EP1061534A2 - Soft magnetic, deformable composite material and process for producing the same - Google Patents
Soft magnetic, deformable composite material and process for producing the same Download PDFInfo
- Publication number
- EP1061534A2 EP1061534A2 EP00119956A EP00119956A EP1061534A2 EP 1061534 A2 EP1061534 A2 EP 1061534A2 EP 00119956 A EP00119956 A EP 00119956A EP 00119956 A EP00119956 A EP 00119956A EP 1061534 A2 EP1061534 A2 EP 1061534A2
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- European Patent Office
- Prior art keywords
- composite material
- silicon
- material according
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- compound
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 239000002131 composite material Substances 0.000 title claims description 25
- 238000000034 method Methods 0.000 title claims description 8
- 239000006247 magnetic powder Substances 0.000 claims abstract description 18
- 239000000843 powder Substances 0.000 claims abstract description 11
- 239000000463 material Substances 0.000 claims abstract description 10
- -1 aluminum compound Chemical class 0.000 claims abstract description 9
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 8
- 239000000919 ceramic Substances 0.000 claims description 18
- 238000000576 coating method Methods 0.000 claims description 17
- 239000011248 coating agent Substances 0.000 claims description 16
- 150000001875 compounds Chemical class 0.000 claims description 16
- 229910052710 silicon Inorganic materials 0.000 claims description 15
- 239000010703 silicon Substances 0.000 claims description 14
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 13
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 6
- 229910052796 boron Inorganic materials 0.000 claims description 6
- 150000003377 silicon compounds Chemical class 0.000 claims description 6
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 5
- 229910052799 carbon Inorganic materials 0.000 claims description 4
- 230000006835 compression Effects 0.000 claims description 4
- 238000007906 compression Methods 0.000 claims description 4
- 229920001709 polysilazane Polymers 0.000 claims description 4
- BGECDVWSWDRFSP-UHFFFAOYSA-N borazine Chemical compound B1NBNBN1 BGECDVWSWDRFSP-UHFFFAOYSA-N 0.000 claims description 3
- 150000001639 boron compounds Chemical class 0.000 claims description 3
- 150000002483 hydrogen compounds Chemical class 0.000 claims description 3
- 239000000047 product Substances 0.000 claims description 3
- UORVGPXVDQYIDP-BJUDXGSMSA-N borane Chemical compound [10BH3] UORVGPXVDQYIDP-BJUDXGSMSA-N 0.000 claims description 2
- 239000007795 chemical reaction product Substances 0.000 claims description 2
- 239000002210 silicon-based material Substances 0.000 claims description 2
- 238000007669 thermal treatment Methods 0.000 claims 4
- 229910000085 borane Inorganic materials 0.000 claims 1
- 150000001718 carbodiimides Chemical class 0.000 claims 1
- 150000001805 chlorine compounds Chemical class 0.000 claims 1
- 125000002524 organometallic group Chemical group 0.000 claims 1
- UORVGPXVDQYIDP-UHFFFAOYSA-N trihydridoboron Substances B UORVGPXVDQYIDP-UHFFFAOYSA-N 0.000 claims 1
- 239000011230 binding agent Substances 0.000 abstract description 7
- 238000004519 manufacturing process Methods 0.000 abstract description 5
- 239000002904 solvent Substances 0.000 abstract description 5
- 239000000126 substance Substances 0.000 abstract description 3
- 229920001169 thermoplastic Polymers 0.000 abstract description 3
- 239000004416 thermosoftening plastic Substances 0.000 abstract description 3
- 239000008187 granular material Substances 0.000 abstract 2
- 125000001931 aliphatic group Chemical group 0.000 abstract 1
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 21
- 238000000197 pyrolysis Methods 0.000 description 14
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 8
- 229910052742 iron Inorganic materials 0.000 description 8
- 239000011521 glass Substances 0.000 description 7
- 239000002243 precursor Substances 0.000 description 7
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 6
- 239000007789 gas Substances 0.000 description 6
- 239000000203 mixture Substances 0.000 description 6
- 230000001681 protective effect Effects 0.000 description 6
