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作 者:Yan Ma Masahito Ueda Tomohiro Yokozeki Toshi Sugahara Yuqiu Yang Hiroyuki Hamada
机构地区:[1]Advanced Fibro-Science, Kyoto Institute of Technology, Kyoto, Japan [2]Department of Mechanical Engineering, College of Science and Technology, Nihon University, Tokyo, Japan [3]Department of Aeronautics and Astronautics, the University of Tokyo, Tokyo, Japan [4]Maruhachi Corporation, Fukui, Japan [5]Key Laboratory of Textile Science & Technology, Ministry of Education, College of Textiles, Donghua University, Shanghai,China
出 处:《Open Journal of Composite Materials》2017年第4期227-249,共23页复合材料期刊(英文)
摘 要:In this work, flexural properties and failure behavior of unidirectional (UD) carbon fiber reinforced polyamide 6 (CF/Nylon 6) and epoxy resin (CF/ Epoxy) laminates were investigated through three-point bending test. The mechanical properties and failure behavior of 0 and 90 degree CF/Nylon 6 and CF/Epoxy laminates were discussed based on the fiber volume fraction, fiber distribution, void content, interfacial properties, transversal tensile strength and fracture toughness. The effects of fiber volume fraction, fiber distribution, void content and their hybrid effect on the flexural properties were investigated. Step-by-step observation and scanning electron microscope observation of laminates after flexural tests were employed to analyze the fracture process.In this work, flexural properties and failure behavior of unidirectional (UD) carbon fiber reinforced polyamide 6 (CF/Nylon 6) and epoxy resin (CF/ Epoxy) laminates were investigated through three-point bending test. The mechanical properties and failure behavior of 0 and 90 degree CF/Nylon 6 and CF/Epoxy laminates were discussed based on the fiber volume fraction, fiber distribution, void content, interfacial properties, transversal tensile strength and fracture toughness. The effects of fiber volume fraction, fiber distribution, void content and their hybrid effect on the flexural properties were investigated. Step-by-step observation and scanning electron microscope observation of laminates after flexural tests were employed to analyze the fracture process.
关 键 词:Polymer MATRIX Composite FLEXURAL Properties FAILURE Behavior UNIDIRECTIONAL PREPREG
分 类 号:TB3[一般工业技术—材料科学与工程]
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