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Frontal Process Zone Toughening Mechanism of Ceramic-Based Nanocomposites

机译:陶瓷基纳米复合材料的正压工艺区增韧机理

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Toughening mechanism for ceramic-based nanocomposites will be presented based on residual stresses around second-phase nano-particles dispersed in matrix grains. The residual thermal stresses around a spherical particle within a concentric sphere of a matrix grain were analyzed to clarify the effects of residual stresses on the toughening mechanism in the frontal process zone. An indirect estimation technique for assessing a critical size of the frontal process zone in ceramics was also proposed using a SEVNB (Single-Edge V-Notched Beam) technique. A three-point flexure test was carried out for nanocomposites and monolithic materials with various depths of a sharp V-shaped notch, and then a critical local stress was calculated at a distance from the notch tip. The frontal process zone size at the beginning of crack propagation, namely, the critical frontal process zone size, was determined as the distance from the notch tip to the point where the local stress has the same value as the flexural strength of the material. The results revealed that both the strength and the critical frontal process zone size must be increased for enhancement of the fracture toughness of ceramics.
机译:基于陶瓷基纳米复合材料的增韧机理将基于分散在基质晶粒中的第二相纳米颗粒周围的残余应力来呈现。分析了基质晶粒的同心球内的球形颗粒周围的残余热应力,以阐明残余应力对额压区域中的增韧机构的影响。使用SEVNB(单边缘V-NOTCHED光束)技术还提出了一种用于评估陶瓷中正面处理区域的临界大小的间接估计技术。为纳米复合材料和单片材料进行三点挠曲测试,具有尖锐V形凹口的各种深度,然后在距离凹口尖端的距离处计算临界局部应力。在裂缝传播开始时的正面处理区尺寸,即临界正面处理区尺寸被确定为从凹口尖端到局部应力与材料的弯曲强度相同的点的距离。结果表明,必须增加强度和临界正面过程尺寸以提高陶瓷的断裂韧性。

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