Effect of rapid thermomechanical fatigue pre-damage on the residual isothermal low-cycle fatigue behavior of a DD6 single-crystal superalloy with a film-cooling hole

IF 6.7 2区 材料科学 Q2 CHEMISTRY, PHYSICAL
Houjun Qin, Changyou Xu, Yantao Sun, Muwei Cheng, Renjie Jiang, Tianyu Fan, Pengfei Ji, Hongbin Zhou, Yongzhao Lv, Jianan Song, Jia Huang, Xiaoguang Yang
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Abstract

Turbine-blade materials often experience sequential thermomechanical fatigue (TMF) and low-cycle fatigue (LCF) loading during service, yet the mechanism governing residual LCF resistance after TMF pre-damage remains unclear. DD6 nickel-based single-crystal superalloy specimens with a film-cooling hole (FCH) and smooth round-bar (RB) geometries were subjected to TMF preloading followed by LCF testing at 980 °C. Residual LCF resistance was evaluated using normalized life fractions, and the damage-transfer process was investigated through fractography, longitudinal-section microscopy, γ/γ′ characterization, EBSD analysis, and microstructure-informed γ/γ′ two-phase cyclic-plasticity simulations. The results show that residual LCF life does not follow a linear life-fraction relationship. At a TMF pre-damage fraction of approximately 25%, the normalized residual LCF life fractions were approximately 0.260 for the FCH specimen and 0.070 for the RB specimen under their respective baseline-normalized conditions. In the FCH specimen, TMF-induced damage was mainly localized near the hole edge, and subsequent LCF failure involved further crack propagation and damage accumulation from this localized region. In contrast, the RB specimen developed a more spatially distributed damage field across the gauge section, resulting in multiple potential sites for crack initiation, interaction, and coalescence during subsequent LCF loading. When the TMF pre-damage fraction reached approximately 45% or higher, both specimen types exhibited very low residual LCF resistance as accumulated damage became sufficiently severe to dominate subsequent failure. These findings demonstrate that residual LCF resistance after TMF preloading is governed not only by the consumed TMF life fraction but also by the spatial localization and connectivity of TMF-induced microstructural damage.
快速热机械疲劳预损伤对带膜冷孔的DD6单晶高温合金残余等温低周疲劳行为的影响
涡轮叶片材料在使用过程中经常经历顺序热机械疲劳(TMF)和低周疲劳(LCF)加载,但TMF预损伤后LCF残余阻力的控制机制尚不清楚。DD6镍基单晶高温合金具有膜冷孔(FCH)和光滑圆棒(RB)的几何形状,在980°C下进行TMF预加载和LCF测试。使用归一化寿命分数评估残余LCF阻力,并通过断口学、纵向切片显微镜、γ/γ′表征、EBSD分析和微观结构信息γ/γ′两相循环塑性模拟来研究损伤传递过程。结果表明,剩余LCF寿命不遵循线性寿命分数关系。在TMF预损伤分数约为25%时,在各自的基线归一化条件下,FCH样品的归一化剩余LCF寿命分数约为0.260,RB样品的归一化剩余LCF寿命分数约为0.070。在FCH试样中,tmf引起的损伤主要集中在孔边缘附近,随后的LCF破坏从这个局部区域进一步扩展和损伤积累。相比之下,RB试样在规范截面上形成了一个更具有空间分布性的损伤场,导致在随后的LCF加载过程中存在多个裂纹萌生、相互作用和合并的潜在位点。当TMF预损伤分数达到约45%或更高时,两种试样类型都表现出非常低的残余LCF阻力,因为累积的损伤变得足够严重,从而主导随后的破坏。这些结果表明,TMF预加载后的残余LCF电阻不仅受消耗的TMF寿命分数的影响,还受TMF诱导的微结构损伤的空间定位和连通性的影响。
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来源期刊
Journal of Alloys and Compounds
Journal of Alloys and Compounds 工程技术-材料科学:综合
CiteScore
11.10
自引率
14.50%
发文量
5146
审稿时长
67 days
期刊介绍: The Journal of Alloys and Compounds is intended to serve as an international medium for the publication of work on solid materials comprising compounds as well as alloys. Its great strength lies in the diversity of discipline which it encompasses, drawing together results from materials science, solid-state chemistry and physics.
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