WO1997034720A1 - Materiau composite et son procede de fabrication - Google Patents
Materiau composite et son procede de fabrication Download PDFInfo
- Publication number
- WO1997034720A1 WO1997034720A1 PCT/DE1997/000482 DE9700482W WO9734720A1 WO 1997034720 A1 WO1997034720 A1 WO 1997034720A1 DE 9700482 W DE9700482 W DE 9700482W WO 9734720 A1 WO9734720 A1 WO 9734720A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- composite material
- phase
- material according
- mpa
- binding metal
- Prior art date
Links
- 239000002131 composite material Substances 0.000 title claims abstract description 41
- 238000000034 method Methods 0.000 title claims abstract description 21
- 238000002360 preparation method Methods 0.000 title abstract 2
- 239000011230 binding agent Substances 0.000 claims abstract description 41
- 238000005266 casting Methods 0.000 claims abstract description 33
- 229920001169 thermoplastic Polymers 0.000 claims abstract description 32
- 229910052751 metal Inorganic materials 0.000 claims abstract description 31
- 239000002184 metal Substances 0.000 claims abstract description 31
- 239000004416 thermosoftening plastic Substances 0.000 claims abstract description 31
- 239000000463 material Substances 0.000 claims abstract description 24
- 239000000725 suspension Substances 0.000 claims abstract description 18
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 14
- 238000005245 sintering Methods 0.000 claims abstract description 14
- 239000010959 steel Substances 0.000 claims abstract description 14
- 239000000919 ceramic Substances 0.000 claims abstract description 10
- 239000011195 cermet Substances 0.000 claims abstract description 9
- 239000007858 starting material Substances 0.000 claims abstract description 7
- 239000000696 magnetic material Substances 0.000 claims abstract description 5
- 238000004663 powder metallurgy Methods 0.000 claims abstract description 4
- 239000000843 powder Substances 0.000 claims description 27
- 239000000203 mixture Substances 0.000 claims description 24
- 239000004033 plastic Substances 0.000 claims description 12
- 229920003023 plastic Polymers 0.000 claims description 12
- 239000001993 wax Substances 0.000 claims description 10
- 238000001746 injection moulding Methods 0.000 claims description 8
- 229910052742 iron Inorganic materials 0.000 claims description 7
- 229910052719 titanium Inorganic materials 0.000 claims description 6
- 239000013543 active substance Substances 0.000 claims description 5
- 229910052759 nickel Inorganic materials 0.000 claims description 5
- -1 Ni2TiAl Inorganic materials 0.000 claims description 4
- 239000005642 Oleic acid Substances 0.000 claims description 4
- 239000010949 copper Substances 0.000 claims description 4
- 229910052802 copper Inorganic materials 0.000 claims description 4
- 229910052758 niobium Inorganic materials 0.000 claims description 4
- WRIDQFICGBMAFQ-UHFFFAOYSA-N (E)-8-Octadecenoic acid Natural products CCCCCCCCCC=CCCCCCCC(O)=O WRIDQFICGBMAFQ-UHFFFAOYSA-N 0.000 claims description 3
- LQJBNNIYVWPHFW-UHFFFAOYSA-N 20:1omega9c fatty acid Natural products CCCCCCCCCCC=CCCCCCCCC(O)=O LQJBNNIYVWPHFW-UHFFFAOYSA-N 0.000 claims description 3
- QSBYPNXLFMSGKH-UHFFFAOYSA-N 9-Heptadecensaeure Natural products CCCCCCCC=CCCCCCCCC(O)=O QSBYPNXLFMSGKH-UHFFFAOYSA-N 0.000 claims description 3
- ZQPPMHVWECSIRJ-UHFFFAOYSA-N Oleic acid Natural products CCCCCCCCC=CCCCCCCCC(O)=O ZQPPMHVWECSIRJ-UHFFFAOYSA-N 0.000 claims description 3
- 239000004698 Polyethylene Substances 0.000 claims description 3
- 235000021355 Stearic acid Nutrition 0.000 claims description 3
- 230000002745 absorbent Effects 0.000 claims description 3
- 239000002250 absorbent Substances 0.000 claims description 3
- 238000001125 extrusion Methods 0.000 claims description 3
- 238000000227 grinding Methods 0.000 claims description 3
- QXJSBBXBKPUZAA-UHFFFAOYSA-N isooleic acid Natural products CCCCCCCC=CCCCCCCCCC(O)=O QXJSBBXBKPUZAA-UHFFFAOYSA-N 0.000 claims description 3
- 239000010410 layer Substances 0.000 claims description 3
- 238000002156 mixing Methods 0.000 claims description 3
- QIQXTHQIDYTFRH-UHFFFAOYSA-N octadecanoic acid Chemical compound CCCCCCCCCCCCCCCCCC(O)=O QIQXTHQIDYTFRH-UHFFFAOYSA-N 0.000 claims description 3
