Ti, Ta, W を含むγ′析出強化型 Ni 基耐熱鋳造合金の合金設計(高温の組織と強度)(<特集>耐熱鋼・耐熱合金)

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The increase in the inlet gas temperature of a gas turbine is the most effective to raise the output efficiency of the turbine. For this purpose, blade materials having superior creep strength and hot corrosion resistance are required. In this study, γ′precipitation hardening nickel-base superalloys being superior in the above two properties have been developed by a computer-aided alloy design. The outline of the computeraided alloy design is as follows. At first, compositions of γ and γ′which are in a state of equilibrium each other, both highly solid solution hardened, and have a small lattice mismatch are selected. Compositions of alloys with optimum amount of γ′can be calculated by the application of the lever rule to the selected γ and γ′compositions and the addition of carbides and boride compositions. The evaluation of the alloy was made by creep rupture tests and a crucible test using a molten Na_2SO_4+25% NaCl salt mixture.
社団法人日本鉄鋼協会の論文
1979-06-01