CN102816442A - Composite material with high heat conductivity - Google Patents
Composite material with high heat conductivity Download PDFInfo
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- CN102816442A CN102816442A CN2012102737174A CN201210273717A CN102816442A CN 102816442 A CN102816442 A CN 102816442A CN 2012102737174 A CN2012102737174 A CN 2012102737174A CN 201210273717 A CN201210273717 A CN 201210273717A CN 102816442 A CN102816442 A CN 102816442A
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- 239000002131 composite material Substances 0.000 title claims abstract description 102
- 239000000463 material Substances 0.000 claims abstract description 17
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 28
- 229910052742 iron Inorganic materials 0.000 claims description 14
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 9
- 229910000831 Steel Inorganic materials 0.000 claims description 8
- 239000010959 steel Substances 0.000 claims description 8
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 7
- 229910052782 aluminium Inorganic materials 0.000 claims description 7
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 7
- 239000011231 conductive filler Substances 0.000 claims description 7
- 229910052802 copper Inorganic materials 0.000 claims description 7
- 239000010949 copper Substances 0.000 claims description 7
- 229910002804 graphite Inorganic materials 0.000 claims description 7
- 239000010439 graphite Substances 0.000 claims description 7
- 239000004033 plastic Substances 0.000 claims description 6
- 229920003023 plastic Polymers 0.000 claims description 6
- -1 silit Chemical compound 0.000 claims description 6
- 229920001971 elastomer Polymers 0.000 claims description 4
- 239000012188 paraffin wax Substances 0.000 claims description 4
- 239000005060 rubber Substances 0.000 claims description 4
- PIGFYZPCRLYGLF-UHFFFAOYSA-N Aluminum nitride Chemical compound [Al]#N PIGFYZPCRLYGLF-UHFFFAOYSA-N 0.000 claims description 3
- 229910021389 graphene Inorganic materials 0.000 claims description 2
- 229910017083 AlN Inorganic materials 0.000 claims 2
- 239000004411 aluminium Substances 0.000 claims 1
- 239000000945 filler Substances 0.000 abstract description 93
- 238000002360 preparation method Methods 0.000 abstract description 4
- 229910003460 diamond Inorganic materials 0.000 abstract 1
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- 238000012360 testing method Methods 0.000 description 40
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- 230000000052 comparative effect Effects 0.000 description 11
- PMHQVHHXPFUNSP-UHFFFAOYSA-M copper(1+);methylsulfanylmethane;bromide Chemical compound Br[Cu].CSC PMHQVHHXPFUNSP-UHFFFAOYSA-M 0.000 description 11
- 239000000843 powder Substances 0.000 description 11
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 11
- 238000010586 diagram Methods 0.000 description 9
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- 229910010271 silicon carbide Inorganic materials 0.000 description 9
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- 239000000203 mixture Substances 0.000 description 6
- 229920003048 styrene butadiene rubber Polymers 0.000 description 6
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- 229910052582 BN Inorganic materials 0.000 description 5
- 230000007797 corrosion Effects 0.000 description 4
- 238000005260 corrosion Methods 0.000 description 4
- 229920000459 Nitrile rubber Polymers 0.000 description 3
- 229920002302 Nylon 6,6 Polymers 0.000 description 3
- 239000002033 PVDF binder Substances 0.000 description 3
- 239000004743 Polypropylene Substances 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 229920003049 isoprene rubber Polymers 0.000 description 3
- 229920001684 low density polyethylene Polymers 0.000 description 3
