Claims
- 1. The process of forming globular shaped carbides in cast iron comprising:
- adding 0.001 to 4.0% boron to alloy cast iron comprising 0.001% to 30% vanadium, titanium, niobium, molybdenum, nickel, copper, tantalum or chromium or mixtures thereof and 1.8% to 4.5% carbon to form a molten cast iron composition, cooling said molten alloy cast iron composition below equilibrium solidification temperature to a super cooled temperature, for solidifying said molten cast iron composition to produce globular shaped carbides having an average size less than the average conventional cast iron carbide particle, continuing solidifying said molten cast iron composition by continuing to cool said molten cast iron composition to super cooled temperature to form globular shaped carbides having said average size less than about 4 microns.
- 2. The process of forming globular shaped carbides in cast iron comprising:
- adding 0.001% to 4.0% boron to alloy cast iron comprising 0.001% to 30% vanadium, titanium, niobium, molybdenum, nickel, copper, tantalum or chromium or mixtures thereof and 1.8% to 4.5% carbon to form a molten cast iron composition, cooling said molten alloy cast iron composition below equilibrium solidification temperature to a super cooled temperature, for solidifying said molten cast iron composition to produce globular shaped carbides having an average size less than the average conventional cast iron carbide particle, said cooling of said molten cast iron composition being to a super cooled temperature of at least about 5.degree. F. below the equilibrium solidification temperature, and continuing said solidifying of said molten cast iron composition by continuing to cool said molten cast iron composition to super cooled temperature to form globular shaped carbides having said average size less than about 4 microns.
- 3. The process of super cooling molten cast iron to improve the toughness and abrasion resistance and tensile strength of cast iron comprising:
- increasing the entropy of a molten cast iron mixture of carbon, iron and vanadium, titanium, molybdenum, nickel, copper, tantalum or chromium or mixtures thereof, to form a molten cast iron composition, super cooling the molten cast iron composition to a temperature below the equilibrium solidification temperature of the molten cast iron composition, solidifying said molten cast iron composition while producing globular carbides having an average size less than the average size of the conventional cast iron carbide, continuing cooling said molten cast iron composition by continuing to cool said molten cast iron composition to super cooled temperature to form globular shaped carbides having said average size less than about 4 microns.
- 4. The process of super cooling molten cast iron to improve the toughness and abrasion resistance and tensile strength of cast iron comprising:
- increasing the entropy of a molten cast iron mixture of carbon, iron and vanadium, titanium, molybdenum, nickel, copper, tantalum or chromium or mixtures thereof, to form a molten cast iron composition, super cooling the molten cast iron composition to a temperature below the equilibrium solidification temperature of the molten cast iron composition, solidifying said molten cast iron composition while producing globular shaped carbides having an average size of the conventional cast iron carbide, said cooling of said molten cast iron composition being to a super cooled temperature of at least about 5.degree. F. below the equilibrium solidification temperature, and continuing said solidifying said molten cast iron composition by continuing to cool said molten cast iron composition to super cooled temperature to form globular shaped carbides having an average size of less than about 4 microns.
BACKGROUND OF THE INVENTION
This application is a continuation-in-part of application Ser. No. 600,552 filed 3/16/84, now abandoned.
US Referenced Citations (2)
Foreign Referenced Citations (8)
Number |
Date |
Country |
53-140218 |
Dec 1978 |
JPX |
54-41216 |
Apr 1979 |
JPX |
55-6440 |
Jan 1980 |
JPX |
1100200 |
Jan 1968 |
GBX |
1302321 |
Oct 1973 |
GBX |
639643 |
Dec 1978 |
SUX |
757604 |
Aug 1980 |
SUX |
850719 |
Jul 1981 |
SUX |
Continuation in Parts (1)
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Number |
Date |
Country |
Parent |
600552 |
Mar 1984 |
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