deposition, this method is easier to realize the transfer of carbon nanotubes and has a simple preparation process.
  • Figure 1 is a schematic diagram of the surface bionic structure of a composite thermal interface material imitating a gecko claw in Embodiment 1 of the present invention.
  • Figure 2 is a silicon wafer template in Embodiment 1 of the present invention.
  • Figure 3 is a structural diagram of a micron-scale array in Embodiment 1 of the present invention.
  • Figure 4 is a surface profile curve of the micron-scale array structure in Embodiment 1 of the present invention.
  • Figure 5 is a scanning electron microscope picture of the carbon nanotubes in Example 1 of the present invention.
  • Figure 6 is a graph showing the adhesion test results of the composite thermal interface material imitating gecko claws in Example 1 of the present invention.
  • Carbon nanotubes were purchased from Aladdin, product number C419574, brand name short multi-walled carbon nanotubes;
  • Vinyl-terminated silicone oil was purchased from Ambia Specialty Silicones, with the brand name VS285CV;
  • the side chain hydrogen-containing silicone oil was purchased from Ambia Specialty Silicones, with the brand name XL1B.
  • the silicon wafer template is etched through the photolithography process to make the surface have a micron-scale array structure.
  • the specific parameters of the micron-scale array structure are: hole depth H 40 microns, hole diameter D 20 microns, and adjacent hole center distance L is 60 microns (observed by confocal microscope, see Figure 2), and then the surface is coated with a layer of polytetrafluoroethylene film with a thickness of 100 nanometers;
  • the matrix of the polymer-based thermal interface material prepolymer is obtained by mixing vinyl-terminated silicone oil (monomer) and side chain hydrogen-containing silicone oil (cross-linking agent) with a mass ratio of 1:0.4, and the filler is aluminum powder.
  • the mass fraction accounts for 90wt% of the polymer-based thermal interface material prepolymer; the aluminum powder is proportioned according to a mass ratio of 3:7 with a particle size of 1 to 6 microns: a particle size of 10 to 20 microns; the preparation process: combine the matrix and After the aluminum powder is stirred and mixed evenly, it is coated on the silicon wafer template obtained in step (1), pre-cured at 120°C for 10 minutes, and then demoulded; the surface of the obtained polymer-based thermal interface material prepolymer has a micron-scale array , and is sticky;
  • the thickness is 500mm; the electrostatic flocking voltage is 50kV, the flocking time is 30 seconds, the thickness of the carbon nanotube implant is about 200 nanometers, and the implantation density is 100mg/cm 2 ; after the flocking is completed, put it Put it into the oven for secondary curing, the curing temperature is 120°C, and the curing time is 2 hours; the schematic diagram of the bionic structure on the surface of the gecko claw-like composite thermal interface material obtained in this example is shown in Figure 1.
  • a Keyence confocal microscope was used to observe the micron-scale array structure on the surface of the silicon wafer template and the thermal interface material prepolymer.
  • Figure 2 shows the surface morphology of the silicon wafer template after etching in step (1). It can be seen that the surface of the silicon wafer has uniform holes;
  • Figure 3 shows the actual picture after the polymer-based thermal interface material prepolymer is demolded from the silicon wafer template in step (2), which shows that the demoulding effect is good, and it can be seen that the micron-scale array structure is evenly distributed in The surface of the thermal interface material prepolymer; its surface profile was observed with a confocal microscope.
  • the height of the micron cylinder is basically the same, 40 microns; the distance between adjacent wave peaks is the same, also 40 microns.
  • Test method Use welding strength tester DAGE4000 to test the adhesion force.
  • Test sample Sample 1 The polymer-based thermal interface material prepolymer with a micron-scale array on the surface obtained in step (2) and implanted with carbon nanotubes according to the relevant operations in step (3) (without secondary curing) ;Sample 2 Common thermal interface material prepolymer obtained with the same components on a common silicon wafer substrate;
  • test sample preparation is shown in the illustration in the upper left corner of Figure 6:
  • sample 1 and sample 2 are placed on the surface of the large silicon wafer (2.56cm*2.56cm). 1cm*1cm area, and then cover it with a small silicon wafer of 1cm*1cm, and treat it at 120°C for 2 hours to completely solidify (after sample 1 is cured, the micron-scale array structure and carbon nanotubes form a bionic structure); among them,
  • the surface of the small silicon wafer in contact with the sample is a rough surface, and the surface of the sample 1 with the bionic structure faces the small silicon wafer.
  • the large silicon wafer is used as a tray, and the probe is pushed outward from the bottom of the small silicon wafer.
  • the small silicon wafer and the large silicon wafer are bonded with a thermal interface material.
  • the thrust the small silicon wafer receives when it is pushed is the adhesive force;
  • Figure 6 shows the stress on the probe during the entire process.
  • the maximum stress is the bonding force of the thermal interface material. Test results show that the bonding force of thermal interface materials with bionic structures on their surfaces becomes stronger.
  • Test method Laser photothermal method, which is a non-contact thermal measurement method that can directly measure the contact thermal resistance of different interfaces in multi-layer samples. Based on the photothermal effect, the surface of the sample to be tested is periodically modulated laser heating, causing Measuring the periodic fluctuations of the sample surface temperature, and using a multi-layer physical model to fit the phase or amplitude of the test signal to determine the contact thermal resistance between the interfaces is one of the most important means of studying the interface thermal resistance.
  • Laser photothermal method test process First, a layer of chromium with a thickness of about 100 nanometers is coated on the surface of the smooth side of the silicon wafer as a light absorption layer. During the test process, the laser is emitted to the chromium layer, and the heat is transferred from the chromium to the silicon wafer. , and then transmitted to the thermal interface material, thereby obtaining the contact thermal resistance between the silicon wafer and the thermal interface material, and the contact thermal resistance between the silicon wafer and the chromium layer.
