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Superalloy having a nickel base matrix, manufactured by powder-metallurgical processing, and gas turbine discs made from this alloy

机译:通过粉末冶金加工制造的具有镍基基体的高温合金,以及由该合金制成的燃气轮机盘

摘要

1. A superalloy comprising a nickel-based matrix and having good mechanical properties when hot, as regards tensile strength, creep strength, oligocyclic fatigue and resistance to cracking, characterised in that the percentage chemical composition by weight is within the following range : Cr 11 to 13 Co 8 to 17 Mo 6 to 8 Nb not more than 1.5 Ti 4 to 5 Al 4 to 5 Hf not more than 1 C, B, Zr none more than 500 ppm Ni remainder of 100.
机译:1.一种包括镍基基质并且在热时具有良好的机械性能的高温合金,所述高温合金具有抗拉强度,蠕变强度,低脂环疲劳性和抗龟裂性,其特征在于化学成分的重量百分比在以下范围内:Cr 11至13 Co 8至17 Mo 6至8 Nb不超过1.5 Ti 4至5 Al 4至5 Hf不超过1 C,B,Zr不超过500 ppm Ni剩余物100。

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