EP3765223A1 - Method for producing a sinter-joined composite body - Google Patents
Method for producing a sinter-joined composite bodyInfo
- Publication number
- EP3765223A1 EP3765223A1 EP19712673.3A EP19712673A EP3765223A1 EP 3765223 A1 EP3765223 A1 EP 3765223A1 EP 19712673 A EP19712673 A EP 19712673A EP 3765223 A1 EP3765223 A1 EP 3765223A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- hard metal
- carbide
- blanks
- blank
- cutting tool
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C29/00—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
- C22C29/02—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides
- C22C29/06—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds
- C22C29/08—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds based on tungsten carbide
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/02—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite layers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/10—Sintering only
- B22F3/1035—Liquid phase sintering
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
- B22F5/10—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of articles with cavities or holes, not otherwise provided for in the preceding subgroups
- B22F5/106—Tube or ring forms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
- B22F2005/001—Cutting tools, earth boring or grinding tool other than table ware
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2999/00—Aspects linked to processes or compositions used in powder metallurgy
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
Definitions
- the invention relates to a method for producing a sintered composite body made of hard metal with the features of the preamble of claim 1 and a sintered cutting tool blank or a sintered cutting tool of at least two carbide blanks having the features of the preamble of claim 10.
- a cemented carbide in the present disclosure is understood as meaning a powder-metallurgically produced particle composite consisting of a hard material phase (eg tungsten carbide, "WC” for short) and a binder metal (eg cobalt, Co, sometimes also referred to as "binder") ,
- the binder metal may optionally be doped, for. B. to limit the grain growth of the hard material phase.
- Sintering in the present disclosure is understood as meaning a joining of at least two hard metal blanks by liquid phase sintering.
- the at least two carbide blanks with respect to at least one hard metal blank, it may be in the form of a green compact, pre-sintered (not sintered to complete theoretical density), or, more preferably, sintered (sintered to complete theoretical density).
- Carbide blanks (which are blanks with a carbide body) are used to make a variety of components or tools:
- Carbide blanks for the production of cutting tools are produced on a large scale, including with internal cooling channels (IK). The positioning of these channels is done with geometrically limited freedoms.
- IK internal cooling channels
- a single carbide grade is usually used, from which all areas of the carbide body are formed.
- material properties such as hardness or toughness.
- Cemented carbide components sintered together in a sinter joining process are now state of the art.
- different carbide types can be combined to bring in individual areas of the body formed hard metals with different properties used and / or realized by combining several body geometric features that can not be represented with conventional manufacturing methods.
- the surface contact of the two bodies to be joined along the entire joining surface for the entire duration of the thermal treatment is critical for a secure and mechanically highly reliable joining connection during sintering.
- the surfaces of the carbide blanks in the region of the joining surface are to be prepared in such a way that play-free contact is achieved. This preparation is labor intensive and costly.
- the object of the invention is to provide a generic method and a generic Zerspanungswerkmaschinemaschinerohlings or Zerspanungswerkmaschines, in which the problems discussed above are avoided.
- the at least two carbide blanks are arranged with each other before Sinterglagen with play and that during sintering a liquid phase of the binder of at least two carbide blanks is produced and maintained until the first hard metal blank of the at least two carbide blanks by diffusion of binder Binder migration increases so much in volume and the second hard metal blank of the at least two carbide blanks is shrunk so much by the decrease in volume because of the diffused binder, that the at least two carbide blanks are connected material-tight with each other after sintering, the joining surfaces must not be present with a high geometric precision , Moreover, the placement of the first carbide blank in the opening or in the cavity of the second carbide blank is simplified because the first carbide blank can be introduced substantially free of force.
- a particular advantage of the method according to the invention is that due to the swelling of the first hard metal blank and the shrinkage of the second hard metal blank, the clearance remaining during insertion disappears anyway, and it therefore does not depend on a positionally correct introduction.
- a cohesive connection is present over the entire surface of the former joining surfaces.
- the first hard metal blank of the at least two carbide blanks has a lower binder content (irrespective of the grain size), this has a smaller thermal expansion coefficient than the second hard metal blank due to the lower binder content. When heated, consequently, the first hard metal blank expands to a lesser extent than the second hard metal blank.
- the coefficient of thermal expansion of conventional hard metals is in the range of 5 - 7 ⁇ 10 6 K ⁇ 1 .
