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CN116478449B - Preparation method and application of one-dimensional core-shell structure heat-conducting filler - Google Patents

Preparation method and application of one-dimensional core-shell structure heat-conducting filler Download PDF

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CN116478449B
CN116478449B CN202310584809.2A CN202310584809A CN116478449B CN 116478449 B CN116478449 B CN 116478449B CN 202310584809 A CN202310584809 A CN 202310584809A CN 116478449 B CN116478449 B CN 116478449B
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shell structure
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boron nitride
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CN116478449A (en
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冯宇
杨凯伦
陈庆国
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Harbin University of Science and Technology
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Abstract

一种一维核壳结构导热填料的制备方法及其应用,涉及聚合物基导热复合材料技术领域。本发明的目的是为了解决如何得到一种兼具导热和绝缘性能的聚合物基复合材料,同时实现低填充量以及优异的稳定性的问题。本发明提供一种一维核壳结构导热填料的制备方法,采用了静电纺丝法,以硅溶胶为基底材料,调节氮化硼纳米片的含量,得到不同氮化硼含量的高导热一维填料,相对于商用的氮化硼纳米片在面内和面外方向都有显著的提高。本发明可获得一种一维核壳结构导热填料的制备方法及其应用。

A preparation method and application of a one-dimensional core-shell structure thermally conductive filler, which relates to the technical field of polymer-based thermally conductive composite materials. The purpose of the present invention is to solve the problem of how to obtain a polymer-based composite material that has both thermal conductivity and insulation properties, while achieving low filling amount and excellent stability. The invention provides a method for preparing a one-dimensional core-shell structure thermally conductive filler, which adopts an electrospinning method, uses silica sol as a base material, and adjusts the content of boron nitride nanosheets to obtain high thermal conductivity one-dimensional fillers with different boron nitride contents. Fillers, compared to commercial boron nitride nanosheets, are significantly improved in both the in-plane and out-of-plane directions. The invention can obtain a preparation method and application of a one-dimensional core-shell structure thermally conductive filler.

Description

一种一维核壳结构导热填料的制备方法及其应用Preparation method and application of one-dimensional core-shell structure thermally conductive filler

技术领域Technical field

本发明涉及聚合物基导热复合材料技术领域,具体涉及一种一维核壳结构导热填料的制备方法及其应用。The invention relates to the technical field of polymer-based thermally conductive composite materials, and in particular to a preparation method and application of a one-dimensional core-shell structure thermally conductive filler.

背景技术Background technique

随着电力电子设备的小型化和集成化,伴随着能量密度的不断提升,对绝缘封装材料的综合性能提出了更高的要求。然而,聚合物极低的热导率(~0.2W/m·K)限制了设备内部的热量释放,会显著降低电力电子设备的稳定性、可靠性和寿命。因此制备兼具导热和绝缘性能的聚合物基复合材料成为了当今研究热点,将导热填料填充到聚合物中制备复合材料是提高聚合物热导率的有效策略。众多研究表明,陶瓷填料的引入可以赋予复合材料高热导率。传统商业导热填料,需要较高的填充量才能使聚合物材料的热导率得到满意的提升,然而这会降低复合材料的绝缘性能和机械性能。同时,高导热填料高昂的价格限制了其推广应用,因此如何实现低填充含量下,兼具高导热、优异绝缘性能的材料仍需要进一步研究。With the miniaturization and integration of power electronic equipment and the continuous improvement of energy density, higher requirements have been placed on the comprehensive performance of insulating packaging materials. However, the extremely low thermal conductivity of polymers (∼0.2 W/m·K) limits the heat release inside the device, which will significantly reduce the stability, reliability, and lifespan of power electronic devices. Therefore, the preparation of polymer-based composite materials with both thermal conductivity and insulation properties has become a hot research topic today. Filling thermally conductive fillers into polymers to prepare composite materials is an effective strategy to improve the thermal conductivity of polymers. Numerous studies have shown that the introduction of ceramic fillers can impart high thermal conductivity to composite materials. Traditional commercial thermally conductive fillers require a higher filling amount to satisfactorily improve the thermal conductivity of the polymer material. However, this will reduce the insulation performance and mechanical properties of the composite material. At the same time, the high price of high thermal conductivity fillers limits their promotion and application. Therefore, how to achieve materials with high thermal conductivity and excellent insulation properties at low filling content still requires further research.

发明内容Contents of the invention

本发明的目的是为了解决如何得到一种兼具导热和绝缘性能的聚合物基复合材料,同时实现低填充量以及优异的稳定性的问题,而提供一种一维核壳结构导热填料的制备方法及其应用。The purpose of the present invention is to solve the problem of how to obtain a polymer-based composite material with both thermal conductivity and insulation properties, while achieving low filling amount and excellent stability, and to provide a preparation of a one-dimensional core-shell structure thermal conductive filler Methods and their applications.

一种一维核壳结构导热填料,由氮化硼纳米片以及包裹在氮化硼纳米片外的二氧化硅层组成,一维核壳结构导热填料中氮化硼纳米片的质量分数为10~80%。A one-dimensional core-shell structure thermally conductive filler, consisting of boron nitride nanosheets and a silicon dioxide layer wrapped around the boron nitride nanosheets. The mass fraction of boron nitride nanosheets in the one-dimensional core-shell structure thermally conductive filler is 10 ~80%.

