| 2195铝锂合金应力松弛时效成形工艺制度 |
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| 引用本文： | 郑强,湛利华,杨有良,王庆.2195铝锂合金应力松弛时效成形工艺制度[J].上海航天,2020,37(3):68-75. |
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| 作者姓名： | 郑强 湛利华 杨有良 王庆 |
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| 作者单位： | 中南大学 机电工程学院，湖南 长沙 410083;中南大学 高性能复杂制造国家重点实验室，湖南 长沙 410083;中南大学 机电工程学院，湖南 长沙 410083;中南大学 高性能复杂制造国家重点实验室，湖南 长沙 410083;中南大学 轻合金研究院，湖南 长沙 410083 |
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| 基金项目： | 国家重点研发计划资助项目(2017YFB0306300);国家科技重大专项资助项目(2017ZX04005001);国家自然科学基金资助项目(51905551，51675538，51601060) |
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| 摘 要： | 以2195-T8态铝锂合金为研究对象,探究工艺参数对其应力松弛时效行为的影响规律。试样经过固溶、淬火,进行不同预变形、时效温度及时效时间条件下的应力松弛时效实验。通过室温拉伸,测得应力松弛时效后试样的力学性能。基于正交试验的极差分析和方差分析,探究了预变形、时效温度和时效时间3个工艺参数对应力松弛量、屈服强度和延伸率的影响权重占比;进一步研究发现预变形不仅可以提高2195铝锂合金时效后的强度,还降低了应力梯度对材料力学性能不均匀性的影响;查明了实现2195铝锂合金应力松弛时效形性协同制造的合理工艺制度:180℃+4%预变形+时效时间12～16 h。研究工作为大型铝锂合金构件应力松弛时效形性协同制造工艺窗口的确定提供了重要支撑。
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| 关 键 词： | 铝锂合金 应力松弛 力学性能 正交试验 应力松弛时效成形工艺 |
| 收稿时间： | 2020/1/29 0:00:00 |
| 修稿时间： | 2020/4/6 0:00:00 |
Stress Relaxation Aging Forming Process System of 2195 Al-Li Alloy |
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| ZHENG Qiang,ZHAN Lihu,YANG Youliang,WANG Qing.Stress Relaxation Aging Forming Process System of 2195 Al-Li Alloy[J].Aerospace Shanghai,2020,37(3):68-75. |
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| Authors: | ZHENG Qiang ZHAN Lihu YANG Youliang WANG Qing |
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| Institution: | School of Mechanical and Electrical Engineering, Central South University, Changsha 410083, Hunan, China;State Key Laboratory of High-Performance Complex Manufacturing, Central South University, Changsha 410083, Hunan, China;School of Mechanical and Electrical Engineering, Central South University, Changsha 410083, Hunan, China;State Key Laboratory of High-Performance Complex Manufacturing, Central South University, Changsha 410083, Hunan, China;Light Alloy Research Institute, Central South University, Changsha 410083, Hunan, China |
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| Abstract: | In this paper, 2195-T8 Al-Li alloy is taken as the research object to explore the influence rules of process parameters on its stress relaxation aging behavior. After solid solution and quenching, the samples are subjected to stress relaxation aging experiments under different pre-deformation, aging temperature, and aging time conditions. The mechanical properties of the samples after stress relaxation aging are measured by stretching at room temperature. Based on the range and variance analyses of the experimental results, the influence weight proportions of three process parameters, i.e., aging temperature, pre-deformation, and aging time, on the stress relaxation amount, yield strength, and elongation are investigated. Further research shows that the pre-deformation can not only improve the strength of 2195 Al-Li alloy after aging, but also reduce the stress gradient influence on the mechanical property nonuniformity of the material. The reasonable technological system for the precision-property collaborative manufacturing of 2195 Al-Li alloy with stress relaxation aging is found out:180 ºC + 4% pre-deformation + aging time in the range from 12 h to 16 h. The research work provides an important support for the determination of the precision-property cooperative manufacturing process window of large Al-Li alloy components with stress relaxation aging. |
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| Keywords: | Al-Li alloy stress relaxation mechanical property orthogonal test stress relaxation aging forming process |
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