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Atomistic simulation of crack propagation along y-TiAl lamellar interface

机译:沿y-Tial Lamellar界面裂纹传播原子模拟

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Due to start-up and shut-down operations of engine, TiAl structural components usually undergo not only static but also cyclic mechanical loading. The crack propagation mechanisms of y-TiAl under two types of loading are studied in this work to reveal the differences of the mechanisms under constant strain rate and cyclic loading. Since the crack prefers to nucleate at the interface, two types of loadings are applied to a y-TiAl interface system with a pre-existing micro-crack at the interface by the means of classical molecular dynamics simulation, the loading direction is along [111] perpendicular to the interface. The evolution of crack tip and dislocation is observed in atomistic scale. The results show that, under both loading types, the crack propagates asymmetrically, Shockley dislocations emit on the (-1-11) slip plane from the right crack tip and slip along [-1-1-2] direction. The dislocations blunt the extension of crack while the left crack tip propagates in a brittle way. During the cyclic loading, different with constant strain rate condition, the crack advances and dislocations slip with increasing loads and retreat during unloading. In addition, the stress decreases and the crack length increases with the increase of the cyclic loading number.
机译:由于发动机的启动和关闭操作,Tial结构部件通常不仅经过静态而且循环机械负载。在这项工作中研究了在两种载荷下的Y-Tial的裂纹繁殖机制,以揭示在恒定应变率和循环载荷下机制的差异。由于裂缝在界面处更喜欢核心,因此通过经典分子动力学模拟的界面具有预先存在的微裂纹,将两种类型的负载施加到Y-Tial接口系统上,加载方向沿[111 ]垂直于界面。以原子规模观察到裂缝尖端和错位的演变。结果表明,在两个负载类型下,裂缝在来自(-1-11)滑移平面上从右裂纹尖端发出的冲击脱位,并沿[-1-1-2]方向滑动。脱位突出裂缝的延伸,而左裂纹尖端以脆性的方式传播。在循环加载期间,不同于恒定应变速率条件,裂缝进展和脱位在卸载期间增加负载和后退。另外,应力降低,随着环状加载数的增加,裂缝长度增加。

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