Austenitic stainless steel alloys, turbocharger components formed from the austenitic stainless steel alloys, and methods for manufacturing the same

Abstract

Disclosed is an austenitic stainless steel alloy that includes or consists of, by weight, about 24.0% to about 26.0% chromium, about 11.0% to about 13.0% nickel, about 1.0% to about 2.5% manganese, about 1.2% to about 1.6% niobium, about 1.0% to about 1.7% silicon, about 0.4% to about 0.5% carbon, about 0.2% to about 0.3% nitrogen, a balance of iron, and other inevitable/unavoidable impurities that are present in trace amounts. The elements zirconium and sulfur are excluded from the alloy beyond impurity levels. Turbocharger turbine housings made of the stainless steel alloy, and methods of making the same, are also disclosed. The stainless steel alloy is suitable for use in turbocharger turbine applications for temperatures up to and beyond about 1,050° C., such as up to about 1070° C.

1 . An austenitic stainless steel alloy, comprising, by weight:
 about 24.0% to about 26.0% chromium;   about 11.0% to about 13.0% nickel;   about 1.0% to about 2.5% manganese;   about 1.2% to about 1.6% niobium;   about 1.0% to about 1.7% silicon;   about 0.4% to about 0.5% carbon;   about 0.2% to about 0.3% nitrogen; and   a balance of iron, and other inevitable/unavoidable impurities that are present in trace amounts, wherein zirconium and sulfur are excluded from the alloy beyond impurity levels.   
     
     
         2 . The austenitic stainless steel alloy of  claim 1  comprising about 24.5% to about 25.5% chromium. 
     
     
         3 . The austenitic stainless steel alloy of  claim 1  comprising about 11.5% to about 12.5% nickel. 
     
     
         4 . The austenitic stainless steel alloy of  claim 1  comprising about 1.2% to about 2.0% manganese. 
     
     
         5 . The austenitic stainless steel alloy of  claim 1  comprising about 1.4% to about 1.6% silicon. 
     
     
         6 . The austenitic stainless steel alloy of  claim 1  comprising about 0.43% to about 0.47% carbon. 
     
     
         7 . The austenitic stainless steel alloy of  claim 1  comprising about 0.22% to about 0.28% nitrogen. 
     
     
         8 . The austenitic stainless steel alloy of  claim 1 , wherein if present, by weight, zirconium is about 0.02% or less and sulfur is about 0.04% or less. 
     
     
         9 . The austenitic stainless steel alloy of  claim 1 , consisting of, by weight:
 about 24.0% to about 26.0% chromium;   about 11.0% to about 13.0% nickel;   about 1.0% to about 2.5% manganese;   about 1.2% to about 1.6% niobium;   about 1.0% to about 1.7% silicon;   about 0.4% to about 0.5% carbon;   about 0.2% to about 0.3% nitrogen; and   a balance of iron, and other inevitable/unavoidable impurities that are present in trace amounts, wherein zirconium and sulfur are excluded from the alloy beyond impurity levels.   
     
     
         10 . A turbocharger turbine component comprising:
 an austenitic stainless steel alloy, wherein the austenitic stainless steel alloy comprises, by weight:   24.0% to 26.0% chromium;   11.0% to 13.0% nickel;   1.0% to 2.5% manganese;   1.2% to 1.6% niobium;   1.0% to 1.7% silicon;   0.4% to 0.5% carbon;   0.22% to 0.28% nitrogen; and   a balance of iron, and other inevitable/unavoidable impurities that are present in trace amounts that is defined for each impurity, if present, as in an amount of less than 0.1%, wherein zirconium, molybdenum, tungsten, and sulfur are excluded from the alloy beyond impurity levels.   
     
     
         11 . The turbocharger turbine component of  claim 10 , wherein the austenitic stainless steel alloy comprises 24.5% to 25.5% chromium. 
     
     
         12 . The turbocharger turbine component of  claim 10 , wherein the austenitic stainless steel alloy comprises 11.5% to 12.5% nickel. 
     
     
         13 . The turbocharger turbine component of  claim 10 , wherein the austenitic stainless steel alloy comprises 1.2% to 2.0% manganese. 
     
     
         14 . The turbocharger turbine component of  claim 10 , wherein the austenitic stainless steel alloy comprises 1.4% to 1.6% silicon. 
     
     
         15 . The turbocharger turbine component of  claim 10 , wherein the austenitic stainless steel alloy comprises 0.43% to 0.47% carbon. 
     
     
         16 . (canceled) 
     
     
         17 . The turbocharger turbine component of  claim 10 , wherein the austenitic stainless steel alloy consists of, by weight:
 24.0% to 26.0% chromium;   11.0% to 13.0% nickel;   1.0% to 2.5% manganese;   1.2% to 1.6% niobium;   1.0% to 1.7% silicon;   0.4% to 0.5% carbon;   0.22% to 0.3%0.28% nitrogen; and   a balance of iron, and other inevitable/unavoidable impurities that are present in trace amounts that is defined for each impurity, if present, as in an amount of less than 0.1%, wherein zirconium, molybdenum, tungsten, and sulfur are excluded from the alloy beyond impurity levels.   
     
     
         18 . The turbocharger turbine component of  claim 10 , wherein the turbocharger turbine component comprises a turbocharger turbine housing. 
     
     
         19 . A vehicle comprising the turbocharger turbine component of  claim 10 . 
     
     
         20 . A method of making a turbocharger turbine component comprising forming the turbocharger turbine component using an austenitic stainless steel alloy, wherein the austenitic stainless steel alloy comprises, by weight:
 24.0% to 26.0% chromium;   11.0% to 13.0% nickel;   1.0% to 2.5% manganese;   1.2% to 1.6% niobium;   1.0% to 1.7% silicon;   0.4% to 0.5% carbon;   0.22% to 0.28% nitrogen; and   a balance of iron, and other inevitable/unavoidable impurities that are present in trace amounts that is defined for each impurity, if present, as in an amount of less than 0.1%, wherein zirconium, molybdenum, tungsten, and sulfur are excluded from the alloy beyond impurity levels.