AU612224B2 - Reinforced rotary drill bit - Google Patents
Reinforced rotary drill bit Download PDFInfo
- Publication number
- AU612224B2 AU612224B2 AU28875/89A AU2887589A AU612224B2 AU 612224 B2 AU612224 B2 AU 612224B2 AU 28875/89 A AU28875/89 A AU 28875/89A AU 2887589 A AU2887589 A AU 2887589A AU 612224 B2 AU612224 B2 AU 612224B2
- Authority
- AU
- Australia
- Prior art keywords
- drill bit
- rotary drill
- bit
- protrusion
- cutting element
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 238000005520 cutting process Methods 0.000 claims description 58
- 230000003014 reinforcing effect Effects 0.000 claims description 30
- 239000011159 matrix material Substances 0.000 claims description 28
- 229910052751 metal Inorganic materials 0.000 claims description 15
- 239000002184 metal Substances 0.000 claims description 15
- 229910000831 Steel Inorganic materials 0.000 claims description 14
- 239000010959 steel Substances 0.000 claims description 14
- 239000007787 solid Substances 0.000 claims description 5
- 230000001154 acute effect Effects 0.000 claims description 3
- 239000003643 water by type Substances 0.000 claims description 3
- 230000015572 biosynthetic process Effects 0.000 description 11
- 238000005755 formation reaction Methods 0.000 description 11
- 239000010432 diamond Substances 0.000 description 9
- 239000012530 fluid Substances 0.000 description 9
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 description 9
- 239000000463 material Substances 0.000 description 8
- 229910003460 diamond Inorganic materials 0.000 description 7
- 239000004927 clay Substances 0.000 description 6
- 238000005553 drilling Methods 0.000 description 6
- 239000011230 binding agent Substances 0.000 description 5
- 238000005219 brazing Methods 0.000 description 4
- 238000005336 cracking Methods 0.000 description 4
- 238000006073 displacement reaction Methods 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- 229910052799 carbon Inorganic materials 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 229910000788 1018 steel Inorganic materials 0.000 description 2
- 235000003934 Abelmoschus esculentus Nutrition 0.000 description 2
- 240000004507 Abelmoschus esculentus Species 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- 235000015076 Shorea robusta Nutrition 0.000 description 1
- 244000166071 Shorea robusta Species 0.000 description 1
- 229910001315 Tool steel Inorganic materials 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 238000009863 impact test Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 239000008188 pellet Substances 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- -1 stainless steel Chemical class 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- E—FIXED CONSTRUCTIONS
- E21—EARTH OR ROCK DRILLING; MINING
- E21B—EARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
- E21B10/00—Drill bits
- E21B10/46—Drill bits characterised by wear resisting parts, e.g. diamond inserts
- E21B10/56—Button-type inserts
- E21B10/567—Button-type inserts with preformed cutting elements mounted on a distinct support, e.g. polycrystalline inserts
Landscapes
- Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Mining & Mineral Resources (AREA)
- Geology (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Environmental & Geological Engineering (AREA)
- Fluid Mechanics (AREA)
- Chemical & Material Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Geochemistry & Mineralogy (AREA)
- Earth Drilling (AREA)
- Excavating Of Shafts Or Tunnels (AREA)
Description
COMMONWEALTH OF AUSTRAL 12 FORM PATENTS ACT 1952 C MPLETE SPECIFICATION FOR OFFICE USE: Class Int.Class Application Number: Lodged: Complete Specification Lodged: Accepted: Published: ."Priority: Related Art: Name of Applicant: NORTON CHRISTENSEN, INC.
0* Address of Applicant: 2532 South 3270 West, Salt Lake City, Utah, 84119, United States of America S* 0 0 "Actual Inventor: Royce A. Anthon and DeWayne C. Fox Address for Service: SHELSTON WATERS, 55 Clarence Street, Sydney Complete Specification for the Invention entitled: V "REINFORCED ROTARY DRILL BIT" The following statement is a full description of this invention, including the best method of performing it known to us:- 1
I
>1 la REINFORCED ROTARY DRILL BIT This invention relates to drill bits, and more particularly to rotary drill bits with diamond cutting elements used in the drilling of bore holes in earth formations.
