金属热处理 ›› 2020, Vol. 45 ›› Issue (6): 149-152.DOI: 10.13251/j.issn.0254-6051.2020.06.031

• 组织与性能 • 上一篇    下一篇

中熵共晶CrCoNiNb0.4合金层状组织的热稳定性

王诚杰, 黄春华, 李剑文   

  1. 昌河飞机工业集团有限责任公司, 江西 景德镇 333002
  • 收稿日期:2019-12-07 出版日期:2020-06-25 发布日期:2020-09-02
  • 作者简介:王诚杰(1992—),男,助理工程师,硕士,主要研究方向为铁基非晶合金和高熵合金,E-mail:1505336491@qq.com

Lamellar structure thermal stability of inmedium-entropy eutectic CrCoNiNb0.4 alloy

Wang Chengjie, Huang Chunhua, Li Jianwen   

  1. AVIC Changhe Aircraft Industrygroup Co., Ltd., Jingdezhen Jiangxi 333002, China
  • Received:2019-12-07 Online:2020-06-25 Published:2020-09-02

摘要: 对CrCoNiNb0.4中熵共晶合金层片状组织的热稳定性进行了研究。结果表明:CrCoNiNb0.4合金共晶层状组织在1023 K及以下温度可以保持较长时间的热稳定性;随热处理时间从24 h增加至168 h,CrCoNiNb0.4合金共晶片层厚度从约0.19 μm增加至约0.39 μm,且片层间隙析出相逐渐增多,同时伴随着边界断裂,边缘球化等层状失效形式的发生,在析出强化相以及层状组织失效的共同作用下,CrCoNiNb0.4合金共晶组织硬度值随热处理时间呈先增大后减小的趋势。

关键词: 中熵共晶合金, CrCoNiNb0.4, 热稳定性

Abstract: Thermal stability of lamellar structure in CrCoNiNb0.4 medium-entropy eutectic alloy was characterized and examined. The results show that the lamellar structures in CrCoNiNb0.4 medium-entropy alloy are stable when the heat treatment temperature is blower than 1023 K. While the heat treatment time increase from 24 h to 168 h, the lamellar spacing of lamellar structures in CrCoNiNb0.4 eutectic alloy increases from about 0.19 μm to about 0.39 μm, and more and more precipitation phases are detected in the lamellar spacing, meanwhile, boundary splitting and edge spheroidization can be found in CrCoNiNb0.4 eutectic alloy. The hardness of CrCoNiNb0.4 eutectic alloy shows a tendency of increase first and decrease later with the increase of heat treatment time under the synergy effect of precipitation strength and lamellar structure failure.

Key words: medium-entropy eutectic alloy, CrCoNiNb0.4, thermal stability

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