Background of the Invention
The invention relates to a rotary drill bit for drilling oil and gas wells and, more particularly, to a drill bit suitable for up to hard formations having cutting preforms of polycrystalline diamonds on tungsten carbide substrates.
In rotary drilling, the bit is fixed on the end of a rotating drill pipe inside a casing, the drill pipe being lowered as the drilling progresses. A heavy artificial substance known as drilling mud is circulated down through the drill pipe, out through the bit and back up the casing to remove rock fragments. The drilling mud cools the bit, washes the cutting elements so they present a clean cutting face whereby the cutting takes place and, as indicated, lifts or carries debris resulting from the drilling to the surface. For the drilling mud to carry out these functions, it is necessary its velocity through the bit's fluid entrances and channels be high without causing an undesirably high back pressure so it moves quickly across the face and is discharged rapidly and efficiently up the junk slots. It is important clogging of the bit be prevented with rapid removal of cuttings and also that undue stress be avoided.
Rapid penetration of the earth and longer runs improve efficiency of the drilling operation very substantially. Preform cutting elements as disclosed in U.S. Pat. Nos. 3,745,623, 3,767,371, 4,109,737 and 4,156,329 have been utilized by the inventor and others to provide improved penetration in soft to medium-hard formations such as salt, shale, anhydrite, carbonates, marls, clay and sandstones. But when drilling in harder formations, difficulties have been encountered. Solutions to such problems have been suggested as disclosed, for example, in U.S. Pat. No. 4,006,788 to L. Garner, which applies to a rotary drill bit provided with rolling cone cutters. The patent spells out the need for rotary rock bits which work well in various types of formations, soft or hard, encountered in deep wells where it is highly desirable to penetrate long distances before changing the bits required.
Summary of the Invention
The invention primarily involves the arrangement of the cutter preform elements, the shape of the drilling face, the relative proportions of the bit body, the structure of the fluid entrances, and the location and relative size of the junk slots to achieve a rock drill capable of relative rapid penetration in deep wells irrespective of the formations encountered. The bit, provided with cutter preform elements of polycrystalline diamonds with tungsten carbide substrates penetrates relatively rapidly for the formation involved with a relatively lengthy drilling time whereby costs per foot drilled are significantly reduced.
A major aspect of the invention lies in the arrangement of the cutter preforms in sets, the cutter preforms on each given set being disposed at equal radius from, and displaced about, the axis of rotation of the bit through equal arcs. Successive sets of cutter preforms remove the formation through which they are penetrating by cutting or shearing action, each set tracing a path which overlaps with the paths of the adjacent set or sets. The peripheral set of cutter preforms is secured within or adjacent to the junk slots and off-sets may be provided in alternately adjacent raised portions which both protect cutter preforms and ensure junk slots remain unclogged. Clogging is also minimized by proportions of the bit body wherein the overall diameter of the body is about twice its length measured along the raised portions which define the junk slots. The fluid entrances from the interior of the bit to its drilling face are of a converging-diverging type constructed from two components, a converging shaped jet element held in place by diverging jet holder component, the combined jet nozzle minimizing flow turbulence, erosion and corrosion which would otherwise result from sharp cornered and straight-necked nozzles.
Strong, but not larger than required, supports for cutter preform elements aid in minimizing resistance of flow of the drilling mud away from the drilling face. A relatively rearward inclination of about 20.degree. relative to a line perpendicular to the drilling face through the axis of the cutter preform element improves its impact resistance whereby energy required to remove a given amount of formation is substantially reduced.
Other objects, adaptabilities and capabilities of the invention will be appreciated by those skilled in the art as the description progresses, reference being had to the accompanying drawings, in which:
Brief Description of the Drawings
FIG. 1 is a side elevation of a drill bit in accordance with the invention;
FIG. 2 is a bottom view, in the operational sense, of the drill bit shown in FIG. 1;
FIG. 3 is a side sectional view taken on section lines III--III of FIG. 2; and
FIG. 4 is a detail sectional view of a jet insertion taken on section lines IV--IV of FIG. 2.
FIG. 5 is a side elevation of a further embodiment of a drill bit in accordance with the invention;
FIG. 6 is a view, similar to FIG. 2, of the embodiment shown in FIG. 5;
FIG. 7 is a sectional view of the crown of the bit of FIGS. 5 and 6 taken on section lines 7--7 of FIG. 6.
FIG. 8 is a plan view of a junk screen received in the bit's crown; and
FIG. 9 illustrates the rake angles of preform cutter elements relative to the direction of rotation.