- 239000004702 low-density polyethylene Substances 0.000 description 3
- 239000011812 mixed powder Substances 0.000 description 3
- 229920001155 polypropylene Polymers 0.000 description 3
- 229920001343 polytetrafluoroethylene Polymers 0.000 description 3
- 239000004810 polytetrafluoroethylene Substances 0.000 description 3
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Abstract
Description
技术领域 technical field
本发明涉及复合材料,特别涉及一种高导热复合材料。 The invention relates to composite materials, in particular to a high thermal conductivity composite material. the
背景技术 Background technique
随着工业生产的日益发展,设备的腐蚀问题在化工、石油、机械、纺织、冶金、航天航空、国防等领域越来越突出,尤其在换热器、导热管等换热场合。传统金属材料已经不能满足其耐腐蚀、高导热的要求。塑料、橡胶等基材具有优良的耐腐蚀性能,但低导热性能限制其在换热设备中的应用。应用高导热填料对这些基材进行共混改性是提高这些基材导热性能的有效途径,通过该方法制备的复合材料具有耐腐蚀、价格低廉、质量轻,易于加工成型等优点。 With the increasing development of industrial production, the corrosion of equipment is becoming more and more prominent in the fields of chemical industry, petroleum, machinery, textile, metallurgy, aerospace, national defense, etc., especially in heat exchange occasions such as heat exchangers and heat pipes. Traditional metal materials can no longer meet the requirements of corrosion resistance and high thermal conductivity. Substrates such as plastic and rubber have excellent corrosion resistance, but their low thermal conductivity limits their application in heat exchange equipment. Blending and modifying these substrates with high thermal conductivity fillers is an effective way to improve the thermal conductivity of these substrates. The composite materials prepared by this method have the advantages of corrosion resistance, low price, light weight, and easy processing and molding. the
尽管不少文献综述了用高导热填料来填充基材制备高导热复合材料的方法,但是,现有高导热复合材料制备方法的主要问题是:单纯从增加填料本身导热系数和增加填充量二方面考虑问题,没有从改变填料的形状和排列方式的角度出发考虑问题;导热填料形状单一,基本为球形(如图1所示)、片状(如图2所示)或圆柱形(如图3所示),没有形状和排列方式的特定控制,强化导热效果差。所制备的导热复合材料无法达到导热性能和力学性能的兼备,导热系数不高,难以满足实际需要的使用性能,限制了导热复合材料的应用。 Although many literatures have reviewed the method of using high thermal conductivity filler to fill the base material to prepare high thermal conductivity composite material, the main problem of the existing high thermal conductivity composite material preparation method is: simply from the two aspects of increasing the thermal conductivity of the filler itself and increasing the filling amount Considering the problem, the problem is not considered from the perspective of changing the shape and arrangement of the filler; the shape of the thermally conductive filler is single, basically spherical (as shown in Figure 1), flake (as shown in Figure 2) or cylindrical (as shown in Figure 3 shown), there is no specific control of the shape and arrangement, and the effect of enhancing thermal conductivity is poor. The prepared thermal conductive composite material cannot achieve both thermal conductivity and mechanical properties, the thermal conductivity is not high, and it is difficult to meet the actual required performance, which limits the application of thermal conductive composite materials. the
发明内容 Contents of the invention
为了克服现有技术的上述缺点与不足,本发明的目的在于提供一种高导热复合材料,在较少的填充量下,就能起到有效强化基材导热的效果。 In order to overcome the above-mentioned shortcomings and deficiencies of the prior art, the object of the present invention is to provide a composite material with high thermal conductivity, which can effectively enhance the thermal conductivity of the base material with a small filling amount. the
本发明的目的通过以下技术方案实现: The purpose of the present invention is achieved through the following technical solutions:
一种高导热复合材料,包括基材与高导热填料,所述高导热填料的形状为正方形、三角形、菱形、椭圆形、T形、工字形、Y形中的任一种。 A high thermal conductivity composite material, including a base material and a high thermal conductivity filler, the shape of the high thermal conductivity filler is any one of square, triangle, rhombus, ellipse, T-shape, I-shape, and Y-shape. the