- OQCDKBAXFALNLD-UHFFFAOYSA-N octadecanoic acid Natural products CCCCCCCC(C)CCCCCCCCC(O)=O OQCDKBAXFALNLD-UHFFFAOYSA-N 0.000 claims description 3
- 229920000573 polyethylene Polymers 0.000 claims description 3
- 230000001681 protective effect Effects 0.000 claims description 3
- 239000008117 stearic acid Substances 0.000 claims description 3
- 239000004094 surface-active agent Substances 0.000 claims description 3
- 239000002347 wear-protection layer Substances 0.000 claims description 3
- 229910001369 Brass Inorganic materials 0.000 claims description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 2
- 238000005299 abrasion Methods 0.000 claims description 2
- 239000000654 additive Substances 0.000 claims description 2
- 125000001931 aliphatic group Chemical group 0.000 claims description 2
- 150000004996 alkyl benzenes Chemical group 0.000 claims description 2
- 239000010951 brass Substances 0.000 claims description 2
- 229910052799 carbon Inorganic materials 0.000 claims description 2
- 125000004432 carbon atom Chemical group C* 0.000 claims description 2
- 229910010293 ceramic material Inorganic materials 0.000 claims description 2
- 239000013078 crystal Substances 0.000 claims description 2
- 239000003599 detergent Substances 0.000 claims description 2
- 238000005553 drilling Methods 0.000 claims description 2
- 238000001704 evaporation Methods 0.000 claims description 2
- 230000008020 evaporation Effects 0.000 claims description 2
- 239000012779 reinforcing material Substances 0.000 claims description 2
- 229910052750 molybdenum Inorganic materials 0.000 claims 5
- 229910052804 chromium Inorganic materials 0.000 claims 4
- 229910052715 tantalum Inorganic materials 0.000 claims 4
- 229910052735 hafnium Inorganic materials 0.000 claims 3
- 150000001247 metal acetylides Chemical class 0.000 claims 3
- 229910052720 vanadium Inorganic materials 0.000 claims 3
- 229910052726 zirconium Inorganic materials 0.000 claims 3
- 229910003310 Ni-Al Inorganic materials 0.000 claims 2
- 238000007792 addition Methods 0.000 claims 2
- 229910052748 manganese Inorganic materials 0.000 claims 2
- 229910052721 tungsten Inorganic materials 0.000 claims 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims 1
- 229910000997 High-speed steel Inorganic materials 0.000 claims 1
- 229910016006 MoSi Inorganic materials 0.000 claims 1
- 229910005883 NiSi Inorganic materials 0.000 claims 1
- 229910009962 Ti2Si Inorganic materials 0.000 claims 1
- 229910010038 TiAl Inorganic materials 0.000 claims 1
- 229910008484 TiSi Inorganic materials 0.000 claims 1
- 229910045601 alloy Inorganic materials 0.000 claims 1
- 239000000956 alloy Substances 0.000 claims 1
- 229910052782 aluminium Inorganic materials 0.000 claims 1
- 229910052796 boron Inorganic materials 0.000 claims 1
- 125000003178 carboxy group Chemical group [H]OC(*)=O 0.000 claims 1
- 238000009694 cold isostatic pressing Methods 0.000 claims 1
- 238000005056 compaction Methods 0.000 claims 1
- 238000007723 die pressing method Methods 0.000 claims 1
- 238000001513 hot isostatic pressing Methods 0.000 claims 1
- 239000002905 metal composite material Substances 0.000 claims 1
- 150000004767 nitrides Chemical class 0.000 claims 1
- 150000002888 oleic acid derivatives Chemical class 0.000 claims 1
- 229910052761 rare earth metal Inorganic materials 0.000 claims 1
- 150000002910 rare earth metals Chemical class 0.000 claims 1
- 229910052710 silicon Inorganic materials 0.000 claims 1
- 229910000601 superalloy Inorganic materials 0.000 claims 1
- 238000004519 manufacturing process Methods 0.000 abstract description 10
- 230000003746 surface roughness Effects 0.000 abstract description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 8
- 239000011162 core material Substances 0.000 description 6
- 238000001816 cooling Methods 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 238000000465 moulding Methods 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000018109 developmental process Effects 0.000 description 2
- 230000009969 flowable effect Effects 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 238000003801 milling Methods 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- ZQPPMHVWECSIRJ-KTKRTIGZSA-N oleic acid Chemical compound CCCCCCCC\C=C/CCCCCCCC(O)=O ZQPPMHVWECSIRJ-KTKRTIGZSA-N 0.000 description 2
