Exploring atomic occupation of ternary alloy elements at L1 2 -Ni 3 Al sub-lattice

The Ni 3 Al phase of L1 2 crystal lattice is the most important strengthening phase for nickel-base super-alloy of an aero-engine. The configuration of atomic occupation of alloy elements at the L1 2 -Ni 3 Al sub-lattice plays a key role in its serving properties in the thermal-mechanic condition. T...

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Published inXibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University Vol. 43; no. 2; pp. 285 - 294
Main Authors WANG, Kun, ZHANG, Jing, MA, Wenlai
Format Journal Article
LanguageEnglish
Published 01.04.2025
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ISSN1000-2758
2609-7125
DOI10.1051/jnwpu/20254320285

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Summary:The Ni 3 Al phase of L1 2 crystal lattice is the most important strengthening phase for nickel-base super-alloy of an aero-engine. The configuration of atomic occupation of alloy elements at the L1 2 -Ni 3 Al sub-lattice plays a key role in its serving properties in the thermal-mechanic condition. Through establishing the phase-field model of a ternary alloy system and solving the micro-diffusion dynamic functions, the spatial-temporal information on the atomic occupation of different L1 2 -Ni 3 Al sub-lattices is tracked, the occupation capability of ternary alloy elements is assessed and the atomic density distribution at single-lattice points is obtained. The atomic occupation of Ni-Al-V and Ni-Al-Cr precipitation phases in the L1 2 -Ni 3 Al sub-lattice after the phase transformation path of FCC→L1 2 +D0 22 is studied. The results show that through the time-related order process, the atomic occupation removes the competitive growth in the homogeneous or heterogeneous phase in the early phase transformation and the random fluctuation that interface migration causes to the sub-lattices. The Ni 3 Al phase is in fact a compound metal alloy phase. The antisite and substitution site are the functions of the binary solute ratio. The addition of Cr and V has an obvious difference in affecting the antisite and substitution site in different sub-lattices, which is related to sub-lattice type, defect type and alloy element type. L1 2 晶格结构Ni 3 Al相为航空发动机镍基高温合金最重要的强化相, 其亚晶格上合金体系组成元素的原子占位配置对热-力环境下服役性能起决定性作用。针对L1 2 -Ni 3 Al内不同亚晶格上原子占位的时-空信息追踪与第三合金化元素的占位能力评估, 通过求解微观扩散动力学方程, 构建三元合金体系相场模型, 得到单晶格格点原子密度分布, 研究了经FCC→L1 2 +D0 22 相变路径后的Ni-Al-Cr与Ni-Al-V沉淀相L1 2 -Ni 3 Al中的原子占位。结果表明, 平衡期占位通过与时间相关的有序化过程消除相变早期的同相/异相竞争生长, 以及界面迁移对亚晶格上原子占位带来的随机波动性影响; Ni-Al-Cr与Ni-Al-V中Ni 3 Al相均为复合金属间化合物相, Ni、Al亚晶格上反位、替位为双溶质比的函数; Cr、V添加对Ni 3 Al中不同亚晶格的反位、替位的影响具有明显差异性, 与晶格类型、缺陷类型以及组元类型相关。
ISSN:1000-2758
2609-7125
DOI:10.1051/jnwpu/20254320285