所述基材为石蜡、塑料或橡胶。 The substrate is paraffin, plastic or rubber. the
所述高导热填料为铜、钢、铁、铝、石墨、石墨烯、碳化硅、氮化铝、氮化硼中的任意一种。 The high thermal conductivity filler is any one of copper, steel, iron, aluminum, graphite, graphene, silicon carbide, aluminum nitride and boron nitride. the
所述高导热填料在基材中定向排列,即高导热填料在基材中按照统一的方向分布,热流方向沿着高导热填料的最大长度方向。 The high thermal conductivity fillers are oriented in the substrate, that is, the high thermal conductivity fillers are distributed in a uniform direction in the substrate, and the heat flow direction is along the maximum length direction of the high thermal conductivity fillers. the
与现有技术相比,本发明具有以下优点和有益效果: Compared with prior art, the present invention has following advantage and beneficial effect:
1、本发明的高导热复合材料通过改变高导热填料形状,实现导热强化,强化导热的效果优于传统的球形、片形和圆柱形填料。从填料形状出发,对导热强化,对填料形状进行人工设计与优化。 1. The high thermal conductivity composite material of the present invention realizes enhanced thermal conductivity by changing the shape of the high thermal conductive filler, and the effect of enhanced thermal conductivity is better than that of traditional spherical, flake and cylindrical fillers. Starting from the shape of the filler, the thermal conductivity is strengthened, and the shape of the filler is artificially designed and optimized. the
2、本发明涉及的高导热复合材料的高导热填料的材料选择范围广、填充量少、复合材料导热性能好。本发明中的高导热填料由常见的高导热材料制成,易于获得,价格低廉;通过控制导热填料的形状,可以实现低填充量下复合材料的高导热效果。 2. The high thermal conductivity filler of the high thermal conductivity composite material involved in the present invention has a wide selection range of materials, less filling amount, and good thermal conductivity of the composite material. The high thermal conductivity filler in the present invention is made of common high thermal conductivity material, which is easy to obtain and low in price; by controlling the shape of the thermal conductivity filler, the high thermal conductivity effect of the composite material can be realized at a low filling amount. the
3、本发明涉及的高导热复合材料的制备方法的实现步骤简单,无需苛刻的加工条件,制备工艺简单;本发明所涉及的塑料、橡胶等基材及导热填料原材料均可直接购买。 3. The preparation method of the high thermal conductivity composite material involved in the present invention has simple steps, does not require harsh processing conditions, and has a simple preparation process; the base materials such as plastics and rubber involved in the present invention and the raw materials of thermally conductive fillers can be purchased directly. the
4、本发明的高导热填料可以定向排列,构建导热网络,实现导热最大化。 4. The high thermal conductivity fillers of the present invention can be oriented and arranged to build a heat conduction network to maximize heat conduction. the
附图说明 Description of drawings
图1为球形填料的示意图。 Figure 1 is a schematic diagram of spherical packing. the
图2为片形填料的示意图。 Figure 2 is a schematic diagram of sheet-shaped packing. the
图3为圆柱形填料的示意图。 Figure 3 is a schematic diagram of a cylindrical packing. the
图4为正方形填料的示意图。 Figure 4 is a schematic diagram of a square packing. the
图5为三角形填料的示意图。 Figure 5 is a schematic diagram of a triangular packing. the
图6为菱形填料的示意图。 Figure 6 is a schematic diagram of a rhomboid packing. the
图7为椭圆形填料的示意图。 Figure 7 is a schematic diagram of an elliptical packing. the
图8为T形填料的示意图。 Figure 8 is a schematic diagram of a T-shaped packing. the
图9为工字形填料的示意图。 Fig. 9 is a schematic diagram of an I-shaped packing. the
具体实施方式 Detailed ways
下面结合实施例及附图,对本发明作进一步地详细说明,但本发明的实施方式不限于此。 The present invention will be described in further detail below in conjunction with the embodiments and the accompanying drawings, but the embodiments of the present invention are not limited thereto. the
实施例1 Example 1
