tool

Abstract

The present invention relates to a tool comprising a cemented carbide part (2) and a maraging steel part (1), the two parts being joined by brazing. The present invention also relates to the production of such a tool, which results in a strong brazed joint and a steel part with uniform hardness.

Description

[Technical Field]

[0001] The present invention relates to a tool comprising a cemented carbide part and a maraging steel part, which parts are joined by brazing. The present invention also relates to the production of such a tool. [Background technology]

[0002] Joining steel with cemented carbide by brazing or welding has long been known in the art of tool making. Several challenges exist when joining steel with cemented carbide, such as differences in CTE (coefficient of thermal expansion), strength of the brazed joint, and undesirable hardness profile of the steel.

[0003] There are solutions that can improve each of these challenges individually, but not all of them are solvable, as the solutions often introduce challenges in other areas.

[0004] The principle of brazing is the use of a brazing material that, when heated, joins two pieces together. There are several ways to heat the brazed joint, one of the most common being induction heating using an induction coil. One advantage of using a coil is that only the localized area around the brazed joint is heated, leaving the rest of the tool unaffected. However, this localized heating can create an undesirable hardness profile in the steel part, which can create challenges when the steel part is to be threaded for fastening, for example, rotary tools or other cutting tools.

[0005] A further drawback of coil heating is that it requires individual handling of each tool, making a more automated industrial process preferable.

[0006] Heating the entire steel and cemented carbide section results in a more uniform hardness profile, but the subsequent temperature increase affects the entire steel section, resulting in a decrease in overall hardness.

[0007] Another potential problem when threading steel parts to fasten cutting tools is wear: since the tool, e.g., the shank, is preferably used for a long time, many changes occur to the cutting tool, and wear of the threads can adversely affect the fastening of the cutting tool.

[0008] One object of the present invention is to provide a tool having both a strong braze joint and a steel portion with a uniform hardness profile and high hardness, resulting in improved wear resistance.

[0009] Another object of the present invention is to provide a process for joining steel and cemented carbide that is easy to use and results in a predictable joint with high strength and a steel part with predictable hardness. [Brief explanation of the drawings]

[0010] [Figure 1] FIG. 10 shows an SEM image of the contact surface between the cemented carbide part and the brazing material of Invention 9 at a magnification of 10,000 times. [Figure 2] FIG. 10 is a SEM image of the contact surface between the cemented carbide part and the brazing material of Invention 9 at a magnification of 40,000 times. [Figure 3] FIG. 10 shows an EDS mapping of element Ti at the interface between a cemented carbide part and a braze material according to an embodiment of the present invention. [Figure 4] FIG. 1 shows an SEM image of the interface between a cemented carbide portion and a braze material at 10,000x magnification according to one embodiment of the present invention. [Figure 5] Figure 1 shows the hardness profile of an induction-heated tool: A: steel part, B: brazed joint, C: cemented carbide. [Figure 6] FIG. 1 shows a schematic diagram of a shear testing device, where 1 is the steel part and 2 is the cemented carbide part. [Figure 7] 1 shows various parts of the brazed joint of Example 7, where A is the cemented carbide part and B is the maraging steel part. [Figure 8]1 shows various parts of the brazed joint of Example 7, where A is the cemented carbide part and B is the maraging steel part. [Figure 9] 1 shows various parts of the brazed joint of Example 7, where A is the cemented carbide part and B is the maraging steel part. [Figure 10] 1 shows the steps of the claimed method, where A is the step of obtaining a cemented carbide part, B is the step of obtaining a maraging steel part, C is the step of disposing a brazing material between the cemented carbide part and the maraging steel part, D is the brazing step, and E is the aging treatment step. [Figure 11] FIG. 1 shows an example of a brazed shank, where A is the cemented carbide part and B is the steel part. DETAILED DESCRIPTION OF THE INVENTION

[0011] The present invention relates to a tool comprising a cemented carbide portion and a maraging steel portion having a hardness between 350 and 600 HVl with a standard deviation between 0 and 20 HVl, the tool further comprising a brazed joint joining the cemented carbide portion and the steel portion, the brazed joint comprising Ti, the brazed joint comprising a TiC layer adjacent to the cemented carbide portion and having a thickness between 0.03 and 5 μm.

