欢迎登录材料期刊网

材料期刊网

高级检索

热障涂层(TBCs)技术已成为当今各国航空发动机推进计划中的3大关键技术之一,其涂层寿命的评估与预测是TBCs技术研究中的重要环节。简述了TBCs的失效形式和对影响其使用寿命关键因素的研究现状,旨在为建立寿命预测模型提供参考。

参考文献

[1] 陈孟成,霍晓,高阳,李建平,李伟光.高温涂层的研究和发展[J].材料工程,1999(06):40-42.
[2] Trunova O.Effect of Thermal and Mechanical Loadings on the Degradation and Failure Models of APS TBCs[M].Germany:RWTH Aachen,2006:1-3.
[3] Nitin P. Padture;Maurice Gell;Eric H. Jordan .Thermal Barrier Coatings for Gas-Turbine Engine Applications[J].Science,2002(5566):280-284.
[4] Taylor M P;Pragnell W M;Evans H E .The influence of on chemical failure and de- lamination in TBC systems[J].Materials and Corrosion,2008,59(06):508513.
[5] A. G. Evans;D. R. Mumm;J. W. Hutchinson;G. H. Meier;F. S. Pettit .Mechanisms controlling the durability of thermal barrier coatings[J].Progress in materials science,2001(5):505-553.
[6] Jones R L .Some Aspects of the Hot Corrosion of Thermal Barrier Coatings[J].Journal of Thermal Spray Technolo- gy,1997,6(01):77-84.
[7] Mennicke C;Mumm D R;Clarke D R .Transient phase evolution during oxidation of a two-phase NiCoCrA1Y bond coat[J].Zeitschrift fur Metallkunde,1999,90(12):1079-1085.
[8] Lee E Y;Biederman R R;Sisson R D .Diffusional inter- actions and reactions between a partially stabilized zirconia thermal barrier coating and the NiCrA1Y bond coat[J].Materilas Science and Engineering A,1989,120/121(01):467-473.
[9] D. R. Mumm and A. G. Evans .ON THE ROLE OF IMPERFECTIONS IN THE FAILURE OF A THERMAL BARRIER COATING MADE BY ELECTRON BEAM DEPOSITION[J].Acta materialia,2000(8):1815-1827.
[10] 周长海 .几种金属材料在压应力及强磁场下的高温氧化[D].大连理工大学,2009.
[11] Miller R A .Life Modeling of Thermal Barrier Coatings for Aircraft Gas Turbine Engines[J].Journal of Engineering for Gas Turbines and Power,Transactions of the ASME,1989,111(02):301-305.
[12] Sun Z Q;Li M S;Zhou Y C .Thermal properties of singe - phase Y2Si05[J].Journal of the European Ceramic Soci- ety,2009,29(04):551-557.
[13] Schulz U;Fritscher K;Peters M .EB-PVD Yz03- and CeOJY203- stabilized zirconia thermal barrier coat- ings Crystal habit and phase composition[J].Surface and Coatings Technology,1996,82(03):259-269.
[14] Vassen R.;Cao X. .Zirconates as New Materials for Thermal Barrier Coatings[J].Journal of the American Ceramic Society,2000(8):2023-2028.
[15] X. Q. Cao;R. Vassen;W. Jungen .Thermal Stability of Lanthanum Zirconate Plasma-Sprayed Coating[J].Journal of the American Ceramic Society,2001(9):2086-2090.
[16] Ahrens M;Vassen R;Stoever D .Stress distribution in plasma-sprayed thermal barrier coatings as a function of interface roughness and oxide scale thickness[J].Sur- face and Coatings Technology,2002,161(01):26-35.
[17] 高阳,潘峰,曾飞,王仁智.喷丸处理对热障涂层中NiCrAlY结合层的影响[J].材料保护,2003(07):11-12.
[18] Dmitry Naumenko;Vladimir shemet;Lorenz singheiser;Willem Josef Quadakkers .Failure mechanisms of thermal barrier coatings on MCrA1Y-type bondcoats associated with the formation of the thermally grown oxide[J].Journal of Materials Science,2009(7):1687-1703.
[19] J. Rosler;M. Baker;K. Aufzug .A parametric study of the stress state of thermal barrier coatings. Part I: creep relaxation[J].Acta materialia,2004(16):4809-4817.
[20] Tolpygo, VK;Clarke, DR .Rumpling of CVD (Ni,Pt)Al diffusion coatings under intermediate temperature cycling[J].Surface & Coatings Technology,2009(20/21):3278-3285.
[21] M. Ranjbar-Far .Simulation of the effect of material properties and interface roughness on the stress distribution in thermal barrier coatings using finite element method[J].Materials & design,2010(2):772-781.
[22] E.TZIMAS;H.MULLEJANS .FAILURE OF THERMAL BARRIER COATING SYSTEMS UNDER CYCLIC THERMOMECHANICAL LOADING[J].Acta materialia,2000(18/19):4699-4707.