将1g图4所示的正方形钢填料和10g石蜡粉末用高速搅拌机预混后,将所得的混合物用双螺杆挤出机造粒,形成高导热复合材料。其中,高导热填料在复合材料中的质量含量为9.1%。将制得的粒料放入标准模具中在57℃下热压成型,按照测试样品尺寸裁取测试样。 After premixing 1 g of the square steel filler shown in Figure 4 and 10 g of paraffin wax powder with a high-speed mixer, the resulting mixture was pelletized with a twin-screw extruder to form a high thermal conductivity composite material. Among them, the mass content of the high thermal conductivity filler in the composite material is 9.1%. The prepared pellets were put into a standard mold for thermocompression molding at 57°C, and the test samples were cut according to the size of the test samples. the
采用DRPL-I导热系数测量仪对样品的热性能进行测试,另外,作为对比例,采用相同方法制取图1、图2、图3所示的传统形状填料填充的复合材料并对其导热系数进行测试。 The DRPL-I thermal conductivity measuring instrument was used to test the thermal properties of the samples. In addition, as a comparative example, the composite materials filled with traditional shapes shown in Figure 1, Figure 2, and Figure 3 were prepared by the same method and their thermal conductivity carry out testing. the
结果表明,通过加入正方形的钢填料制备的导热复合材料的导热系数是纯石蜡的5倍,是球形钢填料填充复合材料的3倍,是片形钢填料填充复合材料的2倍,是圆柱形钢填料填充复合材料的1.5倍。 The results show that the thermal conductivity of the thermally conductive composite material prepared by adding square steel filler is 5 times that of pure paraffin, 3 times that of spherical steel filler-filled composite material, 2 times that of sheet-shaped steel filler-filled composite material, and 3 times that of cylindrical steel filler-filled composite material. The steel filler is 1.5 times that of the composite material. the
实施例2 Example 2
将1g图5所示的三角形铜填料和12g聚偏氟乙烯(PVDF)粉末用高速搅拌机预混后,将所得的混合物用双螺杆挤出机造粒,形成高导热复合材料。其中,高导热填料在复合材料中的质量含量为7.7%。将制得的粒料放入标准模具中在200℃下热压成型,按照测试样品尺寸裁取测试样。 After premixing 1g of the triangular copper filler shown in Figure 5 and 12g of polyvinylidene fluoride (PVDF) powder with a high-speed mixer, the resulting mixture was pelletized with a twin-screw extruder to form a high thermal conductivity composite material. Among them, the mass content of the high thermal conductivity filler in the composite material is 7.7%. The prepared pellets were put into a standard mold and hot-pressed at 200°C, and the test samples were cut according to the size of the test samples. the
采用DRPL-I导热系数测量仪对样品的热性能进行测试,另外,作为对比例,采用相同方法制取图1、图2、图3所示的传统形状填料填充的复合材料并对其导热系数进行测试。 The DRPL-I thermal conductivity measuring instrument was used to test the thermal properties of the samples. In addition, as a comparative example, the composite materials filled with traditional shapes shown in Figure 1, Figure 2, and Figure 3 were prepared by the same method and their thermal conductivity carry out testing. the
结果表明,通过加入三角形的铜填料制备的导热复合材料的导热系数是纯聚偏氟乙烯的6倍,是球形铜填料填充复合材料的4倍,是片形铜填料填充复合材料的3倍,是圆柱形铜填料填充复合材料的1.5倍。 The results show that the thermal conductivity of the thermally conductive composite prepared by adding triangular copper fillers is 6 times that of pure polyvinylidene fluoride, 4 times that of spherical copper filler-filled composites, and 3 times that of sheet-shaped copper filler-filled composites, 1.5 times that of cylindrical copper filler-filled composites. the
实施例3 Example 3
将1g图6所示的菱形石墨填料和11g丁晴橡胶(NBR)用高速搅拌机预混后,将所得的混合粉末在120℃下用开炼塑机进行塑化和混炼,然后将制得的混合材料经破碎机破碎造粒,得到高导热复合材料。其中,高导热填料在复合材料中的质量含量为8.3%。将制得的粒料放入标准模具中在170℃下热压成型,按照测试样品尺寸裁取测试样。 After premixing 1g of the diamond-shaped graphite filler shown in Figure 6 and 11g of nitrile rubber (NBR) with a high-speed mixer, the resulting mixed powder was plasticized and kneaded at 120°C with an open-rolling plastic machine, and then the prepared The mixed material is crushed and granulated by a crusher to obtain a high thermal conductivity composite material. Among them, the mass content of the high thermal conductivity filler in the composite material is 8.3%. The prepared pellets were put into a standard mold and hot-pressed at 170°C, and the test samples were cut according to the size of the test samples. the
