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Mechanical properties of woven laminates and felt composites using carbon fibers Part 2: interlaminar properties

机译:使用碳纤维的机织层压板和毡复合材料的机械性能第2部分:层间性能

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This paper compares interlaminar shear strength, interlaminar fracture toughness and compression-after-impact strength of epoxy resin matrix composites reinforced with carbon fiber woven fabrics and carbon fiber felts, and investigates the influences of weave pattern and needle-punching density. With regard to the weave pattern of fabric layers in woven laminates and felt/resin composites, plain weave with a smaller radius of curvature of yarns is preferable for obtaining higher damage tolerance of the composites. Felt/resin composites have improved interlaminar and damage tolerant properties as compared with woven laminates These properties of the felt/resin composites improve with increasing needle-punching density. The compression-after-impact strength of the woven laminates and felt/resin composites can be uniquely related to the mode I interlaminar fracture toughness regardless of the types of composites, and the result has been interpreted by applying the equation derived by Ilic and Williams [Theoret App1. Fract Mech 6 (2) (1986) 121] Damage tolerance of the felt-reinforced composites utilizing more brittle carbon matrix has also been investigated.
机译:本文比较了碳纤维织物和碳纤维毡增强的环氧树脂基复合材料的层间剪切强度,层间断裂韧性和冲击后压缩强度,并研究了编织方式和针刺密度的影响。关于机织层压板和毡/树脂复合材料中织物层的编织图案,具有较小曲率半径的平纹编织对于获得复合材料的更高的耐损伤性是优选的。与机织层压材料相比,毡/树脂复合材料具有改善的层间和耐损伤性能。毡/树脂复合材料的这些性能随针刺密度的增加而提高。不管复合材料的类型如何,机织层压板和毡/树脂复合材料的冲击后压缩强度都可以与模式I层间断裂韧度唯一相关,并且通过应用Ilic和Williams推导的方程来解释结果[定理App1。 Fract Mech 6(2)(1986)121]还研究了利用较脆的碳基体的毡增强复合材料的损伤容限。

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