Cold expansion fatigue performance investigations of GH4169 inclined hole structures using numerical and experimental methods

IF 6.8 2区 材料科学 Q1 ENGINEERING, MECHANICAL International Journal of Fatigue Pub Date : 2025-04-01 Epub Date: 2024-11-28 DOI:10.1016/j.ijfatigue.2024.108736
Hangjie Shi, Yangjie Zuo
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Abstract

In this paper, the inclined cold expansion (ICE) method of superalloy open hole structures was proposed, which provided valuable insights for the life improvement of aero-engine inclined hole structures. The improvements in the static and fatigue properties of GH4169 specimens with inclined holes were characterized. In addition, tensile and fatigue tests were carried out, and the surface strains were assessed by digital image correlation (DIC). The stiffness degradation and fatigue fracture behavior of GH4169 specimens with inclined holes were also discussed. The results showed that ICE could cause the expansion of inclined hole structures and the enlargement of bulges, resulting in tangential residual compressive stress at the hole edge. With the increase of the hole inclinations, the residual stress of the specimen was more uneven in radial direction, while more uniform in axial direction. The fatigue life of the strengthened all increased under three loading levels. The crack initiation zone moved near the entrance layer after ICE. Moreover, ICE increased the crack growth zone, and significantly inhibited the crack growth rate and stiffness degradation rate.
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GH4169斜孔结构冷胀疲劳性能的数值与实验研究
本文提出了高温合金开孔结构的倾斜冷胀方法,为提高航空发动机斜孔结构的寿命提供了有价值的见解。研究了斜孔对GH4169试样静力性能和疲劳性能的改善。此外,还进行了拉伸和疲劳试验,并采用数字图像相关(DIC)对表面应变进行了评估。讨论了GH4169斜孔试件的刚度退化和疲劳断裂行为。结果表明:冰激作用可引起倾斜孔洞结构的扩展和凸起的扩大,在孔洞边缘产生切向残余压应力;随着孔倾角的增大,试样的残余应力在径向上更加不均匀,在轴向上更加均匀。在3个载荷水平下,强化层的疲劳寿命均有所提高。冰激作用后,裂纹起裂区向入口层附近移动。此外,ICE增大了裂纹扩展区域,显著抑制了裂纹扩展速率和刚度退化速率。
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来源期刊
International Journal of Fatigue
International Journal of Fatigue 工程技术-材料科学:综合
CiteScore
10.70
自引率
21.70%
发文量
619
审稿时长
58 days
期刊介绍: Typical subjects discussed in International Journal of Fatigue address: Novel fatigue testing and characterization methods (new kinds of fatigue tests, critical evaluation of existing methods, in situ measurement of fatigue degradation, non-contact field measurements) Multiaxial fatigue and complex loading effects of materials and structures, exploring state-of-the-art concepts in degradation under cyclic loading Fatigue in the very high cycle regime, including failure mode transitions from surface to subsurface, effects of surface treatment, processing, and loading conditions Modeling (including degradation processes and related driving forces, multiscale/multi-resolution methods, computational hierarchical and concurrent methods for coupled component and material responses, novel methods for notch root analysis, fracture mechanics, damage mechanics, crack growth kinetics, life prediction and durability, and prediction of stochastic fatigue behavior reflecting microstructure and service conditions) Models for early stages of fatigue crack formation and growth that explicitly consider microstructure and relevant materials science aspects Understanding the influence or manufacturing and processing route on fatigue degradation, and embedding this understanding in more predictive schemes for mitigation and design against fatigue Prognosis and damage state awareness (including sensors, monitoring, methodology, interactive control, accelerated methods, data interpretation) Applications of technologies associated with fatigue and their implications for structural integrity and reliability. This includes issues related to design, operation and maintenance, i.e., life cycle engineering Smart materials and structures that can sense and mitigate fatigue degradation Fatigue of devices and structures at small scales, including effects of process route and surfaces/interfaces.
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