[0012] The cemented carbide part can be made of any cemented carbide common in the art. Cemented carbide includes a hard phase embedded in a metal binder phase matrix.

[0013] By hardmetal it is meant here that at least 50% by weight of the hard phase is WC.

[0014] Suitably, the amount of the metal binder phase is between 3 and 20% by weight of the cemented carbide, preferably between 4 and 15% by weight. Preferably, the main component of the metal binder phase is selected from one or more of Co, Ni and Fe, more preferably the main component of the metal binder phase is Co.

[0015] By major component it is meant here that no other elements are added to form a binder phase, but if other components, such as Cr, are added, this will necessarily be dissolved in the binder during sintering.

[0016] In one embodiment of the present invention, the cemented carbide may also include other constituents common to cemented carbide elements selected from Cr, Ta, Ti, Nb, and V present as elements or as carbides, nitrides, or carbonitrides.

[0017] The steel portion is made of maraging steel. Maraging steel is a type of steel that hardens by the precipitation of intermetallic compounds. The maraging steel preferably contains 13-25 wt. % Ni and one or more alloying elements selected from Co, Mo, Ti, Al, and Cr in a total amount of 10-27 wt. % of the alloying elements, preferably 11-23 wt. %. Maraging steel typically contains less carbon than conventional steel, preferably 0.03 wt. % or less carbon. The balance is Fe and unavoidable impurities.

[0018] The maraging steel according to the present invention preferably contains 13-25 wt% Ni, preferably 17-25 wt% Ni. The alloying elements are suitably Co in an amount of 7-15 wt%, preferably 8.5-12.5 wt% Co, Mo in an amount of 3-10 wt%, preferably 3-6 wt% Mo, Ti in an amount of 0.1-1.6 wt%, preferably 0.5-1.2 wt% Ti, 0.05-0.15 wt% Cr, Al in an amount of 0-0.2 wt%, and less than 0.03 wt% C. The balance is Fe and unavoidable impurities.

[0019] In one embodiment of the present invention, the maraging steel has a composition of 17 to 19 wt % Ni, 8.5 to 12.5 wt % Co, 4 to 6 wt % Mo, 0.5 to 1.2 wt % Ti, 0.05 to 0.15 wt % Cr, 0 to 0.2 wt % Al, less than 0.03 wt % C, and the balance being Fe and unavoidable impurities.

[0020] The average hardness of the maraging steel part is suitably between 350 and 600 HVl, preferably between 400 and 460 HVl, and more preferably between 410 and 450 HVl. The hardness is measured by a Vickers hardness tester, applying a load of 1 kgf (kilogram force) and a loading time of 15 seconds. A 3 x 6 indent pattern was applied to the entire material (not the surface) of the maraging steel part. The average value is the average of these measurement points. The standard deviation of the hardness values ​​is suitably between 0 and 20 HVl, preferably between 0 and 14 HVl.

[0021] The brazing technique is so-called active brazing. This means that the joint is not only formed by melting the brazing material to form a metallurgical bond, but also requires a chemical reaction with one or both of the materials being joined. The reactive element in the brazing material is usually Ti, but elements such as Hf, V, Zr, and Cr are also considered active elements. In accordance with the present invention, Ti is the active element.

[0022] By braze joint is meant herein the area or mass between the cemented carbide part and the maraging steel part that is filled with braze material and formed during the brazing process, see below.

[0023] The thickness of the brazed joint is suitably between 20 and 200 μm, preferably between 30 and 100 μm.

[0024] The brazed joint is not a homogeneous phase. Instead, after brazing, the elements in the brazing material form different phases.

[0025] The braze joint preferably contains Ti, which during brazing reacts with carbon in the cemented carbide parts to form a TiC layer at the interface between the braze joint and the cemented carbide parts.

[0026] There are several ways to detect the presence of a TiC layer, depending on what type of equipment is used.

[0027] When a scanning electron microscope (SEM) with sufficiently high resolution is used, the TiC layer is clearly visible adjacent to the cemented carbide portion, see, for example, Figures 1 and 2.

