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高温高熵合金研究进展

李海洋 马兆龙 程兴旺

航空材料学报2025,Vol.45Issue(5):61-77,17.
航空材料学报2025,Vol.45Issue(5):61-77,17.DOI:10.11868/j.issn.1005-5053.2025.000081

高温高熵合金研究进展

Research progress in high-temperature high-entropy alloys

李海洋 1马兆龙 2程兴旺2

作者信息

  • 1. 北京理工大学材料科学与工程学院,北京 100081
  • 2. 北京理工大学材料科学与工程学院,北京 100081||冲击环境材料技术国家级重点实验室,北京 100081||北京理工大学唐山研究院,河北 唐山 063000||北京理工大学(珠海)材料智能研发实验室,广东 珠海 519088
  • 折叠

摘要

Abstract

High-temperature high-entropy alloys(HEAs)show potential to surpass traditional Ni-based alloys through multi-principal element synergy and microstructural regulation.This review systematically examines three systems:high-entropy superalloys(HESAs),refractory HEAs(RHEAs)and refractory high-entropy superalloys(RSAs).HESAs emulate the γ/γ′ dual-phase structure of Ni-based alloys,achieving comparable strength at 800-1000℃.RHEAs utilize refractory elements to form high-melting-point solid solutions with superior performance above 1200℃.RSAs innovate with BCC/B2 nanobasket structures,outperforming Ni-based alloys across 25-1200℃.Current challenges include poor room-temperature ductility,oxidation resistance and phase stability,demanding breakthroughs in multi-scale microstructure control,dynamic phase transformation mechanisms and high-throughput design.Future directions prioritize multi-objective composition optimization,advanced processing,cross-scale characterization,and service-condition evaluation systems to guide extreme-environment applications like aeroengine components and nuclear reactors,etc.

关键词

高温高熵合金/高熵高温合金/难熔高熵合金/难熔高熵超合金/成分设计/微观组织/力学性能

Key words

high-temperature high entropy alloy/high entropy superalloy/refractory high entropy alloy/refractory high entropy superalloy/composition design/microstructure/mechanical property

分类

航空航天

引用本文复制引用

李海洋,马兆龙,程兴旺..高温高熵合金研究进展[J].航空材料学报,2025,45(5):61-77,17.

基金项目

国家自然科学基金(52331006) (52331006)

河北省自然科学基金(E2024105020) (E2024105020)

航空材料学报

OA北大核心

1005-5053

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