首页> 外文期刊>CERAMICS INTERNATIONAL >Effect of oxidation treatment on KD-II SiC fiber-reinforced SiC composites
【24h】

Effect of oxidation treatment on KD-II SiC fiber-reinforced SiC composites

机译:氧化处理对KD-II SiC纤维增强SiC复合材料的影响

获取原文
获取原文并翻译 | 示例
           

摘要

Continuous silicon carbide fiber-reinforced silicon carbide matrix (SiCf/SiC) composites have developed into a promising candidate for structural materials for high-temperature applications in aerospace engine systems. This is due to their advantageous properties, such as low density, high hardness and strength, and excellent high temperature and oxidation resistance. In this study, SiCf/SiC composites were fabricated via polymer infiltration and pyrolysis (PIP) with the lower- oxygen-content KD-II SiC fiber as the reinforcement; a mixture of 2,4,6,8-tetravinyl-2,4,6,8-tetramethylcyclotetrasiloxane (V4) and liquid polycarbosilane (LPCS), known as LPVCS, was used as the precursor; while pyrolytic carbon (PyC) was used as the interface. The effects of oxidation treatment at different temperatures on morphology, structure, composition, and mechanical properties of the KD-II SiC fibers, SiC matrix from LPVCS precursor conversion, and SiCf/SiC composites were comprehensively investigated. The results revealed that the oxidation treatment greatly impacted the mechanical properties of the SiC fiber, thereby significantly influencing the mechanical properties of the SiCf/SiC composite. After oxidation at 1300 degrees C for 1 h, the strength retention rates of the fiber and composite were 41% and 49%, respectively. In terms of the phase structure, oxidation treatment had little effect on the SiC fiber, while greatly influencing the SiC matrix. A weak peak corresponding to silica (SiO2) appeared after high-temperature treatment of the fiber; however, oxidation treatment of the matrix led to the appearance of a very strong diffraction peak that corresponds to SiO2. The analysis of the morphology and composition indicated cracking of the fiber surface after oxidation treatment, which was increasingly obvious with the increase in the oxidation treatment temperature. The elemental composition of the fiber surface changed significantly, with drastically decreased carbon element content and sharply increased oxygen element content.
机译:连续碳化硅纤维增强碳化硅基质(SICF / SIC)复合材料已经开发成用于航空航天发动机系统的高温应用的有希望的结构材料候选者。这是由于其有利的性质,例如低密度,高硬度和强度,以及优异的高温和抗氧化性。在该研究中,通过聚合物浸润和热解(PIP)制造SICF / SiC复合材料作为增强剂的低氧含量KD-II SiC纤维;使用2,4,6,8-四乙烯基-2,4,6,8-四甲基环四硅氧烷(V4)和液体聚氨基硅烷(LPC)的混合物,称为LPVC,用作前体;虽然热解碳(PYC)用作界面。综合研究了氧化处理在不同温度下的氧化处理,从LPVCS前体转化的SiC基质和SiCF / SiC复合材料的不同温度对不同温度的形态,结构,组成和力学性能。结果表明,氧化处理极大地影响了SiC纤维的力学性能,从而显着影响SiCF / SiC复合材料的机械性能。在1300℃下氧化1小时后,纤维和复合材料的强度保留速率分别为41%和49%。就相结构而言,氧化处理对SiC纤维产生影响,同时大大影响SiC基质。对应于二氧化硅(SiO 2)的弱峰出现在纤维的高温处理后;然而,基质的氧化处理导致对应于SiO 2的非常强的衍射峰的外观。氧化处理后的纤维表面的形态和成分分析表明纤维表面的开裂,随着氧化处理温度的增加而越来越明显。纤维表面的元素组成显着变化,碳元素含量急剧下降,急剧增加的氧元素含量。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号