- the coefficient of thermal expansion of tungsten carbide is much lower than that of cobalt (12.4 to 10 -6 K 1) with from 5.2 to 10 6 K. 1
- the thermal expansion coefficient of the cemented carbide scales with the content of binder metal (for example cobalt) approximately according to the mixing rule,
- hard metals with a low content of binder metal have a smaller thermal expansion coefficient than carbide with a higher content of binder metal (cf Hartmetall for the Praktiker, Wolfgang Schedler, VDI Verlag 1988).
- binder migration takes place from the second hard metal blank to the first hard metal blank.
- the binder migration first sets in.
- the binder migration causes a swelling of the first hard metal blank and a shrinkage of the second hard metal blank. It forms preferably over the entire surface of the former joining surfaces a cohesive connection. Due to the presence of a liquid phase, the joining process is stress-free. Any defects in the joint zone (ie, where no complete wetting or bridging of the gap has occurred, for example due to a curvature of the core and / or cladding) can be closed.
- the first hard metal blank forms the first (inner) portion and the second hard metal blank forms the second (outer) portion.
- the second cemented carbide blank Because of the lower coefficient of thermal expansion of the first cemented carbide blank having a lower binder content than the second cemented carbide blank having a higher binder content, the second cemented carbide blank has a stronger contraction tendency than the first hard metal blank. This causes in the finished cutting tool blank or cutting tool that tensile stresses remain in the outer region (shell), which exert compressive stresses on the core (the former first carbide blank) and the joining zone due to the prevailing balance of forces. As a result, a particularly stable connection is achieved.
- the binder migration from the second carbide blank to the first carbide blank begins where the two carbide blanks touch despite the existing game already at the beginning of Sinter shegens.
- the arrangement of the at least two carbide blanks with play can be carried out such that, although there is at least one linear or planar contact zone between the at least two carbide blanks, at least in some areas a gap remains between the at least two carbide blanks.
- the contact in the contact zone can be present directly between the at least two hard metal blanks or indirectly by a film or a film between the at least two carbide blanks (eg to improve wetting or positioning, for example to prevent slipping of the individual components). is arranged.
- the linear or area contact zone may, for. B. can be easily prepared by utilizing the weight of the at least two carbide blanks by a horizontal positioning of the at least two carbide blanks.
- an additional contact force can be applied between the at least two hard metal blanks (eg by weighting or by a clamping device).
- the gap has a gap of about 1 pm to about 200 pm, it is possible for the first and second hard metal blank to be joined to one another or to one another without the influence of force.
- the inner, first hard metal blank does not have to be pressed into the fit of the outer second hard metal blank provided for it before the sintering, but can be pushed into it with a certain play.
- the at least two carbide blanks are finished sintered prior to sintering, d. H. sintered to full density.
- the at least two carbide blanks have a different binder doping, ie additives to cobalt such as M02C, TiC, TaC, vanadium carbide.
- This can influence the grain growth during the production of the at least two carbide blanks before sintering become.
- the different grain size resulting, inter alia, from the different binder doping influences the degree of diffusion of the binder in the subsequent sintering by the different wettability (the smaller the grain size, the greater the capillary action and thus the binder migration).
- the first hard metal blank of the at least two hard metal blanks and the second hard metal blank of the at least two hard metal blanks are arranged along a common longitudinal axis.
- the at least two carbide blanks are arranged axially in front of the sintering joining to one another so that one hard metal blank of the at least two carbide blanks is located axially in front of the other carbide blank of the at least two carbide blanks, whereby an axial gap between the two carbide blanks can arise.
- This arrangement can be carried out both along or parallel in the direction of the longitudinal axis or transversely to the longitudinal axis of at least one carbide blank.
- the first hard metal blank can act, for example, as a closure or plug which is not radially but axially attached to at least partially close an opening in the second hard metal blank.
- the first hard metal blank of the at least two hard metal blanks is located completely within the opening or the hollow space of the second hard metal blank of the at least two hard metal blanks.
- the binder contents in the first and in the second hard metal blank move in a proportion of between 3% by weight and 20% by weight. With different binder contents between the first and the second hard metal blank thus a difference in the binder content of up to 17% by weight is achieved.
- the minimum difference in binder content between the two carbide blanks is 1% by weight, more preferably at least 2% by weight.
- the outer diameter of the second hard metal blank and thus the outer diameter of the composite body or cutting tool and its sintered blank is in a range between 2 mm and 30 mm.
