TY - JOUR
T1 - Microstructure and Thermal Cycling Behavior of Ta2O5 and Y2O3 Co-doped ZrO2 Coatings
AU - Chen, Dong
AU - Lu, Jing
AU - Sun, Chengchuan
AU - Wang, Quansheng
AU - Ning, Xianjin
N1 - Publisher Copyright:
© 2023, ASM International.
PY - 2023/6
Y1 - 2023/6
N2 - Ta2O5-Y2O3 co-doped ZrO2 (TYSZ) powders were prepared by high-temperature solid-phase synthesis, and a TYSZ coating was prepared by atmospheric plasma spraying (APS). The phase structures, coefficient of thermal expansion (CTE), and thermal conductivity of the TYSZ and YSZ coating were studied. Thermal cycling was performed at 1400 °C to evaluate the feasibility of TYSZ as an optimal ceramic material for next-generation gas-turbine thermal barrier coatings. The results indicate that the sintered agglomerated TYSZ powders are regular solid spheres with uniform particle size and good flow performance, which meet the requirements of the APS. The TYSZ coating had a typical layered structure, and the coating bond strength was 27.5 MPa. In contrast to the stable t phase of the powder, the TYSZ coating has a cubic phase due to oxygen defects caused by oxygen escaping during spraying. After high-temperature heat treatment (>1300 °C), the cubic phase of the TYSZ coating reverted to the t phase. Due to the specially designed substitution defects, the coefficient of thermal expansion of TYSZ is slightly lower than that of YSZ, and the thermal conductivity is much lower than that of the YSZ coating. After 84 cycles, spalling and cracking occurred in the TYSZ coating near the bond coat and ceramic interface. The mismatch in the coefficient of thermal expansion between the TYSZ coating and the substrate appears to be the primary reason for the coating failure.
AB - Ta2O5-Y2O3 co-doped ZrO2 (TYSZ) powders were prepared by high-temperature solid-phase synthesis, and a TYSZ coating was prepared by atmospheric plasma spraying (APS). The phase structures, coefficient of thermal expansion (CTE), and thermal conductivity of the TYSZ and YSZ coating were studied. Thermal cycling was performed at 1400 °C to evaluate the feasibility of TYSZ as an optimal ceramic material for next-generation gas-turbine thermal barrier coatings. The results indicate that the sintered agglomerated TYSZ powders are regular solid spheres with uniform particle size and good flow performance, which meet the requirements of the APS. The TYSZ coating had a typical layered structure, and the coating bond strength was 27.5 MPa. In contrast to the stable t phase of the powder, the TYSZ coating has a cubic phase due to oxygen defects caused by oxygen escaping during spraying. After high-temperature heat treatment (>1300 °C), the cubic phase of the TYSZ coating reverted to the t phase. Due to the specially designed substitution defects, the coefficient of thermal expansion of TYSZ is slightly lower than that of YSZ, and the thermal conductivity is much lower than that of the YSZ coating. After 84 cycles, spalling and cracking occurred in the TYSZ coating near the bond coat and ceramic interface. The mismatch in the coefficient of thermal expansion between the TYSZ coating and the substrate appears to be the primary reason for the coating failure.
KW - phase stability
KW - rare-earth oxide
KW - thermal barrier coating
KW - thermal cycling behavior
UR - http://www.scopus.com/inward/record.url?scp=85146754991&partnerID=8YFLogxK
U2 - 10.1007/s11666-022-01525-7
DO - 10.1007/s11666-022-01525-7
M3 - Article
AN - SCOPUS:85146754991
SN - 1059-9630
VL - 32
SP - 1327
EP - 1337
JO - Journal of Thermal Spray Technology
JF - Journal of Thermal Spray Technology
IS - 5
ER -