9.
Earth boring diamond drill bits may typically include an integral bit body which may be of steel faced with an abrasion-resistant material such as tungsten carbide or may itself be fabricated of a hard metal matrix material such as tungsten carbide. A plurality of diamond acutting elements are mounted along the exterior face of the bit body. Each diamond cutter typically may be S mounted on a stud the other end of which is mounted in a recess in the exterior face of the bit body, or the cutter S* mount may be integrally cast with the matrix of the bit body.
The cutting elements are positioned along the leading edges of the bit body so that as the bit body is rotated in its intended direction of use, the cutting elements engage and drill the earth formation. In use, tremendous forces ire exerted on the cutting elements, particularly against the face thereof in the forward to rear direction as the bit is rotated. Additionally, the SHELSTON WATERS PATENT AITORNEYS CLARENCE STREET, SYDNEY
AUSTRALIA
Cables: 'Valid' SydneyTelex: 24422 -2bit and cutting elements are subjected to substantial abrasive forces. In some instances, impact, lateral, and/or abrasive forces have caused drill bit failure and cutter loss.
C
A significant problem encountered when drilling in certain earth formations such as shales, clay, and other water reactive, sticky formations known as "gumbo" has been the tendency of such bits to become clogged during operation. In dealing with such earth formations, bits have been designed with relatively large cutters with strong hydraulics in the proximity of the cutters to remove the cuttings from the cutter faces with a high volume, high velocity, hydraulic fluid flow.
As synthetic diamond technology has advanced, it is now possible to provide large diamond disc cutters up to two inches in diameter for use on bits. These very large cutters have been helpful in drilling in "gumbo" formations. However, the large diameter of the cutting elements has caused problems in providing secure attachment thereof to the exterior face of the rotary S"drill bits. To accommodate such large diameter cutters, drill bits have been fabricated with outwardly extending shoulders or protrusions on which the cutters may be mounted. However, this leaves a relatively small structure beneath and behind the cutter faces to support the cutters. Additionally, blades, ridges and other structures having multiple cutters mount thereon and extending significant distances from the main profile of the bit body are also becoming more common, presenting similar problems.
e a While tungsten carbide or other hard metal S. matrix bits are highly erosion resistant, such materials are relatively brittle and can crack upon being subjected to the impact forces encountered during drilling.
Typically, such cracks have occurred proximate where the cutting element support structures join the matrix body.
3 The shoulders or protrusions on the exterior of the drill bits to accommodate large diameter cutting exposes these areas of the bit to high impact and shear forces. Bits having large cutter elements thereon extending outwardly from the body of the bit are particularly susceptible to cracking and failure due to these high impact and shear forces. If the cutting elements are sheared from the drill bit body, the expensive diamonds on the cutter elements are lost, and the bit may cease to drill.
S. Accordingly, there is a need in the art for a drill bit having increased impact strength and resistance to cracking, particularly in areas supporting the cutter elements.
One broad form of the present invention provides a rotary drill bit, comprising: a bit body which includes a main body portion and at least one integral, outwardly extending protrusion thereon of a hard metal matrix material; .at least one cutting element mounted on the leading face of said at least one protrusion; and a solid, preformed structure for reinforcing said at least one protrusion extending from the hard metal matrix material of the interior of said main body portion into the hard metal matrix material of the protrusion to the rear of said at least one cutting element, at least partially therebehind and in spaced relationship thereto.
A cutting element is mounted on the protrusion and is angled as known in the art to accomplish drilling of an R o u Tnr~ tr3 l 3a earth formation. There may be one or a plurality of individual cutter elements mounted on each protrusion.
