C／C-SiC复合材料具有高比强度、高比模量、高热导率、低热膨胀系数和优异的高温抗氧化性能等特点，是新一代的耐高温陶瓷基复合材料，已经被广泛地用作热结构和热防护材料、制动材料以及空间光学系统零部件等。近年来，随着高超声速飞行器和返回式航天运输工具的快速发展，飞行器面临着更多的有高热流、高压气流以及高速粒子冲蚀的环境，这对C／C-SiC复合材料的高温防护技术提出了更高的要求。C／C-SiC复合材料高温防护的研究主要集中在纤维涂层改性、基体改性和高温防护涂层等3个方面，综合近几年国内外的研究报道，从上述3个方面综述了C／C-SiC复合材料高温防护技术的研究进展，总结了各种高温防护技术的制备方法，比较了3种高温防护技术的特点，最后对C／C-SiC复合材料高温防护技术的发展趋势提出了一些见解。
The C/C-SiC composites as a new generation of the high-temperature resistant ceramic matrix com-posite material has delivered improved performance in several applications such as thermal structure and thermal pro-tection systems,advanced friction systems and space optical systems,because of its high specific strength,high mo-dulus,low thermal expansion coefficient and high-temperature oxidation resistance.However,the oxidation and abla-tion resistance of C/C-SiC composites need to be improved to satisfy the demands for the new generation of hypersonic vehicles and reusable space transportation vehicles operated in the extreme environment with high heat flux,high pres-sure airflow and high speed erosion of particles.For C/C-SiC composites,research mainly focus on three methods in-cluding coating modification of carbon fibers,matrix modification and high-temperature protective surface coating.Ac-cording to both internal and external research reports in recent years,new progresses in high-temperature protection of C/C-SiC composites are described in detail.Preparation methods of coating modification of carbon fibers,matrix modi-fication and high-temperature protective surface coating are concluded,while the characteristics of three high-tempera-ture resistance methods are compared.Finally,several opinions of trends in development of high-temperature protec-tion of C/C-SiC composites are put forward.
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