WO2012128708A1 - Method of preparation of a metal/cemented carbide functionally graded material - Google Patents
Method of preparation of a metal/cemented carbide functionally graded material Download PDFInfo
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- WO2012128708A1 WO2012128708A1 PCT/SE2012/050303 SE2012050303W WO2012128708A1 WO 2012128708 A1 WO2012128708 A1 WO 2012128708A1 SE 2012050303 W SE2012050303 W SE 2012050303W WO 2012128708 A1 WO2012128708 A1 WO 2012128708A1
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- WO
- WIPO (PCT)
- Prior art keywords
- sintering
- layer
- temperature
- fgm
- electrically insulating
- Prior art date
Links
- 239000000463 material Substances 0.000 title claims abstract description 95
- 238000000034 method Methods 0.000 title claims abstract description 65
- 238000002360 preparation method Methods 0.000 title claims abstract description 7
- 229910052751 metal Inorganic materials 0.000 title claims description 23
- 239000002184 metal Substances 0.000 title claims description 23
- 238000005245 sintering Methods 0.000 claims abstract description 85
- 238000002844 melting Methods 0.000 claims abstract description 26
- 230000008018 melting Effects 0.000 claims abstract description 26
- 238000002490 spark plasma sintering Methods 0.000 claims abstract description 26
- 239000002131 composite material Substances 0.000 claims abstract description 14
- 239000000203 mixture Substances 0.000 claims abstract description 13
- 238000011068 loading method Methods 0.000 claims abstract description 7
- 239000010959 steel Substances 0.000 claims description 45
- 229910000831 Steel Inorganic materials 0.000 claims description 44
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 claims description 27
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 23
- 229910002804 graphite Inorganic materials 0.000 claims description 21
- 239000010439 graphite Substances 0.000 claims description 21
- 239000010941 cobalt Substances 0.000 claims description 12
- 229910017052 cobalt Inorganic materials 0.000 claims description 12
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical group [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 12
- 239000011230 binding agent Substances 0.000 claims description 11
- 238000007731 hot pressing Methods 0.000 claims description 10
- CPLXHLVBOLITMK-UHFFFAOYSA-N Magnesium oxide Chemical compound [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 claims description 8
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 8
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 claims description 8
- 239000011888 foil Substances 0.000 claims description 8
- 229910052582 BN Inorganic materials 0.000 claims description 7
- PZNSFCLAULLKQX-UHFFFAOYSA-N Boron nitride Chemical compound N#B PZNSFCLAULLKQX-UHFFFAOYSA-N 0.000 claims description 7
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 7
- 229910045601 alloy Inorganic materials 0.000 claims description 6
- 239000000956 alloy Substances 0.000 claims description 6
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 5
- 229910052581 Si3N4 Inorganic materials 0.000 claims description 4
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 4
- PMHQVHHXPFUNSP-UHFFFAOYSA-M copper(1+);methylsulfanylmethane;bromide Chemical compound Br[Cu].CSC PMHQVHHXPFUNSP-UHFFFAOYSA-M 0.000 claims description 4
- 239000000395 magnesium oxide Substances 0.000 claims description 4
- 239000000377 silicon dioxide Substances 0.000 claims description 4
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 claims description 4
- 229910001092 metal group alloy Inorganic materials 0.000 claims description 3
- 229910052759 nickel Inorganic materials 0.000 claims description 3
- 239000010410 layer Substances 0.000 description 59
- 239000000843 powder Substances 0.000 description 23
- 229910009043 WC-Co Inorganic materials 0.000 description 7
- 239000000919 ceramic Substances 0.000 description 7
- 239000007795 chemical reaction product Substances 0.000 description 6
- 238000004519 manufacturing process Methods 0.000 description 6
- 239000002245 particle Substances 0.000 description 6
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- 229910000851 Alloy steel Inorganic materials 0.000 description 3
- 238000002474 experimental method Methods 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 238000001513 hot isostatic pressing Methods 0.000 description 3
- 239000007791 liquid phase Substances 0.000 description 3
- 239000012071 phase Substances 0.000 description 3
- 239000010935 stainless steel Substances 0.000 description 3
- 229910001220 stainless steel Inorganic materials 0.000 description 3
- 229910001030 Iron–nickel alloy Inorganic materials 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 230000008094 contradictory effect Effects 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 229910003460 diamond Inorganic materials 0.000 description 2
- 239000010432 diamond Substances 0.000 description 2
- 239000011810 insulating material Substances 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 230000003287 optical effect Effects 0.000 description 2
- 238000013021 overheating Methods 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 229910001256 stainless steel alloy Inorganic materials 0.000 description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 239000010937 tungsten Substances 0.000 description 2
- 238000007088 Archimedes method Methods 0.000 description 1
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000005219 brazing Methods 0.000 description 1
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- 238000005520 cutting process Methods 0.000 description 1
- 239000008367 deionised water Substances 0.000 description 1
- 229910021641 deionized water Inorganic materials 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
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- 238000005553 drilling Methods 0.000 description 1
- 239000012777 electrically insulating material Substances 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 238000000265 homogenisation Methods 0.000 description 1
- 238000007654 immersion Methods 0.000 description 1
- 238000011065 in-situ storage Methods 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 239000011229 interlayer Substances 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- BWHLPLXXIDYSNW-UHFFFAOYSA-N ketorolac tromethamine Chemical compound OCC(N)(CO)CO.OC(=O)C1CCN2C1=CC=C2C(=O)C1=CC=CC=C1 BWHLPLXXIDYSNW-UHFFFAOYSA-N 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 238000005065 mining Methods 0.000 description 1
- 239000003129 oil well Substances 0.000 description 1
- 238000000399 optical microscopy Methods 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 238000010422 painting Methods 0.000 description 1
- 239000008188 pellet Substances 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 238000004663 powder metallurgy Methods 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 239000011214 refractory ceramic Substances 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000005488 sandblasting Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
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- 239000002344 surface layer Substances 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- 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
- B22F3/105—Sintering only by using electric current other than for infrared radiant energy, laser radiation or plasma ; by ultrasonic bonding
-
- 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
- B22F7/008—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 characterised by the composition
-
- 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
- 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
- B22F7/04—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 with one or more layers not made from powder, e.g. made from solid metal
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/64—Burning or sintering processes
- C04B35/645—Pressure sintering
-
- 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
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C33/00—Making ferrous alloys
- C22C33/02—Making ferrous alloys by powder metallurgy
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C33/00—Making ferrous alloys
- C22C33/02—Making ferrous alloys by powder metallurgy
- C22C33/0257—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements
- C22C33/0278—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5%
- C22C33/0292—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5% with more than 5% preformed carbides, nitrides or borides
-
- 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
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
- B22F2998/10—Processes characterised by the sequence of their steps
-
- 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
Definitions
- the present invention relates generally to a method of preparation of a metal / cemented carbide, such as a steel / cemented tungsten carbide, functionally graded material shape by sintering, preferably by spark plasma sintering (SPS) .
