CN102382368A - Carbon fiber/cenosphere/polypropylene ternary composited material and preparation method thereof - Google Patents
Carbon fiber/cenosphere/polypropylene ternary composited material and preparation method thereof Download PDFInfo
- Publication number
- CN102382368A CN102382368A CN201110281755XA CN201110281755A CN102382368A CN 102382368 A CN102382368 A CN 102382368A CN 201110281755X A CN201110281755X A CN 201110281755XA CN 201110281755 A CN201110281755 A CN 201110281755A CN 102382368 A CN102382368 A CN 102382368A
- Authority
- CN
- China
- Prior art keywords
- cenosphere
- carbon fiber
- polypropylene
- parts
- cenospheres
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Images
Landscapes
- Compositions Of Macromolecular Compounds (AREA)
Abstract
Description
技术领域 technical field
本发明涉及一种三元复合材料及其制备方法,尤其是碳纤维/空心微珠/聚丙烯三元复合材料及其制备方法。 The invention relates to a ternary composite material and a preparation method thereof, in particular to a carbon fiber/hollow microsphere/polypropylene ternary composite material and a preparation method thereof. the
the
背景技术 Background technique
碳纤维(CF)是一类含碳量超过92%的非石墨形态的纤维的总称,其作为轻质高强的理想增强体,常用于以树脂、金属、陶瓷、水泥等为基体的复合体系中。空心微珠(GB)是一种松散、流动性好的粉体材料,具有隔音性、阻燃性、电绝缘性好,密度小,吸油率低,并且强度高等特点,由于其优异的流动性能,常在填充改性中用于改善流动性能,控制浮纤外露、提高表面光洁度等。空心微珠可以由人工制得或从粉煤灰中分离得到,按其相对密度的不同又可分为漂珠和沉珠;其密度相对较轻的漂珠,密度为0.5~0.75g/ m3。由于其优异的流动性能,常在填充改性中用于改善流动性能,控制浮纤外露、提高表面光洁度等。由于漂珠壁比较薄,在力场作用下易破碎,从而丧失其空心球的意义,因此,漂珠多用于热固性树脂以及浇铸、模压成型的热塑性树脂体系的填充改性中。 Carbon fiber (CF) is a general term for a class of non-graphite fibers with a carbon content of more than 92%. As an ideal reinforcement for light weight and high strength, it is often used in composite systems based on resins, metals, ceramics, and cement. Hollow microspheres (GB) are a kind of loose and fluid powder material, which has the characteristics of sound insulation, flame retardancy, good electrical insulation, low density, low oil absorption, and high strength. Due to its excellent fluidity , often used in filling modification to improve flow performance, control floating fiber exposure, improve surface finish, etc. Hollow microspheres can be artificially produced or separated from fly ash, and can be divided into floating beads and sinking beads according to their relative density; floating beads with relatively light density have a density of 0.5~0.75g/ m3 . Due to its excellent flow properties, it is often used in filling modification to improve flow properties, control floating fiber exposure, and improve surface finish. Because the wall of floating beads is relatively thin, it is easily broken under the action of a force field, thus losing the meaning of its hollow ball. Therefore, floating beads are mostly used in the filling modification of thermosetting resins and thermoplastic resin systems for casting and molding. the
当前常用碳纤维增强树脂基复合材料仍以热固性树脂为主,特别是片状模塑料(SMC)相当广泛地用于汽车零部件的制造,尤其是在美国和德国。由于热固性树脂基复合材料存在着断裂韧性较低、抗损伤能力较差、预浸料使用周期短、制品加工周期长以及废料回收困难等缺点,限制了其进一步发展,迫使人们对现有的热固性复合材料进行增韧改性,与此同时,人们也在寻找新的韧性材料作为基体树脂。 Currently commonly used carbon fiber reinforced resin matrix composites are still dominated by thermosetting resins, especially sheet molding compounds (SMC) are widely used in the manufacture of automotive parts, especially in the United States and Germany. Due to the shortcomings of thermosetting resin-based composites such as low fracture toughness, poor damage resistance, short service life of prepregs, long product processing cycles, and difficulties in waste recycling, their further development is limited, and people are forced to pay attention to existing thermosetting materials. Composite materials are toughened and modified. At the same time, people are also looking for new tough materials as matrix resins. the
