Hardfacing alloy, methods and products
Disclosed is a hardfacing alloy capable of withstanding service abrasion of the order of silicious earth particles and weldable on industrial products, such as tool joints and stabilizers used in oil and gas well drilling, and other industrial products. The hardfacing alloy has a low coefficient of friction resulting from excellent metal to metal resistance and significant reduction in industrial wear on industrial products, such as casing wear. Other embodiments of the invention include tool joints having the hardbanding alloy welded to the outer cylindrical surface to its box and pin members and to stabilizer ribs on the stabilizer used in earth boring, such as boring for oil and gas, other industrial products, and methods of applying the hardfacing alloy to their surfaces. The hardfacing alloy does not require any post weld treatment, has primary borides in its microstructure, the carbons in the alloy are tied up in the formation of secondary carbides which add to the abrasion resistance, and have a quadratic crystallographic structure and a hardness of about 1725 Hv comparable to the prior art hardness of the chromium carbide primary carbide alloys of the prior art but is substantially less brittle than C—Cr—Fe hardfacing alloys.
1. An Iron based hardfacing alloy for welding to a surface to be abrasion resistant, said Iron based hardfacing alloy as welded comprising by weight:
about 0.45 to about 0.8 percent Carbon, about 3.5 to about 4.5 percent Boron,
about 4.5 to about 6.5 percent Niobium, about 2.0 to about 2.5 percent Nickel, and
about 0.8 to about 1.25 percent Manganese, and
said hardfacing alloy having a quadratic crystallographic boride and eutectic structure.
2. The Iron based hardfacing alloy of claim 1 , further comprising the balance by weight Silicon and Iron, including impurities as trace elements.
3. The Iron based hardfacing alloy of claim 2 , further comprising by weight at most about 0.8 percent Silicon.
4. The Iron based hardfacing alloy of claim 3 , wherein said Iron based hardfacing alloy having a hardness of at most about 66 Rc (865 Hv).
5. The Iron based hardfacing alloy of claim 1 , wherein said Iron based hardfacing alloy having a hardness of at most about 66 Rc (865 Hv).
6. The Iron based hardfacing alloy of claim 2 , wherein said Iron based hardfacing alloy having a hardness of at most about 66 Rc (865 Hv).
7. An industrial product having a surface subject to abrasion, comprising:
a layer of an Iron based hardfacing alloy comprising by weight about 0.45 to about 0.8 percent Carbon, about 3.5 to about 4.5 percent Boron, about 4.5 to about 6.5 percent Niobium, about 2.0 to about 2.5 percent Nickel, and about 0.8 to about 1.25 percent Manganese,
said Iron based hardfacing alloy having a quadratic crystallographic boride and eutectic structure, and
said Iron based hardfacing alloy welded to the surface of the industrial product subject to said abrasion.
8. The product of claim 7 , wherein said Iron based hardfacing alloy further comprising the balance by weight Silicon and Iron, including impurities as trace elements.
9. The product of claim 8 , wherein said Iron based hardfacing alloy further comprising at most about 0.8 percent Silicon.
10. The product of claim 9 , wherein said Iron based hardfacing alloy further having a hardness of at most about 66 Rc (865 Hv).
11. The product of claim 8 , wherein said Iron based hardfacing alloy further having a hardness of at most about 66 Rc (865 Hv).
12. The product of claim 7 , wherein said Iron based hardfacing alloy further having a hardness of at most about 66 Rc (865 Hv).
13. The product of claim 7 comprising,
a stabilizer having a cylindrical body and an internally threaded box and an externally threaded pin for connection in a string of drill pipe,
stabilizer ribs having outer surfaces subject to said abrasion extending from an outer surface of said cylindrical body effective to stabilize said string of drill pipe in a well bore,
a layer of said Iron based hardfacing alloy, and
said Iron based hardfacing alloy welded to said outer surfaces of said stabilizer ribs subject to said abrasion.
14. The product of claim 13 , wherein said Iron based hardfacing alloy further comprising the balance by weight Silicon and Iron, including impurities as trace elements.
15. The product of claim 14 , wherein said Iron based hardfacing alloy further comprising at most about 0.8 percent Silicon.
16. The product of claim 15 , wherein said Iron based hardfacing alloy further having a hardness of at most about 66 Rc (865 Hv).
17. The product of claim 14 , wherein said Iron based hardfacing alloy further having a hardness of at most about 66 Rc (865 Hv).
