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Contact deformation of carbon coatings: mechanisms and coating design.

机译:碳涂层的接触变形:机理和涂层设计。

摘要

This thesis presents the results of a study focussed on the elucidation of the mechanisms responsible for determining the structural integrity of carbon coatings on ductile substrates. Through elucidation of these mechanisms, two different coating systems are designed; a multilayered coating and a functionally graded coating. While concentrating upon carbon coatings, the findings of this study are applicable to a broad range of hard coatings on ductile substrates. The thesis concludes with a chapter outlining a brief study of the effects of gold coatings on silicon under contact load at moderate temperatures to complement the major part of the thesis.Carbon coatings with differing mechanical properties were deposited using plasma enhanced chemical vapour deposition (PECVD), filtered assisted deposition (FAD) and magnetron sputtering deposition methods. Combinations of these techniques plus variation of deposition parameters enabled composite multilayered and functionally-graded coatings to also be deposited. Substrates were ductile metals; stainless steel and aluminium. Characterisation of the coating mechanical properties was undertaken using nanoindentation and nano-scratch tests. The same techniques were used to induce fracture within the coatings to allow subsequent analysis of the fracture mechanism. These were ascertained with the assistance of cross-sectional imaging of indents prepared using a focussed ion beam (FIB) mill and transmission electron microscopy (TEM) using specimen preparation techniques also utilising the focussed ion beam mill. A two dimensional axisymmetric finite element model (FEM) was built of the coating systems using the commercial software package, ANSYS. Substrate elastic-plastic properties were ascertained by calibrating load-displacement curves on substrate materials with the finite element model results. Utilising the simulation of spherical indentation, the distribution of stresses and the locations for fracture initiation were ascertained using finite element models. This enabled determination of the influence such factors as substrate mechanical properties, residual stresses in the coatings and importantly the variation of elastic properties of the different coating materials. Based upon the studies of monolithic coatings, simulations were undertaken on multilayer and functionally-graded coatings to optimise design of these coating types. Based on the results of the modelling, multilayered and functionally graded coatings were then deposited and mechanical testing undertaken to confirm the models. Three major crack types were observed to occur as the result of the spherical nanoindentation on the coatings; ring, radial and lateral cracks. Ring cracks were found to initiate from the top surface of the film, usually at some distance from the edge of the spherical contact. Radial cracks usually initiated from the interface between the coating and the substrate directly under the symmetry axis of indentation and propagated outwards in a non symmetrical star-like fashion. Lateral cracks formed either between layers in the multilayer coatings or at the interface with substrate. Ring and radial cracks were found to form upon loading whereas lateral cracks formed upon both loading and unloading