- 239000012188 paraffin wax Substances 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 238000007493 shaping process Methods 0.000 description 2
- 239000002002 slurry Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 229910018072 Al 2 O 3 Inorganic materials 0.000 description 1
- 229910017061 Fe Co Inorganic materials 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- GRYLNZFGIOXLOG-UHFFFAOYSA-N Nitric acid Chemical compound O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 0.000 description 1
- QVYYOKWPCQYKEY-UHFFFAOYSA-N [Fe].[Co] Chemical compound [Fe].[Co] QVYYOKWPCQYKEY-UHFFFAOYSA-N 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 150000007513 acids Chemical class 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 238000005255 carburizing Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 235000019504 cigarettes Nutrition 0.000 description 1
- 238000004320 controlled atmosphere Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000011010 flushing procedure Methods 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 229910017604 nitric acid Inorganic materials 0.000 description 1
- 239000003960 organic solvent Substances 0.000 description 1
- 238000004806 packaging method and process Methods 0.000 description 1
- 239000003973 paint Substances 0.000 description 1
- 239000004014 plasticizer Substances 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 238000005204 segregation Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- 238000007514 turning Methods 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
- B22F3/22—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces for producing castings from a slip
- B22F3/225—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces for producing castings from a slip by injection molding
-
- 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
- B22F3/22—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces for producing castings from a slip
-
- 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
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/04—Making non-ferrous alloys by powder metallurgy
- C22C1/05—Mixtures of metal powder with non-metallic powder
- C22C1/051—Making hard metals based on borides, carbides, nitrides, oxides or silicides; Preparation of the powder mixture used as the starting material therefor
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F1/00—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties
- H01F1/01—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials
- H01F1/03—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity
- H01F1/12—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of soft-magnetic materials
- H01F1/14—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of soft-magnetic materials metals or alloys
- H01F1/20—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of soft-magnetic materials metals or alloys in the form of particles, e.g. powder
- H01F1/22—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of soft-magnetic materials metals or alloys in the form of particles, e.g. powder pressed, sintered, or bound together
- H01F1/24—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of soft-magnetic materials metals or alloys in the form of particles, e.g. powder pressed, sintered, or bound together the particles being insulated
-
- 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
- B22F2005/004—Article comprising helical form elements
-
- 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
- B22F2005/103—Cavity made by removal of insert
-
- 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
-
- 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
Definitions
- the invention relates to composite materials, consisting essentially of a cermet material with a binder metal phase of
- the rest of the binder metal phase a powder metallurgy steel or a metallic or ceramic magnetic material.
- the invention further relates to a method for producing this composite material.
- the starting powders are mixed, homogenized and ground in accordance with the desired quantitative composition before they are subjected to a shaping for producing a green body, which is then sintered.
