WO2018219000A1 - 一种高导热的聚酰亚胺基复合碳膜及其制备方法 - Google Patents
一种高导热的聚酰亚胺基复合碳膜及其制备方法 Download PDFInfo
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- WO2018219000A1 WO2018219000A1 PCT/CN2018/077316 CN2018077316W WO2018219000A1 WO 2018219000 A1 WO2018219000 A1 WO 2018219000A1 CN 2018077316 W CN2018077316 W CN 2018077316W WO 2018219000 A1 WO2018219000 A1 WO 2018219000A1
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- polyimide
- carbon film
- graphene oxide
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- pressure
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Definitions
- the invention relates to a novel heat conductive material and method, in particular to a method for preparing a high thermal conductivity polyimide-based carbon film and a graphene/polyimide composite carbon film with a large thickness by using a graphene oxide adhesive.
- the characteristics of the carbon film are light specific gravity, acid and alkali resistance, organic solvent resistance, good heat transfer and electrical conductivity, thermal shock resistance, wear resistance, self-lubricity, mechanical processing and biocompatibility, and high anisotropy. Therefore, it is widely used in the field of space technology, nuclear industry, and electronic information technology.
- carbon film is mainly prepared by chemical vapor deposition and high molecular carbonization.
- the main disadvantage of chemical vapor deposition is that it is more expensive, and it takes a long period of time to deposit a thicker carbon film, which is technically difficult to achieve.
- the preparation of carbon film material by polymer carbonization is a promising method. The process is simple, the energy consumption is small, and the prepared film has a compact structure and good mechanical strength.
- polyimide As a synthetic resin containing a large number of aromatic heterocyclic structures, polyimide has a high carbonization yield, a compact structure, and a good molding process, and can be prepared into complex components such as films, blocks, and shaped bodies, but At present, there are still problems such as high carbonization temperature, large energy consumption, long carbonization cycle, low carbonization rate of carbonized film, and large brittleness and fragility of the prepared carbonized film.
- a highly thermally conductive carbon film prepared by a polymer carbonization method generally has a thickness of 10 ⁇ m to 100 ⁇ m, and a polyimide-based carbon film or a block having a thickness of more than 100 ⁇ m is sized due to carbonization and graphitization.
- the shrinkage is severe, the internal stress is too large, the carbonization rate is not high, and the graphite sheet spacing is too large or uneven, and the thermal conductivity is usually not higher than 800 W/mK.
- the object of the present invention is to overcome the deficiencies of the prior art and to provide a highly thermally conductive polyimide-based composite carbon film and a preparation method thereof.
- a highly thermally conductive polyimide-based composite carbon film the prepared polyimide carbon-based composite carbon film has a thickness of more than 100 ⁇ m and a porosity of 10 to 40%. There is no delamination, and the spacing between any two adjacent graphite sheets is less than 20 nm.
- preparation method comprises the following steps:
- Graphene oxide having an average size of more than 50 ⁇ m is formulated into an aqueous solution of graphene oxide having a concentration of 1 to 10 mg/mL.
- step 2 compounding a plurality of the polyimide-based carbon films in the step 2, specifically: uniformly coating the graphene oxide solution in the step 1 on the surface of the polyimide-based carbon film, and then applying a plurality of polyacyl groups The imine carbon film is bonded together in the thickness direction.
- the bonded polyimide-based composite carbon film is placed in an oven to be dried, and the temperature of the oven is lower than or equal to 40 °C.
- the dried polyimide-based composite carbon film is placed in a hot pressing chamber of a hot press, heated to a temperature of 0.1 to 5 ° C/min to 200 ° C, and then hot pressed, and the following hot pressing process is repeated.
- 1 ⁇ 5 times maintain the pressure 20MPa, maintain 1h; gradually release the pressure to 0MPa, vacuum the hot pressure chamber for 5min to a vacuum of -100 ⁇ 10KPa; then increase the temperature by 300°C at a rate of 0.1 ⁇ 5°C/min, keep warm 0.5h, then hot pressing, repeat the following hot pressing process 1 ⁇ 5 times: maintain the pressure 60MPa, maintain 1h, gradually release the pressure to 0MPa, vacuum the hot pressure chamber for 5min to the vacuum degree -100 ⁇ 10KPa; hot pressing process Naturally cool down after the end.
- step 5 The polyimide-based composite carbon film after hot pressing in step 5 is heated at a rate of 1-20 ° C / min to 2400 ⁇ 3000 ° C under an inert gas atmosphere for further hot pressing, holding pressure for 0.5 ⁇ 8h; The pressure is 60 MPa. After the temperature reduction is pressed, a highly thermally conductive polyimide-based composite carbon film is obtained.
- a highly thermally conductive graphene/polyimide composite carbon film prepared by using a graphene/polyimide composite carbon film having a thickness of more than 100 ⁇ m, a porosity of 10 to 40%, and a thermal conductivity of 1000 to 1700 W. /mK.
- the obtained graphene/polyimide composite carbon film has no delamination, and the spacing between any two adjacent graphite sheets is less than 20 nm.
- the preparation method of the high thermal conductivity graphene/polyimide composite carbon film comprises the following steps:
- Graphene oxide having an average size of more than 50 ⁇ m is formulated into an aqueous solution of graphene oxide having a concentration of 1 to 10 mg/mL.
- the dried graphene oxide/polyimide composite film is placed in a carbonization furnace under an argon atmosphere, and is gradually heated to 1000 ° C at a rate of 0.1 to 10 ° C/min for heat treatment, and every 100 ° C At a constant temperature of 1 h, the whole process maintains a pressure of 20 MPa to 200 MPa.
- the graphene/polyimide composite carbon film after hot pressing in step 5 is heated to a temperature of 1-20 ° C/min under an inert gas atmosphere to 2500 to 3000 ° C for further hot pressing, and the holding pressure is 0.5 to 0.5. 8h; pressure is 60MPa. After cooling and pressing, a highly thermally conductive graphene oxide/polyimide composite carbon film is obtained.