depending upon the crack driving mechanism. Pop-in events in the load displacement indentation curve were found to be indicative of the formation of ring cracks, while the formation of the other types of cracks was not signified by pop-ins but rather by variations in the slope of the curve. The substrate yield strength was found to influence the initiation of all crack systems while compressive stresses in the coating were seen to only influence the formation of ring and radial cracks. However, it was also noted that the initiation of one form of crack tended to then hinder the subsequent formation of others.In multilayer coatings, the lateral cracks were suppressed, as opposed to the monolayer coating system, but a ring crack was observed. This drawback in the multilayer system was successfully addressed by the design of a graded coating having the highest Young’s modulus at the middle of the film thickness. In this coating, due to the graded nature of the elastic modulus, the stresses at the deleterious locations (top surface and interface) were guided toward the middle of coating and hence increased the load bearing capabilities.The effect of substrate roughness upon the subsequent surface roughness of the coating and also upon the fracture process of the coating during indentation was also investigated. For the coatings deposited on rough substrates, the radial cracks were observed to form initially and this eventfully delayed the initiation of ring cracks. Also the number of radial cracks observed at the interface was found to be proportional to the distribution of the interfacial asperities. In summary, the study elucidated the fracture mechanisms of monolayer, multilayer and graded carbon coatings on ductile substrates under uniaxial and sliding contact loading. The effects of the yield strength, surface roughness of the substrate, along with the residual stress and elastic modulus of the coatings on the fracture of coatings were investigated. The study utilised finite element modelling to explain the experiments observations and to design coating systems.
机译:本论文提出了一项研究结果,重点是阐明决定延性基底上碳涂层结构完整性的机制。通过阐明这些机理,设计了两种不同的涂层系统。多层涂层和功能梯度涂层。在专注于碳涂层的同时,这项研究的结果适用于可延展基材上的各种硬涂层。本文以一章作为结束,概述了在中等温度下接触载荷下金涂层对硅的影响的简要研究,以补充本文的主要内容。采用等离子增强化学气相沉积(PECVD)沉积具有不同机械性能的碳涂层,过滤辅助沉积(FAD)和磁控溅射沉积方法。这些技术的结合以及沉积参数的变化使得复合多层涂层和功能渐变涂层也可以沉积。底材是韧性金属;不锈钢和铝。使用纳米压痕和纳米划痕测试对涂层的机械性能进行表征。使用相同的技术在涂层内引起断裂,以允许随后分析断裂机理。这些是借助于使用聚焦离子束磨机制备的压痕的横截面成像和使用聚焦离子束磨机制备的样品制备技术的透射电子显微镜(TEM)来确定的。使用商用软件包ANSYS,建立了涂层系统的二维轴对称有限元模型(FEM)。通过用有限元模型结果校准基底材料上的载荷-位移曲线来确定基底的弹塑性特性。利用球形压痕的模拟,使用有限元模型确定了应力分布和断裂起始位置。这样就可以确定影响因素,例如基材的机械性能,涂层中的残余应力以及重要的是不同涂层材料的弹性。基于整体涂层的研究,对多层和功能渐变涂层进行了仿真,以优化这些涂层类型的设计。基于建模的结果,然后沉积多层和功能渐变涂层,并进行机械测试以确认模型。观察到三种主要的裂纹类型是涂层上球形纳米压痕的结果。环形,径向和横向裂纹。发现从薄膜的顶表面开始出现环形裂纹,通常在距球形接触边缘一定距离处开始。径向裂纹通常从涂层和基体之间的界面直接在压痕的对称轴下方开始,并以不对称的星形方式向外传播。在多层涂层的各层之间或与基材的界面处形成横向裂纹。发现在加载时会形成环形和径向裂纹,而在加载和卸载时均会形成横向裂纹,这取决于裂纹的驱动机制。发现载荷位移压痕曲线中的弹入事件指示环形裂纹的形成,而其他类型的裂纹的形成并不由弹入指示,而是由曲线斜率的变化指示。发现基材屈服强度会影响所有裂纹系统的萌生,而涂层中的压缩应力仅会影响环形和径向裂纹的形成。然而,还注意到一种形式的裂纹的发生倾向于随后阻碍其他形式的形成。在多层涂层中,与单层涂层体系相反,横向裂纹得到抑制,但是观察到了环裂纹。多层体系中的这一缺陷已通过设计一种在薄膜厚度中间具有最高杨氏模量的渐变涂层而得以成功解决。在这种涂层中,由于弹性模量的渐变性质,有害位置(顶表面和界面)处的应力被引导向涂层中间,因此增加了承重能力。基材粗糙度对后续表面的影响还研究了涂层的粗糙度以及压痕过程中涂层的断裂过程。对于沉积在粗糙基材上的涂层,最初观察到形成了径向裂纹,最终延缓了环裂纹的产生。还发现在界面处观察到的径向裂纹的数量与界面粗糙的分布成比例。综上所述,研究阐明了单层的断裂机理,在单轴和滑动接触载荷下,可延展基材上的多层和渐变碳涂层。研究了屈服强度,基材表面粗糙度以及涂层的残余应力和弹性模量对涂层断裂的影响。该研究利用有限元建模来解释实验观察结果并设计涂层系统。

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