[0028] If the SEM used does not have the resolution to show the TiC layer, the accumulation of Ti and / or C at the interface between the brazing material and the cemented carbide can be confirmed using, for example, SEM-EDS with WDS or SEM-EPMA. The accumulation of Ti, hereafter referred to as the Ti accumulation layer, is a good indicator that a TiC layer has formed, even if it is not visually detected in the SEM image. The Ti accumulation layer is much thicker than the actual TiC layer, which may mean that not all Ti forms TiC. The thickness of the Ti accumulation layer is also partly affected by the analysis method.

[0029] In one embodiment of the present invention, the thickness of the TiC layer is between 0.03 and 5 μm, more preferably between 0.05 and 0.5 μm, and most preferably between 0.05 and 0.25 μm.

[0030] Preferably, the brazed joint further comprises one or more elements selected from Ag, Cu, Sn, In, Zr, Hf, Cr, more preferably Ag, Cu, and Sn.

[0031] The composition of the brazed joint after brazing is difficult to determine because the elements are not uniformly distributed. The easiest way is to identify the brazing material used, if available, since the paste or foil is a homogeneous mixture. The brazed joint may also contain small amounts of elements from the materials being joined, such as Co and W from cemented carbide, and Fe and Ni from maraging steel.

[0032] The amount of Ti and other elements in the brazed joint can also be measured using energy-dispersive X-ray spectroscopy (EDS). However, due to the non-uniform distribution of elements in the brazed joint, many measurement points must be used, resulting in a large standard deviation. Preferably, the brazed joint contains, on average, 30-80 wt. %, preferably 40-75 wt. % Ag, 15-65 wt. %, preferably 20-40 wt. % Cu, 0.3-15 wt. %, preferably 0.5-5 wt. % Ti, and 0-10 wt. %, preferably 0-2 wt. % Sn.

[0033] The brazed joint suitably has a shear strength of at least 130 MPa, preferably at least 140 MPa, more preferably between 140 and 300 MPa. Shear strength is measured by shear testing.

[0034] At the contact surface between the brazed joint and the maraging steel part, Ti also accumulates in the brazed joint and forms a metallic bond with the iron in the maraging steel. The thickness of the Ti accumulation layer on the surface of the maraging steel is preferably between 1 and 10 μm, preferably between 2 and 5 μm, and can be measured, for example, by EDS.

[0035] In one embodiment of the present invention, the maraging steel part is provided, at least on the surface facing the brazed joint, with a Ni layer having an average thickness between 2 and 10 μm, preferably between 4 and 6 μm.

[0036] The Ni layer may be provided as a foil or deposited by any suitable deposition method, such as physical vapor deposition.

[0037] In one embodiment of the present invention, no Ni layer is provided on the maraging steel part.

[0038] In one embodiment of the present invention, the maraging steel has a composition of 17-19 wt% Ni, 8.5-12.5 wt% Co, 4-6 wt% Mo, 0.5-1.2 wt% Ti, 0.05-0.15 wt% Cr, 0-0.2 wt% Al, less than 0.03 wt% C, and the balance Fe and unavoidable impurities. Grade 1.2709 maraging steel is preferably used. The cemented carbide has a composition of 4-15 wt% Co, 0.1-1 wt% Cr, and the balance WC. The brazed joint has an average composition of 55-75 wt% Ag, 20-36 wt% Cu, 1-3 wt% Ti, and 2-8 wt% Sn.

[0039] The tool can be any tool or part of a tool common in the art in which a cemented carbide part is joined to a steel part by brazing, examples being drills, end mills, tool holders such as shanks, etc.

[0040] In one embodiment of the present invention, the tool is a shank used as a tool holder for cutting tools such as inserts, drill heads, etc. The shank is formed of a cemented carbide portion and a steel portion, the cemented carbide portion being used to provide stability and the steel portion being required to create the thread cut for fastening the cutting tool.

