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Al-Li合金搅拌摩擦焊搭接接头的疲劳性能

张丹丹 曲文卿 杨模聪 柴鹏

张丹丹, 曲文卿, 杨模聪, 等 . Al-Li合金搅拌摩擦焊搭接接头的疲劳性能[J]. 北京航空航天大学学报, 2013, 39(5): 674-678.
引用本文: 张丹丹, 曲文卿, 杨模聪, 等 . Al-Li合金搅拌摩擦焊搭接接头的疲劳性能[J]. 北京航空航天大学学报, 2013, 39(5): 674-678.
Zhang D, an, Qu Wenqing, et al. Fatigue property of Al-Li alloy friction stir welded lap joints[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(5): 674-678. (in Chinese)
Citation: Zhang D, an, Qu Wenqing, et al. Fatigue property of Al-Li alloy friction stir welded lap joints[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(5): 674-678. (in Chinese)

Al-Li合金搅拌摩擦焊搭接接头的疲劳性能

基金项目: 北京航空航天大学创新基金资助项目
详细信息
  • 中图分类号: TG453.9

Fatigue property of Al-Li alloy friction stir welded lap joints

  • 摘要: 通过疲劳寿命试验、疲劳断口和金相组织分析,研究了Al-Li合金搅拌摩擦焊搭接接头的疲劳性能,分析了接头前进侧热机影响区(TMAZ, Thermal-Mechanically Affected Zone)出现的"钩状缺陷"对其疲劳性能的影响.结果表明,钩状缺陷容易引起裂纹萌生及扩展,减小接头的有效承载板厚,适当缩短搅拌针长度可以改善钩状缺陷,提高接头力学性能.母材与搭接接头的疲劳S-N曲线研究表明:在高疲劳应力下,接头的疲劳寿命接近母材,但随着疲劳应力水平降低,接头的疲劳寿命急剧下降,200万循环周次下的疲劳强度仅达到80 MPa,为母材的35%.

     

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出版历程
  • 收稿日期:  2012-05-29
  • 修回日期:  2012-11-29
  • 网络出版日期:  2013-05-31

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