- 229920001187 thermosetting polymer Polymers 0.000 description 5
- 230000008030 elimination Effects 0.000 description 4
- 238000003379 elimination reaction Methods 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 239000002245 particle Substances 0.000 description 4
- 238000003825 pressing Methods 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- BLRPTPMANUNPDV-UHFFFAOYSA-N Silane Chemical class [SiH4] BLRPTPMANUNPDV-UHFFFAOYSA-N 0.000 description 3
- CEGOLXSVJUTHNZ-UHFFFAOYSA-K aluminium tristearate Chemical compound [Al+3].CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O CEGOLXSVJUTHNZ-UHFFFAOYSA-K 0.000 description 3
- 229910021529 ammonia Inorganic materials 0.000 description 3
- 239000010410 layer Substances 0.000 description 3
- 239000000314 lubricant Substances 0.000 description 3
- 229920000642 polymer Polymers 0.000 description 3
- 239000000243 solution Substances 0.000 description 3
- 238000005979 thermal decomposition reaction Methods 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 2
- 229910017082 Fe-Si Inorganic materials 0.000 description 2
- 229910017133 Fe—Si Inorganic materials 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- JUJWROOIHBZHMG-UHFFFAOYSA-N Pyridine Chemical compound C1=CC=NC=C1 JUJWROOIHBZHMG-UHFFFAOYSA-N 0.000 description 2
- 229910052581 Si3N4 Inorganic materials 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 210000003298 dental enamel Anatomy 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 238000001746 injection moulding Methods 0.000 description 2
- 239000000696 magnetic material Substances 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 239000003960 organic solvent Substances 0.000 description 2
- 230000035699 permeability Effects 0.000 description 2
- 239000011148 porous material Substances 0.000 description 2
- 229920005989 resin Polymers 0.000 description 2
- 239000011347 resin Substances 0.000 description 2
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 description 2
- 239000007858 starting material Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 239000004593 Epoxy Substances 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 241000446313 Lamella Species 0.000 description 1
- 229920000265 Polyparaphenylene Polymers 0.000 description 1
- 229910000676 Si alloy Inorganic materials 0.000 description 1
- IWBUYGUPYWKAMK-UHFFFAOYSA-N [AlH3].[N] Chemical compound [AlH3].[N] IWBUYGUPYWKAMK-UHFFFAOYSA-N 0.000 description 1
- UBMXAAKAFOKSPA-UHFFFAOYSA-N [N].[O].[Si] Chemical compound [N].[O].[Si] UBMXAAKAFOKSPA-UHFFFAOYSA-N 0.000 description 1
- UMVBXBACMIOFDO-UHFFFAOYSA-N [N].[Si] Chemical compound [N].[Si] UMVBXBACMIOFDO-UHFFFAOYSA-N 0.000 description 1
- OBNDGIHQAIXEAO-UHFFFAOYSA-N [O].[Si] Chemical compound [O].[Si] OBNDGIHQAIXEAO-UHFFFAOYSA-N 0.000 description 1
- NJFMNPFATSYWHB-UHFFFAOYSA-N ac1l9hgr Chemical compound [Fe].[Fe] NJFMNPFATSYWHB-UHFFFAOYSA-N 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 125000000217 alkyl group Chemical group 0.000 description 1
- 229940063655 aluminum stearate Drugs 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- SIPUZPBQZHNSDW-UHFFFAOYSA-N bis(2-methylpropyl)aluminum Chemical compound CC(C)C[Al]CC(C)C SIPUZPBQZHNSDW-UHFFFAOYSA-N 0.000 description 1
- 238000005524 ceramic coating Methods 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 238000009833 condensation Methods 0.000 description 1
- 230000005494 condensation Effects 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- PMHQVHHXPFUNSP-UHFFFAOYSA-M copper(1+);methylsulfanylmethane;bromide Chemical compound Br[Cu].CSC PMHQVHHXPFUNSP-UHFFFAOYSA-M 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 230000005347 demagnetization Effects 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 230000005662 electromechanics Effects 0.000 description 1
- 125000003700 epoxy group Chemical group 0.000 description 1
- 238000007496 glass forming Methods 0.000 description 1
- 150000004678 hydrides Chemical class 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- UGKDIUIOSMUOAW-UHFFFAOYSA-N iron nickel Chemical compound [Fe].[Ni] UGKDIUIOSMUOAW-UHFFFAOYSA-N 0.000 description 1
- 238000004898 kneading Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000001050 lubricating effect Effects 0.000 description 1