一种一维核壳结构导热填料的制备方法,按以下步骤进行:A method for preparing a one-dimensional core-shell structure thermally conductive filler according to the following steps:

步骤一:将正硅酸乙酯、氨水、乙醇和去离子水混合,搅拌均匀后,得到二氧化硅前驱体溶胶;Step 1: Mix ethyl orthosilicate, ammonia, ethanol and deionized water, and stir evenly to obtain a silica precursor sol;

步骤二:将聚乙烯醇、氮化硼纳米片和乙醇混合,搅拌均匀后,得到氮化硼纳米片悬浊液;Step 2: Mix polyvinyl alcohol, boron nitride nanosheets and ethanol, and stir evenly to obtain boron nitride nanosheet suspension;

步骤三:将步骤一中的二氧化硅前驱体溶胶和步骤二中的氮化硼纳米片悬浊液搅拌均匀,得到纺丝液;Step 3: Stir the silica precursor sol in step 1 and the boron nitride nanosheet suspension in step 2 evenly to obtain a spinning solution;

步骤四:将步骤三中的纺丝液真空除泡,进行静电纺丝,得到纤维膜;Step 4: Vacuum defoaming the spinning solution in Step 3, and perform electrospinning to obtain a fiber membrane;

步骤五:将步骤四中的纤维膜煅烧,研磨,得到一维核壳结构导热填料,所述的一维核壳结构导热填料中氮化硼纳米片的质量分数为10%、20%或30%。Step 5: Calculate and grind the fiber membrane in Step 4 to obtain a one-dimensional core-shell structure thermally conductive filler. The mass fraction of boron nitride nanosheets in the one-dimensional core-shell structure thermally conductive filler is 10%, 20% or 30%. %.

一种一维核壳结构导热填料的应用,所述的一维核壳结构导热填料用于制备热塑型或热固型聚合物复合材料,所述的热固型聚合物复合材料为高导热环氧树脂,制备方法如下:Application of a one-dimensional core-shell structure thermally conductive filler. The one-dimensional core-shell structure thermally conductive filler is used to prepare thermoplastic or thermosetting polymer composite materials. The thermosetting polymer composite material is highly thermally conductive. Epoxy resin, preparation method is as follows:

S1、将环氧树脂与固化剂在50~80℃下混合,得到混合液;所述的环氧树脂为E51型环氧树脂,所述的固化剂为甲基六氢苯酐;S1. Mix the epoxy resin and the curing agent at 50-80°C to obtain a mixed liquid; the epoxy resin is E51 type epoxy resin, and the curing agent is methylhexahydrophthalic anhydride;

S2、将一维核壳结构导热填料与有机溶剂混合,并以500~1500rpm/min的转速搅拌1~3h,得到一维填料悬浊液;所述的有机溶剂为乙醇或叔丁醇;S2. Mix the one-dimensional core-shell structure thermally conductive filler with an organic solvent, and stir for 1 to 3 hours at a speed of 500 to 1500 rpm/min to obtain a one-dimensional filler suspension; the organic solvent is ethanol or tert-butanol;

S3、将一维填料悬浊液与混合液混合,并以1000~1500rpm/min的转速搅拌1~3h,真空除泡后热压,得到热固型聚合物复合材料,所述的热固型聚合物复合材料中一维核壳结构导热填料的质量分数为10%、15%、20%、25%或30%。S3. Mix the one-dimensional filler suspension and the mixed liquid, stir for 1 to 3 hours at a speed of 1000 to 1500 rpm/min, vacuum defoaming and hot pressing to obtain a thermosetting polymer composite material. The thermosetting polymer composite material is The mass fraction of the one-dimensional core-shell structure thermally conductive filler in the polymer composite material is 10%, 15%, 20%, 25% or 30%.

本发明的有益效果:Beneficial effects of the present invention:

(1)本发明提供一种一维核壳结构导热填料的制备方法,采用了静电纺丝法,以硅溶胶为基底材料,调节氮化硼纳米片的含量,得到不同氮化硼含量的高导热一维填料,相对于商用的氮化硼纳米片在面内和面外方向都有显著的提高。(1) The present invention provides a method for preparing a one-dimensional core-shell structure thermally conductive filler, which adopts an electrospinning method, uses silica sol as the base material, and adjusts the content of boron nitride nanosheets to obtain high-performance materials with different boron nitride contents. The thermally conductive one-dimensional filler is significantly improved in both in-plane and out-of-plane directions compared to commercial boron nitride nanosheets.

本发明一维核壳结构导热填料具有更高的长径比,更容易在聚合物基体中形成导热通路,同时可以增强导热填料与聚合物基体的相容性,解决了商用氮化硼填料在基体中易团聚的问题。The one-dimensional core-shell structure thermal conductive filler of the present invention has a higher aspect ratio and is easier to form a thermal conductive path in the polymer matrix. At the same time, it can enhance the compatibility between the thermal conductive filler and the polymer matrix and solve the problem of commercial boron nitride filler. The problem of easy agglomeration in the matrix.

(2)本发明提供的一维核壳结构导热填料适用于制备多种形态的复合材料,不管是热固性材料还是热塑性材料,都能有更优异的稳定性和导热性能,同时保证其绝缘性能。(2) The one-dimensional core-shell structure thermally conductive filler provided by the present invention is suitable for preparing various forms of composite materials. Whether they are thermosetting materials or thermoplastic materials, they can have better stability and thermal conductivity while ensuring their insulation properties.

本发明可获得一种一维核壳结构导热填料的制备方法及其应用。The invention can obtain a preparation method and application of a one-dimensional core-shell structure thermally conductive filler.

附图说明Description of the drawings

图1为实施例1中一维核壳结构导热填料SiO2@BNNS 10wt%的扫描电镜图;Figure 1 is a scanning electron microscope image of the one-dimensional core-shell structure thermally conductive filler SiO 2 @BNNS 10wt% in Example 1;

图2为实施例2中一维核壳结构导热填料SiO2@BNNS 20wt%的扫描电镜图;Figure 2 is a scanning electron microscope image of the one-dimensional core-shell structure thermally conductive filler SiO 2 @BNNS 20wt% in Example 2;

图3为实施例3中一维核壳结构导热填料SiO2@BNNS 30wt%的扫描电镜图。Figure 3 is a scanning electron microscope image of the one-dimensional core-shell structure thermally conductive filler SiO 2 @BNNS 30wt% in Example 3.