- the graphene oxide of the step 1 has a carbon to oxygen ratio of 1.8 to 2.1.
- a layer of a graphene oxide aqueous solution having a concentration of 1 to 10 mg/mL is uniformly sprayed on the surface thereof, and then a plurality of polyimide-based carbon films are applied in the thickness direction. Bonded together, after drying, the polyimide-based carbon film can be bonded by graphene oxide, and the bonding between the polyimide-based carbon films is further tightened by further low-temperature hot pressing, and finally the high temperature is passed.
- the high-pressure hot-pressing method improves the degree of graphitization of the carbon film, repairs the structural defects, improves the orientation of the graphite sheet, and makes the carbon film form a three-dimensional graphite structure to the highest degree, ensuring the smooth conduction of the heat conduction path and obtaining a highly thermally conductive polymer.
- An imide-based composite carbon film is an imide-based composite carbon film.
- Figure 1 is a SEM cross-sectional view of a polyimide composite film bonded using an aqueous solution of 4 mg/mL graphene oxide.
- the invention discloses a method for preparing a highly thermally conductive polyimide composite carbon film by utilizing the adhesion property of graphene oxide.
- the polyimide-based carbon film is subjected to hydrophilic treatment, and a layer of a graphene oxide aqueous solution having a concentration of 1 to 10 mg/mL is uniformly sprayed on the surface thereof, and then more
- the polyimide-based carbon film is bonded together in the thickness direction, and after drying, the polyimide-based carbon film can be bonded by graphene oxide, and the polyimide-based carbon film is further pressed by further low-temperature hot pressing.
- the inter-bonding is more compact, and finally the high-temperature and high-pressure hot-pressing treatment method is adopted to increase the degree of graphitization of the carbon film, repair the structural defects, and improve the orientation of the graphite sheet, so that the carbon film forms the three-dimensional graphite structure to the highest degree, ensuring
- the heat conduction path is smooth, and a highly thermally conductive polyimide-based composite carbon film is obtained. Its thickness is more than 100 ⁇ m, the porosity is 10 ⁇ 40%, and the thermal conductivity is 1000 ⁇ 1700W/mK, which has great practical value.
- the invention also discloses a method for preparing a graphene/polyimide composite carbon film by utilizing the adhesion property of graphene oxide.
- a method for preparing a graphene/polyimide composite carbon film by utilizing the adhesion property of graphene oxide.
- the junction is further carbonized by relatively low-temperature hot pressing, and further graphitized by high-temperature and high-pressure hot pressing treatment to form a three-dimensionally ordered graphite layer structure and a relatively complete graphite crystal, thereby ensuring the smooth flow of the heat conduction path.
- a highly thermally conductive graphene/polyimide composite carbon film is obtained. Its thickness is more than 100 ⁇ m, the porosity is 10 ⁇ 40%, and the thermal conductivity is 1000 ⁇ 1700W/mK, which has great practical value.
- Graphene oxide having an average size of more than 50 ⁇ m is formulated into an aqueous solution of graphene oxide having a concentration of 4 mg/mL.
- the dried polyimide-based composite carbon film is placed in a hot pressing chamber of a hot press, heated to a temperature of 0.1 ° C/min to 200 ° C, and then hot pressed, and the following hot pressing process is repeated once. : Maintain the pressure of 20MPa for 1h; gradually release the pressure to 0MPa, vacuum the hot pressure chamber for 5min to a vacuum of -100KPa; then heat the temperature to 300 °C at a rate of 0.1 °C / min, hold for 0.5h, then hot press. Repeat the following hot pressing process once: maintain the pressure of 60MPa, maintain 1h, gradually release the pressure to 0MPa, vacuum the hot pressure chamber for 5min to a vacuum of -100KPa; natural cooling after the end of the hot pressing process.
- the polyimide-based composite carbon film which was hot-pressed in the step 5 was heated to 2400 ° C at a rate of 1 ° C/min under an inert gas atmosphere for further hot pressing, and the holding pressure was maintained for 8 hours; the pressure was 60 MPa. After the temperature reduction is pressed, a highly thermally conductive polyimide-based composite carbon film is obtained.
- the polyimide-based carbon film first forms a monolithic structure by the adhesion of graphene oxide, and further improves the degree of graphitization after further low-temperature hot pressing and high-temperature hot pressing repair defects, thereby finally obtaining a highly thermally conductive polyimide.
- Base composite carbon film first forms a monolithic structure by the adhesion of graphene oxide, and further improves the degree of graphitization after further low-temperature hot pressing and high-temperature hot pressing repair defects, thereby finally obtaining a highly thermally conductive polyimide.
- the original polyimide-based carbon film was tested to have a thickness of 25 ⁇ m, a density of 2.01 g/cm 3 , a porosity of 8.6%, and a thermal conductivity of 1763.2 W/mK; at this time, a polyimide-based composite carbon film The thickness is 106 ⁇ m, the density is 1.98 g/cm 3 , the porosity is 10%, and the thermal conductivity is 1702.4 W/mK. As shown in FIG. 1 , the polyimide-based composite carbon film has no delamination, any two phases. The adjacent graphite sheet spacing is less than 20 nm.
- Graphene oxide having an average size of more than 50 ⁇ m is formulated into an aqueous solution of graphene oxide having a concentration of 4 mg/mL.
- hot pressing After heating at a rate of 5 ° C / min to 200 ° C, hot pressing, repeat the following hot pressing process 5 times: maintain the pressure 20MPa, maintain 1h; gradually release the pressure to 0MPa, vacuum the hot pressure chamber for 5min to vacuum Is 10KPa;
- the polyimide-based composite carbon film which was hot-pressed in the step 5 was heated to 3000 ° C at a rate of 20 ° C / min under an inert gas atmosphere for further hot pressing, and the holding pressure was maintained for 0.5 h; the pressure was 60 MPa. After cooling and pressing, the obtained polyimide-based composite carbon film was obtained.
- the polyimide-based composite carbon film has a thickness of 260 ⁇ m, a density of 1.88 g/cm 3 , a porosity of 14.5%, and a thermal conductivity of 1632.5 W/mK, and the polyimide-based composite carbon.
