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Relation between crack growth behaviour and crack front morphology under hold-time conditions in DA Inconel 718

机译:保持时间下DA Inconel 718中裂纹扩展行为与裂纹前沿形态之间的关系

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摘要

The crack growth behaviour of Direct Aged Inconel 718 was studied at 550 ℃. Experiments were carried out under pure fatigue cycles, hold-time cycles of different durations and a mix of both. Hold-time cycles were systematically associated with complex crack front morphologies. A new numerical approach was developed to assess the effect of crack front morphology on the direct current potential drop technique, mechanical fields at the crack tip and ultimately, measured crack growth rates. Using this approach, a clear relation was established between crack front morphology and its evolution, and the crack growth behaviour under hold-time conditions. Complex crack front morphologies are demonstrated to be responsible for increased crack growth rates. From this, a crack growth mechanism under hold-time conditions is proposed. Finally, the numerical framework here presented is to be considered as a new, easily reproducible, way to properly analyse experimental data when dealing with complex loading cycles and complex crack front morphologies.
机译:在550℃下研究了Direct Aged Inconel 718的裂纹扩展行为。实验是在纯疲劳周期,不同持续时间的保持时间周期以及两者的混合下进行的。保持时间周期与复杂的裂纹前形态有系统地关联。开发了一种新的数值方法来评估裂纹前沿形态对直流电势下降技术,裂纹尖端的机械场以及最终测得的裂纹扩展速率的影响。使用这种方法,在保持时间条件下,裂纹前沿形态与其演化以及裂纹扩展行为之间建立了明确的关系。复杂的裂纹前形态被证明是导致裂纹扩展速率增加的原因。据此,提出了在保持时间条件下的裂纹扩展机制。最后,这里介绍的数值框架被认为是一种在处理复杂的载荷循环和复杂的裂纹前沿形态时能正确分析实验数据的新方法,易于重现。

著录项

  • 来源
    《International Journal of Fatigue》 |2017年第3期|17-27|共11页
  • 作者单位

    Safran Aircraft Engines, etablissement de Villaroche, 77550 Moissy-Cramayel, France,ONERA, The French Aerospace Lab., 29 avenue de la division Leclerc, 92320 Chatillon, France;

    CIRIMAT, INP-ENSIACET, 4 allee Emile Monso, BP 44342, 31010 Toulouse Cedex 4, France;

    ONERA, The French Aerospace Lab., 29 avenue de la division Leclerc, 92320 Chatillon, France;

    ONERA, The French Aerospace Lab., 29 avenue de la division Leclerc, 92320 Chatillon, France;

    Safran Aircraft Engines, etablissement de Villaroche, 77550 Moissy-Cramayel, France;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Crack growth; Hold-time; Crack front shape; Potential drop; DA Inconel 718;

    机译:裂纹增长;保持时间;前部裂纹形状;潜在下降;DA Inconel 718;

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