[1]田蔚,白侠,郭春园.C/C-SiC-HfB2多元陶瓷基复合材料烧蚀机理分析[J].固体火箭技术,2019,42(06):724-729.
 TIAN Wei,BAI Xia,GUO Chunyuan.Oxidation ablation resistance mechanism of C/C-SiC-HfB2 composite[J].Journal of Solid Rocket Technology,2019,42(06):724-729.
点击复制

C/C-SiC-HfB2多元陶瓷基复合材料烧蚀机理分析

参考文献/References:

[1]Fitzer E. The future of carbon-carbon composites[M]. Carbon, 1987, 25(2): 163.[2]刘桂香. 炭/炭复合材料的抗氧化研究[J]. 炭素, 2004 (2): 24-26. LIU Guixiang. Study on the anti-oxidation of carbon/carbon composite[J]. Carbon, 2004 (2): 24-26.[3]HU C, PANG S, TANG S, et al. An integrated composite with a porous Cf/C-ZrB2SiC core between two compact outer layers of Cf/C-ZrB2SiC and Cf/C-SiC[J]. Journal of the European Ceramic Society, 2015, 35: 1113-1117.[4]LIU L, LI H, FENG W, et al. Ablation in different heat fluxes of C/C composites modified by ZrB2ZrC and ZrB2ZrC-SiC particles[J]. Corrosion Science, 2013, 4: 159-167.[5]崔红, 苏君明, 李瑞珍. 添加难熔金属碳化物提高C/C复合材料抗烧蚀性能的研究[J]. 西北工业大学学报, 2000, 18(4): 669-673.CUI Hong, SU Junming, LI Ruizhen. On improving antiablation property of multimatrix C/C to withstand 3700K[J]. Journal of Northwestern Polytechnical University, 2000, 18(4): 669-673.[6]HU C, PANG S, TANG S, et al. Ablation and mechanical behavior of a sandwich-structured composite with an inner layer of Cf/SiC between two outer layers of Cf/SiC-ZrB2ZrC [J]. Corrosion Science, 2014, 80: 54-163.[7]Ravi K, Enneti A. Taguchi analysis on the effect of process parameters on densification during spark plasma sintering of HfB2-20SiC[J].Int. Journal of Refractory Metals and Hard Materials, 2012, 31: 293-296.[8]杨晴晴,唐竹兴. 注凝成型制备HfB2SiC复合陶瓷[J]. 现代技术陶瓷, 2008, 118(4):7-9. YANG Qingqing, TANG Zhuxing. Study on gel-casting processing of HfB-SiC composites[J]. Advanced Ceramics, 2008, 118(4):7-9.[9]王海龙, 赵笑统, 邵刚, 等. HfB2超高温陶瓷复合材料的制备工艺和性能研究[C]//第十九届全国高技术陶瓷学术年会文集. 武汉,2016:71-73.WANG Hailong, ZHAO Xiaotong, SHAO Gang, et al. Preparation and properties of high temperature HfB2 ceramic composites[C]// Proceedings of the 19th National Conference on High Technology Ceramics. Wuhan, 2016: 71-73.[10]孙银洁,李秀涛. 碳纤维增强超高温陶瓷基复合材料的性能与微结构[J]. 宇航材料工艺,2011(6):81-84. SUN Yinjie, LI Xiutao. Properties and microstrures of carbon fiber reinforced ultra-high temperature ceramic matrix composites[J]. Aerospace Material Technology, 2011(6):81-84.[11]王倩,周华丹,柳福提. 六方HfB2晶体电子结构及光学性质的第一性原理计算[J]. 宜宾学院学报, 2016,16(12):93-98. Wang Qian, Zhou Huadan, Liu Futi. First principle calculation of electronic structure and optical properties of hexagon HfB2 crystal[J]. Journal of Yibin College, 2016,16(12):93-98.[12]杨晴晴,唐竹兴. HfB2SiC复合材料研究进展[J]. 现代技术陶瓷,2008(1):14-17. YANG Qingqing, TANG Zhuxing. Progress in HfB2SiC composies[J]. Advanced Ceramics, 2008(1):14-17.[13]郭朝邦. HfB2材料研究进展[J]. 战术导弹技术, 2010(4):32-35.GUO Chaobang. Recent development in HfB2materials[J]. Tactical Missile Technology, 2010(4):32-35.[14]韩杰才,胡平,张幸红. 超高温材料的研究进展[J]. 固体火箭技术, 2005, 28(4):289-294.HAN Jiecai, HU Ping, ZHANG Xinghong. Advances on ultra-high temperature materials[J]. Solid Rocket Technology, 2005, 28(4):289-294.[15]HAN J, HU P, ZHANG X, et al. Oxidation-resistant ZrB2SiC composites at 2200 ℃[J]. Composites Science and Technology, 2008, 68(3-4):799-806.[16]Lespade P, Richet NGoursat P. Oxidation resistance of HfB2SiC composites for protection of carbon based materials[J]. Acta Astronautica, 2005, 60(10-11): 858-864.

相似文献/References:

[1]曹翠微,李照谦,李贺军,等.轴棒法编织三维四向C/C复合材料压缩及弯曲性能[J].固体火箭技术,2011,(02):256.
[2]冯阳阳,崔红,李瑞珍.高温处理对T300级炭纤维结构及性能的影响[J].固体火箭技术,2011,(03):384.
[3]刘姝,孙文强,唐锐,等.高活性铝锂合金的制备及微观结构与水解性能研究[J].固体火箭技术,2012,(03):367.[doi:10.7673/j.issn.1006-2793.2012.03.017]
[4]曹伟锋,李贺军,郭领军,等.两种炭基C/C复合材料的微观结构及弯曲性能对比[J].固体火箭技术,2013,(03):398.
[5]金保宏1,2,高 禹1,等.游离碳对SiC 薄膜微观结构的影响[J].固体火箭技术,2014,(02):258.[doi:10.7673/ j.issn.1006⁃2793.2014.02.022]
 ,,et al.Effects of free carbon on microstructure of SiC film[J].Journal of Solid Rocket Technology,2014,(06):258.[doi:10.7673/ j.issn.1006⁃2793.2014.02.022]
[6]原梅妮,杨延清,弓巧娟,等.SiCp/2024Al复合材料微观结构建模及动态力学性能评估[J].固体火箭技术,2014,(04):541.
[7]孙国栋,李辉,邓娟利.SiC涂层制备工艺对C/C复合材料微观结构及性能的影响[J].固体火箭技术,2016,(01):100.
[8]刘皓,李克智.两种沥青炭的微观结构研究[J].固体火箭技术,2016,(04):565.
[9]秦丽媛,孟松鹤,李金平,等.基于微观图像及内聚力模型的复合材料裂纹扩展模拟[J].固体火箭技术,2017,40(04):501.[doi:10.7673/j.issn.1006-2793.2017.04.018]
 [J].Journal of Solid Rocket Technology,2017,40(06):501.[doi:10.7673/j.issn.1006-2793.2017.04.018]
[10]马新刚,胡伟,谭利敏,等.HTPB微观结构对推进剂力学性能影响[J].固体火箭技术,2017,40(06):730.
 [J].Journal of Solid Rocket Technology,2017,40(06):730.

更新日期/Last Update: 2020-01-14
PDF下载 分享