- at least one cooling channel may be provided which has a diameter of 0.03 mm to 5 mm.
- the at least one cooling channel is wired, d. H. follows a screw curve. If tools made of concrete carbide blanks, for example drilling tools, have spiral grooves, the internal cooling channels preferably extend along the spiral grooves.
- the internal cooling channels should have the same pitch as the spiral grooves, otherwise the cooling channels could be exposed during a grinding process.
- the twist angle of an inner cooling channel is usually related to the outer diameter of the carbide blank for practical reasons.
- the actual slope of the channels is a function of the radial distance of the channel to the longitudinal axis.
- the twist is usually introduced by applying a twist during extrusion. This production route sets certain limits with regard to the achievable external diameter distortion. It can For larger outer diameters only lower twisting can be realized than for smaller outer diameters.
- the twist angle with which the at least one cooling channel extends with respect to the longitudinal axis of the first hard metal blank is z. B. between 15 ° to 60 °, based on the outer diameter of the first hard metal blank. This is possible with an outer diameter of the first carbide blank of 0.7 mm to 40 mm.
- the helix angle can alternatively be described by means of that axial offset over which the at least one cooling channel completes a complete rotation.
- Such an indication is given, for example, as a gradient in millimeters, meaning the axial extension of a 360 ° revolution of a cooling channel.
- the first hard metal blank is produced, for example, in the form of an extrusion process, wherein during extrusion, the at least one cooling channel is mitgeformt.
- helix angle results in a slope of at least 2.5 mm in extruded carbide blanks for micro drills with an outer diameter of at least 0.7 mm.
- the diameter of the at least one cooling channel is at least 0.03 mm.
- the slope is up to 400 mm.
- the diameter of the cooling channels can be up to 5 mm.
- the diameters of the cooling channels are typically between 1.5 mm and 3 mm.
- a cutting tool blank according to the invention or a cutting tool according to the invention having at least two regions of hard metal which differ from one another with regard to their mechanical properties, preferably hardness and / or bending strength and / or toughness, is characterized in that the at least two regions of hard metal at least are arranged in sections to each other so that the first region of the at least two areas of hard metal at least partially within the the second region of the at least two regions is made of cemented carbide and that between the at least two regions of cemented carbide with respect to the binder content is a transition region with a rising from the first region to the second region course, and that based on the hardness of a transition region with a in the direction of second range decreasing hardness profile is present.
- a particularly preferred cutting tool blank or particularly preferred cutting tool is provided which has at least one inner, preferably wired cooling channel.
- the first region has a higher hardness than the second region. This can be achieved for example by a lower binder content and / or a smaller grain size.
- the inner, harder region can be in the finished cutting tool that region which has the cutting edges or a region of the cutting edges. If at least one cooling channel is provided, this should preferably also be arranged in the inner region.
- the region carrying the cutting edges or a cutting region is essentially free of the joining zone. This is in addition to the higher hardness additionally favorable for the mechanical properties of the cutting or a cutting area bearing area.
- the inner region in the finished cutting tool has a lower binder content than the outer region
- the outer region with higher binder content forming the shank has a high toughness and good damping properties.
- the compressive stresses introduced by the method according to the invention with different binder contents bring about a particularly secure connection of the outer and inner regions to the joining zone.
- a tool bevel is formed on the sintered cutting tool such that flutes or cutting edges are formed along a longitudinal section in the first region (hard core) and along an adjacent longitudinal section in the second region (tough shell).
- the front (more stressed) cutting edges are also formed by the harder core; however, the laterally located cutting edges (which form a countersink area) are of the tougher shell.
- the binder content can be measured, for example, by chemical analysis methods such as X-ray fluorescence analysis or energy dispersive X-ray spectroscopy (EDX).
- chemical analysis methods such as X-ray fluorescence analysis or energy dispersive X-ray spectroscopy (EDX).
- the hardness can be measured, for example, by hardness measurement according to Vickers according to ISO 3878, for example in the range HV1 to HV30.
- a preferred embodiment of the invention relates to a Zerspanungswerkmaschinemaschinerohling, preferably for a drill or cutter, more preferably for a cutting tool with at least one inner cooling channel, which may be straight or wired.
- Another preferred embodiment relates to such a cutting tool, ie a further processed blank.
- the invention is particularly advantageous for the production of cutting tool blanks or cutting tools used, which are provided with at least one inner wired cooling channel.