Means for reinforcing the protrusions are provided and extend between the main body portion of the bit and individual protrusions.
S
S*
0D 0 0SS* 9..
00LZI *c 0 In a preferred embodiment, the reinforcing structure comprises a solid preformed arrangement positioned rearwardly of the cutting elements and extending at an acute angle with respect to the main body portion of the bit. The reinforcing structure may be in the form of one or more rods, bars, disks, or wires which are preferably of metal. While steel is the preferred composition for the reinforcing structure, other metals and metal alloys such as stainless steel, nickel alloys or molybdenum may be utilized.
The present invention also encompasses drill bits having a plurality of such protrusions and cutting elements and is particularly suited for use with rotary bits having relatively large diameter cutting elements.
The portions of the matrix on which the elements are mounted are reinforced to provide the bit with greater impact strength and greater resistance to cracking and failure of the bit matrix. Accordingly, it is an object of the present invention to provide a rotary drill bit 02 matrix having improved impact strength and resistance to cracking over prior bits. This, and other objects and advantages of the present invention, will become apparent from the following detailed description, the accompanying drawings, and the appended claims.
Fig. 1 is a perspective view of the rotary drill bit of the present invention; Sfi" Fig. 2 is a diagrammatic sectional view taken through one of the cutting elements along line 2--2 of Fig. 1 and illustrating the reinforcing structure; and Fig. 3 is also a diagrammatic sectional view similar to Fig. 2 illustrating the reinforcing structure in a bit having a somewhat different structure.
The invention is illustrated in the drawings with reference to a typical construction of a rotary earth boring bit. In particular, the invention is illustrated and described with reference to the large compact cutter rotary bit described in greater detail in commonly assigned, copending U.S. Application Serial No. 906,169, filed September 11, 1986. It will also be recognized by those skilled in the art that the configuration of the cutting elements along the exterior face of the matrix may be varied depending upon the desired use of the bit.
Thus, the bit may be designed for either a flat, parabolic, or extended blade crown profile. The invention may also be useful in any hard metal matrix bit configuration which has one or more shoulders, ridges, blades, or other protrusions extending outwardly from the o" main body of the bit.
Referring now to Fig. 1, rotary drill bit 10 of the type disclosed in the above referenced copending application includes an exterior generally cylindrical surface or gage 12 having a bit face 14 on its lowermost portion. Both gage 12 and bit face 14 are formed of the hard metal matrix material of the bit body, such as tungsten carbide. Defined within gage 12 are a plurality of junk slots 16 and 18. The junk slots are designed to 25.. facilitate the upward flow of the drilling fluid and cuttings away from the bit face 14. A number of fluid nozzles 20 are also located on bit face 14. Each of fluid nozzles 20 is designed to provide directed fluid flow to a specific cutting element 22. Each cutting element 22 comprises a tungsten carbide backing 25 having deposited thereon a thin synthetic diamond cutting face 23 which performs the cutting operation.
i I -r -6- Cutting elements 22 are mounted on shoulders or protrusions 24 which extend outwardly from the bit face 14. The cutting elements are secured in place by brazing or otherwise fixing them to the bit face in a conventional manner. For example, cutting elements 22 may be secured to the matrix and to tungsten carbide slug 26 cast into the trailing portion of sockets. 28 (best shown in Fig. 2) on bit face 14 by brazing or other suitable means. In a preferred embodiment, the cutting faces 23 of cutting elements 22 are one inch in diameter or larger.
As shown, each cutter element 22 has an associated fluid nozzle 20 which provides a directed hydraulic flow of fluid to the face of the cutting element. This fluid flow applies a force to chips cut from the earth formation, loosening and removing the chips from the faces of the cutting elements. Additionally, bit includes a plurality of gage cutting elements 30 which comprise smaller diameter diamonds which are mounted on the gage 12 of bit face 14. The gage cutters insure that the drill cuts a path of the desired diameter through the earth formation.