  • Test results Each group of samples is tested at four different points and the average value is taken. The above test results are shown in Table 1.
  • the interface contact thermal resistance between silicon wafer and chromium is basically the same, which is in line with expectations. However, the contact thermal resistance between the thermal interface material with the bionic structure on the surface and the rough silicon wafer surface is significantly lower than the contact thermal resistance between the ordinary thermal interface material and the silicon surface. It shows that this solution can effectively reduce the interface contact thermal resistance.

Abstract

Disclosed in the present invention are a gecko-claw-imitating composite thermal interface material and a preparation method therefor. The method comprises the following steps: (1) preparing a polymer-based thermal interface material prepolymer on a template having a micron-scale array structure on the surface, and demolding same to obtain a polymer-based thermal interface material prepolymer having a micron-scale array structure on the surface; and (2) implanting carbon nanotubes into the micron-scale array structure of the polymer-based thermal interface material prepolymer obtained in step (1) by means of an electrostatic flocking method, and curing same to obtain a gecko-claw-imitating composite thermal interface material. In the present invention, by means of treating the surface structure of a thermal interface material, a micro-nano two-level gecko-claw-imitating structure is formed, such that an interface contact area is effectively increased, an interface adsorption force is enhanced, and interfacial thermal contact resistance is reduced.

Description

一种仿壁虎爪的复合热界面材料及其制备方法A composite thermal interface material imitating gecko claws and its preparation method 技术领域Technical field
本发明涉及电子元器件用非金属功能材料制造技术领域,尤其涉及一种仿壁虎爪的复合热界面材料及其制备方法。The invention relates to the technical field of manufacturing non-metallic functional materials for electronic components, and in particular to a composite thermal interface material imitating gecko claws and a preparation method thereof.
背景技术Background technique
界面广泛存在于器件内部,且由于粗糙度的存在,两个表面贴合在一起时不可避免会夹杂空气间隙,而空气的导热性能极差,因此造成极大的接触热阻,热量无法散出,就会危害器件的使用寿命。为了促进界面导热,热界面材料应运而生。目前,最广泛使用的热界面材料是聚合物基热界面材料,其在所有热界面材料产品中的市场占比接近90% [1]。聚合物基热界面材料由聚合物基体和高导热填料(如金属 [2]、陶瓷 [3]、碳基材料 [4]等)复合而成。聚合物具有柔软、廉价、稳定性好等优点,但是其热导率很低,通常只有0.2W/(m·K)。导热填料如石墨烯、氮化硼、铝粉等,虽然热导率高,但是材质偏硬,不利于与器件界面的贴合。但是,为了提高聚合物基热界面材料的热导率,又不得不提高填料含量。这势必会影响热界面材料的力学性能,进一步影响热界面材料自身与器件界面的接触。力学性能差的热界面材料,不仅不会降低界面热阻,反而引入额外的界面热阻,因此开发出降低热界面材料界面热阻的方法至关重要。 The interface widely exists inside the device, and due to the presence of roughness, air gaps will inevitably be included when the two surfaces are bonded together. The thermal conductivity of air is extremely poor, resulting in a huge contact thermal resistance and the heat cannot be dissipated. , which will endanger the service life of the device. In order to promote interface thermal conduction, thermal interface materials have emerged. Currently, the most widely used thermal interface material is polymer-based thermal interface material, which accounts for nearly 90% of all thermal interface material products [1] . Polymer-based thermal interface materials are composed of polymer matrix and high thermal conductivity fillers (such as metals [2] , ceramics [3] , carbon-based materials [4] , etc.). Polymers have the advantages of softness, cheapness, and good stability, but their thermal conductivity is very low, usually only 0.2W/(m·K). Thermal conductive fillers such as graphene, boron nitride, aluminum powder, etc., although have high thermal conductivity, are relatively hard and are not conducive to bonding with the device interface. However, in order to improve the thermal conductivity of polymer-based thermal interface materials, the filler content has to be increased. This will inevitably affect the mechanical properties of the thermal interface material, and further affect the contact between the thermal interface material itself and the device interface. Thermal interface materials with poor mechanical properties will not only not reduce the interface thermal resistance, but also introduce additional interface thermal resistance. Therefore, it is crucial to develop methods to reduce the interface thermal resistance of thermal interface materials.
