Effect of Microstructural Regulation on CMAS Corrosion Resistance of PS-PVD Coatings

FENG Xiaolong, HE Qing, LI Xinhui, LI Jianchao

Surface Technology ›› 2026, Vol. 55 ›› Issue (3) : 72-83.

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Surface Technology ›› 2026, Vol. 55 ›› Issue (3) : 72-83. DOI: 10.16490/j.cnki.issn.1001-3660.2026.03.007
Special Topic—High-temperature Protective Coatings for Advanced Engines

Effect of Microstructural Regulation on CMAS Corrosion Resistance of PS-PVD Coatings

  • FENG Xiaolong1,2, HE Qing1,2,*, LI Xinhui1,2, LI Jianchao1,2
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Abstract

This study aims to enhance the resistance of columnar-like thermal barrier coatings (TBCs) fabricated by plasma physical vapor deposition (PS-PVD) against Calcium-Magnesium-Alumino-Silicate (CMAS) corrosion, and to elucidate the influence of surface microstructural modification on corrosion resistance and thermal shock lifetime. Yttria-stabilized zirconia (8YSZ) and Yb-modified gadolinium zirconate ((Gd0.9Yb0.1)2Zr2O7,GYbZ) are selected as the ceramic coating and protective layer materials in this work. Owing to the high-power and low-pressure characteristics of the PS-PVD process, controlled adjustment of processing parameters allows mixed-phase (solid-liquid-vapor) deposition, enabling microstructural design and optimization of the coating to meet diverse functional and performance requirements. A PS-PVD process dominated by liquid-phase deposition is developed through optimization of spraying parameters, enabling the formation of a dense protective layer. A tri-layered 8YSZ/GYbZ/dense GYbZ TBC system is continuously deposited on the substrate surface. The thermal shock behavior and CMAS corrosion resistance of the coatings are systematically evaluated, and their microstructure, phase composition, and elemental distribution are characterized by scanning electron microscopy (SEM) and X-ray diffraction (XRD). Results indicate that the protective layer exhibits a predominantly lamellar structure containing a small number of partially molten particles, in sharp contrast to the columnar structures of the underlying 8YSZ and GYbZ layers, leading to a significant improvement in coating density. The protective layer is bonded to the ceramic surface without any detectable interfacial cracks or delamination. In addition, it effectively covers the intercolumnar gaps and seals the open pores on the surface of the ceramic layer, thereby improving surface integrity. Furthermore, its incorporation does not markedly reduce the thermal shock resistance, with the coating sustaining up to 110 water-quenching cycles. For the samples without a protective layer, coating spallation primarily occurs at the thermally grown oxide (TGO) and the ceramic layer leads to large-area delamination of the ceramic coating. In contrast, for the samples with a protective layer, spallation mainly takes place at the interface between the protective layer and the ceramic layer. Owing to the relatively low strain tolerance of the protective layer, significant interfacial stresses are generated initiating crack formation. However, lateral cracks at the interface effectively impede the downward propagation of surface vertical cracks, thereby preventing large-scale delamination of the ceramic layer. Three types of region-specific CMAS powders are synthesized according to the compositions of deposits extracted from the surfaces of engine blades operating in different regions, in order to assess the coating's resistance to CMAS corrosion under various environmental contaminant conditions. CMAS corrosion tests conducted at 1 250 ℃ for 2 h using compositions representative of different geographical sources reveal that the protective layer effectively suppresses CMAS infiltration. This improvement is attributed to two synergistic mechanisms: (i) the dense microstructure providing a physical barrier to melt penetration, and (ii) the in-situ formation of high-melting-point apatite and spinel phases during the CMAS-coating interaction, which increase melt viscosity and further retard infiltration. The average CMAS penetration depth in samples with the protective layer is only 29.8% of that in unprotected coatings. Additionally, the dense protective layer effectively seals open pores, including intercolumnar gaps, feather-like dendritic voids, and microcracks, thereby mitigating CMAS infiltration driven by capillary forces and significantly enhancing the coating's overall corrosion resistance.