Description of the Preferred Embodiments
Referring to the drawings, the drill bit indicated generally by reference numeral 10 which consists of a pin shank 11 and a crown 12 rigidly connected by a weld 14.
Pin shank 11 includes a threaded connection 15 integral with a steel shank 16 which includes a shank angle 17 and a breaker slot 20, also known as a keyway, for threading drill bit 10 onto the end of a rotating drill pipe not shown.
Crown 12 has a further shank portion 21 which, by weld 14, and internally threaded is rigidly affixed to shank 16 and forms a part thereof. Integral with shank portion 21 is the angle shoulder 22. Below shoulder 22 (to its left as seen in FIG. 1) is a side surface 24 which includes four raised portions 25 and a further set of raised portions 26 which alternate with portions 25. The latter raised portions 26 are each surrounded on three sides by a fluid channel known as a junk slot 27. Portions 26 have planar outboard surfaces 30 contrasting with the curved outboard surfaces 31 of each raised portion 25, each such surface 31 coinciding with a cylindrical surface having the same longitudinal axis as the bit's axis of rotation 32. Between adjoining portions 25, slots 27 have three adjoining planar surface strips 34, 35 and 36, the central strips 35 having the same width as the innermost parts of the corresponding portion 26. The bit's face 37 has a central convex portion 40 surrounded by a peripheral portion 41, portion 40 coinciding with a portion of a sphere having its center on the axis 32 and the portion 41 coinciding in part with a cone having its apex and longitudinal axis coinciding with axis 32.
Each raised portion 25 is provided with four gauge buttons 42 which are composed of tungsten carbide and press fitted in portions 25 flush with their outboard surfaces.
From FIG. 2, it will be noted that nineteen preform cutter elements are mounted on face portion 40, eight further preform elements 44 are mounted on conical portion 41 and a still further eight preform cutter elements 44 are mounted in junk slots 27 between each raised portion 26 and its succeeding raised portion 25 adjacent face portion 41. Thus, there are total of twenty-seven preform cutter elements 44 which are mounted on the bit's face 37 and eight further elements 44 are mounted in junk slots 27, for a total of thirty-five cutter elements mounted on crown 12.
As seen in FIG. 2 the most central cutter element designated 44A has an edge which coincides with axis of rotation 32 and succeeding sets of cutter elements 44 are received in successive sets of openings 45 which have their centers coincide with circles 50, 51, 52, 53, 54 and 55, respectively, on face portion 40, and circle 56 on face portion 41, succeeding circles 50 through 56 being shown in dot-dash lines and representing generally the cutting paths of successive sets of cutter elements 44. Commencing after cutting element 44A it will be noted the next three sets, for circles 50, 51 and 52, each have two cutter elements 44 whereas the next successive three sets, coinciding with circles 53, 54 and 55, respectively, each have four cutter elements 44. The last successive set of eight cutter elements 44 on face portion 40 coincides with circle 56. Finally, the last set of cutter elements 44 have the center of their cutting blanks 60 rotate through the circle 57 which, as seen in FIG. 2, is tangent to strips 34 and 36. A circle (not shown) through the centers of the faces of cutting blank 60 coincides with the outboard surfaces of the offset cylindrical portions 25A of each raised portion 25.
As seen in FIG. 3, it will be appreciated each circle 50-55 passes through a centerline 48 at the corresponding surface of the face portion 40 whereby the centerline 48 intersects axis 32 at the same point as the radius for face portion 40. In the following Table I this angle is indicated by the angle alpha (.alpha.). The radius of each circle 50 through 57 is also shown in Table I for succeeding circles together with the number of openings 45 and the angle from the Y axis as seen in FIG. 2 in a counterclockwise direction indicated by arrow 61, the operational direction of rotation of the bit, the angle of the intersection of each centerline with a corresponding circle 50 through 57 being also included in Table I.
Cutter blank 60 is made of a combination of polycrystalline (man made) diamonds and cemented tungsten carbide produced as an integral blank by a high-temperature, high pressure process developed by General Electric Company and currently marketed under the trademark "STRATAPAX." The particular blank is identified by General Electric's product No. 2542. Cutting elements of the type involved are disclosed in U.S. Pat. No. 4,109,737 of H. Bovenkerk which issued Aug. 29, 1978.
Cutting blank 60 is mounted on a pin 62 and is bonded to a bias part 64 which is canted 20 degrees to the rearward relative to the centerline pin 62, the opening 45 receiving pin 62.
