GB2409209A

GB2409209A - A braze alloy, down hole cutting tool and a method of manufacture of said tool

Info

Publication number: GB2409209A
Application number: GB0426395A
Authority: GB
Inventors: Kumar T Kembaiyan
Original assignee: Smith International Inc
Current assignee: Smith International Inc
Priority date: 2003-12-12
Filing date: 2004-12-01
Publication date: 2005-06-22
Anticipated expiration: 2024-12-01
Also published as: GB2409209B; GB0426395D0; US20050089440A1

Abstract

A down hole cutting tool (figure 1, 10) and associated method of manufacture are described. The cutting tool (figure 1, 10) possesses a cutting element support structure 16 with at least one cavity 26, and a cutting element 20 disposed in said cavity 26. A braze alloy 28 is used to secure the cutting element 20 in the cavity 26. The braze alloy 28 is characterised in that it contains Ga, In, or Tl. An embodiment of the braze alloy comprises, in weight percent: 40-60 Ag, 10-40 Cu, 6-30 Zn, 2-10 Sn with at least one of 0.5-10 Ga, 0.5-10 Tl, 0.5-10 In; other elements may be present in trace amounts.

Description

A BRAZE ALLOY, A DOWN HOLE CUTTING TOOL AND A METHOD FOR

MANUFACTURING A DOWN HOLE CUTTING TOOL

The present invention relates to a braze alloy, a down hole cutting tool and a method for manufacturing a down hole cutting tool.

In embodiments, the present invention relates to a braze alloy and to the use of braze alloys in the manufacture of drilling tools for drilling bore holes in earth formations.

1() More particularly, in embodiments, the present invention relates to a braze alloy having alloying elements added to reduce braze temperature and/or increase braze strength. In embodiments, the invention also provides drilling tools and methods for manufacturing drilling tools which include the use of a new braze alloy for brazing cutting elements in drilling tool applications, especially cutting elements including ultrahard material, such as polycrystalline diamond.

2() Earth boring tools, and in particular drill bits, are commonly used in the oil and gas industry for drilling well bores. Figure 1 StlOWS one example of a conventional drilling system for drilling through earth formation. Ihe drilling system includes a drilling rig 1 used to turn a drill string > '0 which extends downward into a well bore 4. Connected to the end of the drill string 2 is a drill bit 6.

Drill bits used for drilling well bores include roller cone drill bits and fixed cutter drill bits. Roller cone drill bits typically include a bit body with an externally breaded connection at one end, and a plurality of roller cones (typically three) rotatably attached to the other end.

Attached to the cones of the bit is a plurality of cuttin elements typically arranged in rows about the surface of the cones. The cutting elements may he inserts or milled steel teeth. Inserts are typically press-fitted into cavities (or pockets) formed in the surface of the roller cones. In certain applications, a hard surface layer or cap can be brazed onto the milled tooth cones of the roller cone bits.

1() The inserts may include a layer of ultrahard material disposed thereon. Ultral-ard material may be bonded to a substrate of the insert in a high temperature high pressure process known in the art.

Fixed cutter drill bits typically include a bit body having a threaded connection at one end and a plurality of cutting elements mounted at the other. The cutting elements are typically mounted in cavities formed around the bit body.

Tn many drill bit designs, these cavities are arranged on blades formed on the bit body to accommodate the placement of the cutting elements on the drill bit. The cutting elements are brazed in the cavities by a braze alloy. The cutting elements typically are compacts which include an ultrahard material, such as polycrystalline diamond (PCD), bonded to a substrate. Ultrahard material may alternatively or additionally include material such as polycrystalline cubic boron nitride (PCBN) or polycrystalline carbonitride (PCN).

Other tools used during drilling operations may also 3() include cutting elements which include ultrahard material, such as polycrystalline diamond or diamond containing material. These tools include other drill bits, reaming tools, fishing tools, milling tools, to name a few.

In general, cutting elements having ultrahard material, in particular diamond containing material, thereon must be brazed at temperatures below 1400 F (about 760 C), and more preferably below 1350 F (about 730"C), to avoid the onset of damage to the ultrahard material. This temperature restriction greatly limits the number of alloys that can be 1() used as braze alloy for cutting elements with ultrahard material because most brazing alloys that provide sufficient shear strength for bonding cutting elements to a drill bit also require brazing at temperatures above 1350 F (about 730"C). Therefore, alloys suitable for brazing cutting elements with ultrahard material thereon have been limited to only a couple of alloys which offer]ow enough brazing temperatures to avoid damage to the ultrahard layer and high enough braze strength to retain cutting elements on drill bits. These alloys generally require brazing temperatures close to or at 1350 F (about 730"C).

Brazing at high temperatures, such as around 1350 F (about 730C) has also been found to result in a build up of residual stresses in the ultrahard material which can increase the chances of cutting elements cracking and chipping during drilling. Residual stresses occur primarily clue to difference in the coefficient of thermal expansion and differences in thermal conductivity of the diamond and the catalytic material used to form a polycrystalline diamond 3() compact (or other diamond containing component). In addition to the residual stresses, polycrystalline diamond has a tendency to gradually revert back to carbon (graphite), which is accelerated at higher temperatures. As a result, cutters brazed at higher temperatures typically have a higher chance of cracking and chipping in the field because of the higher stresses developed due tc> exposure to brazing temperatures.