As shown in Fig. 2, positioned rearwardly of each cutting element 22 is reinforcing means 32 extending between the main body portion of drill bit 10 and protrusion or shoulder 24. As illustrated and previously noted, cutting element 22 includes a hard metal matrix backing 25 of tungsten carbide or the like, and is preferably substantially laterally symmetrical.
The backing 25, having cutting face 23 thereon, i is brazed into socket 28 in the bit matrix. Backing provides shock protection and load resistance to the cutting face 23. As shown in Fig. 2, the bit 10 rotates in the direction of the arrow and encounters impact forces -7on cutting face 23 as indicated by the arrow shown in phantom lines. Typically, the cutting element 22 will have a predetermined rake angle to the formation encountered depending upon placement of cutting element 22 and the bit profile and the desired operation of the bit, which depends upon the formations to be drilled.
Reinforcing means 32 may comprise a longitudinally extending element which takes the form of a rod, bar, disk, or wire. It may also comprise a plurality of such structures. In a preferred embodiment, reinforcing means 32 comprises a threaded rod of cylindrical steel stock, such as 1018 or 1020 steel.
Preferably, the steel stock has no coatings on it and the stock is cleaned of any oxides prior to being used.
As can be seen, reinforcing means 32 is 9. positioned rearwardly of cutting element 22 and extends between the main body of the bit and substantially the 9 9 outermost extnt of protrusion 24. Reinforcing means 32 *q 9 is positioned at an acute angle with respect to the main body of the bit. At such an angle, the reinforcing means is pointed slightly toward cutting element 22.
Reinforcing means 32 also extends at least partially behind cutting element 22 and is also preferably centered with respect to cutting element 22 so that impact forces will be focused thereon.
In the embodiment of the invention illustrated in Fig. 3, a somewhat differently configured bit has a shoulder or protrusion 24, which may be a blade-shaped protrusion emanating from the center of a "fishtail" bit 99 9 toward the gage of the bit. Cutting element 22 is mounted into socket 28 in the bit matrix. As shown, reinforcing rod 32 is positioned rearwardly of cutting element 22 and -8extends between the bit matrix and substantially the outermost extent of shoulder or protrusion 34.
Reinforcing rod 32 is preferably angled so that it is roughly parallel or at a slight angle (as shown) to the surface of cutting element 22 (as shown). Rainforcing rod 32 is disposed in a substantially perpendicular orientation to the profile of the main body portion of the bit.
Rotary drill bits employing the present invention are generally made by powder metallurgical techniques which are known in the art. The bit is formed in a carbon mold having an internal configuration corresponding generally to the required surface shape of the bit body, including protrusions for mounting cutting elements.
Thus, the areas where the junk slots are found on the e finished bit body contain carbon or clay displacement 'material in the mold.
*8 The areas in the mold which correspond to where the cutting elements are to be mounted after furnacing of the bit body are filled with a displacement material such as carbon discs of like size to the cutting elements having clay adjacent thereto so that the furnaced bit body has mounting sockets 28 formed therein. Reinforcing means 32 are positioned in the mold by embedding them in the clay displacement material placed at the outermost extent of the protrusion cavitities from the body mold cavity.
Reinforcing means 32 are positioned rearwardly of where the cutting elements 22 are to be mounted.
Preferably, the reinforcing means 32 is a threaded steel rod which is desirably positioned to be perpendicular to the mold profile from which it protrudes. In other words, when viewed from the perspective of the finished bit.
I_
-9reinforcing means 32 extends from the main profile or surface of the bit in a perpendicular manner to the point on the profile from which it extends.
