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选区激光熔化γ″强化镍基高温合金热处理调控与力学性能研究进展

Research progress on heat treatment regulation and mechanical properties of selective laser melted γ″-strengthened nickel-based superalloys

  • 摘要: 激光增材制造镍基高温合金复杂非平衡凝固组织的热稳定性与传统铸态、锻态不同,使得增材制造合金采用传统的标准热处理工艺无法获得稳定的组织和优异的性能。因此,亟需明晰增材制造非稳态热循环过程中亚稳态析出组织特征与热处理工艺之间的内在关联,理解亚稳态组织热处理过程中的晶粒生长、第二相析出、位错演变等行为。本文针对航空发动机及燃气轮机领域广泛应用的γ″强化镍基高温合金(如IN718 alloy),综述其选区激光熔化成形后的组织特征,热处理后组织演变与力学性能变化规律的研究进展,旨在探究强约束、快速凝固下高温合金组织调控及力学性能提升方法,进一步拓展激光增材制造技术在航空发动机及燃气轮机等热端结构材料的应用。

     

    Abstract: The thermal stability of the complex non-equilibrium solidified microstructure of the selective laser-melted nickel-based superalloy is different from that of the traditional cast and forged counterparts, and the traditional standard heat treatment process cannot obtain stable structures and excellent properties accordingly. Therefore, it is imperative to clarify the inherent relationship between the characteristics of metastable precipitates in non-equilibrium thermal cycles in additive manufacturing and heat treatment processes, to comprehend behaviors such as grain growth, second-phase precipitation, dislocation evolution, etc., during the thermal treatment of metastable structures. The paper focuses on the γ″ strengthening nickel-based high-temperature alloys (such as IN718 alloy), which are widely used in the fields of aviation engines, and gas turbines and summarizing the research progress in microstructure control during heat treatment and mechanical properties after laser selective melting forming. This article aims to explore the methods for regulating the microstructure and improving mechanical properties of high-temperature alloys under rapid solidification, and further expand the application of laser additive manufacturing technology in hot-end structural materials such as aviation engines and gas turbines.

     

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