2012
DOI: 10.1016/j.msea.2012.07.095
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Effect of phase transformations on the fracture toughness of t′ yttria stabilized zirconia

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Cited by 89 publications
(42 citation statements)
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“…It was reported that when temperature exceeds 1200 1C [21], the phase transformation of YSZ from the non-transformable tetragonal (T´) phase to monoclinic (M) phase may occur and therefore deteriorate the durability of TBCs [24][25][26]. Hence, the phase compositions of YSZ before and after the thermal cycling test were investigated.…”
Section: Thermal Cyclic Lifetime Of Tbcsmentioning
confidence: 99%
“…It was reported that when temperature exceeds 1200 1C [21], the phase transformation of YSZ from the non-transformable tetragonal (T´) phase to monoclinic (M) phase may occur and therefore deteriorate the durability of TBCs [24][25][26]. Hence, the phase compositions of YSZ before and after the thermal cycling test were investigated.…”
Section: Thermal Cyclic Lifetime Of Tbcsmentioning
confidence: 99%
“…This is in agreement with the cubic phase evolution in stabilized zirconia e.g., 8YSZ EBPVD coating upon annealing, spark plasma sintered 8 mol.% YbO 1.5 stabilized ZrO 2 (8YbSZ) pellet upon isothermal annealing and 8YSZ pellet upon isothermal annealing. [9][10][11] The 12 h sample contains cubic phase with a volume fraction of 11.26% and two tetragonal phases. The precipitation of the cubic phase proceeds further and it reaches a volume fraction of 19.25% after 48 h.…”
Section: Annealing Time (H)mentioning
confidence: 99%
“…[1][2][3][4][5][6][7][8][9] It has recently been shown that the fracture toughness of t zirconia is linked to the phases present in the material. 10,11 The high initial indentation toughness decreases rapidly at the onset of partitioning of the t phase at a temperature like 1250 • C, and the toughness is recovered subsequently over prolonged thermal exposure of 192 h. Ferroelastic toughening is mainly responsible for the high indentation toughness of t zirconia. 10,11 The magnitude of fracture toughness enhancement is given by 12,13 Γ = 2f s hτ c γ (1) where f s is the volume fraction of the material in the process zone around the crack tip that experiences ferroelastic switching.…”
Section: Introductionmentioning
confidence: 99%
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“…During service of gas turbines, TBCs is subjected to high temperature exposure, sintering and corrosion, which can lead to a change in the microstructure for TBCs, such as, the formation and growth of thermally grown oxide (TGO) at interface, phase transformation, porosity decrease in coating [3][4][5] The TGO formation results in a large compressive stress, which leads to TGO undulation, crack formation, propagation, coalescence and eventually top ceramic coating spallation [6,7]. Phase transformation, such as, the metastable t' phase undergoes transformations, changing from t' YSZ into monoclinic (m) YSZ, which results in a volume expansion in TBCs [8]. The porosity decrease in a top ceramic coating reduces the strain tolerance, which is detrimental to the lifetime of thermal cycling [9].…”
Section: Introductionmentioning
confidence: 99%