采用超声波真空浸渍-碳热还原法将ZrB2引入碳纤维预置体, 结合热梯度化学气相渗透、高温石墨化工艺制备了ZrB2改性C/C复合材料. 氧-乙炔烧蚀测试结果表明, 添加了6.87 wt% ZrB2后, C/C复合材料的线烧蚀率和质量烧蚀率分别下降了64.9%和67.5%. 分析表明, C/C复合材料的烧蚀主要是由热化学和热物理反应控制, 机械剥蚀在烧蚀过程中仅起到次要作用. 烧蚀产物ZrO2/B2O3在烧蚀过程中的挥发会带走大量的热, 从而减少了烧蚀火焰对烧蚀表面的热冲击.
ZrB2 was first introduced into carbon preforms through ultrasonic and vacuum immersion-carbonthermal reduction method. After densification using thermal gradient chemical vapor in-ltration and graphitization, ZrB2 doped C/C composites were prepared. The oxyacetylene ablation results show that the linear and mass ablation rates of the composites after doping with 6.87wt% ZrB2 decreased by 64.9% and 67.5%, respectively. The ablation of C/C composites is mainly controlled by thermochemical and thermophysical reactions and mechanical denudation does not play a dominant role. The evaporation of ZrO2/B2O3 during ablation would take away large amounts of heat, reducing the thermal impact of flame to the ablation surface.
参考文献
[1] | Li H J. Carbon-carbon composites. New Carbon Materials, 2001, 16(2): 79-80.[2] Choury J J. Carbon-carbon Materials for Nozzles of Solid Propellant Rocket Motors. In: 12th Propulsion Conference, Palo Alto, CA, 1976, AIAA-76-609.[3] Shen X T, Li K Z, Li H J, et al. Effect of ZrO2 from the oxidation of ZrC on ablation of ZrC modified carbon/carbon composites. Journal of Inorganic Materials, 2009, 24(5): 943-947.[4] Chen Z K, Xiong X, Li G D, et al. Ablation behaviors of carbon/carbon composites with C-SiC-TaC multi-interlayers. Applied Surface Science, 2009, 255(22): 9217-9223.[5] Li S P, Li K Z, Li H J, et al. Effect of HfC on the ablative and mechanical properties of C/C composites. Materials Science and Engineering A, 2009, 517(1/2): 61-67.[6] Norfolk C, Mukasyan A, Hayes D, et al. Processing of mesocarbon microbeads to high-performance materials: Part I. studies towards the sintering mechanism. Carbon, 2004, 42(1): 11-19.[7] Che X P, Zhu S Z, Xu Q. Synthesis of ultra-fine zirconium diboride powders by liquid-phase method. Journal of Synthetic Crystals, 2009, 38: 199-202.[8] Wang C R, Yang J M, Hoffman W. Thermal stability of refractory carbide/boride composites. Materials Chemistry and Physics, 2002, 74(3): 272-281.[9] Zhao J G, Li K Z, Li H J, et al. The in-uence of thermal gradient on pyrocarbon deposition in carbon/carbon composites during the CVI process. Carbon, 2006, 44(4): 786-791.[10] Guo W M, Xiao H N, Yasuda E, et al. Oxidation kinetics and mechanisms of a 2D-C/C composite. Carbon, 2006, 44(15): 3269-3276.[11] Su J M. Research and application of bulk-needled-felt reinforced carbon composites throat. New Carbon Materials, 1997, 12(4): 46-49.[12] Yin J, Xiong X, Zhang H B, et al. Microstructure and ablation performances of dual-matrix carbon/carbon composites. Carbon, 2006, 44(9): 1690-1694.[13] Li C Y, Li K Z, Ouyang H B, et al. Ablation behavior of HfC modi-ed carbon/carbon composites. Rare Metal Materials and Engineering, 2006, 35(Suppl.2): 365-368. |
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