航空制造技术2024,Vol.67Issue(23) :80-87.DOI:10.16080/j.issn1671-833x.2024.23/24.080

定向凝固FCC/B2双相高熵合金微观组织调控及力学性能研究

Investigation on Microstructure Control and Mechanical Properties of Directionally-Solidified FCC/B2 Dual-Phase High-Entropy Alloy

王立斐 严鹏 刘林翔 王祯 许骏杰 赵婉蓉 王志军
航空制造技术2024,Vol.67Issue(23) :80-87.DOI:10.16080/j.issn1671-833x.2024.23/24.080

定向凝固FCC/B2双相高熵合金微观组织调控及力学性能研究

Investigation on Microstructure Control and Mechanical Properties of Directionally-Solidified FCC/B2 Dual-Phase High-Entropy Alloy

王立斐 1严鹏 2刘林翔 2王祯 1许骏杰 1赵婉蓉 1王志军2
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作者信息

  • 1. 中国航发北京航空材料研究院先进高温结构材料重点实验室,北京 100095
  • 2. 西北工业大学,西安 710072
  • 折叠

摘要

为提升定向凝固FCC/B2 双相高熵合金在宽温域下的综合力学性能,本文基于不同热处理工艺开展了组织调控研究,通过测试其宽温域下的力学性能与表征断口表面,明确不同热处理工艺下的组织演化机理并分析揭示组织特征对合金力学性能的影响机制.结果表明,固溶后进行先高温 800℃再低温 650℃的双级时效处理,可在FCC基体内获得高密度近球形L12 析出相,同时在B2 相内得到板条状的L12 相.高密度的L12 析出相有效强化合金的性能,且L12 相可促进B2 相内的位错运动,有利于提升合金的塑性.相比于铸态,经过热处理后的合金高温力学性能得到明显提升.

Abstract

In this study,the microstructures of the directionally solidified FCC/B2 dual-phase high-entropy alloy were tailored based on different heat treatment processes to improve the mechanical properties in a wide temperature range.The microstructure evolution mechanism under different heat treatment regimes was clarified,and the influence of microstructures on the mechanical properties of the alloy was analyzed.The results show that high-density near spherical L12 precipitates can be obtained in the FCC matrix,while lath-like L12 precipitates can be obtained in the B2 phase after solution treatment followed by double aging at high-temperature 800℃and low-temperature 650℃.High-density precipitates effectively strengthen the alloy,and the L12 phase can promote dislocation movement in the B2 phase,which is beneficial to improve the plasticity of the alloy at the same time.Compared to the as-cast sample,the comprehensive high-temperature mechanical properties of the alloy after heat treatment are improved.

关键词

定向凝固/高熵合金/热处理/高温力学性能/微观组织表征

Key words

Directional-solidification/High-entropy alloys/Heat treatment/High-temperature mechanical properties/Microstructural characterization

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出版年

2024
航空制造技术
北京航空制造工程研究所

航空制造技术

CSTPCD北大核心
影响因子:0.403
ISSN:1671-833X
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