首页> 外国专利> SINGLE CRYSTAL NICKEL-BASED SUPERALLOY HAVING A LOW SPECIFIC GRAVITY, AND BLADE OF A TURBO MACHINE MADE FROM THIS SUPERALLOY

SINGLE CRYSTAL NICKEL-BASED SUPERALLOY HAVING A LOW SPECIFIC GRAVITY, AND BLADE OF A TURBO MACHINE MADE FROM THIS SUPERALLOY

机译:具有低比重的单晶镍基超级合金,以及由这种超级合金制成的涡轮机刀片

摘要

A low density nickel based superalloy having good creep characteristics when hot, and intended in particular for making turbomachine parts by monocrystalline solidification, wherein the composition of the alloy in percentages by weight is as follows: -Co: 5% to 7% Cr: 5% to 10% Mo: 0.5% to 2.5% -W: 3% to 5% Al: 6% to 7.5% Ti: 1.5% to 2.25% -Nb: 0% to 0.5% Ta: 2% to 4% V: 0.3% to 0.6% -Ni: balance to- 100%. - Parts, e.g. turbomachine blades, made from the alloy.
机译:一种低密度的镍基高温合金,热态时具有良好的蠕变特性,尤其适用于通过单晶凝固制造涡轮机械零件,其中合金的重量百分比组成如下:-Co:5%至7%Cr:5 %到10%Mo:0.5%到2.5%-W:3%到5%Al:6%到7.5%Ti:1.5%到2.25%-Nb:0%到0.5%Ta:2%到4%V: 0.3%至0.6%-Ni:余量至-100%。 -零件,例如涡轮机叶片,由合金制成。

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