Therefore, a braze alloy that can be used to braze cutting elements at a reduced brazing temperature is desired.

Additionally, in some drill bit designs, the bond formed 1() between the cutting elements and the cutting element support structure (e.g., blades, cones, bit body surface, etc.) may be the weak link in the bit design. This is a primary reason for cutting element loss, which can result in over loading of adjacent cutting elements which can lead to premature failure 1'-' of the bit. Additionally, when a cutting element falls out of its support structure on the bit, the fallen cutting element may get jammed against the bit, causing further bit damage and acceleratinc3 the premature failure of the bit.

Accordingly, there is also a desire for a braze alloy 2() offering increased braze strength to reduce the risk of cutter loss in some drill bit designs and, in some cases, to allow for the development of more aggressive drill bit designs.

?5 According to a first aspect of the present invention, there is provided a down hole cutting tool, comprising: a cutting element support structure having at least one cavity formed therein; a cutting element having a base portion disposed in the cavity; a braze alloy disposed in the cavity between the cutting element and the cutting element support structure, the braze alloy comprising between about 0.5 O and about 10% by weight of at least one selected from the group of gallium (Ga), indium (In),thallium ('1'1).

Preferably, the tool comprises a drill bit for drilling through earth formations.

According to a second aspect of the present invention, there is provided a method for manufacturing a down hole cutting tool, the cutting tool including a cutting element 1() support structure having at least one cavity formed thereon to support a cutting clement, the method comprising: inserting a base portion of the cutting element into the cavity; locating a braze alloy such that when heated the braze alloy melts and fills a space ire the cavity between the l':, culling element and the cutting element support structure, the braze alloy comprising about 0.5<' to about 10!!, by weight of at least one selected from the group of gallium (Ga), indium (In), thallium (Tl); and heating the braze alloy such that it melts. 2()

Preferably, Rho tool comprises a drill bit for drilling through earth formations.

According to a third aspect of the present invention, there is provided a braze alloy, comprising: at least one selected from the group of indium (In) and thallium (Tl).

The present invention provides a braze alloy that includes indium and/or thallium. In one aspect, a braze N() alloy comprises at least about 0.5''; to about 10'-.; by weight of at least one selected frog the group of indium (In) and thallium (Tl). In one or more embodiments, the braze alloy is used to braze cutting elements in a drilling tool. In one or more embodiments the cutting element comprises a polycrystalline diamond (PCD), polycrystalline cubic boron nitride (PCBN), diamond or a diamond like carbon (DLC) material.

In are embodiment, the present invention also provides a method for manufacturing a down hole cutting tool. In one l() aspect, the drilling tool includes a cutting element support structure. The cutting element support structure has at least one cavity formed therein to support a cutting element.

The method includes placing a cutting element in the cavity and locating braze alloy such that when heated the braze l5 alloy melts and fills a space in the cavity between the cutting element and the cutting element support structure.

The braze alloy has a composition that includes about 0.5% to about 10% by weight of at least one selected from the group of gallium (Ga), indium (In), and thallium (Tl). The method further comprises heating the braze alloy such that it melts.

In one or more embodiments, the method may also include cooling tile braze alloy to form a bond between the cutting element and the cutting element support structure. in one or more embodiments, the drilling tool is an earth boring drill bit for drilling through earth formations. In one or more embodiments the cutting element comprises a polycrystalline diamond (PCD), polycrystalline cubic boron nitride (PCBN), diamond or a diamond like carbon (DLC) material.

Ire an embodiment, the present invention also provides a drilling tool. In one aspect, the drilling tool a cutting element support structure having at least one cavity formed therein. A cutting element is disposed in the cavity. Braze alloy is disposed in the cavity between the cutting element and surfaces of the cutting element support structure. The braze alloy comprises between about 0.5% and about 10% b weight of at least one selected from the Group of gallium (Ga), indium (Tn) and thallium (Tl). In one or more embodiments, the drilling tool is a drill bit. In one or more embodiments the cutting element comprises polycrystalline diamond (PCD) or a diamond like material.

Examples of the present invention will now be described in detail with reference to the accompanying drawings, in which: 1 i, Figure 1 shows one example of a conventional drilling system used for drilling bore holes in earth formations.

Figure 2 shows a perspective view of a fixed cutter drill bit.

Figure 3 shows a perspective view of a roller cone drill hit.

Figure 4 shows a perspective view of one example of a PCD cutter for a fixed cutter drill bit.

Figure 5 shows a perspective view of a cavity formed on a fixed cutter drill bit with braze alloy along a surface 3() thereof and a PCD cutter positioned to be placed in the cavity for attachment to the cutting element support structure by brazing.

Figure 6 shows a cross-sectional view of a cutter brazed in a cavity of a drill hit in accordance with an embodiment of the present invention.

Figure 7 shows a cross sectional view of an insert brazed into the cavity of a drill bit in accordance with an 1() embodiment of the present invention.

