Claims
- 1. An iron-based alloy, comprising:
- 0.35% to 1.0% C;
- 0.0% to 1.0% Si;
- 0.0% to 1.6% Mn;
- 0.10% to 0.35% N;
- 0.0% to 1.0% Al;
- 0.0% to 2.8% Co;
- 14.0% to 25.0% Cr;
- 0.5% to 3.0% Mo;
- 0.0% to 3.0% Ni;
- 0.04% to 0.4% V;
- 0.0% to 3.0% W;
- 0.0% to 0.18% Nb; and
- 0.0% to 0.20% Ti;
- measured as a percentage of total weight of the alloy;
- wherein a total concentration of said C and said N is at least about 0.5% and no greater than about 1.2%; and
- the remainder of the alloy comprising iron and metallurgically required admixtures for the production of machine parts that in their function are exposed to severe stress from sliding superficial friction.
- 2. The iron-based alloy of claim 1, comprising:
- 0.4% to 0.8% C;
- 0.3% to 1.4% Mn;
- 0.12% to 0.29% N;
- 0.0% to 0.8% Al;
- 16. 0% to 19.0% Cr;
- 0.8% to 1.5% Mo;
- 0.0% to 1.5% Ni; and
- 0.05% to 0.2% V.
- 3. A process of using the iron-based alloy of claim 1, comprising:
- manufacturing at least one machine part from said iron-based alloy; and
- installing said at least one machine part to function under conditions of sliding friction.
- 4. The process of using of claim 3, further comprising:
- subjecting said at least one machine part to acidic conditions during functioning.
- 5. The process of using the iron-based alloy of claim 3, wherein said manufacturing at least one machine part comprises manufacturing at least one plunger piston.
- 6. The process of using the iron-based alloy of claim 4, wherein said manufacturing at least one machine part comprises manufacturing at least one plunger piston.
- 7. The process of using the iron-based alloy of claim 3, wherein said manufacturing at least one machine part comprises manufacturing at least one piston ring.
- 8. The process of using the iron-based alloy of claim 4, wherein said manufacturing at least one machine part comprises manufacturing at-least one piston ring.
- 9. A process of making a machine part for functioning under conditions of severe stress from sliding superficial friction, and in a corrosive environment, comprising:
- forming the machine part from an iron-based alloy, comprising:
- 0.35% to 1.0% C;
- 0.0% to 1.0% Si;
- 0.0% to 1.6% Mn;
- 0.10% to 0.35% N;
- 0.0% to 1.0% Al;
- 0.0% to 2.8% Co;
- 14. 0% to 25.0% Cr;
- 0.5% to 3.0% Mo;
- 0.0% to 3.0% Ni;
- 0.04% to 0.4% V;
- 0.0% to 3.0% W;
- 0.0% to 0.18% Nb; and
- 0.0% to 0.20% Ti;
- measured as a percentage of total weight of the alloy;
- tempering the machine part; and
- forming a hardened layer on at least a portion of a surface of the machine part.
- 10. The process of making a machine part according to claim 9, wherein said forming a hardened layer comprises forming a nitride layer on at least a portion of the machine part.
- 11. The process of making a machine part according to claim 9, wherein said forming a hardened layer comprises forming a carbonitride layer on at least a portion of the machine part.
- 12. The process of making a machine part according to claim 9, wherein said forming a hardened layer comprises vapor depositing an aluminum-based carbide layer on at least a portion of the machine part.
- 13. The process of making a machine part according to claim 9, wherein said forming a hardened layer comprises vapor depositing a titanium-based carbide layer on at least a portion of the machine part.
- 14. The process of making a machine part according to claim 9, wherein said forming a hardened layer comprises vapor depositing an aluminum-based nitride layer on at least a portion of the machine part.
- 15. The process of making a machine part according to claim 9, wherein said forming a hardened layer comprises vapor depositing a titanium-based nitride layer on at least a portion of the machine part.
- 16. The process of making a machine part according to claim 9, wherein said forming a hardened layer comprises vapor depositing an aluminum-based oxide layer on at least a portion of the machine part.
- 17. The process of making a machine part according to claim 9, wherein said forming a hardened layer comprises vapor depositing a titanium-based oxide layer on at least a portion of the machine part.
- 18. A machine part formed from an iron-based alloy, comprising:
- 0.35% to 1.0% C;
- 0.0% to 1.0% Si;
- 0.0% to 1.6% Mn;
- 0.10% to 0.35% N;
- 0.0% to 1.0% Al;
- 0.0% to 2.8% Co;
- 14. 0% to 25.0% Cr;
- 0.5% to 3.0% Mo;
- 0.0% to 3.0% Ni;
- 0.04% to 0.4% V;
- 0.0% to 3.0% W;
- 0.0% to 0.18% Nb; and
- 0.0% to 0.20% Ti;
- measured as a percentage of total weight of the alloy;
- wherein a total concentration of said C and said N is at least about 0.5% and no greater than about 1.2%; and
- the remainder of the alloy comprising iron and metallurgically required admixtures for the production of machine parts that in their function are exposed to severe stress from sliding superficial friction.
- 19. The machine part of claim 18, wherein said iron-based alloy comprises:
- 0.4% to 0.8% C;
- 0.3% to 1.4% Mn;
- 0.12% to 0.29% N;
- 0.0% to 0.8% Al;
- 16.0% to 19.0% Cr;
- 0.8% to 1.5% Mo;
- 0.0% to 1.5% Ni; and
- 0.05% to 0.2% V.
- 20. The machine part of claim 18, wherein said machine part comprises a plunger piston, said plunger piston further comprising:
- a hardened layer on at least a portion of an outer surface thereof, said hardened layer being formed from the group consisting of: an aluminum-based carbide layer formed by PVD; an aluminum-based nitride layer formed by PVD; an aluminum-based oxide layer formed by PVD; an aluminum-based carbide layer formed by CVD; an aluminum-based nitride layer formed by CVD; an aluminum-based oxide layer formed by CVD; a titanium-based carbide layer formed by PVD; a titanium-based nitride layer formed by PVD; a titanium-based oxide layer formed by PVD; a titanium-based carbide layer formed by CVD; a titanium-based nitride layer formed by CVD; and a titanium-based oxide layer formed by CVD.
- 21. The machine part of claim 18, wherein said machine part comprises a piston ring for use in internal combustion engines; said piston ring further comprising:
- a hardened layer on at least a portion of an outer surface thereof which is primarily subject to stress from friction, said hardened layer comprising a nitride layer having a thickness of at least 0.05 mm.
- 22. The piston ring of claim 21, wherein said hardened layer has a thickness of at least 0.2 mm.
Priority Claims (1)
Number |
Date |
Country |
Kind |
2051/94 |
Nov 1994 |
ATX |
|
CROSS-REFERENCE TO RELATED APPLICATION
This application claims the priority under 35 U.S.C. 119 of Austrian Application No. A 2051/94, filed on Nov. 4, 1994, the disclosure of which is incorporated herein by reference in its entirety.
US Referenced Citations (4)
Number |
Name |
Date |
Kind |
3990892 |
Machi et al. |
Nov 1976 |
|
4150978 |
Schlatter et al. |
Apr 1979 |
|
4880481 |
Jerlich et al. |
Nov 1989 |
|
4966751 |
Kaede et al. |
Oct 1990 |
|
Foreign Referenced Citations (3)
Number |
Date |
Country |
372983 |
Dec 1983 |
ATX |
392485 |
Apr 1991 |
ATX |
55-134159 |
Oct 1980 |
JPX |