- the following variants of the shaping method are known from the prior art:
- the compacted blank is shaped to the desired geometry in the green state or after its pre-sintering by means of mechanical turning, cutting, drilling and grinding operations.
- the mixed and ground starting powder is granulated and compressed with the aid of plastic binders by means of die presses to the desired final shape.
- the starting powder mixture is made flowable by adding a thermoplastic plastic binder and injection molded under high pressure in accordance with the injection molding process known for plastics.
- the necessary injection molding tools increase the manufacturing costs considerably.
- to remove the introduced Binder's process steps are necessary in which gaseous nitric acid or organic solvents are used, the handling and disposal of which, from an environmental point of view, is further cost-increasing.
- Strand-shaped blanks can be formed using plasticizers such as wax using screw or piston extrusion presses.
- the qualitative and quantitative composition of the composite materials consisting of a cermet material, a hard metal or a powder-metallurgy steel is basically known in the prior art, for example from DE 43 40 652 A1.
- the respective base materials, namely cermets, hard metals or steels can be in pure form or have additives of various types, namely metals, further hard materials, ceramic materials and single-crystal reinforcing materials in whisker or plate form.
- the fundamental difference between the composite materials claimed is that the starting materials are shaped into a non-porous green body by hot casting prior to sintering. Hot casting is basically for the production of ceramic moldings from cfi / Ber. DKG 72 (1995) No. 10, pages 640 to 642.
- the hot casting process which is also referred to as low-pressure hot spraying or low-pressure injection molding, is based on the fact that the powdery starting mixtures are brought into a flowable state by adding a thermoplastic binder, essentially paraffins and / or liquid-melting waxes and surface-active substances - including surfactants or called detergents - are added.
- the surfactants serve as a connection between the solid particles, which they coat "in one layer" and the waxes and / or paraffins.
- cermet, hard metal or steel powder contain components that have much higher densities up to 16 g / cm 3 .
- hot casting can also be used to shape the composite materials characterized in claim 1.
- the hot casting of the suspension consisting of the powdery starting materials and the thermoplastic binder enables the production of molded parts with a high degree of complexity, so undercuts, transverse bores and blind holes, large wall thickness differences, threads, grooves, surface structures, lettering and combinations of the aforementioned shapes can be cost-effectively , in particular by approximately 80% to 90% lower tool costs compared to high-pressure injection molding.
- Application products are, in particular, indexable inserts with complex chip form geometries, milling cutter blanks with a twisted chip chamber, rotor milling cutters, screws, micro-drills, drills and cutting inserts with flushing holes, guide fingers for cigarette manufacture, rotors, pump parts, such as bearing rings, shaft seals and shafts, gear wheels, complex nozzles, bearing shells, Watch case, scissors blanks, Cylinders for metering pumps, control pistons for paint spray guns, balls, work and transport rollers for the packaging industry, paddle wheels and the like.
- the hot casting process according to the invention of cermet, hard metal, steel and / or metallic or ceramic magnet materials is characterized in accordance with claim 17, that the components of the composite materials in the desired quantitative mixing ratio as powdery starting materials after grinding with a thermoplastic binder, the proportion of which in the total amount is 20 to 50% by volume, preferably 30 to 40% by volume, and which has a viscosity between 3 to 6 mPa s, in a stable dispersive suspension with a viscosity between 100 mPa s and 5 Pa s is transferred, this suspension is cast into a shape corresponding to the desired contours of the composite component to be produced without pressure or under a pressure of at most 5 MPa, preferably 0.1 to 1 MPa, at 70 ° C.
- thermoplastic binder to 120 ° C. and at temperatures, which are above the evaporation temperatures of the thermoplastic binder, is heated and the thermoplastic B in which the stripped body is sintered.
- the powder starting mixture and the thermoplastic binder by hot casting, i.e., above the melting temperature of the thermoplastic binder, has the true-to-shape negative contour of the finished component to be manufactured, taking into account the sintering shrinkage.
- the low pressures used do not place as high demands on the mold as in high-pressure injection molding. In particular, less expensive materials can be used as mold material.
