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Ni-based forged alloy material and turbine high-temperature member using the same

机译:镍基锻造合金材料和使用其的涡轮高温部件

摘要

An object of the present invention is to provide a Ni-based forged alloy material in which a tensile strength and a creep property are balanced at a higher level than before using an ultra-strong precipitation-strengthened Ni-based alloy and a turbine high-temperature member using the same. . The Ni-based forged alloy material according to the present invention has a chemical composition in which a γ ′ phase of 50 volume% or more and 70 volume% or less is precipitated in a matrix phase of a γ phase at a temperature of 700 ° C., An aging precipitation γ 'phase grain that precipitates in the crystal grains of the γ phase and a eutectic reaction γ' phase grain that precipitates between the crystal grains of the γ phase. And the Al content is higher than that of the aging precipitation γ ′ phase grains, and the average grain size is 2 μm or more and 40 μm or less.
机译:本发明的目的是提供一种镍基锻造合金材料,其中与使用超强析出强化镍基合金和涡轮高强度涡轮机之前相比,其抗拉强度和蠕变性能在较高的水平上得到平衡。温度成员使用相同。 。根据本发明的Ni基锻造合金材料具有化学组成,其中在700℃的温度下在γ相的基体相中析出50体积%以上且70体积%以下的γ′相。 C.,在γ相的晶粒中析出的时效析出γ′相晶粒和在γ相的晶粒之间析出的共晶反应γ′相晶粒。并且,Al含量高于时效析出γ′相的晶粒,平均粒径为2μm以上且40μm以下。

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