US20130014998A1 - Downhole cutting tool and method - Google Patents
Downhole cutting tool and method Download PDFInfo
- Publication number
- US20130014998A1 US20130014998A1 US13/179,997 US201113179997A US2013014998A1 US 20130014998 A1 US20130014998 A1 US 20130014998A1 US 201113179997 A US201113179997 A US 201113179997A US 2013014998 A1 US2013014998 A1 US 2013014998A1
- Authority
- US
- United States
- Prior art keywords
- cutting
- powder
- base
- cutting tool
- consolidated
- 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.)
- Abandoned
Links
- 238000005520 cutting process Methods 0.000 title claims abstract description 54
- 238000000034 method Methods 0.000 title claims description 12
- 239000000463 material Substances 0.000 claims abstract description 25
- 239000000843 powder Substances 0.000 claims abstract description 25
- 238000004519 manufacturing process Methods 0.000 claims abstract description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 6
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 6
- 229910052582 BN Inorganic materials 0.000 claims description 3
- PZNSFCLAULLKQX-UHFFFAOYSA-N Boron nitride Chemical compound N#B PZNSFCLAULLKQX-UHFFFAOYSA-N 0.000 claims description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 3
- 229910000831 Steel Inorganic materials 0.000 claims description 3
- 239000010941 cobalt Substances 0.000 claims description 3
- 229910017052 cobalt Inorganic materials 0.000 claims description 3
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 3
- 229910052802 copper Inorganic materials 0.000 claims description 3
- 239000010949 copper Substances 0.000 claims description 3
- 229910003460 diamond Inorganic materials 0.000 claims description 3
- 239000010432 diamond Substances 0.000 claims description 3
- 229910052742 iron Inorganic materials 0.000 claims description 3
- 229910052759 nickel Inorganic materials 0.000 claims description 3
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 claims description 3
- 229910010271 silicon carbide Inorganic materials 0.000 claims description 3
- 239000010959 steel Substances 0.000 claims description 3
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 claims description 3
- 239000011159 matrix material Substances 0.000 description 7
- 238000007596 consolidation process Methods 0.000 description 5
- 239000012254 powdered material Substances 0.000 description 4
- 239000002245 particle Substances 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 238000005755 formation reaction Methods 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 229910052786 argon Inorganic materials 0.000 description 1
- 230000004323 axial length Effects 0.000 description 1
- 239000004568 cement Substances 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000005056 compaction Methods 0.000 description 1
- -1 earthen formations Substances 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000011236 particulate material Substances 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 238000002490 spark plasma sintering Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
- B22F7/062—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C26/00—Alloys containing diamond or cubic or wurtzitic boron nitride, fullerenes or carbon nanotubes
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C29/00—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
- C22C29/02—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides
- C22C29/06—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds
- C22C29/065—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds based on SiC
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
- B22F2005/001—Cutting tools, earth boring or grinding tool other than table ware
Definitions
- FIG. 1 is a cross-sectional view a cutting tool
- FIG. 2 is a cross-sectional view of a mold for making the cutting tool of FIG. 1 .
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Geology (AREA)
- Life Sciences & Earth Sciences (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Mining & Mineral Resources (AREA)
- Fluid Mechanics (AREA)
- Environmental & Geological Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Composite Materials (AREA)
- Physics & Mathematics (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Geochemistry & Mineralogy (AREA)
- Powder Metallurgy (AREA)
- Earth Drilling (AREA)
Abstract
A downhole cutting tool includes a base including a first consolidated powder; and at least one cutting feature affixed to the base, the at least one cutting feature including a cutting material suspended in a second consolidated powder, wherein the base and the at least one cutting feature are both consolidated and bonded together simultaneously. Also included is a method of manufacturing a cutting tool.
Description
- Downhole cutting tools have a tendency to crack because they are manufactured from very high strength (and therefore brittle) materials. Further, during manufacture, these tools are often subjected to very high temperatures, such as to wet braze cutting material onto the tools, and extensive machining. These cracks limit the life of such tools, increasing material used, time spent replacing the tools, and overall costs. Additionally, these tools need to be closely inspected for cracks and sometimes repaired even before use, further increasing cost, time and materials. Improvements in downhole cutting tools are accordingly well received by the industry.
