Exploring mechanical response and fatigue properties of laser powdered-bed fusion IN718 superalloy: Crystal plasticity modeling and defect-based life prediction

IF 4.4 2区 工程技术 Q1 ENGINEERING, MECHANICAL
Asif Mahmood , Chuanwen Sun , Wei Li , Muhammad Imran Lashari , Rui Sun , Cheng Li , Zifan Hu
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引用次数: 0

Abstract

The mechanical response and fatigue properties of laser powdered-bed fusion IN718 superalloy were explored experimentally and numerically. Firstly, uniaxial fatigue testing was conducted to investigate failure mechanisms under two stress ratios in the high-cycle and very high-cycle regimes, for the as-built and solution aging conditions. The fracture surfaces reveal the competing crack nucleation behaviors driven by manufacturing or crystallographic defects. Furthermore, solution aging significantly improves fatigue life compared to as-built conditions, demonstrating higher fatigue lives under similar stress levels. Secondly, crystal plasticity finite element (CPFE) modeling was employed to develop a statistically representative volume element, enabling evaluation of the local stress and strain distributions with and without pores under cyclic loading. In addition, model parameters were calibrated using experimental stress–strain data, emphasizing the precision and validity of the proposed model. The computational results show that softened grains oriented 45° to the loading direction exhibit greater deformation. Moreover, the accumulated plastic strain increases as the loading cycles progress. Finally, a fatigue life prediction model was developed, considering the sensitivity of crack nucleation to manufacturing and crystallographic defects, along with CPFE results, showing good consistency between experimental and predicted fatigue lives across different stress levels in high-cycle and very high-cycle regimes.
激光粉末床熔合IN718高温合金的力学响应和疲劳性能研究:晶体塑性建模和基于缺陷的寿命预测
通过实验和数值计算探讨了激光粉末床熔融 IN718 超级合金的机械响应和疲劳特性。首先,进行了单轴疲劳试验,研究了在高循环和超高循环两种应力比下,坯料和固溶时效条件下的失效机理。断裂表面显示了由制造缺陷或晶体学缺陷驱动的竞争性裂纹成核行为。此外,与竣工条件相比,固溶老化显著提高了疲劳寿命,在类似应力水平下显示出更高的疲劳寿命。其次,采用晶体塑性有限元(CPFE)建模来开发具有统计代表性的体积元素,从而能够评估循环加载下有孔隙和无孔隙的局部应力和应变分布。此外,还利用实验应力应变数据对模型参数进行了校准,从而强调了所建模型的精确性和有效性。计算结果表明,与加载方向成 45° 的软化晶粒表现出更大的变形。此外,随着加载循环的进行,累积塑性应变也在增加。最后,考虑到裂纹成核对制造和晶体学缺陷的敏感性,结合 CPFE 结果,建立了疲劳寿命预测模型,结果表明在高循环和超高循环条件下,不同应力水平下的实验疲劳寿命和预测疲劳寿命具有良好的一致性。
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来源期刊
Engineering Failure Analysis
Engineering Failure Analysis 工程技术-材料科学:表征与测试
CiteScore
7.70
自引率
20.00%
发文量
956
审稿时长
47 days
期刊介绍: Engineering Failure Analysis publishes research papers describing the analysis of engineering failures and related studies. Papers relating to the structure, properties and behaviour of engineering materials are encouraged, particularly those which also involve the detailed application of materials parameters to problems in engineering structures, components and design. In addition to the area of materials engineering, the interacting fields of mechanical, manufacturing, aeronautical, civil, chemical, corrosion and design engineering are considered relevant. Activity should be directed at analysing engineering failures and carrying out research to help reduce the incidences of failures and to extend the operating horizons of engineering materials. Emphasis is placed on the mechanical properties of materials and their behaviour when influenced by structure, process and environment. Metallic, polymeric, ceramic and natural materials are all included and the application of these materials to real engineering situations should be emphasised. The use of a case-study based approach is also encouraged. Engineering Failure Analysis provides essential reference material and critical feedback into the design process thereby contributing to the prevention of engineering failures in the future. All submissions will be subject to peer review from leading experts in the field.
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