[0041] The present invention also provides a method of making a tool according to the above, comprising the steps of: obtaining a cemented carbide part and a maraging steel part; disposing a brazing material containing Ti in an amount of 0.3 to 15 wt. % thereof between and in contact with the cemented carbide portion and the maraging steel portion; subjecting the cemented carbide part and the maraging steel part, with the brazing material sandwiched between them, to a brazing process in a furnace at a temperature between 700 and 1200°C for a period of between 5 and 60 minutes, the brazing being carried out under vacuum; subjecting at least the maraging steel portion to an aging treatment at a temperature between 300 and 700°C for 5 minutes to 12 hours; The present invention relates to a method comprising:

[0042] The cemented carbide part and the maraging steel part have the composition as described above. The hardness of the maraging part before brazing may differ from that described above depending on the grade of the maraging steel and whether the steel has been aged or not.

[0043] The shape and size of the cemented carbide and maraging steel portions will depend on the type of tool being made.

[0044] The brazing material (also called filler metal or solder) according to the present invention contains Ti in a total amount of 0.3 to 15% by weight of the brazing material, preferably 1 to 5% by weight. The brazing material of the present invention suitably has a solidus temperature between 488 and 1123°C, preferably between 650 and 780°C. Furthermore, the brazing material of the present invention has a liquidus temperature between 612 and 1180°C, preferably between 750 and 850°C. In addition to Ti, the brazing material further contains one or more elements selected from Ag, Cu, Sn, In, Zr, Hf, and Cr.

[0045] In one embodiment of the present invention, the brazing material comprises Ag in an amount of 30-80 wt%, preferably 40-75 wt%, Cu in an amount of 15-65 wt%, preferably 20-40 wt%, Ti in an amount of 0.3-15 wt%, preferably 0.5-5 wt%, and Sn in an amount of 0-10 wt%, preferably 0-2 wt%.

[0046] Preferably, the brazing material is provided as a foil or a paste.

[0047] The brazing material is applied to the faying surfaces of the cemented carbide portion and the steel portion.

[0048] The thickness of the brazing material before the brazing process is suitably between 25 and 200 μm, preferably between 50 and 100 μm.

[0049] The parts are then placed in a furnace with an inert environment, i.e., a minimum of oxygen. Preferably, the brazing temperature in the furnace is between 750 and 1200°C, preferably between 800 and 950°C, and more preferably between 800 and 830°C. The time the parts are exposed to the high temperature is between 5 and 60 minutes, preferably between 5 and 15 minutes. If the time at high temperature is too short, there will not be enough time for the brazed joint to form and for the Ti to react to achieve the desired brazed joint strength. If the time at high temperature is too long, the Ti-containing brittle reaction zone will grow uncontrolled, adversely affecting joint properties, such as shear strength.

[0050] Brazing is preferably carried out under vacuum or in the presence of a low partial pressure of argon, which is defined herein as a furnace pressure of 5×10 -4 mbar, preferably less than 5 × 10 -5 mbar. If argon is present, the argon pressure is less than 1×10 -2 It is less than mbar.

[0051] During brazing in the furnace, a clamping force may be applied to further strengthen the braze. By clamping force is meant here that the steel part and the cemented carbide part are pressed together, preferably with a force applied by placing an external weight on the carbide part. The force acting on the brazed joint by the weight of the cemented carbide part or the maraging steel part, depending on which part is on top of the other, is not included in these values.

[0052] In one embodiment, a clamping force between 0.5 and 10 MPa, preferably between 2 and 8 MPa, is applied.

[0053] In one embodiment of the present invention, no clamping force is applied.

[0054] After brazing, the parts are subjected to an ageing step by exposing them to a high ageing temperature between 300-700°C, preferably between 500-600°C, and most preferably between 550-600°C, for a period of 5 minutes to 12 hours, preferably 3-6 hours.

[0055] Preferably, the heating rate to the ageing temperature is between 1 and 50°C / min, preferably between 5 and 10°C / min. Preferably, the cooling rate from the ageing temperature to a temperature at least below the solidus temperature of the brazing material is between 1 and 50°C / min, preferably between 5 and 10°C / min.

[0056] The brazing furnace used in accordance with the present invention can be any furnace that provides well-controlled conditions, as described above, with respect to vacuum, heating and cooling rates, etc. The brazing and aging steps can be carried out either in the same furnace or in two separate furnaces.