- 230000005415 magnetization Effects 0.000 description 1
- 150000004706 metal oxides Chemical class 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000006082 mold release agent Substances 0.000 description 1
- 239000011212 mouldable composite material Substances 0.000 description 1
- 210000003739 neck Anatomy 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 150000002825 nitriles Chemical class 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 229910052755 nonmetal Inorganic materials 0.000 description 1
- 150000002899 organoaluminium compounds Chemical class 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 239000005011 phenolic resin Substances 0.000 description 1
- 229920001568 phenolic resin Polymers 0.000 description 1
- 229910000073 phosphorus hydride Inorganic materials 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 239000012704 polymeric precursor Substances 0.000 description 1
- 229920001296 polysiloxane Polymers 0.000 description 1
- UMJSCPRVCHMLSP-UHFFFAOYSA-N pyridine Natural products COC1=CC=CN=C1 UMJSCPRVCHMLSP-UHFFFAOYSA-N 0.000 description 1
- 238000012552 review Methods 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 150000004756 silanes Chemical class 0.000 description 1
- 125000005372 silanol group Chemical group 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
- 239000011734 sodium Substances 0.000 description 1
- HSNUIYJWTSJUMS-UHFFFAOYSA-N sodium;trimethyl(oxido)silane Chemical compound [Na+].C[Si](C)(C)[O-] HSNUIYJWTSJUMS-UHFFFAOYSA-N 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 239000011593 sulfur Substances 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
- 238000005496 tempering Methods 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 238000001149 thermolysis Methods 0.000 description 1
- 238000011282 treatment Methods 0.000 description 1
- TUQLLQQWSNWKCF-UHFFFAOYSA-N trimethoxymethylsilane Chemical compound COC([SiH3])(OC)OC TUQLLQQWSNWKCF-UHFFFAOYSA-N 0.000 description 1
- 230000004580 weight loss Effects 0.000 description 1
Classifications
-
- 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
- H01F1/26—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 by macromolecular organic substances
-
- 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
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F41/00—Apparatus or processes specially adapted for manufacturing or assembling magnets, inductances or transformers; Apparatus or processes specially adapted for manufacturing materials characterised by their magnetic properties
- H01F41/02—Apparatus or processes specially adapted for manufacturing or assembling magnets, inductances or transformers; Apparatus or processes specially adapted for manufacturing materials characterised by their magnetic properties for manufacturing cores, coils, or magnets
- H01F41/0206—Manufacturing of magnetic cores by mechanical means
- H01F41/0246—Manufacturing of magnetic circuits by moulding or by pressing powder
Definitions
- the invention relates to a soft magnetic, mouldable Composite material that has soft magnetic properties Powder contains a non-magnetic coating have, as well as a method for its production.
- Soft magnetic materials are required for the production of temperature, corrosion and solvent resistant magnetic components in the electronics sector and especially in electromechanics. These soft magnetic components require certain properties: they should have a high permeability ( ⁇ max ), a high magnetic saturation (B s ), a low coercive force (H c ) and a high specific electrical resistance ( ⁇ spec ). The combination of these magnetic properties with a high specific electrical resistance results in high switching dynamics, that is to say that the magnetic saturation and demagnetization of such a component take place within a short time.
- EP 0 540 504 B1 discloses soft magnetic powders prepare with a plastic binder and thus through a Injection molding process to produce corresponding components.
- the powder parts in injection moldable Composite materials limited to a maximum of 65% by volume.
- the compression takes place in the case of axial pressing of free-flowing powders with almost no material flow.
- the fill levels of these composite materials are typically at 90-98 vol%.