- wired cooling channels are usually manufactured by means of extrusion molding.
- a disadvantage of the prior art is that - due to the production by extrusion - the production of strong twisting or, in other words, a large angle of twist was difficult because the Umformnect an extruded material is limited.
- that part of the blank (first hard metal blank) which is to have the at least one inner wired cooling channel and a smaller outer diameter than the finished blank may be separately produced. Due to the smaller diameter of the at least one cooling channel having, first carbide blank, the production of the twist or pitch of the carbide blank, Zerspanungstechnikmaschinemaschinerohlings or the finished cutting tool can be simplified. After the separate sintering of the sleeve-shaped part of the blank (second hard metal blank) and the rod-shaped part of the blank (first carbide blank) comprising the at least one cooling channel, both parts can be joined by the method according to the invention to form a composite body in which the first region comprises the at least one Cooling channel and radially considered at least partially located within the second region.
- the outside diameter of the first hard metal blank (in relation to the method) or of the first area (with respect to the cutting tool blank or the cutting tool) is greater than or equal to 0.4 mm to 20 mm, preferably 0.7 mm to 10 mm and / or the outer diameter of the first hard metal blank (with respect to the method) or the second portion (with respect to the cutting tool blank or the cutting tool) in a range of 2 mm to 35 mm. More preferably, the application for micro or micro drills having an outer diameter of the first carbide blank between 0.4 mm and 3 mm.
- Fig. 3a, b a first embodiment of a sintered according to the invention
- Fig. 4a, b a second embodiment of a sintered according to the invention
- FIG. 6a, b a fourth embodiment of a sintered according to the invention
- Fig. 7a, b a fifth embodiment of a sintered according to the invention
- Fig. 9 is a schematic representation of the method according to the invention, Fig. 10 resulting from the method of the preceding figure
- Fig. 11 a is a schematic representation of an embodiment of a
- FIG. 12a a further schematic representation of an embodiment of a
- Cutting tool. 1 relates to an inventive method for producing a composite body 3 made of hard metal, using at least two carbide blanks 1, 2, which differ from each other in relation to a binder content and / or a grain size of the hard material phase.
- the at least two carbide blanks 1, 2 are arranged radially to each other before Sinterglagen so that a first hard metal blank 1 of at least two carbide blanks 1, 2, which has a lower binder content and / or a smaller grain size, viewed radially at least in sections within an opening. 9 or a cavity 10 of the second hard metal blank 2 of the at least two carbide blanks 1, 2 is located. It can be seen in Fig. 1 that the at least two carbide blanks 1, 2 were arranged with radial play to each other in such a way that between the at least two carbide blanks 1, 2 Although at least one linear or planar contact zone, but at least partially a gap. 6 between the at least two carbide blanks 1, 2 remains.
- a liquid phase of the binder of at least two carbide blanks 1, 2 is prepared and maintained until by diffusion of binder of the first hard metal blank 1 of at least two carbide blanks 1, 2 swelled so far and the second hard metal blank 2 of the at least two carbide blanks 1, 2 has shrunk so far that the at least two hard metal blanks 1, 2 are connected to one another in a material-tight manner after sintering joining (see FIG. 2).
- FIGS. 3a to 7a show in each case exemplary embodiments of composite bodies 3 according to the invention in the form of blanks for a cutting tool 7 (see Fig. 10) in a sectional view through a plane which contains a longitudinal axis LA of the composite body 3.
- FIGS. 3b to 7b show associated perspective views, wherein for the sake of better recognition, a dashed representation of hidden and thus invisible lines has been dispensed with.
- the first embodiment of Fig. 3a, b shows a composite body 3, in which the first hard metal blank 1 of the at least two carbide blanks 1, 2 completely within the opening 9 or the cavity 10 of the second hard metal blank 2 of the at least two carbide blanks 1, 2 is located.
- FIGS. 4 a, b to 7 a, b each show a composite body 3, in which the at least two hard metal blanks 1, 2 are arranged axially to each other along the longitudinal axis LA prior to sintering, so that the one carbide blank 1, 2 of the at least two carbide blanks 1, 2 seen axially in sections before the other carbide blank 1, 2 of the at least two carbide blanks 1, 2 is located.
- a straight cooling channel 8 running along the longitudinal axis LA is provided for a cooling liquid.
