Methods of forming and repairing earth-boring tools including replaceable cutting structures
10107044 ยท 2018-10-23
Assignee
Inventors
- Chaitanya K. Vempati (Conroe, TX)
- Timothy K. Marvel (The Woodlands, TX, US)
- Suresh G. Patel (The Woodlands, TX, US)
Cpc classification
E21B10/62
FIXED CONSTRUCTIONS
Y10T29/49742
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B28B23/005
PERFORMING OPERATIONS; TRANSPORTING
Y10T29/49734
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
Y10T29/49746
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B22F2005/001
PERFORMING OPERATIONS; TRANSPORTING
E21B10/006
FIXED CONSTRUCTIONS
Y10T29/49744
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
Y10T29/49741
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B24D3/06
PERFORMING OPERATIONS; TRANSPORTING
B23K31/025
PERFORMING OPERATIONS; TRANSPORTING
International classification
E21B10/62
FIXED CONSTRUCTIONS
B23K31/02
PERFORMING OPERATIONS; TRANSPORTING
B24D3/06
PERFORMING OPERATIONS; TRANSPORTING
B28B23/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
Methods of forming an earth-boring tool may involve attaching one or more cutting elements to a replaceable cutting structure and positioning the replaceable cutting structure proximate a region of a body of an earth-boring tool that is susceptible to at least one of localized wear and localized impact damage. The replaceable cutting structure may be to the body. Methods of repairing an earth-boring tool may involve bringing a replaceable cutting structure proximate at least one portion of a body of an earth-boring tool exhibiting at least one of localized wear and localized impact damage. The replaceable cutting structure may be attached to the earth-boring tool at the at least one portion.
Claims
1. A method of forming an earth-boring tool, comprising: attaching a plurality of cutting elements to an annular attachment member to form a replaceable cutting structure; positioning the replaceable cutting structure proximate each blade of a plurality of blades at least within a shoulder region of a face of a body of an earth-boring tool that is susceptible to at least one of localized wear and localized impact damage, to cause an exposed surface of the attachment member to be at least substantially flush with exposed surfaces of the body adjacent to the attachment member, and the attachment member to extend contiguously around a circumference of the face of the body at least within the shoulder region; and attaching the replaceable cutting structure to the body.
2. The method of forming an earth-boring tool of claim 1, further comprising positioning the replaceable cutting structure over an outlet in fluid communication with an internal plenum of the body.
3. The method of forming an earth-boring tool of claim 2, wherein the annular attachment member comprises a channel extending at least partially through the annular attachment member and wherein positioning the replaceable cutting structure over the outlet in fluid communication with the internal plenum of the body comprises aligning the channel with the outlet.
4. The method of forming an earth-boring tool of claim 1, wherein attaching the replaceable cutting structure to the body comprises one or more of welding the replaceable cutting structure to the body, brazing the replaceable cutting structure to the body, threadedly engaging the replaceable cutting structure with the body, bolting the replaceable cutting structure to the body, affixing the replaceable cutting structure to the body with pins, affixing the replaceable cutting structure to the body with keys, shrink-fitting the replaceable cutting structure with the body, press-fitting the replaceable cutting structure with the body, and capturing the replaceable cutting structure due to shrinkage of the body during a densification process.
5. The method of forming an earth-boring tool of claim 1, wherein attaching the plurality of cutting elements to the annular attachment member comprises attaching a first cutting element of the plurality to the annular attachment member at a first position relative to a centerline of the body and a second cutting element of the plurality to the annular attachment member at a second position relatively closer to the centerline of the body.
6. The method of forming an earth-boring tool of claim 1, wherein positioning the replaceable cutting structure proximate each blade of the plurality of blades at least within the shoulder region of the face of the body comprises positioning the annular attachment member to extend contiguously around a circumference of the face of the body at least within the shoulder region.
7. The method of forming an earth-boring tool of claim 1, wherein attaching the replaceable cutting structure to the body comprises attaching the annular attachment member to each blade of the plurality of blades.
