Ni-based superalloy having high oxidation resistance and gas turbine part
AssigneeHitachi, Ltd.
InventorsHideki Tamaki, Akira Yoshinari, Akira Okayama, Tsuyoshi Takano, Hiroyuki Doi
Life of this patent
Estimating the term…
Loading patent…
AssigneeHitachi, Ltd.
InventorsHideki Tamaki, Akira Yoshinari, Akira Okayama, Tsuyoshi Takano, Hiroyuki Doi
Estimating the term…
A Ni-based alloy hardened with the γ phase, which is able to exhibit not only superior strength at high temperatures, but also excellent hot corrosion resistance and oxidation resistance at high temperatures in spite of containing no Re or reducing the amount of Re. The Ni-based superalloy contains, by weight, C: 0.01 to 0.5%, B: 0.01 to 0.04%, Hf: 0.1 to 2.5%, Co: 0.8 to 15%, Ta: more than 0% but less than 8.5%, Cr: 1.5 to 16%, Mo: more than 0% but less than 1.0%, W: 5 to 14%, Ti: 0.1 to 4.75%, Al: 2.5 to 7%, Nb: more than 0 % but less than 4%, V: 0 to less than 1.0%, Zr: 0 to less than 0.1%, Re: 0 to less than 9%, at least one of platinum group elements: 0 to less than 0.5% in total, at least one of rare earth elements: 0 to less than 0.1% in total, and the rest being Ni except for unavoidable impurities.
A Ni-based superalloy having high oxidation resistance, the superalloy being hardened by dispersing γ′ phases in a γ-phase matrix,
A Ni-based superalloy having high oxidation resistance, the superalloy being hardened by dispersing γ′ phases in a γ-phase matrix, wherein the superalloy contains, by weight, C:
Dependencies are inferred from the claim text.