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材料研究学报  2026, Vol. 40 Issue (6): 474-480    DOI: 10.11901/1005.3093.2025.274
  研究论文 本期目录 | 过刊浏览 |
热处理温度对FeCrVTa0.1W0.1Ti0.1C0.17 多组元合金组织与性能的影响
郭威1,2,3, 张月林1,2, 曹梓恒1,2, 李龙丰1,2, 赵觅4(), 吴树森1,2
1.华中科技大学 材料成形与模具技术全国重点实验室 武汉 430074
2.华中科技大学材料科学与工程学院 武汉 430074
3.深圳华中科技大学研究院 深圳 518057
4.华中科技大学航空航天学院 武汉 430074
Effect of Heat Treatment Temperature on Microstructure and Properties of FeCrVTa0.1W0.1Ti0.1C0.17 Alloy of Multi-components
GUO Wei1,2,3, ZHANG Yuelin1,2, CAO Ziheng1,2, LI Longfeng1,2, ZHAO Mi4(), WU Shusen1,2
1.State Key Laboratory of Materials Processing and Die & Mould Technology, Huazhong University of Science and Technology, Wuhan 430074, China
2.School of Materials Science and Engineering, Huazhong University of Science and Technology, Wuhan 430074, China
3.Shenzhen Huazhong University of Science and Technology Research Institute, Shenzhen 518057, China
4.School of Aerospace Engineering, Huazhong University of Science and Technology, Wuhan 430074, China
引用本文:

郭威, 张月林, 曹梓恒, 李龙丰, 赵觅, 吴树森. 热处理温度对FeCrVTa0.1W0.1Ti0.1C0.17 多组元合金组织与性能的影响[J]. 材料研究学报, 2026, 40(6): 474-480.
Wei GUO, Yuelin ZHANG, Ziheng CAO, Longfeng LI, Mi ZHAO, Shusen WU. Effect of Heat Treatment Temperature on Microstructure and Properties of FeCrVTa0.1W0.1Ti0.1C0.17 Alloy of Multi-components[J]. Chinese Journal of Materials Research, 2026, 40(6): 474-480.

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摘要: 

研究了不同热处理温度对FeCrVTa0.1W0.1Ti0.1C0.17多组元合金显微组织与力学性能的影响。结果表明,在800 ℃、900 ℃热处理的合金中析出的晶内细密Laves相产生强化作用使其强度显著提高(屈服强度达1501 MPa),但是晶界上的富Fe相随着热处理温度的提高由孤立枝晶演变为连续网状结构,成为裂纹扩展优先路径而使合金的塑性下降。在1000 ℃热处理的合金中Laves相的粗化严重弱化其强化作用,而富Fe相则转变为孤立的团块状缓解了晶界脆性使塑性恢复到28.9%、而强度回复到铸态水平。富Fe相的形貌(连通性)是调控FeCrV基多组元合金塑性的关键因素,而Laves相的尺寸影响强度的演变。

关键词 金属材料多主元合金热处理微观组织力学性能析出强化    
Abstract

FeCrV-based alloy FeCrVTa0.1W0.1Ti0.1C0.17 was prepared by vacuum arc melting technique, and subjected to vacuum heat treatment. Then the effect of heat treatment temperatures (800 oC, 900 oC, 1000 oC) on its microstructure and mechanical properties were investigated viacompression tester, hardness tester, scanning electron microscopy, electron probe microanalyzer and X-ray diffractometer. It reveals that heat treatments at 800 and 900 oC may significantly enhance the alloy strength (yield strength up to 1501 MPa) through precipitation strengthening by fine intragranular Laves phases. However, as temperature increases, the Fe-rich phase at grain boundaries evolves from isolated dendrites into a continuous network structure, acting as a preferential path for crack propagation and leading to reduced ductility. At 1000 oC, coarsening of Laves phases severely weakens their strengthening effect, while the Fe-rich phase transforms into isolated blocky particles, alleviating grain boundary embrittlement and restoring ductility to 28.9%, with strength returning to the as-cast level. The results demonstrate that the morphology (connectivity) of the Fe-rich phase is the key factor governing ductility, while the size of Laves phases dominates the evolution of strength. This finding provides a reference for balancing the strength-ductility of FeCrV-based alloys of multi-components.

Key wordsmetallic materials    multi-principal element alloy    heat treatment    microstructure    mechanical properties    precipitation strengthening
收稿日期: 2025-09-11     
ZTFLH:  TG139  
基金资助:国家自然科学基金(52201075);湖北省重点研发计划(2025BAB012);湖北省自然科学基金(2023AFB798);深圳市科技计划(JCYJ20220530160813032);深圳市科技计划(JCYJ20240813153421029)
通讯作者: 赵觅,副教授,zhaomi2018@hust.edu.cn,研究方向为高温结构材料与金属高温腐蚀防护
Corresponding author: ZHAO Mi, Tel: 17508640660, E-mail: zhaomi2018@hust.edu.cn
作者简介: 郭 威,男,1987年生,副研究员
图1  在不同温度热处理后FeCrVTa0.1W0.1Ti0.1C0.17合金的XRD谱
图2  HT800不同倍率的SEM照片
AlloyFeCrVTiTaWC
HT80041.0821.2529.090.710.853.757.70
HT90040.0120.9128.440.190.631.308.52
HT100040.6623.9329.770.620.861.912.26
表1  在不同温度热处理后FeCrVTa0.1W0.1Ti0.1C0.17 合金晶界处富Fe 相的元素
图3  HT900的SEM照片
图4  HT900合金的EDS元素面分布
图5  HT1000微观组织SEM照片
图6  在不同温度热处理后FeCrVTa0.1W0.1Ti0.1C0.17合金的力学性能
AlloyHardness (HV0.2)Yield strength / MPaBreaking strength / MPaPlastic strain / %Breaking strain / %
RT637.1 ± 5.21350 ± 162664 ± 1533.8 ± 0.135.8 ± 0.1
HT800741.0 ± 6.81459 ± 122573 ± 1417.0 ± 0.319.0 ± 0.3
HT900774.2 ± 7.91501 ± 152352 ± 158.9 ± 0.110.7 ± 0.1
HT1000707.6 ± 6.21351 ± 122665 ± 1528.9 ± 0.230.8 ± 0.2
表2  在不同温度热处理后FeCrVTa0.1W0.1Ti0.1C0.17合金的力学性能
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