- thermosetting resins for example epoxies or phenolic resins
- thermosetting resins for example epoxies or phenolic resins
- organic solvents for example Fuels for internal combustion engines
- soluble are, or swell strongly.
- the corresponding Composite components change their dimensions under these conditions, lose their strength and fail completely.
- appropriate composite materials with high temperature and media resistance for example in organic solvents, especially fuels for internal combustion engines.
- Another Problem have so far set the operating conditions for these components among which are both thermoplastics and thermosets no longer represent a suitable binder because they are otherwise would completely decompose.
- Coating the soft magnetic powder with compounds of the boron or aluminum, which in pyrolysis in corresponding Skipping ceramics is another way solvent resistance and temperature resistance of the soft magnetic composite material and the material produced from it Increase molded parts.
- the temperature after a shaping of the material is advantageously chosen so that the coating material is converted into a ceramic, metallic or even intermetallic end product. This results in a high magnetization and a temperature and solvent resistance achieved.
- Silicon compounds selected from the group consisting of from binary hydrogen compounds of silicon, polydialkylsilanes, Carbosilanes, polysilazanes, alkoxyalkylsilanes, Alkyl polysiloxanes, alkyl silanols and compounds of alkylsilanols with elements of the first main group.
- This ensures that a wide connection class of molecular precursor compounds of silicon can be used, which in pyrolysis to different Ceramics, both based on silicon-oxygen, or also on a silicon-nitrogen or silicon-nitrogen-oxygen basis to provide can and optimized according to the desired requirement profile are.
- the applications of the component to be manufactured so can the corresponding ceramics that also one Influence on the magnetic field strength and the switching time which has soft magnetic connections. It is also possible to change the temperature range for the Choose application accordingly.
- Soft magnetic powder boron compounds selected from the group consisting of borazole, pyridine or other ⁇ -donor borane adducts, for example borane-phosphine, borane-phosphinite, Borane-sulfur or borane-nitrogen adducts, Borosilazanes and polyborazanes are used, so that in simple way after the thermolysis different boron-containing Ceramics can be made available in a simple manner can
- a polyazalane as an aluminum precursor compound to use, which in very small quantities of 0.2-2% by weight, based on the total weight can be. This makes aluminum-nitrogen ceramics as Coating for the soft magnetic powder produced, wherein the weight fraction of the soft magnetic powder especially is high.
- the inorganic, or silicon, boron and organoaluminium compounds used for coating the soft magnetic powders which are predominantly polymeric in character, have good sliding or lubricating properties. After hardening, they thus represent a thermosetting binder, which is converted into a ceramic or into alloy additives for ferrous metals by subsequent thermal decomposition (pyrolysis). In connection with oxidation-sensitive magnetic materials, such as pure iron or pure nickel, the pyrolysis takes place under protective gas. In order to obtain composite bodies with a small proportion of pores, the volume shrinkage occurring during the pyrolysis must be small, which is ensured by the compounds used. Silicon hydrogen compounds (silicon hydrides) are one example.
- Silicon hydrides with multiple Si atoms can be melted and thus also serve as lubricants for the coated magnetic powders. Depending on the hydride used, they decompose into Si and H 2 at higher temperatures. When the temperature increases further, the Si alloys in a surface layer, for example with pure iron powder. The Fe-Si alloy layer has a higher electrical resistance and a lower melting point than pure iron. The iron powder particles coated with Fe-Si sinter together to form composite bodies with a higher electrical resistance than pure iron. An alternative to this is the deposition of high-purity silicon on iron powder particles by thermal decomposition of SiH 4 . The method is common in semiconductor manufacturing for the build-up of silicon layers and in the tempering of glasses. Low molecular weight silicon hydrides are self-igniting, so that all process steps take place under protective gas.
- a silicon carbide ceramic according to the invention is used, for example prepared by pyrolysis of polydialkylsilanes. In Connection with powders from the series of ferrous metals the elimination of carbon-containing compounds in the Pyrolysis to carburize. Through annealing treatments in hydrogen-containing The atmosphere then becomes the metal of the Carbon content withdrawn again.
- Precursor compounds for BN ceramics as coating material are pyrolyzed under an ammonia atmosphere.