随着化石能源的日渐减少和人们对生态环境的日益重视,节能减排已成为全世界共同努力的目标。这使得航天和航空设备、轨道交通运输设备、船舶、汽车等国防、交通运输装备制造业面临着严峻的挑战。“轻量化”是目前交通运输装备制造业节能减排的重要手段之一,也是目前交通运输装备制造业的重要发展方向与研究课题。 With the decrease of fossil energy and people's increasing attention to the ecological environment, energy conservation and emission reduction has become a common goal of the world. This makes aerospace and aviation equipment, rail transportation equipment, ships, automobiles and other national defense and transportation equipment manufacturing industries face severe challenges. "Lightweight" is one of the important means of energy saving and emission reduction in the transportation equipment manufacturing industry, and it is also an important development direction and research topic of the transportation equipment manufacturing industry. the
近二十年来,由于汽车工业的快速发展和复合材料在汽车材料应用领域的迅速扩大,热固性复合材料的有害气体挥发和废弃物回收问题显得尤为突出。随着人类环境保护意识的日益增强,在“2007年世界碳纤维前景”(Global Outlook of Carbon Fiber 2007)会议上,弗柏福奇公司复合材料工程师迈克尔·斯金纳指出,从未来发展趋势看,汽车设计者将更偏爱有利于回收和环保的热塑性复合材料。2008年世界碳纤维前景会上更将“汽车上应用的前景”作为4大专题之一。正是由于碳纤维增强热塑性树脂基复合材料其优异的性能及广阔的应用前景,无论是国家还是个人对这类高性能的复合材料的制备工艺及配方都高度保密。 In the past two decades, due to the rapid development of the automobile industry and the rapid expansion of the application of composite materials in the field of automotive materials, the problem of volatilization of harmful gases and waste recycling of thermosetting composite materials has become particularly prominent. With the increasing awareness of human environmental protection, at the "Global Outlook of Carbon Fiber 2007" (Global Outlook of Carbon Fiber 2007) conference, Michael Skinner, a composite material engineer at Furber Fauci, pointed out that from the perspective of future development trends, Automobile designers will prefer thermoplastic composite materials that are conducive to recycling and environmental protection. At the 2008 World Carbon Fiber Prospects Conference, "Prospects for Automotive Applications" was taken as one of the four major topics. It is precisely because of the excellent performance and broad application prospects of carbon fiber reinforced thermoplastic resin matrix composites that both the country and individuals keep the preparation process and formula of such high-performance composites highly confidential. the
the
发明内容 Contents of the invention
本发明针对碳纤维增强热塑性树脂基复合材料广阔的应用前景,提供一种强度和韧度显著增强、适用范围较为广泛的碳纤维/空心微珠/聚丙烯三元复合材料及其制备方法。 Aiming at the broad application prospects of carbon fiber-reinforced thermoplastic resin-based composite materials, the invention provides a carbon fiber/hollow microsphere/polypropylene ternary composite material with significantly enhanced strength and toughness and a relatively wide application range and a preparation method thereof. the
本发明的技术方案:碳纤维/空心微珠/聚丙烯三元复合材料,其特征在于:三种物质的重量配比为: Technical solution of the present invention: carbon fiber/hollow microsphere/polypropylene ternary composite material, characterized in that: the weight ratio of the three substances is:
聚丙烯100份,碳纤维2—30份,空心微珠大于0小于30份。 100 parts of polypropylene, 2-30 parts of carbon fiber, and more than 0 and less than 30 parts of hollow microspheres.
所述碳纤维/空心微珠/聚丙烯三元复合材料的制备方法,其特征在于: The preparation method of the carbon fiber/hollow microsphere/polypropylene ternary composite material is characterized in that:
(1)首先按照工艺要求准备碳纤维、空心微珠、聚丙烯; (1) First prepare carbon fiber, hollow microspheres and polypropylene according to the process requirements;
(2)对空心微珠进行表面处理:用有机溶剂为溶剂配制浓度为0.5%—3%的硅烷偶联剂溶液,避光混合浸润空心微珠0.5—3小时;然后滤掉处理液,用等离子水淋洗3—5次;最后,烘干后冷却; (2) Surface treatment of the hollow microspheres: use an organic solvent as the solvent to prepare a silane coupling agent solution with a concentration of 0.5%-3%, and mix and infiltrate the hollow microspheres in the dark for 0.5-3 hours; then filter out the treatment solution and use Plasma water rinse 3-5 times; finally, cool after drying;
(3)将碳纤维/空心微珠/聚丙烯三种物质按照其重量配比加入,混合均匀; (3) Add carbon fiber/hollow microsphere/polypropylene according to their weight ratio and mix evenly;
(4)需要制作制件时,将配合好的复合材料加入注射机,进行注射成型,得到三元复合材料及其制件。 (4) When parts need to be made, add the prepared composite materials into the injection machine for injection molding to obtain ternary composite materials and their parts.
