具有应力集中特征的镍基高温合金循环裂纹萌生的实验与分析研究

Alex Torkaman, S. Fiebiger, Nathan O’Nora, Devin O’Neal, A. Gordon
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引用次数: 0

摘要

涡轮关键部件裂纹萌生周期的准确预测是涡轮机械设计中的一个重要问题,特别是在具有高度集中应力的部件,如带冷却孔的涡轮叶片中。一些粘塑性和寿命方法已经成功地用于预测安定和失效循环,但是仍然存在一些复杂的因素,给传统方法带来了挑战。因此,采用考虑各向同性和多向硬化的本构建模的新方法已被开发出来,以更好地捕捉材料循环行为的演变。平均应力和应力集中因素的存在是使用本构模型可以更好地解释的一些并发症。本文对具有高应力集中特征的镍基高温合金试样在平均应力循环条件下的实验寿命和理论寿命进行了评价。试样的几何形状和载荷被设计成模拟F级IGT涡轮叶片的尾缘孔。实验是在两个峰值应力值的高温下进行的,以确定在类似于发动机的工作温度下对施加载荷的敏感性。采用著名的Manson-Coffin方法和Morrow平均应力校正以及两种不同的应变范围评估方法对裂纹萌生周期进行了分析评估。第一种方法是传统的Ramberg Osgood勒索,该方法已在行业中广泛使用。第二种方法是基于本构Chaboche模型的线性化有限元模拟。Chaboche模型的常数由Ramberg-Osgood常数确定,该方法考虑了屈服面演变和硬化常数,以及可用于模拟停留时间效应的速率相关应力松弛因子。讨论了利用本构模型减少计算时间的方法。将分析结果与实验数据进行了比较,并讨论了两种方法的优缺点,包括计算时间。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Experimental and Analytical Investigation of Cyclic Crack Initiation in Nickel Based Super Alloy With Stress Concentration Features
Accurate prediction of cycles to crack initiation in critical turbine components is a major issue in turbomachinery design, especially in components with highly concentrated stress such as turbine blades with cooling holes. Several viscoplastic and lifing methods have been used successfully to predict shakedown and cycles to failure, however complicating factors still exist that produce challenges for traditional methods. Therefore newer methods utilizing constitutive modeling with consideration for isotropic and polytropic hardening have been developed to better capture evolution of cyclic behavior of the material. Presence of mean stress and stress concentration factors are some of the complications that can be better accounted for using constitutive models. The present paper evaluates experimental and theoretical life of specimen made from nickel based super alloy with high stress concentration features under cyclic conditions with mean stress. The specimen geometry and loading were designed to mimic trailing edge holes in an F class IGT turbine blade. Experiments were conducted at an elevated temperature at two peak stress values to determine sensitivity to applied load at operating temperature similar to engine. Cycles to crack initiation are analytically evaluated using the well-known Manson-Coffin method with Morrow mean stress correction and two distinct methods for strain range evaluation. First method is the traditional Ramberg Osgood shakedown that has been extensively used in the industry. Second method is constitutive Chaboche based model run with linearized FEM results. Constants for Chaboche model are determined from Ramberg-Osgood constants with a method that takes into account yield surface evolution and hardening constants, in addition to rate dependent stress relaxation factor that can be used to model dwell time effects. Methods to decrease computational time with constitutive model are discussed. Analytical results are compared with the experimental data, and advantages and disadvantages of both methods including computational times are discussed.
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