首页|溶胶-凝胶法合成SiZrNOC陶瓷前驱体的微观结构和相演化

溶胶-凝胶法合成SiZrNOC陶瓷前驱体的微观结构和相演化

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陶瓷材料作为一种高强度、高硬度、耐磨性、耐高温的材料,在航空航天领域拥有着广阔的前景.通过溶胶凝胶法以硅酸四乙酯作为硅源,二苯基甲烷二异氰酸酯作为氮源,正丙醇锆作为锆源合成了SiZrNOC预陶瓷聚合物.通过失重率测试结果显示,当Zr/N比为3∶1 时,陶瓷产率最高,达到 53%.使用扫描电子显微镜对陶瓷微观结构进行分析,结果表明,随着热解温度的升高,材料的内部结构变得规整,致密化程度显著增强.设计的陶瓷材料将有能力改善或扩展其在未来航空航天相关领域的应用.为开发高温下具有热稳定性和抗氧化性的材料提供了一个新的选择.
Microstructure and phase evolution of ceramic precursors SiZrNOC synthesized via sol-gel method
Ceramic materials,as a kind of high strength,high hardness,abrasion resistance,and high-temperature resistance materials,have exhibited a broad prospect in the aerospace field.SiZrNOC pre-ceramic polymers were synthesized by sol-gel method using tetraethyl silicate as silicon source,diphenylmethane diisocyanate as nitrogen source,and zirconium n-propanol as zirconium source.The highest ceramic yield of 53%was achieved when the Zr/N ratio was 3∶1,as shown by the results of the weight loss rate test.Analysis of the ceramic microstructure by using scanning electron microscopy showed that the internal structure of the material became regular with increasing pyrolysis temperature,and densification was significantly enhanced.The ceramic materials designed can improve or extend their use in future aerospace-related applications.It provides a new option for developing materials with thermal stability and oxidation resistance at high temperatures.

ceramic precursor SiZrNOCsol-gel methodtransformation ceramics precursorhigh-temperature stability

杨洋、张志新、赵广东

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黑龙江大学 化学化工与材料学院,哈尔滨 150080

SiZrNOC陶瓷先驱体 溶胶凝胶法 前驱体转化陶瓷 高温稳定性

国家自然科学基金

51972082

2024

黑龙江大学工程学报
黑龙江大学

黑龙江大学工程学报

影响因子:0.358
ISSN:2095-008X
年,卷(期):2024.15(2)
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