- a metal / cemented carbide such as a steel / cemented tungsten carbide
- SPS spark plasma sintering
- the common cemented carbide graded tools are usually fabricated by making tungsten carbide (WC, often referred to as hard metal) bi-layers with different content of binder phase, such as cobalt (Co), and/or various tungsten carbide grain sizes and sinter-bonding them with steel.
- WC tungsten carbide
- binder phase such as cobalt (Co)
- Co cobalt
- This process is metastable and the graded microstructure is very sensitive to the sintering conditions such as sintering temperature, holding time and other factors. It is usually difficult to make a final material with a cobalt gradient because of the flow of liquid phase cobalt and its homogenization during sintering at high temperature.
- a functionally graded material is a material design concept which provides a joining solution to relieve the residual thermal stresses and to incorporate incompatible properties of two dissimilar materials, such as the heat, the wear, and the oxidation resistance of a refractory ceramic, such as for example cemented carbide, with the high toughness, the high strength, and the machinability of a metal, such as steel, by placing graded composite interlayers of the two materials between the pure end layers.
- microstructure with the composition change The matrix is replaced gradually from metal to ceramic, and the microstructure profile varies concurrently from (i) a pure metal, (ii) a metal-rich region (the ceramic particles are dispersed in metal matrices), (iii) intertwined composites (networks of metal and ceramic phases with comparable volume fractions), (iv) a ceramic-rich region (the metal matrix diminishes and turns into discrete phases or particles in ceramic matrices), to finally (v) a pure ceramic.
- FGMs can be prepared through different techniques such as conventional powder metallurgy processing, vapour deposition and sintering techniques.
- the spark plasma sintering method also referred to as for example field assisted sintering technique (FAST) is a powerful sintering technique which allows very rapid heating under high mechanical pressures. This process, hereafter referred to as SPS, has proved to be very well suited for the production of functionally graded materials.
- Other sintering techniques could possibly also be used for preparing FGMs, such as for example direct hot-pressing, hot-pressing or hot isostatic pressing.
- tungsten carbide has the higher sintering temperature, approximately 200°C higher than steel. It is necessary to sinter the FGM component at a proper temperature at which the whole component can be fully sintered.
- the appropriate sintering temperature of tungsten carbide by SPS is generally 1 00- 200°C higher than this limit. The sintering temperature is influenced by the tungsten carbide grain size and the content of binder material.
- An object of the present invention is to prepare a metal / cemented carbide functionally graded material by sintering, preferably by spark plasma sintering (SPS), in order to combine a tough metal base with a hard carbide surface in an economical way.
- the functionally graded material can be a steel/cemented tungsten carbide (steel / WC-Co FGM) .
- the end product is a fully dense
- compositionally gradient shape with pure metal and pure cemented carbide alloy as two end surfaces pure metal layer / x number of composite layers / pure cemented carbide layer
- Another end product can be a dense compositionally gradient shape with pure metal as one end surface and a metal-cemented carbide composite on the other end surface.
- the term "cemented" means that the carbide alloy powder includes an amount of metallic binder, such as for example cobalt, nickel, iron, or their alloys. During the sintering process, the tungsten carbide particles are captured in the metallic binder and cemented together by forming a metallurgical bond.
- metallic binder such as for example cobalt, nickel, iron, or their alloys.
- the base layer can be a steel alloy, a stainless steel alloy or other metallic material.
- the invention relates to a method of preparation of a FGM shape with a first surface comprising up to 1 00% of a first material and a second surface comprising up to 1 00% of a second material.
- the method is characterized in that it comprises the steps of: selecting the first material with a first sintering temperature and a first melting temperature and the second material with a second sintering temperature and a second melting temperature , wherein the first melting temperature is higher than the second melting temperature, loading a first layer of the first material in a sintering mold referred to as die, adding at least one intermediate layer on the first layer, the intermediate layer comprising a mix of the first and second material creating an intermediate graded composite region, loading a second layer of the second material on the at least one intermediate layer, adding an electrically insulating layer on the second layer of the second material, adding a pressure on the layers creating a FGM shape, and sintering the whole shape under a predetermined time, pressure and temperature.
- the method can further comprise adding an electrically insulating layer before loading the first layer of the first material.
- the method can comprise adding an electrically insulating layer on all surfaces around the material to be sintered.
- the layers are preferably added as powders, but solid blocks of the pure materials and composites can also be used.
- the electrically insulating layer added on the second material enforces the current from the sintering process to flow only through the die and not through the second layer of the FGM- shape.
- the temperature increase in the second layer becomes limited.
- the temperature in the first layer is high enough to sinter the first material but it does not exceed the melting temperature of the second material.
- the resulting end product from the process is a near fully dense FGM without any melted material.