- the first hard metal blank 1 projects in sections out of the second hard metal blank 2. Unlike shown, the first hard metal blank 1 can also be flush with the second hard metal blank 2 (FIG. 3 a) or can also be arranged sunk in it.
- FIGS. 5a, b two helical cooling channels 8 extending along the longitudinal axis LA are provided for a cooling liquid.
- the first hard metal blank 1 projects in sections from the second hard metal blank 2. However, it can also be provided that the first hard metal blank 1 is flush with the second hard metal blank 2.
- b is a along the longitudinal axis LA extending, straight cooling channel 8 is provided for a cooling liquid, branch off from which transverse to the longitudinal axis LA two cooling channels 8 and open into outlet openings 1 1 for the cooling liquid.
- the first carbide blank 1 do not extend along the longitudinal axis LA of the second hard metal blank 2, but in an area parallel thereto or at an angle obliquely thereto.
- the first hard metal blank 1 could for example also be arranged in at least one of the laterally arranged on the composite body 3 outlet openings 1 1 and thus, for example, act only as a stopper or as an outlet nozzle, throttle or the like.
- a step 12 is provided in the second hard metal blank 2 (before sintering joining) or in the second region 4 (after sintering joining) which forms an axial stop for the first hard metal blank 1 (before sintering joining) represents the first area 5 (after sintering).
- a stop could also be provided in the other embodiments.
- FIG. 8 is intended to schematically illustrate the diffusion process, which results in binder particles 13 diffusing from a region of higher binder concentration / higher binder content in the first hard metal blank 1 into a region of lower binder concentration in the second hard metal blank 2.
- This balancing of the binder content (Co content) also results in a volume and / or mass flow during diffusion.
- FIG. 9 The individual steps of a method according to the invention are shown in FIG. 9:
- step 14 the two carbide blanks 1, 2 are prepared, for. B. by a pressing and subsequent sintering process. Subsequently, for reasons of higher precision, optionally in step 15, a grinding process is carried out on one or both carbide blanks 1, 2. It may also be provided that at least one of the two carbide blanks 1, 2 is produced by an eroding process, the precision required for sintering joining is generated directly by the eroding method with respect to the geometry and / or the joint surface. A post-processing step such as grinding or honing can be omitted or only partially done.
- the two carbide blanks are arranged or aligned with each other in step 16 with radial play and sintered together in this arrangement in step 17.
- the resulting composite body 3 can be further processed in step 18, for. B. to a Zerspanungstechnikmaschinerohling or cutting tool 7 (see Fig .. 10), in which a shaft through the second hard metal blank 2 and 1 1 cutting through the first hard metal blank 1 are formed.
- a Zerspanungstechnikmaschinerohling or cutting tool 7 see Fig .. 10
- a shaft through the second hard metal blank 2 and 1 1 cutting through the first hard metal blank 1 are formed.
- temperatures of, for example, 1 100 ° C to 1600 ° C are used.
- the sintering in step 17 can take place under pressure, with pressures between 0 bar and 1000 bar are conceivable.
- the particle sizes of the binder are included between about 0.4 mhh - about 5 pm, the weight-based binder content is between 3% by weight and 20% by weight.
- Fig. 1 a shows the two carbide blanks 1, 2 with different binder content.
- the binder content of the first hard metal blank 1 is about 6% by weight
- the binder content of the second hard metal blank 2 is about 10% by weight.
- Individual measurement points MP represent, for example and schematically, the binder content, the hardness or the toughness of the carbide blanks 1, 2, which is explained in greater detail in FIG.
- FIG. 11b shows in a diagram the different measured values of the measuring points MP from FIG. 11a along the abscissa (x-axis).
- the numbers on the x-axis do not directly indicate a radial distance, but the number of the measuring point.
- the hardness in Vickers (HV) is given in a range between 1560 and 1720.
- the fracture toughness of the material (Ki c ) is shown on the right along the ordinate (y-axis). The value extends in a range from 9.5 to 11, 0 [MPa * m 0 ' 5 ].
- the first (inner) area 5 with the binder content of 6% by weight can be seen; on the left, the second (outer) area 4 with the binder content of 10% by weight can be seen.
- the particle size of the binder, in this embodiment tungsten carbide, is less than 1 pm.
- the measuring points represented in the form of triangles show the hardness in Vickers (HV), the measuring points shown in the form of circles show the fracture toughness (Ki c ). It can thus be seen from the diagram and the measurement that differences in hardness and fracture toughness result between the first region 5 and the second region 4, which is due to the different binder content.