- the average grain size of the powdered raw materials is less than 15 ⁇ m (for steel and magnetic Substances below 100 ⁇ m), it can be in particular ⁇ 3 p and / or the viscosity of the suspension is between 100 mPa s and 2000 mPa s. Variations in the average grain size are included insofar as, for example, some of the powdered starting materials can have a coarser grain and the rest can have a finer grain.
- the thermoplastic binder consists of waxes and / or paraffins, to which 2 to 30% by volume of surface-active substances, preferably with an aliphatic hydrocarbon residue or alkylbenzene residue with 10 to 22 C atoms, are added.
- surface-active substances preferably with an aliphatic hydrocarbon residue or alkylbenzene residue with 10 to 22 C atoms.
- the suspension is preferably cast in casting molds made of brass, copper, steel or plastic.
- the thermoplastic binder can be driven out in stages, namely in a first stage at temperatures up to 300 ° C. at which 50 to 80% by volume of the thermoplastic binder is expelled. be driven.
- the residual content of the thermoplastic binder remaining in the hot-cast molded body can then be used in the course of further treatment with a view to greater strength of the blank.
- the rest of the thermoplastic binder is then expelled at higher temperatures.
- the thermoplastic binder is preferably expelled in a protective gas atmosphere, as a result of which undesired reactions of the green body with the furnace atmosphere can be avoided.
- the shaped body in the first stage, can be coated with an absorbent material (a powder bed), such as Al 2 O 3 powder, or lie on a ceramic base, in particular A1 2 0 3 , and the second stage can be carried out in a sintering furnace.
- a powder bed such as Al 2 O 3 powder
- the powder bed and the ceramic underlay serve as an aid for sucking up the liquefied binder.
- the residual content of thermoplastic binder in the molded body is preferably 20 to 30% by volume before being transferred to the sintering furnace, this residual content ensuring adequate stabilization of the molded body.
- the two-stage binder removal can optionally also be exploited to that targeted in the first stage at temperatures up to 300 * C acids present as surface-active substances, such as oleic acid, stearic acid, etc., are cracked, and the resulting cracking carbon for carburizing of Shaped body are used.
- C acids present as surface-active substances such as oleic acid, stearic acid, etc.
- the hot casting according to the invention is not only limited to the production of moldings of homogeneous composition. Inhomogeneities in the form of changing substance compositions can be achieved by casting molds with two different pouring channels, into which suspensions of different compositions are poured. In particular, different compositions can be cast on top of one another or next to one another, which merge into one another at the respective interfaces and also make it possible to set radial composition gradients if the cast core material is encapsulated by a material of a different composition.
- a core can first be produced in a first mold by hot or injection molding, which is then transferred to a second mold and encased in a shell made of hot-moldable material.
- abrasion-resistant wear protection layers can preferably be cast around a tough core, wherein the wear protection layers can consist of one or more layers of the same or different material composition.
- a strand of plastic preferably polyethylene or wax or another material that can be melted out at the sintering temperature, is firmly adhered as a placeholder for a later channel and that the molded body consisting of the strand and the core is then extrusion-coated in a casting mold by hot casting and the one thus produced Composite body is sintered, the strand thermally decomposing.
- the strand can be formed in a linear form, for example in the case of piercing tools, or in a spiral form in the case of drill blanks.
- a hard material powder mixture of 94% by mass of WC and 6% by mass of Co is mixed, ground and then with a thermoplastic binder, which is 45% by volume based on the total mixture, to give a 75 ° C. warm suspension been melted.
- 70% by volume of the thermoplastic binder consisted of a low-chain paraffin, 20% by volume of wax and 10% by volume of oleic acid.
- the hot slip suspension has a viscosity that is greater than 100 mPas. If smaller viscosity values were reached, powdery WC / Co was refilled in an amount until the desired minimum viscosity was reached and the dispersion was stable.
- the slip is put into a casting mold without pressure or at a maximum of 1 MPa via sprue channels, the inner contours of which correspond to the molded component to be produced, taking into account the sintering shrinkage.
