High rigid spheroidal graphite cast iron
US-9834831-B2 · Dec 5, 2017 · US
US9506421B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9506421-B2 |
| Application number | US-201214239240-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 17, 2012 |
| Priority date | Aug 17, 2011 |
| Publication date | Nov 29, 2016 |
| Grant date | Nov 29, 2016 |
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A cylinder liner for an internal combustion engine may include a cast iron alloy having a pearlitic structure with at least 70% of graphitization with spheroidal graphite morphology. The cast iron alloy may include at least 2.8% to 4.0% in weight of carbon; 1.8% to 3.5% in weight of silicon; 0.2% to 1.0% in weight of manganese; a maximum of 0.5% in weight of phosphorus; a maximum of 0.05% in weight of sulfur; a maximum of 0.5% in weight of vanadium; a maximum of 0.5% in weight of molybdenum; 0.2% to 1.5% in weight of nickel; a maximum of 0.3% in weight of tin; 0.005% to 0.06% in weight of magnesium.
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The invention claimed is: 1. A Cylinder liner for an internal combustion engine, comprising: a cast iron alloy having a pearlitic structure with at least 70% of graphitization with spheroidal graphite morphology, the cast iron alloy including: at least 2.8% to 4.0% in weight of carbon; 1.8% to 3.5% in weight of silicon; 0.2% to 1.0% in weight of manganese; a maximum of 0.5% in weight of phosphorus; a maximum of 0.05% in weight of sulfur; a maximum of 0.5% in weight of vanadium; a maximum of 0.5% in weight of molybdenum; 0.2% to 1.5% in weight of nickel; a maximum of 0.3% in weight of tin; 0.005% to 0.06% in weight of magnesium; at least one of the elements copper, cobalt, titanium, niobium, boron, aluminum, molybdenum, zirconium, nitrogen, antimony, arsenic and bismuth in a total of up to 7.0% of the total weight of the alloy, and iron as remainder; an inner diameter having an induction hardening thermal treatment and a hardness between 300 HV to 835 HV; and an elasticity modulus of at least 130 GPa; wherein the inner diameter includes up to 1.5 mm of a martensitic structure throughout an extent of the inner diameter. 2. The cylinder liner according to claim 1 , wherein the cast iron alloy includes up to 15% in weight of ferrite. 3. The cylinder liner according to claim 1 , wherein the cast iron alloy includes a tensile strength higher than 500 Megapascal (MPa). 4. The cylinder liner according to claim 1 , wherein the cast iron alloy includes a fatigue strength greater than 230 Megapascal (MPa). 5. The cylinder liner according to claim 1 , further comprising a reduced wall thickness. 6. The cylinder liner according to claim 5 , wherein the wall thickness is reduced between 3 and 35 percent as compared to a wall thickness of approximately 9.5 mm. 7. The cylinder liner according to claim 3 , wherein the cast iron alloy includes a fatigue strength greater than 230 Megapascal (MPa). 8. The cylinder liner accord to claim 1 , wherein the pearlitic structure includes at least 99% of spheroidal graphitization. 9. A cast iron alloy for a cylinder liner, comprising: a pearlitic structure with at least 70% of graphitization with spheroidal graphite morphology; at least 2.8% to 4.0% in weight of carbon; 1.8% to 3.5% in weight of silicon; 0.2% to 1.0% in weight of manganese; a maximum of 0.5% in weight of phosphorus; a maximum of 0.05% in weight of sulfur; a maximum of 0.5% in weight of vanadium; a maximum of 0.5% in weight of molybdenum; 0.2% to 1.5% in weight of nickel; a maximum of 0.3% in weight of tin; 0.005% to 0.06% in weight of magnesium; at least one of the elements copper, cobalt, titanium, niobium, boron, aluminum, molybdenum, zirconium, nitrogen, antimony, arsenic and bismuth in a total of up to 7.0% of total weight, and iron as the remainder; an inner diameter having an induction hardening thermal treatment and a hardness between 300 HV to 835 HV, wherein the inner diameter includes up to 1.5 mm of a martensitic structure throughout an extent of the inner diameter; and an elasticity modulus of at least 130 GPa. 10. The cast iron alloy according to claim 9 , further comprising up to 15% in weight of ferrite. 11. The cast iron alloy according to claim 9 , further comprising a tensile strength higher than 500 Megapascal (MPa). 12. The cast iron alloy according to claim 9 , further comprising a fatigue strength greater than 230 MPa. 13. The cast iron alloy according to claim 9 , further comprising a reduced wall thickness. 14. The cast iron alloy according to claim 13 , wherein the wall thickness is reduced between 3 and 35 percent as compared to a wall thickness of approximately 9.5 mm. 15. The cast iron alloy according to claim 9 , wherein the pearlitic structure includes at least 99% of spheroidal graphitization. 16. The cast iron alloy according to claim 11 , further comprising a fatigue strength greater than 230 MPa.
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