Abstract
Thermal barrier coatings (TBCs) are widely used in the aviation industry to improve the service life of components being exposed to high temperatures. Providing a higher resistance compared to conventional coatings, TBCs also improve the performance and lifetime of materials through their thermal insulating characteristic. Resistance of gas turbine components, particularly turbine blades, vanes and combustion chambers, is required to be improved against failures such as corrosion, oxidation and thermal shock as well, since turbine inlet temperatures should be increased to improve the performance of gas turbine engines. Accordingly, it is aimed to obtain a better resistance and durability against the failure mechanisms through enhancement of the methods and materials used in thermal barrier coatings. In this study, thermal barrier coatings used in gas turbines as well as their structure, also the relevant failure mechanisms and the new material groups used in TBCs are discussed.
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References
Heveran CM, Xu JP, Sarin VK et al (2013) Simulation of stresses in TBC–EBC coating systems for ceramic components in gas turbines. Surf Coat Tech 235:354–360
Keyvani A, Saremi M, Sohi MH (2011) Oxidation resistance of YSZ-alumina composites compared to normal YSZ TBC coatings at 1100 °C. J Alloy Compd 509:8370–8377
Davis JR (1997) Protective coatings for superalloys, heat-resistance materials. ASM International, Ohio
Lu Z, Myoung SW, Kim EH et al (2014) Microstructure evolution and thermal durability with coating thickness in APS thermal barrier coatings. Mater Today: Proc 1:35–43
Pujol G, Ansart F, Bonino JP et al (2013) Step-by-step investigation of degradation mechanisms induced by CMAS attack on YSZ materials for TBC applications. Surf Coat Tech 237:71–78
Schulz U, Fritscher K, Leyens C (2000) Two-source jumping beam evaporation for advanced EB-PVD TBC systems. Surf Coat Tech 40:133–134
Padture NP, Gell M, Jordan EH (2002) Thermal barrier coatings for gas-turbine engine applications. Science 296:280–284
Bahadori E, Javadpour S, Shariat MH et al (2013) Preparation and properties of ceramic Al2O3 coating as TBCs on MCrAlY layer applied on Inconel alloy by cathodic plasma electrolytic deposition. Surf Coat Tech 228:611–614
Ma K, Schoenung JM (2011) Isothermal oxidation behavior of cryomilled NiCrAlY bond coat: homogeneity and growth rate of TGO. Surf Coat Tech 205:5178–5185
Evans HE (2011) Oxidation failure of TBC systems: an assessment of mechanisms. Surf Coat Tech 206:1512–1521
Evans AG, Mumm DR, Hutchinson JW et al (2001) Mechanisms controlling the durability of thermal barrier coatings. Prog Mater Sci 46:505–553
Taylor TA, Walsh PN (2004) Thermal expansion of MCrAlY alloys. Surf Coat Tech 177:24–31
Zhang Q, Li CJ, Li CX et al (2008) Study of oxidation behavior of nanostructured NiCrAlY bond coatings deposited by cold spraying. Surf Coat Tech 202:3378–3384
Richer P, Yandouzi M, Beauvais L et al (2010) Oxidation behaviour of CoNiCrAlY bond coats produced by plasma, HVOF and cold gas dynamic spraying. Surf Coat Tech 204:3962–3974
Su L, Zhang W, Sun Y et al (2014) Effect of TGO creep on top-coat cracking induced by cyclic displacement instability in a thermal barrier coating system. Surf Coat Tech 254:410–417
Chen WR, Wu X, Marple BR et al (2008) Pre-oxidation and TGO growth behaviour of an air-plasma-sprayed thermal barrier coating. Surf Coat Tech 202:3787–3796
Karaoglanli AC, Altuncu E, Ozdemir I et al (2011) Structure and durability evaluation of YSZ + Al2O3 composite TBCs with APS and HVOF bond coats under thermal cycling conditions. Surf Coat Tech 205:369–373
Karaoglanli AC, Ogawa K, Turk A et al (2013) Progress in gas turbine performance. Intech, Crotia
Peng H, Wang L, Guo L et al (2012) Degradation of EB-PVD thermal barrier coatings caused by CMAS deposits. Prog Nat Sci Mater Int 22:461–467
Rätzer-Scheibe HJ, Schulz U (2007) The effects of heat treatment and gas atmosphere on the thermal conductivity of APS and EB-PVD PYSZ thermal barrier coatings. Surf Coat Tech 201:7880–7888
Sampath S, Schulz U, Jarligo MO, Kuroda S (2012) Processing science of advanced thermal-barrier systems. MRS Bull Mater Res Soc 37:903–910
Xu H, Guo H (2011) Thermal barrier coatings. Woodhead Publishing, Cambridge
Saremi M, Afrasiabi A, Kobayashi A (2007) Bond coat oxidation and hot corrosion behavior of plasma sprayed YSZ coating on Ni superalloy Trans JWRI 36:41–45