Key words

PS-PVD / thermal barrier coatings / CMAS / corrosion behavior / dense coating

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FENG Xiaolong, HE Qing, LI Xinhui, LI Jianchao. Effect of Microstructural Regulation on CMAS Corrosion Resistance of PS-PVD Coatings[J]. Surface Technology. 2026, 55(3): 72-83

References

[1] WEI Z Y, MENG G H, CHEN L, et al.Progress in Ceramic Materials and Structure Design Toward Advanced Thermal Barrier Coatings[J]. Journal of Advanced Ceramics, 2022, 11(7): 985-1068.
[2] 曹学强. 新型热障涂层材料研究进展[J]. 硅酸盐学报, 2020, 48(10): 1622-1635.
CAO X Q.Development on New Thermal Barrier Coating Materials[J]. Journal of the Chinese Ceramic Society, 2020, 48(10): 1622-1635.
[3] 魏晓东, 侯国梁, 赵荻, 等. 氧化物掺杂YSZ热障涂层的最新研究进展[J]. 表面技术, 2020, 49(6): 92-103.
WEI X D, HOU G L, ZHAO D, et al.Recent Research Progress on Oxide Doped YSZ Thermal Barrier Coatings[J]. Surface Technology, 2020, 49(6): 92-103.
[4] MILLER R A.Thermal Barrier Coatings for Aircraft Engines: History and Directions[J]. Journal of Thermal Spray Technology, 1997, 6(1): 35-42.
[5] SCHULZ U, LEYENS C, FRITSCHER K, et al.Some Recent Trends in Research and Technology of Advanced Thermal Barrier Coatings[J]. Aerospace Science and Technology, 2003, 7(1): 73-80.
[6] DEMASI-MARCIN J T, GUPTA D K. Protective Coatings in the Gas Turbine Engine[J]. Surface and Coatings Technology, 1994, 68: 1-9.
[7] ZHANG Y, GUO L, ZHAO X X, et al.Toughening Effect of Yb2O3 Stabilized ZrO2 Doped in Gd2Zr2O7 Ceramic for Thermal Barrier Coatings[J]. Materials Science and Engineering: A, 2015, 648: 385-391.
[8] GUO L, GUO H B, PENG H, et al.Thermophysical Properties of Yb2O3 Doped Gd2Zr2O7 and Thermal Cycling Durability of (Gd0.9Yb0.1)2Zr2O7/YSZ Thermal Barrier Coatings[J]. Journal of the European Ceramic Society, 2014, 34(5): 1255-1263.
[9] WANG X Z, GUO L, ZHANG H L, et al.Structural Evolution and Thermal Conductivities of (Gd1-x Ybx)2Zr2O7 (x=0, 0.02, 0.04, 0.06, 0.08, 0.1) Ceramics for Thermal Barrier Coatings[J]. Ceramics International, 2015, 41(10): 12621-12625.
[10] 石佳, 魏亮亮, 张宝鹏, 等. 等离子物理气相沉积热障涂层研究进展[J]. 航空材料学报, 2018, 38(2): 1-9.
SHI J, WEI L L, ZHANG B P, et al.Research Process in Plasma Spray Physical Vapor Deposited Thermal Barrier Coatings[J]. Journal of Aeronautical Materials, 2018, 38(2): 1-9.
[11] LI X, DENG C M, NIU S P, et al.Effect of Calcination Temperature on the Microstructure, Composition and Properties of Nanometer Agglomerated 8YSZ Powders for Plasma Spray-Physical Vapor Deposition (PS-PVD) and Coatings Thereof[J]. Ceramics International, 2021, 47(12): 16632-16640.
[12] ANWAAR A, WEI L, GUO H B, et al.Plasma-Powder Feedstock Interaction during Plasma Spray-Physical Vapor Deposition[J]. Journal of Thermal Spray Technology, 2017, 26(3): 292-301.
[13] HARDER B J, ZHU D M, SCHMITT M P, et al.Microstructural Effects and Properties of Non-Line-of-Sight Coating Processing via Plasma Spray-Physical Vapor Deposition[J]. Journal of Thermal Spray Technology, 2017, 26(6): 1052-1061.
[14] GAO L H, GUO H B, WEI L L, et al.Microstructure and Mechanical Properties of Yttria Stabilized Zirconia Coatings Prepared by Plasma Spray Physical Vapor Deposition[J]. Ceramics International, 2015, 41(7): 8305-8311.
[15] GAO L H, WEI L L, GUO H B, et al.Deposition Mechanisms of Yttria-Stabilized Zirconia Coatings during Plasma Spray Physical Vapor Deposition[J]. Ceramics International, 2016, 42(4): 5530-5536.