- said first material is a cemented carbide and said second material is a metal or metal alloy, preferably said first material is cemented tungsten carbide and said second material is steel.
- the first material includes a metallic binder.
- the metallic binder may be cobalt and the amount of cobalt can be between 5 and 25wt%.
- the binder can also be nickel, iron, or their alloys.
- said electrically insulating layer is chosen from any of the materials boron nitride, alumina, zirconia, silicon nitride, aluminum nitride, silica, magnesia.
- the steel/cemented tungsten carbide FGM is sintered, the most preferred insulating material is boron nitride.
- the insulating layer can either be a powder or a solid disc.
- the insulating layer can also be added as liquid through spraying or painting.
- the sintering takes place under a sintering temperature of between 1 000 °C and 1 200 °C, preferably between 1 050°C and 1 1 50°C, more preferably between 1 070 °C and 1 1 20°C and most preferably 1 1 00 °C, a pressure of between 20 and 1 20 MPa, preferably between 50 and 90 MPa, more preferably between 65 and 80 MPa and most preferably 75 MPa, and a sintering time of between 5 and 30 min, preferably between 1 0 and 20 min, more preferably 1 5 min.
- the sintering takes place under a sintering temperature of between 900 °C and 1 200 °C, preferably between 950°C and 1 1 50°C, a pressure of between 20 and 1 20 MPa, preferably between 30 and 75 MPa, and a sintering holding time of between 2 and 30 min, preferably between 5 and 20 min .
- the shape is sintered using one of the following sintering techniques; spark plasma sintering (SPS) or direct hot pressing (DHP).
- Possible sintering techniques are also hot pressing (HP) or hot isostatic pressing (HIP). But preferably, spark plasma sintering (SPS) is used.
- HP hot pressing
- HIP hot isostatic pressing
- SPS spark plasma sintering
- the sintering pressure is applied through two punches arranged on opposite sides of the loaded material in the die.
- the dies are lined with a graphite foil and this is also inserted between the first and second surface of the FGM shape and the two punches.
- the dies are graphite dies surrounded by graphite felt.
- the dies are surrounded by a carbon fiber composite material (CFC) .
- the graphite foil ensures good electric and thermal contacts between the die and the punches and also facilitates removal of the sintered compact without damaging the die or punch surfaces.
- the dies are lined with a layer of the insulating material.
- the method further comprises the step: removing the electrically insulating layer after the sintering process has been performed.
- Removal of the remains of the insulating layer after sintering can be performed through sand blasting or similar.
- the end product is a pure FGM ready to be manufactured into a cemented carbide tool.
- the end product can also be a finished cemented carbide tool with no need for further processing.
- All individual features of the above methods may be combined or exchanged unless such combination or exchange is clearly contradictory.
- the sintering conditions such as holding time and pressure, depend on the size of the FGM shape and the die dimension .
- Fig. 1 shows a longitudinal cross-section of a FGM die setup
- Table 1 lists the relative densities and the sintering conditions during sintering of individual steel and cemented carbide powders by SPS
- Table 2 lists the relative densities and the sintering conditions during sintering of steel / WC-Co FGM compacts by SPS at 1 1 00°C/75MPa/l 5min/50°C/min.
- the read temperatures mentioned in the description can differ between different sintering furnaces depending on how the temperature is measured.
- the temperature is measured with a pyrometer focused on a hole on the outer surface of the die.
- FIG. 1 shows a longitudinal cross-section of the die setup for producing a FGM-shape 4 according to the invention.
- Powders of at least a first and a second material M l , M2 are sintered under a pressure created by punches 3a, 3b in a die 1 , preferably a graphite die.
- the sintering process creates samples of the FGM shape 4, for example cylindrical-shaped discs. Other shapes including any polygonal-shaped discs can also be sintered.
- the sintering process is performed by spark plasma sintering under a high temperature and pressure on the closed die to create a dense/near fully dense FGM-shape.
- the powder layers to be sintered can be cold-pressed prior to the sintering.
- the sintering takes preferably place at a sintering temperature of between 1 000 °C and 1 200 °C, preferably between 1 050°C and 1 1 50°C, more preferably between 1 070 °C and 1 1 20°C and most preferably 1 1 00 °C, a pressure of between 20 and 1 20 MPa, preferably between 50 and 90 MPa, more preferably between 65 and 80 MPa and most preferably 75 MPa, and a sintering time of between 5 and 30 min, preferably between 1 0 and 20 min, more preferably 1 5 min.
- Different sintering techniques can be used, such as for example spark plasma sintering (SPS) or direct hot pressing (DHP) .
- SPS spark plasma sintering
- DHP direct hot pressing
- Other sintering techniques are also hot pressing (HP) or hot isostatic pressing (HIP) .
- the FGM shape has a first layer 11 with a first surface 4a comprising up to 1 00% of the first material M l and a second layer 12 with a second surface 4b comprising up to 1 00% of the second material M2.
- a third layer 13 comprising a mix of the first and second material M l , M2 is added.
- the at least one third layer is creating an intermediate graded composite region l c.
- the numbers of graded layers are between two and ten, with a 50- 1 0vol% gradient change.
- other numbers of layers are of course also possible, as is a non-linear gradient change in composition .
- the first material M l has a first sintering temperature Ts l and a first melting temperature Tm l and the second material M2 has a second sintering temperature Ts2 and a second melting temperature Tm2.
- the sintering temperature during the SPS- process needs to reach the first sintering temperature Ts l of the first material but not exceed the second melting temperature Tm2 of the second material. Otherwise, this can lead to melting of the second material M2.
- an electrically insulating layer 5 of an electrically insulating powder is placed on the second surface 4b of the FGM-shape 4, between the second layer 12 of the second material M2 and the graphite punch 3b.
- the function of the electrically insulating powder is to enforce the current to flow only through the die and not through the second layer 12 of the FGM-shape.