- the casting mold is then cooled to room temperature, the molding is removed and under protective gas in a powder bed up to 300 ° C. heated, except for a residual content of thermoplastic binder between 20 and 30% of the binder is driven off.
- the molded body is placed on a graphite base in a sintering furnace and sintered at approx. 1450'C. In the warm-up phase up to 500 ° C, the residual binder is driven out into the gas phase.
- thermoplastic binder consisted of 70% by volume of a low-chain paraffin, 24% by volume of wax and 6% by volume of stearic acid.
- the thermoplastic binder was heated to 80 ° C. in a heatable mixing device and 2/3 of the powder mixture was added and mixed until the viscosity of the suspension decreased. The rest of the powder is then added and again mixed intensively.
- the suspension has a viscosity above 100 mPas.
- the slip thus produced is poured into a mold for a coil core under a pressure of 1 MPa and cooled. After cooling, the green compact is removed removed from the divisible casting mold and thermally debindered in an alumina powder bed in a push-through furnace under a hydrogen stream and sintered at 1350 ° C. for 4 hours.
- cermets and powder-metallurgical steel starting grades of the type mentioned have been processed.
- the starting grain sizes of the powder metallurgical materials were either on average below 1 ⁇ m (so-called fine grain). or below 2 ⁇ m.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Manufacturing & Machinery (AREA)
- Dispersion Chemistry (AREA)
- Power Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Powder Metallurgy (AREA)
Abstract
L'invention concerne des matériaux composites qui comprennent principalement: un cermet comportant une phase métallique de liaison de 3 à 30 % en masse, avec un reste formé d'au moins une phase carbonitrure; ou un métal dur comportant au moins une phase solide dure de 65 à 99 %, avec un reste formé d'un résidu de phase de métal de liaison; ou un acier produit par métallurgie des poudres; ou un matériau magnétique métallique ou céramique. L'invention concerne également un procédé permettant de fabriquer ce matériau composite. Pour résoudre le problème consistant à trouver des matériaux composites et un procédé de fabrication qui permette de produire des matériaux composites peu coûteux sous la forme de pièces moulées de géométrie complexe et avec une rugosité de surface la plus réduite possible, il est proposé de fabriquer ledit matériau par moulage à chaud suivi de frittage. Pour cela, on transforme, à l'aide d'un liant thermoplastique, les produits de départ pulvérulents en une suspension dispersive stable ayant une viscosité comprise entre 100 mPa et 5 Pa, on coule cette suspension sans pression ou sous une pression maximale de 5 MPa, à une température comprise entre 70 et 120 °C, puis on la chauffe, le liant thermoplastique étant expulsé avant le frittage du corps devenu exempt de liant.
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19610410 | 1996-03-16 | ||
DE19610410.6 | 1996-03-16 | ||
DE19613309 | 1996-04-03 | ||
DE19613309.2 | 1996-04-03 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1997034720A1 true WO1997034720A1 (fr) | 1997-09-25 |
Family
ID=26023863
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/DE1997/000482 WO1997034720A1 (fr) | 1996-03-16 | 1997-03-10 | Materiau composite et son procede de fabrication |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE19709651A1 (fr) |
WO (1) | WO1997034720A1 (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US12357061B2 (en) * | 2021-12-23 | 2025-07-15 | Eta Sa Manufacture Horlogère Suisse | Portable object comprising a middle devoid of fastening horns and a removable bracelet |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DK1306148T3 (da) * | 2001-10-29 | 2007-01-29 | Ceratizit Luxembourg Sarl | Fremgangsmåde til gelstöbning af emner ud fra keramik-, glas- eller metalpulver |