As is conventional, elements which will form the internal fluid passages and nozzles in the finished bit are also positioned in the mold at this time. A steel blank is also positioned in the mold at this time. A hard metal matrix material such as tungsten carbide is then added to the mold. A binder material, preferably a copper-based alloy, in the form of pellets or other small particles, is then poured over the matrix material. The filled mold is then placed in a furnace and heated to above the melting point of the binder, typically above about 1100 degrees C. The molten binder passes through :015 and infiltrates the matrix material.
After cooling, the matrix and binder are consolidated into a solid body which is bonded to the steel blank. After further cooling, the bit body is removed from the mold. The steel blank is then welded or otherwise secured to an upper body or shank. Clay and other displacement material is removed at this time.
Because reinforcing means 32 was embedded in the clay, the portion of the reinforcing means which extends from the bit body is machined off flush to the trailing edge of the protrusion.
Cutting elements 22 are then mounted to the bit body. As is conventional, cutting element 22 is mounted into socket 28 and backing 25 secured therein by brazing with a suitable metal brazing material. The gage cutting elements may also be mounted to the exterior of the bit body at this time.
-i 1 In order that the invention may be more readily understood, reference is made to the following example, which is intended to illustrate the invention, but is not to be taken as limiting the scope thereof.
Example In order to demonstrate the reinforcing capabilities of the structure of the present invention an impact test was made. The test measured the resistance to i0 fracture by impact forces of a matrix material reinforced by a steel rod such as the preferred reinforcing rods of the present invention.
Samples of matrix material were fabricated in a conventional manner by filling a cylindrical mold with tungsten carbide matrix material and a copper-based alloy binder. The mold was sized to produce a sample specimen six inches in length with a 1/2 inch diameter. The matrices were furnaced at 2150 degrees F for 60 minutes.
Previous testing established that such a sample, when subjected to an impact force with a Charpy Impact Tester, would fracture at an impact force of about 3.5 ftlb.
Sample specimen I included a 3/16 inch diameter mild 1018 steel rod positioned centrally within the specimen. Sample specimen 2 included a 3/16 inch diameter threaded mild 1018 steel rod positioned centrally within the specimen. Sample specimen 3 included a 1/8 inch diameter tool steel rod positioned centrally within the specimen. All steel rods were grit blasted prior to placement in the respective mold to remove any oxides.
'300' All sample specimens were then cut in two to form two three inch long bars (labeled A and 13 below) and tested using a Charpy Impact Tester. The results are reported in Table I below.
i i. -q -11- TABLE I Specimen Impact Force Result 1A 25.0 ftlb incomplete break 1B 23.5 ftlb break 2A 11.0 ftlb break 2B 11.7 ftlb break 2A 4.75 ftlb break 2B 5.75 ftlb break While certain representative embodiments and details have been shown for purposes of illustrating the invention, it will be apparent to those skilled in the art that various changes in the methods and apparatus disclosed herein may be made without departing from the scope of the invention, which is defined in the appended claims. For example, multiple cutting elements may be mounted on each protrusion; half-circular or other shape cutting elements may be used; several reinforcing elements may be employed for a single protrusion; U or V-shaped o.o reinforcing elements may be used either right side up or upside down; reinforcing elements of a variety of cross-sections, including but not limited to square, rectangular, triangular, elliptical, half-circular, etc., may be employed.
~A
Claims (9)
1. A rotary drill bit, comprising: a bit body which includes a main body portion and at least one integral, outwardly extending protrusion thereon of a hard metal matrix material; at least one cutting element mounted on the leading face of said at least one protrusion; and a solid, preformed structure for reinforcing said at least one protrusion extending from the hard metal matrix material of the interior of said main body portion into the hard metal matrix material of the protrusion to the rear of said at least one cutting element, at least partially there'behind and in spaced relationship thereto.
2. The rotary drill bit of claim 1 in which said solid preformed structure is a rod, bar, disk, or wire.
3. The rotary drill bit of claim 1 in which said preformed structure is fabricated from steel.
4. The rotary drill bit of claim 1 in which said preformed structure is of cylindrical steel stock.
The rotary drill bit of claim 4 in which said cylindrical steel stock is threaded.
