Journal Home > Volume 11 , Issue 9

Yttria-stabilized zirconia (YSZ) has been used as a thermal barrier coating (TBC) material in gas turbines for several decades. Although continuous efforts have been made to develop novel TBC materials that can work at a higher temperature, no single material other than YSZ has all the desired attributes for the TBCs. In this paper, we report the in-situ synthesis of quasi-binary GdNbO4/Gd3NbO7 composites based on the simple Gd2O3–Nb2O5 binary phase diagram. The fracture toughness of these quasi-binary composites is remarkably enhanced compared with the value predicted by the rule of mixtures because the ferroelastic domain switching is more activated due to the residual stress in the quasi-binary composites, which triggers more crack defections due to the enlarged process zone. Additionally, the Gd3NbO7 phase provides a low thermal conductivity due to the substantial chemical inhomogeneity, which diffuses phonons. Gd3NbO7/GdNbO4 exhibits a balanced thermal conductivity of 1.6 W/(m·K) at 1073 K and a toughness value of 2.76 MPa·m0.5, and these values are among the best comprehensive properties that have been obtained for new TBC materials. The work demonstrates a feasible approach of designing a new TBC material with balanced properties and can be easily fabricated.


menu
Abstract
Full text
Outline
Electronic supplementary material
About this article

In-situ synthesis of gadolinium niobate quasi-binary composites with balanced mechanical and thermal properties for thermal barrier coatings

Show Author's information Yi HANaPeng-an ZONGaMuzhang HUANGaZesheng YANGaYingjie FENGaWei PANaPeng ZHANGa,b( )Chunlei WANa( )
State Key Laboratory of New Ceramics and Fine Processing, School of Materials Science and Engineering, Tsinghua University, Beijing 100084, China
Institute of Welding and Surface Engineering Technology, Faculty of Materials and Manufacturing, Beijing University of Technology, Beijing 100124, China

Abstract

Yttria-stabilized zirconia (YSZ) has been used as a thermal barrier coating (TBC) material in gas turbines for several decades. Although continuous efforts have been made to develop novel TBC materials that can work at a higher temperature, no single material other than YSZ has all the desired attributes for the TBCs. In this paper, we report the in-situ synthesis of quasi-binary GdNbO4/Gd3NbO7 composites based on the simple Gd2O3–Nb2O5 binary phase diagram. The fracture toughness of these quasi-binary composites is remarkably enhanced compared with the value predicted by the rule of mixtures because the ferroelastic domain switching is more activated due to the residual stress in the quasi-binary composites, which triggers more crack defections due to the enlarged process zone. Additionally, the Gd3NbO7 phase provides a low thermal conductivity due to the substantial chemical inhomogeneity, which diffuses phonons. Gd3NbO7/GdNbO4 exhibits a balanced thermal conductivity of 1.6 W/(m·K) at 1073 K and a toughness value of 2.76 MPa·m0.5, and these values are among the best comprehensive properties that have been obtained for new TBC materials. The work demonstrates a feasible approach of designing a new TBC material with balanced properties and can be easily fabricated.

Keywords: thermal conductivity, fracture toughness, residual stress, thermal barrier coating (TBC)

References(54)