降低界面热阻的方法既可以从物理角度出发,也可以从化学角度出发。化学方法通过借助化学反应来降低界面热阻,实现的条件相对苛刻。而物理方法通过优化表面结构来改善界面接触,使用条件更加简单。Prasher [5]研究了表面粗糙度对界面接触热阻的影响,以几组不同粗糙度的铜基板作为接触面,以导热硅脂和相变复合材料作为热界面材料,测量不同组合的界面热阻,发现随着粗糙度的增大,器件与热界面材料的接触面积随之增大,从而降低接触热阻。其使用的方法比较简单,适合用于本身具有一定粗糙度的器件界面,且热界面 材料的粗糙度需要和器件界面的粗糙度相匹配才有效。关于表面结构的优化方法,生物界总能带来灵感。譬如,壁虎因具有飞檐走壁的能力,成为仿生学界的宠儿 [6]。研究者发现壁虎足部具有密集、高长径比、微米级刚毛阵列,刚毛材质柔韧,末端有众多纳米级绒毛。研究者认为这种微纳多层级结构变相地增大了界面间的接触面积,使接触面的范德华力翻倍增长,因此形成强大的黏附力 [6]。目前,关于仿壁虎爪的研究主要关注于黏附性能的提高。碳纳米管是一种中空、高导热材料,力学性能与壁虎爪微观结构相似,因此成为仿壁虎爪的绝佳材料 [7][8][9]。因为黏附性能与导热性能存在一定的正相关,所以也有人将这种仿生结构应用到热界面材料上。陈等人 [10]提出基于碳纳米管阵列的热界面材料,但是,不足之处在于他提出的结构并没有完全仿照壁虎爪。壁虎爪结构的特点是具有微-纳两层级结构。由于碳纳米管采用化学气相沉积法直接制备,很难转移到微米级阵列上。 The method of reducing interface thermal resistance can be based on both a physical and chemical perspective. Chemical methods use chemical reactions to reduce interface thermal resistance, and the conditions for implementation are relatively harsh. The physical method improves interface contact by optimizing the surface structure, and the use conditions are simpler. Prasher [5] studied the effect of surface roughness on interface contact thermal resistance. Several groups of copper substrates with different roughness were used as contact surfaces, and thermal conductive silicone grease and phase change composite materials were used as thermal interface materials to measure the interface heat of different combinations. It is found that as the roughness increases, the contact area between the device and the thermal interface material increases, thereby reducing the contact thermal resistance. The method used is relatively simple and is suitable for device interfaces that have a certain roughness. The roughness of the thermal interface material needs to match the roughness of the device interface to be effective. Regarding the optimization methods of surface structure, the biological world can always bring inspiration. For example, the gecko has become the darling of the bionics community because of its ability to fly over walls and fly over walls [6] . Researchers found that gecko feet have dense, high-aspect-ratio, arrays of micron-sized bristles. The bristles are made of flexible material and have numerous nano-sized hairs at their ends. Researchers believe that this micro-nano multi-level structure increases the contact area between the interfaces in a disguised manner, doubling the van der Waals force on the contact surface, thus forming a strong adhesion force [6] . Currently, research on imitation gecko claws mainly focuses on improving adhesion properties. Carbon nanotubes are a hollow, highly thermally conductive material with mechanical properties similar to the microstructure of gecko claws, making them an excellent material for imitating gecko claws [7][8][9] . Because there is a certain positive correlation between adhesion performance and thermal conductivity, some people have also applied this bionic structure to thermal interface materials. Chen et al. [10] proposed a thermal interface material based on carbon nanotube arrays. However, the disadvantage is that the structure he proposed did not completely imitate the gecko claw. The structure of the gecko claw is characterized by a micro-nano two-level structure. Since carbon nanotubes are directly prepared by chemical vapor deposition, they are difficult to transfer to micron-scale arrays.
上述技术方案虽然一定程度上降低了接触热阻,但同时存在其它问题:Although the above technical solution reduces the contact thermal resistance to a certain extent, it also has other problems:
在热界面材料表面做一些简单的微米级结构,通常只有当与器件界面本身的粗糙度相匹配时,才能起到降低界面热阻的效果,具有一定的局限性;Making some simple micron-level structures on the surface of thermal interface materials can usually only reduce the interface thermal resistance when it matches the roughness of the device interface itself, which has certain limitations;
仿壁虎爪结构能够有效地增强接触面的相互作用,但是鲜有应用到热界面材料上面。主要原因是目前仿壁虎爪研究主要集中在粘附性材料方面,转移到导热材料上需要克服一些问题。热界面材料通常是由高导热填料和基体组成的复合材料,材质不均匀,制备微米双层级结构更加困难。The imitation gecko claw structure can effectively enhance the interaction of the contact surface, but it is rarely applied to thermal interface materials. The main reason is that the current research on imitation gecko claws mainly focuses on adhesive materials, and some problems need to be overcome when transferring to thermally conductive materials. Thermal interface materials are usually composite materials composed of highly thermally conductive fillers and matrices. The materials are uneven and it is more difficult to prepare micron double-layer structures.
由于碳纳米管采用化学气相沉积法制备,无法直接生长在热界面材料表面,即使先在热界面材料表面刻蚀出微米级阵列结构,也很难将碳纳米管阵列转移到微米级结构上。Since carbon nanotubes are prepared by chemical vapor deposition, they cannot grow directly on the surface of the thermal interface material. Even if the micron-scale array structure is first etched on the surface of the thermal interface material, it is difficult to transfer the carbon nanotube array to the micron-scale structure.
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发明内容Contents of the invention
针对上述技术问题,本发明提供一种仿壁虎爪的复合热界面材料及其制备方法,降低热界面材料本身与器件界面的接触热阻。In view of the above technical problems, the present invention provides a composite thermal interface material imitating a gecko claw and a preparation method thereof, which reduces the thermal contact resistance between the thermal interface material itself and the device interface.
为实现上述目的,本发明采取的技术方案为:In order to achieve the above objects, the technical solutions adopted by the present invention are:
一方面,本发明提供一种仿壁虎爪的复合热界面材料的制备方法,包括以 下步骤:On the one hand, the present invention provides a method for preparing a composite thermal interface material imitating gecko claws, which includes the following steps:
(1)在表面具有微米级阵列结构的模板上制备聚合物基热界面材料预聚体,脱模后获得表面具有微米级阵列结构的聚合物基热界面材料预聚体;(1) Prepare a polymer-based thermal interface material prepolymer on a template with a micron-scale array structure on the surface, and obtain a polymer-based thermal interface material prepolymer with a micron-scale array structure on the surface after demoulding;
(2)通过静电植绒法将碳纳米管植入到步骤(1)得到的聚合物基热界面材料预聚体的微米级阵列结构上,固化后即得到所述仿壁虎爪的复合热界面材料。(2) Implant carbon nanotubes into the micron-scale array structure of the polymer-based thermal interface material prepolymer obtained in step (1) through electrostatic flocking. After solidification, the composite thermal interface imitating gecko claws is obtained. Material.
作为优选地实施方式,所述碳纳米管植入的密度为30~100mg/cm 2As a preferred embodiment, the density of the carbon nanotubes implanted is 30 to 100 mg/cm 2 .
