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首页> 外文期刊>Journal of Thermal Spray Technology >Elastic Modulus Evolution and Behavior of Si/Mullite/BSAS-Based Environmental Barrier Coatings Exposed to High Temperature in Water Vapor Environment
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Elastic Modulus Evolution and Behavior of Si/Mullite/BSAS-Based Environmental Barrier Coatings Exposed to High Temperature in Water Vapor Environment

机译:水蒸气环境中高温暴露于Si / Mullite / BSAS的环境屏障涂层的弹性模量演化和行为

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Si-based ceramics (e.g., SiC and Si_3N_4) are known as promising high-temperature structural materials in various components where metals/alloys reached their ultimate performances (e.g., advanced gas turbine engines and structural components of future hypersonic vehicles). To alleviate the surface recession that Si-based ceramics undergo in a high-temperature environmental attack (e.g., H_2O vapor), appropriate refractory oxides are engineered to serve as environmental barrier coatings (EBCs). The current state-of-the-art EBCs multilayer system comprises a silicon (Si) bond coat, mullite (3Al_2O_3·2SiO_2) interlayer and (1 - x)BaO·xSrO·Al_2O_3·2SiO_2, 0 ≤ x ≤ 1 (BSAS) top coat. In this article, the role of high-temperature exposure (1300℃) performed in H_2O vapor environment (for time intervals up to 500 h) on the elastic moduli of air plasma sprayed Si/mullite/BSAS layers deposited on SiC substrates was investigated via depth-sensing indentation. Laser-ultrasonics was employed to evaluate the E values of as-sprayed BSAS coatings as an attempt to validate the indentation results. Fully crystalline, crack-free, and near-crack-free as-sprayed EBCs were engineered under controlled deposition conditions. The absence of phase transformation and stability of the low elastic modulus values (e.g., ~60-70 GPa) retained by the BSAS top layers after harsh environmental exposure provides a plausible explanation for the almost crack-free coatings observed. The relationships between the measured elastic moduli of the EBCs and their microstructural behavior during the high-temperature exposure are discussed.
机译:硅基陶瓷(例如SiC和Si_3N_4)被公认为在金属/合金达到其最终性能的各种组件(例如高级燃气轮机和未来超音速飞行器的结构组件)中具有前景的高温结构材料。为了减轻硅基陶瓷在高温环境下(例如H_2O蒸气)遭受的表面凹陷,对适当的耐火氧化物进行了工程设计,以用作环境屏障涂层(EBC)。当前最先进的EBC多层系统包括硅(Si)粘合涂层,莫来石(3Al_2O_3·2SiO_2)中间层和(1-x)BaO·xSrO·Al_2O_3·2SiO_2,0≤x≤1(BSAS)面漆。在本文中,研究了在H_2O蒸气环境(时间间隔长达500小时)中进行的高温暴露(1300℃)对沉积在SiC衬底上的空气等离子喷涂Si /莫来石/ BSAS层的弹性模量的作用。深度感应压痕。激光超声被用来评估喷涂的BSAS涂层的E值,以验证压痕结果。在受控的沉积条件下设计了完全结晶,无裂纹和几乎无裂纹的喷涂EBC。在恶劣的环境下暴露后,BSAS顶层仍未保持相变和低弹性模量值(例如〜60-70 GPa)的稳定性,这为观察到的几乎无裂纹的涂层提供了合理的解释。讨论了在高温下测量的EBC的弹性模量与其微观结构行为之间的关系。

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