[1]
Mercer C, Williams JR, Clarke DR, et al. On a ferroelastic mechanism governing the toughness of metastable tetragonal-prime (t’) yttria-stabilized zirconia. Proc R Soc A 2007, 463: 1393–1408.
[2]
Clarke DR, Oechsner M, Padture NP. Thermal-barrier coatings for more efficient gas-turbine engines. MRS Bull 2012, 37: 891–898.
[3]
Padture NP, Gell M, Jordan EH. Thermal barrier coatings for gas-turbine engine applications. Science 2002, 296: 280–284.
[4]
Padture NP. Advanced structural ceramics in aerospace propulsion. Nat Mater 2016, 15: 804–809.
[5]
Cao XQ, Vassen R, Stoever D. Ceramic materials for thermal barrier coatings. J Eur Ceram Soc 2004, 24: 1–10.
[6]
Saputra R, Walvekar R, Khalid M, et al. Synthesis and thermophysical properties of ethylammonium chloride–glycerol–ZnCl2 ternary deep eutectic solvent. J Mol Liq 2020, 310: 113232.
[7]
Ren XR, Pan W. Mechanical properties of high-temperature-degraded yttria-stabilized zirconia. Acta Mater 2014, 69: 397–406.
[8]
Pan W, Phillpot SR, Wan CL, et al. Low thermal conductivity oxides. MRS Bull 2012, 37: 917–922.
[9]
Vaßen R, Jarligo MO, Steinke T, et al. Overview on advanced thermal barrier coatings. Surf Coat Technol 2010, 205: 938–942.
[10]
Clarke DR, Levi CG. Materials design for the next generation thermal barrier coatings. Annu Rev Mater Res 2003, 33: 383–417.
[11]
Zhu DM, Miller RA. Development of advanced low conductivity thermal barrier coatings. Int J Appl Ceram Technol 2005, 1: 86–94.
[12]
Xu Q, Pan W, Wang JD, et al. Rare-earth zirconate ceramics with fluorite structure for thermal barrier coatings. J Am Ceram Soc 2006, 89: 340–342.
[13]
Wan CL, Pan W, Xu Q, et al. Effect of point defects on the thermal transport properties of (LaxGd1–x)2Zr2O7: Experiment and theoretical model. Phys Rev B 2006, 74: 144109.
[14]
Feng J, Xiao B, Wan CL, et al. Electronic structure, mechanical properties and thermal conductivity of Ln2Zr2O7 (Ln = La, Pr, Nd, Sm, Eu and Gd) pyrochlore. Acta Mater 2011, 59: 1742–1760.
[15]
Curran JA, Kalkancı H, Magurova Y, et al. Mullite-rich plasma electrolytic oxide coatings for thermal barrier applications. Surf Coat Technol 2007, 201: 8683–8687.
[16]
Tian ZL, Zheng LY, Wang JM, et al. Theoretical and experimental determination of the major thermo–mechanical properties of RE2SiO5 (RE = Tb, Dy, Ho, Er, Tm, Yb, Lu, and Y) for environmental and thermal barrier coating applications. J Eur Ceram Soc 2016, 36: 189–202.
[17]
Du AB, Wan CL, Qu ZX, et al. Thermal conductivity of monazite-type REPO4 (RE = La, Ce, Nd, Sm, Eu, Gd). J Am Ceram Soc 2009, 92: 2687–2692.
[18]
Xie XY, Guo HB, Gong SK, et al. Lanthanum–titanium–aluminum oxide: A novel thermal barrier coating material for applications at 1300 ℃. J Eur Ceram Soc 2011, 31: 1677–1683.
[19]
Zhang P, Choy KL. The synthesis of thermochemically stable single phase lanthanum titanium aluminium oxide. Ceram Int 2016, 42: 3261–3267.
[20]
Gadow R, Lischka M. Lanthanum hexaaluminate—novel thermal barrier coatings for gas turbine applications— materials and process development. Surf Coat Technol 2002, 151–152: 392–399.
[21]
Ma W, Mack DE, Vaßen R, et al. Perovskite-type strontium zirconate as a new material for thermal barrier coatings. J Am Ceram Soc 2008, 91: 2630–2635.
[22]
Shian S, Sarin P, Gurak M, et al. The tetragonal–monoclinic, ferroelastic transformation in yttrium tantalate and effect of zirconia alloying. Acta Mater 2014, 69: 196–202.
[23]
Limarga AM, Shian S, Leckie RM, et al. Thermal conductivity of single- and multi-phase compositions in the ZrO2–Y2O3–Ta2O5 system. J Eur Ceram Soc 2014, 34: 3085–3094.
[24]
Pitek FM, Levi CG. Opportunities for TBCs in the ZrO2–YO1.5–TaO2.5 system. Surf Coat Technol 2007, 201: 6044–6050.
[25]
Yang J, Pan W, Han Y, et al. Mechanical properties, oxygen barrier property, and chemical stability of RE3NbO7 for thermal barrier coating. J Am Ceram Soc 2020, 103: 2302–2308.
[26]
Guo L, Yan Z, Dong X, et al. Composition-microstructure-mechanical property relationships and toughening mechanisms of GdPO4-doped Gd2Zr2O7 composites. Compos B: Eng 2019, 161: 473–482.
[27]
Wang CM, Guo L, Zhang Y, et al. Enhanced thermal expansion and fracture toughness of Sc2O3-doped Gd2Zr2O7 ceramics. Ceram Int 2015, 41: 10730–10735.
[28]
Chen L, Jiang YH, Chong XY, et al. Synthesis and thermophysical properties of RETa3O9 (RE = Ce, Nd, Sm, Eu, Gd, Dy, Er) as promising thermal barrier coatings. J Am Ceram Soc 2018, 101: 1266–1278.
[29]
Du AB, Pan W, Ahmad K, et al. Enhanced mechanical properties of machinable LaPO4/Al2O3Composites by spark plasma sintering. Int J Appl Ceram Technol 2009, 6: 236–242.
[30]
Ma W, Jarligo MO, Mack DE, et al. New generation perovskite thermal barrier coating materials. J Therm Spray Technol 2008, 17: 831–837.
[31]
Rödel J, Kelly JF, Lawn BR. In situ measurements of bridged crack interfaces in the scanning electron microscope. J Am Ceram Soc 1990, 73: 3313–3318.
[32]