- the film has no delamination, and the spacing between any two adjacent graphite sheets is not less than 20 nm.
- Graphene oxide having an average size of more than 50 ⁇ m is formulated into an aqueous solution of graphene oxide having a concentration of 1 mg/mL.
- the dried polyimide-based composite carbon film is placed in a hot press chamber of a hot press, heated at a rate of 2 ° C/min to 200 ° C, and then hot pressed, and the following hot pressing process is repeated 5 times.
- Repeat the following hot pressing process 5 times maintain the pressure 60 MPa, maintain 1 h, gradually release the pressure to 0 MPa, vacuum the hot pressure chamber for 5 min to a vacuum of -50 KPa; natural cooling after the end of the hot pressing process.
- the polyimide-based composite carbon film which was hot-pressed in the step 5 was heated to 2800 ° C at a rate of 5 ° C/min under an inert gas atmosphere for further hot pressing, and the holding pressure was maintained for 2 hours; the pressure was 60 MPa. After cooling and pressing, the obtained polyimide-based composite carbon film was obtained.
- the polyimide-based composite carbon film has a thickness of 258 ⁇ m, a density of 1.85 g/cm 3 , a porosity of 15.9%, and a thermal conductivity of 1615.2 W/mK, and the polyimide-based composite carbon.
- the film has no delamination, and the spacing between any two adjacent graphite sheets is not less than 20 nm.
- Graphene oxide having an average size of more than 50 ⁇ m is formulated into an aqueous solution of graphene oxide having a concentration of 10 mg/mL.
- the dried polyimide-based composite carbon film is placed in a hot press chamber of a hot press, heated at a rate of 2 ° C/min to 200 ° C, and then hot pressed, and the following hot pressing process is repeated 5 times.
- Repeat the following hot pressing process 5 times maintain the pressure 60 MPa, maintain 1 h, gradually release the pressure to 0 MPa, vacuum the hot pressure chamber for 5 min to a vacuum of -50 KPa; natural cooling after the end of the hot pressing process.
- the polyimide-based composite carbon film which was hot-pressed in the step 5 was heated to 2800 ° C at a rate of 5 ° C/min under an inert gas atmosphere for further hot pressing, and the holding pressure was maintained for 2 hours; the pressure was 60 MPa. After cooling and pressing, the obtained polyimide-based composite carbon film was obtained.
- the polyimide-based composite carbon film has a thickness of 271 ⁇ m, a density of 1.84 g/cm 3 , a porosity of 16.4%, and a thermal conductivity of 1595.2 W/mK, and the polyimide-based composite carbon.
- the film has no delamination, and the spacing between any two adjacent graphite sheets is not less than 20 nm.
- Graphene oxide having an average size of more than 50 ⁇ m is formulated into an aqueous solution of graphene oxide having a concentration of 4 mg/mL.
- a plurality of polyimide-based carbon films treated with the size of 5 cm*5 cm are subjected to the step 2 to be composited, specifically: uniformly coating the graphite oxide in the step 1 on the surface of the polyimide-based carbon film.
- the olefin solution is then bonded to a plurality of polyimide-based carbon films in the thickness direction.
- the dried polyimide-based composite carbon film is placed in a hot press chamber of a hot press, heated at a rate of 2 ° C/min to 200 ° C, and then hot pressed, and the following hot pressing process is repeated 5 times.
- Repeat the following hot pressing process 5 times maintain the pressure 60 MPa, maintain 1 h, gradually release the pressure to 0 MPa, vacuum the hot pressure chamber for 5 min to a vacuum of -50 KPa; natural cooling after the end of the hot pressing process.
- the polyimide-based composite carbon film which was hot-pressed in the step 5 was heated to 2800 ° C at a rate of 5 ° C/min under an inert gas atmosphere for further hot pressing, and the holding pressure was maintained for 2 hours; the pressure was 60 MPa. After the temperature reduction is pressed, a highly thermally conductive polyimide-based composite carbon film is obtained.
- the polyimide-based carbon film first forms a monolithic structure by the adhesion of graphene oxide, and further improves the degree of graphitization after further low-temperature hot pressing and high-temperature hot pressing repair defects, thereby finally obtaining a highly thermally conductive polyimide.
- Base composite carbon film After testing, the polyimide-based composite carbon film has a thickness of 3.17 m, a density of 1.54 g/cm 3 , a porosity of 30%, and a thermal conductivity of 1249.5 W/mK.
- the polyimide-based composite carbon film has no Layering phenomenon, the spacing between any two adjacent graphite sheets is less than 20 nm.
- Graphene oxide having an average size of more than 50 ⁇ m is formulated into an aqueous solution of graphene oxide having a concentration of 4 mg/mL.
- the dried graphene oxide/polyimide composite film is placed in a carbonization furnace under an argon atmosphere, and is gradually heated to a temperature of 1000 ° C at a rate of 5 ° C/min for heat treatment, and is kept at a constant temperature every 100 ° C. 1h, the whole process maintained a pressure of 20MPa.
- the polyimide film first forms a monolithic structure by the adhesion of graphene oxide, and further increases the degree of graphitization by further relatively low-temperature hot-pressure heat treatment to make carbonization and high-temperature hot-pressure repair defects, and finally obtains a highly thermally conductive polymer.
- An imide-based composite carbon film An imide-based composite carbon film.
- the original polyimide-based carbon film was tested to have a thickness of 31 ⁇ m, a density of 2.03 g/cm 3 , a porosity of 7.7%, and a thermal conductivity of 1733.2 W/mK; at this time, graphene/polyimide composite carbon
- the film has a thickness of 126 ⁇ m, a density of 1.97 g/cm 3 , a porosity of 10.5%, and a thermal conductivity of 1697.5 W/mK.
- the polyimide-based composite carbon film has no delamination, and any two adjacent graphite sheets. The layer spacing is less than 20 nm.