具体实施方式Detailed ways

具体实施方式一:本实施方式一种一维核壳结构导热填料,由氮化硼纳米片以及包裹在氮化硼纳米片外的二氧化硅层组成,一维核壳结构导热填料中氮化硼纳米片的质量分数为10~80%。Specific Embodiment 1: This embodiment is a one-dimensional core-shell structure thermally conductive filler, which is composed of boron nitride nanosheets and a silicon dioxide layer wrapped around the boron nitride nanosheets. The one-dimensional core-shell structure thermally conductive filler contains nitride The mass fraction of boron nanosheets is 10-80%.

具体实施方式二:本实施方式与具体实施方式一不同点是:所述的氮化硼纳米片的粒径为50nm~10um。Specific Embodiment 2: The difference between this embodiment and Specific Embodiment 1 is that the particle size of the boron nitride nanosheets is 50 nm to 10 um.

其他步骤与具体实施方式一相同。Other steps are the same as the first embodiment.

具体实施方式三:本实施方式一种一维核壳结构导热填料的制备方法,按以下步骤进行:Specific Embodiment Three: In this embodiment, a method for preparing a one-dimensional core-shell structure thermally conductive filler is carried out according to the following steps:

步骤一:将正硅酸乙酯、氨水、乙醇和去离子水混合,搅拌均匀后,得到二氧化硅前驱体溶胶;Step 1: Mix ethyl orthosilicate, ammonia, ethanol and deionized water, and stir evenly to obtain a silica precursor sol;

步骤二:将聚乙烯醇、氮化硼纳米片和乙醇混合,搅拌均匀后,得到氮化硼纳米片悬浊液;Step 2: Mix polyvinyl alcohol, boron nitride nanosheets and ethanol, and stir evenly to obtain boron nitride nanosheet suspension;

步骤三:将步骤一中的二氧化硅前驱体溶胶和步骤二中的氮化硼纳米片悬浊液搅拌均匀,得到纺丝液;Step 3: Stir the silica precursor sol in step 1 and the boron nitride nanosheet suspension in step 2 evenly to obtain a spinning solution;

步骤四:将步骤三中的纺丝液真空除泡,进行静电纺丝,得到纤维膜;Step 4: Vacuum defoaming the spinning solution in Step 3, and perform electrospinning to obtain a fiber membrane;

步骤五:将步骤四中的纤维膜煅烧,研磨,得到一维核壳结构导热填料,所述的一维核壳结构导热填料中氮化硼纳米片的质量分数为10%、20%或30%。Step 5: Calculate and grind the fiber membrane in Step 4 to obtain a one-dimensional core-shell structure thermally conductive filler. The mass fraction of boron nitride nanosheets in the one-dimensional core-shell structure thermally conductive filler is 10%, 20% or 30%. %.

本实施方式的有益效果:Beneficial effects of this implementation:

(1)本实施方式提供一种一维核壳结构导热填料的制备方法,采用了静电纺丝法,以硅溶胶为基底材料,调节氮化硼纳米片的含量,得到不同氮化硼含量的高导热一维填料,相对于商用的氮化硼纳米片在面内和面外方向都有显著的提高。(1) This embodiment provides a method for preparing a one-dimensional core-shell structure thermally conductive filler, which adopts the electrospinning method, uses silica sol as the base material, and adjusts the content of boron nitride nanosheets to obtain different boron nitride contents. High thermal conductivity one-dimensional filler, compared with commercial boron nitride nanosheets, is significantly improved in both the in-plane and out-of-plane directions.

本实施方式一维核壳结构导热填料具有更高的长径比,更容易在聚合物基体中形成导热通路,同时可以增强导热填料与聚合物基体的相容性,解决了商用氮化硼填料在基体中易团聚的问题。The one-dimensional core-shell structure thermally conductive filler in this embodiment has a higher aspect ratio, which makes it easier to form a thermally conductive path in the polymer matrix. At the same time, the compatibility between the thermally conductive filler and the polymer matrix can be enhanced, solving the problem of commercial boron nitride filler. The problem of easy agglomeration in the matrix.

(2)本实施方式提供的一维核壳结构导热填料适用于制备多种形态的复合材料,不管是热固性材料还是热塑性材料,都能有更优异的稳定性和导热性能,同时保证其绝缘性能。(2) The one-dimensional core-shell structure thermally conductive filler provided by this embodiment is suitable for preparing various forms of composite materials. Whether they are thermosetting materials or thermoplastic materials, they can have better stability and thermal conductivity while ensuring their insulation properties. .

具体实施方式四:本实施方式与具体实施方式三不同点是:步骤一中正硅酸乙酯、氨水、乙醇与去离子水的体积比为(10~15):(15~30):(15~30):(5~10),所述的正硅酸乙酯的浓度为0.1~4mol/L,所述的氨水的浓度为0.5~2mol/L,所述乙醇的浓度为5~20mol/L。Specific embodiment four: The difference between this embodiment and the third embodiment is: in step one, the volume ratio of ethyl orthosilicate, ammonia water, ethanol and deionized water is (10~15): (15~30): (15 ~30): (5~10), the concentration of the ethyl orthosilicate is 0.1~4mol/L, the concentration of the ammonia solution is 0.5~2mol/L, and the concentration of the ethanol is 5~20mol/ L.

其他步骤与具体实施方式三相同。Other steps are the same as the third embodiment.

具体实施方式五:本实施方式与具体实施方式三或四不同点是:步骤二中聚乙烯醇、氮化硼纳米片与乙醇的质量比为3:1:(5~10)。Specific Embodiment 5: The difference between this embodiment and Specific Embodiment 3 or 4 is that the mass ratio of polyvinyl alcohol, boron nitride nanosheets and ethanol in step two is 3:1: (5-10).

其他步骤与具体实施方式三或四相同。Other steps are the same as the third or fourth embodiment.

具体实施方式六:本实施方式与具体实施方式三至五之一不同点是:步骤三中二氧化硅前驱体溶胶与氮化硼纳米片悬浊液的质量比为1:(2~10)。Specific Embodiment Six: The difference between this embodiment and one of Specific Embodiments Three to Five is that the mass ratio of the silicon dioxide precursor sol and the boron nitride nanosheet suspension in step three is 1: (2-10) .

