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THERMAL AND MECHANICAL FATIGUE LOADING - MECHANISMS OF CRACK INITIATION AND CRACK GROWTH

机译:热和机械疲劳载荷-裂纹萌生和裂纹扩展的机理

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The present contribution is focused on the experimental investigations and numerical simulations of the deformation behaviour and crack development in the austenitic stainless steel X6CrNiNb18-10 (AISI-347) under thermal and mechanical cyclic loading in HCF and LCF regimes. The main objective of this research is the understanding of the basic mechanisms of fatigue damage and development of simulation methods, which can be applied further in safety evaluations of nuclear power plant components. In this context the modelling of crack initiation and crack growth inside the material structure induced by varying thermal or mechanical loads are of particular interest. The mechanisms of crack initiation depend among other things on the art of loading, microstructure, material properties and temperature. The Nb-stabilized austenitic stainless steel in the solution-annealed condition was chosen for the investigations. Experiments with two kinds of cyclic loading - pure thermal and pure mechanical - were carried out and simulated. The fatigue behaviour of the steel X6CrNiNb18-10 under thermal loading was studied within the framework of the joint research project. Interrupted thermal cyclic tests in the temperature range of 150 °C to 300 °C combined with nondestructive residual stress measurements (XRD) and various microscopic investigations, e.g. in SEM, were used to study the effects of thermal cyclic loading on the material. This thermal cyclic loading leads to thermal induced stresses and strains. As a result intrusions and extrusions appear inside the grains (at the surface), at which micro-cracks arise and evolve to a dominant crack. Finally, these micro-cracks cause continuous and significant decrease of residual stresses. The fatigue behaviour of the steel X6CrNiNb18-10 under mechanical loading at room temperature was studied in the framework of the research project. With a combination of interrupted LCF tests and EBSD measurements the deformation induced transformation of a fcc austenite into a bcc α'-martensite was observed in different stages of the specimen lifetime. The plastic zones develop at the crack tips, in which stress and strain amplitudes are much higher than the nominal loading, and enable martensitic transformation in the surrounding of the crack tip. The consequence of this is that cracks grow in the "martensitic tunnels". The short and long crack growth behaviours of the steel X6CrNiNb18-10 under mechanical loading at room temperature and T = 288 °C were studied for different loading parameters. Moreover, the R-ratio was modified in order to study the effect of crack closure at the crack tip for long cracks. Several FE-models of specimens with different geometries and microstructures were created and cyclically loaded according to the experimental boundary conditions. A plastic constitutive law based on a Chaboche type model was implemented as a user subroutine in the FE software ABAQUS. The corresponding material parameters were identified using uniaxial LCF tests of X6CrNiNb18-10 with different strain amplitudes and at different temperatures. These calculations aimed in the estimation of stress and strain distributions in the critical areas in which the crack initiation was expected.
机译:本研究的重点是在HCF和LCF制度下,在热和机械循环载荷下,奥氏体不锈钢X6CrNiNb18-10(AISI-347)的变形行为和裂纹发展的实验研究和数值模拟。这项研究的主要目的是对疲劳损伤的基本机理的理解和仿真方法的发展,这些方法可以进一步应用于核电站部件的安全性评估中。在这种情况下,特别关注在材料结构内部由变化的热或机械载荷引起的裂纹萌生和裂纹扩展的建模。裂纹萌生的机理尤其取决于载荷,微观结构,材料性能和温度的领域。研究中选择了固溶退火状态的Nb稳定奥氏体不锈钢。进行并模拟了两种循环载荷(纯热载荷和纯机械载荷)的实验。在联合研究项目的框架内,研究了X6CrNiNb18-10钢在热载荷下的疲劳行为。在150°C至300°C的温度范围内进行中断的热循环测试,结合无损残余应力测量(XRD)和各种微观研究,例如在SEM中,被用来研究热循环载荷对材料的影响。这种热循环载荷导致热诱导的应力和应变。结果,在晶粒内部(在表面)出现了侵入和挤压,在该处出现了微裂纹并发展为主要裂纹。最后,这些微裂纹会导致残余应力的持续显着降低。在研究项目的框架内,研究了X6CrNiNb18-10钢在室温下的机械载荷下的疲劳行为。结合中断的LCF测试和EBSD测量,在样品寿命的不同阶段观察到了由变形诱发的fcc奥氏体向bccα'-马氏体的转变。塑性区在裂纹尖端处发展,其中应力和应变幅度远远高于标称载荷,并在裂纹尖端周围产生马氏体相变。其结果是在“马氏体隧道”中裂纹扩展。研究了X6CrNiNb18-10钢在室温和T = 288°C的机械载荷下对于不同载荷参数的短时和长时裂纹扩展行为。此外,为了研究长裂纹的裂纹尖端处的裂纹闭合效应,对R比率进行了修改。根据实验边界条件,创建了几种具有不同几何形状和微观结构的标本的有限元模型,并对其进行循环加载。在有限元软件ABAQUS中,将基于Chaboche类型模型的塑性本构定律作为用户子例程实现。使用X6CrNiNb18-10的单轴LCF测试,在不同的应变幅度和不同的温度下,确定了相应的材料参数。这些计算的目的在于估计预期裂纹产生的关键区域的应力和应变分布。

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