Each cutter element 44 has at the rear of pin 62 a channel 65 which defines part of an opening 66, the other portion of opening 66 being defined in the crown 12 as shown. Such opening 66 receives a lock pin 67 for maintaining each cutter element 44 in the desired rake alignment.
To insert each cutter 44, the material surrounding opening 45 is heated to a range of 1800.degree. to 1900.degree. F. and cutter element 44 is pressed into the opening 45 until the disc 63, on which cutting blank 60 is mounted, is pressing on the surface of the crown 12 with the channel 65 being aligned to define opening 66. The objective is to achieve a tight shrink-press fit combination. With the opening 66 properly aligned, lock pin 67 is pressed into place and the next cutter element 44 is placed in appropriate opening 45, by the same process, the sequence of openings and time for inserting each cutter element being such the temperature of face 37 does not exceed 1250.degree. F. except in the immediate vicinity of the opening 45 involved.
Referring to FIG. 4, a jet opening for supplying drilling mud in face 37 is shown. It will be noted from FIG. 2 there are four such jet openings 70. Each opening 70 has a threaded portion 71, and an enlarged portion 72 and a bore 74 which connects with fluid entrance 75.
Enlarged portion 72 receives a nozzle throat 76 which is sealed in portion 72 by a high temperature sealant such as, for example, the Haliburton "Howcoweld." A nozzle flared piece 77 is received in the threaded portion 71 and also sealed in place by a high temperature sealant such as Haliburton's "Howcoweld." It will be noted nozzle piece 77 includes a pair of notches 80 for receipt of a tool for turning piece 77 whereby it is received by threaded portion 71 and nozzle throat 76 is firmly seated against shoulders 81 which are disposed between bore 74 and enlarged portion 72.
Preferably, the surface of the drill bit 10 is case hardened to minimize undesirable scarring of the bit during operation.
In field tests, drill bits constructed in accordance with the invention have operated as follows:
The following observations were made from field tests:
1. Retention of cutting elements in the drilling bit was excellent;
2. The bit operated very well in strata of all types including hard strata.
3. The cost per foot drilled by drilling bits in accordance with the invention compared with conventional bits frequently provides savings in the range of fifty to one hundred percent.
4. The effective life of the bit for hard formations is about forty-eight hours in which period roughly a penetration of 1500 to 1800 feet can be reasonably anticipated.
5. The wear on individual cutter elements increased as their distance from the axis of rotation increased.
6. There was a need to increase the flow areas for the drilling mud to minimize loss of effective jet action.
7. Recirculation of junk in the drilling mud can be a source of difficulty and should be minimized.
As a result of the foregoing observations, modifications were incorporated in the bit whereby the further embodiment illustrated in FIGS. 5 through 9 was constructed. This drill bit, designated generally by reference numeral 90, has a pin shank 11 which is essentially the same as that of the first embodiment. Here and with other components similar to those in the first embodiment, the same reference numerals are used. Thus, in crown 92 of drill bit 90, gauge buttons 42 and preform cutter elements 44 are essentially identical to those shown in the first embodiment. However, it will be recognized the placement of such elements on crowns 12 and 92 is different.
Crown 92 includes a bit face 94 which has a convex portion 95 and a conical portion 96 which coincides with the surface of a truncated cone.
The cylindrical sides or surface 97 of crown 92 have five raised portions 100 welded thereto. Such raised portions including four openings each receiving gauge buttons 42. Thus with five raised portions 100, twenty gauge buttons 42 are required. Preferred are serrated compact General Electric type gauge buttons (No. 59S3AH) which are pressed to be flush with the surface.
The spaces between raised portions 100, which are identified by reference numerals 101, function as junk slots and it will be noted raised portions corresponding to portions 26, as shown in the first embodiment, have been eliminated in this embodiment. The area of spaces 101 is roughly double that of portions 100. The purpose is to maximize space provided for discharge of drilling mud while retaining sufficient surface through raised portions 100 to maintain drill bit 90 in its proper location relative to the shaft which is being carved out by the drill bit.
The axis of rotation of drill bit 90 is axis 102. Convex portions 95 of face 94 has a radius of 5.25 inches from a point on axis 102. The diameter of surface 97 is 7.45 inches and the radius of portion 95 as seen from above is 2.99 inches. The overall diameter of the crown 92, considered as a cylinder coinciding with the surfaces of raised portions 100, is 8.467 inches. However, it will be noted from FIG. 6 the preform cutter elements farthest from axis 102 circumscribe a circle having a diameter of 8.495 inches. Thus, the tops of the outmost cutting blanks 60, as manufactured, cut an opening somewhat larger than the diameter circumscribed by the outer surfaces of raised portions 100.
