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Valuation of TMF Lifetime Calculation Methods and their Limitations of Usability

机译:TMF寿命计算方法的评估及其可用性的局限性

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Cyclic loading of metallic engineering components at constant elevated or fluctuating temperature causes a complex evolution of damage which can hardly be described. At the same time the thermal expansion is restricted in some regions, due to the complex geometry of the components. Therefore, mechanical stresses occur and cyclic plastic deformation leads to thermo-mechanical fatigue (TMF) of the material. A careful analysis and comparison of the experimental results, based on a systematical variation of the relevant influence factors, allow to develop empirical models for computing the fatigue life of thermo-mechanical loaded components made of Ni alloys (IN718, Ni200/201). Different lifetime calculation methods were executed and analyzed to fulfil the requirements for the fatigue analysis of components made of these alloys. In addition, the model parameters can be optimized using these results. Based on the parameters, which define the usability of the investigated lifetime models, e.g. temperature, stress, plastic strain, the limiting combination of the parameters can be described. This graphical representation of the "border line" or limiting combination can also be used for any other materials. The results show that the main lifetime calculation models can only applied in a limited range. This limited range is mainly defined by temperature, strain constraining and their combination.
机译:在恒定的升高或波动的温度下,金属工程部件的循环载荷会导致破坏的复杂演变,这很难描述。同时,由于部件的复杂几何形状,热膨胀在某些区域受到限制。因此,会发生机械应力,并且周期性的塑性变形会导致材料的热机械疲劳(TMF)。基于相关影响因素的系统变化,对实验结果进行仔细的分析和比较,可以开发经验模型来计算由Ni合金(IN718,Ni200 / 201)制成的热机械负载部件的疲劳寿命。执行并分析了不同的寿命计算方法,以满足对这些合金制成的部件进行疲劳分析的要求。此外,可以使用这些结果优化模型参数。基于参数,这些参数定义了所研究寿命模型的可用性,例如温度,应力,塑性应变,参数的极限组合都可以描述。 “边界线”或限制组合的图形表示也可以用于任何其他材料。结果表明,主要寿命计算模型只能在有限的范围内应用。该有限范围主要由温度,应变约束及其组合来定义。

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