作为优选地实施方式,步骤(1)中,所述微米级阵列结构包括多个微米级柱状孔洞;所述柱状孔洞的孔深H为20微米~40微米,所述柱状孔洞的孔直径D为20微米~30微米,所述多个微米级柱状孔洞相邻孔洞的圆心距离L为40~90微米。As a preferred embodiment, in step (1), the micron-scale array structure includes a plurality of micron-scale columnar holes; the hole depth H of the columnar holes is 20 microns to 40 microns, and the hole diameter D of the columnar holes is 20 to 30 microns, and the center distance L between adjacent holes of the plurality of micron-sized columnar holes is 40 to 90 microns.
在某些具体的实施方式中,步骤(1)中,所述表面具有微米级阵列结构的模板为硅基底,In some specific embodiments, in step (1), the template with a micron-scale array structure on its surface is a silicon substrate,
优选地,所述微米级阵列结构由光刻技术刻蚀得到;Preferably, the micron-scale array structure is etched by photolithography technology;
优选地,还包括对所述模板镀疏水薄膜的前处理;Preferably, it also includes pre-treatment of coating the template with a hydrophobic film;
优选地,所述疏水薄膜为聚四氟乙烯膜,厚度优选为100~200纳米;Preferably, the hydrophobic film is a polytetrafluoroethylene film, and the thickness is preferably 100 to 200 nanometers;
优选地,所述聚四氟乙烯膜采用等离子体增强化学气相沉积(PECVD)法镀于所述模板的表面。Preferably, the polytetrafluoroethylene film is plated on the surface of the template using plasma enhanced chemical vapor deposition (PECVD).
作为优选地实施方式,步骤(1)中,所述聚合物基热界面材料预聚体的组分包括聚合物基体和填料;As a preferred embodiment, in step (1), the components of the polymer-based thermal interface material prepolymer include a polymer matrix and fillers;
在本发明的技术方案中,所述聚合物基体没有特别的限制,具体可列举出环氧树脂、聚丁二烯、聚氨酯、丙烯酸树脂和聚二甲基硅氧烷等,优选为柔性高分子聚合物,例如聚二甲基硅氧烷(PDMS);In the technical solution of the present invention, the polymer matrix is not particularly limited. Specific examples include epoxy resin, polybutadiene, polyurethane, acrylic resin, polydimethylsiloxane, etc., and is preferably a flexible polymer. Polymers such as polydimethylsiloxane (PDMS);
在某些具体的实施方式中,所述聚合物基体包括单体和交联剂;所述单体优选为端乙烯基硅油,所述交联剂优选为侧链含氢硅油;所述端乙烯基硅油与侧链含氢硅油的质量比优选为1:(0.4~0.8);In some specific embodiments, the polymer matrix includes a monomer and a cross-linking agent; the monomer is preferably a vinyl-terminated silicone oil, and the cross-linking agent is preferably a side chain hydrogen-containing silicone oil; the vinyl-terminated silicone oil The mass ratio of the base silicone oil and the side chain hydrogen-containing silicone oil is preferably 1: (0.4~0.8);
在本发明的技术方案中,所述填料的种类没有特别的限制,具体可列举出铝粉、氧化铝粉、氮化硼、银粉、石墨烯、碳纤维等,优选为铝粉;所述填料的用量没有特别的限制,以铝粉作为填料,其质量分数占所述聚合物基热界面材料预聚体的80wt%~92wt%,以碳纤维或石墨烯作为填料,其质量分数占所述聚合物基热界面材料预聚体的20wt%~40wt%。In the technical solution of the present invention, the type of filler is not particularly limited. Specific examples include aluminum powder, alumina powder, boron nitride, silver powder, graphene, carbon fiber, etc., preferably aluminum powder; There is no special restriction on the amount. Aluminum powder is used as a filler, and its mass fraction accounts for 80wt% to 92wt% of the polymer-based thermal interface material prepolymer. Carbon fiber or graphene is used as a filler, and its mass fraction accounts for 80wt% to 92wt% of the polymer-based thermal interface material prepolymer. 20wt%~40wt% of the base thermal interface material prepolymer.
优选地,所述填料按照粒径1~6微米:粒径10~20微米的质量比为(2/8~3/7):1进行配比;Preferably, the filler is proportioned according to a mass ratio of particle size 1 to 6 microns: particle size 10 to 20 microns (2/8 to 3/7): 1;
具体地,步骤(1)中,所述制备聚合物基热界面材料预聚体的具体步骤为:将聚合物基热界面材料预聚体的各组分混合均匀后,涂覆于表面具有微米级阵列结构的模板上,100℃~150℃预固化10~20分钟,脱模;在本发明的技术方案中,通过上述步骤得到的聚合物基热界面材料预聚体的表面具有微米级阵列结构,且具有粘性。Specifically, in step (1), the specific steps for preparing the polymer-based thermal interface material prepolymer are: after mixing each component of the polymer-based thermal interface material prepolymer evenly, apply it on the surface with micron On the template of the hierarchical array structure, pre-cure at 100°C to 150°C for 10 to 20 minutes, and then demould; in the technical solution of the present invention, the surface of the polymer-based thermal interface material prepolymer obtained through the above steps has a micron-scale array structure and viscosity.
作为优选地实施方式,步骤(2)中,所述碳纳米管的外径为5~15纳米,长度为0.5~2微米;As a preferred embodiment, in step (2), the outer diameter of the carbon nanotube is 5 to 15 nanometers, and the length is 0.5 to 2 microns;
优选地,所述碳纳米管经过羟基化处理。Preferably, the carbon nanotubes undergo hydroxylation treatment.
作为优选地实施方式,步骤(2)中,所述静电植绒的电压为20~100kV;As a preferred embodiment, in step (2), the voltage of the electrostatic flocking is 20-100kV;
优选地,所述静电植绒的植绒时间为20~60秒。Preferably, the flocking time of the electrostatic flocking is 20 to 60 seconds.
作为优选地实施方式,步骤(2)中,所述固化的温度为100~150℃;As a preferred embodiment, in step (2), the curing temperature is 100-150°C;
优选地,所述固化的时间为1.5~2.5小时。Preferably, the curing time is 1.5 to 2.5 hours.
