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Fretting fatigue damage accumulation and crack nucleation in high-strength steels.

机译:高强度钢的微动疲劳损伤累积和裂纹形核。

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摘要

The current research focused on the process of fretting fatigue crack nucleation and growth in two high strength structural steels: PH 13-8 Mo stainless steel and quenched and tempered 4340 steel. Carefully controlled fretting fatigue experiments were conducted to observe the influence of relative slip amplitude, contact size, and fatigue stress amplitude on the nature of the fretting fatigue cracking process and life of these two materials. Both materials experienced significant reductions in fatigue strength due to fretting, with PH 13-8 Mo stainless steel exhibiting a greater susceptibility to fretting than 4340 steel for the experimental conditions used. Cracks nucleated within the first 200 cycles of fretting fatigue, corresponding to less than 0.2% of the total fretting fatigue life, for both materials. In addition, significant damage was observed after 5,000 to 10,000 cycles of fretting fatigue. A significant refinement in grain size, characterized by a non-etch region and considerably higher hardness than the bulk material, was observed in PH 13-8 Mo stainless steel but not in 4340 steel. Possible reasons for this difference are presented and discussed. A fracture mechanics approach was implemented to estimate fatigue lives, which were compared to experimental fretting fatigue results. Cases of uniform cyclic stress and a linearly varying near surface cyclic stress field, which was used to simulate the presence of fretting stresses, were employed. Results indicate that such simplistic fracture mechanics methods can accurately characterize the fretting fatigue life at higher stress amplitudes where crack propagation would be expected to dominate the total fatigue life. Determination of the fretting fatigue behavior at stress amplitudes near the fretting fatigue limit is less amenable to the fracture mechanics methods used. Reasons for this are explored and possible methods to better determine fretting fatigue endurance limit behavior are discussed.
机译:当前的研究集中在两种高强度结构钢的微动疲劳裂纹成核和生长过程中:PH 13-8 Mo不锈钢和调质4340钢。进行了仔细控制的微动疲劳试验,以观察相对滑动幅度,接触尺寸和疲劳应力幅度对这两种材料的微动疲劳破裂过程的性质和寿命的影响。两种材料都因微动而使疲劳强度显着降低,在所使用的实验条件下,PH 13-8 Mo不锈钢比4340钢表现出更大的微动敏感性。对于这两种材料,裂纹在微动疲劳的前200个循环内成核,相当于小于微动疲劳总寿命的0.2%。此外,在微动疲劳5,000至10,000次循环后,观察到明显的损坏。在PH 13-8 Mo不锈钢中观察到晶粒尺寸的显着细化,其特征在于非蚀刻区域且硬度明显高于散装材料,而在4340钢中则未观察到。提出并讨论了造成这种差异的可能原因。实施了断裂力学方法来估计疲劳寿命,并将其与实验性微动疲劳结果进行了比较。使用了均匀的循环应力和线性变化的近表面循环应力场的情况,这些情况用于模拟微动应力的存在。结果表明,这种简单的断裂力学方法可以准确地表征较高应力振幅下的微动疲劳寿命,在该应力振幅下,裂纹扩展将主导总疲劳寿命。确定在微动疲劳极限附近的应力振幅下的微动疲劳行为不太适合所使用的断裂力学方法。探究了其原因,并讨论了更好地确定微动疲劳极限性能的可能方法。

著录项

  • 作者

    Pape, John Andrew.;

  • 作者单位

    Georgia Institute of Technology.;

  • 授予单位 Georgia Institute of Technology.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2002
  • 页码 298 p.
  • 总页数 298
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;
  • 关键词

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