- Graphene oxide having an average size of more than 50 ⁇ m is formulated into an aqueous solution of graphene oxide having a concentration of 4 mg/mL.
- the dried graphene oxide/polyimide composite film is placed in a carbonization furnace under an argon atmosphere, and is gradually heated to 1000 ° C at a rate of 2 ° C/min for heat treatment, and is kept at a constant temperature every 100 ° C. 1h, the whole process maintained a pressure of 60MPa.
- the polyimide film first forms a monolithic structure by the adhesion of graphene oxide, and further increases the degree of graphitization by further relatively low-temperature hot-pressure heat treatment to make carbonization and high-temperature hot-pressure repair defects, and finally obtains a highly thermally conductive polymer.
- An imide-based composite carbon film The graphene/polyimide composite carbon film has been tested to have a thickness of 1.76 mm, a density of 1.82 g/cm 3 , a porosity of 17.3%, and a thermal conductivity of 1387.3 W/mK.
- This graphene/polyimide composite The carbon film has no delamination, and the spacing between any two adjacent graphite sheets is less than 20 nm.
Abstract
本发明公开了一种高导热的聚酰亚胺基复合碳膜及其制备方法。将聚酰亚胺基碳膜表面均匀涂覆一层氧化石墨烯水溶液,再覆盖另一张同样均匀涂覆了一层氧化石墨烯水溶液的聚酰亚胺基碳膜,反复此操作,待其干燥后,聚酰亚胺基碳膜之间通过氧化石墨烯实现粘接从而形成厚膜。通过进一步低温热压使得聚酰亚胺基碳膜之间粘结更加紧实,最终经过低温加热预还原,高温高压热处理修复缺陷即可得到高导热的聚酰亚胺基厚碳膜。该高导热的聚酰亚胺基厚碳膜的厚度大于100μm,面向热导率甚至能达到1700W/mK以上,在高频率高热流密度器件中有较大的使用前景。
Description
本发明涉及新型导热材料及方法,尤其涉及一种利用氧化石墨烯粘接剂制备厚度较大的高导热的聚酰亚胺基碳膜和石墨烯/聚酰亚胺复合碳膜。
碳膜的特性是比重轻、耐酸碱、耐有机溶剂,传热和导电性好,耐热冲击、耐磨损,自润滑性、机械加工性和生体相容性好、异向性大。因而,在空间技术领域、核工业、电子信息技术领域等被广泛应用。
目前主要采用化学气相沉积和高分子碳化法制备碳膜。化学气相沉积的主要缺点是成本较贵,同时沉积较厚的碳膜需要很长的周期,技术上很难实现。高分子碳化法制备碳膜材料是一种很有前景的方法,工艺简单,能耗少,制备的薄膜结构紧密,有很好的力学强度。聚酰亚胺作为一种含有大量芳香杂环结构的合成树脂,具有碳化产率较高,结构致密,同时具有很好的成型工艺,可以制备成薄膜、块体、异型体等复杂构件,但是目前仍然存碳化温度高、耗能大、碳化周期长、碳化膜碳化率较低,制备的碳化膜脆性较大且易碎等问题。
但是目前,经过高分子碳化法制备的高导热的碳膜通常厚度为10μm~100μm,而厚度在一百微米以上的聚酰亚胺基碳膜或者块材,由于在碳化和石墨化过程中尺寸收缩严重、内应力太大、碳化率不高以及其中的石墨片层间距偏大或不均匀等问题,其面向导热率通常不高于800W/mK。
发明内容
本发明的目的是克服现有技术的不足,提供一种高导热的聚酰亚胺基复合碳膜及其制备方法。
本发明的目的是通过以下技术方案实现的:一种高导热的聚酰亚胺基复合碳膜,所制备的聚酰亚胺碳基复合碳膜的厚度大于100μm,孔隙率为10~40%,无分层现象,任意两个相邻的石墨片层间距小于20nm。
进一步地,所述制备方法包含如下步骤:
(1)将平均尺寸大于50μm的氧化石墨烯配制成浓度为1~10mg/mL氧化石墨烯水溶液。
(2)将商用聚酰亚胺基碳膜进行氧等离子体进行处理,使之具有亲水性。
(3)将多张步骤2中的聚酰亚胺基碳膜进行复合,具体为:在聚酰亚胺 基碳膜表面均匀涂覆步骤1中的氧化石墨烯溶液,然后将多张聚酰亚胺基碳膜沿厚度方向粘接在一起。
(4)将粘接后的聚酰亚胺基复合碳膜放置在烘箱烘干,烘箱的温度低于等于40℃。
