全部 标题 作者
关键词 摘要

OALib Journal期刊
ISSN: 2333-9721
费用:99美元

查看量下载量

相关文章

更多...
航空学报  2014 

新型高温/超高温热障涂层及制备技术研究进展

DOI: 10.7527/S1000-6893.2014.0161, PP. 2722-2732

Keywords: 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

Full-Text   Cite this paper   Add to My Lib

Abstract:

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,1150℃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(PAEB-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。

References

[1]  Pint B.A.. The Oxidation Behavior of Oxide-Dispersed β-NiAl: IShort-Term Performance at 1200 °C[J].Oxidation of Metals, 1998, 49(5-6):531-559
[2]  Haynes J.A.,Pint BA.,More K.L.,et al. Influence of Sulfur,Platinum,and Hafnium on the Oxidation Behavior of CVD NiAl Bond Coatings[J].Oxidation of Metals, 2002, 58(5-6):513-544
[3]  Hara M, Matsuda Y., Fukumoto M., et al. .Formation of Ni-Aluminide Coating Containing Hf by Molten-Salt Electrodeposition and Cyclic-Oxidation Resistance[J].Oxidation of Metals, 2008, 70:295-306
[4]  Barrett C.A.. Effect of 01 at.% Zirconium on the Cyclic Oxidation Resistance of β-NiAl[J].Oxidation of Metals, 1988, 30(5-6):361-390
[5]  Hamadi S, Bacos M.P., Poulain M., et al. .Oxidation Resistance of a Zr-Doped NiAl Coating Thermochemical-ly Deposited on a Nickel-Based Superalloy[J].Surface & Coatings Technology, 2009, 204:756-760
[6]  Jedlinski J, Mrowec S..The Influence of Implanted Yttrium on the Oxidation Behaviour of β-NiAl[J].Materials Science and Engineering, 1987, 87:281-287
[7]  Mrowec S, Jedlinski J., Gil A.. The Influence of Cer-tain Reactive Elements on the Oxidation Behaviour of Chromia and Alumina-forming Alloys[J].Materials Science and Engineering A, 1989, 120:169-173
[8]  冀晓鹃, 宫声凯, 徐惠彬, 等.添加稀土元素对热障涂层 陶瓷层晶格畸变的影响[J].航空学报, 2007, 28(1):196-200
[9]  JI X J, GONG S K, XU H B, et al.Influence of rare earth elements additions in YSZ ceramic coatings of thermal barrier coatings on lattice distortion[J].Acta Aeronautica Et Astronautic Sinica, 2007, 28(1):196-200
[10]  张红菊.多元稀土氧化物掺杂二氧化锆基热障涂层的制备及热循环性能研究[M]. 北京:北京航空航天大学,2009
[11]  Zhang H J.Preparation and thermal cycling properties study of the multicomponent rare earth oxides doped zirconia Thermal Barrier Coatings[M].Beijing: Beihang University, 2009
[12]  Ma W.Gong SK.,Xu H. B.,et al. The thermal cycling behavior of Lanthanum-Cerium Oxide thermal barrier coating prepared by EB-PVD[J].Surface & Coatings Technology, 2006, 200(16-17):5113-5118
[13]  Ma W.Gong SK.,Xu H. B.,et al. On improving the phase stability and thermal expansion coefficients of lanthanum cerium oxide solid solutions[J].Scripta Materialia, 2006, 54(8):1505-1508
[14]  Ma W.Gong SK.,Li H. F.,et al. Novel thermal barrier coatings based on La2Ce2O78YSZ double-ceramic-layer systems deposited by electron beam physical vapor deposition[J].Surface & Coatings Technology, 2008, 202(12):2704-2708
[15]  Guo L, Guo H.B.,Gong SK.,et al. Improvement on the phase stability,mechanical properties and thermal insulation of Y2O3-stabilized ZrO2 by Gd2O3 and Yb2O3 co-doping[J].Ceramics International, 2013, 39(8):9009-9015
[16]  Guo HB., Zhang T., Wang S.X., et al. .Effect of Dy on Oxide Scale Adhesion of NiAl Coatings at 1200 °C[J].Corrosion Science, 2011, 53:2228-2232
[17]  Li DQ., Guo H.B., Wang D., et al..Cyclic Oxidation of β-NiAl with Various Reactive Element Dopants at 1200 °C[J].Corrosion Science, 2013, 66:125-135
[18]  Zhang T, Guo H.B., Gong S.K., et al..Effects of Dy on the Adherence of Al2O3/NiAl Interface: A Combined First-Principles and Experimental Studies[J].Corrosion Science, 2013, 66:59-66
