首页> 外文期刊>Engineering Fracture Mechanics >An applied method for fatigue life assessment of engineering components using rigid-insert crack closure model
【24h】

An applied method for fatigue life assessment of engineering components using rigid-insert crack closure model

机译:使用刚性插入裂纹闭合模型对工程部件疲劳寿命评估的应用方法

获取原文
获取原文并翻译 | 示例
           

摘要

The purpose of this paper is to provide a new method for analyzing and evaluating the fatigue crack closure load and estimating the life of engineering components using RICC (Rigid-Insert Crack Closure Model), non-destructive replica technique, and a new sample. For this purpose, first, the method of solving the RICC model has been changed from linear approximation to nonlinear state and therefore, a significant improvement in the accuracy of the model results has been achieved. Then, using the model, a new formulation for the influence line in the points of sample is obtained, which has a significant accuracy. The formulation of the RICC model results in a set of equations that can help to determine the closure load and the characteristics of the load-displacement diagram using the residual crack mouth opening displacement in zero load (residual CMOD), which is the only empirical input parameter of Model. The new formulation method has been applied to a standard sample that has the same conditions as a real instance. The amount of residual crack openness in zero load (crack residual displacement) was measured using the replica technique and COD-gage simultaneously on a standard sample and were investigated using the obtained relationships and the accuracy of the outcomes. To prove the reliability, model results have been investigated through doing the experimental tests on aluminum alloys. Finally, the results obtained from the proposed relationship for the analysis and evaluation of the crack closure load and fatigue life were compared with the experimental results, which showed acceptable results.
机译:本文的目的是提供一种新方法,用于分析和评估疲劳裂纹闭合负荷,并使用RICC(刚性插入裂缝闭合模型),非破坏性复制品技术和新样品估算工程部件的寿命。为此目的,首先,求解RICC模型的方法已经从线性近似改变为非线性状态,因此,已经实现了模型结果的准确性的显着改善。然后,使用该模型,获得样品点中的影响线的新配方,其具有显着的精度。 RICC模型的配方导致一组方程,其可以帮助使用零负荷(残差CMOD)中的残余裂缝口开口位移来确定闭合载荷和负载 - 位移图的特性,这是唯一的经验输入模型参数。新的配方方法已应用于具有与实例相同的条件的标准样本。在标准样品上同时使用复制品技术和COD-Gage测量零载荷(裂纹残留位移)的残留裂纹开放量,并使用所获得的关系和结果的准确性来研究。为了证明可靠性,通过在铝合金上进行实验试验,研究了模型结果。最后,与实验结果进行了比较了从拟议的裂缝闭合载荷和疲劳寿命的分析和评估的关系中获得的结果,其显示出可接受的结果。

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