本发明的碳纤维/空心微珠/聚丙烯三元复合材料,相对于现有技术,具有如下特点: Compared with the prior art, the carbon fiber/hollow microsphere/polypropylene ternary composite material of the present invention has the following characteristics:
1、本发明以热塑性聚丙烯树脂作为基体材料,用碳纤维及空心微珠对其进行共混改性,最终获得了在较少碳纤维添加的情况下同时增强增韧的碳纤维/空心微珠/聚丙烯三元共混体系。 1. The present invention uses thermoplastic polypropylene resin as a matrix material, and uses carbon fiber and hollow microspheres to carry out blending modification on it, and finally obtains carbon fiber/hollow microspheres/polypropylene that is simultaneously reinforced and toughened under the condition of less carbon fiber addition. Propylene ternary blend system. the
2、在碳纤维/聚丙烯复合体系中引入第三相空心微珠,在冲击过程中主要的承受载体由碳纤维变成了空心微珠,从而实现了复合体系的增韧,而且在相同添加量下,相对于添加PP-g-MAH,添加空心微珠对体系力学性能的影响更为显著,成本也明显降低。 2. Introduce the third phase of hollow microspheres into the carbon fiber/polypropylene composite system. During the impact process, the main bearing carrier changes from carbon fiber to hollow microspheres, thereby realizing the toughening of the composite system, and at the same addition amount , compared with the addition of PP-g-MAH, the effect of adding hollow microspheres on the mechanical properties of the system is more significant, and the cost is also significantly reduced. the
3、本发明的三元复合材料,具有较为广泛的应用前景;其制备方法简单,操作者能够较快掌握。 3. The ternary composite material of the present invention has relatively wide application prospects; its preparation method is simple, and operators can quickly master it. the
附图说明 Description of drawings
图1是本发明对空心微珠进行表面处理工艺流程图; Fig. 1 is that the present invention carries out surface treatment process flow chart to hollow microsphere;
图2是空心微珠添加量对复合材料拉伸及缺口冲击性能的影响示意图。 Figure 2 is a schematic diagram of the effect of the addition of hollow microspheres on the tensile and notched impact properties of the composite material.
the
具体实施方式 Detailed ways
如图1中,本发明碳纤维/空心微珠/聚丙烯三元复合材料,其特征在于,三种物质的重量配比为: As shown in Figure 1, the carbon fiber/hollow microsphere/polypropylene ternary composite material of the present invention is characterized in that the weight ratio of the three substances is:
聚丙烯100份,碳纤维2—30份,空心微珠大于0小于30份 ; 100 parts of polypropylene, 2-30 parts of carbon fiber, hollow microspheres greater than 0 and less than 30 parts;
对空心微珠进行表面处理:首先,用有机溶剂(如甲醇、乙醇、甲醚、乙醚、甲醛等)为溶剂配制浓度为0.5%—3%的硅烷偶联剂溶液,避光混合浸润空心微珠0.5—3小时;然后滤掉处理液,用等离子水淋洗3—5次;最后,烘干后冷却;烘干温度一般在80℃以下,以避免空心微珠损失。本发明硅烷偶联剂,除了KH560溶液以外,还有其他合适的硅烷偶联剂,如KH550、KH570、KH592、DL602、DL171等,能够对空心微珠进行表面处理,满足工艺使用要求。 Surface treatment of hollow microspheres: first, use organic solvents (such as methanol, ethanol, methyl ether, ether, formaldehyde, etc.) Beads for 0.5-3 hours; then filter out the treatment solution and rinse with plasma water for 3-5 times; finally, cool after drying; the drying temperature is generally below 80°C to avoid loss of hollow microbeads. In addition to the KH560 solution, the silane coupling agent of the present invention also has other suitable silane coupling agents, such as KH550, KH570, KH592, DL602, DL171, etc., which can perform surface treatment on hollow microspheres and meet the requirements of the process.
