塑性区对增材制造316L多轴缺口疲劳影响研究
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作者单位:

南京航空航天大学飞行器先进设计技术国防重点学科实验室,南京 210016

作者简介:

通讯作者:

王英玉,女,副教授,E-mail:yywang@nuaa.edu.cn。

中图分类号:

V215.2

基金项目:

国家自然科学基金(51875276)。


Effect of Plastic Region on Multiaxial Notch Fatigue Life of Additive Manufactured 316L
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Affiliation:

Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle, Nanjing University of Aeronautics & Astronautics, Nanjing 210016, China

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    摘要:

    采用疲劳试验和有限元分析相结合的方法,研究了选区激光熔化增材制造316L不锈钢缺口件在多轴载荷下缺口根部塑性区及其对缺口件疲劳寿命的影响。对增材制造316L不锈钢缺口件进行了单轴、比例和90°非比例路径下的疲劳试验,研究了缺口几何尺寸、载荷水平和载荷路径等对缺口根部塑性区的影响,在此基础上提出了缺口根部塑性区的表征方法,利用缺口根部最大von Mises应力和提出的塑性区影响因子f构造疲劳损伤参量,结合光滑件的单轴S-N曲线预测缺口件的多轴疲劳寿命。试验结果证明本文所提出方法的预测疲劳寿命大多在3倍误差分散带以内。

    Abstract:

    The plastic region at the notch root under multiaxial loading and its effect on fatigue life of 316L stainless steel notched specimens manufactured by selective laser melting are studied by means of fatigue tests and finite element analysis. The fatigue tests of 316L stainless steel notched specimens that are additively manufactured are carried out under uniaxial, proportional and 90° non-proportional loading paths. The effects of notch geometry, stress amplitude and loading path on the plastic region at the notch root are studied. Based on this, the characterization methods of plastic regions at the notch root are proposed. The fatigue damage parameters are constructed by using the maximum von Mises stress at the notch root and the proposed plastic region influence factor f. Finally, the multiaxial fatigue lives of notched specimens are estimated by the proposed method in conjunction with the uniaxial S-N curve of smooth specimens. The results demonstrate that the majority of the estimated lives by using the proposed method fall within the three-time scatter band.

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引用本文

王英玉,董星亮,龚帅,姚卫星.塑性区对增材制造316L多轴缺口疲劳影响研究[J].南京航空航天大学学报,2022,54(1):140-149

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  • 收稿日期:2021-02-06
  • 最后修改日期:2021-05-25
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  • 在线发布日期: 2022-02-05
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