- FIG. 12a also schematically shows another embodiment with a different binder content in the first region 5. In this case, this is 7.5% by weight.
- the first hard metal blank 1 is produced, for example, in the form of an extrusion process, wherein the at least one cooling channel 8 is co-formed during the extrusion.
- FIG. 13a shows a first hard metal blank 1, on which the helix angle a is registered.
- the helix angle a is determined by the slope of the twisting with respect to the longitudinal axis LA at the outer diameter d r of the first hard metal blank 1.
- the helix angle a is between 15 ° to 60 °.
- ribs on the outer circumference of the first hard metal blank 1 can be seen, which result from extrusion, wherein the outer diameter d r of the first hard metal blank 1 is determined at the area between the ribs.
- the diameter of a cooling channel 8 is indicated by d k .
- FIG. 13 b shows the gradient S, which results from the twist of the at least one cooling channel 8.
- the slope S thus results from the axial offset of the at least one wired cooling channel 8 along the longitudinal axis LA per completed rotation through 360 ° about the longitudinal axis LA. This results in dependence on the helix angle a, a slope S of at least 2.5 mm in extruded carbide blanks 1 for microdrill with an outer diameter d r of at least 0.7 mm.
- the diameter d k of the at least one cooling channel 8 is at least 0.03 mm.
- the slope S is up to 353 mm.
- the diameter d k of the cooling channels is between 2 mm to 5 mm.
- FIG 14a shows a cutting tool blank produced by the method according to the invention with an inner, first and an outer, second region 5, 4, wherein the first region 5 has a greater hardness (and a lower binder content, and thus a smaller thermal expansion coefficient) than that second area 4.
- FIGS. 14b and 14c show the result of a processing step in which, for example by grinding, in the region of an axial end of the Cutting tool blanks according to Fig. 14a, the outer region 4 and the joining zone between the inner and the outer region 5, 4 were substantially completely removed so that the area carrying the cutting or a cutting portion 19 is substantially free of the joining zone.
- the cutting area 19 is arranged exclusively on the inner area 5 in this embodiment of a cutting tool 7.
- the tougher shell (outer region 4) with more favorable damping properties forms the shaft section.
- FIGS. 15a and 15b differs from that of FIGS. 14a-c only insofar as at least one cutting edge extends here on the conical part on the jacket (outer region 4), which can thus serve as countersink.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
- Composite Materials (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Drilling Tools (AREA)
- Powder Metallurgy (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ATGM50038/2018U AT16369U1 (en) | 2018-03-12 | 2018-03-12 | Process for producing a sintered composite body |
PCT/AT2019/060080 WO2019173855A1 (en) | 2018-03-12 | 2019-03-08 | Method for producing a sinter-joined composite body |
Publications (1)
Publication Number | Publication Date |
---|---|
EP3765223A1 true EP3765223A1 (en) | 2021-01-20 |
Family
ID=67209578
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP19712673.3A Pending EP3765223A1 (en) | 2018-03-12 | 2019-03-08 | Method for producing a sinter-joined composite body |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP3765223A1 (en) |
CN (1) | CN112118927B (en) |
AT (1) | AT16369U1 (en) |
WO (1) | WO2019173855A1 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111957973A (en) * | 2020-09-15 | 2020-11-20 | 苏州瑞森硬质合金有限公司 | Production process of light alloy rod with spiral hole inside |
SE545894C2 (en) * | 2021-06-22 | 2024-03-05 | Sandvik Machining Solutions Ab | Method for manufacturing an article comprising cemented carbide and an inserted object |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4710235A (en) * | 1984-03-05 | 1987-12-01 | Dresser Industries, Inc. | Process for preparation of liquid phase bonded amorphous materials |
JPS63125602A (en) * | 1986-11-12 | 1988-05-28 | Sumitomo Electric Ind Ltd | Hard alloy for tool |
US5541006A (en) * | 1994-12-23 | 1996-07-30 | Kennametal Inc. | Method of making composite cermet articles and the articles |
GB2343682B (en) * | 1998-09-16 | 2001-03-14 | Hitachi Powdered Metals | Manufacturing method of sintered composite machine component having inner part and outer part |