- A downhole cutting tool includes a base including a first consolidated powder; and at least one cutting feature affixed to the base, the at least one cutting feature including a cutting material suspended in a second consolidated powder, wherein the base and the at least one cutting feature are both consolidated and bonded together simultaneously.
- A method of manufacturing a cutting tool includes layering a first powder and a second powder in a die, the second powder comprising cutting material suspended therein; and simultaneously consolidating the first and second powders to form a base and at least one cutting feature, respectively, the simultaneous consolidating also bonding the base to the at least one cutting feature.
- The following descriptions should not be considered limiting in any way. With reference to the accompanying drawings, like elements are numbered alike:
-
FIG. 1 is a cross-sectional view a cutting tool; and -
FIG. 2 is a cross-sectional view of a mold for making the cutting tool ofFIG. 1 . - A detailed description of one or more embodiments of the disclosed apparatus and method are presented herein by way of exemplification and not limitation with reference to the Figures.
- Referring now to
FIG. 1 , atool 10 is shown having abase 12 and a plurality ofcutting features 14. A plurality ofwatercourses 16 is interspaced with the plurality ofcutting features 14, between adjacent ones of the cutting features. Thewatercourses 16 are for enabling the flow of fluid to and from thecutting features 14, for example, to cool the cutting features, wash away any cuttings, etc. Thetool 10 is intended to be used downhole to cut or mill, for example, rock, earthen formations, cement, tubulars for fishing, downhole obstructions, etc. Opposite from the cutting features 14, thebase 12 terminates in aneck 18. Theneck 18 is securable to a shoe casing or the like, via welds, threads, a friction fit, etc. Accordingly, theneck 18 may have an axial length that significantly shorter than prior shoe heads or ends. - The base 12 (including the neck 18) and the
cutting features 14 are both formed from consolidated or compacted powder material or matrixes. Processes contemplated herein for consolidating powdered materials include high velocity compaction and/or adiabatic processes, available by Utron of Manassas, Va.; Hydropulsor of Karlskoga, Sweden; and LMC of DeKalb, Ill. For example, in the high velocity or adiabatic process, a piston or ram is actuated at very high speed by igniting a gas such as argon. Other processes include field assisted sintering technology (FAST) or spark plasma sintering, in which an up to 300 ton force is applied to powder in a die while pulses of electrical current are passed through the powder to create extremely high localized temperatures between powdered particles. Another process is disclosed in U.S. Pat. No. 4,539,175, which patent is hereby incorporated by reference, in which a preform is first made by at least partially consolidating powder in a first die, moving the preform into a second die containing a bed of heated ceramic particles, and then compressing the particles to solidify the powder with a hydraulic ram or the like to full density or near full density. - In any of these processes, the powder is first layered in a die and then subjected to pressure, heat, etc. For example, a
die 20 and aram 22 is shown inFIG. 2 having powdered material ormatrix 12′ and 14′ layered therein. The prime symbol is used to identify the powdered material or matrix that form the elements having the corresponding numeral without the prime symbol (e.g., thematerial 14′ forms thecutting features 14, thematerial 12′ forms thebase 12 with the neck 18).Inserts 24 may be included for formation of thewatercourses 16 in thebase 12. - By layering the
base material 12′ and thecutting feature material 14′ in the die 20, simultaneous consolidation is possible. Additionally and also simultaneously with the consolidation of thematerials 12′ and 14′, the heat and/or pressure of the consolidation process bonds thecutting features 14 to thebase 12. Advantageously, the need to perform a separate bonding operation is avoided by layering the two materials in the same die, saving time and manufacturing cost. Further, not having to perform a separate bonding operation avoids the cracking issues of prior systems because additional machining to the tool, such as to form watercourses, and the application of very high temperatures to the tool, such as to wet braze cutting material to the base of the tool at temperatures approaching 1900° F., can be avoided. Of course, one could grind or machine watercourses into thebase 12 after consolidation, if desired, and this would still avoid the need for a separate bonding operation. - Although heat and pressure is applied to the
