Corrosion and wear resistant iron based alloy useful for internal combustion engine valve seat inserts and method of making and use thereof
An iron-based corrosion resistant and wear resistant alloy includes (in weight percentage) carbon from about 1.6 to 3%, silicon from about 0.8 to 2.1%, manganese up to 1.0%, chromium from about 12.0 to 15.0%, molybdenum from about 2.0 to 4.0%, nickel from about 0.2 to 0.8%, copper up to 4.0%, boron up to 0.5%, and the balance including iron and incidental impurities. The alloy is suitable for use in elevated temperature applications such as in valve seat inserts for combustion engines.
1. An iron-based alloy having a copper precipitation strengthening mechanism comprising, in weight percentage:
carbon from about 1.6 to 3.0%;
silicon from about 0.8 to 2.1%;
manganese up to 1.0%;
chromium from about 12.0 to 15.0%;
molybdenum from about 2.0 to 4.0%;
nickel from about 0.2 to 0.8%;
copper from about 0.4 to 4.0%;
phosphorus from about 0.005 to about 0.015%;
boron from about 0.15 to 0.5%; and
balance iron and incidental impurities;
wherein the alloy has a microstructure comprising tempered martensite.
2. The alloy of claim 1 , further comprising:
sulfur from about 0.005 to 0.01%;
nitrogen up to about 0.5%; and
iron from about 74.0 to 81.0%.
3. The alloy of claim 1 , comprising, in weight percentage:
carbon from about 1.8 to 2.2%;
silicon from about 0.8 to 1.2%;
manganese from about 0.3 to 0.6%;
chromium from about 13.0 to 14.0%;
molybdenum from about 2.1 to 2.5%;
nickel from about 0.2 to 0.5%;
copper from about 0.4 to 2.0%;
boron from about 0.15 to 0.2%; and
balance iron and incidental impurities.
4. The alloy of claim 1 , wherein the alloy is vanadium-free, titanium-free, niobium free, tantalum-free, and/or tungsten-free.
5. The alloy of claim 1 , wherein the alloy is vanadium-free, titanium-free, niobium-free, tantalum-free, and tungsten-free.
6. The alloy of claim 1 , wherein the alloy is in a hardened and tempered condition having a hardness of at least about 45 to about 50 Rockwell C.
7. The alloy of claim 1 , wherein the alloy is in a hardened and tempered condition and exhibits a Vickers hot hardness at a temperature of 800° F. of at least about 415.
8. The alloy of claim 1 , wherein the alloy is in a hardened and tempered condition and exhibits a high temperature compressive yield strength at 800° F. of at least about 100 ksi.
9. A part for an internal combustion engine comprising the alloy of claim 1 .
10. A valve seat insert comprising the alloy of claim 1 .
11. A valve seat insert for use in an internal combustion engine, said valve seat insert made of an iron-based alloy comprising, in weight percent:
carbon from about 1.6 to 3.0%;
silicon from about 0.8 to 2.1%;
manganese up to 1.0%;
chromium from about 12.0 to 15.0%;
molybdenum from about 2.0 to 4.0%;
nickel from about 0.2 to 0.8%;
copper from about 0.4 to 4.0%;
phosphorus from about 0.005 to about 0.015%;
boron from about 0.15 to 0.5%, and
balance iron and incidental impurities;
wherein the alloy has a microstructure comprising tempered martensite.
12. A method of manufacturing the valve seat insert of claim 11 , comprising casting the iron-based alloy and machining a piece of the iron-based alloy.
13. A method of manufacturing the valve seat insert of claim 11 , comprising compacting powder of the iron-based alloy into a shaped piece and sintering the shaped piece of the iron-based alloy.
14. A method of manufacturing an internal combustion engine comprising inserting the valve seat insert of claim 11 in a cylinder head of the internal combustion engine.
15. A valve seat insert for a diesel engine comprising the alloy of claim 1 .
16. A valve seat insert for a diesel engine using EGR comprising the alloy of claim 1 .
17. A valve seat insert comprising the alloy of claim 1 , wherein the valve seat insert is in the form of a casting.
18. A valve seat insert comprising the alloy of claim 1 , wherein the valve seat insert is in the form of a pressed and sintered compact.
19. A method of manufacturing the valve seat insert of claim 11 , comprising machining a piece of the iron-based alloy.
20. A method of manufacturing an internal combustion engine comprising inserting the valve seat insert of claim 11 in a cylinder head of the internal combustion engine.
21. The method of claim 20 , wherein the engine is a diesel or natural gas engine.
22. A method of operating an internal combustion engine comprising closing a valve against the valve seat insert of claim 11 to close a cylinder of the internal combustion engine and igniting fuel in the cylinder to operate the internal combustion engine.