(5)将烘干后的聚酰亚胺基复合碳膜置于热压机的热压腔中,以0.1~5℃/min的速率升温到200℃后进行热压,重复以下热压过程1~5次:维持压力20MPa,维持1h;逐渐释放压力至0MPa,对热压腔抽真空5min至真空度为-100~10KPa;然后再以0.1~5℃/min的速率升温300℃,保温0.5h,然后进行热压,重复以下热压过程1~5次:维持压力60MPa,维持1h,逐渐释放压力至0MPa,对热压腔抽真空5min至真空度为-100~10KPa;热压过程结束后自然降温。
(6)将步骤5热压后的聚酰亚胺基复合碳膜在惰性气体氛围下以1-20℃/min的速率升温到2400~3000℃进行进一步热压,保温保压0.5~8h;压力为60MPa。降温压制后,得到高导热的聚酰亚胺基复合碳膜。
一种高导热的石墨烯/聚酰亚胺复合碳膜,所制备的石墨烯/聚酰亚胺复合碳膜的厚度大于100μm,孔隙率为10~40%,面向热导率为1000~1700W/mK。得到的石墨烯/聚酰亚胺复合碳膜无分层现象,任意两个相邻的石墨片层间距小于20nm。
高导热的石墨烯/聚酰亚胺复合碳膜的制备方法包含如下步骤:
(1)将平均尺寸大于50μm的氧化石墨烯配制成浓度为1~10mg/mL氧化石墨烯水溶液。
(2)将多张聚酰亚胺膜进行复合,具体为:在聚酰亚胺膜表面均匀涂覆步骤1中的氧化石墨烯溶液,然后将多张聚酰亚胺膜沿厚度方向粘接在一起。
(3)将粘接后的氧化石墨烯/聚酰亚胺复合膜放置在烘箱烘干,烘箱的温度低于40℃。
(5)将烘干后的氧化石墨烯/聚酰亚胺复合膜置于氩气氛围的碳化炉中,以0.1~10℃/min的速率逐渐升温到1000℃进行热处理,并且每隔100℃,恒温1h,整个过程维持压力20MPa~200MPa。
(6)将步骤5热压后的石墨烯/聚酰亚胺复合碳膜在惰性气体氛围下以1-20℃/min的速率升温到2500~3000℃进行进一步热压,保温保压0.5~8h;压力为60MPa。降温压制后,得到高导热的氧化石墨烯/聚酰亚胺复合碳膜。
进一步地,所述的步骤1的氧化石墨烯的碳氧比1.8~2.1。
本发明将聚酰亚胺基碳膜进行亲水处理后,在其表面均匀喷涂一层浓度 为1~10mg/mL的氧化石墨烯水溶液,然后将多张聚酰亚胺基碳膜沿厚度方向粘接在一起,待其干燥后聚酰亚胺基碳膜可通过氧化石墨烯实现粘结,通过进一步低温热压使得聚酰亚胺基碳膜之间粘结更加紧实,最终再经过高温高压热压处理的方式,提高碳膜的石墨化程度,修复结构缺陷,提高了石墨片的取向程度,使得碳膜最高程度的形成三维石墨结构,保证了导热通路的畅通,得到高导热的聚酰亚胺基复合碳膜。
图1为使用4mg/mL氧化石墨烯水溶液粘接成的聚酰亚胺复合膜的SEM截面图
本发明公开了一种利用氧化石墨烯的粘接性能制备高导热的聚酰亚胺复合碳膜的方法。为实现聚酰亚胺膜的粘结,本发明将聚酰亚胺基碳膜进行亲水处理后,在其表面均匀喷涂一层浓度为1~10mg/mL的氧化石墨烯水溶液,然后将多张聚酰亚胺基碳膜沿厚度方向粘接在一起,待其干燥后聚酰亚胺基碳膜可通过氧化石墨烯实现粘结,通过进一步低温热压使得聚酰亚胺基碳膜之间粘结更加紧实,最终再经过高温高压热压处理的方式,提高碳膜的石墨化程度,修复结构缺陷,提高了石墨片的取向程度,使得碳膜最高程度的形成三维石墨结构,保证了导热通路的畅通,得到高导热的聚酰亚胺基复合碳膜。其厚度大于100μm,孔隙率为10~40%,热导率为1000~1700W/mK,具有很大的实际应用价值。
本发明还公开了一种利用氧化石墨烯的粘接性能制备石墨烯/聚酰亚胺复合碳膜的方法。通过在聚酰亚胺膜表面均匀喷涂一层氧化石墨烯水溶液,然后将多张聚酰亚胺膜沿厚度方向粘接在一起,待其干燥后聚酰亚胺膜可通过氧化石墨烯实现粘结,通过进一步相对低温热压使其碳化,和再经过高温高压热压处理的方式使其石墨化,形成三维有序堆积的石墨层状结构和较为完整的石墨晶体,保证了导热通路的畅通,得到高导热的石墨烯/聚酰亚胺复合碳膜。其厚度大于100μm,孔隙率为10~40%,热导率为1000~1700W/mK,具有很大的实际应用价值。
下面结合附图及实施例对本发明作进一步的描述。本实施例只用于对本发明做进一步的说明,不能理解为对本发明保护范围的限制,本领域的技术人员根据上述发明的内容做出一些非本质的改变和调整,均属于本发明的保护范围。
实施例1:
(1)将平均尺寸大于50μm的氧化石墨烯配制成浓度为4mg/mL氧化石墨烯水溶液。
(2)将厚度为25μm的商用聚酰亚胺基碳膜进行氧等离子体进行处理,使之具有亲水性。
(3)将四张尺寸为10cm*10cm进过步骤2处理后的聚酰亚胺基碳膜进行复合,具体为:在聚酰亚胺基碳膜表面均匀涂覆步骤1中的氧化石墨烯溶液,然后将多张聚酰亚胺基碳膜沿厚度方向粘接在一起。
(4)将粘接后的聚酰亚胺基复合碳膜放置在烘箱烘干,烘箱的温度为40℃。
(5)将烘干后的聚酰亚胺基复合碳膜置于热压机的热压腔中,以0.1℃/min的速率升温到200℃后进行热压,重复以下热压过程1次:维持压力20MPa,维持1h;逐渐释放压力至0MPa,对热压腔抽真空5min至真空度为-100KPa;然后再以0.1℃/min的速率升温300℃,保温0.5h,然后进行热压,重复以下热压过程1次:维持压力60MPa,维持1h,逐渐释放压力至0MPa,对热压腔抽真空5min至真空度为-100KPa;热压过程结束后自然降温。
(6)将步骤5热压后的聚酰亚胺基复合碳膜在惰性气体氛围下以1℃/min的速率升温到2400℃进行进一步热压,保温保压8h;压力为60MPa。降温压制后,得到高导热的聚酰亚胺基复合碳膜。
经过以上步骤,聚酰亚胺基碳膜先通过氧化石墨烯的粘接作用形成整体结构,再经过进一步低温热压和高温热压修复缺陷提高石墨化程度,最终得到高导热的聚酰亚胺基复合碳膜。经测试,原聚酰亚胺基碳膜的厚度为25μm,密度为2.01g/cm