DE10300283B3 (en) * | 2003-01-02 | 2004-06-09 | Arno Friedrichs | Hard metal workpiece manufacturing method using extrusion for formation of lesser hardness material into rod-shaped carrier for greater hardness material |
AT7056U1 (en) * | 2003-12-22 | 2004-09-27 | Ceratizit Austria Gmbh | USE OF A TOOL ALLOY FOR TOOLS |
US8637127B2 (en) * | 2005-06-27 | 2014-01-28 | Kennametal Inc. | Composite article with coolant channels and tool fabrication method |
GB2459272A (en) * | 2008-04-15 | 2009-10-21 | Element Six | Diamond enhanced carbide type materials |
DE102008042065A1 (en) * | 2008-09-12 | 2010-03-25 | Robert Bosch Gmbh | Method for producing a component from a composite material and component from a composite material |
US8272816B2 (en) * | 2009-05-12 | 2012-09-25 | TDY Industries, LLC | Composite cemented carbide rotary cutting tools and rotary cutting tool blanks |
KR102210170B1 (en) * | 2013-03-15 | 2021-01-29 | 산드빅 인터렉츄얼 프로퍼티 에이비 | Method of joining sintered parts of different sizes and shapes |
US20160263665A1 (en) * | 2015-03-11 | 2016-09-15 | Kennametal lnc. | Composite blanks and tooling for cutting applications |
-
2018
- 2018-03-12 AT ATGM50038/2018U patent/AT16369U1/en unknown
-
2019
- 2019-03-08 CN CN201980018641.0A patent/CN112118927B/en active Active
- 2019-03-08 EP EP19712673.3A patent/EP3765223A1/en active Pending
- 2019-03-08 WO PCT/AT2019/060080 patent/WO2019173855A1/en unknown
Also Published As
Publication number | Publication date |
---|---|
AT16369U1 (en) | 2019-07-15 |
WO2019173855A1 (en) | 2019-09-19 |
CN112118927A (en) | 2020-12-22 |
CN112118927B (en) | 2023-07-04 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1846186B1 (en) | Deep hole drill | |
DE102013104222A1 (en) | Hybrid cutting tool, chip removal section and method of making a cutting tool | |
EP3247813B1 (en) | Hard metal-cermet composite material and method for the production thereof | |
EP2121226A1 (en) | Cutting element for a rock drill and method for producing a cutting element for a rock drill | |
DE3309860A1 (en) | DRILLING TOOL | |
EP2200773B1 (en) | Only partly ground tool rod made of sintered material | |
EP2992978B1 (en) | Die module set for pressing tools for producing screws | |
DE102009043850A1 (en) | Tool | |
WO2010034410A1 (en) | Tool for machining | |
WO2019173855A1 (en) | Method for producing a sinter-joined composite body | |
WO2018166889A1 (en) | Tool body and a method for the production thereof | |
DE19604061A1 (en) | Core storey | |
DE2733925C2 (en) | Process for making composite extrusions | |
EP0458774B2 (en) | Hard metal, or ceramics, blank and method and tool for manufacture of same | |
DE102013210355A1 (en) | Cutting tool and method for producing a cutting tool | |
DE102011080225A1 (en) | Method and treatment element blank for producing a treatment element for a screw machine | |
DE102008052743A1 (en) | Tool i.e. twist drill, for machining workpiece, has regions provided along axial extension of tool, geometrically defined cutting edge and center axis, where regions are alternately made of ductile and hard materials | |
DE102011001177B4 (en) | Multi-edged drilling tool | |
DE102005009030A1 (en) | Chipping tool for micro-precision work has shaft region with narrow part adjacent to cutting region | |
DE102017208039B4 (en) | Process for manufacturing a rotary tool and rotary tool | |
DE10202954B4 (en) | Method for producing a rod-shaped drill made of hard metal or ceramic | |
EP3862135A1 (en) | Focusing tube and use of same | |
DE102021112643A1 (en) | Process for producing a bimetal screw, base body of a bimetal screw and bimetal screw | |
EP3458213B1 (en) | Method for the powder-metallurgical production of a rod-like body | |
DE4413295C1 (en) | Cobalt-cemented tungsten carbide body prodn. |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: UNKNOWN |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE |
|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE |
|
17P | Request for examination filed |
Effective date: 20200826 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
AX | Request for extension of the european patent |
Extension state: BA ME |
|
DAV | Request for validation of the european patent (deleted) | ||
DAX | Request for extension of the european patent (deleted) | ||
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: EXAMINATION IS IN PROGRESS |
|
17Q | First examination report despatched |
Effective date: 20230220 |