复合材料科学与工程 ›› 2026, Vol. 0 ›› Issue (9): 138-146.DOI: 10.19936/j.cnki.2096-8000.20260928.016

• 无人机 • 上一篇    下一篇

无人机领域耐高温二氧化硅气凝胶隔热材料研究进展

姬东昊1,2, 卢威3, 孟博1, 赵婉彤1, 艾素芬1*, 季生洪1, 刘佳1   

  1. 1.北京卫星制造厂有限公司,北京 100080;
    2.北华航天工业学院 材料工程学院,廊坊 065009;
    3.北京空间飞行器总体设计部,北京 100094
  • 收稿日期:2026-04-07 出版日期:2026-09-28 发布日期:2026-09-23
  • 通讯作者: 艾素芬(1979—),女,博士,研究员,研究方向为航天高性能隔热材料,sufenai529s@163.com。
  • 作者简介:姬东昊(1999—),男,硕士研究生,研究方向为高温隔热材料。

Research progress on high-temperature resistance of SiO2 aerogel thermal insulation materials in unmanned aerial vehicles

JI Donghao1,2, LU Wei3, MENG Bo1, ZHAO Wantong1, AI Sufen1*, JI Shenghong1, LIU Jia1   

  1. 1. Beijing Spacecraft Manufacturing Factory Co., Ltd., Beijing 100080, China;
    2. School of Materials Engineering, North China Institute of Aerospace Engineering, Langfang 065009, China;
    3. Beijing Institute of Spacecraft System Engineering, Beijing 100094, China
  • Received:2026-04-07 Online:2026-09-28 Published:2026-09-23

摘要: 二氧化硅(SiO2)气凝胶凭借其独特的纳米结构具有优异的隔热性能,在无人机领域已得到广泛应用,但其长期使用温度通常不超过650 ℃,极大地限制了其在无人机发动机高温部位的应用。硅源前驱体的种类和反应特性决定了SiO2气凝胶纳米颗粒的尺寸和晶型,高温下纳米多孔结构的收缩坍塌以及晶型变化影响其耐高温性能。本文综述了有机硅酯、掺杂前驱体、无机前驱体和结晶型前驱体所制备的SiO2气凝胶在耐温性方面的研究进展。研究表明,通过掺杂改性、增大SiO2溶胶颗粒尺寸、调控前驱体颗粒晶型等改性方式,可将SiO2气凝胶耐温性提高至1 200 ℃以上。同时,结合当前研究现状,对耐高温SiO2气凝胶未来的发展方向进行了展望。

关键词: 无人机, 二氧化硅气凝胶, 耐高温, 硅源, 前驱体

Abstract: Silica (SiO2) aerogels exhibit excellent thermal insulation properties owing to their unique nanostructure, and have been widely used in the field of unmanned aerial vehicles (UAVs). However, their practical applications in high-temperature parts of engines are severely restricted by the limitation that their long-term service temperature cannot exceed 650 ℃. The type and reaction characteristics of silicon precursors determine the particle size and crystal phase of SiO2 aerogel nanoparticles. At elevated temperatures, the shrinkage and collapse of nanoporous structures, as well as crystal phase transitions, significantly affect their thermal stability. This paper reviews the research progress on the high-temperature resistance of SiO2 aerogels prepared from organosilicates, doped precursors, inorganic precursors and crystalline precursors. Research has shown that the high-temperature resistance of SiO2 aerogels can be improved to above 1 200 ℃ through modification strategies such as element doping, increasing the particle size of SiO2 sol particles, and regulating the crystal form of precursor particles. Combined with the current research status, the future development directions of high-temperature-resistant SiO2 aerogels are discussed.

Key words: unmanned aerial vehicles, SiO2 aerogel, high-temperature resistant properties, silicon sources, precursor

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