US7247186B1 (en) * | 2003-05-20 | 2007-07-24 | Exxonmobil Research And Engineering Company | Advanced erosion resistant carbonitride cermets |
CN100415919C (zh) * | 2003-05-20 | 2008-09-03 | 埃克森美孚研究工程公司 | 高级抗侵蚀碳氮化物金属陶瓷 |
GB2429980A (en) * | 2005-09-08 | 2007-03-14 | John James Saveker | Material comprising a carbide, boride or oxide and tungsten carbide |
BRPI0809028B1 (pt) | 2007-03-21 | 2016-01-12 | Hoeganaes Ab Publ | compósitos poliméricos de pós metálicos |
EP2143957B2 (fr) * | 2008-07-10 | 2016-08-10 | Grundfos Management A/S | Composant d'écoulement d'une pompe |
DE102012213263A1 (de) | 2011-09-20 | 2013-03-21 | Robert Bosch Gmbh | Handwerkzeugvorrichtung mit zumindest einer Ladespule |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1533035B1 (de) * | 1965-06-17 | 1971-04-01 | Tavkoezlesi Ki | Verfahren zur pulvermetallurgischen herstellung von sinter teilen aus metall und oder metalloxidpulver mittels pasten guss |
DE2422425A1 (de) * | 1973-05-09 | 1974-11-28 | Mallory & Co Inc P R | Verfahren und vorrichtung zur herstellung von gegenstaenden |
US4948426A (en) * | 1989-10-17 | 1990-08-14 | Sumitomo Metal Mining Company Limited | Sintering metal powder and a process for making a sintered metal product |
EP0443048A1 (fr) * | 1989-09-14 | 1991-08-28 | Sumitomo Electric Industries Ltd | Procede de production de carbure cemente ou d'alliage de cermet |
EP0516165A2 (fr) * | 1991-05-31 | 1992-12-02 | Sumitomo Electric Industries, Limited | Procede pour la production d'un corps dur fritte |
EP0576282A2 (fr) * | 1992-06-24 | 1993-12-29 | Sumitomo Special Metals Co., Ltd. | Procédé de préparation d'aimants frittés du type R-Fe-B utilisant moulage pour injection |
US5401292A (en) * | 1992-08-03 | 1995-03-28 | Isp Investments Inc. | Carbonyl iron power premix composition |
DE4332971A1 (de) * | 1993-09-28 | 1995-03-30 | Fischer Artur Werke Gmbh | Verfahren zur Herstellung von ineinandergreifenden Teilen |
-
1997
- 1997-03-10 WO PCT/DE1997/000482 patent/WO1997034720A1/fr active Application Filing
- 1997-03-10 DE DE19709651A patent/DE19709651A1/de not_active Withdrawn
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1533035B1 (de) * | 1965-06-17 | 1971-04-01 | Tavkoezlesi Ki | Verfahren zur pulvermetallurgischen herstellung von sinter teilen aus metall und oder metalloxidpulver mittels pasten guss |
DE2422425A1 (de) * | 1973-05-09 | 1974-11-28 | Mallory & Co Inc P R | Verfahren und vorrichtung zur herstellung von gegenstaenden |
EP0443048A1 (fr) * | 1989-09-14 | 1991-08-28 | Sumitomo Electric Industries Ltd | Procede de production de carbure cemente ou d'alliage de cermet |
US4948426A (en) * | 1989-10-17 | 1990-08-14 | Sumitomo Metal Mining Company Limited | Sintering metal powder and a process for making a sintered metal product |
EP0516165A2 (fr) * | 1991-05-31 | 1992-12-02 | Sumitomo Electric Industries, Limited | Procede pour la production d'un corps dur fritte |
EP0576282A2 (fr) * | 1992-06-24 | 1993-12-29 | Sumitomo Special Metals Co., Ltd. | Procédé de préparation d'aimants frittés du type R-Fe-B utilisant moulage pour injection |
US5401292A (en) * | 1992-08-03 | 1995-03-28 | Isp Investments Inc. | Carbonyl iron power premix composition |
DE4332971A1 (de) * | 1993-09-28 | 1995-03-30 | Fischer Artur Werke Gmbh | Verfahren zur Herstellung von ineinandergreifenden Teilen |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US12357061B2 (en) * | 2021-12-23 | 2025-07-15 | Eta Sa Manufacture Horlogère Suisse | Portable object comprising a middle devoid of fastening horns and a removable bracelet |
Also Published As
Publication number | Publication date |
---|---|
DE19709651A1 (de) | 1997-10-30 |
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