In embodiments, the present invention provides a braze alloy that includes one or more alloying elements to reduce braze temperature. In some embodiments, the alloying lo elements may also increase braze strength. Braze alloys in accordance with one or more embodiments of the invention may be used in drilling tool applications, such as for brazing cutting elements in a drilling tool, as described below. In some embodiments the present invention also provides down () hole cutting tools and methods for manufacturing down hole cutting tools which include the use of an improved braze alloy that has been shown to be useful in drilling tool applications.

A braze alloy in accordance with one embodiment of the present invention includes about 0.5 wit to about 10 wt ; at least one selected from the group of gallium (Ga), indium (Tn), and/or thallium ('hi), or any combination thereof. The inventor has determined that the addition of one or more combinations of the above alloying elements can result in an improved braze alloy. The braze alloy may be used for brazing cutting elements of drill bits, especially for cutting elements that include ultrahard material thereon. In particular, these alloying elements may be used to lower braze temperature and/or increase braze strength of alloys used for drill bit applications compared to conventional braze alloys.

In another embodiment, the present invention provides a down hole cutting tool which includes a braze alloy comprising between about 0.5 ,, and about 10 o by weight of at least one element selected from the group of gallium (Ga), indium (In), and thallium (T1), or any combination thereof.

The braze alloy may be used to braze cutting elements to a cutting element support structure (e.g., cutting face, blades, cones, etc.) of a drilling tool. The drilling tool may include a tool body with a cutting element support structure connected to or integrally formed with the tool body. The tool may comprise a drill bit for drilling through earth formations, such as a fixed cutter drill, roller cone () drill bit, or a hammer bit. In other ermbodirnents, the tool may comprise a reaming tool, a fishing tool, milling tool, hole opener, or similar tool. Because embodiments of the invention may include any type of tool used in drilling operations, how the cutting element support structure is -' connected to or configured with the tool body is not intended as a limitation on the ir-rvcrltior-r.

In accordance with one or more embodiments of the invention, a cutting element support structure includes at 3() least one cavity (e.g., pocket or recessed portion) formed in the cutting element support structure and adapted to accept a base portion of a cutting element therein. The cutting element may include ultrahard material, such as any material c-omposition involving diamond.

When a drilling tool is assembled, the base portion of the cutting element is located in the cavity of tile cutting element support structure and may be bonded or attached to the cutting element support structure by brazing. The brazing can be accomplished by placing a braze alloy in the l() cavity of the cutting element support structure between surfaces of the cavity and the base of a cutting element positioned (or to be positioned) therein. In some cases the brazing material may be placed in the cavity before the cutting element is positioned in the cavity. In other cases l': the cutting element may be placed in the cavity and the brazing material positioned in or located near the cavity such that when the brazing material is heated it melts and flows into the cavity between the cutting element and surfaces of the cavity. Heat is applied to the assembly and 2() braze alloy to melt the braze alloy. During the heating process, the cutting element may be rotated to eliminate trapped gas pockets, inclusions, or voids and to ensure a complete, uniform coating of braze alloy between the cutting element and the cavity surfaces. The braze alloy is then cooled to form a bond between tile cutting element and the cutting element support structure.

Example embodiments of drilling tools formed using a braze material as set forth above will now be described with 3() respect to the attached figures, wherein similar reference characters are used for similar parts throughout the views for simplicity.

Figure 2 shows an earth boring drill bit 10, which r5 comprises a fixed cutter drill bit. The drill bit JO includes a bit body 12. The bit body 12 may be formed of a matrix material, such as a tungsten carbide powder infiltrated with an alloy binder material, or may be a mact-lned steel body. The bit body 12 includes a threaded l(l connection 14 at one end for coupling the bit 10 to a drilling string assembly (not shown). The bit body 12 also includes a cutting element support structure which, in this example, comprises a pl urality of blades 16. The blades 16 are radially arranged and extend outward at the other end of the bit body 12. Each of the blades 16 includes a plurality of cavities (26 in Figures 5 and 6) formed therein along the periphery to accept and support a base of a cutting element therein.

The cutting elements in this example comprise polycrystalline diamond or diamond like compact cutters, which are hereafter be referred to as "PDC cutters" or "cutters" 20. A perspective view of a cutter 20 is shown for example in Figure 4. Figure 5, is an illustration of a cutter 20 to be inserted into a cavity 26 of a drill bit, wherein braze alloy 28 is disposed along the surface of the cavity 26. Figure 6 shows a partial cross-sectional view of a cutter 20 brazed in a cavity 26 of a drill bit blade 16.

As illustrated in Figures 4-6, a base portion of the cutter 8() 20 is inserted in the cavity 26 of the blade 16 and fixed Iherein by brazing (braze alloy 28). In this example, the braze alloy 28 comprises between about 0.5 6 and about 10 o by weight of at least one selected from the group of gallium (Ga), indium (In), and thallium (Tl), or any combination thereof. As shown in Figure 2, the PDC cutters 20 are arranged to extend along the periphery of each of the blades 16 so that they engage with earth formation when the drill bitt 10 is positioned on a bottom of a bore hole and rotated under an applied weight on bit.

