Cobalt-rich wear resistant alloy and method of making and use thereof
View Patent ↗A cobalt-rich wear resistant and corrosion resistant alloy comprises in weight %, 0.5 to 1.2% C, 0.6 to 2.1% Si, 17 to 24% Cr, 27 to 38.5% Fe, 1.4 to 20% W, 3.8 to 9.7% Mo, less than 1% Ni and balance Co. A preferred cobalt-rich alloy comprises in weight %, 0.5 to 0.9 C, 0.75 to 1.15% Si, 17.5 to 20.5 Cr, 27.0 to 32.0 Fe, 12.5 to 16.5 W, 6.25 to 8.25 Mo, 0.45 to 1.00 Ni and balance Co. The alloy preferably has a microstructure free of primary carbides and comprises up to about 50% by volume eutectic reaction phases in a solid solution matrix. The solid solution matrix is an αFe-αCo face-centered cubic solution with W, Cr and Mo as solute elements and the eutectic reaction products comprise a (Co,Cr) 7 (W,Mo) 6 phase and an αFe-αCo phase. The alloy is useful as a valve seat insert for internal combustion engines such as diesel engines.
1. A cobalt-rich wear resistant and corrosion resistant alloy consisting of in weight %:
0.5 to 1.2% C;
0.6 to 2.1% Si;
17 to 24% Cr;
27 to 38.5% Fe;
1.4 to 20% W;
3.8 to 9.7% Mo;
less than 1% Ni;
up to 1.5% each of Ti, Al, Zr, Hf, Ta, V, Nb or Cu; and/or up to 0.5% each of Mg, B or Y;
balance Co.
2. The alloy of claim 1 , wherein C is 0.5 to 0.9%, Si is 0.75 to 1.15%, Cr is 17.5 to 20.5%, Fe is 27.0 to 32.0%, W is 12.5 to 16.5% W, Mo is 6.25 to 8.25% and Ni is 0.45 to 1.00%.
3. The alloy of claim 1 , having a microstructure free of primary carbides and comprising up to 50% by volume eutectic reaction phases in a solid solution matrix.
4. The alloy of claim 3 , wherein the solid solution matrix is an αFe-αCo face-centered cubic solid solution with W, Cr and Mo as solute elements.
5. The alloy of claim 3 , wherein the eutectic reaction products comprise a (Co,Cr) 7 (W,Mo) 6 phase and an αFe-αCo phase.
6. A valve seat insert made of the alloy of claim 1 .
7. The valve seat insert of claim 6 , wherein C is 0.5 to 0.9%, Si is 0.75 to 1.15%, Cr is 17.5 to 20.5%, Fe is 27.0 to 32.0%, W is 12.5 to 16.5%, Mo is 6.25 to 8.25% and Ni is 0.45 to 1.00%, the Fe and Co being present in an Fe:Co ratio of 0.7 to 1.1.
8. The valve seat insert of claim 6 , wherein the insert is a casting and the microstructure includes 40 to 60% by volume eutectic reaction phases in a solid solution matrix.
9. The valve seat insert of claim 6 , wherein the insert has an as-cast hardness from about 47 to about 53 Rockwell C, a compressive yield strength from about 105 ksi to about 115 ksi at room temperature; and/or a compressive yield strength from about 70 ksi to about 90 ksi at 1000° F.
10. The valve seat insert of claim 6 , wherein the insert has an ultimate tensile rupture strength from about 85 ksi to about 95 ksi at room temperature; and/or an ultimate tensile rupture strength from about 75 ksi to about 85 ksi at about 1000° F.
11. The valve seat insert of claim 6 , wherein the insert exhibits a dimensional stability of less than about 0.25×10 −3 inches per inch of insert outside diameter (O.D.) after about 20 hours at about 1200° F.
12. The valve seat insert of claim 6 , wherein:
(a) the insert exhibits an HV10 Vickers hardness from about 465 HV10 at about room temperature to about 310 HV10 at about 1000° F.; or
(b) the insert exhibits a decrease in hardness of 40% or less when heated from about room temperature to about 1000° F.
13. A method of manufacturing an internal combustion engine comprising inserting the valve seat insert of claim 6 in a cylinder head of the internal combustion engine.
14. The method of claim 13 , wherein the engine is a diesel engine.
15. A method of operating an internal combustion engine comprising closing a valve against the valve seat insert of claim 6 to close a cylinder of the internal combustion engine and igniting fuel in the cylinder to operate the internal combustion engine.
16. The method of claim 15 , wherein the engine is a diesel engine.
17. The method of claim 15 , wherein the valve:
(i) is composed of a high-temperature, nickel-chromium alloy strengthened by precipitation hardening; or a high-temperature, nickel-based superalloy; or
(ii) the valve is hard-faced with a high temperature, wear-resistant cobalt-based alloy strengthened by carbides; or is hard-faced with a high-temperature, wear-resistant cobalt-based alloy strengthened by Laves phases.
18. A method of making a cobalt-rich wear resistant and corrosion resistant alloy comprising in weight %:
0.5 to 1.2% C;
0.6 to 2.1% Si;
17 to 24% Cr;
27 to 38.5% Fe;
1.4 to 20% W;
3.8 to 9.7% Mo;
less than 1% Ni;
balance Co;
wherein the alloy is:
(a) cast from a melt at a temperature of from about 2800° F. to about 3000° F.; or
(b) pressed into a shaped component and sintered at a temperature from about 2000° F. to about 2350° F.
19. The method of claim 18 , wherein the alloy is cast from a melt at a temperature from about 2875° F. to about 2915° F.; and further comprising heat treating the cast alloy at a temperature from about 1300° F. to about 1500° F. for about 2 to about 10 hours in an inert, oxidizing, reducing atmosphere or in a vacuum.