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Towards multifunctional thermal environmental barrier coatings (TEBCs) based on rare-earth pyrosilicate solid-solution ceramics

机译:朝基于稀土吡塞硅酸盐固溶陶瓷的多功能热环境阻挡涂层(TEBCS)

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摘要

The concept of thermal environmental barrier coatings (TEBCs) for SiC-based ceramic matrix composite (CMCs) hot-section components in gas-turbine engines is elucidated. Here, a single dense TEBC layer made of low thermal-conductivity rare-earth (RE) pyrosilicate solid-solutions is expected to perform multiple functions. Several binary solid-solutions are investigated, with some satisfying the following critical requirements for dense TEBCs: (i) good thermal-expansion match with CMCs, (ii) high-temperature phase stability up to 1700 degrees C, (iii) low thermal conductivity, and (iv) resistance to high-temperature attack by calcia-magnesia-aluminosilicate (CMAS) melts. Other considerations and future outlook pertaining to the TEBCs concept are discussed. (C) 2018 Acta Materialia Inc. Published by Elsevier Ltd. All rights reserved.
机译:阐明了用于燃气涡轮发动机中的SiC基陶瓷基质复合物(CMC)热段组分的热环境阻隔涂层(TEBC)的概念。 这里,预期由低导热偏置稀土(RE)吡塞硅酸盐固溶体制成的单致密TEBC层进行多种功能。 研究了几种二元固溶解决方案,一些令人满意的致密TEBCS的关键要求:(i)与CMC的良好热膨胀匹配,(ii)高达1700℃的高温相位稳定性,(iii)低导热率 (IV)通过钙镁氧化铝 - 铝硅酸盐(CMAS)熔化对高温攻击的抗性。 讨论了与TEBCS概念有关的其他考虑因素和未来前景。 (c)2018 Acta Materialia Inc. elsevier有限公司出版。保留所有权利。

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