Wear-resistant material
A wear-resistant material which comprises certain concentrations of carbon, nitrogen, oxygen, niobium/tantalum as well as other metallic elements. The material comprises a metal matrix and hard phases embedded therein. The hard phases comprise one or more of carbides, nitrides, carbonitrides, and oxide carbonitrides and have a diameter of from about 0.2 μm to about 50 μm. This abstract is neither intended to define the invention disclosed in this specification nor intended to limit the scope of the invention in any way.
1. A wear-resistant material, wherein the material comprises, in % by weight:
Carbon (C) from more than 0.3 to about 3.5
Nitrogen (N) from about 0.05 to about 4.0
Oxygen (O) from more than 0.002 to about 0.25
Niobium or tantalum or both niobium and tantalum (Nb/Ta) from about 3.0 to about 18.0
remainder metallic elements and impurities,
and wherein a microstructure of the material comprises a metal matrix and hard phases embedded therein, the hard phases comprising one or more of carbides, nitrides, and carbonitrides of at least Nb/Ta and having a diameter of from about 0.2 μm to about 50 μm.
2. The material of claim 1 , wherein the matrix comprises a martensitic microstructure.
3. The material of claim 1 , wherein the material comprises from more than 0.3 to not more than about 3.0% by weight of C.
4. The material of claim 1 , wherein the material comprises at least about 0.5% to about 3.5% by weight of C.
5. The material of claim 1 , wherein the material comprises at least about 0.15% to about 4.0% by weight of N.
6. The material of claim 1 , wherein the material comprises at least niobium.
7. The material of claim 6 , wherein the material comprises from about 3.0 to not more than a total of about 15.0% by weight of Nb/Ta.
8. The material of claim 1 , wherein the material comprises from about 0.2% to about 1.5% by weight of Si.
9. The material of claim 1 , wherein the material comprises from about 0.3% to about 2.0% by weight of Mn.
10. The material of claim 1 , wherein the material comprises from about 10.0% to about 20.0% by weight of Cr.
11. The material of claim 1 , wherein the material comprises from about 0.5% to about 3.0% by weight of Mo.
12. The material of claim 1 , wherein the material comprises from about 0.1% to about 1.0% by weight of V.
13. The material of claim 1 , wherein the material comprises from about 0.001% to about 1.0% by weight of titanium.
14. The material of claim 1 wherein the material comprises, in % by weight:
Carbon (C) from about 0.5 to about 2.5
Nitrogen (N) from about 0.15 to about 0.6
Silicon (Si) from about 0.2 to about 1.5
Manganese (Mn) from about 0.3 to about 2.0
Chromium (Cr) from about 10.0 to about 20.0
Nb/Ta from about 3.0 to about 15.0
Molybdenum (Mo) from about 0.5 to about 3.0
Vanadium (V) from about 0.1 to about 1.0
Titanium (Ti) from about 0.001 to about 1.0
remainder Iron (Fe) and production-caused impurities,
and wherein:
%C=0.3+%Nb+2×(%V+%Ti)/U
U having a value of from greater than 6 to lower than 10, and wherein the material has a high corrosion resistance.
15. The material of claim 1 wherein the material comprises, in % by weight:
Carbon (C) from more than 0.3 to about 1.0
Nitrogen (N) from about 1.0 to about 4.0
Silicon (Si) from about 0.2 to about 1.5
Manganese (Mn) from about 0.3 to about 1.5
Chromium (Cr) from about 10.0 to about 20.0
Nb/Ta from about 3.0 to about 15.0
Molybdenum (Mo) from about 0.5 to about 3.0
Vanadium (V) from about 0.1 to about 1.0
Titanium (Ti) from about 0.001 to about 1.0
remainder Iron (Fe) and production-caused impurities,
and wherein:
%N=0.3+%Nb+2×(%V+%Ti)/U1
U1 having a value of from greater than 4 to lower than 8, and wherein the material has a high corrosion resistance.
16. The material of claim 1 wherein the material comprises, in % by weight:
Carbon (C) from about 0.5 to about 3.0
Nitrogen (N) from about 0.15 to about 0.6
Silicon (Si) from about 0.2 to about 1.5
Manganese (Mn) from about 0.3 to about 2.0
Chromium (Cr) from about 10.0 to about 20.0
Nb/Ta from about 3.0 to about 15.0
Molybdenum (Mo) from about 0.5 to about 3.0
Vanadium (V) from about 0.1 to about 1.0
Titanium (Ti) from about 0.001 to about 1.0
remainder Iron (Fe) and production-caused impurities,
and wherein:
%C=0.3+%Nb+2×(%V+%Ti)/U2+Cr/U3
U2 having a value of from greater 6 to lower than 10, and
U3 having a value of from greater than 9 to lower than 17, and wherein the material has a high corrosion resistance.
17. The material of claim 1 with high temperature hardness and ductility, wherein the material comprises, in % by weight:
Carbon (C) from about 1.0 to about 3.5
Nitrogen (N) from about 0.05 to about 0.4
Silicon (Si) from about 0.2 to about 1.5
Manganese (Mn) from about 0.3 to about 1.0
Chromium (Cr) from about 2.5 to about 6.0
Nb/Ta from about 3.0 to about 18.0
Molybdenum (Mo) from about 2.0 to about 10.0
Tungsten (W) from about 0.1 to about 12.0
Vanadium (V) from about 0.1 to about 3.0
Cobalt (Co) from about 0.1 to about 12.0
Titanium (Ti) from about 0.001 to about 1.0
remainder Iron (Fe) and production-caused impurities,
and wherein:
%C=0.6+%Nb+2×(% V+%Ti)/U4+2×%Mo+%W/U5
U4 having a value of from about 6 to about 10, and
U5 having a value of from about 80 to about 100, and wherein the material has high temperature hardness and ductility.
18. A metal cutting tool which comprises the material of claim 17 .