8. The method of forming an earth-boring tool of claim 1, wherein attaching the plurality of cutting elements to the annular attachment member comprises at least partially embedding a first cutting element of the plurality within the attachment member at a first position relative to a centerline of the body and at least partially embedding a second cutting element of the plurality within the attachment member at a second position relatively closer to the centerline of the body.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) While the specification concludes with claims particularly pointing out and distinctly claiming that which is regarded as the present disclosure, various features and advantages of embodiments of this disclosure may be more readily ascertained from the following description of embodiments of the disclosure when read in conjunction with the accompanying drawings, in which:
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DETAILED DESCRIPTION
(11) Some of the illustrations presented herein are not meant to be actual views of any particular earth-boring tool, cutting element, or replaceable cutting structure, but are merely idealized representations that are employed to describe embodiments of the present disclosure. Additionally, elements common between figures may retain the same or similar numerical designation.
(12) Although some embodiments of the present disclosure are depicted as being used and employed in earth-boring rotary drill bits, such as fixed-cutter rotary drill bits, persons of ordinary skill in the art will understand that replaceable cutting structures in accordance with the present disclosure may be employed with any earth-boring tool. Accordingly, the terms earth-boring tool and earth-boring drill bit, as used herein, mean and include any type of bit or tool used for drilling during the formation or enlargement of a wellbore in a subterranean formation and include, for example, rolling cone bits, core bits, eccentric bits, bicenter bits, reamers, expandable reamers, mills, drag bits, hybrid bits, impregnated bits, and other drilling bits and tools known in the art.
(13) As used herein, the teen cutting element means and includes any structure configured to engage an earth formation including, by way of example and without limitation, tungsten carbide inserts, polycrystalline diamond compact (PDC) cutting elements and inserts, thermally stable polycrystalline (TSP) diamond compact cutting elements, natural diamonds, superabrasive-impregnated elements, and other cutting element materials and structures as known in the art. In addition, cutting elements and cutting faces thereof may include any geometric shape or configuration, such as, for example, cylindrical, dome-shaped, tombstone, chisel-shaped, pyramids, and other shapes and configurations as known in the art.
(14) Referring to
(15) A replaceable cutting structure 12 may be attached to the earth-boring tool 10 at the shoulder region 18. In other embodiments, a replaceable cutting structure may be attached to an earth-boring tool at other locations such as, for example, on the face of a rotary drag bit, on the face of an impregnated bit, on a supporting ring of cutting elements of a roller cone on a rolling cone drill bit. In further embodiments, a replaceable cutting structure may be attached to an earth-boring tool on a formation-engaging portion of a reamer tool, on a region of a hybrid bit susceptible to at least one of localized wear and localized impact damage, or on any other portion of an earth-boring tool that is susceptible to at least one of localized wear and localized impact damage as a result of drilling.
(16) As shown in
(17) The attachment member 26 may comprise at least one cutting element accommodation recess in an underside thereof. At least one cutting element 24 already attached to an earth-boring tool 10 (see
(18) The size of the replaceable cutting structure 12 may correspond to a predicted radially and circumferentially extending region of localized wear occurring on a shoulder region 18 or other region of a body 13 of an earth-boring tool 10 as a result of use of the earth-boring tool 10 in a drilling or reaming operation. The region of localized wear may be predicted using computer modeling, such as, for example, finite element analysis, or by observation of localized wear in the field. Thus, the replaceable cutting structure 12 may be sized to enable easy replacement of a region of a body 13 of an earth-boring tool 10 most susceptible to localized wear and, therefore, most likely to cause premature failure of the earth-boring tool 10. In addition, the replaceable cutting structure 12 may enable replacement of a worn portion of an earth-boring tool with a replaceable cutting structure 12 having increased wear resistance, impact strength, fracture toughness, or any combination of these.
(19) Referring again to
(20) The earth-boring tool 10, itself may comprise at least one cutting element accommodation recess. At least one cutting element 24 attached to an attachment member 26 (see
(21) As shown in
(22) The attachment member 26 may comprise at least one cutting element accommodation recess. At least one cutting element 24 attached to a body 13 of an earth-boring tool 10 (see
(23) As previously noted, size of the replaceable cutting structure 12 may correspond to a predicted region of localized wear on a shoulder region 18 or other region of an earth-boring tool 10. The region of localized wear may be predicted using computer modeling, such as, for example, finite element analysis, or by observation of localized wear in the field. Thus, the replaceable cutting structure 12 may be sized to enable easy replacement of a region of an earth-boring tool 10 most susceptible to localized wear and, therefore, most likely to cause premature failure of the earth-boring tool 10.