Zhang P, Feng YJ, Li Y, et al. Thermal and mechanical properties of ferroelastic RENbO4 (RE = Nd, Sm, Gd, Dy, Er, Yb) for thermal barrier coatings. Scripta Mater 2020, 180: 51–56.
[33]
Adachi T, Sekino T, Nakayama T, et al. Measurement of microscopic stress distribution of multilayered composite by X-ray stress analysis. Mater Lett 2003, 57: 3057–3062.
[34]
Shokrieh MM, Ghanei Mohammadi AR. 3-Nondestructive testing (NDT) techniques in the measurement of residual stresses in composite materials: An overview. In: Residual Stresses in Composite Materials, 2nd edn. Woodhead Publishing, 2021: 71–109.
DOI
[35]
Prevey PS. X-ray diffraction residual stress techniques. In: Materials Characterization. ASM International, 1986: 380–392.
DOI
[36]
Roytburd AL, Ouyang J, Artemev A. Polydomain structures in ferroelectric and ferroelastic epitaxial films. J Phys: Condens Matter 2017, 29: 163001.
[37]
Roitburd AL. Equilibrium structure of epitaxial layers. Phys Stat Sol (a) 1976, 37: 329–339.
[38]
Ayatollahi MR, Zakeri M. An improved definition for mode I and mode II crack problems. Eng Fract Mech 2017, 175: 235–246.
[39]
Davidge RW, Green TJ. The strength of two-phase ceramic/glass materials. J Mater Sci 1968, 3: 629–634.
[40]
Agar JC, Damodaran AR, Okatan MB, et al. Highly mobile ferroelastic domain walls in compositionally graded ferroelectric thin films. Nat Mater 2016, 15: 549–556.
[41]
Yang J, Han Y, Shahid M, et al. A promising material for thermal barrier coating: Pyrochlore-related compound Sm2FeTaO7. Scripta Mater 2018, 149: 49–52.
[42]
Feng J, Xiao B, Zhou R, et al. Thermal expansion and conductivity of RE2Sn2O7 (RE = La, Nd, Sm, Gd, Er and Yb) pyrochlores. Scripta Mater 2013, 69: 401–404.
[43]
Zhao M, Ren XR, Yang J, et al. Low thermal conductivity of rare-earth zirconate–stannate solid solutions (Yb2Zr2O7)1–x (Ln2Sn2O7)x (Ln = Nd, Sm). J Am Ceram Soc 2016, 99: 293–299.
[44]
Wang YJ, Zhang L, Wu WJ, et al. Enhancement of thermal properties of ytterbium–cerium oxide by zirconium doping for thermal barrier coatings. Philos Mag Lett 2019, 99: 309–316.
[45]
Lehmann H, Pitzer D, Pracht G, et al. Thermal conductivity and thermal expansion coefficients of the lanthanum rare-earth-element zirconate system. J Am Ceram Soc 2003, 86: 1338–1344.
[46]
Chen L, Wu P, Song P, et al. Potential thermal barrier coating materials: RE3NbO7 (RE = La, Nd, Sm, Eu, Gd, Dy) ceramics. J Am Ceram Soc 2018, 101: 4503–4508.
[47]
Yang J, Qian X, Pan W, et al. Diffused lattice vibration and ultralow thermal conductivity in the binary Ln–Nb–O oxide system. Adv Mater 2019, 31: e1808222.
[48]
Yang J, Wan CL, Zhao M, et al. Effective blocking of radiative thermal conductivity in La2Zr2O7/LaPO4 composites for high temperature thermal insulation applications. J Eur Ceram Soc 2016, 36: 3809–3814.
[49]
Vassen R, Stuke A, Stöver D. Recent developments in the field of thermal barrier coatings. J Therm Spray Technol 2009, 18: 181–186.
[50]
Sarin P, Hughes RW, Lowry DR, et al. High-temperature properties and ferroelastic phase transitions in rare-earth niobates (LnNbO4). J Am Ceram Soc 2014, 97: 3307–3319.
[51]
Mendelson MI. Average grain size in polycrystalline ceramics. J Am Ceram Soc 1969, 52: 443–446.
[52]
Taya M, Hayashi S, Kobayashi AS, et al. Toughening of a particulate-reinforced ceramic-matrix composite by thermal residual stress. J Am Ceram Soc 1990, 73: 1382–1391.
[53]
Ren XR, Guo SC, Zhao M, et al. Thermal conductivity and mechanical properties of YSZ/LaPO4 composites. J Mater Sci 2014, 49: 2243–2251.
[54]
Du LF, Yang SM, Zhang P, et al. Pinning effect of different shape second-phase particles on grain growth in polycrystalline: Numerical and analytical investigations. Compos Interfaces 2018, 25: 357–368.
File
40145_0622_ESM.pdf (719.1 KB)
Publication history
Copyright
Acknowledgements
Rights and permissions

Publication history

Received: 20 February 2022
Revised: 07 June 2022
Accepted: 16 June 2022
Published: 17 August 2022
Issue date: September 2022

Copyright

© The Author(s) 2022.

Acknowledgements

This work was supported by the National Key R&D Program of China (No. 2021YFB3702300), the National Natural Science Foundation of China (No. 52022042), and the China Postdoctoral Science Foundation (No. 2019M650670).

Rights and permissions

Open Access This article is licensed under a Creative Commons Attribution 4.0 International License, which permits use, sharing, adaptation, distribution and reproduction in any medium or format, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons licence, and indicate if changes were made.

The images or other third party material in this article are included in the article’s Creative Commons licence, unless indicated otherwise in a credit line to the material. If material is not included in the article’s Creative Commons licence and your intended use is not permitted by statutory regulation or exceeds the permitted use, you will need to obtain permission directly from the copyright holder.

To view a copy of this licence, visit http://creativecommons.org/licenses/by/4.0/.

Return