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首页> 外文期刊>Journal of Materials Science >Fatigue crack propagation in microcapsule-toughened epoxy
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Fatigue crack propagation in microcapsule-toughened epoxy

机译:微胶囊增韧环氧树脂中的疲劳裂纹扩展

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摘要

The addition of liquid-filled urea-formaldehyde (UF) microcapsules to an epoxy matrix leads to significant reduction in fatigue crack growth rate and corresponding increase in fatigue life. Mode-I fatigue crack propagation is measured using a tapered double-cantilever beam (TDCB) specimen for a range of microcapsule concentrations and sizes: 0, 5, 10, and 20% by weight and 50, 180, and 460 μm diameter. Cyclic crack growth in both the neat epoxy and epoxy filled with microcapsules obeys the Paris power law. Above a transition value of the applied stress intensity factor ΔK T, which corresponds to loading conditions where the size of the plastic zone approaches the size of the embedded microcapsules, the Paris law exponent decreases with increasing content of microcapsules, ranging from 9.7 for neat epoxy to approximately 4.5 for concentrations above 10 wt% microcapsules. Improved resistance to fatigue crack propagation, indicated by both the decreased crack growth rates and increased cyclic stress intensity for the onset of unstable fatigue-crack growth, is attributed to toughening mechanisms induced by the embedded microcapsules as well as crack shielding due to the release of fluid as the capsules are ruptured. In addition to increasing the inherent fatigue life of epoxy, embedded microcapsules filled with an appropriate healing agent provide a potential mechanism for self-healing of fatigue damage.
机译:将液体填充的脲甲醛(UF)微胶囊添加到环氧基质中会导致疲劳裂纹扩展速率显着降低,并相应地延长疲劳寿命。使用锥形双悬臂梁(TDCB)样品测量微胶囊浓度和尺寸范围(重量百分比为0、5、10和20%,直径分别为50、180和460μm)时,I型疲劳裂纹扩展。纯环氧树脂和填充有微胶囊的环氧树脂的循环裂纹扩展均符合巴黎幂定律。高于所施加的应力强度因子ΔKT 的过渡值时,该过渡值对应于塑料层大小接近嵌入式微囊大小的加载条件,巴黎定律指数随微囊含量的增加而降低,范围为对于纯环氧为9.7,对于浓度超过10 wt%的微胶囊,约为4.5。对疲劳裂纹扩展的抵抗力的提高,表现为裂纹增长速率的降低和周期性疲劳强度的增加,这是由于不稳定的疲劳裂纹增长的开始所致,这归因于嵌入的微囊体所引起的增韧机制以及由于释放的微囊而引起的裂纹屏蔽。胶囊破裂时液体流失。除了增加环氧树脂的固有疲劳寿命外,填充有适当愈合剂的嵌入式微囊还为疲劳损伤的自我修复提供了潜在的机制。

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  • 来源
    《Journal of Materials Science 》 |2006年第19期| 6266-6273| 共8页
  • 作者单位

    Department of Theoretical and Applied Mechanics and the Beckman Institute for Advanced Science and Technology University of Illinois at Urbana-ChampaignMaterials Science and Technology Division MS G-755 Los Alamos National Laboratory;

    Department of Aerospace Engineering and the Beckman Institute for Advanced Science and Technology University of Illinois at Urbana-Champaign;

    Department of Theoretical and Applied Mechanics and the Beckman Institute for Advanced Science and Technology University of Illinois at Urbana-Champaign;

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