又一方面,本发明提供上述制备方法得到的仿壁虎爪的复合热界面材料。In another aspect, the present invention provides a gecko claw-like composite thermal interface material obtained by the above preparation method.
上述技术方案具有如下优点或者有益效果:The above technical solution has the following advantages or beneficial effects:
本发明提供一种仿壁虎爪的复合热界面材料及其制备方法,通过对热界面材料的表面结构的处理,降低热界面材料与器件界面的接触热阻。本发明首先用表面具有微米级阵列结构的模板在聚合物基热界面材料预聚体的表面倒出微米级阵列,然后用静电植绒技术将碳纳米管阵列植入到微米级阵列结构上,形成微-纳米两层级仿壁虎爪结构,这种结构能够有效的增加界面接触面积,增强 界面吸附力,从而降低界面接触热阻。本发明采用静电植绒的方式引入碳纳米管阵列,相比于用化学气相沉积直接生长碳纳米管,本方法更容易实现碳纳米管的转移,制备工艺简单。The invention provides a composite thermal interface material imitating a gecko claw and a preparation method thereof. By processing the surface structure of the thermal interface material, the contact thermal resistance of the interface between the thermal interface material and the device is reduced. The invention first uses a template with a micron-scale array structure on the surface to pour a micron-scale array on the surface of the polymer-based thermal interface material prepolymer, and then uses electrostatic flocking technology to implant the carbon nanotube array onto the micron-scale array structure. Forming a micro-nano two-level imitation gecko claw structure, this structure can effectively increase the interface contact area, enhance the interface adsorption force, thereby reducing the interface contact thermal resistance. The present invention uses electrostatic flocking to introduce carbon nanotube arrays. Compared with directly growing carbon nanotubes using chemical vapor deposition, this method is easier to realize the transfer of carbon nanotubes and has a simple preparation process.
附图说明Description of drawings
图1是本发明实施例1中的仿壁虎爪的复合热界面材料表面仿生结构的示意图。Figure 1 is a schematic diagram of the surface bionic structure of a composite thermal interface material imitating a gecko claw in Embodiment 1 of the present invention.
图2是本发明实施例1中的硅片模板。Figure 2 is a silicon wafer template in Embodiment 1 of the present invention.
图3是本发明实施例1中的微米级阵列的结构图。Figure 3 is a structural diagram of a micron-scale array in Embodiment 1 of the present invention.
图4是本发明实施例1中的微米级阵列结构的表面轮廓曲线。Figure 4 is a surface profile curve of the micron-scale array structure in Embodiment 1 of the present invention.
图5是本发明实施例1中的碳纳米管的扫描电子显微镜图片。Figure 5 is a scanning electron microscope picture of the carbon nanotubes in Example 1 of the present invention.
图6是本发明实施例1中的仿壁虎爪的复合热界面材料的粘接力测试结果图。Figure 6 is a graph showing the adhesion test results of the composite thermal interface material imitating gecko claws in Example 1 of the present invention.
具体实施方式Detailed ways
下述实施例仅仅是本发明的一部分实施例,而不是全部的实施例。因此,以下提供的本发明实施例中的详细描述并非旨在限制要求保护的本发明的范围,而是仅仅表示本发明的选定实施例。基于本发明的实施例,本领域技术人员在没有作出创造性劳动的前提下所获得的所有其他实施例,都属于本发明的保护范围。The following embodiments are only some of the embodiments of the present invention, rather than all of the embodiments. Therefore, the detailed description of the embodiments of the invention provided below is not intended to limit the scope of the claimed invention but rather to represent selected embodiments of the invention. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without any creative work fall within the protection scope of the present invention.
在本发明中,若非特指,所有的设备和原料等均可从市场购得或是本行业常用的。下述实施例中的方法,如无特别说明,均为本领域的常规方法。In the present invention, unless otherwise specified, all equipment and raw materials can be purchased from the market or are commonly used in the industry. The methods in the following examples are all conventional methods in the art unless otherwise specified.
下列实施例中:In the following examples:
碳纳米管(CNT)购自阿拉丁,货号C419574,品牌名为短多壁碳纳米管;Carbon nanotubes (CNT) were purchased from Aladdin, product number C419574, brand name short multi-walled carbon nanotubes;
端乙烯基硅油购自安必亚特种有机硅,牌号为VS285CV;Vinyl-terminated silicone oil was purchased from Ambia Specialty Silicones, with the brand name VS285CV;
侧链含氢硅油购自安必亚特种有机硅,牌号为XL1B。The side chain hydrogen-containing silicone oil was purchased from Ambia Specialty Silicones, with the brand name XL1B.