[23] Zhu D;Miller R A .Investigation of thermal high cycle and low cycle fatigue mechanisms of thick thermal barrier coatings[J].Materials Science and Engineering A,1998,245(02):212-223.
[24] Gayda J;Gabb T B;Miner R V .Low cycle fatigue behav- iour of a plasma - sprayed coating material[J].Interna- tional Journal of Fatigue,1986,8(04):217-223.
[25] Wright P K .Influence of cyclic strain on life of a PVD TBC[J].Materials Science and Engineering A,1998,245(02):191-200.
[26] Kadioglu Y;Sehitoglu H .Thermomechanical fatigue be- havior of coated and bare Nickel- based superalloy single crystals[J].Journal of Engineering Materials and Tech- nology,1997,118(01):94-102.
[27] Baufeld B.;Mullejans H.;Peteves S.;Bressers J.;Stamm W.;Tzimas E. .Thermal-mechanical fatigue of MAR-M 509 with a thermal barrier coating[J].Materials Science & Engineering, A. Structural Materials: Properties, Misrostructure and Processing,2001(1/2):231-239.
[28] Park SY;Kim JH;Kim MC;Song HS;Park CG .Microscopic observation of degradation behavior in yttria and ceria stabilized zirconia thermal barrier coatings under hot corrosion[J].Surface & Coatings Technology,2005(2/3):357-365.
[29] X.H. Zhong;Y.M. Wang;Z.H. Xu .Hot-corrosion behaviors of overlay-clad yttria-stabilized zirconia coatings in contact with vanadate-sulfate salts[J].Journal of the European Ceramic Society,2010(6):1401-1408.
[30] Hertl W .Vanadia reactions with yttria stabilized zirconia[J].Journal of Applied Physics,1988,63(11):5514-5520.
[31] Zhong X H;Wang Y M;Xu Z H et al.Influence of laser-glazing on hot corrosion resistance of yttria-stabilized zirconia TBC in molten salt mixture of V2 05 and Na2 SO4[J].Materials and Corrosion,2009,60(11):882-888.
[32] Miller R A;Bemdt C C .Performance of thermal barrier coatings in high heat flux environments[J].Thin Solid Films,1984,119(02):195-202.
[33] Batista C;Portinha A;Ribeiro RM;Teixeira V;Oliveira CR .Evaluation of laser-glazed plasma-sprayed thermal barrier coatings under high temperature exposure to molten salts[J].Surface & Coatings Technology,2006(24):6783-6791.
[34] Dongming Zhu;Robert A. Miller .Sintering and creep behavior of plasma-sprayed zirconia-and hafnia-based thermal barrier coatings[J].Surface & Coatings Technology,1998(1/3):114-120.
[35] Vassen R.;Mallener W.;Stamm W.;Stover D.;Czech N. .Influence of impurity content and porosity of plasma-sprayed yttria-stabilized zirconia layers on the sintering behaviour[J].Surface & Coatings Technology,2001(2/3):135-140.
[36] Jie Wu;Xuezheng Wei;Nitin P. Padture .Low-Thermal-Conductivity Rare-Earth Zirconates for Potential Thermal-Barrier-Coating Applications[J].Journal of the American Ceramic Society,2002(12):3031-3035.
[37] K. A. Khor;J. Yang .Plasma sprayed ZrO2-Sm2O3 coatings: lattice parameters, tetragonality (c/a) and transformability of tetragonal zirconia phase[J].Journal of Materials Science Letters,1997(12):1002-1004.
[38] Ibegazene H.;Diot C.;Alperine S. .YTTRIA-STABILIZED HAFNIA-ZIRCONIA THERMAL BARRIER COATINGS - THE INFLUENCE OF HAFNIA ADDITION ON TBC STRUCTURE AND HIGH-TEMPERATURE BEHAVIOUR[J].Journal of Materials Science,1995(4):938-951.
[39] Brian Gleeson .Thermal Barrier Coatings for Aeroengine Applications[J].Journal of Propulsion & Power,2006(2):375-383.
[40] C. Mercer;S. Faulhaber;A.G. Evans .A delamination mechanism for thermal barrier coatings subject to calcium-magnesium-alumino-silicate (CMAS) infiltration[J].Acta materialia,2005(4):1029-1039.
上一张 下一张
上一张 下一张
计量
  • 下载量()
  • 访问量()
文章评分
  • 您的评分:
  • 1
    0%
  • 2
    0%
  • 3
    0%
  • 4
    0%
  • 5
    0%