期刊文献+

新型高温/超高温热障涂层及制备技术研究进展 被引量:54

Research Progress on New High/ultra-high Temperature Thermal Barrier Coatings and Processing Technologies
原文传递
导出
摘要 简单介绍了先进航空发动机高温/超高温热障涂层(TBCs)的研究背景、意义和现状;简述了近年来国际上在新一代超高温TBCs方面的研究进展。重点介绍了近年来北京航空航天大学在新型高温/超高温TBCs方面的研究成果,包括新型超高温、高隔热陶瓷隔热层材料,1 150℃以上新型抗高温氧化金属粘结层材料,以及电子束物理气相沉积(EB-PVD)、等离子体激活EB-PVD(PA EB-PVD)和等离子物理气相沉积(PS-PVD)等新型制备工艺。最后对TBCs在未来高性能航空发动机上的应用及发展趋势进行了展望。 The research background,significance and current status of high/ultra-high temperature thermal barrier coatings (TBCs) for aero-engine applications are briefly highlighted.The recent research progress in new generation TBCs for ultrahigh temperature applications is reviewed.Emphasis is laid on the recent research achievements of Beihang University which involves new ceramic topcoat materials with superior-high temperature capabilities and thermal barrier performances,novel metallic bond coat materials with good oxidation resistance at temperatures above 1 150 ℃,new processing technologies of TBCs including electron beam physical vapor deposition (EB-PVD),plasma activated EB-PVD (PA EB-PVD) and plasma spray physical vapor deposition (PS-PVD).Eventually,the prospective trends of TBCs for advanced aero-engine applications are forecast.
出处 《航空学报》 EI CAS CSCD 北大核心 2014年第10期2722-2732,共11页 Acta Aeronautica et Astronautica Sinica
基金 国家自然科学基金(375888 51201005)~~
关键词 航空发动机 热障涂层 陶瓷层 粘结层 等离子体激活 电子束物理气相沉积 等离子物理气相沉积 aero-engines thermal barrier coatings ceramics bonding layer plasma activated electron beam physical vapor deposition plasma spray physical vapor deposition
  • 相关文献

参考文献47

  • 1Goward G W.Progress in coatings for gas turbine airfoils[J].Surface & Coatings Technology,1998,108(1/2/3):73-79.
  • 2Milller R A.Thermal barrier coatings for aircraft engines:history and directions[J].Journal of Thermal Spray Technology,1997,6(1):35-42.
  • 3Rebollo N R,Fabrichnay O,Levi C G.Phase stability of Y+Gd co-doped zirconia[J].Zeitschrift Fur Metallkunde,2003,94(3):163-170.
  • 4Rahaman M N,Gross J R,Dutton R E,et al.Phase stability,sintering,and thermal conductivity of plasmasprayed ZrO2-Gd2O3 compositions for potential thermal barrier coating applications[J].Acta Materialia,2006,54(6):1615-1621.
  • 5Leoni M,Jones R,Scardi P.Phase stability of scandia-yttria-stabilized zirconia TBCs[J].Surface & Coatings Technology,1998,108-109:107-113.
  • 6Friedrich C,Gadow R,Schirmer T.Lanthanum hexaaluminate—a new material for atmospheric plasma spraying of advanced thermal barrier coatings[J].Journal of Thermal Spray Technology,2001,10(4):592-859.
  • 7Bansal N P,Zhu D M.Thermal properties of oxides with magnetoplumbite structure for advanced thermal barrier coatings[J].Surface & Coatings Technology,2008,202(12):2698-2703.
  • 8Lehmann H,Pitzer D,Pracht G,et al.Thermal conductivity and thermal expansion coefficients of the lanthanum rare-earth-element zirconate system[J].Journal of the American Ceramic Society,2003,86(8):1338-1344.
  • 9Duderstadt E C,Bangalore A N.Thermal barrier coating system with intermetallic overlay bond coat:U.S.Patent,5238752[P].1993-08-24.
  • 10Schnitt-Thoms K G,Hertter M.Improved oxide resistance of thermal barrier coatings[J].Surface & Coatings Technology,1999,120-121:84-88.

二级参考文献75

  • 1谭福奎.晶格振动对热传导的贡献[J].黔西南民族师范高等专科学校学报,2004(3):71-73. 被引量:3
  • 2胡艳军,彭平,周惦武,李贵发,郑采星,韩绍昌.3d过渡金属在NiAl中占位的第一原理计算[J].中国有色金属学报,2004,14(12):2102-2107. 被引量:8
  • 3Matsumoto K, Itoh Y, Kameda T, EB-PVD Process and Thermal Properties of Hafnia-Based Thermal Barrier Coating [ J ]. Science and Technology of Advanced Materials, 2003(4) : 153 - 158.
  • 4Miller R A, Current Status of Thermal Barrier Coatings-an Overview[J]. SurCoat Technol, 1987, 30:1-11.
  • 5Miller R A, Thermal Barrier Coatings for Aircraft Engines : History and Directions[J]. J Thermal Spray Tech, 1997(6) : 35 -42.
  • 6Cao X Q, Vassen R, Stoever D, Ceramic Materials for Thermal Barrier Coatings [ J ]. Journal of the European Ceramic Society, 2004, 24: 1-10.
  • 7Goward G W. Protective Coating Systems for High-Temperature Gas Turbine Components[J~. Mat Sci Tech, 1986(2) : 194 -200.
  • 8Hecht R J, Goward G W, Elam R C. High Temperature NiCoCrAlY Coatings: United States, Patent No. 3928026[ P], 1975.
  • 9Zhu D M, Miller R A, Thermal Conductivity and Sintering Behavior of Advanced Thermal Barrier Coatings [ R ]. Ohio : Ohio Aerospace Institute, Brook Park, Ohio, 2002.
  • 10Zhu D M, Miller R A. Development of Advanced Low Conductivity Thermal Barrier Coatings [ J ]. International Journal of Applied Ceramic Technology, 2004 ( 1 ) : 86 - 94.

共引文献164

同被引文献555

引证文献54

二级引证文献177

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