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首页> 外文期刊>Journal of Materials Science >Hygrothermal effects on the shear properties of carbon fiber/epoxy composites
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Hygrothermal effects on the shear properties of carbon fiber/epoxy composites

机译:湿热对碳纤维/环氧树脂复合材料剪切性能的影响

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摘要

The environmental factors, such as humidity and temperature, can limit the applications of composites by deteriorating the mechanical properties over a period of time. Environmental factors play an important role during the manufacture step and during composite’s life cycle. The degradation of composites due to environmental effects is mainly caused by chemical and/or physical damages in the polymer matrix, loss of adhesion at the fiber/matrix interface, and/or reduction of fiber strength and stiffness. Composite’s degradation can be measure by shear tests because shear failure is a matrix dominated property. In this work, the influence of moisture in shear properties of carbon fiber/epoxy composites (laminates [0/0]s and [0/90]s) have been investigated. The interlaminar shear strength (ILSS) was measured by using the short beam shear test, and Iosipescu shear strength and modulus (G 12) have been determinated by using the Iosipescu test. Results for laminates [0/0]s and [0/90]s, after hygrothermal conditioning, exhibited a reduction of 21% and 18% on the interlaminar shear strenght, respectively, when compared to the unconditioned samples. Shear modulus follows the same trend. A reduction of 14.1 and 17.6% was found for [0/0]s and [0/90]s, respectively, when compared to the unconditioned samples. Microstructural observations of the fracture surfaces by optical and scanning electron microscopies showed typical damage mechanisms for laminates [0/0]s and [0/90]s.
机译:环境因素(例如湿度和温度)会在一段时间内降低机械性能,从而限制复合材料的应用。在制造步骤和复合材料的生命周期中,环境因素起着重要的作用。由于环境影响,复合材料的降解主要是由聚合物基质中的化学和/或物理损坏,纤维/基质界面处的粘合性丧失和/或纤维强度和刚度降低引起的。复合材料的降解可以通过剪切测试来衡量,因为剪切破坏是基体主导的特性。在这项工作中,研究了水分对碳纤维/环氧树脂复合材料(层压[0/0] s 和[0/90] s )的剪切性能的影响。使用短梁剪切试验测量层间剪切强度(ILSS),并使用Iosipescu试验确定Iosipescu的剪切强度和模量(G 12 )。湿热条件下,层压板[0/0] s 和[0/90] s 的结果显示,层间剪切强度分别降低了21%和18%。未经处理的样品。剪切模量遵循相同的趋势。与未处理样品相比,[0/0] s 和[0/90] s 分别降低了14.1和17.6%。用光学和扫描电子显微镜观察断裂表面的显微结构,发现了[0/0] s 和[0/90] s 层压板的典型损伤机理。

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  • 来源
    《Journal of Materials Science 》 |2006年第21期| 7111-7118| 共8页
  • 作者单位

    Divisão de Materiais Instituto de Aeronáutica e Espaço CTAFatigue and Aeronautic Material Research Group Department of Material and Technology UNESP;

    Divisão de Materiais Instituto de Aeronáutica e Espaço CTA;

    Divisão de Materiais Instituto de Aeronáutica e Espaço CTA;

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