This invention relates to improvements to earth-boring bits having rotating cones with cutting structures and in particular to hardfacing a spear point to enhance wear resistance.
In drilling bore holes in earthen formations by the rotary method, rock bits fitted with one, two or three rolling cutters are employed. The bit is s secured to the lower end of a drill string that is rotated from the surface, or the bit is rotated by downhole motor or turbines. The cutters mounted on the bit roll and slide upon the bottom of the bore hole as the bit is rotated, thereby engaging and disengaging the formation material to be removed. The roller cutters are provides with cutting elements that are forced to penetrate and gouge the bottom of the borehole by weights of the drill string. The cuttings from the bottom and sidewalls of the borehole are washed away by drilling fluid that is pumped down from the surface through the hollow drill string.
One type of cutting element in widespread use is a tungsten carbide insert which is interference pressed into an aperture in the cutter body. Tungsten carbide is metal which is harder than the steel body of the cutter and has a cylindrical portion and a cutting tip portion. The cutting tip portion is formed in various configurations, such as chisel, hemispherical or conical, depending upon the type of formation to be drilled. Some of the inserts have very aggressive cutting structure designs and carbide grades that allow the bits to drill in both soft and medium formations with the same bit.
Another type of rolling cutter earth-boring bit is commonly known as a “steel-tooth” or “milled-tooth” bit. Typically these bits are for penetration into relatively soft geological formations of the earth. The strength and fracture-toughness of the steel teeth permits the use of relatively long teeth, which enables the aggressive gouging and scraping actions that are advantageous for rapid penetration of soft formations with low compressive strengths.
However, it is rare that geological formations consist entirely of soft material with low compressive strength. Often, there are streaks of hard, abrasive materials that a steel-tooth bit should penetrate economically without damage to the bit. Although steel teeth possess good strength, abrasion resistance is inadequate to permit continued rapid penetration of hard or abrasive streaks. Consequently, it has been common in the arts since at least the 1930s to provide a layer of wear-resistance metallurgical material called “hardfacing” over those portions of the teeth to the severest wear. The hardfacing typically consists of extremely hard particles, such as sintered, cast, or macro-crystalline tungsten carbide, dispersed in a steel matrix. Such hardfacing materials are applied by welding a metallic matrix to the surface to be hardfaced and applying the hard particles to the matrix to form a uniform dispersion of hard particles in the matrix.
Unlike a tungsten carbide insert bit teeth of a steel-tooth bit are not susceptible to stress cracking due to excessive heat. A steel-tooth bit would be able to drill the relatively soft non-abrasive formations mentioned above with case stress cracking on heel rows of insert bits. However, because of the hardness and thickness of adjacent formations, a steel-tooth bit would wear too quickly, thus is not a preferred choice in those areas.
In this invention, the bit has a cutter which has tungsten carbide inserts and a spear point. The spear point has a neck that joins a smooth portion of the cutter and blades that extend from the neck and converge to an apex. The blades define valleys or spaces between them.
A layer of hardfacing is applied to the entire spear point including the interim spaces and the neck. This hardfacing may be of a conventional type comprising tungsten carbide particles in a steel alloy matrix.
Referring to
First cone 29 has an outer row 39 and an intermediate row 41 of compacts 35, which are located adjacent the gage surface of first cone 29. An inner row 43 is located a short distance inward from intermediate row 41 toward the bit axis. A thin annular conical band 45 is located between intermediate row 41 and inner row 43. First cone 29 has a spear point 47 that is conventional and comprises radially extending blades. A layer of hardfacing 49 is applied over spear 47 and a segment of a nose section 50 of cone 29. A conical surface 51 extends from inner row 43 to the neck portion of spear point 47. A layer of hardfacing 49 may be applied to a portion of conical surface 51 near the neck portion of spear 47. The hardfacing 49 of spear 47 reduces the amount of wear in the nose area 50. Hardfacing 49, combined with the use of compacts 35 on inner row 43, intermediate row 41, and outer rows 39 reduces the total amount of wear of cone 29.
Second cone 31 has an outer row 53 and an intermediate row 55 of compacts 35. The nose portion 56 of cone 31 extends axially from intermediate row 55, forming conical band 57. In this embodiment, an inner row 59 of compacts 35 are located on the nose portion 56 of cone 31. Alternatively, milled steel teeth could be formed on the nose portion 56 of cone 31, in place of compacts 35 on inner row 59. If an inner row of steel teeth were formed on the nose portion 56 of cone 31, hardfacing could be applied over the teeth and sections of the nose portion 56 of cone 31 and conical band 57.
Third cone 33 has an outer row 61 and an intermediate row 63 of compacts 35. The nose portion of cone 33 extends axially from intermediate row 63, forming conical band 65. In this embodiment an inner row 67 of compacts 35 are located on the nose portion of cone 33. An additional set of small compacts 68 are located on the end 69 of the nose portion of cone 33. Alternatively, milled steel teeth could be formed on the nose portion of cone 33, in place of compacts 35 on inner row 67 and compacts 68 on nose end 69. If an inner row of steel teeth were placed on the nose portion of cone 33, hardfacing could be applied over the teeth, and sections of the nose portion of cone 33 and conical band 65.
In operation, bit 27 is run conventionally. The combination of compacts 35, inserts 37, and hardfacing 49 applied to the nose section 50 of cone 29 reduces wear and erosion, increasing the life of the bit 27. While the invention has been shown in only one of its forms, it should be apparent to those skilled in the art that it is not so limited but is susceptible to various changes without departing from the scope of the invention.
This application claims priority to provisional application 61/088,991, filled Aug. 14, 2008.
Number | Date | Country | |
---|---|---|---|
61088991 | Aug 2008 | US |