Twin-Boundary Assisted Crack Tip Plasticity and Toughening in Lamellar γ-TiAl

A. Neogi, R. Janisch
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引用次数: 23

Abstract

The internal twin-boundaries in lamellar γ-TiAl alloys, namely true-twin (TT), rotational boundary(RB), and pseudo-twin (PT), are known to be effective in strengthening the TiAl microstructures. Nevertheless, for designing microstructures with optimised mechanical properties, a better understanding of the role of these boundaries on fracture behavior is still required. To this end, we study how and to what degree crack advancement is affected by the local lattice orientation and atomic structure at the various twin boundaries. Molecular statics simulations were performed in conjunction with a linear elastic fracture mechanics based analysis, to understand the inter-lamellar and as well as trans-lamellar crack advancement at a TT, RB, and PT interface. The fracture toughness as well as the crack advancement mechanisms of the inter-lamellar cracks depend critically on the propagation direction. For instance, cracks along ⟨11‾2] in the TT, RB, and PT plane always emit dislocations at the crack tip, while the cracks along the opposite direction are brittle in nature. When it comes to trans-lamellar crack advancement, the crack tip shows significant plastic deformation and toughening for all inter-faces. However, at a TT, a brittle crack is able to penetrate through the interface at a higher applied load, and propagates in the adjacent γ′ phase, while in the case of RB and PT, the crack tip is blunted and arrested at or near the boundary, resulting in dislocation emission and crack tip toughening. This suggests that a variation of the sequence of the different rotational boundaries could be a possibility to tune the crack tip plasticity and toughening in lamellar TiAl.
片层γ-TiAl双界辅助裂纹尖端塑性与增韧
层状γ-TiAl合金的内部孪晶界,即真孪晶界(TT)、旋转孪晶界(RB)和伪孪晶界(PT),对TiAl组织的强化是有效的。然而,为了设计具有最佳力学性能的微观结构,仍然需要更好地了解这些边界在断裂行为中的作用。为此,我们研究了不同孪晶边界处的局部晶格取向和原子结构如何以及在多大程度上影响裂纹扩展。分子静力学模拟与基于线弹性断裂力学的分析相结合,以了解TT、RB和PT界面的片层间和片层间裂纹进展情况。层间裂纹的断裂韧性和裂纹扩展机制与扩展方向密切相关。例如,在TT、RB、PT平面上沿⟨11 * 2]方向的裂缝总是在裂缝尖端发出位错,而沿相反方向的裂缝本质上是脆性的。跨层裂纹扩展时,裂纹尖端各界面均表现出明显的塑性变形和增韧。然而,在高载荷下,脆性裂纹能够穿透界面,并在相邻的γ′相中扩展,而在RB和PT的情况下,裂纹尖端在边界或附近被钝化和阻止,导致位错发射和裂纹尖端增韧。这表明,改变不同旋转边界的顺序可能是调整层状TiAl裂纹尖端塑性和增韧的一种可能性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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