- RCP Cubbon RAPRA Review Report No. 76, Polymeric Precursors for Ceramic Materials, Vol. 7, No. 4, 1994.
- Borazole B 3 N 3 H 6
- B 3 N 3 H 6 which splits off under reduced pressure at 90 ° CH 2 and turns into a polymer analogous to polyphenylene, has proven to be particularly suitable for soft-magnetic composite materials with a ceramic coating.
- the elimination of H 2 continues until the hexagonal modification of BN is reached at approx. 750 ° C.
- the pyrolysis takes place only under protective gas, for example argon or nitrogen, and not in an ammonia atmosphere.
- the resulting slight weight loss of 5.1% results in low shrinkage and thus a small pore volume in the combination of BN and the magnetic powder.
- polyazalanes As a suitable starting material for the coating of magnetic powders with an aluminum nitride ceramic, polyazalanes were found. These were by thermal condensation of Diisobutylaluminum hydride synthesized with unsaturated nitriles, which leads to curable liquid polyazalanes. This was used to coat the magnetic powders.
- the polyazalans also serve as a thermoset glide and binder, which after subsequent pyrolysis crosslinked to a non-melting solid at 200 ° C. and in the next process step completely under an inert atmosphere pyrolyzed to AlN.
- Carbosilanes and polysilazanes have proven to be a suitable starting material for coating magnetic powders with a silicon nitride ceramic.
- Silicon nitride Si 3 N 4 is formed by pyrolysis of these compounds in an ammonia atmosphere. Pyrolysis under protective gas produced a coating with silicon carbonitrides of the formula SiN x C y .
- Glasses, enamels and glazes are combinations of metal and non-metal oxides of different compositions.
- An embodiment for the production of glass-like coatings of soft magnetic powders is the use of silanes with several silanol groups which form polymers when water is added with the elimination of alcohol.
- the product NH 2100 manufactured by Hüls is a not yet fully cross-linked, soluble and meltable polycondensate of trimethoxymethylsilane (CH 3 Si (OCH 3 ) 3 ) x and is an excellent precursor material for a glass-like coating of magnetic powders.
- the electrical resistance drops to 5 ⁇ m (pure iron has 0.1 ⁇ m), while the bending strength increases to 80 N / mm 2 .
- the iron-iron sintered bridges and the strength increase, while the specific electrical resistance continues to decrease.
- the corresponding glasses or enamels are formed by adding further compounds which can be converted into glass-forming oxides. Their composition is selected with a view to good adhesion to the magnetic powder.
- an addition of aluminum stearate serves both as a lubricant for removal from the press tool and after its thermal decomposition to Al 2 0 3 as a glass former.
- phosphated iron powder (AB 100.32, Höganäs) is wetted in the kneader with a solution of 2.4 g of methylpolysiloxane prepolymer (NH 2100, Nünchritz chemical plant) in acetone. After adding a solution of 46.3 g sodium trimethylsilanolate in acetone, a gel coat forms around the iron particles. After the acetone has been evaporated in a kneader, 5 g of aluminum tristearate are added and this is melted at 140 ° C. while kneading. The aluminum tristearate acts as a lubricant and mold release agent during the subsequent axial pressing of the composite material.
- the methylpolysiloxane prepolymer When the compacts are heated to 200 ° C under protective gas, the methylpolysiloxane prepolymer initially hardens. When the temperature is increased further to 800 ° C., all the products used pyrolyze and melt to about 40 g of a glass with the approximate composition 27 g Si0 2 , 12.8 g Na 2 O and 0.3 g A1 2 0 3 .
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- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Dispersion Chemistry (AREA)
- Physics & Mathematics (AREA)
- Spectroscopy & Molecular Physics (AREA)
- Manufacturing & Machinery (AREA)
- Soft Magnetic Materials (AREA)
- Powder Metallurgy (AREA)
Abstract
Description
Die Erfindung betrifft einen weichmagnetischen, formbaren Verbundwerkstoff, der weichmagnetische Eigenschaften aufweisende Pulver enthält, die eine nichtmagnetische Beschichtung aufweisen, sowie ein Verfahren zu dessen Herstellung.The invention relates to a soft magnetic, mouldable Composite material that has soft magnetic properties Powder contains a non-magnetic coating have, as well as a method for its production.