18. The product of claim 13 , wherein said Iron based hardfacing alloy further having a hardness of at most about 66 Rc (865 Hv).
19. A tool joint for connecting drill pipe having a diameter, said tool joint having a cylindrical body, an internally threaded box which has an outer cylindrical surface of a diameter greater than the drill pipe diameter, and an externally threaded pin, comprising:
at least one layer of an Iron based hardfacing alloy comprising by weight about 0.45 to about 0.8 percent Carbon, about 3.5 to about 4.5 percent Boron,
about 4.5 to about 6.5 percent Niobium, about 2.0 to about 2.5 percent Nickel, and
about 0.8 to about 1.25 percent Manganese,
said Iron based hardfacing alloy having a quadratic crystallographic boride and eutectic structure,
said Iron based hardfacing alloy welded to said outer cylindrical surface of said box, and
said Iron based hardfacing alloy thereby providing surface resistance to abrasion.
20. The tool joint of claim 19 , wherein said Iron based hardfacing alloy further comprising the balance by weight Silicon and Iron, including impurities as trace elements.
21. The tool joint of claim 20 , wherein said Iron based hardfacing alloy further comprising at most about 0.8 percent Silicon.
22. The tool joint of claim 21 , wherein said Iron based hardfacing alloy further having a hardness of at most about 66 Rc (865 Hv).
23. The tool joint of claim 20 , wherein said Iron based hardfacing alloy further having a hardness of at most about 66 Rc (865 Hv).
24. The tool joint of claim 19 , wherein said Iron based hardfacing alloy further having a hardness of at most about 66 Rc (865 Hv).
25. The tool joint of claim 19 wherein:
the outer cylindrical surface of said box has a reduced diameter portion extending along a portion of its length, and
the layer of said Iron based hardfacing alloy is welded to said reduced diameter portion.
26. The tool joint of claim 25 , wherein said Iron based hardfacing alloy further comprising the balance by weight Silicon and Iron, including impurities as trace elements.
27. The tool joint of claim 26 , wherein said Iron based hardfacing alloy further comprising at most about 0.8 percent Silicon.
28. The tool joint of claim 27 , wherein said Iron based hardfacing alloy further having a hardness of at most about 66 Rc (865 Hv).
29. The tool joint of claim 26 , wherein said Iron based hardfacing alloy further having a hardness of at most about 66 Rc (865 Hv).
30. The tool joint of claim 25 , wherein said Iron based hardfacing alloy further having a hardness of at most about 66 Rc (865 Hv).
31. A method of prolonging the life of an industrial product having a surface and subject to abrasion, comprising:
welding a layer of an Iron based hardfacing alloy to a portion of the surface of the industrial product subject to the abrasion,
said Iron based hardfacing alloy comprising by weight about 0.45 to about 0.8 percent Carbon, about 3.5 to about 4.5 percent Boron, about 4.5 to about 6.5 percent Niobium, about 2.0 to about 2.5 percent Nickel, and about 0.8 to about 1.25 percent Manganese, and
said Iron based hardfacing alloy having a quadratic crystallographic boride and eutectic structure.
32. The method of claim 31 , wherein said Iron based hardfacing alloy further comprising the balance by weight Silicon and Iron, including impurities as trace elements.
33. The method of claim 32 , wherein said Iron based hardfacing alloy further comprising at most about 0.8 percent Silicon.
34. The method of claim 33 , wherein said Iron based hardfacing alloy further having a hardness of at most about 66 Rc (865 Hv).
35. The method of claim 32 , wherein said Iron based hardfacing alloy further having a hardness of at most about 66 Rc (865 Hv).
36. The method of claim 31 , wherein said Iron based hardfacing alloy further having a hardness of at most about 66 Rc (865 Hv).
37. The method of claim 31 , further comprising a cored tubular wire wherein:
said Iron based hardfacing alloy is in said tubular wire.
38. The method of claim 37 , wherein said Iron based hardfacing alloy further comprising the balance by weight Silicon and Iron, including impurities as trace elements.
39. The method of claim 38 , wherein said Iron based hardfacing alloy further comprising at most about 0.8 percent Silicon.
40. The method of claim 39 , wherein said Iron based hardfacing alloy further having a hardness of at most about 66 Re (865 Hv).
41. The method of claim 38 , wherein said Iron based hardfacing alloy further having a hardness of at most about 66 Rc (865 Hv).
42. The method of claim 37 , wherein said Iron based hardfacing alloy further having a hardness of at most about 66 Rc (865 Hv).