Controlled thermal expansion of welds to enhance toughness
View Patent ↗A method is provided for forming a metallic overlay having enhanced toughness. The metallic overlay may be a weld, a metallic coating, or similar application. The method includes applying a glass forming metallic alloy to a substrate while the alloy is in a molten or semi-molten state. At the interface of the metallic alloy overlay and the substrate the substrate metal becomes at least partially molten and combines with the alloy to form metallurgical bonds. When the metallic alloy cools it experiences a high relative degree of thermal contraction. The metallurgical bonds between the substrate and the alloy constrain the contraction of the alloy at the interface with the substrate. This results in the inducement of compressive stresses in the metallic alloy overlay. The induced compressive stresses inhibit the formation of cracks in the overlay and/or mitigation of the effects of any cracks in the overlay.
1. A method for forming a metallic overlay comprising:
supplying a metal substrate with a thermal expansion coefficient “X”;
supplying a metallic alloy which has a thermal expansion coefficient “Y”, wherein said metallic alloy has a coefficient of thermal expansion “Y” greater than 15% of that of said substrate “X” and wherein Fe and Cr comprises at least 90 wt % of said metallic alloy, and C is present at levels of about 1.0 wt %, and Mo is present at levels of about 1.0–2.0 wt %;
melting said metallic alloy and applying said metallic alloy to said metal substrate to form an alloy/substrate interface;
forming metallurgical bonds between said metallic alloy and said substrate at said alloy/substrate interface; and
causing said alloy to shrink while said alloy is constrained at said alloy/substrate interface thereby developing a residual compressive stress in said metallic alloy, wherein said metallic alloy has a hardness of greater than 750 kg/mm 2 .
2. The method of claim 1 wherein said alloy is comprised of a mixture of Fe, Cr, Mo, W, B, C, Si and Mn.
3. The method of claim 2 , wherein Fe is present at levels above 50.0 wt %.
4. The method of claim 2 , wherein Fe, Cr, Mo, and W comprise at least 90 wt % of said mixture.
5. The method of claim 1 wherein Fe and Cr comprise at least 90 wt. % of said metallic alloy, and Mo is present at levels of about 1.0–2.0 wt. %, and B is present at levels of about 3.0–4.0 wt %, W is present at levels of about 1.0–2.0 wt %, C is present at levels of about 0.1–1.2 wt % Si is present at levels of 0.1–1.0 wt % and Mn is present at levels of 0.1–1.0 wt %.
6. The method according to claim 2 wherein said metallic alloy has a composition of about 65.9 wt % Fe, 25.3 wt % Cr, 1.0 wt % Mo, 1.8 wt % W, 3.5 wt % B, 1.2 wt % C, 0.5 wt % Si, 0.8 wt % Mn.
7. The method according to claim 2 wherein said metallic alloy has a composition of 64.9 wt % Fe, 26.0 wt % Cr, 1.0 wt % Mo, 1.4 wt % W, 3.6 wt % B, 1.2 wt % C, 1.0 wt % Si, 0.8 wt % Mn.
8. The method according to claim 1 wherein said metallic alloy has a composition of 68.0 wt % Fe, 23.2 wt % Cr, 1.2 wt % Mo, 1.5 wt % W, 3.6 wt % B, 0.9 wt % C, 0.7 wt % Si, 0.8 wt % Mn.
9. The method according to claim 1 wherein applying said metallic alloy comprises welding.
10. The method according to claim 1 wherein applying said metallic alloy comprises thermal spray coating.
11. The method according to claim 1 wherein said metallic alloy has a coefficient of thermal expansion in the range of 12 to 17 ppm/° C.
12. A method for forming a metallic overlay comprising:
supplying a metal substrate with a thermal expansion coefficient “X”;
supplying a metallic alloy which has a thermal expansion coefficient “Y”, wherein said metallic alloy has a coefficient of thermal expansion “Y” greater than 15% of that of said substrate “X” and wherein said metallic alloy has a yield strength “Z” and wherein Fe and Cr comprises at least 90 wt % of said metallic alloy, and C is present at levels of about 1.0 wt %, and Mo is present at levels of about 1.0–2.0 wt %;
melting said metallic alloy and applying said metallic alloy to said metal substrate to form an alloy/substrate interface;
forming metallurgical bonds between said metallic alloy and said substrate at said alloy/substrate interface; and
causing said alloy to shrink while said alloy is constrained at said alloy/substrate interface thereby developing a residual compressive stress in said metallic alloy, wherein said compressive stress does not exceed the yield strength “Z” and wherein said metallic alloy has a hardness of greater than about 850 kg/mm 2 .
13. The method of claim 12 wherein said compressive yield strength is greater than about 1520 MPa at room temperature.