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Ceramic-based abradable sealing coatings for advanced aeroengines: Materials design, structural strategies, and multifunctional performance
Leyao Wang, Shuqi Wang, Guoliang Chen, Yongchun Zou, Shuang Yu, Enyu Xie, Qingyuan Zhao, Zhiyun Ye, Jiahu Ouyang, Yaming Wang, Dechang Jia, Yu Zhou
Extreme Materials, 2025, 1(4): 33-58.   DOI: 10.1016/j.exm.2025.08.003

Material Service temperature ( C) CTE (×10-6 K-1) Thermal stability Key advantages Limitations
YSZ < 1200 ∼10.7 (matches superalloy) Good Mature system, tunable porosity, good oxidation resistance Upper temp limit ∼1200C, poor CMAS resistance
DySZ ~1200 Similar to YSZ Better than YSZ Improved phase stability, thermal shock resistance Higher hardness, more blade wear
YbSZ ~1200 Similar to YSZ Better than YSZ Good thermal stability Limited service temperature range
InFeO3(ZnO)m < 1400 ∼11.5 Stable up to 1400C Low hardness, good abradability Poor erosion resistance
LMA < 1600 - Excellent High fracture toughness, low thermal conductivity Uneven porosity, cracking under shock
YAG < 1600 - Excellent Good CMAS resistance, tunable porosity (SPPS) -
BSAS < 1300 4-6(matches CMCs) Good Good abradability, low silica activity Glass phase formation at high temperature
YbMS < 1500 7.5 Excellent Good thermal stability CTE mismatch, interface spallation
YbDS < 1400 4.5 Good Good CTE match, abradability Poor water vapor/oxygen corrosion resistance
Table 2 Comparison of key performance indicators of coating materials for ASCs.
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