本发明的碳纤维,长度较短,为2mm—7mm,单丝直径0.7mm左右。 The carbon fiber of the present invention has a relatively short length of 2 mm to 7 mm, and a single filament diameter of about 0.7 mm. the
本发明的碳纤维/空心微珠/聚丙烯三元复合材料的制备方法, The preparation method of carbon fiber/hollow microsphere/polypropylene ternary composite material of the present invention,
1、首先按照工艺要求准备碳纤维、空心微珠、聚丙烯; 1. First prepare carbon fiber, hollow microspheres and polypropylene according to the process requirements;
2、对空心微珠进行表面处理:用有机溶剂(如甲醇、乙醇、甲醚、乙醚、甲醛等)为溶剂配制浓度为0.5%—3%的硅烷偶联剂KH560溶液,避光混合浸润空心微珠0.5—3小时;然后滤掉处理液,用等离子水淋洗3~5次;最后,烘干后冷却; 2. Surface treatment of hollow microspheres: use organic solvents (such as methanol, ethanol, methyl ether, ether, formaldehyde, etc.) microbeads for 0.5-3 hours; then filter out the treatment solution and rinse with plasma water for 3-5 times; finally, dry and cool;
3、将碳纤维/空心微珠/聚丙烯三种物质按照其重量配比加入,混合均匀; 3. Add carbon fiber/hollow microspheres/polypropylene according to their weight ratio and mix evenly;
4、需要制作制件时,将配合好的复合材料加入注射机,进行注射成型,得到所需的三元复合材料及其制件。 4. When it is necessary to make parts, put the prepared composite material into the injection machine for injection molding to obtain the required ternary composite material and its parts.
选用现有技术的注射机,其注射工艺为:TTI-95G注射机,料筒温度控制在190~230℃之间,注射压力为50~80MPa,保压压力取注射压力的80%左右,冷却时间为15S。 Select the existing technology injection machine, the injection process is: TTI-95G injection machine, the barrel temperature is controlled between 190-230 °C, the injection pressure is 50-80 MPa, the holding pressure is about 80% of the injection pressure, cooling The time is 15S. the
根据不同的性能需要,碳纤维的含量可以为2、3、4、5、6、7、8、9、10、15、20、22、25、28、30份,空心微珠为0.1、0.2、0.5、1、2、3、4、5、8、9、10、12、13、15、16、、18、19、20、22、25、28、30份,均能满足其要求。 According to different performance requirements, the content of carbon fiber can be 2, 3, 4, 5, 6, 7, 8, 9, 10, 15, 20, 22, 25, 28, 30 parts, and the content of hollow microbeads can be 0.1, 0.2, 0.5, 1, 2, 3, 4, 5, 8, 9, 10, 12, 13, 15, 16, 18, 19, 20, 22, 25, 28, 30 copies can all meet the requirements. the
具体实施例:采用聚丙烯100份,碳纤维5份,空心微珠分别为0、5份、10份、15份和20份,分别制备注射试样CF5、GB5、GB10、GB15、GB20。 Specific examples: 100 parts of polypropylene, 5 parts of carbon fiber, and 0, 5, 10, 15 and 20 parts of hollow microspheres were used to prepare injection samples CF5, GB5, GB10, GB15 and GB20 respectively. the
一般而言,随着填料添加量的增多,复合体系的流动性会急剧下降,然而对于空心微珠其添加量的增多却使得复合体系的流动性得到提高,主要源于其球状结构和较大的硬度。用RM-200A型转矩流变仪对添加0~20份空心微珠时CF/GB/PP复合材料的最大转矩及平衡转矩进行测定,温度210℃,转速30r/ min,加料量40g,测试结果如下表所示。 Generally speaking, as the amount of filler increases, the fluidity of the composite system will decrease sharply. However, the increase in the amount of hollow microspheres will improve the fluidity of the composite system, mainly due to its spherical structure and larger diameter. hardness. Use the RM-200A torque rheometer to measure the maximum torque and equilibrium torque of the CF/GB/PP composite material when adding 0~20 parts of hollow microspheres, the temperature is 210°C, the speed is 30r/min, and the amount of feed is 40g , the test results are shown in the table below. the
the
由上表可知,添加空心微珠后,体系的流变性能并未像多数文献所述。当空心微珠添加量为5份时,体系的最大转矩最大为70.2 N·m,体系的最大转矩相对CF/PP体系不仅未变小反而有所增加;而随着空心微珠添加量的增多,体系的最大转矩才逐渐变小,当空心微珠添加量达到20份时,体系的最大转矩为50.1 N·m,相对CF/PP体系下降了17.9%;添加空心微珠后,体系的平衡转矩均有所增加,认为主要是微珠破裂引起,即证实了空心微珠的添加的确会对成型加工设备造成的磨损增加。 It can be seen from the above table that after adding hollow microspheres, the rheological properties of the system are not as described in most literatures. When the amount of hollow microspheres is 5 parts, the maximum torque of the system is 70.2 N·m, and the maximum torque of the system is not smaller than that of the CF/PP system but increases; The maximum torque of the system gradually decreases when the amount of hollow microspheres increases. When the amount of hollow microspheres reaches 20 phr, the maximum torque of the system is 50.1 N m, which is 17.9% lower than that of the CF/PP system. After adding hollow microspheres , the balance torque of the system has increased, which is mainly caused by the breakage of microbeads, which proves that the addition of hollow microbeads will indeed increase the wear of molding processing equipment. the