采用DRPL-I导热系数测量仪对样品的热性能进行测试,另外,作为对比例,采用相同方法制取图1、图2、图3所示的传统形状填料填充的复合材料并对其导热系数进行测试。 The DRPL-I thermal conductivity measuring instrument was used to test the thermal properties of the samples. In addition, as a comparative example, the composite materials filled with traditional shapes shown in Figure 1, Figure 2, and Figure 3 were prepared by the same method and their thermal conductivity carry out testing. the
结果表明,通过加入菱形的石墨填料制备的导热复合材料的导热系数是纯丁晴橡胶的7倍,是球形石墨填料填充复合材料的5倍,是片形石墨填料填充复合材料的3倍,是圆柱形石墨填料填充复合材料的2倍。 The results show that the thermal conductivity of the thermally conductive composite material prepared by adding diamond-shaped graphite filler is 7 times that of pure NBR, 5 times that of spherical graphite filler-filled composite material, and 3 times that of sheet-shaped graphite filler-filled composite material. Cylindrical graphite filler fills the composite 2 times. the
实施例4 Example 4
将1g图7所示的椭圆形铁填料和10g低密度聚乙烯(LDPE)粉末用高速搅拌机预混后,将所得的混合物用双螺杆挤出机造粒,形成高导热复合材料。其中,高导热填料在复合材料中的质量含量为9.1%。将制得的粒料放入标准模具中在170℃下热压成型,按照测试样品尺寸裁取测试样。 After premixing 1g of the elliptical iron filler shown in Figure 7 and 10g of low-density polyethylene (LDPE) powder with a high-speed mixer, the resulting mixture was pelletized with a twin-screw extruder to form a high thermal conductivity composite material. Among them, the mass content of the high thermal conductivity filler in the composite material is 9.1%. The prepared pellets were put into a standard mold and hot-pressed at 170°C, and the test samples were cut according to the size of the test samples. the
采用DRPL-I导热系数测量仪对样品的热性能进行测试,另外,作为对比例,采用相同方法制取图1、图2、图3所示的传统形状填料填充的复合材料并对其导热系数进行测试。 The DRPL-I thermal conductivity measuring instrument was used to test the thermal properties of the samples. In addition, as a comparative example, the composite materials filled with traditional shapes shown in Figure 1, Figure 2, and Figure 3 were prepared by the same method and their thermal conductivity carry out testing. the
结果表明,通过加入椭圆形的铁填料制备的导热复合材料的导热系数是纯低密度聚乙烯的8倍,是球形铁填料填充复合材料的5倍,是片形铁填料填充复合材料的4倍,是圆柱形铁填料填充复合材料的1.5倍。 The results show that the thermal conductivity of the thermally conductive composite prepared by adding elliptical iron fillers is 8 times that of pure low-density polyethylene, 5 times that of spherical iron filler-filled composites, and 4 times that of sheet-shaped iron filler-filled composites , 1.5 times that of cylindrical iron filler filled composites. the
实施例5 Example 5
将1g图8所示的T形铝填料和10g聚丙烯(PP)粉末用高速搅拌机预混后,将所得的混合物用双螺杆挤出机造粒,形成高导热复合材料。其中,高导热填料在复合材料中的质量含量为9.1%。将制得的粒料放入标准模具中在190℃下热压成型,按照测试样品尺寸裁取测试样。 After premixing 1g of the T-shaped aluminum filler shown in Figure 8 and 10g of polypropylene (PP) powder with a high-speed mixer, the resulting mixture was pelletized with a twin-screw extruder to form a high thermal conductivity composite material. Among them, the mass content of the high thermal conductivity filler in the composite material is 9.1%. The prepared pellets were put into a standard mold and hot-pressed at 190°C, and the test samples were cut according to the size of the test samples. the
采用DRPL-I导热系数测量仪对样品的热性能进行测试,另外,作为对比例,采用相同方法制取图1、图2、图3所示的传统形状填料填充的复合材料并对其导热系数进行测试。 The DRPL-I thermal conductivity measuring instrument was used to test the thermal properties of the samples. In addition, as a comparative example, the composite materials filled with traditional shapes shown in Figure 1, Figure 2, and Figure 3 were prepared by the same method and their thermal conductivity carry out testing. the
结果表明,通过加入T形的铝填料制备的导热复合材料的导热系数是纯聚丙烯的7倍,是球形铝填料填充复合材料的4倍,是片形铝填料填充复合材料的3倍,是圆柱形铝填料填充复合材料的2倍。 The results show that the thermal conductivity of the thermally conductive composite material prepared by adding T-shaped aluminum filler is 7 times that of pure polypropylene, 4 times that of the composite material filled with spherical aluminum filler, and 3 times that of the composite material filled with sheet-shaped aluminum filler. Cylindrical aluminum filler fills the composite 2 times. the
