3Al2O3·2SiO2 ebc的纳米划伤测试:诱导损伤评估和粘附强度评估

IF 2.7 Q1 MATERIALS SCIENCE, CERAMICS
C. Botero, L. Cabezas, V. Sarin, L. Llanes, E. Jiménez-Piqué
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引用次数: 0

摘要

在本研究中,采用化学气相沉积(CVD)技术在碳化硅(SiC)衬底上沉积莫来石(3Al2O3·2SiO2)薄膜,通过增加负载纳米划痕实验研究其结构完整性。薄膜是由化学计量组成的莫来石柱在与SiC衬底接触的富硅层中生长而成。在相对较低的划痕载荷下,3Al2O3·2SiO2薄膜受到了可控的损伤。径向和侧向开裂应用,直到最终分层和重复切屑实现随着载荷的增加。分析了3Al2O3∙2SiO2膜的内在完整性和作为结构单元的3Al2O3∙2SiO2 /SiC包覆体系的性能。借助先进的表面和亚表面表征技术,表征了纳米划伤在涂层体系中引起的损伤形态和形态,并确定了划伤损伤的微观机制。最后,利用文献中提出的不同模型,以附着能和界面断裂韧性来确定膜的附着力。这项研究的结果有助于理解基于EBC/ sic的系统的机械性能和结构完整性,这些系统在过去几年中越来越多地应用于燃气轮机和飞机发动机的新应用中。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Nanoscratch Testing of 3Al2O3·2SiO2 EBCs: Assessment of Induced Damage and Estimation of Adhesion Strength
In this study, the structural integrity of mullite (3Al2O3·2SiO2) films, deposited on silicon carbide (SiC) substrates using chemical vapor deposition (CVD), was investigated via increasing load nanoscratch tests. The films were configured by mullite columns of stoichiometric composition growing from a silica-rich layer in contact with the SiC substrate. Controlled damage was induced in the 3Al2O3·2SiO2 films at relatively low scratch loads. Radial and lateral cracking were applied until final delamination and repeated chipping were achieved as the load increased. The intrinsic integrity of the 3Al2O3∙2SiO2 film and the performance of the coated 3Al2O3·2SiO2/SiC system, regarded as a structural unit, were analyzed. With the aid of advanced characterization techniques at the surface and subsurface levels, the configuration and morphology of the damage induced in the coated system by the nanoscratch tests were characterized, and the scratch damage micromechanisms were identified. Finally, the adhesion of the film, in terms of energy of adhesion and interfacial fracture toughness, was determined using different models proposed in the literature. The results from this investigation contribute to the understanding of the mechanical performance and structural integrity of EBC/SiC-based systems, which over the past few years have increasingly been implemented in novel applications for gas turbines and aircraft engines.
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来源期刊
CiteScore
3.00
自引率
7.10%
发文量
66
审稿时长
10 weeks
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