Ni-based superalloy, and turbine rotor and stator blades for gas turbine using the same
View Patent ↗An object of the present invention is to provide a Ni-based superalloy, especially for a conventional casting, having a good balance among high temperature strength, corrosion resistance and oxidation resistance, as compared to a conventional material. The Ni-based superalloy comprises Cr, Co, Al, Ti, Ta, W, Mo, Nb, C, B, and inevitable impurities, the balance being Ni, the Ni-based superalloy having a superalloy composition comprising, by mass, 13.1 to 16.0% Cr, 11.1 to 20.0% Co, 2.30 to 3.30% Al, 4.55 to 6.00% Ti, 2.50 to 3.50% Ta, 4.00 to 5.50% W, 0.10 to 1.20% Mo, 0.10 to 0.90% Nb, 0.05 to 0.20% C, and 0.005 to 0.02% B.
1. A Ni-based superalloy comprising Cr, Co, Al, Ti, Ta, W, Mo, Nb, Hf, C, B, Re, Zr, O, N, and inevitable impurities, the balance being Ni, the Ni-based superalloy having a superalloy composition comprising, by mass, 13.1 to 16.0% Cr, 13.1 to 18.0% Co, 2.30 to 3.30% Al, 4.55 to 6.00% Ti, 2.50 to 3.50% Ta, 4.00 to 4.90% W, 0.10 to 1.20% Mo, 0.10 to 0.90% Nb, 0.01 to 0.04% Hf, 0.05 to 0.20% C, 0.005 to 0.02% B, 0.003 to 0.50% Re, 0.01 to 0.05% Zr, 0.001 to 0.005% O and 0.001 to 0.005% N.
2. The Ni-based superalloy according to claim 1 , wherein the Ni-based superalloy has a superalloy composition comprising, by mass, 0.003 to 0.10% Re, and 0.01 to 0.03% Zr.
3. The Ni-based superalloy according to claim 2 , wherein the Ni-based superalloy has a superalloy composition comprising, by mass, 13.1 to 14.3% Cr, 2.60 to 3.30% Al, 4.65 to 5.50% Ti, 2.70 to 3.30% Ta, 4.55 to 4.90% W, 0.10 to 1.10% Mo, 0.10 to 0.65% Nb, 0.10 to 0.18% C, and 0.015 to 0.02% B.
4. The Ni-based superalloy according to claim 3 , wherein the Ni-based superalloy has a superalloy composition comprising, by mass, 13.7 to 14.1% Cr, 14.1 to 17.0% Co, 3.00 to 3.20% Al, 4.70 to 5.10% Ti, 2.90 to 3.20% Ta, 4.55 to 4.85% W, 0.70 to 1.00% Mo, 0.25 to 0.45% Nb, and 0.12 to 0.17% C.
5. A cast product comprising a Ni-based superalloy according to claim 1 .
6. A turbine rotor blade for a gas turbine comprising a Ni-based superalloy according to claim 1 .
7. A turbine stator blade for a gas turbine comprising a Ni-based superalloy according to claim 1 .