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金属学报  2026, Vol. 62 Issue (6): 1021-1031    DOI: 10.11900/0412.1961.2025.00348
  研究论文 本期目录 | 过刊浏览 |
AlCrFeCoNi低膨胀合金的成分设计及组织和性能优化
许鼎锋1,2, 韩飞扬1,2, 姜琦成1,2, 王欢1,2, 尚利媛1,2, 卢一平1,2()
1 大连理工大学 材料科学与工程学院 辽宁省凝固控制与数字化制备技术重点实验室 大连 116024
2 大连理工大学 材料科学与工程学院 辽宁省高熵合金材料工程研究中心 大连 116024
Composition Design and Optimization of Microstructure and Properties for an AlCrFeCoNi Low-Expansion Alloy
XU Dingfeng1,2, HAN Feiyang1,2, JIANG Qicheng1,2, WANG Huan1,2, SHANG Liyuan1,2, LU Yiping1,2()
1 Key Laboratory of Solidification Control and Digital Preparation Technology (Liaoning Province), School of Materials Science and Engineering, Dalian University of Technology, Dalian 116024, China
2 Engineering Research Center of High-Entropy Alloy Materials (Liaoning Province), School of Materials Science and Engineering, Dalian University of Technology, Dalian 116024, China
引用本文:

许鼎锋, 韩飞扬, 姜琦成, 王欢, 尚利媛, 卢一平. AlCrFeCoNi低膨胀合金的成分设计及组织和性能优化[J]. 金属学报, 2026, 62(6): 1021-1031.
Dingfeng XU, Feiyang HAN, Qicheng JIANG, Huan WANG, Liyuan SHANG, Yiping LU. Composition Design and Optimization of Microstructure and Properties for an AlCrFeCoNi Low-Expansion Alloy[J]. Acta Metall Sin, 2026, 62(6): 1021-1031.

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摘要: 

针对传统因瓦(Invar)合金因室温屈服强度不足而难以应用于承重件的问题,本工作通过在FeCoNi合金体系中引入Al、Cr元素并结合热机械处理,旨在开发兼具低膨胀与高强度的新型Al1Cr1(Fe65Co4Ni31)98合金。结果表明,该合金经热机械处理后晶粒显著细化,马氏体体积分数升高至8.91%,并伴随孪晶和高密度缺陷的生成。在-60~100 ℃范围内,合金热膨胀系数降低至1.10 × 10-6~2.04 × 10-6-1。除了Invar效应外,这种低膨胀行为还源于升温过程中马氏体相减少引起的体积收缩部分抵消了晶格热振动,以及界面和缺陷抑制了非谐性晶格振动,同时该微观组织特征使合金的屈服强度和抗拉强度分别达到324和452 MPa,断后伸长率保持在20%以上。与典型的Fe-Ni系Invar合金相比,本工作设计的合金在具有高比强度的同时保持了较低的热膨胀系数,表明合金成分设计与热机械处理的协同优化能够在低膨胀与力学性能之间实现优异平衡,为形变敏感构件的材料设计提供了新思路。

