首页> 外文期刊>International Journal of Fatigue >Modelling of the fatigue crack growth of a coated single crystalline nickel-based superalloy under thermal mechanical loading
【24h】

Modelling of the fatigue crack growth of a coated single crystalline nickel-based superalloy under thermal mechanical loading

机译:热机械载荷下镀层单晶镍基高温合金疲劳裂纹扩展的建模

获取原文
获取原文并翻译 | 示例
           

摘要

The focus of this paper is the simulation of fatigue crack growth of the coated single crystalline nickel-based superalloy PWA 1484 under thermal mechanical loading. Thus, two physical models are superimposed in terms to firstly calculate the deformation behavior under instationary thermal and mechanical loading (TMF) and secondly to model crack propagation after initial brittle cracking of the coating layer on the basis of cyclic crack tip opening displacement (CTOD). All material parameters implemented in the models were evaluated from monotonic isothermal tensile and creep tests as well as from isothermal low cycle fatigue (LCF) experiments. The calculated fatigue crack growth was validated by in situ crack growth measurements using the beachmark technique. Hence, crack propagation initiated by the brittle coating system closely to the experimental results using rectangular flat specimen geometry instead of corner-crack (CC) specimens. The comparison of the simulated lifetimes to the experimental results provides remarkable accuracy of the physically-based lifetime model.
机译:本文的重点是在热机械载荷下模拟镀层单晶镍基高温合金PWA 1484的疲劳裂纹扩展。因此,两个物理模型的叠加方式是:首先计算在稳态热和机械载荷(TMF)下的变形行为,其次基于循环裂纹尖端开口位移(CTOD)对涂层初始脆性开裂后的裂纹扩展进行建模。 。通过单调等温拉伸和蠕变测试以及等温低周疲劳(LCF)实验评估了模型中实现的所有材料参数。计算出的疲劳裂纹扩展通过使用滩涂技术的现场裂纹扩展测量进行了验证。因此,由脆性涂层系统引发的裂纹扩展接近于使用矩形扁平样品几何体而不是角裂纹(CC)样品的实验结果。仿真寿命与实验结果的比较为基于物理的寿命模型提供了显着的准确性。

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