From melt pool to performance: A review of microstructural engineering in the additive manufacturing of nickel-based superalloys

IF 7.9 Q1 ENGINEERING, MULTIDISCIPLINARY
Hedayat Hamdi , Sadaf Sadatabhari , Atefeh Tajik , Abbas Zarei Hanzaki , Ahmad Hatamiyan , Hamid Reza Abedi
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Abstract

This review critically and systematically analyses recent progress in additively manufactured (AM) Ni-based superalloys, mapping processing–microstructure–property linkages relevant to qualification of hot-section hardware in aerospace and energy, including turbine blades, combustion chambers, and injectors. Comparisons are drawn across laser/electron powder-bed fusion and directed energy deposition. We explain how melt-pool dynamics and cooling rate govern grain architecture and boundary character, micro-/macro-texture, micro-segregation, and phase evolution-strengthening γ′/γ″ (γ'/γ'') and carbides versus deleterious Laves/TCP. Key defects, such as porosity, lack of fusion, hot cracking, and residual stress, are linked to the tensile response, hardness stability, and creep/fatigue resistance. Practical process windows are identified, and optimization strategies are synthesized in terms of power, scan speed, hatch spacing, layer thickness, preheating, shielding, and feedstock quality; for illustration, scan speeds on the order of 1100–1700 mm/s in l-PBF IN718 shift strength/porosity trade-offs. Post-processing routes (stress-relief, solution/aging, HIP) that reduce defects, tailor metastable constituents, and restore near-isotropy are summarized. Representative alloys (IN718, IN625, Hastelloy X) illustrate trade-offs between γ′ fraction, Nb-rich Laves formation, and build rate. Remaining gaps include standardized powder specifications, robust in-situ monitoring with model-informed control, cross-platform comparability, and long-duration oxidation/hot-corrosion datasets to support design allowable. Overall, the review offers practical guidance for engineering microstructure and properties in AM Ni-based superalloys and accelerates industrial qualification for critical service environments.
从熔池到性能:镍基高温合金增材制造的显微组织工程研究进展
本文对增材制造(AM)镍基高温合金的最新进展进行了批判性和系统的分析,绘制了与航空航天和能源领域热断面硬件(包括涡轮叶片、燃烧室和喷油器)鉴定相关的加工-显微组织-性能联系。比较了激光/电子粉末床融合和定向能沉积。我们解释了熔池动力学和冷却速度如何控制晶粒结构和边界特征,微观/宏观织构,微观偏析和相演化-强化γ'/γ″(γ'/γ ")和碳化物与有害的Laves/TCP。关键缺陷,如孔隙度、熔合不足、热裂和残余应力,与拉伸响应、硬度稳定性和抗蠕变/疲劳性有关。确定了实用的工艺窗口,从功率、扫描速度、舱口间距、层厚、预热、屏蔽和原料质量等方面综合了优化策略;例如,在l-PBF IN718中,扫描速度为1100 - 1700mm /s,可以在强度/孔隙度方面进行权衡。总结了后处理路线(应力消除,溶液/时效,HIP),减少缺陷,定制亚稳成分,恢复近各向同性。代表性合金(IN718, IN625,哈氏合金X)说明了γ′分数,富铌laaves形成和构建速率之间的权衡。剩下的差距包括标准化的粉末规格、具有模型信息控制的强大的现场监测、跨平台的可比性,以及支持设计允许的长期氧化/热腐蚀数据集。总体而言,该综述为增材制造镍基高温合金的工程组织和性能提供了实用指导,并加速了关键服务环境的工业鉴定。
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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来源期刊
Results in Engineering
Results in Engineering Engineering-Engineering (all)
CiteScore
5.80
自引率
34.00%
发文量
441
审稿时长
47 days
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