首页> 外文期刊>International Journal of Fracture >ELEVATED TEMPERATURE FATIGUE CRACK GROWTH RATE MODEL FOR NI-BASE SUPERALLOYS
【24h】

ELEVATED TEMPERATURE FATIGUE CRACK GROWTH RATE MODEL FOR NI-BASE SUPERALLOYS

机译:基于镍的高温合金的高温疲劳裂纹扩展速率模型

获取原文
获取原文并翻译 | 示例
           

摘要

Several time-dependent mechanisms are operational in the crack growth process of Ni-base superalloys at elevated temperature. Creep deformation during periods of sustained loading, oxygen diffusion at the crack tip, and oxidation reactions at and in front of the crack tip all contribute to the kinetics of crack growth. A crack growth rate model has been derived that attempts to capture the physics of these various rate processes. The proposed model assumes small-scale creep at the crack tip and incorporates the Hutchinson-Rice-Rosengren stress field equations to satisfy this condition. The model also includes stress-assisted diffusion of an environmental species at the crack tip. A process reaction rate is related to the time-rate of crack growth providing a model that accounts for these time-dependent processes. An evaluation of the form of the model is provided by comparison of the model with experimental crack growth data.
机译:在高温下镍基高温合金的裂纹扩展过程中,有几种时间相关的机制起作用。持续载荷,蠕变在尖端处的氧气扩散以及尖端及其前端的氧化反应期间的蠕变变形都有助于裂纹扩展的动力学。已经得出了裂纹扩展速率模型,试图捕获这些不同速率过程的物理性质。提出的模型假设裂纹尖端出现小范围蠕变,并结合了Hutchinson-Rice-Rosengren应力场方程来满足该条件。该模型还包括裂纹尖端处环境物种的应力辅助扩散。过程反应速率与裂纹扩展的时间速率有关,从而提供了一个模型来说明这些与时间相关的过程。通过将模型与实验裂纹扩展数据进行比较,可以对模型的形式进行评估。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号