Cerium oxide stabilized zirconia（ZrO₂-CeO）
| powder | brand | Main components（%） | Coating Function and Application | Particle size distribution（μm） | Product images |
|---|---|---|---|---|---|
Yttrium oxide stabilized zirconia （ZrO₂-Y₂O₃） | TCR-832 | Y₂O₃:8.00 ZrO₂:92.00 | Melting point: 2480 ℃ Characteristics: high temperature resistance, heat shock resistance, and high temperature gas cavitation resistance. Application: Thermal barrier coatings for jet engine combustion chambers and gas turbine blades; High temperature gas particle erosion resistant coating for rocket nozzles and missile nose cones, and high-temperature protective coating for heat-treated annealing furnace rollers. | 45~90 15~45 10~30 |  |
Yttrium oxide stabilized zirconia （ZrO₂-Y₂O₃） | TCR-832A | Y₂O₃:8.00 ZrO₂:92.00 | |||
Yttrium oxide stabilized zirconia （ZrO₂-Y₂O₃） | TCR-835 | Y₂O₃:20.00 ZrO₂:80.00 | |||
Yttrium oxide stabilized zirconia （ZrO₂-Y₂O₃） | TCR-836 | Y₂O₃:13.00 ZrO₂:87.00 | |||
Yttrium oxide stabilized zirconia （ZrO₂-Y₂O₃） | TCR-837 | Y₂O₃:65.00 ZrO₂:35.00 | |||
MSZ （ZrO₂-MgO） | TCR-871 | MgO:22.00 ZrO₂:78.00 | Melting point: 2820 ℃ Characteristics: Moderate hardness, high temperature resistivity, high dielectric constant, resistance to molten metal erosion and alkaline slag erosion. Application: High temperature thermal barrier coatings for missile nose cones, gas turbine blades, aviation engine combustion chambers, internal combustion engine combustion chambers, annealing furnace rollers, muffle tanks, and other applications. | 45~90 15~45 10~30 | |
Cerium oxide stabilized zirconia （ZrO₂-CeO） | TCR-875 | CeO:22.00 ZrO₂:78.00 | Melting point: 2400 ℃ Characteristics: Low thermal conductivity, strong resistance to high temperature oxidation. Application: High temperature resistant thermal barrier ceramic coating for aircraft engines, heat-resistant combustion catalytic coating for internal combustion engines. | 45~90 15~45 10~30 | |
Calcium oxide stabilized zirconia （ZrO₂-CaO） | TCR-878 | CaO:4.00 ZrO₂:96.00 | Melting point: 2535-2550 ℃ Characteristics: Moderate hardness, good toughness, high temperature resistance, insulation, and thermal shock resistance. Application: High temperature gas erosion resistance and thermal barrier coating for rocket flame nozzles, rocket engine combustion chambers, internal combustion engine combustion chambers, and gas turbine heat flow components. | 45~75 15~45 10~30 | |