In general, polycrystalline diamond or diamond like compacts have been used in industrial applications including rock drilling and metal machining for many years. Referring to Figure 4, typically, ire these applications, a compact of ultrahard material 22, such as polycrystalline diamond ("PCD"), is bonded to a substrate material 24 to form a cutter 20. The substrate material is typically a sistered metal-carbide, such as a tungsten carbide sistered with a cobalt binder. Tile ultrahard material 22 bonded to the substrate 24 sometimes referred to as a diamond table. The substrate 24 and ultrahard material 22 together form the PDC cutter 20. Methods for making diamond and composite compacts are described, for example in U.S. Patent Nos. 3,745,623; 3,609,818; 3,850,591; 4,394,170; 4,403,015; 4,525,178; and 4,647546; and 4,954,139. Onc example of a prior art brazing method for drill bits is disclosed in U.S. Pat. No. 4,45.3,605, to Short., Jr, which is incorporated herein by reference.

Cutting elements comprising ultrahard material may also ]() be used on other types of drilling tools, such as roller cone drill bits, r-earning tools, fishing tools, stabilizer blades, milling tools, and hole openers. For example, as shown in Figure 3, a drill bit 30 may comprise a roller cone bit which includes a bit body 32. The bit body 32 may be formed of any suitable material sects as matrix material or machined steel.

the bit body 32 includes a threaded connection 34 at one end for coupling the bit 30 to a drilling string assembly (not shown), and a plurality of legs 35 extending from the other end. The cutting element support structure in this example comprises a plurality of roller cones 36 which are rotatably 1() mounted to a cantilever jourr-ral (not shown) extending from each of the legs 35. Each cf the roller cones 36 includes a plurality of cavities (not shown) formed its conical surface.

Fach cavity is adapted to accept and support a base of a cutting element therein. L5

In the example shown, the cutting elements comprise inserts 40. As shown in Figure 7, an insert include a substrate 44 having a layer of ultrahard material 42 disposed thereon. The ultrahard material 42 may comprise 2() polycrystalline diamond ("PCD"). The substrate 44 may be formed of any suitable material, such as tungsten carbide sistered with a cobalt binder. The insert in Figure 7 is shown mounted in the cavity 46 of a roller cone 36 arty fixed therein by brazing (braze alloy 48). The braze alloy 48 2'> comprises between about 0.5'0 and about 10' by weight of at least one selected from the group of gallium (Ca), indium (In), and thallium (Tl), or any combination thereof.

As shown in Figure 3, tie inserts 40 are arranged to N() extend from the surface of each cone 36 so that they engage with earth formation when the drill bit 30 is placed on the bottom of a bore hole and rotated under an applied weight on bit. The drill bit 30 is designed such that when the inserts on the cones 36 contact earth formation at on the bottom of a bore hole and the bit 30 is rotated, the cones 36 roll around the bottom of the bore hole forcing the inserts 40 to crush and gouge earth formation as the roller cones 36 rotate.

As previously stated, once a cutting element having a layer of ultrahard material, in particular a diamond containing material, is formed, the cutting element's exposure to high temperatures, especially temperatures above about 1350 F should be avoided to prevent damage to the ultrahard material and to minimize the build up of residual l'> stresses that can develop.

One conventional braze alloy commercially used for i:'razing cutting elements in drilling tool applications is known by the trade name "BAg-." It is also referred by the SAE/ASTM Unified Numberir-g System (UNS) for metals and alloy by the number 'P07450'. BAg-1 has a typical composition of 44-46 6 silver (Ag), 14-16 , copper (Cu), 14-18'-: zinc (Zn), and ?3-25 <i cadmium (Cd). BAg-1 was originally the favored braze alloy in the industry because it offered sufficient braze strength (at the time) at the lowest brazing temperature, which was typically between 1250- 1300 F (675-700 C).

However, this alloy was later declared environmentally unfriendly because it contained cadmium, which was determined to be carcinogenic. As a result, the use of BAg-1 and other () cadmium containing alloys was prohibited in many countries.

This led to an industry wide shift to a braze alloy known by the trade name "BAg-7" (UNS number P07563), which is now considered the braze alloy of choice for many drill bit manufacturing applications.

r' BAg-7 has a typical composition of 55-57 O silver (Ag), 21-23'i copper (Cu), 15-19'c zinc (Zn), and 4.5-5.5-3O tin (So).

Although Bag-7 has a higher brazing temperature than BAg-1, is currently widely favored and used because it is cadmium- free and has the lowest brazing temperature, good braze 1() strength, good wetting and flow of all of the cadmium-free alloys used for brazing. BAg-7 is typically used for brazing cutters with ultrahard material at temperatures of around 1350 F (730 C). BAg-7 is currently commercially available from braze alloy suppliers, such as Bellman-Melcor, Inc. Because the brazing temperature required for BAg-7 is very close to temperatures that cause damage to ultrahard material, brazing must be per-formed at precise temperatures when brazing cutting elements with ultrahard material to () avoid damaging the ultrahard material. Additionally, because brazing at higher temperatures can result in a build up of higher stresses that may lead to early failure of cutting element due to cracking, chipping, or delamination, a braze alloy that can be Eased to br-azc cutting elements at lower 2'-' temperatures is desired.

