期刊文献+

固渗+EB-PVD法制备炭/炭复合材料防氧化复合涂层研究 被引量:2

RESEARCH ON ANTI-OXIDATION COATING OF CARBON/CARBON COMPOSITES PREPARED BY PACK CEMENTATION EB-PVD PROCESS
下载PDF
导出
摘要 制备出了SiC/SiC-Al2O3-Y2O3炭/炭复合材料防氧化复合涂层,该复合涂层的内层SiC基涂层采用料浆固渗法制备,SiC-Al2O3-Y2O3外层涂层采用大功率电子束物理气相沉积法。研究表明,电子束物理气相沉积法能达到较好的沉积效果,在制备过程中形成了柱状晶结构的涂层,使得涂层具有更高的应变容限,涂层非常均匀致密。用SEM、XPS和EDS等分析方法分析了涂层的防氧化机理。结果表明:在制备过程和氧化过程中,涂层内会发生复杂的物理和化学变化,生成硅酸盐氧化物,显示出电子束物理气相沉积法在制备炭/炭复合材料防氧化涂层方面独特的优势。 An anti-oxldation multilayer coating d SiC/ SiC -Al2O3- Y2O3 had been prepared in this research. The inner layer d SiC was made by pack cementation, and the out layer of SiC - Al2O3 - Y2O3 multilayer was made by high - power electron beam physics vapor deposition(EB - PVD). The results showed that electron beam physics vapor deposition could improve deposition effect. There was a kind of column crystal structure generated on the coating during the procese of preparation, which made the coating have higher strain capability. SEM, XPS and EDS were used to analyse the anti - oxidation mechanism of the coating. The results showed that during the process of preparation and oxidation, some complicated physical and chemical reactions took place at interior coating, and formed silicate oxides, which showed unique superiority of EB - PVD on the preparation of oxidation resistance coatings for C/C composites.
出处 《炭素技术》 CAS CSCD 2007年第3期1-5,共5页 Carbon Techniques
基金 武器装备重点实验室预研基金项目(51469010305HK0101) 教育部新世纪优秀人才资助计划(NCET-05-0195) 北京特色新材料产业关键技术开发项目(Y406001040211)
关键词 炭/炭复合材料 电子束物理气相沉积 涂层 防氧化 Carbon/carbon composites electron beam physics vapor deposition coatings oxidation
  • 相关文献

参考文献13

  • 1D W MCKEE.Oxidation behavior and protection of carbon/carbon composites[J].Carbon,1987,25(4):551~557.
  • 2M E WESTWOOD,J D WEBSTER,R J DAY,F H HAYES and R TAYLOR.Oxidation protection for carbon fibre composites-review[J] J Mat Sci,1996,18(16):1389~1397.
  • 3B P JIANG.Oxidation behavior of C/C composites with/without CVD ceramic coatings[D].Ph.D.Dissertation,the Graduate Factuate of Aulurn Unversity U.S.1995.
  • 4T L DHAMI,O P BAHL and B R AWASTHY.Oxidation-resistant carbon-carbon composites up to 1700℃[J].Carbon,1995,33(4):479~490.
  • 5C A A CAIRO,M L A GRACA,C R M SILVA and J C BRESSIANI.Functionally gradient ceramic coating for carbon-carbon antioxidation protection[J].Journal of the European Ceramic Society,2001,21(3):325~329.
  • 6R Y LUO,J W CHENG,T M WANG.Oxidation behavior and protection of carbon/carbon composites prepared using rapid directional diffused CVI techniques[J].Carbon,2002,40(11):1965~1972.
  • 7R Y LUO,Z YANG,L F LI.Effect of additives on mechanical properties of oxidation-resistant carbon/carbon composite fabricated by rapid CVD method[J].Carbon,2000,38(15):2109~2115.
  • 8J F HUANG,X R ZENG,H J U,X B XIONG,M HUANG.Mullite-Al2O3-SiC oxidation protective coating for carbon/carbon composites.Carbon 2003;41(14):2825~2829.
  • 9李美姮,张重远,孙晓峰,管恒荣,胡壮麒,胡望宇,宫声凯.电子束物理气相沉积热障涂层的高温氧化行为[J].金属学报,2002,38(9):989-993. 被引量:8
  • 10项民,张琦,骆军华.电子束物理气相沉积热障涂层寿命预测模型[J].宇航材料工艺,2005,35(5):57-59. 被引量:2

二级参考文献14

  • 1楼翰一,唐幼军,孙晓峰,管恒荣.K17F高温合金溅射微晶层的抗高温氧化行为[J].金属学报,1994,30(3). 被引量:13
  • 2Siegmann S D ,Brown C A. Scale-sensitive fractal analysis for understanding the influence of substrate roughness in thermal spraying. In: Berndt C C ed. Proceedings of the first united thermal spray conference, Materials Park, OH - USA:ASM International, 1998:149 ~ 158.
  • 3Dayanda M A,Sohn Y H. Interdiffusion between McrAIY coatings and selected Ni-base alloys. In : Narendra BD,Janet MH , Jacob J eds. Proceedings of the symposium on high temperature coatings-Ⅰ, Warrendale , pennsylvania : Minerals ,Metals & Materials Society, 1995:107 ~ 120.
  • 4Padture N P, Gell M, Jordan E H. Thermal barrier coatings for gas-turbine engine application. Science, 2002;296: 280 ~ 284.
  • 5Demasi J T, Sheffler K D, Ortiz M. Thermal barrier coating life prediction model development. Phase Ⅰ Final Report, Contract NAS3-23944, NASA CR- 182230.
  • 6Meier S M, Nissley D M, Sheffler K D. Thermal barrier coating life prediction model development. Phase Ⅱ Final Report, Contract NAS3 - 23944, NASA CR - 189111.
  • 7Cruse T A,Stewart S E, Ortiz M. Thermal barrier coating life prediction model development. Journal of Enginnering for Gas Turbines and Power, 1988; 110:610~616.
  • 8Meier S M, Nissley D M, Sheffler K D et al. Thermal barrier coating life prediction model development. Journal of Enginnering for Gas Turbines and Power, 1992; 114:258 ~ 263.
  • 9Miller R A. Life modeling of thermal barrier coatings for aircraft gas turbine engines. J . Eng. Gas Turb. & Power , 1989 ;111:301~305.
  • 10Meier S M, Gupla D K. The evolution of thermal barrier coatings in gas turbine engine application. Journal of Enginnering of Gas Turbines and Power, 1994;116:250 ~257.

共引文献8

同被引文献19

引证文献2

二级引证文献7

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部