[0057] Steel parts are typically subjected to machining operations, such as thread cutting, etc. To allow machining of the steel part, the hardness should not be too high, and depending on the type of maraging steel grade selected, an aging treatment step can be carried out either before or after machining of the steel part to achieve the desired hardness and wear resistance in the finished tool.

[0058] In one embodiment of the present invention, the ageing treatment is carried out immediately after the brazing step, and any machining operations on the steel, such as thread cutting, are carried out on the already aged maraging steel, i.e. after the ageing step.

[0059] In another embodiment of the invention, the ageing treatment is carried out after any machining operations on the steel, such as thread cutting for example. [Example]

[0060] (The present invention) Steel parts made of maraging steel 1.2709 were obtained along with cemented carbide parts with the composition 10 wt. % Co, 1 wt. % other carbides, and the remainder WC.

[0061] The brazing material was obtained in the form of a foil with a thickness of 100 μm. The brazing material had a composition of 65.0 wt% Ag, 28.0 wt% Cu, 2.0 wt% Ti, and 5.0 wt% Sn. The solidus temperature was about 700°C, and the liquidus temperature was about 750°C.

[0062] A foil was placed between the maraging steel part and the cemented carbide part so that both pieces were in contact with the foil. The assembled joint pieces were then placed in a Schmetz vacuum furnace (type: EU80 / 1H 30 x 45 x 30 6 bar System * 2RV * ) and the temperature was first increased to 815°C at a rate of 20°C / min. The brazing temperature of 815°C was maintained for a time t brazing The temperature was maintained for 100° C., after which the specimen was cooled at a rate of 5° C. / min to 300° C. After reaching 300° C., the specimen was allowed to free cool.

[0063] For some of the samples, the surface of the maraging steel part facing the brazing material was coated with a Ni layer having an average thickness of 4.7 μm with a standard deviation of 0.2 μm, which was applied by Arc Physical Vapor Deposition. TIFF0007749671000001.tif53170

[0064] After the brazing process, the brazed specimens were subjected to an aging process to preserve the hardness of the maraging steel. The specimens were placed in a furnace, and the temperature was first increased to 580°C at a rate of 5°C / min. The temperature of 580°C was maintained for 3 hours, after which the specimens were cooled to 300°C at a rate of 5°C / min. After reaching 300°C, the specimens were allowed to free cool. [Example]

[0065] (The present invention) The tool shanks were manufactured by joining a steel part made of maraging steel 1.2709 to a cemented carbide part with the composition 10 wt. % Co, 1 wt. % other carbides, and the remainder WC.

[0066] The brazing material was obtained in the form of a foil with a thickness of 100 μm. The brazing material had the following composition by weight: 65.0% Ag, 28.0% Cu, 2.0% Ti, and 5.0% Sn. The solidus temperature was about 700°C and the liquidus temperature was about 750°C.

[0067] The foil was placed between the maraging steel part and the cemented carbide part, and the assembled joint pieces were placed in a Schmetz vacuum furnace (type: EU80 / 1H 30 x 45 x 30 6 bar System). * 2RV * ) and the temperature was first increased to 815°C at a rate of 20°C / min. The brazing temperature of 815°C was maintained for a time t brazing = 15 minutes, after which the specimen was ramped down to 300°C at a rate of 5°C / min. After reaching 300°C, the specimen was allowed to free cool.

[0068] The tool manufactured according to this example will be referred to as present invention 9 hereinafter. [Example]

[0069] (Comparative Example) Steel parts made of maraging steel 1.6582 (34CrNiMo6) were obtained along with cemented carbide parts with the composition 10 wt% Co, 0.4 wt% Cr and the remainder WC.

[0070] The brazing material was Ag49Zn23Cu16Mn7.5Ni4.5 in wire form and was applied as a ring with a diameter of 1-2 mm.

[0071] The pieces are joined by induction heating the brazed joint quickly to 700°C using a coil and holding for 15 seconds, after which the powder is cut off and the tool is cooled to room temperature. Figure 5 shows the hardness values ​​of the steel part, with the measurement points along the line from the brazed joint on the steel part, across the brazed joint to the cemented carbide part.

