Low nickel austenitic stainless steel
View Patent ↗Various embodiments of the invention provide a low nickel austenitic stainless steel alloy composition including about 0.6% to about 0.8% by weight carbon; about 16% to about 18% by weight chromium; about 4.5% to about 5.5% by weight nickel; about 2.0% to about 5.0% by weight manganese; about 0.8% to about 1.2% by weight tungsten; about 0.8% to about 1.2% by weight molybdenum; about 0.65% to about 0.85% by weight niobium; about 0.3% to about 1.0% by weight silicon; balance iron and unavoidable impurities, wherein percentages are based on the overall weight of the composition. The invention further provides articles, such as turbine housings, prepared using the inventive alloys.
1. An alloy composition comprising:
about 0.6% to about 0.8% by weight carbon;
about 16% to about 18% by weight chromium;
about 4.5% to about 5.5% by weight nickel;
about 2.0% to about 5.0% by weight manganese;
about 0.8% to about 1.2% by weight tungsten;
about 0.8% to about 1.2% by weight molybdenum;
about 0.65% to about 0.85% by weight niobium;
about 0.3% to about 1.0% by weight silicon;
balance iron and unavoidable impurities, wherein percentages are based on the overall weight of the composition, and wherein the alloy comprises an austenitic structure having at least one of MC or M 7 C 3 carbides.
2. The alloy composition of claim 1 , further comprising one or more trace elements.
3. The alloy composition of claim 2 , wherein the one or more trace elements comprise one or more of the following:
up to about 0.15% by weight nitrogen;
up to about 0.005% by weight boron;
up to about 0.03% by weight phosphorus; and
up to about 0.03% by weight sulfur.
4. The alloy of claim 1 further comprising the austenitic structure having M 23 C 6 carbides formed during long-term thermal soaking.
5. A turbine housing or turbine manifold formed from an alloy comprising the alloy composition of claim 1 .
6. The turbine housing or turbine manifold of claim 5 , wherein the turbine housing or turbine manifold has an ultimate tensile strength of at least 465 MPa at room temperature when measured according to ASTM E8.
7. The turbine housing or turbine manifold of claim 5 , wherein the turbine housing or turbine manifold has a yield strength (proof stress) of at least 370 MPa at room temperature when measured according to ASTM E8.
8. The turbine housing or turbine manifold of claim 5 , wherein the turbine housing or turbine manifold exhibits a percent elongation of at least 2% at room temperature when measured according to ASTM E8.
9. The turbine housing or turbine manifold of claim 5 , wherein the turbine housing or turbine manifold has a hardness at room temperature between 170 and 260 BHN, wherein the hardness is measured in conformance with EN ISO 6506-1:2005.
10. An alloy composition comprising:
about 0.6% to about 0.75% by weight carbon;
about 16% to about 18% by weight chromium;
about 4.5% to about 5.5% by weight nickel;
about 2.0% to about 4.5% by weight manganese;
about 0.8% to about 1.2% by weight tungsten;
about 0.8% to about 1.2% by weight molybdenum;
about 0.65% to about 0.85% by weight niobium;
about 0.3% to about 1.0% by weight silicon;
balance iron and unavoidable impurities, wherein percentages are based on the overall weight of the composition, and wherein the alloy comprises an austenitic structure having at least one of MC or M 7 C 3 carbides.
11. The alloy composition of claim 10 , further comprising one or more trace elements.
12. The alloy composition of claim 11 , wherein the one or more trace elements comprise one or more of the following:
up to about 0.15% by weight nitrogen;
up to about 0.005% by weight boron;
up to about 0.03% by weight phosphorus; and
up to about 0.03% by weight sulfur.
13. The alloy of claim 10 further comprising the austenitic structure having M 23 C 6 carbides formed during long-term thermal soaking.
14. A turbine housing or turbine manifold formed from an alloy comprising the alloy composition of claim 10 .
15. The turbine housing or turbine manifold of claim 14 , wherein the turbine housing or turbine manifold has an ultimate tensile strength of at least 465 MPa at room temperature when measured according to ASTM E8.
16. The turbine housing or turbine manifold of claim 14 , wherein the turbine housing or turbine manifold has a yield strength (proof stress) of at least 370 MPa at room temperature when measured according to ASTM E8.
17. The turbine housing or turbine manifold of claim 14 , wherein the turbine housing or turbine manifold exhibits a percent elongation of at least 2% at room temperature when measured according to ASTM E8.
18. The turbine housing or turbine manifold of claim 14 , wherein the turbine housing or turbine manifold has a hardness at room temperature between 170 and 260 BHN, wherein the hardness is measured in conformance with EN ISO 6506-1:2005.