金属热处理 ›› 2025, Vol. 50 ›› Issue (3): 113-117.DOI: 10.13251/j.issn.0254-6051.2025.03.018

• 工艺研究 • 上一篇    下一篇

时效温度对2195铝锂合金应力松弛时效行为的影响

张力文, 刘强, 豆卫涛   

  1. 西安航空职业技术学院 航空制造工程中心, 陕西 西安 710089
  • 收稿日期:2024-09-16 修回日期:2025-01-22 出版日期:2025-03-25 发布日期:2025-05-14
  • 作者简介:张力文(1989—),男,副教授,博士研究生,主要研究方向为铝合金蠕变时效成形,E-mail:375350782@qq.com
  • 基金资助:
    西安航空职业技术学院2023年度校级重点项目—陕西高校青年创新团队“航空关键结构件精确控形控性技术应用创新团队”(23XHZK-05)

Effect of aging temperature on stress relaxation aging behavior of 2195 Al-Li alloy

Zhang Liwen, Liu Qiang, Dou Weitao   

  1. Aerospace Manufacturing Engineering Center, Xi'an Aeronautical Polytechnic Institute, Xi'an Shaanxi 710089, China
  • Received:2024-09-16 Revised:2025-01-22 Online:2025-03-25 Published:2025-05-14

摘要: 对2195铝锂合金进行加载应力250 MPa、不同温度(160、170、180 ℃)时效17 h的应力松弛时效试验,并利用MTS CMT5205万能材料试验机和扫描透射电镜研究了时效温度对2195铝锂合金应力松弛行为、力学性能及析出相的影响。结果表明,不同时效温度下,合金的应力松弛曲线均表现出两个阶段特征:应力松弛速率减小阶段和恒速应力松弛阶段。随着时效温度增加,初始应力松弛速率和蠕变应变均增大,180 ℃下应力松弛17 h后的蠕变应变比160 ℃的提高了约62%,表明提高时效温度可以促进应力松弛过程和蠕变应变的累积。此外,合金的拉伸强度随着时效温度的升高而增大。在180 ℃时效条件下,合金的屈服强度和抗拉强度较160 ℃的分别提高了约20%和10%,而断后伸长率随时效温度升高而降低,180 ℃时效条件下的断后伸长率较160 ℃的下降约27.6%。不同时效温度下,合金中析出相均为T1相,且随时效温度增加,T1相分布更弥散、数量更多、尺寸更细小,有利于提高合金的强度。

关键词: 2195铝锂合金, 时效温度, 应力松弛, 析出相

Abstract: Stress relaxation aging tests were conducted on 2195 Al-Li alloy under a loading stress of 250 MPa, with aging at different temperatures (160, 170 and 180 ℃) for 17 h. The effect of aging temperature on the stress relaxation behavior, mechanical properties, and precipitates of the alloy was investigated by using MTS CMT5205 universal material testing machine and scanning transmission electron microscope (STEM). The results show that the stress relaxation curves exhibit two distinct stages: a stage of decreasing stress relaxation rate followed by a stage of constant stress relaxation rate. As the aging temperature increases, both the initial stress relaxation rate and creep strain are enhanced. Specifically, the creep strain after stress relaxation at 180 ℃ for 17 h is approximately 62% higher than that at 160 ℃, indicating that increasing the aging temperature can accelerate the stress relaxation process and the accumulation of creep strain. Furthermore, the tensile strength of the alloy increase with the rising of aging temperature. Under the aging condition of 180 ℃, the yield strength and tensile strength of the alloy are approximately 20% and 10% higher, respectively, than those at 160 ℃. Meanwhile, the elongation after fracture decreases as the temperature rises, and that under the aging condition of 180 ℃ is about 27.6% lower than that at 160 ℃. At different aging temperatures, the precipitated phase in the alloy is always the T1 phase. Moreover, as the aging temperature increases, the T1 phase becomes more dispersedly distributed, with a larger quantity and smaller size, which is beneficial for enhancing the strength of the alloy.

Key words: 2195 Al-Li alloy, aging temperature, stress relaxation, precipitated phase

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