实施例1:Example 1:
本实施例中的仿壁虎爪的复合热界面材料的制备过程如下:The preparation process of the gecko claw-like composite thermal interface material in this embodiment is as follows:
(1)通过光刻工艺刻蚀硅片模板,使其表面具有微米级阵列结构,微米级阵列结构的具体参数为:孔深H 40微米,孔直径D 20微米,相邻孔圆心距离L为60微米(共聚焦显微镜观测得到,见图2),然后将其表面镀上一层厚度为100纳米的聚四氟乙烯膜;(1) The silicon wafer template is etched through the photolithography process to make the surface have a micron-scale array structure. The specific parameters of the micron-scale array structure are: hole depth H 40 microns, hole diameter D 20 microns, and adjacent hole center distance L is 60 microns (observed by confocal microscope, see Figure 2), and then the surface is coated with a layer of polytetrafluoroethylene film with a thickness of 100 nanometers;
(2)聚合物基热界面材料预聚体的基体由质量比为1:0.4的端乙烯基硅油(单体)和侧链含氢硅油(交联剂)混合得到,填料为铝粉,其质量分数占聚合物基热界面材料预聚体的90wt%;其中铝粉按照粒径1~6微米:粒径10~20微米的质量比为3:7进行配比;制备过程:将基体和铝粉搅拌混合均匀后,涂覆于步骤(1)得到的硅片模板上,120℃预固化10分钟,然后脱模;得到的聚合物基热界面材料预聚体的表面带有微米级阵列,且具有粘性;(2) The matrix of the polymer-based thermal interface material prepolymer is obtained by mixing vinyl-terminated silicone oil (monomer) and side chain hydrogen-containing silicone oil (cross-linking agent) with a mass ratio of 1:0.4, and the filler is aluminum powder. The mass fraction accounts for 90wt% of the polymer-based thermal interface material prepolymer; the aluminum powder is proportioned according to a mass ratio of 3:7 with a particle size of 1 to 6 microns: a particle size of 10 to 20 microns; the preparation process: combine the matrix and After the aluminum powder is stirred and mixed evenly, it is coated on the silicon wafer template obtained in step (1), pre-cured at 120°C for 10 minutes, and then demoulded; the surface of the obtained polymer-based thermal interface material prepolymer has a micron-scale array , and is sticky;
(3)将碳纳米管粉末进行羟基化,过程为将碳纳米管粉末浸入质量分数为30%过氧化氢溶液和质量分数为20%的氨水的混合溶液中浸泡12h,过氧化氢溶液和氨水的体积比为1:1,然后用酒精洗涤、烘干;(3) Hydroxylate the carbon nanotube powder. The process is to immerse the carbon nanotube powder in a mixed solution of 30% mass fraction hydrogen peroxide solution and 20% mass fraction ammonia water for 12 hours. The hydrogen peroxide solution and ammonia water are The volume ratio is 1:1, then wash and dry with alcohol;
取1g羟基化处理的碳纳米管粉末(图5所示,外径为15纳米,长度为0.5~2微米)在5cm*5cm的平面内铺展开,放入静电植绒设备的底部;将步骤(2)获得的聚合物基热界面材料预聚体置于碳纳米管粉末正上方20cm距离处对其表面的微米级阵列结构进行植绒,聚合物基热界面材料预聚体的尺寸为3cm*3cm,厚度为500mm;静电植绒电压为50kV,植绒时间为30秒,碳纳米管植入的厚度约为200纳米,植入密度为100mg/cm 2;植绒结束后,将其放入烘箱,进行二次固化,固化温度120℃,固化时间为2小时;本实施例得到的仿壁虎爪的复合热界面材料表面的仿生结构的示意图如图1所示。 Take 1g of hydroxylated carbon nanotube powder (shown in Figure 5, outer diameter is 15 nanometers, length is 0.5-2 microns), spread it in a 5cm*5cm plane, and place it at the bottom of the electrostatic flocking equipment; follow the steps (2) The obtained polymer-based thermal interface material prepolymer is placed at a distance of 20cm directly above the carbon nanotube powder to flock the micron-scale array structure on its surface. The size of the polymer-based thermal interface material prepolymer is 3cm. *3cm, the thickness is 500mm; the electrostatic flocking voltage is 50kV, the flocking time is 30 seconds, the thickness of the carbon nanotube implant is about 200 nanometers, and the implantation density is 100mg/cm 2 ; after the flocking is completed, put it Put it into the oven for secondary curing, the curing temperature is 120°C, and the curing time is 2 hours; the schematic diagram of the bionic structure on the surface of the gecko claw-like composite thermal interface material obtained in this example is shown in Figure 1.
效果测试:Effect test:
(1)形貌表征(1) Morphological characterization
采用基恩士共聚焦显微镜观测硅片模板和热界面材料预聚体表面的微米级 阵列结构。A Keyence confocal microscope was used to observe the micron-scale array structure on the surface of the silicon wafer template and the thermal interface material prepolymer.
图2所示为步骤(1)中刻蚀后的硅片模板的表面形貌,可以看出硅片的表面有均匀的孔洞;Figure 2 shows the surface morphology of the silicon wafer template after etching in step (1). It can be seen that the surface of the silicon wafer has uniform holes;
图3所示为步骤(2)中的聚合物基热界面材料预聚体从硅片模板上脱模后的实际图,表明脱模效果较好,可以看出微米级阵列结构均匀的分布在热界面材料预聚体的表面;用共聚焦显微观测其表面轮廓,如图4所示,微米圆柱的高度基本一致,为40微米;相邻波峰间距一致,也为40微米。Figure 3 shows the actual picture after the polymer-based thermal interface material prepolymer is demolded from the silicon wafer template in step (2), which shows that the demoulding effect is good, and it can be seen that the micron-scale array structure is evenly distributed in The surface of the thermal interface material prepolymer; its surface profile was observed with a confocal microscope. As shown in Figure 4, the height of the micron cylinder is basically the same, 40 microns; the distance between adjacent wave peaks is the same, also 40 microns.
(2)粘接力测试(2) Adhesion test
测试方法:采用焊接强度测试仪DAGE4000,测试粘接力。Test method: Use welding strength tester DAGE4000 to test the adhesion force.
测试样品:试样①步骤(2)得到的表面带有微米级阵列的聚合物基热界面材料预聚体且按照步骤(3)中的相关操作植入碳纳米管(不进行二次固化);试样②在普通的硅片基底上以相同组分得到的普通热界面材料预聚体;Test sample: Sample ① The polymer-based thermal interface material prepolymer with a micron-scale array on the surface obtained in step (2) and implanted with carbon nanotubes according to the relevant operations in step (3) (without secondary curing) ;Sample ② Common thermal interface material prepolymer obtained with the same components on a common silicon wafer substrate;
测试样品制样如图6中左上角的插图所示:每组样品制备四片小样,其中,将试样①和试样②放置在大硅片(2.56cm*2.56cm)表面上的4个1cm*1cm区域处,然后将1cm*1cm的小硅片覆盖其上,120℃处理2小时使其完全固化(试样①固化后,微米级阵列结构和碳纳米管构成仿生结构);其中,小硅片与试样接触的面为粗糙面,试样①具有仿生结构的面朝向小硅片。The test sample preparation is shown in the illustration in the upper left corner of Figure 6: Four small samples are prepared for each group of samples. Among them, sample ① and sample ② are placed on the surface of the large silicon wafer (2.56cm*2.56cm). 1cm*1cm area, and then cover it with a small silicon wafer of 1cm*1cm, and treat it at 120°C for 2 hours to completely solidify (after sample ① is cured, the micron-scale array structure and carbon nanotubes form a bionic structure); among them, The surface of the small silicon wafer in contact with the sample is a rough surface, and the surface of the sample ① with the bionic structure faces the small silicon wafer.
