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Effects of RRA Treatments on Microstructures and Properties of a New High-strength Aluminum-Lithium Alloy-2A97

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文摘 A new high strength 2A97 Al-Cu-Li-X alloy was subjected to triple-aging of retrogression and re-aging treatments (RRA). Transmission electron microscopy (TEM), differential scanning calorimetry (DSC), and tensile tests were used to investigate the effects of RRA treatment on the microstructures and properties. DSC test reveals the reversion temperature range of the strengthening δ' (Al3Li)phase. The results show that the microstructure consists of δ' (Al3Li) phase, T1 (Al2CuLi) phase and θ"/θ'(Al2Cu) phase for 2A97 alloy treated by a triple-aging ora retrogression and re-aging treatment in the following order: (1) at 165 ℃×30 min, (2) at 220 ℃ or 240 ℃×15 min, (3) at 165 ℃×24 h. The plastic deformation, incorporated into the treatment after secondary high temperature aging, promotes the T1 precipitation during final re-aging. The tensile properties of the alloy treated by the retrogression and re-aging treatment reach the peak level of alloy single-aged at 165 ℃ in T6 temper.
来源 Chinese Journal of Aeronautics ,2007,20(2):187-192 【核心库】
DOI 10.1016/s1000-9361(07)60031-4
关键词 2A97 ; Al-Cu-Li-X alloy ; RRA treatments ; triple aging;microstructure ; reversion
地址

1. School of Materials & Metallurgy, Northeastern University, Shenyang, 110004  

2. Beijing Institute of Aeronautical Materials, Beijing, 100095

语种 英文
文献类型 研究性论文
ISSN 1000-9361
学科 航空
基金 国家973计划
文献收藏号 CSCD:2911964

参考文献 共 12 共1页

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