- the first material M l is preferably a cemented carbide and the second material M2 a metal. More preferably, the first material M l is cemented tungsten carbide and the second material M2 is steel.
- the first material M l includes a metallic binder such as for example cobalt Co or an iron-nickel alloy Fe-Ni.
- the electrically insulating layer can be chosen from any of the electrically insulating materials of boron nitride, alumina, zirconia, silicon nitride, aluminum nitride, silica, magnesia, but preferably boron nitride BN is used. This material can either be a powder or a solid disc.
- the inner walls of the dies 1 can be lined with thin graphite foil 2 inserted between the shape 4 and the two punches 3a, 3b.
- a graphite foil can also be inserted between the first and second surface l a, 1 b of the FGM shape 1 and the two punches (3a, 3b) .
- the graphite foil 2 ensures good electric and thermal contacts between the die 1 and the punches 3a, 3b, and also facilitates removal of the sintered compact without damaging the die 1 or punch surfaces 3a, 3b.
- the graphite dies 1 can be surrounded by graphite felt 6 to reduce the heat loss by radiation from the outer die surface.
- the temperature can for example be measured at a hole 7 in the graphite die 6.
- the steel and tungsten carbide composite powder mixtures were dry mixed at room temperature for one hour in plastic containers with tungsten carbide milling rods on a jar rolling mill.
- the steel / WC-Co FGMs were designed to comprise four composite interlopers between the pure steel and tungsten carbide layers at the two ends.
- the composites consisted of steel - cemented carbide mixtures with a 20vol% gradient change (i.e. 80/20, 60/40, 40/60, 20/80 vol%).
- the total six layers were loaded in order, layer by layer, in a graphite die and a BN insulating layer was interposed between the punch and the steel layer.
- a steel / cemented tungsten carbide FGM disc ( ⁇ 20x6 mm) was successfully sintered according to the above conditions. It was fully dense and no cracks could be observed. Experiments have also successfully been performed with discs of the sizes 020x8.25 mm and I 2x7.25 mm.
- the samples 4 were sintered with and without an electrically insulating layer 5 of boron nitride powder BN placed between the steel powder to be sintered and the graphite punches 3a, 3b.
- the powders inside the closed dies were first cold-pressed. Then, the samples were sintered in vacuum in a spark plasma sintering unit (SPS-5.40 MK-VI system from SPS Syntex Inc, Japan). Once the p re-determined SPS-pressure was applied, the dies were heated to 600 °C in 3 minutes and then heated further at a rate of 50-1 00 °C/min to the desired holding temperature. The holding time was between 5 and 1 5 minutes. The temperature was measured with an optical pyrometer focused on a hole 7 at the half height of the outer surface of the die.
- SPS-5.40 MK-VI system from SPS Syntex Inc, Japan
- the resulting sintered discs were blasted to remove the residues of graphite foil and BN layer, and then polished with # 1 20 silicon carbide grinding paper.
- the relative densities were measured by Archimedes method (European Standard EN 993-1 ) using deionized water as the immersion medium.
- the possible existence of surface cracks in the sintered pellets was examined visually and through optical microscopy (Olympus SZxl 2 model, Olympus Optical Co. Ltd, Japan).
- Tables 1 and 2 The relative densities and the sintering conditions are listed in Tables 1 and 2, wherein Table 1 lists sintering of individual steel and cemented carbide powders by SPS and Table 2 lists sintering of steel / WC-Co FGM compacts by SPS at 1 1 00°C/75MPa/1 5min/50°C/min .
Abstract
The invention relates to a method of preparation of a FGM shape with a first surface comprising up to 100% of a first material and a second surface comprising up to 00% of a second material using sintering, preferably spark plasma sintering (SPS). The method comprises the steps of: selecting the first material with a first sintering temperature and a first melting temperature and the second material with a second sintering temperature and a second melting temperature, wherein the first melting temperature is higher than the second melting temperature,loading a first layer of the first material in a die, adding at least one intermediate layer on the first layer, the intermediate layer comprising a mix of the first and second material creating an intermediate graded composite region and loading a second layer of the second material on the at least one intermediate layer. The invention is characterized in that an electrically insulating layer is added on the second layer of the second material which enforces the current from the sintering process to flow only through the die and not through the second layer of the FGM-shape.
Description
METHOD OF PREPARATION OF A METAL / CEMENTED CARBIDE FUNCTIONALLY GRADED MATERIAL
Technical field
[0001 ] The present invention relates generally to a method of preparation of a metal / cemented carbide, such as a steel / cemented tungsten carbide, functionally graded material shape by sintering, preferably by spark plasma sintering (SPS) .
Background art
[0002] Previous attempts have been made to consolidate a steel / cemented tungsten carbide gradient component (as a complete tool without brazing) which can be used as a carbide tool in areas where components are exposed to excessive wear and shocks, such as cutting picks used in the mining industry, and wear graders in the road maintenance applications e.g. snow plows and road cleaning, etc. Preferred materials to combine are for example steel and cemented tungsten carbide to offer a tough steel base with a hard and wear resistant carbide surface.
[0003] The common cemented carbide graded tools are usually fabricated by making tungsten carbide (WC, often referred to as hard metal) bi-layers with different content of binder phase, such as cobalt (Co), and/or various tungsten carbide grain sizes and sinter-bonding them with steel. This process is metastable and the graded microstructure is very sensitive to the sintering conditions such as sintering temperature, holding time and other factors. It is usually difficult to make a final material with a cobalt gradient because of the flow of liquid phase cobalt and its homogenization during sintering at high temperature.
[0004] An alternative is to make a gradient composition which changes from the steel base to the cemented carbide surface, i .e. a functionally graded material (FGM).