关键词 因瓦合金低膨胀热机械处理马氏体力学性能    
Abstract

Low-expansion alloys are essential structural-functional materials for advanced technologies requiring stringent dimensional stability. They are key components in precision metrology, electronic and microwave devices, cryogenic systems, and ultraprecision manufacturing equipments, where thermal deformation must be strictly controlled. However, conventional Fe-Ni Invar alloys possess insufficient mechanical strength despite their exceptionally low coefficient of thermal expansion, which limits their applicability in load-bearing environments. Design concept of high-entropy alloys offer a promising pathway to overcome this limitation through multiprinciple element alloy design and the associated synergistic effects. In this work, a novel low-expansion alloy, Al1Cr1(Fe65Co4Ni31)98, was developed by introducing Al and Cr into the multicomponent system and applying thermomechanical processing to tailor and refine its microstructure. This design strategy aims to achieve the synergistic optimization of thermal expansion behavior and mechanical performance. Additionally, in situ XRD during heating was employed to elucidate the underlying mechanism and monitor phase evolution. After thermomechanical processing, the alloy exhibited pronounced grain refinement and an increased martensite volume fraction of 8.91%. The microstructure further contained abundant deformation twins and a high density of lattice defects, which collectively enhanced the mechanical strength and thermal stability. Within the temperature range of -60 oC to 100 oC, the coefficient of thermal expansion decreased to 1.10 × 10-6-2.04 × 10-6oC-1. In addition to the Invar effect, this ultralow expansion behavior is attributed to the partial compensation of lattice thermal vibrations by the volume contraction associated with martensite reduction during heating, together with the suppression of anharmonic lattice vibrations induced by interfaces and defects. Meanwhile, the refined microstructure delivered an excellent combination of strength and ductility, achieving a yield strength of 324 MPa, an ultimate tensile strength of 452 MPa, and a fracture elongation greater than 20%. Compared with conventional Invar alloys, the designed alloy exhibited a higher specific strength while maintaining a low coefficient of thermal expansion. These results demonstrate that the synergistic optimization of compositional design and thermomechanical processing enables the exceptional integration of low thermal expansion with robust mechanical properties, offering valuable guidance for developing dimensionally stable structural alloys.

Key wordsInvar alloy    low expansion    thermomechanical processing    martensite    mechanical property
收稿日期: 2025-10-29     
ZTFLH:  TG132.1  
基金资助:国家自然科学基金项目(U2341261);辽宁省科技计划联合计划项目(2024JH2/102600019);大连市高层次人才创新支持计划项目(2023RG006)
通讯作者: 卢一平,luyiping@dlut.edu.cn,主要从事先进合金的设计与制备研究
Corresponding author: LU Yiping, professor, Tel: (0411)84709400, E-mail: luyiping@dlut.edu.cn
作者简介: 许鼎锋,男,1996年生,博士生
第一联系人:韩飞扬(共同第一作者),男,2002年生,硕士生
AlloyFeCoNiAlCr
Al0.5Cr0.564.353.9630.690.500.50
Al1Cr163.703.9230.381.001.00
Al1.5Cr1.563.053.8830.071.501.50
表1  低膨胀合金的名义成分 (atomic fraction / %)
图1  均匀化热处理后低膨胀合金的热膨胀系数和拉伸力学性能
AlloyYS / MPaUTS / MPaTE / %
Al0.5Cr0.520131644
Al1Cr121339050
Al1.5Cr1.526337846
表2  均匀化热处理后低膨胀合金的拉伸强度和塑性
图2  均匀化热处理后低膨胀合金微观组织的电子探针表征
图3  Al1Cr1合金的物相分析
Item

fcc

(111)

bcc

(110)

fcc

(200)

bcc

(200)

fcc

(220)

bcc

(211)

fcc

(311)

fcc

(222)

Rhkl100.0100.042.250.017.680.06.54.5
40 oC13523.02784.002114.34497.251147.74424.121189.31544.36
50 oC13501.09769.092104.07447.971117.16441.421092.35524.49
60 oC13318.11754.632138.23489.521147.14434.471270.59530.41
70 oC13408.39754.182162.88478.251180.26431.021263.75516.45
80 oC13627.21755.642149.57477.471151.49405.401178.39539.94
90 oC13394.20758.282137.34435.911110.13425.501136.75549.34
100 oC13571.93749.342143.34443.711104.66396.191149.75535.87
表3  图3b中衍射峰强度的理论值和不同温度下的测量值
图4  热机械处理后Al1Cr1合金的热膨胀系数和拉伸力学性能
图5  热机械处理后Al1Cr1合金的微观组织表征
图6  热机械处理后Al1Cr1合金的原位升温XRD谱
Temperature oCaγ nmaα nmfγ %fα %
400.3592570.28676592.02057.9795
500.3592780.28678692.12547.8746
600.3592950.28678892.12717.8729
700.3593020.28680292.21187.7882
800.3593140.28680792.31907.6810
900.3593350.28681092.41097.5891
1000.3593460.28682092.49927.5008
表4  热机械处理后Al1Cr1合金不同温度下各相的晶格常数和体积分数
图7  Al1Cr1合金的差示扫描量热曲线
图8  比强度与热膨胀系数的Ashby图[10,11,36~49]
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