其他步骤与具体实施方式三至五相同。Other steps are the same as specific embodiments three to five.

具体实施方式七:本实施方式与具体实施方式三至六之一不同点是:步骤一中的搅拌时间为3~8h,步骤二中的搅拌时间为1~3h,步骤三中的搅拌时间为3~8h。Specific Embodiment Seven: The difference between this embodiment and one of Specific Embodiments Three to Six is: the stirring time in step one is 3 to 8 hours, the stirring time in step two is 1 to 3 hours, and the stirring time in step three is 3~8h.

其他步骤与具体实施方式三至六相同。Other steps are the same as specific embodiments three to six.

具体实施方式八:本实施方式与具体实施方式三至七之一不同点是:步骤四中静电纺丝采用静电纺丝机,纺丝参数如下:不锈钢针头内径为0.17~3.5mm;正极板电压为5~30kV,负极板电压为5~30kV;针头平移速度为50~100mm/min;推注速度为0.3~1mm/s,接收距离为15~25cm。Specific Embodiment 8: The difference between this embodiment and one of Specific Embodiments 3 to 7 is that in step four, an electrospinning machine is used for electrospinning. The spinning parameters are as follows: the inner diameter of the stainless steel needle is 0.17~3.5mm; the positive plate voltage The voltage of the negative plate is 5~30kV; the needle translation speed is 50~100mm/min; the injection speed is 0.3~1mm/s, and the receiving distance is 15~25cm.

其他步骤与具体实施方式三至七相同。Other steps are the same as specific implementation modes three to seven.

具体实施方式九:本实施方式与具体实施方式三至八之一不同点是:步骤四中静电纺丝后,置于60~100℃的烘箱中干燥1~3h;步骤五中煅烧步骤如下:先以5~15℃/min的升温速率升温至400~600℃,并在400~600℃下保温0.5~2h;保温结束后以5~15℃/min的升温速率继续升温至600~1300℃,并在600~1300℃下保温2~4h。Specific embodiment nine: The difference between this embodiment and one of specific embodiments three to eight is: after electrospinning in step four, it is dried in an oven at 60 to 100°C for 1 to 3 hours; the calcining step in step five is as follows: First, heat up to 400~600°C at a heating rate of 5~15°C/min, and keep it at 400~600°C for 0.5~2h; after the insulation, continue to heat up to 600~1300°C at a heating rate of 5~15°C/min. , and keep it at 600~1300℃ for 2~4h.

其他步骤与具体实施方式三至八相同。Other steps are the same as specific embodiments three to eight.

具体实施方式十:本实施方式一种一维核壳结构导热填料的应用,所述的一维核壳结构导热填料用于制备热塑型或热固型聚合物复合材料,所述的热固型聚合物复合材料为高导热环氧树脂,制备方法如下:Specific Embodiment 10: This embodiment uses an application of a one-dimensional core-shell structure thermally conductive filler. The one-dimensional core-shell structure thermally conductive filler is used to prepare thermoplastic or thermosetting polymer composite materials. The thermosetting Type polymer composite material is high thermal conductivity epoxy resin, and the preparation method is as follows:

S1、将环氧树脂与固化剂在50~80℃下混合,得到混合液;所述的环氧树脂为E51型环氧树脂,所述的固化剂为甲基六氢苯酐;S1. Mix the epoxy resin and the curing agent at 50-80°C to obtain a mixed liquid; the epoxy resin is E51 type epoxy resin, and the curing agent is methylhexahydrophthalic anhydride;

S2、将一维核壳结构导热填料与有机溶剂混合,并以500~1500rpm/min的转速搅拌1~3h,得到一维填料悬浊液;所述的有机溶剂为乙醇或叔丁醇;S2. Mix the one-dimensional core-shell structure thermally conductive filler with an organic solvent, and stir for 1 to 3 hours at a speed of 500 to 1500 rpm/min to obtain a one-dimensional filler suspension; the organic solvent is ethanol or tert-butanol;

S3、将一维填料悬浊液与混合液混合,并以1000~1500rpm/min的转速搅拌1~3h,真空除泡后热压,得到热固型聚合物复合材料,所述的热固型聚合物复合材料中一维核壳结构导热填料的质量分数为10%、15%、20%、25%或30%。S3. Mix the one-dimensional filler suspension and the mixed liquid, stir for 1 to 3 hours at a speed of 1000 to 1500 rpm/min, vacuum defoaming and hot pressing to obtain a thermosetting polymer composite material. The thermosetting polymer composite material is The mass fraction of the one-dimensional core-shell structure thermally conductive filler in the polymer composite material is 10%, 15%, 20%, 25% or 30%.

采用以下实施例验证本发明的有益效果:The following examples are used to verify the beneficial effects of the present invention:

实施例1:一种一维核壳结构导热填料的制备方法,按以下步骤进行:Example 1: A method for preparing a one-dimensional core-shell structure thermally conductive filler, proceed as follows:

步骤一:将15mL正硅酸乙酯、30mL氨水、30mL乙醇和10mL去离子水置于烧杯中,搅拌8h后,得到二氧化硅前驱体溶胶;Step 1: Place 15 mL of ethyl orthosilicate, 30 mL of ammonia, 30 mL of ethanol and 10 mL of deionized water in a beaker. After stirring for 8 hours, a silica precursor sol is obtained;

所述的正硅酸乙酯的浓度为0.2mol/L,所述的氨水的浓度为0.8mol/L,所述乙醇的浓度为10mol/L。The concentration of ethyl orthosilicate is 0.2 mol/L, the concentration of ammonia water is 0.8 mol/L, and the concentration of ethanol is 10 mol/L.