[0072] This sample is referred to herein as Comparative Example 1. [Example]

[0073] (Comparative Example) Steel parts made from carbon-hardening hot-work steel 1.2344 were obtained along with cemented carbide parts with a composition of 10 wt.% Co, 1 wt.% other carbides, and the remainder WC. The hot-work steel components were in a prehardened state. The steel was quenched from 1060°C with N2 in a vacuum furnace, followed by three 10-minute relaxations at 200°C. The average hardness value of the quenched 1.2344 parts was 582 HVl, with a standard deviation of 66 HVl.

[0074] Brazing material 1 was obtained in the form of a 100 μm thick foil. Brazing material 2 was obtained in the form of a paste. Brazing material 1 had a composition of 60.0 wt% Ag, 24.0 wt% Cu, 14.0 wt% In, and 2.0 wt% Ti. Its solidus temperature was approximately 620°C and its liquidus temperature was approximately 720°C. Brazing material 2 had a composition of 59.0 wt% Ag, 27.25 wt% Cu, 12.5 wt% In, and 1.25 wt% Ti. Its solidus temperature was approximately 605°C and its liquidus temperature was approximately 715°C.

[0075] The brazing material was placed between the maraging steel part and the cemented carbide part so that both pieces were in contact with the brazing material. The assembled joint pieces were placed in a furnace, and the temperature was first raised to 500°C at a rate of 20°C / min and held for 5 minutes. Then, from the brazing temperature of 500°C, the temperature was increased to the brazing temperature T BrazingThe temperature was increased to 685°C (Brazing Material 1) and 715°C (Brazing Material 2). Brazing was maintained for a dwell time of 4 minutes, after which the coupons were allowed to cool to room temperature by free cooling.

[0076] The hardness was measured and the results are shown in Table 2.

[0077] The two samples at 685°C (Braze Material 1) and 715°C (Braze Material 2) are designated herein as Comparative Example 2 and Comparative Example 3, respectively.

[0078] Shear strength values ​​were not determined. [Example]

[0079] (Comparative Example) Steel parts made from carbon hardened hot work steel 1.2344 were obtained along with cemented carbide parts with the composition 10 wt% Co, 1 wt% other carbides and the remainder WC.

[0080] The brazing material was obtained in the form of a foil with a thickness of 100 μm. The brazing metal had a composition of 100.0% Cu by weight. The melting temperature was 1085° C.

[0081] A foil was placed between the maraging steel part and the cemented carbide part, and the assembled joint pieces were placed in a furnace. The temperature was first raised to 650°C at a rate of 20°C / min and held for 5 minutes. Then, from the brazing temperature of 650°C, the brazing temperature T Brazing The temperature was increased to 1100°C. Brazing The pressure was maintained for a residence time of 15 minutes, after which the specimen was cooled down to 850°C at a cooling rate of 50 K / min. -1 The specimens were quenched from 850°C with N2 at a fan frequency of 1000kJ / s.

[0082] The cemented carbide-steel joints with carbon hardened hot work steel 1.2344 were then subjected to two ageing treatments at 630°C for 2 hours.

[0083] This sample is referred to herein as Comparative Example 4. [Example]

[0084] (Comparative Example) Steel parts made from carbon hardened cold work steel 1.2714 were obtained along with cemented carbide parts with the composition 10 wt% Co, 1 wt% other carbides, and the remainder WC.

[0085] The brazing material was obtained in the form of a foil with a thickness of 100 μm. Brazing material 1 had a composition of 100.0% Cu by weight. The melting temperature was 1085° C.

[0086] A foil was placed between the maraging steel part and the cemented carbide part, and the assembled joint pieces were placed in a furnace. The temperature was first raised to 650°C at a rate of 20°C / min and held for 5 minutes. Then, from the brazing temperature of 650°C, the brazing temperature T Brazing The temperature was increased to 1100°C. Brazing was maintained for a residence time of 15 minutes, after which free cooling was initiated to room temperature.

