The thermal shock resistance of ZrO
2 stabilized by oxides of rare earth element (La, Nd, Ce, Sm, Gd, Dy, Er, and Yb) has been investigated by subjecting disk-shaped specimens to a heat cycle of 1100°C/room temperature at a maximum cooling rate of about 500°C/min. Among these ZrO
2 ceramics, only ZrO
2-Yb
2O
3 system shows improved thermal shock resistance. Especially ZrO
2-8wt% Yb
2O
3 consisting of monoclinic and cubic phases exhibits thermal shock resistance superior to that of ZrO
2-7wt% Y
2O
3 commonly used in the thermal barrier coating for jet engine components. An increase in thermal shock resistance of ZrO
2-8wt% Yb
2O
3 is considered to have resulted from their smaller cubic phases compared with those of ZrO
2-7wt% Y
2O
3. Furthermore, the addition of 2wt% Al
2O
3 to the ZrO
2-8wt% Yb
2O
3 leads to a remarkable thermal shock resistance enhancement. The thermal shock resistance of ZrO
2 ceramics is associated with the volume change during the martensitic transformation of monoclinic→←tetragonal phase. The improved thermal shock resistance of ZrO
2-8wt% Yb
2O
3-2 wt% Al
2O
3 seems to be attributable to its morphology of small and isolated monoclinic grains in the matrix. On the other hand, ZrO
2-8wt% Yb
2O
3 with large agglomerated monoclinic grains is assumed to accelerate the initiation and propagation of cracks in the monoclinic grains during the martensitic transformation and consequently results in poor thermal shock resistance.
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