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Microstructural evolution and mechanical behavior of friction spot welded 2198-T8 Al-Li alloy during aging treatment

机译:时效处理中摩擦点焊2198-T8 Al-Li合金的组织演变和力学行为

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摘要

The microstructure and mechanical properties of friction spot welding (FSpW) 2198-T8 alloy during aging treatment were studied. Whereafter, the fracture process before and after aging treatment was observed by using the in-situ straining transmission electron microscopy method. The results show that fined equiaxed grains remained with predominant T-1 phase re-precipitated in the microstrucuture of FSpW 2198-T8 Al-Li alloy after aging treatment. With the extension of holding time (12 h -48 h), grains gradually grew up in the range of 9.2-13.2 mu m and the size and volume fraction of T-1 phases were also increased. Tensile strengths of thermal-mechanical coupling zone (TMCZ) of FSpW 2198-T8 alloy first increased and then decreased after aging treatment. When aging at 175 degrees C for 36 h, the strength reached the maximum (435 MPa) with the elongation decreased to 11.4%. Meanwhile, the fracture mode of TMCZ zone transformed from ductile brittle mixed fracture to brittle fracture after aging treatment. And cracks initiated at and propagated along precipitate-free zones (PFZs) after aging treatment. (C) 2016 Elsevier Ltd. All rights reserved.
机译:研究了摩擦点焊(FSpW)2198-T8合金时效处理的组织和力学性能。之后,通过原位应变透射电子显微镜法观察时效处理前后的断裂过程。结果表明,时效处理后的FSpW 2198-T8 Al-Li合金的显微组织中保留了细小的等轴晶粒,且主要的T-1相重新析出。随着保温时间的延长(12 h -48 h),晶粒在9.2-13.2μm的范围内逐渐长大,T-1相的尺寸和体积分数也增加。 FSpW 2198-T8合金的热机械耦合区(TMCZ)的拉伸强度在时效处理后首先增加,然后降低。当在175摄氏度下老化36小时时,强度达到最大值(435 MPa),而伸长率降低至11.4%。同时,TMCZ区的断裂方式从延性脆性混合断裂转变为时效处理后的脆性断裂。时效处理后,裂纹在无沉淀区(PFZs)处开始并沿裂纹扩展。 (C)2016 Elsevier Ltd.保留所有权利。

著录项

  • 来源
    《Materials & design》 |2017年第2期|224-230|共7页
  • 作者单位

    Beijing Univ Aeronaut & Astronaut, Sch Mat Sci & Engn, Key Lab Aerosp Mat & Performance, Natl Minist Educ, Beijing 100191, Peoples R China;

    Beijing Univ Aeronaut & Astronaut, Sch Mat Sci & Engn, Key Lab Aerosp Mat & Performance, Natl Minist Educ, Beijing 100191, Peoples R China;

    Aluminum Corp China, Beijing 100082, Peoples R China;

    Beijing Univ Aeronaut & Astronaut, Sch Mat Sci & Engn, Key Lab Aerosp Mat & Performance, Natl Minist Educ, Beijing 100191, Peoples R China;

    Beijing Univ Aeronaut & Astronaut, Sch Mat Sci & Engn, Key Lab Aerosp Mat & Performance, Natl Minist Educ, Beijing 100191, Peoples R China;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Al-Li alloy; Friction spot welding; Aging treatment; Microstructural evolution; Mechanical property;

    机译:铝锂合金;摩擦点焊;时效处理;组织演变;力学性能;

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