Microstructural and Nanomechanical Characterization of CrCoAlHf/YSZ Multilayer Coatings Deposited by DC/RF Magnetron Sputtering

Syed Faizan Altaf, Atikur Rahman, M. F. Wani
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Abstract

This study presents the microstructural, chemical, and nanomechanical behavior of multilayer coatings of Cr/CoAlHf/YSZ deposited on Inconel 718 alloy using combined DC/RF magnetron sputtering with a focus on coatings deposited at 300°C for high-temperature aerospace applications. FESEM and EDS analyses indicate the formation of a multilayer structure with high density and minimal porosity, as well as homogeneous elemental distribution of the Cr, CoAlHf, and YSZ layers, implying that no interfacial diffusion is occurring. X-ray diffraction (XRD) patterns confirm the formation of stable phases, including ZrO2, Y2O3, Cr, HfO2, and a Co–Cr–Al–Hf solid solution. Nanoindentation shows stable deformation behavior and high load-bearing capacity, where hardness exhibited an increasing trend from 7.94 to 11.25 GPa in the range of 500–2500 µN, decreasing to 10.70 GPa at 3500 µN, which is explained as the change of reverse indentation size effect (r-ISE) to conventional indentation size effect (ISE) for the change of applied loads. Nano-scratch testing at gradually increased ramp loads confirms good coating adhesion, characterized by stable frictional behavior and minimal surface damage. XPS survey analysis confirms the chemical integrity of the multilayer system, with both strong Zr3d and Y3p peaks indicating the YSZ top layer, and distinct signals for Co, Cr, Al, and Hf, indicating the underlying bond coat. Overall, the results reveal that deposition at 300°C is beneficial for favorable microstructural evolution, chemical stability, and enhanced nanomechanical performance, making the CoCrAlHf/YSZ multilayer a promising protective coating for Inconel 718 components exposed to extreme aerospace service environments.

Abstract Image

DC/RF磁控溅射沉积CrCoAlHf/YSZ多层涂层的微观结构和纳米力学特性
本研究介绍了采用DC/RF磁控溅射技术在Inconel 718合金上沉积Cr/CoAlHf/YSZ多层涂层的微观结构、化学和纳米力学行为,重点研究了在300°C下沉积用于高温航空航天应用的涂层。FESEM和EDS分析表明,该过程形成了高密度、孔隙率最小的多层结构,且Cr、CoAlHf和YSZ层元素分布均匀,表明未发生界面扩散。x射线衍射(XRD)图证实了稳定相的形成,包括ZrO2、Y2O3、Cr、HfO2和Co-Cr-Al-Hf固溶体。纳米压痕表现出稳定的变形行为和较高的承载能力,在500 ~ 2500µN范围内,硬度呈上升趋势,从7.94增加到11.25 GPa,在3500µN范围内下降到10.70 GPa,这可以解释为施加载荷变化的反向压痕尺寸效应(r-ISE)转变为常规压痕尺寸效应(ISE)。在逐渐增加的斜坡载荷下,纳米划痕测试证实了涂层的良好附着力,其特征是稳定的摩擦行为和最小的表面损伤。XPS调查分析证实了多层体系的化学完整性,强烈的Zr3d和Y3p峰表明YSZ顶层,Co, Cr, Al和Hf的信号明显,表明下面的结合层。总体而言,结果表明,在300°C下沉积有利于良好的微观组织演变,化学稳定性和增强的纳米力学性能,使CoCrAlHf/YSZ多层膜成为暴露在极端航空航天服务环境下的Inconel 718部件的有前途的保护涂层。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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