(24) Referring to
(25) The earth-boring tool 10 may comprise at least one cutting element accommodation recess. At least one cutting element 24 attached to an attachment member 26 of a replaceable cutting structure 12 (see
(26) Attachment members 26 of replaceable cutting structures 12, such as blade segments 23, may comprise strong, tough, and impact- and abrasion-resistant materials suitable for use in earth-boring applications. For example, an attachment member 26 may comprise a metal or metal alloy, such as, for example, steel, or may comprise a cermet material, such as, for example, sintered tungsten carbide in a matrix material. A hardfacing material may, optionally, be disposed on an exterior portion of the attachment member 26.
(27) Attachment members 26 may be formed by casting a metal part and subsequently machining desired features, such as, for example, attachment surfaces or pockets for receiving cutting elements 24, into the metal part. Alternatively, attachment members 26 may be formed by distributing a plurality of hard particles, such as, for example, tungsten carbide particles, and a plurality of particles comprising a matrix material, such as, for example, copper, copper-based alloys, cobalt, and cobalt-based alloys, in a mold (not shown). In some cases, the matrix material may be melted and infiltrated into the plurality of hard particles. In other cases, the hard particles and particles comprising a matrix material may then be pressed in the mold to form a green part. The hard particles and particles comprising a matrix material may then be subjected to a densification process. For example, the green part may be subjected to heat and pressure to at least partially sinter the green part. The green part may be partially sintered to form a brown part, or may be sintered to a final density. The green, brown, or fully sintered part may also have desired features, such as, for example, attachment surfaces or cutting element 24 pockets, formed therein. Such desired features may be machined, for example, in a green or brown part, or may be molded into an infiltrated part or a fully sintered part. Cutting elements 24 may be attached to the attachment member 26 in pockets formed therein by welding, brazing, shrink-fit, by being captured due to shrinkage of the attachment member 26 during a densification process, or by other means as known in the art. Cutting elements 24 may be attached to the attachment member 26 before or after the attachment member 26 is, itself attached to a body 13 of an earth-boring tool 10.
(28) Replaceable cutting structures 12 may be attached to bodies 13 of earth-boring tools 10. For example, at least one replaceable cutting structure 12 may be attached to a body 13 of an earth-boring tool 10 by welding, by brazing, by shrink-fit, by press-fit, by screws, by bolts, by pins, by keys, by mutually engaging threads on a replaceable cutting structure 12 and a body 13, by being captured due to shrinkage of an earth-boring tool 10 during a densification process, or by other means as known in the art. Alternatively, at least one preformed replaceable cutting structure 12 may be placed in a mold. The body 13 of an earth-boring tool 10 may then be cast in the mold around the replaceable cutting structure 12, thereby attaching it to the body 13 of the earth-boring tool 10.
(29) In operation, a replaceable cutting structure 12 may be subjected to greater wear than other regions of an earth-boring tool 10 during a drilling or reaming operation, resulting in localized wear of the replaceable cutting structure 12. For example, as a rotary drag bit rotates in a borehole and engages the underlying earth formation, the combination of abrasive wear, impact forces, and vibrations may cause the replaceable cutting structure 12 to wear down more quickly than other portions and features of the earth-boring tool 10, such as, for example, other portions of the face 14, and the gage region 16. When an operator determines that the replaceable cutting structure 12 has worn down to a selected extent, or when the bit ceases to drill an underlying earth formation at an acceptable rate in the borehole, the earth-boring tool 10 may be extracted from the borehole. The body 13 of the bit and remaining portions of the replaceable cutting structure 12 may be machined to return a seat 28 at a shoulder region 18 of the body 13 to a geometry it exhibited prior to being deployed in the borehole or to a new, selected geometry. Another replaceable cutting structure 12 may then be attached to the body 13, and the earth-boring tool 10 redeployed in the borehole or deployed in another borehole. Therefore, replaceable cutting structures 12 may increase the useful life of an earth-boring tool 10 by enabling replacement of the region most susceptible to localized wear and, therefore, most likely to cause premature failure of the earth-boring tool 10.
(30) An earth-boring tool 10 may comprise one or more failure detection features. Referring to
(31) As shown in
(32) Referring to
(33) While the present disclosure has been described herein with respect to certain embodiments, those of ordinary skill in the art will recognize and appreciate that it is not so limited. Rather, many additions, deletions, and modifications to the embodiments described herein may be made without departing from the scope of the disclosure as hereinafter claimed, including legal equivalents. In addition, features from one embodiment may be combined with features of another embodiment while still being encompassed within the scope of the disclosure as contemplated by the inventors.