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Stainless steel alloys, turbocharger turbine housings formed from the stainless steel alloys, and methods for manufacturing the same

机译:不锈钢合金,由该不锈钢合金形成的涡轮增压器涡轮机壳体及其制造方法

摘要

Disclosed is an austenitic stainless steel alloy that includes, by weight, about 22% to about 28% chromium, about 3.5% to about 6.5% nickel, about 1% to about 6% manganese, about 0.5% to about 2.5% silicon, about 0.3% to about 0.6% carbon, about 0.2% to about 0.8% nitrogen, and a balance of iron. Molybdenum, niobium, and tungsten are excluded. The alloy is suitable for use in turbocharger turbine housing applications for temperature up to about 980° C.
机译:公开了一种奥氏体不锈钢合金,该合金包括按重量计约22%至约28%的铬,约3.5%至约6.5%的镍,约1%至约6%的锰,约0.5%至约2.5%的硅,约碳含量为0.3%至0.6%,氮含量为0.2%至0.8%,其余为铁。排除钼,铌和钨。该合金适用于温度高达980°C的涡轮增压器涡轮机壳体应用。

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