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Prediction of fatigue endurance of Ni-Base superalloy, IN738LC with protective coatings

机译:防护涂料预测Ni-Base高温合金的疲劳耐久性,In738LC

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摘要

The effect of protective coatings on the high-cycle fatigue strength of Ni-base superalloy, IN738LC, was first modeled, summarizing the previous studies which covered the fatigue failure of the IN738LC specimens with three kinds of protectivecoatings: the CoCrAlY alloy overlay coated IN738LC, the CoNiCrAlY alloy overlay coated IN738LC, and the combined coatings in which the aluminide coating was conducted with different thickness on the CoNiCrAlY overlay coated IN738LC. The effect was foundto be condensed into the following roles, depending on the mechanical properties of the coating material and substrate: the role as a fatigue crack initiator, the role to make a geometrical change of fatigue crack, and the role to induce a stressconcentration. A new semi-empirical method to predict the fatigue endurance of the coated material was proposed, by applying the concept of latent, or fictitious crack, which has been originally introduced by Haddad et al. to explain the dependence ofcrack length on threshold of fatigue cracks in monolithic materials. In the proposed method the coating and the incidental diffusion zone were treated as a part of latent crack interacting with the substrate, depending on the mechanical properties ofcoating material. It was shown that the proposed method gave a good estimation corresponding well with the experimental results.
机译:保护涂层对Ni-Base超合金高循环疲劳强度的影响,首先进行了建模的,总结了以前的研究,这些研究涵盖了三种防护统一的疲劳失效,包括三种防护统一:涂上738磅的共和平合金覆盖层,涂覆在738LC的同胞合金覆盖层,以及铝化物涂层的组合涂层,在同显式覆盖层上涂覆在738LC上。发现效果被凝结成以下典型,取决于涂料和基材的机械性能:作为疲劳裂纹引发剂的作用,作用制造疲劳裂纹的几何变化,以及诱导应激浓度的作用。提出了一种预测涂层材料的疲劳耐久性的新的半经验方法,通过应用潜伏或虚构的裂缝,其最初由Haddad等人引入。解释单片材料中疲劳裂缝阈值的依赖性。在该方法中,取决于涂料材料的机械性能,将涂层和偶然扩散区作为与基材相互作用的潜裂纹的一部分。结果表明,该方法对实验结果进行了良好的估计。

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