实施例6 Example 6
将1g图9所示的工字形碳化硅(SiC)填料和12g尼龙66(PA66)粉末用高速搅拌机预混后,将所得的混合物用双螺杆挤出机造粒,形成高导热复合材料。其中,高导热填料在复合材料中的质量含量为7.7%。将制得的粒料放入标准模具中在270℃下热压成型,按照测试样品尺寸裁取测试样。 After premixing 1g of the I-shaped silicon carbide (SiC) filler shown in Figure 9 and 12g of nylon 66 (PA66) powder with a high-speed mixer, the resulting mixture was pelletized with a twin-screw extruder to form a high thermal conductivity composite material. Among them, the mass content of the high thermal conductivity filler in the composite material is 7.7%. The prepared pellets were put into a standard mold and hot-pressed at 270°C, and the test samples were cut according to the size of the test samples. the
采用DRPL-I导热系数测量仪对样品的热性能进行测试,另外,作为对比例,采用相同方法制取图1、图2、图3所示的传统形状填料填充的复合材料并对其导热系数进行测试。 The DRPL-I thermal conductivity measuring instrument was used to test the thermal properties of the samples. In addition, as a comparative example, the composite materials filled with traditional shapes shown in Figure 1, Figure 2, and Figure 3 were prepared by the same method and their thermal conductivity carry out testing. the
结果表明,通过加入工字形的碳化硅填料制备的导热复合材料的导热系数是纯尼龙66的9倍,是球形碳化硅填料填充复合材料的6倍,是片形碳化硅填料填充复合材料的4倍,是圆柱形碳化硅填料填充复合材料的3倍。 The results show that the thermal conductivity of the thermally conductive composite material prepared by adding I-shaped silicon carbide filler is 9 times that of pure nylon 66, 6 times that of the composite material filled with spherical silicon carbide filler, and 4 times that of the composite material filled with sheet-shaped silicon carbide filler. times, which is 3 times that of cylindrical silicon carbide filler-filled composites. the
实施例7 Example 7
将1g Y形氮化铝(AlN)填料和10g聚四氟乙烯粉末(PTFE)末用高速搅拌机预混后,将所得的混合物用双螺杆挤出机造粒,形成高导热复合材料。其中,高导热填料在复合材料中的质量含量为9.1%。将制得的粒料放入标准模具中在170℃下热压成型,按照测试样品尺寸裁取测试样。 After premixing 1g of Y-shaped aluminum nitride (AlN) filler and 10g of polytetrafluoroethylene powder (PTFE) powder with a high-speed mixer, the resulting mixture was pelletized with a twin-screw extruder to form a high thermal conductivity composite material. Among them, the mass content of the high thermal conductivity filler in the composite material is 9.1%. The prepared pellets were put into a standard mold and hot-pressed at 170°C, and the test samples were cut according to the size of the test samples. the
采用DRPL-I导热系数测量仪对样品的热性能进行测试,另外,作为对比例,采用相同方法制取图1、图2、图3所示的传统形状填料填充的复合材料并对其导热系数进行测试。 The DRPL-I thermal conductivity measuring instrument was used to test the thermal properties of the samples. In addition, as a comparative example, the composite materials filled with traditional shapes shown in Figure 1, Figure 2, and Figure 3 were prepared by the same method and their thermal conductivity carry out testing. the
结果表明,通过加入Y形的氮化铝填料制备的导热复合材料的导热系数是聚四氟乙烯的6.5倍,是球形氮化铝填料填充复合材料的3倍,是片形氮化铝填料填充复合材料的2倍,是圆柱形氮化铝填料填充复合材料的1.5倍。 The results show that the thermal conductivity of the thermally conductive composite material prepared by adding Y-shaped aluminum nitride filler is 6.5 times that of polytetrafluoroethylene, 3 times that of the composite material filled with spherical aluminum nitride filler, and 3 times that of the composite material filled with sheet-shaped aluminum nitride filler. 2 times that of composite materials, and 1.5 times that of cylindrical aluminum nitride filler-filled composite materials. the
实施例8 Example 8