[0005] A functionally graded material (FGM) is a material design concept which provides a joining solution to relieve the residual thermal stresses and to incorporate incompatible properties of two dissimilar materials, such as the heat, the wear, and the oxidation resistance of a refractory ceramic, such as for example cemented carbide, with the high toughness, the high strength, and the machinability of a metal, such as steel, by placing graded composite interlayers of the two materials between the pure end layers.
[0006] Generally, in a metal / ceramic FGM system with a graded region consisting of several composite layers, there is a gradual variation of the
microstructure with the composition change. The matrix is replaced gradually from metal to ceramic, and the microstructure profile varies concurrently from (i) a pure metal, (ii) a metal-rich region (the ceramic particles are dispersed in metal matrices), (iii) intertwined composites (networks of metal and ceramic phases with comparable volume fractions), (iv) a ceramic-rich region (the metal matrix diminishes and turns into discrete phases or particles in ceramic matrices), to finally (v) a pure ceramic.
[0007] FGMs can be prepared through different techniques such as conventional powder metallurgy processing, vapour deposition and sintering techniques. The spark plasma sintering method (SPS), also referred to as for example field assisted sintering technique (FAST), is a powerful sintering technique which allows very rapid heating under high mechanical pressures. This process, hereafter referred to as SPS, has proved to be very well suited for the production of functionally graded materials. Other sintering techniques could possibly also be used for preparing FGMs, such as for example direct hot-pressing, hot-pressing or hot isostatic pressing.
[0008] For materials such as steel / tungsten carbide, there is a difference in the materials' sintering temperatures. In this case tungsten carbide has the higher sintering temperature, approximately 200°C higher than steel. It is necessary to sinter the FGM component at a proper temperature at which the whole component
can be fully sintered. When sintering, especially when using spark plasma sintering, it is critical not to sinter steel or stainless steel alloys above around 1 000°C otherwise melting occurs due to local overheating spots, which can reach a temperature close to the melting point of steel, i.e. = 1 500°C. On the other hand, the appropriate sintering temperature of tungsten carbide by SPS is generally 1 00- 200°C higher than this limit. The sintering temperature is influenced by the tungsten carbide grain size and the content of binder material.
[0009] One method of preparing a cemented carbide / steel FGM is described in paper JJpn Soc Powder Powder Metall. Vol 47, No 5, pp. 564-568, 2000, wherein a Japanese group reported the preparation of cemented carbide / steel FGM using SPS by sinter bonding WC-Co bi-layers with a steel substrate. The FGM had a gradient in WC grain size and cobalt composition. It consisted of 3 layers: steel/WC-40Co/WC-25Co. The particle size of WC in the surface layer is coarser than that in the middle layer and the end product was not fully dense. They have used the material in oil well drilling tools.
[001 0] At the 2002 International Conference on Functionally Graded Materials, NJ, D. K. Agrawal et al. presented a method of producing compositionally gradient steel / tungsten carbide-cobalt-diamond FGM systems (steel / WC-25Co-dia FGM) by microwave heating. In-situ hot pressing was needed to prevent mushrooming of sintered samples. The outcome of the production process was fairly dense product depending on the steel composition, the sintering temperature and the diamond coating type. When using microwave heating, a special and expensive equipment has to be used.
[001 1 ] In US2007/02 1 491 3 Al , the formation of various bi-layers WC-Co FGM by liquid phase sintering (LPS) is described. Because the liquid phase cobalt normally homogenizes during sintering, a complex process of enriching/deficienting each layer with an element of for example carbon is used. The exact gradient
composition will be a function of the sintering time and temperature and the dimension of the part to be made.
[001 2] Another way of preparing a tungsten carbide / stainless steel FGM
(stainless steel / WC-25Co) by SPS is presented by Y. Kawakami et al. in Solid State Phenomena Vol 1 27, pp. 1 79-1 84, 2007. Here they tried to prepare the compositionally gradient material by using a special shape graphite mold set (with upper thinner part and lower thicker part) to overcome the difference between the two sintering temperatures of stainless steel and tungsten carbide. Even so, it was hard to obtain a properly sintered body and the process is sensitive to the sintering temperature and the number of graded layers.
[001 3] Therefore, there is a need for a simple yet effective production method for the fabrication of a metal / cemented carbide functionally graded material
(preferably a steel/tungsten carbide FGM) that is highly dense and has no cracking.
Summary of invention
[001 4] An object of the present invention is to prepare a metal / cemented carbide functionally graded material by sintering, preferably by spark plasma sintering (SPS), in order to combine a tough metal base with a hard carbide surface in an economical way. The functionally graded material can be a steel/cemented tungsten carbide (steel / WC-Co FGM) . The end product is a fully dense
compositionally gradient shape with pure metal and pure cemented carbide alloy as two end surfaces (pure metal layer / x number of composite layers / pure cemented carbide layer) . Another end product can be a dense compositionally gradient shape with pure metal as one end surface and a metal-cemented carbide composite on the other end surface.
[001 5] The term "cemented" means that the carbide alloy powder includes an amount of metallic binder, such as for example cobalt, nickel, iron, or their alloys.
During the sintering process, the tungsten carbide particles are captured in the metallic binder and cemented together by forming a metallurgical bond.
[001 6] The base layer can be a steel alloy, a stainless steel alloy or other metallic material.
[001 7] Thus, the invention relates to a method of preparation of a FGM shape with a first surface comprising up to 1 00% of a first material and a second surface comprising up to 1 00% of a second material. The method is characterized in that it comprises the steps of: selecting the first material with a first sintering temperature and a first melting temperature and the second material with a second sintering temperature and a second melting temperature , wherein the first melting temperature is higher than the second melting temperature, loading a first layer of the first material in a sintering mold referred to as die, adding at least one intermediate layer on the first layer, the intermediate layer comprising a mix of the first and second material creating an intermediate graded composite region, loading a second layer of the second material on the at least one intermediate layer, adding an electrically insulating layer on the second layer of the second material, adding a pressure on the layers creating a FGM shape, and sintering the whole shape under a predetermined time, pressure and temperature.