步骤二:将18g聚乙烯醇、6g氮化硼纳米片和36g乙醇加入到新烧杯中,搅拌3h至均匀,得到氮化硼纳米片悬浊液;Step 2: Add 18g polyvinyl alcohol, 6g boron nitride nanosheets and 36g ethanol into a new beaker, stir for 3 hours until uniform, and obtain boron nitride nanosheet suspension;

所述的氮化硼纳米片的粒径为50nm~10um。The particle size of the boron nitride nanosheets is 50nm-10um.

步骤三:取等质量的二氧化硅前驱体溶胶和氮化硼纳米片悬浊液,搅拌8h后,得到纺丝液。Step 3: Take equal masses of silica precursor sol and boron nitride nanosheet suspension, and stir for 8 hours to obtain a spinning solution.

步骤四:将纺丝液真空除泡后用10mL针管抽取开始进行纺丝,接通电压,一头连接接收器铝箔(负极),另一头连接用于静电纺丝的注射器针头(正极),进行静电纺丝,得到纤维膜;Step 4: After vacuum defoaming the spinning solution, use a 10mL syringe to extract it and start spinning. Turn on the voltage, connect one end to the receiver aluminum foil (negative pole), and the other end to the syringe needle (positive pole) used for electrospinning, and conduct electrostatic Spinning to obtain fiber membrane;

静电纺丝采用静电纺丝机,纺丝参数如下:不锈钢针头内径为0.21mm;电压为20kV(负极电压-5kV,正极电压15kV);针头平移速度为60mm/min;推注速度为0.3mm/s,接收距离为25cm。Electrospinning uses an electrospinning machine, and the spinning parameters are as follows: the inner diameter of the stainless steel needle is 0.21mm; the voltage is 20kV (negative voltage -5kV, positive voltage 15kV); the needle translation speed is 60mm/min; the injection speed is 0.3mm/ s, the receiving distance is 25cm.

步骤五:纺丝结束后,将前驱体纤维膜从铝箔上取下,置于100℃的烘箱中干燥1h,以蒸发剩余的溶剂;然后置于马弗炉中,先以15℃/min的升温速率升温至500℃,并在500℃下保温2h;保温结束后以15℃/min的升温速率继续升温至1200℃,并在1200℃下保温4h,最后研磨,得到一维核壳结构导热填料,氮化硼纳米片的质量分数为10%,命名为SiO2@BNNS10wt%。Step 5: After spinning, remove the precursor fiber membrane from the aluminum foil and dry it in an oven at 100°C for 1 hour to evaporate the remaining solvent; then place it in a muffle furnace, first at 15°C/min. The heating rate is increased to 500°C, and the temperature is maintained at 500°C for 2 hours; after the insulation is completed, the temperature is continued to be heated to 1200°C at a heating rate of 15°C/min, and maintained at 1200°C for 4 hours, and finally ground to obtain a one-dimensional core-shell structure for thermal conductivity. The filler, the mass fraction of boron nitride nanosheets is 10%, named SiO 2 @BNNS10wt%.

实施例2:本实施例提供了一种一维核壳结构导热填料的制备,方法步骤同实施例1,不同之处在于步骤二中加入氮化硼的质量为9g;步骤四中推注速度为0.4mm/min,接收距离为25cm,电压为24kV(负极电压-12kV,正极电压+12kV),最终得到的一维核壳结构导热填料中氮化硼的含量为20wt%,命名为SiO2@BNNS 20wt%。Example 2: This example provides the preparation of a one-dimensional core-shell structure thermally conductive filler. The method steps are the same as Example 1. The difference is that the mass of boron nitride added in step two is 9g; the injection speed in step four is is 0.4mm/min, the receiving distance is 25cm, and the voltage is 24kV (negative voltage -12kV, positive voltage +12kV). The content of boron nitride in the finally obtained one-dimensional core-shell structure thermal conductive filler is 20wt%, named SiO 2 @BNNS 20wt%.

实施例3:本实施例提供了一种一维核壳结构导热填料的制备,方法步骤同实施例1,不同之处在于步骤二中加入氮化硼质量为13g;步骤四中推注速度为0.5mm/min,接收距离为25cm,电压为26kV(负极电压-13kV,正极电压13kV),最终得到的一维核壳结构导热填料中氮化硼的含量为30wt%,命名为SiO2@BNNS 30wt%。Example 3: This example provides the preparation of a one-dimensional core-shell structure thermally conductive filler. The method steps are the same as Example 1. The difference is that the mass of boron nitride added in step two is 13g; the injection speed in step four is 0.5mm/min, the receiving distance is 25cm, the voltage is 26kV (negative voltage -13kV, positive voltage 13kV), the content of boron nitride in the finally obtained one-dimensional core-shell structure thermal conductive filler is 30wt%, named SiO 2 @BNNS 30wt%.

实施例4:本实施例提供了一种高导热环氧树脂的制备,包括如下步骤:Embodiment 4: This embodiment provides the preparation of a highly thermally conductive epoxy resin, including the following steps:

S1、将E51型环氧树脂与甲基六氢苯酐固化剂在60℃下混合,得到混合液;S1. Mix E51 epoxy resin and methylhexahydrophthalic anhydride curing agent at 60°C to obtain a mixed solution;

S2、称取实施例1中制得的SiO2@BNNS10wt%的量为2.47g、3.924g、5.559g、7.412g和8.52g(即高导热环氧树脂中SiO2@BNNS10wt%的质量占比分别为10wt%、15wt%、20wt%、25wt%和30wt%)分别与无水乙醇以1500rpm/min的转速搅拌3h,得到一维填料悬浊液;S2. Weigh the SiO 2 @BNNS 10wt% prepared in Example 1 to be 2.47g, 3.924g, 5.559g, 7.412g and 8.52g (i.e. the mass proportion of SiO 2 @BNNS 10wt% in the high thermal conductive epoxy resin (10wt%, 15wt%, 20wt%, 25wt% and 30wt% respectively) were stirred with absolute ethanol at a speed of 1500rpm/min for 3h to obtain a one-dimensional filler suspension;

S3、将一维填料悬浊液与混合液混合,并以1000~1500rpm/min的转速搅拌1~3h,转移至真空烘箱中真空除泡,随后进行热压,得到热固型聚合物复合材料。S3. Mix the one-dimensional filler suspension and the mixed liquid, stir for 1 to 3 hours at a speed of 1000 to 1500 rpm/min, transfer to a vacuum oven for vacuum defoaming, and then perform hot pressing to obtain a thermosetting polymer composite material. .