[16] 黄璐, 刘梅军, 杨冠军. 等离子-物理气相沉积(PS-PVD)的材料输运行为与沉积机理研究进展[J]. 中国表面工程, 2022, 35(1): 10-24.
HUANG L, LIU M J, YANG G J.Research Progress on Material Transportation Behavior and Deposition Mechanism of Plasma Spray-Physical Vapor Deposition (PS-PVD)[J]. China Surface Engineering, 2022, 35(1): 10-24.
[17] BOJDO N, FILIPPONE A, PARKES B, et al.Aircraft Engine Dust Ingestion Following Sand Storms[J]. Aerospace Science and Technology, 2020, 106: 106072.
[18] SATPATHY R, RANI S, ALAM Z, et al.Effectiveness of Lanthanum Zirconate and Yttria Stabilised Zirconia Freestanding APS Thermal Barrier Coatings Against Natural CMAS Attack at High Temperatures[J]. Materials at High Temperatures, 2020, 37(6): 416-424.
[19] SHINOZAKI M, ROBERTS K A, VAN DE GOOR B, et al. Deposition of Ingested Volcanic Ash on Surfaces in the Turbine of a Small Jet Engine[J]. Advanced Engineering Materials, 2013, 15(10): 986-994.
[20] LEVI C G, HUTCHINSON J W, VIDAL-SÉTIF M H, et al. Environmental Degradation of Thermal-Barrier Coatings by Molten Deposits[J]. MRS Bulletin, 2012, 37(10): 932-941.
[21] WELLMAN R G, NICHOLLS J R.Erosion, Corrosion and Erosion-Corrosion of EB PVD Thermal Barrier Coatings[J]. Tribology International, 2008, 41(7): 657-662.
[22] WITZ G, SHKLOVER V, STEURER W, et al.High-Temperature Interaction of Yttria Stabilized Zirconia Coatings with CaO-MgO-Al2O3-SiO2 (CMAS) Deposits[J]. Surface and Coatings Technology, 2015, 265: 244-249.
[23] ZHUO X S, SUN X M, WU J, et al.Molten CMAS Resistance Strategy for PS-PVD TBCS Based on Laser Textured and Al-Modified Bionic Structure[J]. NPJ Materials Degradation, 2024, 8: 85.
[24] ZHAO H X, ZENG Z J, ZHANG X F, et al.Towards Enhanced Corrosion Resistance of PS-PVD TBCS in Marine Environments by Structural Design[J]. Surface and Coatings Technology, 2024, 494: 131391.
[25] LIU Y, WANG J, ZHANG H, et al.Molten CMAS resistance of PS-PVD (Gd,Y)3Al5O12/YSZ Composite Thermal Barrier Coatings[J]. Surf Coat Technol, 2025, 498: 131205.
[26] LIU W, GANG Y, LUO J, et al.CMAS Corrosion Behavior of YSZ Thermal Barrier Coatings Prepared by PS-PVD[J]. Aeronaut Manuf Technol, 2023, 66(12): 45-51.
[27] SONG X, GUO Y Q, ZHU Q Y, et al.Basicity of Volcanic Ash Determining the Degradation of Thermal Barrier Coatings at Elevated Temperatures[J]. Journal of Materials Science & Technology, 2025, 232: 283-293.
[28] KWOK Q S M, JONES D E G, NUNEZ G F, et al. Characterization of Bio-Fuel and Bio-Fuel Ash[J]. Journal of Thermal Analysis and Calorimetry, 2004, 78(1): 173-184.
[29] MILLER S F, MILLER B G.The Occurrence of Inorganic Elements in Various Biofuels and Its Effect on Ash Chemistry and Behavior and Use in Combustion Products[J]. Fuel Processing Technology, 2007, 88(11/12): 1155-1164.
[30] RAMIREZ VELASCO J H, KILAZ G, KENTTÄMAA H I, et al. Application of Biofuel Impurities and Effect on the Hot Corrosion of Yttria-Stabilized Zirconia Thermal Barrier Coatings[J]. Surface and Coatings Technology, 2019, 358: 340-346.
[31] RAMIREZ VELASCO J H, PETROSKY K, KILAZ G, et al. Thermochemical Interaction of Biofuel Impurities with Yttria-Stabilized Zirconia Thermal Barrier Coatings[J]. Ceramics International, 2021, 47(17): 24675-24682.
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