[0087] The cemented carbide-steel joint with the carbon-hardened cold-worked steel 1.2714 part was then heated by torch for 10 minutes to a temperature of 850°C and then quenched in oil to room temperature, after which tension relaxation was carried out in a vacuum furnace at 200°C for 2 hours.

[0088] The cemented carbide-steel joint with the carbon hardened cold work steel 1.2714 section was then aged at 500°C for 2 hours.

[0089] This sample will be referred to as Comparative Example 5 hereinafter. [Example]

[0090] The assembled joint pieces were evaluated by measuring the shear strength of the brazed joint, the hardness of the maraging steel section, and, if necessary, the hardness of the TiC layer of the brazed joint.

[0091] To evaluate the joint strength characteristics, shear tests were performed on the specimens using a shear device setup as shown in Figure 6, where 1 is a steel part in the shape of a steel cylinder (φ = 20 mm, h = 5 mm) and 2 is a cemented carbide part in the shape of a cemented carbide cylinder (φ = 10 mm, h = 5 mm). The steel cylinder is placed in the gap of the shear strength test device so that it can only move in the direction of loading. Notches eroded into the surface of the device hold the joined parts in a precise position and ensure the introduction of evenly distributed forces into the brazed joint. The applied force was constantly increased until the brazed joint broke and the cemented carbide cylinder was sheared. The quotient of the maximum measured force and the initial joint area (A = 78, 5 mm) was then calculated. 2 ) to calculate the ultimate shear strength. The brazing material was not removed before determining the shear strength of the brazed joint. The same method was applied when testing rods.

[0092] The hardness of the maraging 1.2709 steel section was measured with a Vickers hardness tester by applying a load of 1 kgf (kilogram force) and a loading time of 15 seconds on the cross section of the maraging steel section. The complete profile (approximately 20 × 5 mm) of the maraging steel 1.2709 section in the cross section was measured. 2 A 3x6 notch pattern was applied covering the area.

[0093] SEM-EDS technique was used to analyze the contact surfaces between the brazed joints of Inventions 1 to 8 and the cemented carbide. The SEM used was a Jeol JSM-7001F, a high-resolution field emission scanning electron microscope (FE-SEM) equipped with a thermal field emission cathode (Schottky). The thickness of the TiC layer in the brazed joints of Inventions 1 to 8 was measured on SEM images at a magnification of 10,000x. The TiC layer was identified by appearance in backscattered electron mode. Figure 4 shows an SEM image of Invention 2, in which the TiC layer is clearly visible. The TiC layer thickness values ​​provided in Table 2 are the average of three measurements, all of which were taken in the center of the brazed joint, i.e., away from the edges.

[0094] Ti accumulation can be identified and measured using EDS as a Ti accumulation layer. By accumulation layer, we mean the thickness of the accumulation estimated from the EDS scan. The values ​​in Table 2 are provided as intervals because they are estimates based on visual inspection of the EDS scan.

[0095] To analyze the contact surface between the brazed joint of Invention 9 and the cemented carbide, a different SEM was used: a field emission SEM (SU7000, Hitachi) equipped with a Schottky gun. Images were acquired using an electron beam with an incident energy of 10 keV, and the signal was collected by a photodiode-type backscattered electron detector. In the backscattered electron mode, the TiC layer was identified by appearance. Figure 1 shows an SEM image of Invention 9 at 10,000x magnification, in which the TiC layer is clearly visible. Figure 2 shows an SEM image of Invention 9 at 40,000x magnification. The thickness values ​​in Table 2 are the average of five measurements, all of which were taken at the center of the brazed joint, i.e., away from the edges, on the SEM image at 10,000x magnification.

[0096] In Figure 3, the accumulation of Ti is shown using EDS.

[0097] It was confirmed that this accumulation was indeed a TiC layer by analyzing Ti and C using EPMA. TIFF0007749671000002.tif102170 [Example]

[0098] The brazed joints of Examples 1 to 2 were analyzed by SEM-EDS and SEM images, along with EDS mapping for three different parts of the brazed joint, Parts 1, 2, and 3, shown in Figures 7 and 8, respectively. As can be seen, the brazed joints are not homogeneous.