图2表示空心微珠添加量对复合材料拉伸及缺口冲击性能的影响:随着空心微珠添加量的增多,复合体系的拉伸强度先增大后降低,当空心微珠添加量为15份时,拉伸强度达到最大为37.2MPa,较纯PP提高了46.5%,较未加PP-g-MAH的CF/PP提高了8.8%,接近添加PP-g-MAH的CF/PP体系的最佳值37.9MPa;而缺口冲击强度则随着空心微珠添加量的增多一直增大,但增大趋势逐渐减缓,当添加量为20份时,缺口冲击强度最大为12.0KJ/m2,较纯PP提高了30.4%,较未加PP-g-MAH的CF/PP提高了33.3%,大于添加PP-g-MAH的CF/PP体系的最佳值10.3KJ/m2;但当空心微珠添加量为5份时,三元复合体系的力学性能极差,拉伸强度和缺口冲击强度分别为27.0MPa和5.0KJ/m2,远低于其它试样。 Figure 2 shows the effect of the amount of hollow microspheres on the tensile and notched impact properties of the composite: with the increase of the amount of hollow microspheres, the tensile strength of the composite system first increases and then decreases. When the amount of hollow microspheres is 15 The tensile strength reaches a maximum of 37.2MPa, which is 46.5% higher than that of pure PP, and 8.8% higher than that of CF/PP without PP-g-MAH, which is close to that of CF/PP system with PP-g-MAH added. The optimum value is 37.9MPa; while the notched impact strength increases with the increase of hollow microspheres, but the increasing trend gradually slows down. Pure PP has increased by 30.4%, which is 33.3% higher than that of CF/PP without PP-g-MAH, which is greater than the best value of 10.3KJ/m2 for CF/PP system with PP-g-MAH added; but when hollow microspheres When the addition amount is 5 parts, the mechanical properties of the ternary composite system are extremely poor, and the tensile strength and notched impact strength are 27.0MPa and 5.0KJ/m2 respectively, which are far lower than other samples. the
Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201110281755XA CN102382368A (en) | 2011-09-21 | 2011-09-21 | Carbon fiber/cenosphere/polypropylene ternary composited material and preparation method thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201110281755XA CN102382368A (en) | 2011-09-21 | 2011-09-21 | Carbon fiber/cenosphere/polypropylene ternary composited material and preparation method thereof |
Publications (1)
Publication Number | Publication Date |
---|---|
CN102382368A true CN102382368A (en) | 2012-03-21 |
Family
ID=45822235
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201110281755XA Pending CN102382368A (en) | 2011-09-21 | 2011-09-21 | Carbon fiber/cenosphere/polypropylene ternary composited material and preparation method thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN102382368A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103030890A (en) * | 2012-12-29 | 2013-04-10 | 重庆理工大学 | Light polymer base fibrilia reinforced composite and fabrication method thereof |
CN105906938A (en) * | 2016-05-20 | 2016-08-31 | 安徽德源电缆集团有限公司 | Cable filling material and production method thereof |
CN112172272A (en) * | 2020-09-30 | 2021-01-05 | 重庆理工大学 | A fireproof material for drones |
CN117903529A (en) * | 2024-03-19 | 2024-04-19 | 浙江群鹿新材料股份有限公司 | Modified engineering plastic, preparation method thereof and preparation method of cooking cup |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1637055A (en) * | 2003-12-26 | 2005-07-13 | 日本聚丙烯有限公司 | Polypropylene-based resin composition and molded article thereof |
CN101921427A (en) * | 2010-08-06 | 2010-12-22 | 奇瑞汽车股份有限公司 | Functional high-polymer decorative composite material and preparation method thereof |
-
2011
- 2011-09-21 CN CN201110281755XA patent/CN102382368A/en active Pending
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1637055A (en) * | 2003-12-26 | 2005-07-13 | 日本聚丙烯有限公司 | Polypropylene-based resin composition and molded article thereof |