Jones RL (1997) Some aspects of the hot corrosion of thermal barrier coatings. J Therm Spray Technol 6:77–84
Ghosh S (2014) Thermal behavior of glass–ceramic bond coat in a TBC system. Vacuum 101:367–370
Karger M, Vaßen R, Stöver D (2011) Atmospheric plasma sprayed thermal barrier coatings with high segmentation crack densities: spraying process, microstructure and thermal cycling behavior. Surf Coat Tech 206:16–23
Guo HB, Vaßen R, Stöver D (2004) Atmospheric plasma sprayed thick thermal barrier coatings with high segmentation crack density. Surf Coat Tech 186:353–363
Sun J, Fu QG, Liu GN et al (2015) Thermal shock resistance of thermal barrier coatings for nickel-based superalloy by supersonic plasma spraying. Ceram Int 41:9972–9979
Wright PK, Evans AG (1999) Mechanisms governing the performance of thermal barrier coatings. Curr Opin Solid St M 4:255–265
Aygun A (2008) Novel Thermal Barrier Coatings (TBCs) that are resistant to high temperature attack by CaO-MgO-Al2O3-SiO2 (CMAS) glassy deposits, PhD thesis, The Ohio State University
Steinke T, Sebold D, Mack DE et al (2010) A novel test approach for plasma-sprayed coatings tested simultaneously under CMAS and thermal gradient cycling conditions. Surf Coat Tech 2057:2287–2295
Li L, Hitchman N, Knapp J (2010) Failure of thermal barrier coatings subjected to CMAS attack. J Therm Spray Technol 19:148–155
Clarke DR, Levi CG (2003) Materials design for the next generation thermal barrier coating. Ann Rev Mater Res 33:383–417
Strangman T, Raybould D, Jameel A et al (2007) Damage mechanisms, life prediction, and development of EB-PVD thermal barrier coatings for turbine airfoils. Surf Coat Tech 202:658–664
Nicholls JR, Deakinand MJ, Rickerby DS (1999) A Comparison between the erosion behaviour of thermal spray and electron physical beam vapour deposition thermal barrier coatings. Wear 352:233–235
Bose S, Demasi J (1997) Thermal barrier coating experience in gas turbine engines. J Therm Spray Technol 6:99–104
Han M, Zhou G, Huang J, Chen S (2014) Optimization selection of the thermal conductivity of the top ceramic layer in the double-ceramic-layer thermal barrier coatings based on the finite element analysis of thermal insulation. Surf Coat Tech 240:320–326
Hass DD, Slifka AJ, Wadley HNG (2001) Low thermal conductivity vapor deposited zirconia microstructures. Acta Mater 49:973–983
Ferdinando MD, Fossati A, Lavacchi A et al (2010) Isothermal oxidation resistance comparison between air plasma sprayed, vacuum plasma sprayed and high velocity oxygen fuel sprayed CoNiCrAlY bond coats. Surf Coat Tech 204:2499–2503
Richer P, Yandouzi M, Beauvais L et al (2010) Oxidation behaviour of CoNiCrAlY bond coats produced by plasma, HVOF and cold gas dynamic spraying. Surf Coat Tech 204:3962–3974
Ma W, Jarligo MO, Mack DE, Pitzer D et al (2008) New generation perovskite thermal barrier coating materials. J Therm Spray Technol 17:5–6
Clarke DR, Levi CG (2003) Materials design for the next generation thermal barrier coatings. Ann Rev Mater Res 33:383–417
Habibi MH, Wang L, Liang J et al (2013) An investigation on hot corrosion behavior of YSZ-Ta2O5 in Na2SO4 + V2O5 salt at 1100 °C. Corr Sci 75:409–414
Nicholls JR (2003) Advances in coating design for high-performance gas turbines. MRS Bull 28:659–670
Levi CG (2004) Emerging materials and processes for thermal barrier systems. Curr Opin Solid State Mater Sci 8(1):77–91
Ning XJ, Li CX, Li CJ, Yang GJ (2006) Modification of microstructure and electrical conductivity of plasma-sprayed YSZ deposit through postdensification process. Mater Sci Eng 428(1–2):98–105
Vassen R, Cao X, Tietz F, Basu D, Stöver D (1999) Zirconates as new materials for thermal barrier coatings. J Am Ceram Soc 83:2023–2028
Stöver D, Funke C (1999) Directions of the development of thermal barrier coatings in energy applications. J Mater Process Tech 195:92–93
Schulz U, Fritscher K, Leyens C (2000) Two-source jumping beam evaporation for advanced EB-PVD system. Surf Coat Tech 40:133–134
Guo X, Wang Z (1998) Effect of niobia on the defect structure of yttria-stabilized zirconia. J Euro Ceram Soc 18:237–240
Xu H, Wu J (2011) Thermal barrier coatings. Woodhead Publishing, Cambridge
Liu H, Li S, Li Q et al (2010) Investigation on the phase stability, sintering and thermal conductivity of Sc2O3–Y2O3–ZrO2 for thermal barrier coating application. Mater Design 31:2972–2977