[001 8] The method can further comprise adding an electrically insulating layer before loading the first layer of the first material.
[001 9] The method can comprise adding an electrically insulating layer on all surfaces around the material to be sintered.
[0020] The layers are preferably added as powders, but solid blocks of the pure materials and composites can also be used.
[002 1 ] When using this method for creating a FGM-shape, the electrically insulating layer added on the second material enforces the current from the sintering process to flow only through the die and not through the second layer of the FGM- shape. Thus, the temperature increase in the second layer becomes limited. The temperature in the first layer is high enough to sinter the first material but it does not exceed the melting temperature of the second material. The resulting end product from the process is a near fully dense FGM without any melted material.
[0022] Adding an electrically insulating layer on all sides of the material to be sintered, thus surrounding it totally, will result in a directed current flow that goes totally around the material instead of through the material. In this way locally over heated spots are avoided and melting prevented.
[0023] In embodiments of the invention said first material is a cemented carbide and said second material is a metal or metal alloy, preferably said first material is cemented tungsten carbide and said second material is steel.
[0024] When using a cemented carbide, such as for example cemented tungsten carbide, and combining it with a metal or metal alloy, preferably steel, it is possible to combine the high wear resistance of the carbide with the high toughness, the high strength, and the machinability of the metal. Due to the different sintering and melting temperatures of the respective materials, these materials are especially suitable to sinter using the above described inventive method.
[0025] In another embodiment, the first material includes a metallic binder. The metallic binder may be cobalt and the amount of cobalt can be between 5 and 25wt%. The binder can also be nickel, iron, or their alloys.
[0026] During the sintering process, the carbide particles are captured in the metallic binder and cemented together by forming a metallurgical bond. The result is a more dense FGM.
[0027] In another embodiment, said electrically insulating layer is chosen from any of the materials boron nitride, alumina, zirconia, silicon nitride, aluminum nitride, silica, magnesia.
[0028] All above mentioned materials are electrically insulating. When
steel/cemented tungsten carbide FGM is sintered, the most preferred insulating material is boron nitride. The insulating layer can either be a powder or a solid disc. The insulating layer can also be added as liquid through spraying or painting.
[0029] In one embodiment of the method, the sintering takes place under a sintering temperature of between 1 000 °C and 1 200 °C, preferably between 1 050°C and 1 1 50°C, more preferably between 1 070 °C and 1 1 20°C and most preferably 1 1 00 °C, a pressure of between 20 and 1 20 MPa, preferably between 50 and 90 MPa, more preferably between 65 and 80 MPa and most preferably 75 MPa, and a sintering time of between 5 and 30 min, preferably between 1 0 and 20 min, more preferably 1 5 min.
[0030] In one embodiment of the method, the sintering takes place under a sintering temperature of between 900 °C and 1 200 °C, preferably between 950°C and 1 1 50°C, a pressure of between 20 and 1 20 MPa, preferably between 30 and 75 MPa, and a sintering holding time of between 2 and 30 min, preferably between 5 and 20 min .
[003 1 ] In one embodiment the shape is sintered using one of the following sintering techniques; spark plasma sintering (SPS) or direct hot pressing (DHP).
Possible sintering techniques are also hot pressing (HP) or hot isostatic pressing (HIP). But preferably, spark plasma sintering (SPS) is used.
[0032] In another embodiment, the sintering pressure is applied through two punches arranged on opposite sides of the loaded material in the die.
[0033] In one embodiment, the dies are lined with a graphite foil and this is also inserted between the first and second surface of the FGM shape and the two punches. In another embodiment, the dies are graphite dies surrounded by graphite felt. In another embodiment, the dies are surrounded by a carbon fiber composite material (CFC) .
[0034] The graphite foil ensures good electric and thermal contacts between the die and the punches and also facilitates removal of the sintered compact without damaging the die or punch surfaces.
[0035] In another embodiment, the dies are lined with a layer of the insulating material.
[0036] In one embodiment of the method, the method further comprises the step: removing the electrically insulating layer after the sintering process has been performed.
[0037] Removal of the remains of the insulating layer after sintering can be performed through sand blasting or similar. The end product is a pure FGM ready to be manufactured into a cemented carbide tool. The end product can also be a finished cemented carbide tool with no need for further processing.
[0038] All individual features of the above methods may be combined or exchanged unless such combination or exchange is clearly contradictory.
[0039] The sintering conditions, such as holding time and pressure, depend on the size of the FGM shape and the die dimension .
Brief description of drawings
[0040] The invention is now described, by way of example, with reference to the accompanying drawings, in which:
Fig. 1 shows a longitudinal cross-section of a FGM die setup
Table 1 lists the relative densities and the sintering conditions during sintering of individual steel and cemented carbide powders by SPS
Table 2 lists the relative densities and the sintering conditions during sintering of steel / WC-Co FGM compacts by SPS at 1 1 00°C/75MPa/l 5min/50°C/min.
Description of embodiments
[0041 ] The invention will now be described in more detail in respect of embodiments and in reference to the accompanying drawings. All examples herein should be seen as part of the general description and therefore possible to combine in any way in general terms. Again, individual features of the various embodiments and methods may be combined or exchanged unless such combination or exchange is clearly contradictory to the overall method of production of the functionally graded material shape.
[0042] The read temperatures mentioned in the description can differ between different sintering furnaces depending on how the temperature is measured. In the
examples stated herein the temperature is measured with a pyrometer focused on a hole on the outer surface of the die.
[0043] The exact sintering temperature, holding time and pressure are dependent of the size and geometry of the sintered components as well as the design of the sintering tool, comprising the die and the two punches closing the die.