对比例1:Comparative example 1:

本对比例提供了一种纯环氧树脂的制备,方法步骤同实施例4,不同之处仅在于SiO2@BNNS 10wt%的量为0g,得到纯环氧树脂,其性能参数如表1所示。This comparative example provides a preparation of pure epoxy resin. The method steps are the same as in Example 4. The only difference is that the amount of SiO2@BNNS 10wt% is 0g. Pure epoxy resin is obtained, and its performance parameters are shown in Table 1. .

对比例2:Comparative example 2:

本对比例提供了一种柔性导热膜的制备,方法步骤同实施例4,不同之处仅在于采用用量分别为2.47g、3.924g、5.559g、7.412g和8.52g的二维氮化硼纳米片分别代替实施例1制得的SiO2@BNNS 10wt%,得到高导热环氧树脂,其性能参数如表1所示。This comparative example provides a preparation of a flexible thermally conductive film. The method steps are the same as in Example 4. The only difference is that the amounts of two-dimensional boron nitride nanoparticles used are 2.47g, 3.924g, 5.559g, 7.412g and 8.52g respectively. The sheets were used to replace 10wt% of SiO2@BNNS prepared in Example 1 to obtain a high thermal conductive epoxy resin, whose performance parameters are shown in Table 1.

表1为本实施例所得高导热环氧树脂性能参数;Table 1 shows the performance parameters of the high thermal conductivity epoxy resin obtained in this example;

表1Table 1

表1是SiO2@BNNS10wt%作为填料制得的高导热环氧树脂以及以二维氮化硼纳米片作为填料制得的高导热环氧树脂的性能数据对比表。如表1所示,所有填量下一维填料SiO2@BNNS 10wt%作为导热填料的高导热环氧树脂,其面内和面外导热性能相对于氮化硼纳米片,导热系数有不同程度提升,且仍能保持良好的绝缘性能,因此更适合作为各种材料的导热填料,可以进一步提升聚合材料的导热性能。Table 1 is a comparison table of performance data between high thermal conductivity epoxy resin made with SiO 2 @BNNS 10wt% as filler and high thermal conductivity epoxy resin made with two-dimensional boron nitride nanosheets as filler. As shown in Table 1, all filling amounts of the next-dimensional filler SiO 2 @BNNS 10wt% are used as high thermal conductivity epoxy resins as thermal conductive fillers. Compared with boron nitride nanosheets, their in-plane and out-of-plane thermal conductivity have different thermal conductivity coefficients. It can be improved and still maintain good insulation properties, so it is more suitable as a thermal conductive filler for various materials, which can further improve the thermal conductivity of polymer materials.

图1为实施例1中一维核壳结构导热填料SiO2@BNNS 10wt%的扫描电镜图,图2为实施例2中一维核壳结构导热填料SiO2@BNNS 20wt%的扫描电镜图,图3为实施例3中一维核壳结构导热填料SiO2@BNNS 30wt%的扫描电镜图。Figure 1 is a scanning electron microscope image of the one-dimensional core-shell structure thermally conductive filler SiO 2 @BNNS 10wt% in Example 1. Figure 2 is a scanning electron microscope image of the one-dimensional core-shell structure thermally conductive filler SiO 2 @BNNS 20wt% in Example 2. Figure 3 is a scanning electron microscope image of the one-dimensional core-shell structure thermally conductive filler SiO 2 @BNNS 30wt% in Example 3.

如图1-3所示,可以注意到SiO2@BNNS纤维均匀且具有高长径比。随着SiO2@BNNS纤维中h-BN含量的增加,SiO2@BNNS的纤维直径逐渐增加。同时,煅烧后的SiO2@BNNS纤维随着BNNS含量的增加,纤维的形状变得不再规则,越来越多的BNNS出现在纤维的表面,增加了纤维的粗糙程度。并且高长径比的SiO2@BNNS导热填料更容易在聚合物基体中形成导热通路,同时可以增强导热填料与聚合物基体的相容性,解决了商用氮化硼填料在基体中易团聚的问题。As shown in Figure 1-3, it can be noticed that the SiO 2 @BNNS fibers are uniform and have a high aspect ratio. As the h-BN content in SiO 2 @BNNS fibers increases, the fiber diameter of SiO 2 @BNNS gradually increases. At the same time, as the BNNS content of the calcined SiO 2 @BNNS fiber increases, the shape of the fiber becomes less regular, and more and more BNNS appear on the surface of the fiber, increasing the roughness of the fiber. Moreover, the high aspect ratio SiO 2 @BNNS thermally conductive filler is easier to form a thermal conductive path in the polymer matrix, and at the same time can enhance the compatibility between the thermally conductive filler and the polymer matrix, solving the problem that commercial boron nitride filler is easy to agglomerate in the matrix. question.

