Process and method to increase the hardness of Fe-Cr-C weld overlay alloy
View Patent ↗A method of preparing a mechanical component with an Fe—Cr—C hardfacing weld overlay alloy for improving the resistance of the mechanical component to abrasion, erosion or erosion/corrosion for use in very abrasive, erosion or erosive/corrosive environments by significantly increasing the hardness of the weld overlay is disclosed. To improve the resistance to abrasion, erosion or corrosion, a weld overlay of a Fe—Cr—C hardfacing alloy is applied onto the surface of a metallic component, such as tubes, pipes, or vessels. Welding and cladding methods including gas-metal-arc welding (GMAW), gas-tungsten-arc welding (GTAW), and laser cladding may be utilized. Then, the component is heat-treated at elevated temperatures for a sufficient time, resulting in additional hardening and thus further increasing the weld overlay's resistance to abrasion, erosion, or erosion/corrosion.
1. A method of improving the resistance of a mechanical component to abrasion, erosion or erosion/corrosion for use in very abrasive, erosion or erosive/corrosive environments, comprising:
(a) applying a weld overlay of a Fe—Cr—C hardfacing alloy onto the surface of a metallic component using welding and cladding methods; and
(b) heat-treating the weld overlay and component at a temperature between about 1400 to 2000 degrees Fahrenheit for about one hour, resulting in additional hardening of the weld overlay to a final hardness of between Rockwell C-50 to C-60 increasing the weld overlay's resistance to abrasion, erosion, or erosion/corrosion;
wherein the hardfacing alloy comprises 10-30% chromium; the cooling from the heat-treatment temperature is furnace cooled or air cooled at a rate slow enough to eliminate the forming of martensite or bainite phases during cooling; and the hardening resulting from the heat-treating is not a result of martensite or bainite formation during cooling from the heat-treating.
2. The method of claim 1 wherein the Fe—Cr—C hardfacing alloys are produced in castings.
3. The method of claim 1 wherein a HF35 hardfacing alloy wire is utilized for preparing the weld overlay, the HF35 hardfacing alloy wire comprises about 0.8-1.2% carbon, about 20-23% chromium, about 2.5-3.5% nickel, about 0.2-0.5% zirconium, about 0.5-1.0% molybdenum, about 1.0-2.0% manganese, about 1.0-2.0% silicon, and balance iron along with impurities and incidental elements.
4. The alloy of claim 1 wherein an initial hardness of the weld overlay in the as-overlaid condition is between Rockwell C-35 and C-40 and said final hardness of between Rockwell C-50 and C-60 is achieved after the heat-treatment.
5. The method of claim 1 wherein a hardfacing alloy wire is utilized for preparing the weld overlay, the hardfacing alloy wire is an alloy composition within the following chemical compositional ranges: about 0.5-2.0% carbon, about 10-30% chromium, about 1.0-8.0% nickel, about 0.2-0.5% zirconium, about 1.0-2.0% manganese, about 0.5-3.0% silicon, about 0.5-3.0% molybdenum, about 0.0-3.0% tungsten, about 0.0-0.5% boron, and balance iron along with impurities and incidental elements.
6. The method of claim 1 wherein the weld overlay is applied to pressure boundary components including tubes, pipes, and vessels.
7. The method of claim 1 wherein the weld overlay is applied using gas-metal-arc welding (GMAW), or gas-tungsten-arc welding (GTAW).
8. The method of claim 1 wherein the weld overlay is applied using arc welding methods selected from the group of submerged arc welding, electrostag welding and plasma transfer arc welding.
9. The method of claim 1 wherein the weld overlay is applied using laser cladding.