测试过程中,大硅片作为托盘,探针从小硅片的底部向外推,小硅片和大硅片之间用热界面材料粘连,小硅片被推动瞬间受到的推力即粘接力;图6显示探针在整个过程中的受力情况,最大受力即为热界面材料的粘接力。测试结果显示,表面带有仿生结构的热界面材料的粘接力变强。During the test, the large silicon wafer is used as a tray, and the probe is pushed outward from the bottom of the small silicon wafer. The small silicon wafer and the large silicon wafer are bonded with a thermal interface material. The thrust the small silicon wafer receives when it is pushed is the adhesive force; Figure 6 shows the stress on the probe during the entire process. The maximum stress is the bonding force of the thermal interface material. Test results show that the bonding force of thermal interface materials with bionic structures on their surfaces becomes stronger.
(3)基于光热法测试的界面热阻(3) Interface thermal resistance based on photothermal method test
测试方法:激光光热法,其是一种可以直接测量多层样品中不同界面接触热阻的非接触式热测量方法,基于光热效应,对待测样品表面进行周期性的调制激光加热,引起待测样品表面温度的周期性波动,并利用多层物理模型拟合测试信号的相位或幅值,确定界面间的接触热阻,是研究界面热阻最重要手段 之一。Test method: Laser photothermal method, which is a non-contact thermal measurement method that can directly measure the contact thermal resistance of different interfaces in multi-layer samples. Based on the photothermal effect, the surface of the sample to be tested is periodically modulated laser heating, causing Measuring the periodic fluctuations of the sample surface temperature, and using a multi-layer physical model to fit the phase or amplitude of the test signal to determine the contact thermal resistance between the interfaces is one of the most important means of studying the interface thermal resistance.
本实施例通过激光光热法测试了两组样品的接触热导:In this example, the contact thermal conductivity of two groups of samples was tested using the laser photothermal method:
①步骤(3)得到的仿壁虎爪的复合热界面材料与100微米厚的粗糙硅片表面的接触热阻;① Contact thermal resistance between the gecko claw-like composite thermal interface material obtained in step (3) and the rough silicon wafer surface with a thickness of 100 microns;
②与上述聚合物基热界面材料组分相同的未做表面处理且未复合碳纳米管的普通热界面材料与100微米厚的粗糙硅片表面的接触热阻;②Contact thermal resistance between an ordinary thermal interface material with the same components as the above polymer-based thermal interface material without surface treatment and without composite carbon nanotubes and a rough silicon wafer surface with a thickness of 100 microns;
激光光热法测试过程:首先在硅片光滑一侧的表面镀一层厚度约为100纳米的铬作为光吸收层,测试过程中,激光发射至铬层上,热量由铬传递到硅片上,再传至热界面材料上,由此获得硅片与热界面材料之间的接触热阻,以及硅片与铬层之间的接触热阻。Laser photothermal method test process: First, a layer of chromium with a thickness of about 100 nanometers is coated on the surface of the smooth side of the silicon wafer as a light absorption layer. During the test process, the laser is emitted to the chromium layer, and the heat is transferred from the chromium to the silicon wafer. , and then transmitted to the thermal interface material, thereby obtaining the contact thermal resistance between the silicon wafer and the thermal interface material, and the contact thermal resistance between the silicon wafer and the chromium layer.
测试结果:每组样品测试四处不同的点,取平均值。上述测试结果如表1所示。硅片与铬的界面接触热阻基本一致,符合预期。但是,表面做了仿生结构的热界面材料与粗糙硅片表面的接触热阻明显低于普通的热界面材料与硅表面的接触热阻。说明本方案相能有效降低界面接触热阻。Test results: Each group of samples is tested at four different points and the average value is taken. The above test results are shown in Table 1. The interface contact thermal resistance between silicon wafer and chromium is basically the same, which is in line with expectations. However, the contact thermal resistance between the thermal interface material with the bionic structure on the surface and the rough silicon wafer surface is significantly lower than the contact thermal resistance between the ordinary thermal interface material and the silicon surface. It shows that this solution can effectively reduce the interface contact thermal resistance.
表1Table 1
Figure PCTCN2022113646-appb-000001
Figure PCTCN2022113646-appb-000001
Figure PCTCN2022113646-appb-000002
Figure PCTCN2022113646-appb-000002
以上所述仅是本发明的优选实施方式,应当指出:对于本技术领域的普通技术人员来说,在不脱离本发明原理的前提下,还可以做出若干改进和润饰,这些改进和润饰也应视为本发明的保护范围。The above are only the preferred embodiments of the present invention. It should be pointed out that those of ordinary skill in the art can make several improvements and modifications without departing from the principles of the present invention. These improvements and modifications can also be made. should be regarded as the protection scope of the present invention.