CN101921427A (en) * | 2010-08-06 | 2010-12-22 | 奇瑞汽车股份有限公司 | Functional high-polymer decorative composite material and preparation method thereof |
Non-Patent Citations (1)
Title |
---|
吴成宝等: "玻璃微珠填充聚丙烯复合材料的力学性能研究", 《塑料科技》 * |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103030890A (en) * | 2012-12-29 | 2013-04-10 | 重庆理工大学 | Light polymer base fibrilia reinforced composite and fabrication method thereof |
CN103030890B (en) * | 2012-12-29 | 2015-07-22 | 重庆理工大学 | Light polymer base fibrilia reinforced composite and fabrication method thereof |
CN105906938A (en) * | 2016-05-20 | 2016-08-31 | 安徽德源电缆集团有限公司 | Cable filling material and production method thereof |
CN112172272A (en) * | 2020-09-30 | 2021-01-05 | 重庆理工大学 | A fireproof material for drones |
CN112172272B (en) * | 2020-09-30 | 2022-10-21 | 重庆理工大学 | Fireproof material for unmanned aerial vehicle |
CN117903529A (en) * | 2024-03-19 | 2024-04-19 | 浙江群鹿新材料股份有限公司 | Modified engineering plastic, preparation method thereof and preparation method of cooking cup |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN103727203B (en) | compound gear and gear shaft | |
CN101613944B (en) | A method for improving the impact resistance of resin-based carbon fiber composite materials | |
CN106478019B (en) | A kind of bonding mortar using cullet Stainless-steel fibre | |
CN108164820A (en) | A kind of plant fiber/PP composite materials and preparation method thereof | |
CN102146196B (en) | Preparation method of high-damping epoxy resin composite material | |
CN110804250A (en) | Improved high-strength scratch-resistant polypropylene material and preparation method thereof | |
CN102382368A (en) | Carbon fiber/cenosphere/polypropylene ternary composited material and preparation method thereof | |
CN101781444A (en) | Method for preparing rare-earth-modified glass-fiber epoxy-resin composite materials | |
CN105038217A (en) | Carbon fiber reinforced nylon micro-foaming material and preparation method thereof | |
CN104845288A (en) | High-toughness glass fiber reinforced polymer alloy and preparation method thereof | |
Yu et al. | Carbon fiber reinforced epoxy resin matrix composites | |
CN104403265A (en) | Polyetheretherketone/hollow fly-ash bead/glass fiber composite material and preparation method thereof | |
CN106810863B (en) | A kind of pbo fiber epoxy resin composite material and preparation method thereof | |
CN102775732A (en) | Formula of composite high-performance nonmetal material | |
CN110437589A (en) | A kind of carbon fibre composite and preparation method thereof for fuel battery double plates | |
CN103450557B (en) | A kind of preparation method of polypropylene PP nano level enhancing modified particle | |
CN103756314B (en) | For the preparation method of the bimaleimide resin of matrix material liquid condition shaping | |
CN107446348A (en) | A kind of high-performance long fiber reinforced nylon composite material and preparation method thereof | |
CN105733064A (en) | Glass fiber reinforced waste polyethylene composite material | |
CN101670644A (en) | Preparation method for clamp material of aerial oil pipe | |
CN109666264A (en) | A kind of RTM molding bamboo fiber felt enhancing thermosetting resin based composites and preparation method | |
CN108707279A (en) | A kind of eutectic lapping defect exempts from spray coating polypropylene composite material and preparation method without current mark | |
Lee et al. | Preparation and Characterization of a High Toughness Carbon/epoxy Composite | |
CN104592758A (en) | Method for pretreatment of short-staple reinforcing silicon rubber by using silane coupling agent | |
CN103724993B (en) | A kind of water adsorption glass fiber reinforced nylon 6 matrix material and preparation method thereof fast |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C12 | Rejection of a patent application after its publication | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20120321 |