There is also a growing desire for braze alloy that <:'fEcrs increased braze strength so that longer lasting drill bits and drill bits with more aggressive cutting structures, () car- be developed. Tile retch of penetration (ROP) achievable by a drill bit can be increased by providing drill bits that have more aggressive cutting structure designs, such as more aggressive cutting profiles. Particularly, in the case of fixed cutter bits, this may translate to more cutters on the hit, with the cutters arranged and oriented at more aggressive angles to gouge and break up more formation with each rotation of the bit. More aggressive cutting structures may be achieved by reducing the area available for brazing cutting elements to a cutting element support structure.

Because braze strength is generally a function of braze alloy 1() strength and braze area, reducing the braze area typically will result in a reduction in braze strength unless a braze alloy having a higher yield or shear strength is used.

In particular, rig rates are very expensive. Thus, time I r) saved by drilling a well at a faster rate can result in large savings in the drilling operation. Well bores can be drilled at faster rates by, for example, using drill hits that achieve higher rates of penetration (ROP) and/or by using drill bits that last longer and, thus, can he used to drill 2() longer segments of the well before being pulled to the surface for repair or replacement.

In general, the strength of an alloy may be increased by adding particular alloying elerneTIts to the alloy. However, 2: conventional alloying elements typically added to a braze alloy to increase braze strength will also result in an increase in the melting point of the braze alloy, which means a higher brazing temperature. In brazing cutting elements with ultrahard material, higher brazing temperature may 3() result in thermal damage to the ultrahard material.

Additionally, alloyir-rg elements typically used to decrease brazing temperature often result in a decrease in braze strength. As a result, braze alloys containing alloying elements other than those currently being used in standard alloys considered acceptable for drilling applications are r) typically not embraced as acceptable braze alloy alternatives.

Embodiments of the present invention provide drill bits and methods for brazing cutting elements, especially for temperature sensitive applications, that involve a braze alloy alloyed to contain one or more alloying elements that can be added to, advantageously, reduce brazing temperature arid, in some examples, increased braze strength compared to conventional braze alloys used in drill bit applications that do not include these alloying elements.

In one embodiment, a method for brazing a cutting element to a drill bit includes placing braze alloy into a cavity of a cutting element support structure of the drill A) bit. The braze alloy includes about 0.5% to about 10% by weight of at least one selected from the group of gallium (Ga), indium (In), thallium (T1). The method also includes inserting at least a portion the cutting element into the cavity. The method further includes heating the braze alloy ?5 such that it melts between the cutting element and the cavity, and cooling the braze alloy to form a bond between tic cutting element and the cutting element support structure.

:() In accordance with the above method, gallium (Ga), indium (In), and/or thallium (T1) may be added to conventional braze alloys used for drill bit applications to decrease the temperature required for brazing, and in some cases to also increase the resulting braze strength-. Using a braze alloy as described above for drill bit applications may advantageously allow for the development of more aggressive drill bit designs.

In addition to the above elements, a braze alloy used in accordance with one or more embodiments of the invention may 1() also include silver, copper, tin, and/or zinc. Braze alloys used for brazing cutting elements with ultrahard material thereon, typically includes at least 40':, by weight silver (Ag). The braze alloy may include at least about lOto by weight copper (Cu). The braze alloy may include at least 1'> about 6?, by weight zinc (Zn). The braze alloy may include at least about 2'c; by weight tin (Sn). In some embodiments, the braze alloy includes between about 40 wt.?; to about 60 wt"i silver, about 10 at i; to about 40 wt. '2, copper, about 6 wt%i to about 30 wt% zinc, and about 2 : to about 10?tin.

As stated above, braze alloy in accordance with embodiments of the present invention will also include about 0.5 at% to about:10 wt'', at least one selected from the group of gallium (Ga), indium (In), and/or thallium (T1), or any combination thereof. In some embodiments, the amount of the al least one selected from the group of gallium (Ga), indium (fn), and thallium (T1), or any combination thereof will be between about It and aoout 8% by weight. In particular embodiment, the amount may be betweenabout 2'', and about 5 'O. ]8

In one embodiment, the braze alloy that is used comprises around 3" of at least one solocted from the group of gallium (Ga), indium (in), and thallium (Tl); and around 56'', by weight silver, around 19% by weight copper, around l7 :i by weight zinc, and around 5'i by weight tin. In a particular embodiment, the at least one selected comprises gallium (Ga).

In other embodiments, the at least one selected indium (In) or thallium (Tl).

The addition of one or any combination of the above alloying elements may result in an improved braze alloy for brazing cutting elements of drill bits, especially for cutting elements that include ultrahard material thereon.

For example, in one embodiment, a conventional silver based braze alloy, such as BAg-7, alloyed to decrease its braze temperature and increase its braze strength by adding one or more elements selected from the group of gallium (Ga), indium (In), and thallium (Tl) may be used to braze PDC cutters to a fixed cutter dri11 bit. These elements can he added in any combination totaling between about 0.5 , and about 10% by weight. Advantageously, adding one or more of these elements to the composition of the braze alloy may result in a braze alloy with a lower braze temperature than the conventional braze alloy, BAg-7. By providing a braz alloy that can be used to braze cutting elements a brazing temperature lower than that of the conventional braze alloy, can advantageously reduce the residual stresses developed in the ultrahard material of the cutting clement during brazing.

