2021International Journal of Applied Ceramic TechnologyRequires access

The morphology, thermal property, and failure mechanism of GdNdZrO thermal barrier coatings by EB‐PVD

Zaoyu Shen, Zheng Liu, Guanxi Liu, Limin He, Rende Mu, Zhenhua Xu

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Abstract

Abstract Nowadays, the Gd 2 Zr 2 O 7 thermal barrier coatings (TBCs) have been evaluated as a promising alternative to yttria‐stabilized zirconia (YSZ). Thus, this investigation focuses on the thermal property, morphology, and failure mechanism of double ceramic layers (DCLs) GdNdZrO/YSZ advanced TBCs. The GdNdZrO coatings with columnar morphology have been deposited on NiCoCrAlYHf bond coating using an electron beam physical vapor deposition method. Material characterizations mainly include X‐ray diffraction, scanning electron microscope, and transmission electron microscopy. The thermal conductivity of GdNdZrO ceramic material is 0.494 W/mK at 1200°C. The thermal shock life of GdNdZrO/YSZ TBCs shows an average shock life of 5235 cycles. The TBC degradation occurs on the crack area within thermally grown oxide layer leading to the interface instability. The interface broken might play an important role in the failure mechanism of TBCs.

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What this paper is about

Abstract Nowadays, the Gd 2 Zr 2 O 7 thermal barrier coatings (TBCs) have been evaluated as a promising alternative to yttria‐stabilized zirconia (YSZ). Thus, this investigation focuses on the thermal property, morphology, and failure mechanism of double ceramic layers (DCLs) GdNdZrO/YSZ advanced TBCs. The GdNdZrO coatings with columnar morphology have been deposited on NiCoCrAlYHf bond coating using an electron beam physical vapor deposition method. Material characterizations mainly include X‐ray diffraction, scanning electron microscope, and transmission electron microscopy. The thermal conductivity of GdNdZrO ceramic material is 0.494 W/mK at 1200°C. The thermal shock life of GdNdZrO/YSZ TBCs shows an average shock life of 5235 cycles. The TBC degradation occurs on the crack area within thermally grown oxide layer leading to the interface instability. The interface broken might play an important role in the failure mechanism of TBCs.

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Available abstract

Abstract Nowadays, the Gd 2 Zr 2 O 7 thermal barrier coatings (TBCs) have been evaluated as a promising alternative to yttria‐stabilized zirconia (YSZ). Thus, this investigation focuses on the thermal property, morphology, and failure mechanism of double ceramic layers (DCLs) GdNdZrO/YSZ advanced TBCs. The GdNdZrO coatings with columnar morphology have been deposited on NiCoCrAlYHf bond coating using an electron beam physical vapor deposition method. Material characterizations mainly include X‐ray diffraction, scanning electron microscope, and transmission electron microscopy. The thermal conductivity of GdNdZrO ceramic material is 0.494 W/mK at 1200°C. The thermal shock life of GdNdZrO/YSZ TBCs shows an average shock life of 5235 cycles. The TBC degradation occurs on the crack area within thermally grown oxide layer leading to the interface instability. The interface broken might play an important role in the failure mechanism of TBCs.

Key concepts: Thermal barrier coating, Materials science, Yttria-stabilized zirconia, Thermal shock, Scanning electron microscope, Ceramic, Composite material, Cubic zirconia

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