The precise locations of preform cutter elements 44 on crown 92, as shown in FIG. 6, are set forth in the following Table II:
Comparison of Table II with Table I reveals that following the most central cutter element 44A in FIG. 2 and 44B in FIG. 6, there are eight additional sets of cutter elements 44 in FIG. 2 whereas in FIG. 6 there are nine additional sets of cutter elements 44, such sets being in corresponding circles 50B through 58B. In Table II, the radius of each circle 50B through 58B is measured perpendicular to axis 32. The angle A-1 is the number of degrees from the Y axis as seen in FIG. 6 in a counterclockwise direction indicated by arrow 61B, also the operational direction of the bit, where such angle intersects with centerline 48 for each cutter element 44 in a corresponding circle 50B through 58B. In addition, as will be understood by reference to FIG. 9, the rake angle of the elements faces (viewed along their corresponding axis 48) has been modified from zero degrees cutter elements 44 in the first embodiment to a +71/2.degree. for preform cutter elements 44 in circles 50B, 51B, and 52B, and a +5.degree. for preform cutter elements 44 in circle 53B, 54B and 55B. Preform cutter elements 44 in circle 56B have a zero rake angle, whereas cutter elements 44 in circles 57B and 58B have a minus 5.degree. rake angle.
In view of the foregoing, it will be appreciated as seen in FIG. 6, the most central cutter element designated 44B has an edge which coincides with the axis of rotation 102 and succeeding sets of cutter elements 44 are received in successive sets of openings 45B which have their centers coincide with circles 58B, 51B, 52B, 53B, 54B and 55B, respectively, on convex portion 95, and on circles 56B and 57B on conical portion 96. Circle 58B in this embodiment represents surface 97.
The first three sets of cutting elements 44 each have two cutter elements which are 180.degree. apart. The next four cutter elements 53B, 54B, 55B and 56B, each have four cutter elements 44. These sets each have such cutter elements spaced 90.degree. apart. Circle 57B has six cutter elements 44 which are spaced apart 60.degree.. Finally, the last set of eight cutter elements 44 in circle 58B are spaced apart by 45.degree..
It will be further noted, whereas the first embodiment discloses four jet openings, the instant embodiment has six jet openings 70, such openings 70 being identical to those shown in FIG. 4 of the first embodiment.
From the foregoing, it will be appreciated in the second embodiment the gauge buttons have been increased from sixteen to twenty, the preform cutter elements have been increased from thirty-five to thirty-seven and the number of jet openings have been increased from four to six. The four outermost jets are centered at a radius of about 2.3168 inches from axis 102 and are spaced 90.degree. apart. At the same time the space provided for the junk slots has also been enlarged.
FIG. 8 discloses an optional junk screen 105 which may be optionally seated on shoulder 108 at fluid entrance 75B within crown 92 to prevent recirculation of junk in the drilling mud into fluid entrance 75B and under crown 92.
In an initial test of the second embodiment, bit 90 drilled 3204 feet in 183 continuous hours of drilling for an average of 17.51 feet per hour. It went into the hole at about 7300 feet.
In operations, the bit 10 or 90 is affixed by means of the threaded connection 15 on the end of a rotating drill pipe inside a casing, the drill pipe being lowered drilling progresses. A heavy artificial "mud" is circulated down through the drill pipe, into the bit's fluid entrances, out through the bit's jet openings, and back up via the junk slots and the casing. The accumulated junk, that is the rock fragments and the like, is filtered out before the mud is recirculated into the drill pipe and any junk missed is stopped by screen 105 on the second embodiment. A relax oil base type drilling mud with mud weight of about 12.2 to 15.4 has been used with success. The bit face velocity is in a range of about 275 to 325 feet per second.
The drawings are reasonably to scale. They are intended to disclose the relationship of the various components whether or not specifically described as such in the foregoing specification. Claim language directed to the various elements of the invention should be construed to cover corresponding structure in the specification and equivalents thereof. For example, "rake angle" of a cutter element is intended to refer to the rake angle illustrated in FIG. 9. Also, it is to be understood that although preferred embodiments of the invention have been described above, the inventive concepts may be applied to other applications and modifications within the scope of the appended claims.