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Effect of pre-deformation on aging creep of Al-Li-S4 alloy and its constitutive modeling 被引量:9
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作者 王萌 湛利华 +2 位作者 杨有良 阳凌 黄明辉 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2015年第5期1383-1390,共8页
A set of uniaxial tensile creep tests at different pre-deformations, aging temperatures and stress levels were carried out for Al-Li-S4 alloy, and the creep behavior and the effects of pre-deformation on mechanical pr... A set of uniaxial tensile creep tests at different pre-deformations, aging temperatures and stress levels were carried out for Al-Li-S4 alloy, and the creep behavior and the effects of pre-deformation on mechanical properties and microstructures were determined under basic thermodynamics conditions of aging forming. The results show that pre-deformation shortens the time of primary creep and raises the second steady-state creep rate. Then, the total creep strain is greater, but in the range of test parameters it is still smaller than that without pre-deformation. In addition, transmission electron microscopy(TEM) observation shows that pre-deformation promotes the formation of T1 phase and θ′ phase and makes them distribute more dispersively, while inhibits the generation of δ′ phase, which leads to the improvement of mechanical properties of the alloy. A unified constitutive model reflecting the effects of aging mechanism, stress levels and different pre-deformations was established. The fitting results agree with the experimental data well. 展开更多
关键词 al-li-s4 alloy aging creep PRE-DEFORMATION mechanical properties microstructure constitutive model
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基于DFR法的Al-Li-S4铝锂合金铆接结构疲劳可靠性分析 被引量:5
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作者 陈安 许飞 +1 位作者 闫文伟 董登科 《航空工程进展》 CSCD 2016年第1期101-105,共5页
Al-Li-S4是新一代铝锂合金,常被用作机身材料,而铆接结构在飞机各个重要受力结构中也具有广泛的应用。为了研究Al-Li-S4铝锂合金铆接结构的疲劳性能,通过试验统计得到两种铆接结构的细节疲劳额定值(DFR),并借助扫描电镜观察其疲劳裂纹... Al-Li-S4是新一代铝锂合金,常被用作机身材料,而铆接结构在飞机各个重要受力结构中也具有广泛的应用。为了研究Al-Li-S4铝锂合金铆接结构的疲劳性能,通过试验统计得到两种铆接结构的细节疲劳额定值(DFR),并借助扫描电镜观察其疲劳裂纹的萌生和扩展行为。结果表明:Al-Li-S4铝锂合金铆接搭接结构的DFR值为102.24 MPa,铆钉填充锪窝孔连接结构的DFR值为169.41 MPa;Al-Li-S4铝锂合金疲劳断口的分析表征其具有良好的抗疲劳损伤性能。研究结果可为新型民用飞机选材、疲劳设计和寿命评估提供参考。 展开更多
关键词 细节疲劳额定值 al-li-s4铝锂合金 铆接结构 疲劳断口
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蠕变时效应力对Al-Li-S4合金变形及组织性能的影响和本构模型 被引量:3
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作者 杨英格 湛利华 黄明辉 《热加工工艺》 CSCD 北大核心 2016年第20期207-210,共4页
对Al-Li-S4合金进行了固溶、淬火及不同应力的高温蠕变时效试验,对蠕变后的试样进行了力学性能测试及TEM微观组织观察,研究了蠕变时效应力对该合金变形行为及微观组织与力学性能的影响。结果表明:与无应力时效相比,材料的强度及蠕变速... 对Al-Li-S4合金进行了固溶、淬火及不同应力的高温蠕变时效试验,对蠕变后的试样进行了力学性能测试及TEM微观组织观察,研究了蠕变时效应力对该合金变形行为及微观组织与力学性能的影响。结果表明:与无应力时效相比,材料的强度及蠕变速率都有明显的提升。通过对蠕变行为的分析,建立了Al-Li-S4合金的本构模型,进一步对试验数据回归,得到了蠕变本构方程中的材料常数。 展开更多
关键词 al-li-s4 合金 蠕变时效 力学性能 微观组织 本构模型
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Creep behavior and mechanical properties of Al-Li-S4 alloy at different aging temperatures 被引量:7
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作者 ZHOU Chang ZHAN Li-hua +8 位作者 SHEN Ru-lin ZHAO Xing YU Hai-liang HUANG Ming-hui LI He YANG You-liang HU Li-bin LIU De-bo HU Zheng-gen 《Journal of Central South University》 SCIE EI CAS CSCD 2020年第4期1168-1175,共8页
Creep age forming techniques have been widely used in aerospace industries. In this study, we investigated the effect of aging temperature(143 °C-163 °C) on the creep behavior of Al-Li-S4 aluminum alloy and ... Creep age forming techniques have been widely used in aerospace industries. In this study, we investigated the effect of aging temperature(143 °C-163 °C) on the creep behavior of Al-Li-S4 aluminum alloy and their mechanical properties at room temperature. The mechanical properties were tested by tensile testing, and the microstructural evolution at different aging temperatures was examined by transmission electron microscopy. Results show that the creep strains and the room-temperature mechanical properties after creep aging increase with the aging temperature. As the aging temperature increases, the creep strain increases from 0.018% at 143 °C to 0.058% at 153 °C, and then to 0.094% at 163 °C. Within 25 h aging, the number of creep steps increases and the duration time of the same steps is shortened with the growth of aging temperatures. Therefore, the increase in aging temperatures accelerates the progress of the entire creep. Two main strengthening precipitates θ′(Al2 Cu) and T1(Al2 Cu Li) phases were characterized. This work indicates that the creep strain and mechanical properties of Al-Li-S4 alloys can be improved by controlling aging temperatures. 展开更多
关键词 al-li-s4 alloy creep behavior mechanical properties aging temperature
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A unified constitutive model for multiphase precipitation and multi-stage creep ageing behavior of Al−Li−S4 alloy 被引量:4
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作者 He LI Li-hua ZHAN +5 位作者 Ming-hui HUANG Xing ZHAO Chang ZHOU Li-bin HU Zheng-gen HU De-bo LIU 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2021年第5期1217-1234,共18页
A unified constitutive model is presented to predict the recently observed“multi-stage”creep behavior of Al−Li−S4 alloy.The corresponding microstructural variables related to the yield strength and creep deformation... A unified constitutive model is presented to predict the recently observed“multi-stage”creep behavior of Al−Li−S4 alloy.The corresponding microstructural variables related to the yield strength and creep deformation of the alloy during the creep ageing process,including dislocations and multiple precipitates,have been characterized in detail by X-ray diffraction(XRD)and transmission electron microscopy(TEM).For the yield strength,the model considers the multiphase strengthening behavior of the alloy based on strengthening mechanisms,which includes shearable T1 precipitate strengthening,non-shearable T1 precipitate strengthening andθ′precipitate strengthening.Based on creep deformation mechanism,the“multi-stage”creep behavior of the alloy is predicted by introducing the effects of interacting microstructural variables,including the radius of multiple precipitates,dislocation density and solute concentration,into the creep stress−strain model.It is concluded that the results calculated by the model are in a good agreement with the experimental data,which validates the proposed model. 展开更多
关键词 constitutive modelling Al−Li−S4 alloy creep age forming MICROSTRUCTURES numerical algorithms
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