[19]  郭洪波, 宫声凯, 徐惠彬.先进航空发动机热障涂层技术研究进展[J].中国材料进展, 2009, 29(910):18-26
[20]  Guo H B, Gong S K, Xu H B.Progress inThermal Barrier Coatings for Advanced Aeroengines[J].Materials China, 2009, 29(910):18-26
[21]  Guo H.B.,Vassen R,Stover D.. Atmospheric plasma sprayed thick thermal barrier coatings with high segmentation crack density[J].Surface & Coatings Technology, 2004, 186(3):353-363
[22]  Xu H B, Guo H B, Liu F S, etc..Development of Gradient Thermal Barrier Coatings and Their Hot-Fatigue Behavior[J].Surf Coat Technol., 2000, 130:133-139
[23]  Muehlberger E, Meyer P.LPPS-Thin Film Processes: Overview of Origin and Future Possibilities[J].Thermal Spray., 2009, :737-740
[24]  Von Niessen K, Gindrat M.Vapor phase deposition using a plasma spray process.[J].Journal of engineering for gas turbines and power., 2011, 133(6):133-141
[25]  Hospach A.Mauer G,Va?en R.,et al. Columnar-Structured Thermal Barrier Coatings (TBCs) by Thin Film Low-Pressure Plasma Spraying (LPPS-TF)[J].Journal of Thermal Spray Technology, 2011, 20(1-2):116-120
[26]  Mauer G, Hospach A., Va?en R..Process develop-ment and coating characteristics of plasma spray-PVD[J].Surface & Coatings Technology, 2013, 220:219-224
[27]  Huang, H; Eguchi, K; Kambara, M.Ultrafast thermal plasma physical vapor deposition of yttria-stabilized zirconia for novel thermal barrier coatings[J].Journal of thermal spray technology, 2006, 15(4):83-91
[28]  GOWARD G W.Progress in coatings for gas turbine airfoils[J].Surface & Coatings Technology, 1998, 108(123):73-79
[29]  Milller R.A.. Thermal Barrier Coatings for Aircraft Engines: History and Directions[J].Journal of Thermal Spray Technology, 1997, 6(1):35-42
[30]  Rebollo N.R.,Fabrichnay O,Levi C. G.. Phase sta-bility of Y+Gd co-doped zirconia[J].Zeitschrift Fur Metall-kunde, 2003, 94(3):163-170
[31]  Rahaman M.N.,Gross JR.,Dutton R. E.,et al. Phase stability,sintering,and thermal conductivity of plasma-sprayed ZrO2-Gd2O3 compositions for potential thermal barrier coating applications[J].Acta Materialia, 2006, 54(6):1615-1621
[32]  Leoni M, Jones R., Scardi P..Phase stability of scan-dia–yttria-stabilized zirconia TBCs.[J].Surface & Coatings Technology, 1998, 108:107-113
[33]  Friedrich 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
[34]  Bansal N.P.,Zhu DM.. Thermal properties of oxides with magnetoplumbite structure for advanced thermal barrier coatings[J].Surface & Coatings Technology, 2008, 202(12):2698-2703
[35]  Lehmann H.Pitzer D,Pracht G.,et al. Thermal con-ductivity and thermal expansion coefficients of the lanthanum rare-earth-element zirconate system[J].Journal of the American Ceramic Society, 2003, 86(8):1338-1344
[36]  Duderstadt E.C., Bangalore A.N.. Thermal Barrier Coating System with Intermetallic Overlay Bond Coat[P]. U.S. Patent: 5238752, 1993-08-24
[37]  Schnitt-Thoms K.G., Hertter M.. Improved Oxide Resistance of Thermal Barrier Coatings[J].Surface & Coat-ings Technology, 1999, 120-121:84-88
[38]  Felten E.J.,Pettit FS.. Use of Platinum and Rhodium to Improve Oxide Adherence on Ni-8Cr-6Al Alloys[J].Oxidation of Metals, 1976, 10(1):189-233
[39]  Pint B.A.,Treska M,Hobbst L.W.. The Effect of Various Oxide Dispersions on the Phase Composition and Morphology of A12O3 Scales Grown on β-NiAl[J].Oxida-tion of Metals, 1997, 47(1-2):1-20

Full-Text

Contact Us

service@oalib.com

QQ:3279437679

WhatsApp +8615387084133