This may also result in a braze alloy having an increased braze strength over the conventional material. 1 9

Embodiments of the invention may also include braze alloys previously considered to be outside of the temperature range acceptable for brazing cutting elements with ultrahard material thereon. These braze alloys may be alloyed by adding between about 0.5' and about 10': of at least one clement selected from the group of gallium (Ga), indium (In), and/or thallium (T1), or any combination thereof to lower their braze temperature to a temperature more acceptable for 1() Ihcsc brazing applications.

Also, in one or more embodiments, braze alloys used in accordance with the descriptions above may contain small quantities of other elements, such as iron, silicon, phosphorous, sulfur, platinum, palladium, lead, gold, aluminum, magnesium, germanium, carbon, and oxygen. These elements may be present in trace amounts.

Referring to Figures 5 and 6, a braze alloy 28 in 2() accordance with one of the above descriptions can be used to braze a cutter 20 in a cavity 26 of a drill bit (for example, in Figure 2). In this application, the braze alloy 28 is disposed between the surfaces of the cavity 26 and the substrate 24 of the cutter 20. Tile drill bit assembly is then preheated in a furnace and then additional heat is applied, such as by means of oxyacetylene torch, to the braze alloy 28 to melt tics braze alloy 28 between the cutter 20 and the cutter cavity 26. Alternatively, the bit can be heated in a furnace along with the braze alloy in a controlled atmosphere. The bit is then removed and the braze alloy 28 is allowed to cool and solidify to form a metallurgical bond with the cutter 20 to the cavity 26. Cooling may be enhanced, such as by using fans, cooling fluid in contact with the bit body, or other cooling equipment. The result is a drill bit comprising a cutting element support structure rim having at least one cavity formed thereon for accepting a base portion of a cutting element. Braze alloy having a composition in accordance with are embodiment above is disposed in the at least one cavity between the base portion of the cutting element at the cavity surfaces of the cutting l() element support structure.

A suitable braze alloy can be obtained from the company l)egussa Lottechnik of Germany, and sold under the trade name "BrazeTec 5662." BrazeTec 5662 generally includes about 56% l5 by weight silver, about I 9't?, by weight copper, about 17 6 by weight zinc, about 5'6 by weight tin, and about 3QO by weight gallium. This braze alloy is primarily considered for automotive, electrical and tooling applications. The braze alloy has not beer- sold or marketed for drill bit applications because it was not considered a successful option until identified by the inventor and tested to support the inventor's conclusion on acceptable alloying materials lowering braze temperature wit-out sacrificing tine braze strength and material properties required in a braze alloy 2?5 used for drill bit applications. Based on tests ?perforrned using BrazeTec 5662, it has been determined that in accordance with embodiments of the present invention this material can be used as a good alternative braze alloy and offers some preferred brazing characteristics, such as lower 3() braze temperature and higher shear strength when used to braze cutting elements of drill bits compared to conventional braze alloys currently being used in the drilling industry.

Tn particular, it was shown that BrazGTec 5662 could be used to successfully braze cutting elements on drill bits at temperatures around 1250 F (about 675 C), which is 100 F (about 38 C) lower than for the current braze alloy, BAg-7, currently used for these applications. The use of this braze alloy at the standard brazing temperature of around 1350 F 1() (about 730 C) resulted in average cutting element push-out loads of around 24,000 pounds required to dislodge cutting elements from the pockets of the bit body material. The push-out load has been determined to represent the 'braze strength' of the braze alloy wt-ict- represents the strength of the metallurgical /chemical bond between the cutting element and the cutter pocket. This is about 20-'c-; higher than that required to for cutting elements brazed using BAg-7 (which is typically about 20,000 pounds) as the braze alloy 2() In another example, a cutting elerner-t was brazed at a temperature of about 1250 F using BrazeTec 5662. The brazing temperature in this case is about 100 F lower than the standard brazing temperature for these applications. In this case, the push-out load required to dislodge cutting elements was around 21,700 pounds. Thus, even at this lower brazing temperature use of BrazeTec 5662 resulted in a push out load of about 10% higher than that required using BAg-7 as the braze alloy and brazed at fire stander-d brazing temperature of around 1350 F. 3()

Those skilled in the art wi ll appreciate that braze alloys in accordance with the present invention can be made using any manufacturing techniques well known ire rho art.

Generally, such manufacture ng techniques incl ude Mel ting the constituent compositional elements of the alloy together an forming an ingot from the molten alloy. After being produced, the particular braze alloy desired can be provided i n a variety of f orms suitable f or brazing purposes.