[0044] FIG. 1 shows a longitudinal cross-section of the die setup for producing a FGM-shape 4 according to the invention. Powders of at least a first and a second material M l , M2 are sintered under a pressure created by punches 3a, 3b in a die 1 , preferably a graphite die. The sintering process creates samples of the FGM shape 4, for example cylindrical-shaped discs. Other shapes including any polygonal-shaped discs can also be sintered. The sintering process is performed by spark plasma sintering under a high temperature and pressure on the closed die to create a dense/near fully dense FGM-shape. The powder layers to be sintered can be cold-pressed prior to the sintering. The sintering takes preferably place at a sintering temperature of between 1 000 °C and 1 200 °C, preferably between 1 050°C and 1 1 50°C, more preferably between 1 070 °C and 1 1 20°C and most preferably 1 1 00 °C, a pressure of between 20 and 1 20 MPa, preferably between 50 and 90 MPa, more preferably between 65 and 80 MPa and most preferably 75 MPa, and a sintering time of between 5 and 30 min, preferably between 1 0 and 20 min, more preferably 1 5 min. Different sintering techniques can be used, such as for example spark plasma sintering (SPS) or direct hot pressing (DHP) . Preferably spark plasma sintering (SPS) is used. Other sintering techniques are also hot pressing (HP) or hot isostatic pressing (HIP) .
[0045] The FGM shape has a first layer 11 with a first surface 4a comprising up to 1 00% of the first material M l and a second layer 12 with a second surface 4b comprising up to 1 00% of the second material M2. Between the first layer 11 of the
first material Ml and the second layer 12 of the second material M2 at least one third layer 13 comprising a mix of the first and second material M l , M2 is added. The at least one third layer is creating an intermediate graded composite region l c. Preferably the numbers of graded layers are between two and ten, with a 50- 1 0vol% gradient change. However, other numbers of layers are of course also possible, as is a non-linear gradient change in composition .
[0046] The first material M l has a first sintering temperature Ts l and a first melting temperature Tm l and the second material M2 has a second sintering temperature Ts2 and a second melting temperature Tm2. The first melting
temperature Tm l is higher than the second melting temperature Tm2. Thus, in order to achieve a fully dense FGM-shape, the sintering temperature during the SPS- process needs to reach the first sintering temperature Ts l of the first material but not exceed the second melting temperature Tm2 of the second material. Otherwise, this can lead to melting of the second material M2.
[0047] In order to decrease the temperature increase locally in the second material M2, an electrically insulating layer 5 of an electrically insulating powder is placed on the second surface 4b of the FGM-shape 4, between the second layer 12 of the second material M2 and the graphite punch 3b. The function of the electrically insulating powder is to enforce the current to flow only through the die and not through the second layer 12 of the FGM-shape.
[0048] The first material M l is preferably a cemented carbide and the second material M2 a metal. More preferably, the first material M l is cemented tungsten carbide and the second material M2 is steel. The first material M l includes a metallic binder such as for example cobalt Co or an iron-nickel alloy Fe-Ni.
[0049] The electrically insulating layer can be chosen from any of the electrically insulating materials of boron nitride, alumina, zirconia, silicon nitride,
aluminum nitride, silica, magnesia, but preferably boron nitride BN is used. This material can either be a powder or a solid disc.
[0050] The inner walls of the dies 1 can be lined with thin graphite foil 2 inserted between the shape 4 and the two punches 3a, 3b. A graphite foil can also be inserted between the first and second surface l a, 1 b of the FGM shape 1 and the two punches (3a, 3b) . The graphite foil 2 ensures good electric and thermal contacts between the die 1 and the punches 3a, 3b, and also facilitates removal of the sintered compact without damaging the die 1 or punch surfaces 3a, 3b.
[005 1 ] The graphite dies 1 can be surrounded by graphite felt 6 to reduce the heat loss by radiation from the outer die surface. The temperature can for example be measured at a hole 7 in the graphite die 6.
Examples
[0052] The present invention is further illustrated by the following experimental results, which should not limit the claims in any way. For example, other metals and cemented carbide powders than steel/cemented tungsten carbide can be used. Other sintering techniques than SPS can also be used.
[0053] At the beginning, basic SPS experiments for single steel and tungsten carbide powders were carried out to find an optimum sintering condition at which both materials become highly dense. Fabrication of steel / cemented tungsten carbide FGM compacts was thereafter performed. Steel powders with low carbon content and cemented tungsten powders of about 1 0wt% cobalt composition were used in the experiment.
[0054] For the FGM gradient layers, the steel and tungsten carbide composite powder mixtures were dry mixed at room temperature for one hour in plastic containers with tungsten carbide milling rods on a jar rolling mill.
[0055] The steel / WC-Co FGMs were designed to comprise four composite interlopers between the pure steel and tungsten carbide layers at the two ends. The composites consisted of steel - cemented carbide mixtures with a 20vol% gradient change (i.e. 80/20, 60/40, 40/60, 20/80 vol%). The total six layers were loaded in order, layer by layer, in a graphite die and a BN insulating layer was interposed between the punch and the steel layer.
[0056] A steel / cemented tungsten carbide FGM disc (©20x6 mm) was successfully sintered according to the above conditions. It was fully dense and no cracks could be observed. Experiments have also successfully been performed with discs of the sizes 020x8.25 mm and I 2x7.25 mm.
[0057] The sintering was done in ordinary cylindrical graphite molds.
[0058] During the sintering of single steel powders, the samples 4 were sintered with and without an electrically insulating layer 5 of boron nitride powder BN placed between the steel powder to be sintered and the graphite punches 3a, 3b.
[0059] The powders inside the closed dies were first cold-pressed. Then, the samples were sintered in vacuum in a spark plasma sintering unit (SPS-5.40 MK-VI system from SPS Syntex Inc, Japan). Once the p re-determined SPS-pressure was applied, the dies were heated to 600 °C in 3 minutes and then heated further at a rate of 50-1 00 °C/min to the desired holding temperature. The holding time was between 5 and 1 5 minutes. The temperature was measured with an optical pyrometer focused on a hole 7 at the half height of the outer surface of the die.