Weichmagnetischen Werkstoffe werden zur Herstellung von temperatur-, korrosions- und lösungsmittelbeständigen magnetischen Bauteilen im Elektroniksektor und insbesondere in der Elektromechanik benötigt. Dabei bedürfen diese weichmagnetischen Bauteile gewisser Eigenschaften: sie sollen eine hohe Permeabilität (µmax), eine hohe magnetische Sättigung (Bs), eine geringe Koerzitivfeldstärke (Hc) und einen hohen spezifischen elektrischen Widerstand (ρspez) aufweisen. Die Kombination dieser magnetischen Eigenschaften mit einem hohen spezifischen elektrischen Widerstand ergibt eine hohe Schaltdynamik, das heißt, die magnetische Sättigung und die Entmagnetisierung eines derartigen Bauteiles erfolgen innerhalb kurzer Zeit. Soft magnetic materials are required for the production of temperature, corrosion and solvent resistant magnetic components in the electronics sector and especially in electromechanics. These soft magnetic components require certain properties: they should have a high permeability (µ max ), a high magnetic saturation (B s ), a low coercive force (H c ) and a high specific electrical resistance (ρ spec ). The combination of these magnetic properties with a high specific electrical resistance results in high switching dynamics, that is to say that the magnetic saturation and demagnetization of such a component take place within a short time.
Bislang werden beispielweise Weicheisenbleche zu Lamellenpaketen verklebt, um als Anker von Elektromotoren zu dienen. Die Lagenisolation wirkt jedoch nur in einer Richtung. Aus dem EP 0 540 504 B1 ist bekannt, weichmagnetische Pulvern mit einem Kunststoffbinder aufzubereiten und damit durch ein Spritzgußverfahren entsprechende Bauteile herzustellen. Um die für das Spritzgießen notwendige Fließfähigkeit zu gewährleisten, sind die Pulveranteile in spritzgießfähigen Verbundwerkstoffen auf maximal 65 Vol.-% begrenzt. Demgegenüber erfolgt beispielsweise bei axialem Verpressen die Verdichtung von rieselfähigen Pulvern nahezu ohne Materialfluß. Die Füllgrade dieser Verbundwerkstoffe liegen typischerweise bei 90-98 Vol.-%. Die durch axiales Verpressen von Pulvern geformten Bauteile zeichnen sich im Vergleich zu spritzgegossenen deshalb durch wesentlich höhere Permeabilitäten und höhere magnetische Feldstärken im Sättigungsbereich aus. Axiales Verpressen von Pulvern aus Reineisen oder EisenNickel mit Duroplastharzen, beispielweise Epoxiden oder Phenolharzen hat jedoch den Nachteil, daß die bislang verwendeten thermoplastischen und duroplastischen Bindemittel bei erhöhter Temperatur in organischen Lösungsmitteln, beispielsweise Kraftstoffen für Verbrennungsmotoren, löslich sind, beziehungsweise stark aufquellen. Die entsprechenden Verbundbauteile ändern unter diesen Bedingungen ihre Abmessungen, verlieren ihre Festigkeit und versagen gänzlich. Es war bislang nicht möglich, entsprechende Verbundwerkstoffe mit hoher Temperatur- und Medienbeständigkeit, beispielsweise in organischen Lösungsmitteln, insbesondere Kraftstoffen für Verbrennungsmotoren, herzustellen. Ein weiteres Problem stellten bislang diejenigen Einsatzbedingungen dieser Bauteile dar, unter denen sowohl Thermoplaste als auch Duroplaste kein geeignetes Bindemittel mehr darstellen, da sie sich sonst vollständig zersetzen würden. So far, for example, soft iron sheets have become lamella packages glued to serve as an anchor for electric motors. However, the layer insulation only works in one direction. Out EP 0 540 504 B1 discloses soft magnetic powders prepare with a plastic binder and thus through a Injection molding process to produce corresponding components. Around to ensure the flowability required for injection molding, are the powder parts in injection moldable Composite materials limited to a maximum of 65% by volume. In contrast for example, the compression takes place in the case of axial pressing of free-flowing powders with almost no material flow. The fill levels of these composite materials are typically at 90-98 vol%. By axially pressing powders molded components stand out compared to injection molded ones therefore by much higher permeabilities and higher magnetic field strengths in the saturation range. Axial pressing of pure iron or iron-nickel powders with thermosetting resins, for example epoxies or phenolic resins has the disadvantage, however, that the previously used thermoplastic and thermosetting binders elevated temperature in organic solvents, for example Fuels for internal combustion engines, soluble are, or swell strongly. The corresponding Composite components change their dimensions under these conditions, lose their strength and fail completely. It was not possible until now, appropriate composite materials with high temperature and media resistance, for example in organic solvents, especially fuels for internal combustion engines. Another Problem have so far set the operating conditions for these components among which are both thermoplastics and thermosets no longer represent a suitable binder because they are otherwise would completely decompose.