Claims (19)

  1. 一种仿壁虎爪的复合热界面材料的制备方法,其特征在于,包括以下步骤:A method for preparing a composite thermal interface material imitating gecko claws, which is characterized by including the following steps:
    (1)在表面具有微米级阵列结构的模板上制备聚合物基热界面材料预聚体,脱模后获得表面具有微米级阵列结构的聚合物基热界面材料预聚体;(1) Prepare a polymer-based thermal interface material prepolymer on a template with a micron-scale array structure on the surface, and obtain a polymer-based thermal interface material prepolymer with a micron-scale array structure on the surface after demoulding;
    (2)通过静电植绒法将碳纳米管植入到步骤(1)得到的聚合物基热界面材料预聚体的微米级阵列结构上,固化后即得到所述仿壁虎爪的复合热界面材料。(2) Implant carbon nanotubes into the micron-scale array structure of the polymer-based thermal interface material prepolymer obtained in step (1) through electrostatic flocking. After solidification, the composite thermal interface imitating gecko claws is obtained. Material.
  2. 根据权利要求1所述的制备方法,其特征在于,所述碳纳米管植入的密度为30~100mg/cm 2The preparation method according to claim 1, characterized in that the density of the carbon nanotubes implanted is 30 to 100 mg/cm 2 .
  3. 根据权利要求1所述的制备方法,其特征在于,步骤(1)中,所述微米级阵列结构包括多个微米级孔洞;所述孔洞的孔深H为20微米~40微米,所述孔洞的孔直径D为20微米~30微米,所述多个微米级孔洞相邻孔洞的圆心距离L为40~90微米。The preparation method according to claim 1, characterized in that, in step (1), the micron-scale array structure includes a plurality of micron-scale holes; the hole depth H of the holes is 20 microns to 40 microns, and the holes The hole diameter D is 20-30 microns, and the distance L between the centers of adjacent holes of the plurality of micron-sized holes is 40-90 microns.
  4. 根据权利要求1所述的制备方法,其特征在于,步骤(1)中,所述微米级阵列结构由光刻技术刻蚀得到。The preparation method according to claim 1, characterized in that in step (1), the micron-scale array structure is etched by photolithography technology.
  5. 根据权利要求1所述的制备方法,其特征在于,步骤(1)中,还包括对所述模板镀疏水薄膜的前处理。The preparation method according to claim 1, characterized in that step (1) further includes pre-treatment of plating the template with a hydrophobic film.
  6. 根据权利要求5所述的制备方法,其特征在于,所述疏水薄膜为聚四氟乙烯膜。The preparation method according to claim 5, characterized in that the hydrophobic film is a polytetrafluoroethylene film.
  7. 根据权利要求6所述的制备方法,其特征在于,所述疏水薄膜的厚度为100~200纳米。The preparation method according to claim 6, wherein the thickness of the hydrophobic film is 100 to 200 nanometers.
  8. 根据权利要求6所述的制备方法,其特征在于,所述聚四氟乙烯膜采用等离子体增强化学气相沉积法镀于所述模板的表面。The preparation method according to claim 6, wherein the polytetrafluoroethylene film is plated on the surface of the template using a plasma enhanced chemical vapor deposition method.
  9. 根据权利要求1所述的制备方法,其特征在于,步骤(1)中,所述聚合物基热界面材料预聚体的组分包括聚合物基体和填料。The preparation method according to claim 1, characterized in that in step (1), the components of the polymer-based thermal interface material prepolymer include a polymer matrix and a filler.
  10. 根据权利要求9所述的制备方法,其特征在于,所述聚合物基体包括单 体和交联剂。The preparation method according to claim 9, characterized in that the polymer matrix includes monomers and cross-linking agents.
  11. 根据权利要求10所述的制备方法,其特征在于,所述单体为端乙烯基硅油,所述交联剂为侧链含氢硅油。The preparation method according to claim 10, characterized in that the monomer is vinyl-terminated silicone oil, and the cross-linking agent is side chain hydrogen-containing silicone oil.
  12. 根据权利要求11所述的制备方法,其特征在于,所述端乙烯基硅油与侧链含氢硅油的质量比为1:(0.4~0.8)。The preparation method according to claim 11, characterized in that the mass ratio of the terminal vinyl silicone oil and the side chain hydrogen-containing silicone oil is 1: (0.4-0.8).
  13. 根据权利要求1所述的制备方法,其特征在于,步骤(2)中,所述碳纳米管的外径为5~15纳米,长度为0.5~2微米。The preparation method according to claim 1, characterized in that, in step (2), the outer diameter of the carbon nanotube is 5 to 15 nanometers, and the length is 0.5 to 2 microns.
  14. 根据权利要求1所述的制备方法,其特征在于,步骤(2)中,所述碳纳米管经过羟基化处理。The preparation method according to claim 1, characterized in that, in step (2), the carbon nanotubes undergo hydroxylation treatment.
  15. 根据权利要求1所述的制备方法,其特征在于,步骤(2)中,所述静电植绒的电压为20~100kV。The preparation method according to claim 1, characterized in that in step (2), the voltage of the electrostatic flocking is 20-100kV.
  16. 根据权利要求15所述的制备方法,其特征在于,步骤(2)中,所述静电植绒的植绒时间为20~60秒。The preparation method according to claim 15, characterized in that in step (2), the flocking time of the electrostatic flocking is 20 to 60 seconds.
  17. 根据权利要求1所述的制备方法,其特征在于,步骤(2)中,所述固化的温度为100~150℃。The preparation method according to claim 1, characterized in that in step (2), the curing temperature is 100-150°C.
  18. 根据权利要求17所述的制备方法,其特征在于,步骤(2)中,所述固化的时间为1.5~2.5小时。The preparation method according to claim 17, characterized in that in step (2), the curing time is 1.5 to 2.5 hours.
  19. 权利要求1-18任一所述的制备方法得到的仿壁虎爪的复合热界面材料。A composite thermal interface material imitating a gecko claw obtained by the preparation method according to any one of claims 1 to 18.
PCT/CN2022/113646 2022-08-19 2022-08-19 Gecko-claw-imitating composite thermal interface material and preparation method therefor WO2024036611A1 (en)

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