Claims (9)

1.一种一维核壳结构导热填料,其特征在于所述的一维核壳结构导热填料由氮化硼纳米片以及包裹在氮化硼纳米片外的二氧化硅层组成,一维核壳结构导热填料中氮化硼纳米片的质量分数为10~80%,所述的氮化硼纳米片的粒径为50nm~10um。1. A one-dimensional core-shell structure thermally conductive filler, characterized in that the one-dimensional core-shell structure thermally conductive filler is composed of boron nitride nanosheets and a silicon dioxide layer wrapped outside the boron nitride nanosheets. The one-dimensional core The mass fraction of boron nitride nanosheets in the shell structure thermally conductive filler is 10 to 80%, and the particle size of the boron nitride nanosheets is 50 nm to 10um. 2.如权利要求1所述的一种一维核壳结构导热填料的制备方法,其特征在于该制备方法按以下步骤进行:2. The preparation method of a one-dimensional core-shell structure thermally conductive filler as claimed in claim 1, characterized in that the preparation method is carried out according to the following steps: 步骤一:将正硅酸乙酯、氨水、乙醇和去离子水混合,搅拌均匀后,得到二氧化硅前驱体溶胶;Step 1: Mix ethyl orthosilicate, ammonia, ethanol and deionized water, and stir evenly to obtain a silica precursor sol; 步骤二:将聚乙烯醇、氮化硼纳米片和乙醇混合,搅拌均匀后,得到氮化硼纳米片悬浊液;Step 2: Mix polyvinyl alcohol, boron nitride nanosheets and ethanol, and stir evenly to obtain boron nitride nanosheet suspension; 步骤三:将步骤一中的二氧化硅前驱体溶胶和步骤二中的氮化硼纳米片悬浊液搅拌均匀,得到纺丝液;Step 3: Stir the silica precursor sol in step 1 and the boron nitride nanosheet suspension in step 2 evenly to obtain a spinning solution; 步骤四:将步骤三中的纺丝液真空除泡,进行静电纺丝,得到纤维膜;Step 4: Vacuum defoaming the spinning solution in Step 3, and perform electrospinning to obtain a fiber membrane; 步骤五:将步骤四中的纤维膜煅烧,研磨,得到一维核壳结构导热填料,所述的一维核壳结构导热填料中氮化硼纳米片的质量分数为10%、20%或30%。Step 5: Calculate and grind the fiber membrane in Step 4 to obtain a one-dimensional core-shell structure thermally conductive filler. The mass fraction of boron nitride nanosheets in the one-dimensional core-shell structure thermally conductive filler is 10%, 20% or 30%. %. 3.根据权利要求2所述的一种一维核壳结构导热填料的制备方法,其特征在于步骤一中正硅酸乙酯、氨水、乙醇与去离子水的体积比为(10~15):(15~30):(15~30):(5~10),所述的正硅酸乙酯的浓度为0.1~4mol/L,所述的氨水的浓度为0.5~2mol/L,所述乙醇的浓度为5~20mol/L。3. A method for preparing a one-dimensional core-shell structure thermally conductive filler according to claim 2, characterized in that the volume ratio of ethyl orthosilicate, ammonia water, ethanol and deionized water in step one is (10~15): (15~30): (15~30): (5~10), the concentration of the ethyl orthosilicate is 0.1~4mol/L, the concentration of the ammonia water is 0.5~2mol/L, the The concentration of ethanol is 5~20mol/L. 4.根据权利要求2所述的一种一维核壳结构导热填料的制备方法,其特征在于步骤二中聚乙烯醇、氮化硼纳米片与乙醇的质量比为3:1:(5~10)。4. The preparation method of a one-dimensional core-shell structure thermally conductive filler according to claim 2, characterized in that the mass ratio of polyvinyl alcohol, boron nitride nanosheets and ethanol in step two is 3:1: (5~ 10). 5.根据权利要求2所述的一种一维核壳结构导热填料的制备方法,其特征在于步骤三中二氧化硅前驱体溶胶与氮化硼纳米片悬浊液的质量比为1:(2~10)。5. The preparation method of a one-dimensional core-shell structure thermally conductive filler according to claim 2, characterized in that the mass ratio of the silicon dioxide precursor sol and the boron nitride nanosheet suspension in step three is 1: ( 2~10). 6.根据权利要求2所述的一种一维核壳结构导热填料的制备方法,其特征在于步骤一中的搅拌时间为3~8h,步骤二中的搅拌时间为1~3h,步骤三中的搅拌时间为3~8h。6. A method for preparing a one-dimensional core-shell structure thermally conductive filler according to claim 2, characterized in that the stirring time in step one is 3~8h, the stirring time in step two is 1~3h, and in step three The stirring time is 3~8h. 7.根据权利要求2所述的一种一维核壳结构导热填料的制备方法,其特征在于步骤四中静电纺丝采用静电纺丝机,纺丝参数如下:不锈钢针头内径为0.17~3.5mm;正极板电压为5~30kV,负极板电压为5~30kV;针头平移速度为50~100mm/min;推注速度为0.3~1mm/s,接收距离为15~25cm。7. A method for preparing a one-dimensional core-shell structure thermally conductive filler according to claim 2, characterized in that the electrospinning in step four adopts an electrostatic spinning machine, and the spinning parameters are as follows: the inner diameter of the stainless steel needle is 0.17~3.5mm. ; The positive plate voltage is 5~30kV, the negative plate voltage is 5~30kV; the needle translation speed is 50~100mm/min; the bolus speed is 0.3~1mm/s, and the receiving distance is 15~25cm. 8.根据权利要求2所述的一种一维核壳结构导热填料的制备方法,其特征在于步骤四中静电纺丝后,置于60~100℃的烘箱中干燥1~3h;步骤五中煅烧步骤如下:先以5~15℃/min的升温速率升温至400~600℃,并在400~600℃下保温0.5~2 h;保温结束后以5~15℃/min的升温速率继续升温至600~1300℃,并在600~1300℃下保温2~4 h。8. A method for preparing a one-dimensional core-shell structure thermally conductive filler according to claim 2, characterized in that after electrospinning in step four, it is placed in an oven at 60 to 100°C for drying for 1 to 3 hours; in step five, The calcination steps are as follows: first heat up to 400~600°C at a heating rate of 5~15°C/min, and keep it at 400~600°C for 0.5~2 h; after the insulation, continue to heat up at a heating rate of 5~15°C/min. to 600~1300℃, and keep at 600~1300℃ for 2~4 hours. 9.如权利要求1所述的一种一维核壳结构导热填料的应用,其特征在于所述的一维核壳结构导热填料用于制备热塑型或热固型聚合物复合材料,所述的热固型聚合物复合材料的制备方法如下:9. The application of a one-dimensional core-shell structure thermally conductive filler as claimed in claim 1, characterized in that the one-dimensional core-shell structure thermally conductive filler is used to prepare thermoplastic or thermosetting polymer composite materials, so The preparation method of the thermosetting polymer composite material is as follows: S1、将环氧树脂与固化剂在50~80℃下混合,得到混合液;所述的环氧树脂为E51型环氧树脂,所述的固化剂为甲基六氢苯酐;S1. Mix the epoxy resin and the curing agent at 50~80°C to obtain a mixed liquid; the epoxy resin is E51 type epoxy resin, and the curing agent is methylhexahydrophthalic anhydride; S2、将一维核壳结构导热填料与有机溶剂混合,并以500~1500rpm/min的转速搅拌1~3h,得到一维填料悬浊液;所述的有机溶剂为乙醇或叔丁醇;S2. Mix the one-dimensional core-shell structure thermally conductive filler with an organic solvent, and stir for 1 to 3 hours at a speed of 500 to 1500 rpm/min to obtain a one-dimensional filler suspension; the organic solvent is ethanol or tert-butanol; S3、将一维填料悬浊液与混合液混合,并以1000~1500rpm/min的转速搅拌1~3h,真空除泡后热压,得到热固型聚合物复合材料,所述的热固型聚合物复合材料中一维核壳结构导热填料的质量分数为10%、15%、20%、25%或30%。S3. Mix the one-dimensional filler suspension and the mixed liquid, stir for 1 to 3 hours at a speed of 1000 to 1500 rpm/min, vacuum defoaming and hot pressing to obtain a thermosetting polymer composite material. The thermosetting polymer composite material The mass fraction of the one-dimensional core-shell structure thermally conductive filler in the polymer composite is 10%, 15%, 20%, 25% or 30%.
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Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2860008A1 (en) * 2013-10-14 2015-04-15 Esk Ceramics GmbH&Co. Kg Components produced by the thermoplastic processing of polymer boron nitride compounds, polymer boron nitride compounds for producing such components, method for producing such components and use of the same
CN108946797A (en) * 2018-09-05 2018-12-07 河南工程学院 The barium titanate@boron nitride composite and preparation method of one-dimensional nucleocapsid structure
CN109503889A (en) * 2018-12-17 2019-03-22 安徽大学 A kind of preparation method of silver nanowires hydridization filler and composite material using the filler
CN110218390A (en) * 2019-06-13 2019-09-10 合肥工业大学 A kind of PP composite material with the filling of core-shell structure heat filling
CN110452418A (en) * 2019-09-25 2019-11-15 桂林电子科技大学 A kind of high thermal conductivity Kapton and preparation method thereof of core-shell structure heat filling preparation
CN110628080A (en) * 2019-09-26 2019-12-31 中国石油大学(北京) A kind of three-dimensional thermally conductive filler and its preparation method and application
CN110734644A (en) * 2019-06-24 2020-01-31 上海大学 heat-conducting insulating boron nitride polymer composite material and preparation method thereof
CN110951254A (en) * 2019-11-24 2020-04-03 上海大学 Boron nitride composite high-thermal-conductivity insulating polymer composite material and preparation method thereof
CN112500650A (en) * 2020-10-20 2021-03-16 南京工业大学 Low-cost polymer-based heat-conducting and insulating composite material and preparation method thereof
CN112876741A (en) * 2021-01-19 2021-06-01 湖南柯盛新材料有限公司 Boron nitride heterogeneous filler and preparation method thereof, fiber-reinforced epoxy resin heat-conducting composite material and preparation method and application thereof
CN113087971A (en) * 2021-04-07 2021-07-09 广东思泉新材料股份有限公司 Heterostructure heat-conducting filler, preparation method and application thereof, silicon rubber heat-conducting and insulating composite material and preparation method thereof

