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LZC/YSZ DCL TBCs by EB-PVD: Microstructure,low thermal conductivity and high thermal cycling life
Authors:Zaoyu Shen  Limin He  Zhenhua Xu  Rende Mu  Guanghong Huang
Affiliation:Key Laboratory of Advanced Corrosion and Protection for Aviation Materials, Beijing Institute of Aeronautical Materials, Aero Engine Corporation of China, Beijing 100095, PR China
Abstract:Thermal barrier coatings (TBCs) with low thermal conductivity have triggered tremendous attention due to their promising application in the gas turbine engines. Albeit recent studies have investigated double ceramic layers (DCL) with pyrochlore (A2B2O7) phase, it still remains a big challenge for controlling element content and investigating the relationship between the complex hierarchical architectures and their thermal performances. Here we describe a series of DCL La2O3-ZrO2-CeO2 (LZC)/Y2O3-stabilized ZrO2 (YSZ) coating under different current of electron beam by electron beam-physical vapor deposition (EB-PVD). The formation of hierarchical architecture with feathery microstructure and intra-columnar have been investigated in detail. The DCL coatings achieve a high thermal cycling life and relatively low thermal conductivity at controlling current of electron beam from 1.0 A to 1.3 A. This work may open new opportunities to rationally design other promising TBCs.
Keywords:Corresponding author    Thermal barrier coatings  Electron beam-physical vapor deposition  Feathery microstructure  Thermal conductivity  Thermal cycling lifetime
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