3,孔隙率为8.6%,导热率为1763.2W/mK;此时,聚酰亚胺基复合碳膜的厚度为106μm,密度为1.98g/cm
3,孔隙率为10%,导热率为1702.4W/mK,如图1所示,此聚酰亚胺基复合碳膜无分层现象,任意两个相邻的石墨片层间距小于20nm。
实施例2:
(1)将平均尺寸大于50μm的氧化石墨烯配制成浓度为4mg/mL氧化石墨烯水溶液。
(2)将厚度为25μm的商用聚酰亚胺基碳膜进行氧等离子体进行处理,使之具有亲水性。
(3)将十张尺寸为10cm*10cm进过步骤2处理后的聚酰亚胺基碳膜进行复合,具体为:在聚酰亚胺基碳膜表面均匀涂覆步骤1中的氧化石墨烯溶液,然后将多张聚酰亚胺基碳膜沿厚度方向粘接在一起。
(4)将粘接后的聚酰亚胺基复合碳膜放置在烘箱烘干,烘箱的温度为40℃。
(5)将烘干后的聚酰亚胺基复合碳膜置于热压机的热压腔中,进行以下处理:
(5.1)以5℃/min的速率升温到200℃后进行热压,重复以下热压过程5次:维持压力20MPa,维持1h;逐渐释放压力至0MPa,对热压腔抽真空5min至真空度为10KPa;
(5.2)然后再以5℃/min的速率升温300℃,保温0.5h,然后进行热压,重复以下热压过程5次:维持压力60MPa,维持1h,逐渐释放压力至0MPa,对热压腔抽真空5min至真空度为10KPa;
热压过程结束后自然降温。
(6)将步骤5热压后的聚酰亚胺基复合碳膜在惰性气体氛围下以20℃/min的速率升温到3000℃进行进一步热压,保温保压0.5h;压力为60MPa。降温压制后,得到的聚酰亚胺基复合碳膜。
经过以上步骤,此时,聚酰亚胺基复合碳膜的厚度为260μm,密度为1.88g/cm
3,孔隙率为14.5%,导热率为1632.5W/mK,此聚酰亚胺基复合碳膜无分层现象,任意两个相邻的石墨片层间距不小于20nm。
实施例3:
(1)将平均尺寸大于50μm的氧化石墨烯配制成浓度为1mg/mL氧化石墨烯水溶液。
(2)将厚度为25μm的商用聚酰亚胺基碳膜进行氧等离子体进行处理,使之具有亲水性。
(3)将十张尺寸为10cm*10cm进过步骤2处理后的聚酰亚胺基碳膜进行复合,具体为:在聚酰亚胺基碳膜表面均匀涂覆步骤1中的氧化石墨烯溶液,然后将多张聚酰亚胺基碳膜沿厚度方向粘接在一起。
(4)将粘接后的聚酰亚胺基复合碳膜放置在烘箱烘干,烘箱的温度为40℃。
(5)将烘干后的聚酰亚胺基复合碳膜置于热压机的热压腔中,以2℃/min的速率升温到200℃后进行热压,重复以下热压过程5次:维持压力20MPa,维持1h;逐渐释放压力至0MPa,对热压腔抽真空5min至真空度为-50KPa;然后再以2℃/min的速率升温300℃,保温0.5h,然后进行热压,重复以下热压过程5次:维持压力60MPa,维持1h,逐渐释放压力至0MPa,对热压腔抽真空5min至真空度为-50KPa;热压过程结束后自然降温。
(6)将步骤5热压后的聚酰亚胺基复合碳膜在惰性气体氛围下以5℃/min的速率升温到2800℃进行进一步热压,保温保压2h;压力为60MPa。降温压制后,得到的聚酰亚胺基复合碳膜。
经过以上步骤,此时,聚酰亚胺基复合碳膜的厚度为258μm,密度为1.85g/cm
3,孔隙率为15.9%,导热率为1615.2W/mK,此聚酰亚胺基复合碳膜无分层现象,任意两个相邻的石墨片层间距不小于20nm。
实施例4:
(1)将平均尺寸大于50μm的氧化石墨烯配制成浓度为10mg/mL氧化石墨烯水溶液。
(2)将厚度为25μm的商用聚酰亚胺基碳膜进行氧等离子体进行处理,使之具有亲水性。
(3)将十张尺寸为10cm*10cm进过步骤2处理后的聚酰亚胺基碳膜进行复合,具体为:在聚酰亚胺基碳膜表面均匀涂覆步骤1中的氧化石墨烯溶液,然后将多张聚酰亚胺基碳膜沿厚度方向粘接在一起。
(4)将粘接后的聚酰亚胺基复合碳膜放置在烘箱烘干,烘箱的温度为40℃。
(5)将烘干后的聚酰亚胺基复合碳膜置于热压机的热压腔中,以2℃/min的速率升温到200℃后进行热压,重复以下热压过程5次:维持压力20MPa,维持1h;逐渐释放压力至0MPa,对热压腔抽真空5min至真空度为-50KPa;然后再以2℃/min的速率升温300℃,保温0.5h,然后进行热压,重复以下热压过程5次:维持压力60MPa,维持1h,逐渐释放压力至0MPa,对热压腔抽真空5min至真空度为-50KPa;热压过程结束后自然降温。
(6)将步骤5热压后的聚酰亚胺基复合碳膜在惰性气体氛围下以5℃/min的速率升温到2800℃进行进一步热压,保温保压2h;压力为60MPa。降温压制后,得到的聚酰亚胺基复合碳膜。
经过以上步骤,此时,聚酰亚胺基复合碳膜的厚度为271μm,密度为1.84g/cm
3,孔隙率为16.4%,导热率为1595.2W/mK,此聚酰亚胺基复合碳膜无分层现象,任意两个相邻的石墨片层间距不小于20nm。
实施例5:
(1)将平均尺寸大于50μm的氧化石墨烯配制成浓度为4mg/mL氧化石墨烯水溶液。
(2)将厚度为30μm的商用聚酰亚胺基碳膜进行氧等离子体进行处理,使之具有亲水性。
(3)将一百张尺寸为5cm*5cm进过步骤2处理后的聚酰亚胺基碳膜进行复合,具体为:在聚酰亚胺基碳膜表面均匀涂覆步骤1中的氧化石墨烯溶液,然后将多张聚酰亚胺基碳膜沿厚度方向粘接在一起。
(4)将粘接后的聚酰亚胺基复合碳膜放置在烘箱烘干,烘箱的温度为40℃。
(5)将烘干后的聚酰亚胺基复合碳膜置于热压机的热压腔中,以2℃/min的速率升温到200℃后进行热压,重复以下热压过程5次:维持压力20MPa,维持1h;逐渐释放压力至0MPa,对热压腔抽真空5min至真空度为-50KPa;然后再以2℃/min的速率升温300℃,保温0.5h,然后进行热压,重复以下热压过程5次:维持压力60MPa,维持1h,逐渐释放压力至0MPa,对热压腔抽真空5min至真空度为-50KPa;热压过程结束后自然降温。