[0099] The various elements in the three different parts of the brazed joint were analyzed by measuring the chemical composition of the area by mapping with EDS, and the results are shown in Table 3. As can be seen, there is some Fe, Ni, and Ti from the steel, as well as some W and Co from the cemented carbide. TIFF0007749671000003.tif29170

[0100] As is evident from Table 3, the distribution of elements within the brazed joint varies between different parts of the same brazed joint, and to obtain a very good average composition of the brazed joint, more than one part of the brazed joint needs to be analyzed.

Claims

1. a cemented carbide part, the cemented carbide comprising a hard phase embedded in a metal binder phase matrix, at least 50 wt. % of the hard phase being WC; a maraging steel portion having a hardness between 350 and 600 HVl with a standard deviation between 0 and 20 HVl; a braze joint joining the cemented carbide portion and the steel portion; A tool comprising: The tool, wherein the braze joint comprises Ti, and the braze joint comprises a TiC layer adjacent to the cemented carbide portion having a thickness between 0.03 and 5 μm.

2. The tool of claim 1 , wherein the maraging steel portion has a hardness between 400 and 460 HV1 with a standard deviation between 0 and 14 HV1.

3. The tool according to claim 1 or 2, wherein the brazed joint has a thickness of between 20 and 200 μm.

4. 4. The tool of claim 1, wherein the shear strength of the brazed joint is at least 130 MPa.

5. The tool of claim 1 , wherein the braze joint comprises Cu, Ag, and Sn.

6. 6. The tool of any one of claims 1 to 5, wherein the brazed joint comprises Ag in an amount of 30-80 wt.%, Cu in an amount of 15-65 wt.%, Ti in an amount of 0.3-15 wt.%, and Sn in an amount of 0-10 wt.%.

7. 7. The tool according to any one of claims 1 to 6, wherein the maraging steel comprises 13-25 wt.% Ni, one or more alloying elements selected from Co, Mo, Ti, Al, and Cr in an amount of 10-27 wt.%, less than 0.3 wt.% C, and the balance Fe.

8. 8. The tool according to any one of claims 1 to 7, wherein the maraging steel comprises 13 to 25 wt.% Ni, 7 to 15 wt.% Co, 3 to 10 wt.% Mo, 0.1 to 1.6 wt.% Ti, 0.05 to 0.15 wt.% Cr, 0 to 0.2 wt.% Al, less than 0.3 wt.% C, and the balance being Fe and unavoidable impurities.

9. 9. A method of making a tool according to any one of claims 1 to 8, comprising the steps of: obtaining a cemented carbide part; obtaining a maraging steel part; disposing a brazing material between and in contact with the cemented carbide portion and the maraging steel portion, the brazing material comprising Ti in an amount of 0.3 to 15 wt. % thereof; subjecting the cemented carbide part and the maraging steel part, with the brazing material sandwiched between them, to a brazing process in a furnace at a temperature between 700 and 1200°C for a period of between 5 and 60 minutes, wherein the brazing is carried out under vacuum; subjecting at least said maraging steel portion to an aging treatment step at a temperature between 300 and 700°C for a period of 5 minutes to 12 hours; A method of making a tool, comprising:

10. 10. The method of making a tool according to claim 9, wherein the brazing step is carried out at a temperature between 700 and 950°C for a period of between 5 and 15 minutes.

11. A method of making a tool according to any one of claims 9 to 10, wherein the ageing step is carried out at a temperature between 550 and 600°C for a period of 3 to 6 hours.

12. 12. The method of making a tool according to any one of claims 9 to 11, wherein the braze material has a solidus temperature between 488 and 1123°C and a liquidus temperature between 612 and 1180°C, and wherein the braze material further comprises one or more elements selected from Ag, Cu, Sn, In, Zr, Hf, and Cr in addition to Ti.

13. A method of making a tool according to any one of claims 9 to 12, wherein the thickness of the brazing material before brazing is between 25 and 200 μm.

14. A method of making a tool according to any one of claims 9 to 13, wherein a clamping force of between 0.5 and 10 MPa is applied during the brazing step.

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