Thermal insulation properties of YSZ coatings: Suspension Plasma Spraying (SPS) versus Electron Beam Physical Vapor Deposition (EB-PVD) and Atmospheric Plasma Spraying (APS)
Improving efficiency of hot section components of aero engines such as turbine blades or nozzle guide vanes is critical for the aircraft industry. Over many years, the development of advanced Thermal Barrier Coatings (TBCs) has been a field of active research to achieve this purpose. Electron Beam P...
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Published in | Surface & coatings technology Vol. 318; pp. 122 - 128 |
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Main Authors | , , , , , , |
Format | Journal Article |
Language | English |
Published |
Lausanne
Elsevier B.V
25.05.2017
Elsevier BV Elsevier |
Subjects | |
Online Access | Get full text |
ISSN | 0257-8972 1879-3347 |
DOI | 10.1016/j.surfcoat.2016.06.010 |
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Abstract | Improving efficiency of hot section components of aero engines such as turbine blades or nozzle guide vanes is critical for the aircraft industry. Over many years, the development of advanced Thermal Barrier Coatings (TBCs) has been a field of active research to achieve this purpose. Electron Beam Physical Vapor Deposition (EB-PVD) and Atmospheric Plasma Spraying (APS) processes are widely used to apply TBCs on metal substrates. High costs and rather high thermal conductivities of EB-PVD coatings, as well as low thermal lifetime of APS ones, are real drawbacks for next generations of turbine engines. In this study, Suspension Plasma Spraying (SPS) was assessed to improve TBC thermal properties. It was shown that the SPS process allows to perform columnar microstructure easily tunable in terms of both compaction of columnar structure and thermal conductivity. Thermal conductivities were in the 0.7–1.25W·m−1·K−1 range for SPS coatings while values of 0.9 and 1.5W·m−1·K−1 were measured for APS and EB-PVD coatings, respectively. The effect of heat conduction paths, which impact thermal diffusivity values, was highlighted for the columnar structure.
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•The influence of SPS columnar microstructures on thermal conductivity is studied•Controlling the column compaction allows to reduce heat conduction between them•Thermal conductivity of YSZ SPS coatings has been calculated by combination of flash method measurements and DSC analysis•Thermal diffusivity values seem strongly linked to heat conduction between columns |
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AbstractList | Improving efficiency of hot section components of aero engines such as turbine blades or nozzle guide vanes is critical for the aircraft industry. Over many years, the development of advanced Thermal Barrier Coatings (TBCs) has been a field of active research to achieve this purpose. Electron Beam Physical Vapor Deposition (EB-PVD) and Atmospheric Plasma Spraying (APS) processes are widely used to apply TBCs on metal substrates. High costs and rather high thermal conductivities of EB-PVD coatings, as well as low thermal lifetime of APS ones, are real drawbacks for next generations of turbine engines. In this study, Suspension Plasma Spraying (SPS) was assessed to improve TBC thermal properties. It was shown that the SPS process allows to perform columnar microstructure easily tunable in terms of both compaction of columnar structure and thermal conductivity. Thermal conductivities were in the 0.7–1.25W·m−1·K−1 range for SPS coatings while values of 0.9 and 1.5W·m−1·K−1 were measured for APS and EB-PVD coatings, respectively. The effect of heat conduction paths, which impact thermal diffusivity values, was highlighted for the columnar structure.
[Display omitted]
•The influence of SPS columnar microstructures on thermal conductivity is studied•Controlling the column compaction allows to reduce heat conduction between them•Thermal conductivity of YSZ SPS coatings has been calculated by combination of flash method measurements and DSC analysis•Thermal diffusivity values seem strongly linked to heat conduction between columns Improving efficiency of hot section components of aero engines such as turbine blades or nozzle guide vanes is critical for the aircraft industry. Over many years, the development of advanced Thermal Barrier Coatings (TBCs) has been a field of active research to achieve this purpose. Electron Beam Physical Vapor Deposition (EB-PVD) and Atmospheric Plasma Spraying (APS) processes are widely used to apply TBCs on metal substrates. High costs and rather high thermal conductivities of EB-PVD coatings, as well as low thermal lifetime of APS ones, are real drawbacks for next generations of turbine engines. In this study, Suspension Plasma Spraying (SN) was assessed to improve TBC thermal properties. It was shown that the SN process allows to perform columnar microstructure easily tunable in terms of both compaction of columnar structure and thermal conductivity. Thermal conductivities were in the 0.7-1.25W.m-1.K-1 range for SN coatings while values of 0.9 and 1.25W.m-1.K-1 were measured for APS and EB-PVD coatings, respectively. The effect of heat conduction paths, which impact thermal diffusivity values, was highlighted for the columnar structure. |
Author | Bernard, Benjamin Rémy, Benjamin Quet, Aurélie Malié, André Schick, Vincent Bianchi, Luc Joulia, Aurélien |
Author_xml | – sequence: 1 givenname: Benjamin surname: Bernard fullname: Bernard, Benjamin email: benjamin.bernard@cea.fr organization: CEA-DAM, Le Ripault, BP 16, 37260 Monts, France – sequence: 2 givenname: Aurélie surname: Quet fullname: Quet, Aurélie email: aurelie.quet@cea.fr organization: CEA-DAM, Le Ripault, BP 16, 37260 Monts, France – sequence: 3 givenname: Luc surname: Bianchi fullname: Bianchi, Luc email: luc.bianchi@cea.fr organization: Safran, Pôle Matériaux et Procédés, Rue de Jeunes Bois, Châteaufort, CS 80112, 78772, Magny-Les-Hameaux, France – sequence: 4 givenname: Aurélien surname: Joulia fullname: Joulia, Aurélien email: aurelien.joulia@safran.fr organization: Safran, Pôle Matériaux et Procédés, Rue de Jeunes Bois, Châteaufort, CS 80112, 78772, Magny-Les-Hameaux, France – sequence: 5 givenname: André surname: Malié fullname: Malié, André email: andre.malie@snecma.fr organization: Safran-Snecma, Rue Maryse Bastié, BP 129, 86101 Châtellerault, France – sequence: 6 givenname: Vincent surname: Schick fullname: Schick, Vincent email: vincent.schick@univ-lorraine.fr organization: LEMTA Université de Lorraine, 2 Avenue de la forêt de Haye, BP 160, 54504, Vandoeuvre-Lès-Nancy, France – sequence: 7 givenname: Benjamin surname: Rémy fullname: Rémy, Benjamin email: benjamin.remy@univ-lorraine.fr organization: LEMTA Université de Lorraine, 2 Avenue de la forêt de Haye, BP 160, 54504, Vandoeuvre-Lès-Nancy, France |
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Keywords | YSZ Thermal diffusivity Thermal conductivity Columnar microstructure Thermal Barrier Coating Suspension Plasma Spraying |
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SubjectTerms | Aircraft components Aircraft industry Airplane engines Coating effects Columnar microstructure Columnar structure Conduction heating Conductive heat transfer Conductivity Electron beams Electron-beam physical vapor deposition Engineering Sciences Guide vanes Heat transfer Mechanics Microstructure Physical vapor deposition Plasma spraying Studies Substrates Suspension Plasma Spraying Thermal Barrier Coating Thermal barrier coatings Thermal conductivity Thermal diffusivity Thermal insulation Thermics Turbine blades Turbine engines YSZ Yttria-stabilized zirconia |
Title | Thermal insulation properties of YSZ coatings: Suspension Plasma Spraying (SPS) versus Electron Beam Physical Vapor Deposition (EB-PVD) and Atmospheric Plasma Spraying (APS) |
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