非均相片层设计以调整一种新型高效复合合金的力学行为

Yu Yin, Qiyang Tan, Qiang Sun, W. Ren, Jingqi Zhang, Shiyang Liu, Yingang Liu, M. Bermingham, Houwen Chen, Mingxing Zhang
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引用次数: 15

摘要

为了提高Fe 35 Ni 35 Cr 25 Mo 5复合合金(CCA)的力学性能,提出了一种新的非均相片层(HL)设计策略。冷轧后单步热处理(800℃,保温1h)得到HL组织。这种HL结构由粗晶FCC基体(5 ~ 20 μm)的交替片层区域和含有超细晶粒或亚晶粒(200 ~ 500 nm)以及纳米沉淀物(20 ~ 500 nm)和退火孪晶的区域组成。经800℃退火后的HL组织试样具有优异的抗拉性能,屈服强度大于1.0 GPa,延展性为~13%。退火孪晶和装饰HL结构的纳米沉淀的形成是在具有高密度晶格缺陷(如高密度位错壁和变形孪晶)的剪切带处σ相的部分再结晶和析出同时发生的结果。后者限制了再结晶晶粒的生长,导致在HL组织内形成超细亚晶粒。高屈服强度是由含有纳米沉淀物的非均相片层结构引起的多级异质变形诱导(HDI)强化和沉淀强化引起的。延性源于多种变形机制的共存,在初始阶段始于位错滑移和层错的形成,随后在高应变水平上发生纳米孪晶。这种HL设计策略,包括成分和热机械工艺设计,以及由此产生的微观结构调整,为开发具有更高性能的成本效益的cca打开了更广阔的窗口。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Heterogeneous Lamella Design to Tune the Mechanical Behaviour of a New Cost-Effective Compositionally Complicated Alloy
A novel heterogeneous lamella (HL) design strategy was proposed to improve mechanical properties of a new cost-effective Fe 35 Ni 35 Cr 25 Mo 5 compositionally complicated alloy (CCA). A HL structure was produced by single-step heat treatment (800 °C for 1h) after cold rolling. This HL structure consists of alternative lamellae regions of coarse-grained FCC matrix (5∼20 μm), and regions containing ultra-fine grains or subgrains (200∼500 nm) together with nanoprecipitates (20-500 nm) and annealing twins. The 800 °C annealed sample with HL structure demonstrated a superior tensile property, with yield strength over 1.0 GPa and ductility of ~13%. Formation of the annealing twins and nanoprecipitates decorated HL structure was a result of the concurrent partial recrystallization and precipitation of σ phase at the shear bands with a high density of lattice defects (e.g. high-density dislocation walls and deformation twins). The latter restricted the growth of recrystallized grains, leading to the formation of ultrafine subgrains within the HL structure. The high yield strength resulted from the multistage hetero-deformation induced (HDI) strengthening and precipitation strengthening associated with heterogeneous lamella structures containing nanoprecipitates. The ductility was originated from the coexistence of multiple deformation mechanisms, which started with dislocation slip and formation of stacking faults at the initial stage, followed by nano-twinning at the higher strain level. This HL design strategy, comprising of composition and thermomechanical process designs, and the resultant microstructure tuning, open a broader window for development of cost-effective CCAs with enhanced performance.
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