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Boron-bearing species in ceramic matrix composites for long-term aerospace applications

机译:长期航空航天应用中陶瓷基复合材料中的含硼物质

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Boron-bearing refractory species are introduced in non-oxide ceramic matrix fibrous composites (such as SiC/SiC composites) to improve their oxidation resistance under load at high temperatures with a view to applications in the aerospace field. B-doped pyrocarbon and hex-BN have been successfully used as interphase (instead of pure pyrocarbon) either as homogeneous or multilayered fiber coatings, to arrest and deflect matrix cracks formed under load (mechanical fuse function) and to give toughness to the materials. A self-healing multilayered matrix is designed and used in a model composite, which combines B-doped pyrocarbon mechanical fuse layers and B- and Si-bearing compound (namely B4C and SiC) layers forming B2O3-based fluid healing phases when exposed to an oxidizing atmosphere. All the materials are deposited by chemical vapor infiltration. Lifetimes under tensile loading of several hundreds hours at high temperatures are reported. (C) 2003 Published by Elsevier Inc. [References: 27]
机译:为了在航空航天领域中的应用,将含硼的耐火物质引入非氧化物陶瓷基纤维复合材料(例如SiC / SiC复合材料)中,以提高其在高温下的负荷下的抗氧化性。掺B的焦碳和Hex-BN已成功地用作均相或多层纤维涂层的相间(代替纯焦碳),以阻止和偏转在载荷作用下形成的基体裂纹(机械熔断器功能)并赋予材料韧性。设计了一种可自我修复的多层基质,并将其用于模型复合材料中,该复合材料将B掺杂的热碳机械熔断层与B和含硅化合物(即B4C和SiC)层结合在一起,形成B2O3基流体愈合阶段。氧化气氛。所有材料都是通过化学气相渗透沉积的。据报道在高温下数百小时的拉伸载荷下的寿命。 (C)2003年由Elsevier Inc.出版。[参考:27]

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