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AUSTENITIC STAINLESS STEEL ALLOYS AND TURBOCHARGER COMPONENTS FORMED FROM THE STAINLESS STEEL ALLOYS

机译:由不锈钢合金形成的奥氏体不锈钢合金和涡轮增压器部件

摘要

Disclosed is an austenitic stainless steel alloy that includes or consists of, by weight, about 24.0% to about 26.0% chromium, about 13.0% to about 20.0% nickel, about 4.5% to about 5.5% manganese, about 1.2 to about 1.5% niobium, about 1.0% to about 2.0% silicon, about 0.4% to about 0.5% carbon, about 0.2% to about 0.3% nitrogen, and a balance of iron with inevitable / unavoidable impurities. The elements tungsten and molybdenum are excluded beyond impurity levels. Turbocharger turbine housings made of the stainless steel alloy are also disclosed. The stainless steel alloy is suitable for use in turbocharger turbine applications for temperatures beyond about 1050 °C, such as up to about 1070 °C.
机译:公开了一种奥氏体不锈钢合金,其包括或由重量,约24.0%至约26.0%铬,约13.0%至约20.0%镍,约4.5%至约5.5%锰,约1.2至约1.5%铌 ,约1.0%至约2.0%的硅,约0.4%至约0.5%碳,约0.2%至约0.3%的氮,以及具有不可避免的/不可避免的杂质的铁的平衡。 钨钨和钼的元素被排除在杂质水平之外。 还公开了由不锈钢合金制成的涡轮增压器涡轮壳体。 不锈钢合金适用于涡轮增压器涡轮机应用,用于超过约1050°C的温度,例如高达约1070℃。

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