细化硬氮化物涂层的晶粒尺寸,缓解韧性金属基材的疲劳性能退化

IF 5.7 2区 材料科学 Q1 ENGINEERING, MECHANICAL
Zhaolu Zhang
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引用次数: 0

摘要

本文提出了通过减小涂层晶粒尺寸和揭示其内在机理来减轻硬质氮化涂层对坚韧金属基体的副作用的有效途径。利用物理气相沉积硬质镀层晶粒尺寸的厚度依赖效应,采用过滤阴极真空电弧沉积方法在2A70铝合金疲劳试样表面制备了晶粒尺寸分别为9.6 nm、16.5 nm和23.4 nm的TiN镀层。旋转弯曲疲劳试验表明,在9.6 nm、16.5 nm和23.4 nm晶粒尺寸下,TiN涂层的2A70、2A70的中位疲劳极限分别为165.83 MPa、127.5 MPa、113.75 MPa和112.5 MPa。在高周疲劳载荷下,晶粒尺寸为9.6 nm的TiN涂层对基体疲劳性能的破坏最小。TiN的抗疲劳性能决定了其对金属基体疲劳行为的损伤程度。分子动力学分析表明,TiN涂层在经历不同的疲劳载荷循环后,最大应力随晶粒尺寸的增大而增大。在交变载荷下,晶粒小、晶界多导致TiN涂层中主要的晶间滑动。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Grain size refinement of hard nitride coating to mitigate fatigue performance degradation in ductile metal substrate
This paper proposes an effective way to relieve the side effect of hard nitride coating on tough metal substrate by reducing coating grain size and revealing its inner mechanism. Utilizing the thickness-dependent effect of physical vapor deposited hard coating grain size, TiN coatings with grain sizes of 9.6 nm, 16.5 nm, and 23.4 nm were prepared on the surface of 2A70 aluminum alloy fatigue specimen by filtered cathodic vacuum arc deposition. Rotating bending fatigue tests revealed that the median fatigue limits of 2A70, 2A70 with TiN coating at grain sizes of 9.6 nm, 16.5 nm, and 23.4 nm are 165.83 MPa, 127.5 MPa, 113.75 MPa, and 112.5 MPa, respectively. Under high-cycle fatigue loading, the TiN coating with a grain size of 9.6 nm exhibits the least damage to the substrate’s fatigue performance. And the fatigue resistance of TiN determines its damage extent to metal substrate’s fatigue behavior. Molecular dynamics analysis shows that the maximum stress experienced by TiN coatings increases with grain size after undergoing various fatigue loading cycles. Under alternating loads, smaller grains with more grain boundaries lead to predominant intergranular sliding in the TiN coating.
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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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