首页> 外文会议>Advanced ceramic matrix composites: science and technology of materials, design, applications, performance and integration >CALCIUM-MAGNESIUM ALUMINO-SILICATES (CMAS) REACTION MECHANISMS AND RESISTANCE OF ADVANCED TURBINE ENVIRONMENTAL BARRIER COATINGS FOR SIC/SIC CERAMIC MATRIX COMPOSITES
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CALCIUM-MAGNESIUM ALUMINO-SILICATES (CMAS) REACTION MECHANISMS AND RESISTANCE OF ADVANCED TURBINE ENVIRONMENTAL BARRIER COATINGS FOR SIC/SIC CERAMIC MATRIX COMPOSITES

机译:SIC / SIC陶瓷基复合材料中先进的涡轮机环境屏障涂料的钙镁铝硅酸盐(CMAS)反应机理和耐性

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摘要

Environmental barrier coatings (EBCs) and SiC/SiC ceramic matrix composites (CMCs) systems will play a crucial role in future turbine engines for hot-section component applications because of their ability to significantly increase engine operating temperatures, reduce engine weight and cooling requirements. The development of prime-reliant environmental barrier coatings is an essential requirement to enable the applications of the 2700-3000℉ EBC - CMC systems. This presentation primarily focuses on the reaction mechanisms of advanced NASA environmental barrier coating systems, when in contact with Calcium-Magnesium Alumino-Silicates (CMAS) at high temperatures. Advanced oxide-silicate defect cluster environmental barrier coatings are being designed for ultimate balanced controls of the EBC temperature capability and CMAS reactivity, thus improving the CMAS resistance. Further CMAS mitigation strategies are also discussed.
机译:环保屏障涂层(EBC)和SiC / SiC陶瓷基复合材料(CMC)系统将在未来的热截面部件涡轮发动机中发挥关键作用,因为它们能够显着提高发动机工作温度,降低发动机重量和冷却要求。开发能够应用底漆的环境屏障涂料是实现2700-3000℉EBC-CMC系统应用的基本要求。本演讲主要关注先进的NASA环境屏障涂料系统在高温下与钙镁铝硅酸盐(CMAS)接触时的反应机理。先进的氧化物-硅酸盐缺陷簇环境隔离涂层被设计用于最终平衡地控制EBC温度能力和CMAS反应性,从而提高CMAS耐受性。还讨论了其他CMAS缓解策略。

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