将1g图9所示的工字形氮化硼(BN)填料和12g丁苯橡胶(SBR)粉末用高速搅拌机预混后,将所得的混合粉末在120℃下用开炼塑机进行塑化和混炼,然后将制得的混合材料经破碎机破碎造粒,得到高导热复合材料。其中,高导热填料在复合材料中的质量含量为7.7%。将制得的粒料放入标准模具中在175℃下热压成型,按照测试样品尺寸裁取测试样。 After premixing 1g of the I-shaped boron nitride (BN) filler shown in Figure 9 and 12g of styrene-butadiene rubber (SBR) powder with a high-speed mixer, the resulting mixed powder was plasticized and mixed with an open-rolling plastic machine at 120°C. After kneading, the prepared mixed material is crushed and granulated by a crusher to obtain a high thermal conductivity composite material. Among them, the mass content of the high thermal conductivity filler in the composite material is 7.7%. The prepared pellets were put into a standard mold and hot-pressed at 175°C, and the test samples were cut according to the size of the test samples. the
采用DRPL-I导热系数测量仪对样品的热性能进行测试,另外,作为对比例,采用相同方法制取图1、图2、图3所示的传统形状填料填充的复合材料并对其导热系数进行测试。 The DRPL-I thermal conductivity measuring instrument was used to test the thermal properties of the samples. In addition, as a comparative example, the composite materials filled with traditional shapes shown in Figure 1, Figure 2, and Figure 3 were prepared by the same method and their thermal conductivity carry out testing. the
结果表明,通过加入工字形的氮化硼填料制备的导热复合材料的导热系数是丁苯橡胶的8倍,是球形氮化硼填料填充复合材料的4倍,是片形氮化硼填料填充复合材料的3倍,是圆柱形氮化硼填料填充复合材料的1.5倍。 The results show that the thermal conductivity of the thermally conductive composite material prepared by adding I-shaped boron nitride filler is 8 times that of styrene-butadiene rubber, 4 times that of spherical boron nitride filler-filled composite material, and the thermal conductivity of sheet-shaped boron nitride filler-filled composite material. 3 times that of the material, and 1.5 times that of the cylindrical boron nitride filler-filled composite. the
实施例9 Example 9
将1g Y形碳化硅(SiC)填料和10g异戊橡胶(IR)粉末用高速搅拌机预混后,将所得的混合粉末在100℃下用开炼塑机进行塑化和混炼,然后将制得 的混合材料经破碎机破碎造粒,得到高导热复合材料。其中,高导热填料在复合材料中的质量含量为9.1%。将制得的粒料放入标准模具中在180℃下热压成型,按照测试样品尺寸裁取测试样。 After premixing 1g of Y-shaped silicon carbide (SiC) filler and 10g of isoprene rubber (IR) powder with a high-speed mixer, the resulting mixed powder was plasticized and kneaded with an open mill at 100°C, and then the prepared The obtained mixed material is crushed and granulated by a crusher to obtain a high thermal conductivity composite material. Among them, the mass content of the high thermal conductivity filler in the composite material is 9.1%. The prepared pellets were put into a standard mold and hot-pressed at 180°C, and the test samples were cut according to the size of the test samples. the
采用DRPL-I导热系数测量仪对样品的热性能进行测试,另外,作为对比例,采用相同方法制取图1、图2、图3所示的传统形状填料填充的复合材料并对其导热系数进行测试。 The DRPL-I thermal conductivity measuring instrument was used to test the thermal properties of the samples. In addition, as a comparative example, the composite materials filled with traditional shapes shown in Figure 1, Figure 2, and Figure 3 were prepared by the same method and their thermal conductivity carry out testing. the
结果表明,通过加入Y形的碳化硅填料制备的导热复合材料的导热系数是纯异戊橡胶的6倍,是球形碳化硅填料填充复合材料的4倍,是片形碳化硅填料填充复合材料的3倍,是圆柱形碳化硅填料填充复合材料的2倍。 The results show that the thermal conductivity of the thermally conductive composite material prepared by adding Y-shaped silicon carbide filler is 6 times that of pure isoprene rubber, 4 times that of the composite material filled with spherical silicon carbide filler, and 4 times that of the composite material filled with sheet-shaped silicon carbide filler. 3 times, which is 2 times that of cylindrical silicon carbide filler-filled composite materials. the
实施例10 Example 10
将12g丁苯橡胶(SBR)粉末和1g图9所示的工字形铁填料在120℃下在模具中熔化,将模具的上下板接通强电流形成磁场,填料在熔化的基体中被磁化,磁化后的填料由于磁场的作用,形成定向排列,即工字形铁填料在基材中按照统一的方向分布,热流方向沿着工字形铁填料的最大长度方向。冷却后得到高导热复合材料。其中,高导热填料在复合材料中的质量含量为7.7%。 Melt 12g of styrene-butadiene rubber (SBR) powder and 1g of the I-shaped iron filler shown in Figure 9 in the mold at 120°C, connect the upper and lower plates of the mold with a strong current to form a magnetic field, and the filler is magnetized in the molten matrix. The magnetized fillers form a directional arrangement due to the action of the magnetic field, that is, the I-shaped iron fillers are distributed in a uniform direction in the base material, and the heat flow direction is along the maximum length direction of the I-shaped iron fillers. After cooling, a high thermal conductivity composite material is obtained. Among them, the mass content of the high thermal conductivity filler in the composite material is 7.7%. the
