Austenitic ductile cast iron
View Patent ↗The invention provides an austenitic ductile cast iron alloy composition including about 2.2% to about 2.4% by weight carbon; about 3.5% to about 4.0% by weight silicon; about 28% to about 29% by weight nickel; about 2.5% to about 3.0% by weight chromium; about 0.9% to about 1.1% by weight molybdenum; and greater than about 50% iron, wherein percentages are based on the overall weight of the composition. The invention further provides articles, such as turbocharger housings, prepared using the inventive alloys.
1. An austenitic ductile cast iron alloy composition comprising:
about 2.2% to about 2.4% by weight carbon;
about 3.5% to about 6.0% by weight silicon;
about 28% to about 29% by weight nickel;
about 2.5% to about 3.0% by weight chromium;
about 0.9% to about 1.1% by weight molybdenum;
less than about 0.0001% by weight tin and antimony; and
greater than about 50% iron,
wherein percentages are based on the overall weight of the composition, and
wherein the cast iron has an austenitic structure having graphite that is essentially spheroidal, with a combined amount of Form I and II graphite according to ASTM A 247 at a level of about 70% or greater based on total graphite weight, and at least about 87% of the combined amount of Form I and II graphite comprises Form I, according to ASTM A 247 and based on total graphite weight.
2. The cast iron alloy composition of claim 1 , further comprising about 0.035% to about 0.090% by weight magnesium, based on the overall weight of the composition.
3. The alloy composition of claim 1 , further comprising one or more trace elements.
4. The alloy composition of claim 3 , wherein said one or more trace elements comprise one or more of the following:
up to about 0.10% manganese;
up to about 0.08% phosphorus; and
up to about 0.03% sulfur;
based on the overall weight of the composition.
5. The alloy composition of claim 3 , wherein said one or more trace elements is each present in an amount up to about 0.1% by weight, based on the overall weight of the composition.
6. The alloy composition of claim 3 , wherein said one or more trace elements are present in a total amount up to about 0.15% by weight, based on the overall weight of the composition.
7. A turbine housing or turbine manifold formed from an alloy composition according to claim 1 .
8. The turbine housing or turbine manifold of claim 7 , wherein said turbine housing or turbine manifold, has an ultimate tensile strength at of at least about 380 MPa at room temperature when measured according to ASTM E8.
9. The turbine housing or turbine manifold of claim 7 , wherein said turbine housing or turbine manifold has a 0.2% proof stress at room temperature of at least about 210 MPa when measured according to ASTM E8.
10. The turbine housing or turbine manifold of claim 7 , wherein said turbine housing or turbine manifold exhibits a percent elongation of at least about 10% at rupture at room temperature when measured according to ASTM E8.
11. The turbine housing or turbine manifold of claim 7 , wherein said turbine housing or turbine manifold has a hardness at room temperature of less than about 300 HBW 5/750, wherein the hardness is measured in conformance with EN ISO 6506-1.
12. An austenitic ductile cast iron alloy composition consisting of:
about 2.2% to about 2.4% by weight carbon;
about 3.5% to about 6.0% by weight silicon;
about 28% to about 29% by weight nickel;
about 2.5% to about 3.0% by weight chromium;
about 0.9% to about 1.1% by weight molybdenum;
about 0.035% to about 0.090% by weight magnesium;
less than about 0.0001% by weight tin and antimony; and
balance iron and unavoidable impurities,
wherein percentages are based on the overall weight of the composition.
13. The cast iron alloy composition of claim 12 , wherein the cast iron has an austenitic structure having graphite that is essentially spheroidal with a combined level of Form I and II according to ASTM A 247 at a level of about 70% or greater based on total graphite weight.
14. The cast iron alloy composition of claim 13 , wherein the Form I and II graphite comprises at least about 70% graphite with Form I according to ASTM A 247 and based on total graphite weight.
15. A turbine housing or turbine manifold formed from an alloy composition according to claim 12 .
16. The turbine housing or turbine manifold of claim 15 , wherein said turbine housing or turbine manifold has an ultimate tensile strength at room temperature of at least about 380 MPa when measured according to ASTM E8.
17. The turbine housing or turbine manifold of claim 15 , wherein turbine housing or turbine manifold has a 0.2% proof stress at room temperature of at least about 210 MPa when measured according to ASTM E8.
18. The turbine housing or turbine manifold of claim 15 , wherein said turbine housing or turbine manifold exhibits a percent elongation of at least 10% at failure at room temperature when measured according to ASTM E8.
19. The turbine housing or turbine manifold of claim 15 , wherein said turbine housing or turbine manifold has a hardness at room temperature of less than about 300 HBW 5/750, wherein the hardness is measured in conformance with EN ISO 6506-1.