1() The braze alloy in accordance with an embodiment of the present invention may be formed in any suitable manner known in the art or cast using any suitable technique known in the art into any desired form. For example, the braze alloys can be in a sheet form, strip form, wire form, rod form, foil form, powder form, shot form, chip form, paste form, etc. In one or more embodiments, a braze alloy as described above may be used to braze a cutter to one selected from the group of a bit body such as fixed cutter drill bit body, an impregnated bit body, a t-arrrrner bit body or a milled tooth body, or any other down hol e products, such as reaming tools, fishing tools, and stabilizer blades, milling tools, and hole openers. To one or more embodiments, a braze alloy in accordance with trhc above description may be used for brazing ultrahard material on the ends of cutting elements formed on milled tooth bits. In one or more embodiments, a braze alloy as described above may be used to braze diamond grit metal matrix inserts on to bit bodies. Diamond grit metal matrix inserts are formed from diamond grit hot pressed together 3() with a metal binder material to form an insert.

In one or more embodiments, a braze alloy as described herein may also be advantageously used in applications where higher braze strength is desired without increasing the melting point of the braze alloy. In one or more embodiments, a braze alloy may be provided in a form such as one selected from the group of a powder, a disc, a water, a paste, and a wire. In one or more embodiments, braze alloy coated or impregnated base metals can be joined by any brazing process known in the art or described above.

Those skilled in the art will appreciate that in general braze alloy in accordance with one or more embodiments of the invention may be advantageously applied to any ultrahard material application involving a metal/diamond combination, lo' because by an alloy which allows for alloying at lower temperatures without sacrificing braze strength will advantageously reduce the risk associated with damaging the diamond during brazing and may also result in lower residual stresses in the final product.

Embodiments of the present invention may include one or more of the following advantages. One or more embodiments may provide a method for brazing Gutting elements which involves lower brazing temperatures lo reduce the amount of residual stresses remaining in the ultrahard material of the Gutting element after brazing. One or more embodiments may provide a drilling tool which includes a braze alloy with increased braze strength compar-cd to that offered by conventional braze alloys used in these applications, such as () BAg-7. One or more embodiments may advantageously allow for drill bits having more aggressive cutting structure designs.

One or more embodiments of the invention may include a braze alloy alloyed to reduce the temperature required for brazing to decrease the residual stresses in the ultrahard material resulting from brazing. ()ne or more embodiments of the invention may provide drill bits which have superior cutter retention, improved performance, and/or extended life ove drill bits manufactured using conventional braze alloys for drill bit applications. Other advar-tages will be apparent to those of ordinary skill in the art.

While the present invention has been described with respect to specific embodiments and applications thereof, numerous alternatives, modifications, and applications, and variations will be apparent to those skilled in the art having read the forogoing description. The invention is intended to embrace those alternatives, modifications, and variations as fall within the broad scope of the appended claims. Accordingly, the scope of tie invention should be limited only by the attached claims.

Claims

1. A down hole cutting tool, comprising: a cutting element support structure having at least one cavity formed therein; a cutting element having a base portion disposed in the cavity; a braze alloy disposed in the cavity between the cutting element and the cutting element support structure, the braze 1() alloy comprising between about 0.5% and about 10 .. by weight ot at least one selected from the group of gallium (Ga), indium (In), thallium (Tl).

2. A tool according to claim l, further comprising a tool body, wherein the cutting element support structure is disposed on the tool body and comprises at least one radially extending blade integrally formed with the tool body, the blade having the at least one cavity formed therein to support the cutting element. ?()

:

3. A tool according to claim 1 or 2, wherein the tool comprises a drill bit for drilling earth formations.

4. A tool according to claim 3, wherein the drill bit comprises a bit body, and the cutting element support structure comprises a plurality of radially extending blades formed continuous with tile bit body.

5. A tool according to clairT-.3 or 4, wherein at least one 3() of the drill bit body and the cutting element support structure comprises at least one selected from (a) steel and (b) tungsten carbide infiltrated with an alloy binder.

6. A tool according to any of claims 1 to 5, wherein the r:: cutting element comprises a substrate having ultrahard material disposed thereon.

/. A tool according to claim 6, wherein the ultrahard material compr.ises polycrystalline diamond. 1 0

8. A tool according to any of claims 1 to 7, wherein the braze alloy further comprises at least one selected from the group consisting of silver, copper, tin, and zinc.

L5

9. A tool according to any of claims 1 to 8, wherein the braze alloy comprises silver in an amount of at least about 40% by weight.

IO. A tool according to any of claims 1 to 9, wherein the braze alloy further comprises copper in are amount of at least about 10 o by weight.

11. A tool according to any of claims] to 10, wherein the braze alloy further comprises zinc in an amount of at least about 6% by weight.

12. A tool according to any of claims:I to 11, wherein the braze alloy further- comprises tin in an amount of at least about 2% by weight. :0

13. A tool according to any of claims 1 to 12, wherein the braze alloy comprises between about l% and about 8': of at least one selected from the group of gallium (Ga), indium (lo), and thallium (T1). i:

14. A tool according to any of claims 1 to 13, wherein the braze alloy comprises between about 2'.. and about 5 , of at least one selected from the group of gallium (Ga), indium (In), and thallium (T1). 1 0

15. A tool according lo any of claims 1 to 14, wherein the braze alloy comprises around 3% of at least one selected from the group of gallium (Ga), indi.um (in), thallium (T1); and the braze alloy further comprises around 56: by weight I r] silver, around 19 , by weight copper, around 17: by weight zinc, and around TO by weight tin.