[0060] After sintering, the resulting sintered discs were blasted to remove the residues of graphite foil and BN layer, and then polished with # 1 20 silicon carbide grinding paper. The relative densities were measured by Archimedes method (European Standard EN 993-1 ) using deionized water as the immersion medium.
The possible existence of surface cracks in the sintered pellets was examined visually and through optical microscopy (Olympus SZxl 2 model, Olympus Optical Co. Ltd, Japan).
[0061 ] The relative densities and the sintering conditions are listed in Tables 1 and 2, wherein Table 1 lists sintering of individual steel and cemented carbide powders by SPS and Table 2 lists sintering of steel / WC-Co FGM compacts by SPS at 1 1 00°C/75MPa/1 5min/50°C/min .
[0062] From the results, it can be seen that when no BN insulation was used the melting of steel occurred when the SPS temperature was 1 1 00°C which implies that the temperature was locally at the powder particle surfaces much higher than that measured on the die surface and very close to the melting point of the steel alloy (1 5 1 6°C). When BN was used, the current flow through the steel powder was inhibited, which prevented the local overheating and thus no melting was observed. The tungsten carbide alloy was well densified at this sintering temperature of 1 1 00 °C when a holding time of 1 5 minutes was applied under a pressure of 75 MPa.
[0063] The steel / WC-Co FGM compacts were properly sintered with high densities by the sintering process described above and no cracks were observed.
Claims
1 . A method of preparation of a FGM shape (4) with a first surface (4a) comprising up to 1 00% of a first material (M l ) and a second surface (4b) comprising up to 1 00% of a second material (M2), comprising the steps:
(i) selecting the first material (M l ) with a first sintering temperature (Ts l ) and a first melting temperature (Tm l ) and the second material (M2) with a second sintering temperature (Ts2) and a second melting temperature (Tm2), wherein the first melting temperature (Tm l ) is higher than the second melting temperature (Tm2),
(ii) loading a first layer (11 ) of the first material (M l ) in a sintering mold
referred to as die (1 ),
(iii) adding at least one intermediate layer (13) on the first layer (11 ), the
intermediate layer (13) comprising a mix of the first and second material (M l , M2) creating an intermediate graded composite region (l c),
(iv) loading a second layer (12) of the second material (M2) on the at least one intermediate layer (13)
(v) adding an electrically insulating layer (5) on the second layer (12) of the second material (M2),
(vi) adding a pressure on the layers (11 -13) creating a FGM shape (1 ), and
(vii) sintering the whole shape (1 ) under a predetermined time, pressure and temperature.
2. A method according to claim 1 , wherein an electrically insulting layer is added before the first layer (11 ) of the first material (M l )
3. A method according to claim 1 or 2, wherein an electrically insulating layer is added on all surfaces around the material to be sintered.
4. A method according to claim 1 , 2 or 3, wherein said first material (M l ) is a cemented carbide and said second material (M2) is a metal or a metal alloy.
5. A method according to claim 4, wherein said first material (M l ) is cemented tungsten carbide and said second material (M2) is steel.
6. A method according to claim 4 or 5, wherein the first material (M l ) includes a metallic binder.
7. A method according to claim 6, wherein the metallic binder is cobalt (Co), nickel (Ni), iron (Fe), or their alloys.
8. A method according to claim 7, wherein the amount of cobalt (Co) is between 5 and 25wt%.
9. A method according to any of the above claims, wherein said electrically insulating layer is chosen from any of the materials boron nitride, alumina, zirconia, silicon nitride, aluminum nitride, silica, magnesia.
1 0. A method according to any of the above claims, wherein the shape (4) is sintered using one of the following sintering techniques; spark plasma sintering (SPS) or direct hot pressing (DHP).
1 1 . A method according to any of the above claims, wherein the sintering takes place under a sintering temperature of between 900 °C and 1 200 °C, preferably between 950°C and 1 1 50°C, a pressure of between 20 and 1 20 MPa, preferably between 30 and 75 MPa, and a sintering holding time of between 2 and 30 min, preferably between 5 and 20 min.
1 2. A method according to any of the above claims, wherein the sintering takes place under a sintering temperature of between 1 000 °C and 1 200 °C, preferably between 1 050°C and 1 1 50°C, more preferably between 1 070 °C and 1 1 20°C and most preferably 1 1 00 °C, a pressure of between 20 and 1 20 MPa, preferably between 50 and 90 MPa, more preferably between 65 and 80 MPa and most preferably 75 MPa, and a sintering time of between 5 and 30 min, preferably between 1 0 and 20 min, more preferably 1 5 min.
1 3. A method according to any of the above claims, wherein the sintering pressure is applied by two punches (3a, 3b) arranged on opposite sides of the loaded material in the die (1 ) .
1 4. A method according to claim 1 3 wherein the dies (1 ) are lined with a graphite foil (2) and a graphite foil (2) is also inserted between the first and second surface (4a, 4b) of the FGM shape (4) and the two punches (3a, 3b).
1 5. A method according to any of the above claims, wherein the dies (1 ) are lined with an electrically insulating layer.
1 6. A method according to claim 1 5, wherein said electrically insulating layer is chosen from any of the materials boron nitride, alumina, zirconia, silicon nitride, aluminum nitride, silica, magnesia.
1 7. A method according to any of the above claims, wherein the dies ( 1 ) are graphite dies surrounded by graphite felt (6).
1 8. A method according to any of the above claims, wherein the method further comprises the step:
(viii) removing the of electrically insulating layer (5) after the sintering process has been performed.
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Cited By (13)
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CN103182506A (en) * | 2013-03-29 | 2013-07-03 | 华南理工大学 | TiCp/M2 high-speed steel composite material and SPS (spark plasma sintering) preparation method thereof |
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