首页> 外文会议>International Workshop on Advanced Metallic Materials and Processing Techniques for Aeronautical Applications; 20051118-20; Nanjing(CN) >Numerical simulation of mechanics of electron beam physical vapour deposition Ni/Ni_3Al microlaminates
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Numerical simulation of mechanics of electron beam physical vapour deposition Ni/Ni_3Al microlaminates

机译:Ni / Ni_3Al微叠层电子束物理气相沉积机理的数值模拟

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The rupture behavior of electron beam physical vapour deposition(EBPVD) Ni/Ni_3Al microlaminates composites subjected to tensile load were studied through the numerical method of finite element. 2D model and 3D model of EBPVD Ni/Ni_3Al microlaminates with a centre crack were built respectively. A new scheme for building 3D crack point models was proposed and different types of elements were used. And stress intensity factors around the tip of the crack were obtained correspondingly. The results indicate that the key of the stress intensity factor for 2D model is presumably the average of the keys for 3D model in thickness and the key at the interface is the biggest, which suggests the propagation of the crack greatly likely happen at the interface.
机译:通过有限元数值方法研究了电子束物理气相沉积(EBPVD)Ni / Ni_3Al微层合复合材料在拉伸载荷作用下的断裂行为。分别建立了具有中心裂纹的EBPVD Ni / Ni_3Al微薄板的2D模型和3D模型。提出了一种构建3D裂纹点模型的新方案,并使用了不同类型的元素。并相应地获得了裂纹尖端附近的应力强度因子。结果表明,2D模型的应力强度因子的关键可能是3D模型的关键厚度的平均值,而界面处的关键最大,这表明裂纹的扩展很可能发生在界面处。

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