高超声速飞行器热防护材料与结构的研究进展  

Research Progress on the Thermal Protection Materials and Structures in Hypersonic Vehicles

作　　者：杨亚政[1] 杨嘉陵[1] 方岱宁[2] 

机构地区：[1]北京航空航天大学固体力学研究所 [2]清华大学航天航空学院工程力学系,北京100084

出　　处：《应用数学和力学》2008年第1期47-56,共10页Applied Mathematics and Mechanics

摘　　要：高超声速飞行器是航空航天的一个重要发展方向,在未来国防安全中起着重要作用.高超声速飞行器热防护材料与结构是高超声速飞行器设计与制造的关键技术之一,它关系到飞行器的安全.高超声速飞行器热防护材料与结构主要有金属TPS热防护系统、超高温陶瓷、C/C复合材料等.从材料制备、抗氧化、力学与物理性能表征等方面综述了热防护材料与结构的研究与应用现状,评述了其发展趋势.Hypersonic vehicles represent furore trends of military equipments and play an important role in future war. Thermal protection materials and structures, which relate to the safety of hypersonic vehicles, are one of the most key techniques in design and manufacture of hypersonic vehicles. Among these materials and structures, such as metallic temperature protection structure, the a-high temperature ceramics and carbon/carbon composites are usually adopted in design. The recent progresses of research and application of ultra-high temperature materials in preparation, oxidation resistance, mechanical and physical characterization were summarized.

关 键 词：高超声速飞行器 高温 热防护 

分 类 号：V250.1[一般工业技术—材料科学与工程]