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2860008A1 (en) * 2013-10-14 2015-04-15 Esk Ceramics GmbH&Co. Kg Components produced by the thermoplastic processing of polymer boron nitride compounds, polymer boron nitride compounds for producing such components, method for producing such components and use of the same
CN108946797A (en) * 2018-09-05 2018-12-07 河南工程学院 The barium titanate@boron nitride composite and preparation method of one-dimensional nucleocapsid structure
CN109503889A (en) * 2018-12-17 2019-03-22 安徽大学 A kind of preparation method of silver nanowires hydridization filler and composite material using the filler
CN110218390A (en) * 2019-06-13 2019-09-10 合肥工业大学 A kind of PP composite material with the filling of core-shell structure heat filling
CN110734644A (en) * 2019-06-24 2020-01-31 上海大学 heat-conducting insulating boron nitride polymer composite material and preparation method thereof
CN110452418A (en) * 2019-09-25 2019-11-15 桂林电子科技大学 A kind of high thermal conductivity Kapton and preparation method thereof of core-shell structure heat filling preparation
CN110628080A (en) * 2019-09-26 2019-12-31 中国石油大学(北京) A kind of three-dimensional thermally conductive filler and its preparation method and application
CN110951254A (en) * 2019-11-24 2020-04-03 上海大学 Boron nitride composite high-thermal-conductivity insulating polymer composite material and preparation method thereof
CN112500650A (en) * 2020-10-20 2021-03-16 南京工业大学 Low-cost polymer-based heat-conducting and insulating composite material and preparation method thereof
CN112876741A (en) * 2021-01-19 2021-06-01 湖南柯盛新材料有限公司 Boron nitride heterogeneous filler and preparation method thereof, fiber-reinforced epoxy resin heat-conducting composite material and preparation method and application thereof
CN113087971A (en) * 2021-04-07 2021-07-09 广东思泉新材料股份有限公司 Heterostructure heat-conducting filler, preparation method and application thereof, silicon rubber heat-conducting and insulating composite material and preparation method thereof

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