6. The rotary drill bit of claim 2 in which said preformed structure is positioned at an acute angle with respect to said main body portion of said bit body.
7. The rotary drill bit of claim 1 in which said reinforcing structure comprises a longitudinally extending element disposed in substantially perpendicular orientation to the profile of said main body portion. /^S 13
8. The rotary drill bit of claim 1 in which said reinforcing structure extends to substantially the outermost portion of said protrusion.
9. The rotary drill bit of claim 1 in which said protrusion supports a single, substantially laterally symmetrical cutting element, and said reinforcing structure comprises a rodlike element centered with respect to and to the rear of said cutting element. A rotary drill bit substantially as herein described with reference to Figures 1 and 2 or Figures 1 and 3 of the accompanying drawings. •DATED this 19th day of APRIL, 1991 NORTON CHRISTENSEN, INC .Attorney: PETER HEATHCOTE Fellow Institute of Patent Attorneys of Australia 9. of SHELSTON WATERS i 9 9 9 1VL^"HW
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14937488A | 1988-01-28 | 1988-01-28 | |
US149374 | 1988-01-28 |
Publications (2)
Publication Number | Publication Date |
---|---|
AU2887589A AU2887589A (en) | 1989-08-03 |
AU612224B2 true AU612224B2 (en) | 1991-07-04 |
Family
ID=22529996
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AU28875/89A Expired - Fee Related AU612224B2 (en) | 1988-01-28 | 1989-01-27 | Reinforced rotary drill bit |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP0326176A3 (en) |
AU (1) | AU612224B2 (en) |
CA (1) | CA1314866C (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA1314866C (en) * | 1988-01-28 | 1993-03-23 | Royce A. Anthon | Reinforced rotary drill bit |
US5007493A (en) * | 1990-02-23 | 1991-04-16 | Dresser Industries, Inc. | Drill bit having improved cutting element retention system |
US5213171A (en) * | 1991-09-23 | 1993-05-25 | Smith International, Inc. | Diamond drag bit |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0066435A1 (en) * | 1981-06-01 | 1982-12-08 | Dresser Industries,Inc. | Drill bit having abradable cutter protection |
EP0263660A2 (en) * | 1986-10-06 | 1988-04-13 | De Beers Industrial Diamond Division (Proprietary) Limited | Cutting component |
EP0326176A2 (en) * | 1988-01-28 | 1989-08-02 | Norton Christensen, Inc. | Reinforced rotary drill bit |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3175194D1 (en) * | 1980-01-10 | 1986-10-02 | Stonehouse Ltd | Rotary drill bits |
EP0145421B1 (en) * | 1983-12-03 | 1989-07-26 | Reed Tool Company Limited | Improvements in or relating to the manufacture of rotary drill bits |
-
1989
- 1989-01-27 CA CA000589326A patent/CA1314866C/en not_active Expired - Fee Related
- 1989-01-27 AU AU28875/89A patent/AU612224B2/en not_active Expired - Fee Related
- 1989-01-30 EP EP89101527A patent/EP0326176A3/en not_active Withdrawn
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0066435A1 (en) * | 1981-06-01 | 1982-12-08 | Dresser Industries,Inc. | Drill bit having abradable cutter protection |
EP0263660A2 (en) * | 1986-10-06 | 1988-04-13 | De Beers Industrial Diamond Division (Proprietary) Limited | Cutting component |
EP0326176A2 (en) * | 1988-01-28 | 1989-08-02 | Norton Christensen, Inc. | Reinforced rotary drill bit |
Also Published As
Publication number | Publication date |
---|---|
CA1314866C (en) | 1993-03-23 |
EP0326176A2 (en) | 1989-08-02 |
EP0326176A3 (en) | 1990-03-21 |
AU2887589A (en) | 1989-08-03 |
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