(6)将步骤5热压后的聚酰亚胺基复合碳膜在惰性气体氛围下以5℃/min的速率升温到2800℃进行进一步热压,保温保压2h;压力为60MPa。降温压制后,得到高导热的聚酰亚胺基复合碳膜。
经过以上步骤,聚酰亚胺基碳膜先通过氧化石墨烯的粘接作用形成整体结构,再经过进一步低温热压和高温热压修复缺陷提高石墨化程度,最终得到高导热的聚酰亚胺基复合碳膜。经测试,得到聚酰亚胺基复合碳膜的厚度为3.17m,密度为1.54g/cm
3,孔隙率为30%,导热率为1249.5W/mK,此聚酰亚胺基复合碳膜无分层现象,任意两个相邻的石墨片层间距小于20nm。
实施例6:
(1)将平均尺寸大于50μm的氧化石墨烯配制成浓度为4mg/mL氧化石墨烯水溶液。
(2)将四张厚度为100μm的聚酰亚胺膜进行复合,具体为:在聚酰亚胺膜表面均匀涂覆步骤1中的氧化石墨烯溶液,然后将多张聚酰亚胺膜沿厚度方向粘接在一起。
(3)将粘接后的氧化石墨烯/聚酰亚胺复合膜放置在烘箱烘干,烘箱的温度低于40℃。
(5)将烘干后的氧化石墨烯/聚酰亚胺复合膜置于氩气氛围的碳化炉中,以5℃/min的速率逐渐升温到1000℃进行热处理,并且每隔100℃,恒温1h,整个过程维持压力20MPa。
(6)将步骤5热压后的石墨烯/聚酰亚胺复合碳膜在惰性气体氛围下以20℃/min的速率升温到2800℃进行进一步热压,保温保压0.5h;压力为60MPa, 得到高导热的氧化石墨烯/聚酰亚胺复合碳膜。
经过以上步骤,聚酰亚胺膜先通过氧化石墨烯的粘接作用形成整体结构,再经过进一步相对低温热压热处理使其碳化和高温热压修复缺陷提高石墨化程度,最终得到高导热的聚酰亚胺基复合碳膜。经测试,原聚酰亚胺基碳膜的厚度为31μm,密度为2.03g/cm
3,孔隙率为7.7%,导热率为1733.2W/mK;此时,石墨烯/聚酰亚胺复合碳膜的厚度为126μm,密度为1.97g/cm
3,孔隙率为10.5%,导热率为1697.5W/mK,此聚酰亚胺基复合碳膜无分层现象,任意两个相邻的石墨片层间距小于20nm。
实施例7:
(1)将平均尺寸大于50μm的氧化石墨烯配制成浓度为4mg/mL氧化石墨烯水溶液。
(2)将50张厚度为100μm的聚酰亚胺膜进行复合,具体为:在聚酰亚胺膜表面均匀涂覆步骤1中的氧化石墨烯溶液,然后将多张聚酰亚胺膜沿厚度方向粘接在一起。
(3)将粘接后的氧化石墨烯/聚酰亚胺复合膜放置在烘箱烘干,烘箱的温度低于40℃。
(5)将烘干后的氧化石墨烯/聚酰亚胺复合膜置于氩气氛围的碳化炉中,以2℃/min的速率逐渐升温到1000℃进行热处理,并且每隔100℃,恒温1h,整个过程维持压力60MPa。
(6)将步骤5热压后的石墨烯/聚酰亚胺复合碳膜在惰性气体氛围下以5℃/min的速率升温到2500℃进行进一步热压,保温保压8h;压力为60MPa。得到高导热的氧化石墨烯/聚酰亚胺复合碳膜。
经过以上步骤,聚酰亚胺膜先通过氧化石墨烯的粘接作用形成整体结构,再经过进一步相对低温热压热处理使其碳化和高温热压修复缺陷提高石墨化程度,最终得到高导热的聚酰亚胺基复合碳膜。经测试,石墨烯/聚酰亚胺复合碳膜的厚度为1.76mm,密度为1.82g/cm
3,孔隙率为17.3%,导热率为1387.3W/mK,此石墨烯/聚酰亚胺复合碳膜无分层现象,任意两个相邻的石墨片层间距小于20nm。
Claims (6)
- 一种高导热的聚酰亚胺基复合碳膜,其特征在于,聚酰亚胺碳基复合碳膜的厚度大于100μm,孔隙率为10~40%,无分层现象,任意两个相邻的石墨片层间距小于20nm。
- 一种权利要求1所述的高导热的聚酰亚胺基复合碳膜的制备方法,其特征在于,包含如下步骤:(1)将平均尺寸大于50μm的氧化石墨烯配制成浓度为1~10mg/mL氧化石墨烯水溶液。(2)将聚酰亚胺基碳膜进行氧等离子体进行处理,使之具有亲水性。(3)将多张步骤2处理后的聚酰亚胺基碳膜进行复合,具体为:在聚酰亚胺基碳膜表面均匀涂覆步骤1中的氧化石墨烯溶液,然后将多张聚酰亚胺基碳膜沿厚度方向粘接在一起。(4)将粘接后的聚酰亚胺基复合碳膜放置在烘箱烘干,烘箱的温度低于等于40℃。(5)将烘干后的聚酰亚胺基复合碳膜置于热压机的热压腔中,以0.1~5℃/min的速率升温到200℃后进行热压,重复以下热压过程1~5次:维持压力20MPa,维持1h,释放压力至0MPa,对热压腔抽真空5min至真空度为-100~10KPa;然后再以0.1~5℃/min的速率升温300℃,保温0.5h后进行热压,重复以下热压过程1~5次:维持压力60MPa,维持1h,逐渐释放压力至0MPa,对热压腔抽真空5min至真空度为-100~10KPa;热压过程结束后自然降温。(6)将步骤5热压后的聚酰亚胺基复合碳膜在惰性气体氛围下以1-20℃/min的速率升温到2400~3000℃进行进一步热压,保温保压0.5~8h;压力为60MPa。降温压制后,得到高导热的聚酰亚胺基复合碳膜。
- 根据权利要求2所述的方法,其特征在于,所述的步骤1的氧化石墨烯的碳氧比1.8~2.1。
- 一种高导热的石墨烯/聚酰亚胺复合碳膜,其特征在于,所制备的石墨烯/聚酰亚胺复合碳膜的厚度大于100μm,孔隙率为10~40%,面向热导率为1000~1700W/mK;且无分层现象,任意两个相邻的石墨片层间距小于20nm。