tool 10, this heat and pressure is applied only to the powdered materials or matrixes and is required to consolidate thepowders 12′ and 14′. In fact, when in powdered or matrix form, high temperatures can be desired for the creation of high density parts. Importantly, the heat is applied only during consolidation, not after the part is formed, such as prior cast tools that tend to crack from subsequent applications of heat. Additionally, the increased strength obtainable by simultaneously bonding and consolidating the components of thetool 10 avoids the need for welded support members, which were previously used and resulted in prior tools being subjected to even more heat. As a result, cracking will not readily occur according to the current invention, and instead, a single, bonded, and fully dense part is produced. - In one embodiment, the
matrix 14′ that forms thecutting features 14 comprises a polymeric or metallic composition of, for example, nickel, copper, iron, cobalt, or some other material exhibiting suitable bonding and strength qualities, having an embedded cutting material therein, which is one or more hard particulate materials such as tungsten carbide, cubic boron nitride, diamond, silicon carbide and combinations including at least one of the foregoing and other similar materials mixed therein before the matrix is cured. The mixture in one embodiment will be homogenous while in other embodiments the cutting materials mixed into the matrix may be concentrated in certain areas to affect mechanical properties (strength, wear resistance, wear pattern, etc.) of thecutting features 14 of thecutting tool 10. One embodiment utilizes a matrix material that is proprietary to and commercially available from Protech Centerform Inc, Houston, Tex. In one embodiment, thebase material 12′ is a powdered steel such that thebase 12 can be welded or threaded onto a shoe casing or the like. - While the invention has been described with reference to an exemplary embodiment or embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof Therefore, it is intended that the invention not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this invention, but that the invention will include all embodiments falling within the scope of the claims. Also, in the drawings and the description, there have been disclosed exemplary embodiments of the invention and, although specific terms may have been employed, they are unless otherwise stated used in a generic and descriptive sense only and not for purposes of limitation, the scope of the invention therefore not being so limited. Moreover, the use of the terms first, second, etc. do not denote any order or importance, but rather the terms first, second, etc. are used to distinguish one element from another. Furthermore, the use of the terms a, an, etc. do not denote a limitation of quantity, but rather denote the presence of at least one of the referenced item.
Claims (10)
1. A downhole cutting tool comprising:
a base including a first consolidated powder; and
at least one cutting feature affixed to the base, the at least one cutting feature including a cutting material suspended in a second consolidated powder, wherein the base and the at least one cutting feature are both consolidated and bonded together simultaneously.
2. The cutting tool of claim 1 , wherein the first consolidated powder comprises steel.
3. The cutting tool of claim 1 , wherein the second consolidated powder comprises nickel, copper, iron, cobalt, or combinations including at least one of the foregoing.
4. The cutting tool of claim 1 , wherein the cutting material comprises tungsten carbide, cubic boron nitride, diamond, silicon carbide, or combinations including at least one of the foregoing.
5. The cutting tool of claim 1 , further including at least one watercourse proximate the at least one cutting feature.
6. A method of manufacturing a cutting tool comprising:
layering a first powder and a second powder in a die, the second powder comprising cutting material suspended therein; and
simultaneously consolidating the first and second powders to form a base and at least one cutting feature, respectively, the simultaneous consolidating also bonding the base to the at least one cutting feature.
7. The method of claim 6 , wherein the first powder comprises steel.
8. The method of claim 6 , wherein the second powder comprises nickel, copper, iron, cobalt, or combinations including at least one of the foregoing.
9. The method of claim 6 , wherein the cutting material comprises tungsten carbide, cubic boron nitride, diamond, silicon carbide, or combinations including at least one of the foregoing.