Suresh G, Seenivasan G, Krishnaiah MV, Murti PS (1997) Investigation of the thermal conductivity of selected compounds of gadolinium and lanthanum. J Nucl Mater 249:259–261
Saruhan B, Francois P, Kritscher K et al (2004) EB-PVD processing of pyrochlore-structured La2Zr2O7-based TBCs. Surf Coat Tech 182:175–183
Stöver D, Pracht G, Lehmann H et al (2004) New material concepts for the next generation of plasma-sprayed thermal barrier coatings. J Therm Spray Technol 13:76–83
Vassen R, Traeger F, Stöver D (2004) New thermal barrier coatings based on pyrochlore/YSZ double layer systems. Int J Appl Ceram Techl 1:351–356
Cao X, Vassen R, Fischer W et al (2003) Lanthanum-cerium oxide as a thermal barrier-coating material for high-temperature applications. Adv Mater 15:1438–1442
Ma W, Gong SK, Xu HB et al (2006) On improving the phase stability and thermal expansion coefficients of lanthanum cerium oxide solid solutions. Scripta Mater 54:1505–1508
Ma W, Gong SK, Xu HB et al (2006) The thermal cycling behavior of lanthanum-cerium oxide thermal barrier coating prepared by EB–PVD. Surf Coat Tech 200:5113–5118
Xu Z, He L, Mu R et al (2009) Double-ceramic-layer thermal barrier coatings of La2Zr2O7/YSZ deposited by electron beam-physical vapor deposition. J Alloy Compd 473:509–515
Schulz U, Fritscher K, Peters M (1996) EB-PVD Y2O3- and CeO2Y2O3-stabilized zirconia thermal barrier coatings—crystal habit and phase composition. Surf Coat Tech 82:259–269
Leyens C, Schulz U, Fritscher K (2003) Oxidation and lifetime of PYSZ and CeSZ coated Ni-base substrates with MCrAlY bond layers. Mater High Temp 20:475–480
Wu J, Wei X, Padture NP et al (2002) Low thermal conductivity rare-earth zirconates for possible thermal-barrier coatings application. J Am Ceram Soc 85:3031–3035
Lee KN (2006) In the gas turbine handbook. NETL, Cleveland
Zhu DM, Miller RA (2002) In: Lin HT, Singht M (eds) Thermal conductivity and sintering behavior of advanced thermal barrier coatings, 4th edn. The American Ceramic Society, Florida
Zhu DM, Chen YL, Miller RA (2003) Defect clustering and nano-phase structure characterization of multi-component rare earth oxide doped zirconia-yttria thermal barrier coatings. Ceram Eng Sci Proc 24:525–534
Almeida DS, Silva CRM, Nono MCA et al (2007) Thermal conductivity investigation of zirconia co-doped with yttria and niobia EB-PVD TBCs. Mater Sci Eng, A 443:60–65
Tamarin YA, Kachanov EB, Zherzdev SV (1997) Thermophysical properties of ceramic layers in TBC-EB. Mater Sci Forum 251–254:949–956
Nicholls JR, Lawson KJ, Johnstone A et al (2001) Low thermal conductivity EB-PVD thermal barrier coatings. Mater Sci Forum 369:595–606
Nicholls JR, Lawson KJ, Johnstone A et al (2002) Methods to reduce the thermal conductivity of EB-PVD TBCs. Surf Coat Tech 151–152:383–391
Gao W, Li Z (2008) Developments in high temperature corrosion and protection of materials. Woodhead Publishing, Cambridge
Thornton J, Majumdar A, Mcadam G (1997) Enhanced cerium migration in ceria-stabilised zirconia. Surf Coat Tech 94(95):112–117
Agarwal AK, Pandey A, Gupta AK et al (2014) Novel combustion concepts for sustainable energy development. Springer, India
Singh J, Wolfe DE, Miller RA et al (2004) Tailored Microstructure of zirconia and hafnia-based thermal barrier coatings with low thermal conductivity and high hemispherical reflectance by EB-PVD. J Mater Sci 39:1975–1985
Gadow R, Lischka M (2002) Lanthanum hexaaluminate—novel thermal barrier coatings for gas turbine applications—materials and process development. Surf Coat Tech 151:392–399
Cao XQ, Vassen R, Stöver D (2004) Ceramic materials for thermal barrier coatings. J Euro Ceram Soc 24:1–10
Cao XQ, Zhang YF, Zhang JF (2008) Failure of the plasma-sprayed coating of lanthanum hexaluminate. J Euro Ceram Soc 28:1979–1986
Acknowledgments
This work was partially supported by The Scientific and Technological Research Council of Turkey (TUBITAK, 113R049).
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Karaoglanli, A.C., Doleker, K.M., Ozgurluk, Y. (2017). State of the Art Thermal Barrier Coating (TBC) Materials and TBC Failure Mechanisms . In: Öchsner, A., Altenbach, H. (eds) Properties and Characterization of Modern Materials . Advanced Structured Materials, vol 33. Springer, Singapore. https://doi.org/10.1007/978-981-10-1602-8_34
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DOI: https://doi.org/10.1007/978-981-10-1602-8_34
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