采用DRPL-I导热系数测量仪对样品的热性能进行测试,另外,作为对比例,采用相同方法制取图1、图2、图3所示的传统形状填料填充的复合材料并对其导热系数进行测试。 The DRPL-I thermal conductivity measuring instrument was used to test the thermal properties of the samples. In addition, as a comparative example, the composite materials filled with traditional shapes shown in Figure 1, Figure 2, and Figure 3 were prepared by the same method and their thermal conductivity carry out testing. the
结果表明,通过加入工字形的铁填料制备的导热复合材料的导热系数是丁苯橡胶的15倍,是球形铁填料填充复合材料的9倍,是片形铁填料填充复合材料的8倍,是圆柱形铁填料填充复合材料的6.5倍。 The results show that the thermal conductivity of the thermally conductive composite material prepared by adding I-shaped iron filler is 15 times that of styrene-butadiene rubber, 9 times that of the composite material filled with spherical iron filler, and 8 times that of the composite material filled with sheet-shaped iron filler. Cylindrical iron filler fills 6.5 times of composite material. the
实施例11 Example 11
将12g丁苯橡胶(SBR)粉末和1g的工字形氮化铝填料在120℃下在模具中熔化,将模具的上下板接通强直流电形成强电场,工字形氮化铝填料在电场作用下形成定向排列,冷却后得到高导热复合材料。其中,高导热填料在复合材料中的质量含量为7.7%。 Melt 12g of styrene-butadiene rubber (SBR) powder and 1g of I-shaped aluminum nitride filler in the mold at 120°C, connect the upper and lower plates of the mold with strong direct current to form a strong electric field, and the I-shaped aluminum nitride filler under the action of the electric field Orientation is formed, and high thermal conductivity composite materials are obtained after cooling. Among them, the mass content of the high thermal conductivity filler in the composite material is 7.7%. the
采用DRPL-I导热系数测量仪对样品的热性能进行测试,另外,作为对比例,采用相同方法制取图1、图2、图3所示的传统形状填料填充的复合材料并对其导热系数进行测试。 The DRPL-I thermal conductivity measuring instrument was used to test the thermal properties of the samples. In addition, as a comparative example, the composite materials filled with traditional shapes shown in Figure 1, Figure 2, and Figure 3 were prepared by the same method and their thermal conductivity carry out testing. the
结果表明,通过加入工字形的氮化铝填料制备的导热复合材料的导热系数 是丁苯橡胶的17倍,是球形氮化铝填料填充复合材料的9.5倍,是片形氮化铝填料填充复合材料的9倍,是圆柱形氮化铝填料填充复合材料的7倍。 The results show that the thermal conductivity of the thermally conductive composite material prepared by adding I-shaped aluminum nitride filler is 17 times that of styrene-butadiene rubber, 9.5 times that of spherical aluminum nitride filler-filled composite material, and 9.5 times that of sheet-shaped aluminum nitride filler-filled composite material. 9 times that of the material, and 7 times that of the cylindrical aluminum nitride filler-filled composite. the
上述实施例为本发明较佳的实施方式,但本发明的实施方式并不受所述实施例的限制,其他的任何未背离本发明的精神实质与原理下所作的改变、修饰、替代、组合、简化,均应为等效的置换方式,都包含在本发明的保护范围之内。 The above-mentioned embodiment is a preferred embodiment of the present invention, but the embodiment of the present invention is not limited by the embodiment, and any other changes, modifications, substitutions and combinations made without departing from the spirit and principle of the present invention , simplification, all should be equivalent replacement methods, and are all included in the protection scope of the present invention. the
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CN108457132A (en) * | 2018-04-10 | 2018-08-28 | 浙江舒康科技有限公司 | Aluminium ammonia heat pipe paper mould hot-pressing drying mold and drying means |
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