10. A tool manufactured by the process of claim 6 .
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/179,997 US20130014998A1 (en) | 2011-07-11 | 2011-07-11 | Downhole cutting tool and method |
BR112014000439A BR112014000439A2 (en) | 2011-07-11 | 2012-06-29 | downhole cutting tool and method |
CA2839718A CA2839718A1 (en) | 2011-07-11 | 2012-06-29 | Downhole cutting tool and method |
PCT/US2012/044866 WO2013009496A2 (en) | 2011-07-11 | 2012-06-29 | Downhole cutting tool and method |
EP20120810677 EP2732122A4 (en) | 2011-07-11 | 2012-06-29 | Downhole cutting tool and method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/179,997 US20130014998A1 (en) | 2011-07-11 | 2011-07-11 | Downhole cutting tool and method |
Publications (1)
Publication Number | Publication Date |
---|---|
US20130014998A1 true US20130014998A1 (en) | 2013-01-17 |
Family
ID=47506797
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US13/179,997 Abandoned US20130014998A1 (en) | 2011-07-11 | 2011-07-11 | Downhole cutting tool and method |
Country Status (5)
Country | Link |
---|---|
US (1) | US20130014998A1 (en) |
EP (1) | EP2732122A4 (en) |
BR (1) | BR112014000439A2 (en) |
CA (1) | CA2839718A1 (en) |
WO (1) | WO2013009496A2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10385638B2 (en) | 2014-12-23 | 2019-08-20 | Ga Drilling, A.S. | Method of removing materials by their disintegration by action of electric plasma |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4554986A (en) * | 1983-07-05 | 1985-11-26 | Reed Rock Bit Company | Rotary drill bit having drag cutting elements |
US20090293672A1 (en) * | 2008-06-02 | 2009-12-03 | Tdy Industries, Inc. | Cemented carbide - metallic alloy composites |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4368788A (en) * | 1980-09-10 | 1983-01-18 | Reed Rock Bit Company | Metal cutting tools utilizing gradient composites |
US4554130A (en) * | 1984-10-01 | 1985-11-19 | Cdp, Ltd. | Consolidation of a part from separate metallic components |
US7513320B2 (en) * | 2004-12-16 | 2009-04-07 | Tdy Industries, Inc. | Cemented carbide inserts for earth-boring bits |
US7776256B2 (en) * | 2005-11-10 | 2010-08-17 | Baker Huges Incorporated | Earth-boring rotary drill bits and methods of manufacturing earth-boring rotary drill bits having particle-matrix composite bit bodies |
US7628228B2 (en) * | 2006-12-14 | 2009-12-08 | Longyear Tm, Inc. | Core drill bit with extended crown height |
US20080202814A1 (en) * | 2007-02-23 | 2008-08-28 | Lyons Nicholas J | Earth-boring tools and cutter assemblies having a cutting element co-sintered with a cone structure, methods of using the same |
-
2011
- 2011-07-11 US US13/179,997 patent/US20130014998A1/en not_active Abandoned
-
2012
- 2012-06-29 BR BR112014000439A patent/BR112014000439A2/en not_active IP Right Cessation
- 2012-06-29 EP EP20120810677 patent/EP2732122A4/en not_active Withdrawn
- 2012-06-29 CA CA2839718A patent/CA2839718A1/en not_active Abandoned
- 2012-06-29 WO PCT/US2012/044866 patent/WO2013009496A2/en active Application Filing
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4554986A (en) * | 1983-07-05 | 1985-11-26 | Reed Rock Bit Company | Rotary drill bit having drag cutting elements |
US20090293672A1 (en) * | 2008-06-02 | 2009-12-03 | Tdy Industries, Inc. | Cemented carbide - metallic alloy composites |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10385638B2 (en) | 2014-12-23 | 2019-08-20 | Ga Drilling, A.S. | Method of removing materials by their disintegration by action of electric plasma |
Also Published As
Publication number | Publication date |
---|---|
EP2732122A4 (en) | 2015-03-18 |
WO2013009496A2 (en) | 2013-01-17 |
WO2013009496A3 (en) | 2013-04-11 |
BR112014000439A2 (en) | 2017-02-14 |
EP2732122A2 (en) | 2014-05-21 |
CA2839718A1 (en) | 2013-01-17 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: BAKER HUGHES INCORPORATED, TEXAS Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:LYNDE, GERALD D.;REEL/FRAME:026766/0459 Effective date: 20110811 |
|
STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |