What is claimed is:
1. A nickel alloy for exhaust system components, wherein the nickel alloy is used for exhaust system components of a vehicle engine, the nickel alloy comprising:
0.01-0.2 wt % C;
0.1-1.0 wt % Si;
0.1-1.5 wt % Mn;
8-24 wt % Cr;
0.1-2.5 wt % Nb;
0.1-4.0 wt % Al;
0.01-1 wt % Co;
0.01-5.0 wt % Mo;
0.01-4 wt % W;
0.1-1 wt % Ta;
0.1-2.4 wt % Ti;
4.0-11.0 wt % Fe; and
a remainder comprising Ni and any impurities,
wherein the nickel alloy has an oxidation weight gain of 0.7 g/m 2 or less at a temperature higher than 20° C., and
wherein the nickel alloy has an abrasion amount of 2.0 mg or less at a temperature higher than 20° C.
2. The nickel alloy of claim 1 , wherein the nickel alloy contains a Ta—Ti based compound and a complex carbide of (Cr,Mo) 23 C 6 .
3. The nickel alloy of claim 2 , wherein the nickel alloy has a tensile strength of 950 MPa or more at a temperature higher than 20° C.
4. The nickel alloy of claim 3 , wherein the nickel alloy has a fatigue strength of 350 MPa or more at the temperature higher than 20° C.
5. The nickel alloy of claim 1 , wherein the nickel alloy has a tensile strength of 950 MPa or more at a temperature higher than 20° C.
6. The nickel alloy of claim 5 , wherein the nickel alloy has a fatigue strength of 350 MPa or more at the temperature higher than 20° C.
7. The nickel alloy of claim 1 , wherein the nickel alloy has a fatigue strength of 350 MPa or more at a temperature higher than 20° C.
8. The nickel alloy of claim 1 , wherein the nickel alloy has a tensile strength of 1050 MPa or more at 20° C., and has an elongation A5 of 13% or more at a temperature higher than 20° C.
9. The nickel alloy of claim 1 , wherein the nickel alloy has a tensile strength of 950 MPa or more at a temperature of 850° C.
10. The nickel alloy of claim 9 , wherein the nickel alloy has a fatigue strength of 350 MPa or more at the temperature of 850° C.
11. The nickel alloy of claim 1 , wherein the nickel alloy has a fatigue strength of 350 MPa or more at a temperature of 850° C.
12. The nickel alloy of claim 1 , wherein the temperature is 850° C.
13. A nickel alloy for exhaust system components, wherein the nickel alloy is used for exhaust system components of a vehicle engine, the nickel alloy consisting of:
0.01-0.2 wt % C;
0.1-1.0 wt % Si;
0.1-1.5 wt % Mn;
8-24 wt % Cr;
0.1-2.5 wt % Nb;
0.1-4.0 wt % Al;
0.01-1 wt % Co;
0.01-5.0 wt % Mo;
0.01-4 wt % W;
0.1-1 wt % Ta;
0.1-2.4 wt % Ti;
4.0-11.0 wt % Fe; and
a remainder consisting of Ni and any impurities,
wherein the nickel alloy has an oxidation weight gain of 0.7 g/m 2 or less at a temperature higher than 20° C., and
wherein the nickel alloy has an abrasion amount of 2.0 mg or less at a temperature higher than 20° C.