Surface hardenable stainless steels
Alloys, a process for preparing the alloys, and manufactured articles including the alloys are described herein. The alloys include, by weight, about 11.5% to about 14.5% chromium, about 0.01% to about 3.0% nickel, about 0.1% to about 1.0% copper, about 0.1% to about 0.2% carbon, about 0.01% to about 0.1% niobium, 0% to about 5% cobalt, 0% to about 3.0% molybdenum, and 0% to about 0.5% titanium, the balance essentially iron and incidental elements and impurities.
1. A method for preparing a martensitic, stainless steel case hardened alloy strengthened by copper nucleated nitride precipitates, said alloy comprising the following constituents in combination by weight percent, about 11.5 to about 14.5 Cr, about 0.1 to about 3.0 Ni, about 0.1 to about 1.0 Cu, about 0.1 to about 0.3 C, up to about 0.4 N, about 0.01 to about 0.1 Nb, 0 to about 5.0 Co, up to about 3 Mo, up to about 0.5 Ti, and the balance Fe and incidental elements and impurities, said alloy having a microstructure comprising a martensite matrix with nanoscale copper particles and alloy nitride precipitates selected from the group consisting of alloy nitride precipitates enriched with a transition metal nucleated on the copper precipitates, said alloy nitride precipitates having a hexagonal structure, said alloy nitride precipitates including one or more alloying elements selected from the group consisting of Fe, Ni, Cr, Co and Mo coherent with the matrix, said alloy nitride precipitates having two dimensional coherency with the matrix and said alloy substantially free of cementite carbide precipitates, said method comprising the steps of:
(a) preparing a melt of said aforesaid constituents substantially absent N;
(b) casting a form from said melt;
(c) optionally homogenizing the form;
(d) optionally working the form; and
(e) solution nitriding the form to effect the microstructure.
2. A martensite, stainless steel case hardened alloy strengthened by copper nucleated nitride precipitates selected from the group consisting of:
an alloy comprising about 12.4% chromium, about 1.4% nickel, about 0.3% copper, about 0.14% carbon, 0.29% N, about 0.05% niobium, about 2.8% cobalt, about 1.5% molybdenum, and about 0.006% titanium, and the balance iron and incidental elements and impurities;
an alloy comprising about 12.0% chromium, about 1.7% nickel, about 0.3% copper, about 0.2% carbon, about 0.33% N, about 0.04% niobium, about 1.5% molybdenum, and about 0.01% titanium, and the balance iron and incidental elements and impurities;
an alloy comprising about 12.9% chromium, about 1.3% nickel, about 0.4% copper, about 0.1% carbon, about 0.3% N, about 0.05% niobium, about 3.0% cobalt, about 1.3% molybdenum, and about 0.008% titanium, and the balance iron and incidental elements and impurities;
an alloy comprising about 13.9% chromium, about 1.2% nickel, about 0.3% copper, about 0.12% carbon, about 0.36% N, about 0.05% niobium, about 3.0% cobalt, about 0.9% molybdenum, and about 0.02% titanium, and the balance iron and incidental elements and impurities;
an alloy comprising about 14.1% chromium, about 0.4% nickel, about 0.3% copper, about 0.14% carbon, about 0.36% nitrogen, about 0.04% niobium, about 1.6% cobalt, about 0.02% molybdenum, and about 0.01% titanium;
each said alloy having a microstructure comprising a martensite matrix with nanoscale copper particles and alloy nitride precipitates enriched with a transition metal nucleated on the copper precipitates, said alloy nitride precipitates having a hexagonal structure, said alloy nitride precipitates including alloying elements selected from the group consisting of Cr, Co and Mo coherent with the matrix, said alloy nitride precipitates having two dimensional coherency with the matrix and said alloy substantially free of cementite carbide precipitates.
3. An alloy of claim 2 , wherein the alloy has a core δ-ferrite solvus temperature of at least 1180° C.
4. An alloy of claim 2 , wherein the alloy has a case martensite start temperature of about 140° C. to 300° C.