16. A tool according to claim 14 or 15, wherein the at least one selected comprises gallium (Ga). 2()

17. A method for manufacturing a down hole cutting tool, the cutting tool including a cutting element support structure having at least one cavity formed thereon to support a cutting element, the method comprising: 2'-i inserting a base portion of the cutting element into the cavity) locating a braze alloy such that when heated the braze alloy melts and fills a space in the cavity between the cutting element. and the cutting element support structure, :() the braze alloy comprising about 0.5% to about 10 6 by weight of at least one selected from the group of gallium (Ca), indium (In), thallium (Tl); and heating the braze alloy such that it melts.

18. A method according to claim 17, wherein the locating comprises p]. acing the braze alloy in the cavity prior to the inserting of the cutting element.

19. A method according to claim 17 or 13, wherein the locating comprises placing the braze alloy proximal. the space between the cutting clement and the cutting element support structure.

20. A method according to any of claims 17 to 19, further comprising cooling the braze alloy such that it bonds the cutting element Lo the cutting element support structure.

21. A method according to any of claims 17 to 20, wherein the tool comprises a drill bit for drilling earth formation. 2()

22. A method according to any of claims 17 to 21, wherein the drill bit further comprises a bit. body and the cutting element support structure comprises a blade formed continuous with the bit body.

23. A method according to any of claims 17 to 22, wherein the cutting element comprises a substrate having ult.rahard material disposed thereon.

24. A method according to any of claims 17 to 23, wherein the ultrahard material comprises polycrystal].ine diamond.

25. A method according to any of claims 17 to 24, wherein the braze alloy further comprises at least one selected from tile group of silver, copper, tin, and zinc.

26. A method according to any of claims 17 to 25, wherein the braze alloy comprises silver in an amount of at least about 40% by weight.

lo) 2/. A method according to any of claims 17 to 26, wherein the braze alloy further comprises copper in an amount of at Least about J0 ,i by weight.

28. A method according to any of claims 17 to 27, wherein I r:) the braze alloy further comprises zinc in an amount of at least about 6 o by weight.

29. A method accordir-g to any of claims 17 to 28, wherein the braze alloy further comprises tin in an amount of at ?(.) least about 2'o by weight.

30. A method according to any of claims 17 to 29, wherein the braze alloy comprises between about 1 .s and about 8% of at least one selected from the group of gallium (Ga), indium (In), and thallium (T1).

31. A method according to any of claims 17 to 30, wherein tie braze alloy comprises between about 2'2, and about 5% of least one selected from the group of gallium (Ga), indium N() (In), and thallium (T1).

32. A method according to any of claims 17 to 31, wherein the braze alloy comprises around 3'-0 of at least one selected from the group of galliuTn (Ga), indium (In), and thallium (Tl); and the braze alloy further comprises around 56 o by -: weight silver, around 19"s by weight copper, around 17'o by weight zinc, and around 5' by weight tin.

33. A method according to any of claims 17 to 32, wherein the at least one selected comprises gallium (Ga). lo)

34. A braze alloy, comprising: at least one selected from the group of indium (In) and -gallium (Tl).

35. An alloy according to Claim 34, wherein the braze alloy, comprises about 0. 5 ' to about 10'2, by weight of at the least one selected from the group of indium (In) and thallium (Tl).

36. An alloy according to claims 34 or 35, further comprising gallium.

37. An alloy according to any of claims 34 to 36, further comprising at J. east one selected from the group of silver, copper, tin, and zinc.

38. An alloy according to any of claims 34 to 37, wherein the alloy comprises silver in an amount of at least 40 , by weight.

39. An alloy according to any of claims 34 to 38, wherein the alloy further comprising copper in an amount of at least about 10% by weight.

40. An alloy according to any of claims 34 to 39, wherein the alloy further comprising zinc in an amount cuff at least about 6% by weight.

41. An alloy according lo any of claims 34 to 40, wherein 1() lt-re alloy further comprising tin in an amount of at least about 2? by weight.

42. An alloy according to any of claims 34 to 41, further comprising gallium.

43. An alloy according to any of claims 34 to 42, wherein the alloy comprises between about 1', and about 8% of at least one selected from the group of iridium (In) and thallium (Tl).

2()

44. An alloy according to any of claims 34 to 43, wherein the alloy comprises between about 2': and about 5% of at least ore selected from the group of indium (In) and thallium (Tl).

45. An alloy according to any of claims 34 to 44, wherein the alloy comprises around 3% of at least one selected from tic group of indium (in) and thallium (Tl); and the alloy further comprises around 56'', by weight silver, around 19': by weight copper, around 17% by weight zinc, and around 5% by weight tin.

46. An alloy according to any of claims 34 to 45, wherein the at least one selected comprises indium (in).

47. An alloy according to any of claims 34 to 45, wherein the at least one selected comprises thallium (I]).

48. A braze alloy s.:hstantially as shown in and/or described with reference to any of Figures 1 to 7 of the accompanying drawings. 1()

49. A down hole cutting tool substantially as shown in and/or described with reference to any of Figures 1 to 7 of the accompanying drawings.

50. A method for manufacturing a down hole cutting tool substantially as shown in and/or described with reference to any of Figures 1 to 7 Off the accompanying drawings.