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首页> 外文期刊>International Journal of Fatigue >Experimental investigation of the time and temperature dependent growth of fatigue cracks in Inconel 718 and mechanism based lifetime prediction
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Experimental investigation of the time and temperature dependent growth of fatigue cracks in Inconel 718 and mechanism based lifetime prediction

机译:Inconel 718中疲劳裂纹的时间和温度依赖性增长的实验研究以及基于机理的寿命预测

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The following contribution deals with the growth of cracks in low-cycle fatigue (LCF) and thermomechan-ical fatigue (TMF) tested specimens of Inconel 718 measured by using the replica method. The specimens are loaded with different strain rates. The material shows a significantly higher crack growth rate if the strain rate is decreased. Electron backscatter diffraction (EBSD) is adopted to identify the failure mechanism and the misorientation relationship of failed grain boundaries in secondary cracks. The analyzed cracks propagated mainly transgranular but also intergranular failure can be observed in some areas. It is found that grain boundaries with coincidence site lattice (CSL) boundary structure are generally less susceptible for intergranular failure than grain boundaries with random misorientation. For modeling the experimentally identified crack behavior an existing model for fatigue crack growth based on the mechanism of time dependent elastic-plastic crack tip blunting is enhanced to describe environmental effects based on the mechanism of oxygen diffusion at the crack tip. For the diffusion process the temperature dependent parabolic diffusion law is assumed. As a result, the time dependent cyclic crack tip opening displacement (ACTOD) is used as representative value to describe both mechanisms. Thus, most of the included model parameters characterize the deformation behavior of the material and can be determined by independent material tests. With the determined material properties, the proposed model describes the experimentally measured crack growth curves very well. The model is validated based on predictions of the number of cycles to failure of LCF as well as in-phase and out-of-phase TMF tests in the temperature range between room temperature and 650℃.
机译:以下贡献涉及通过复制法测量的Inconel 718低循环疲劳(LCF)和热机械疲劳(TMF)测试的试样中裂纹的扩展。样品加载有不同的应变率。如果降低应变速率,则材料显示出明显更高的裂纹扩展速率。采用电子背散射衍射(EBSD)技术识别二次裂纹的失效机理和失效晶界的失取向关系。在某些区域,可以观察到分析的裂纹主要沿晶界传播,但也沿晶间破裂。发现具有重合位点晶格(CSL)边界结构的晶界通常比具有随机取向错误的晶界更不易发生晶间破坏。为了对实验确定的裂纹行为进行建模,基于时间相关的弹塑性裂纹尖端钝化机理的现有疲劳裂纹扩展模型得到了增强,以基于裂纹尖端的氧扩散机理来描述环境效应。对于扩散过程,假设温度依赖于抛物线扩散定律。结果,时间相关的循环裂纹尖端张开位移(ACTOD)被用作代表值来描述这两种机制。因此,大多数包含的模型参数表征了材料的变形行为,可以通过独立的材料测试确定。利用确定的材料特性,提出的模型很好地描述了实验测量的裂纹扩展曲线。该模型基于对LCF失效循环次数的预测,以及在室温至650℃的温度范围内的同相和异相TMF测试进行验证。

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