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CAST NICKEL-IRON-BASE ALLOY COMPONENT AND PROCESS OF FORMING CAST NICKEL-IRON-BASE ALLOY COMPONENT

机译:铸镍铁基合金成分及成形镍铁基合金成分的过程

摘要

PROBLEM TO BE SOLVED: To secure oxidation resistance, thermomechanical fatigue resistance, creep strength at high temperature in a stator component that is a high-temperature gas flow channel component of a gas turbine.;SOLUTION: A cast nickel-iron-base alloy component includes, by weight, about 12.0% to about 16.5% Cr, about 1.0% to about 2.0% Al, about 2.0% to about 3.0% Ti, about 2.0% to about 3.0% W, about 3.0 to about 5.0% Mo, up to about 0.1% Nb, up to about 0.2% Mn, up to about 0.1% Si, about 0.05% to about 0.10% C, about 0.003 to about 0.010% B, about 35% to about 37% Fe, and balance essentially Ni and inevitable impurities. The nickel-iron-base alloy component has a creep rupture life greater than about 1,000 hours at about 25 ksi to about 30 ksi at about 1,400°F. A method for forming the cast nickel-iron-base alloy component is also disclosed.;COPYRIGHT: (C)2013,JPO&INPIT
机译:要解决的问题:为确保定子组件(在燃气轮机的高温气流通道组件中)的高温下的抗氧化性,抗热机械疲劳性,高温蠕变强度。解决方案:铸造的镍铁基合金组件包括按重量计约12.0%至约16.5%的Cr,约1.0%至约2.0%的Al,约2.0%至约3.0%的Ti,约2.0%至约3.0%的W,约3.0至约5.0%的Mo至约0.1%的Nb,至多约0.2%的Mn,至多约0.1%的Si,约0.05%至约0.10%的C,约0.003至约0.010%的B,约35%至约37%的Fe和基本平衡的Ni和不可避免的杂质。镍-铁基合金组分的蠕变断裂寿命在约25ksi至约1400°F下约30ksi时大于约1,000小时。还公开了一种铸造镍铁基合金零件的形成方法。;版权所有:(C)2013,日本特许厅&INPIT

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