- 一种高导热的石墨烯/聚酰亚胺复合碳膜的制备方法,其特征在于,包含如下步骤:(1)将平均尺寸大于50μm的氧化石墨烯配制成浓度为1~10mg/mL氧化 石墨烯水溶液。(2)将多张聚酰亚胺膜进行复合,具体为:在聚酰亚胺膜表面均匀涂覆步骤1中的氧化石墨烯溶液,然后将多张聚酰亚胺膜沿厚度方向粘接在一起。(3)将粘接后的氧化石墨烯/聚酰亚胺复合膜放置在烘箱烘干,烘箱的温度低于40℃。(5)将烘干后的氧化石墨烯/聚酰亚胺复合膜置于氩气氛围的碳化炉中,以0.1~5℃/min的速率逐渐升温到1000℃进行热处理,并且每隔100℃,恒温1h,整个过程维持压力20MPa~200MPa。(6)将步骤5热压后的石墨烯/聚酰亚胺复合碳膜在惰性气体氛围下以1-20℃/min的速率升温到2500~3000℃进行进一步热压,保温保压0.5~8h;压力为60MPa。降温压制后,得到高导热的氧化石墨烯/聚酰亚胺复合碳膜。
- 根据权利要求5所述的方法,所述的步骤1的氧化石墨烯的碳氧比1.8~2.1。
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Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103663444A (zh) * | 2013-12-17 | 2014-03-26 | 张家港康得新光电材料有限公司 | 一种散热用石墨烯复合膜及其制备方法 |
CN104293308A (zh) * | 2014-09-09 | 2015-01-21 | 湖南南方搏云新材料有限责任公司 | 一种高导热石墨膜及其制备工艺 |
CN104495798A (zh) * | 2014-11-28 | 2015-04-08 | 苏州格优碳素新材料有限公司 | 一种石墨导热膜的制造方法 |
KR20150045314A (ko) * | 2013-10-18 | 2015-04-28 | 에스케이씨 주식회사 | 코팅된 열전도성 탄소 입자를 이용한 그라파이트 시트 및 이의 제조방법 |
CN107090275A (zh) * | 2017-05-27 | 2017-08-25 | 杭州高烯科技有限公司 | 一种高导热的石墨烯/聚酰亚胺复合碳膜及其制备方法 |
CN107162594A (zh) * | 2017-05-31 | 2017-09-15 | 杭州高烯科技有限公司 | 一种高导热的聚酰亚胺基复合碳膜及其制备方法 |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP6424036B2 (ja) * | 2014-07-24 | 2018-11-14 | 株式会社カネカ | グラファイトの接合方法、およびグラファイト接着用積層体 |
JP6634601B2 (ja) * | 2016-05-09 | 2020-01-22 | パナソニックIpマネジメント株式会社 | グラファイトプレートとその製造方法 |
-
2018
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Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20150045314A (ko) * | 2013-10-18 | 2015-04-28 | 에스케이씨 주식회사 | 코팅된 열전도성 탄소 입자를 이용한 그라파이트 시트 및 이의 제조방법 |
CN103663444A (zh) * | 2013-12-17 | 2014-03-26 | 张家港康得新光电材料有限公司 | 一种散热用石墨烯复合膜及其制备方法 |
CN104293308A (zh) * | 2014-09-09 | 2015-01-21 | 湖南南方搏云新材料有限责任公司 | 一种高导热石墨膜及其制备工艺 |
CN104495798A (zh) * | 2014-11-28 | 2015-04-08 | 苏州格优碳素新材料有限公司 | 一种石墨导热膜的制造方法 |
CN107090275A (zh) * | 2017-05-27 | 2017-08-25 | 杭州高烯科技有限公司 | 一种高导热的石墨烯/聚酰亚胺复合碳膜及其制备方法 |
CN107162594A (zh) * | 2017-05-31 | 2017-09-15 | 杭州高烯科技有限公司 | 一种高导热的聚酰亚胺基复合碳膜及其制备方法 |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109956466A (zh) * | 2019-04-10 | 2019-07-02 | 湖南大学 | 一种兼具面内方向和厚度方向高热导率的石墨烯基复合膜及其制备方法 |
CN109956466B (zh) * | 2019-04-10 | 2021-09-03 | 湖南大学 | 一种兼具面内方向和厚度方向高热导率的石墨烯基复合膜及其制备方法 |
WO2021049218A1 (ja) * | 2019-09-12 | 2021-03-18 | 株式会社カネカ | 表層多孔質グラファイトシート |
JPWO2021049218A1 (zh) * | 2019-09-12 | 2021-03-18 | ||
CN114364526A (zh) * | 2019-09-12 | 2022-04-15 | 株式会社钟化 | 表层多孔性石墨片 |
JP7137713B2 (ja) | 2019-09-12 | 2022-09-14 | 株式会社カネカ | 表層多孔質グラファイトシート |
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