In dem Artikel von H. P. Baldus und M. Jansen in: "Angewandte Chemie 1997, 109, Seite 338-394", werden moderne Hochleistungskeramiken beschrieben, die aus molekularen Vorläufern durch Pyrolyse gebildet werden und teilweise ebenfalls magnetische Eigenschaften aufweisen. Diese Keramiken sind äußerst temperatur- und lösungsmittelstabil.In the article by H. P. Baldus and M. Jansen in: "Angewandte Chemie 1997, 109, pages 338-394 ", become modern high-performance ceramics described from molecular precursors formed by pyrolysis and partly also magnetic Have properties. These ceramics are extreme temperature and solvent stable.
Durch die Beschichtung von weichmagnetischen Pulverkörnern mit einer siliziumhaltigen Verbindung, die bei Pyrolyse in eine siliziumhaltige Keramik übergeht, ist es möglich, die Koerzitivfeldstärke zu erhöhen, und die Temperaturstabilität eines aus diesem Verbundwerkstoff hergestellten Formteils entscheidend zu verbessern.By coating soft magnetic powder grains with a silicon-containing compound, which in pyrolysis in a silicon-containing ceramic passes over, it is possible to Increase coercive force, and temperature stability a molded part made from this composite material to improve decisively.
Beschichten des Weichmagnetpulvers mit Verbindungen des Bors beziehungsweise des Aluminiums, die bei Pyrolyse in entsprechende Keramiken übergehen, ist eine weitere Möglichkeit, die Lösemittelbeständigkeit und die Temperaturbeständigkeit des weichmagnetischen Verbundwerkstoffes und der daraus hergestellten Formteile zu erhöhen.Coating the soft magnetic powder with compounds of the boron or aluminum, which in pyrolysis in corresponding Skipping ceramics is another way solvent resistance and temperature resistance of the soft magnetic composite material and the material produced from it Increase molded parts.
Weitere vorteilhafte Ausgestaltungen und Weiterbildungen der Erfindung sind in den Unteransprüchen aufgeführt.Further advantageous refinements and developments of Invention are listed in the subclaims.
So wird bei einer Beschichtung der Pulverkörner mit einem Material aus einer Vorläuferkeramik, auch Precursorkeramik" genannt, welche entweder Silicium, Aluminium oder Bor als Hauptbestandteile enthält, die Temperatur nach einer Formgebung des Materials vorteilhaft so gewählt, daß sich das Beschichtungsmaterial in ein keramisches, metallisches oder sogar intermetallisches Endprodukt umwandelt. Damit wird eine hohe Magnetisierung und eine Temperatur- und Lösemittelbeständigkeit erzielt. So when coating the powder grains with a material from a precursor ceramic, too Precursor ceramic ", which contains either silicon, aluminum or boron as the main constituents, the temperature after a shaping of the material is advantageously chosen so that the coating material is converted into a ceramic, metallic or even intermetallic end product. This results in a high magnetization and a temperature and solvent resistance achieved.
In besonders bevorzugter Weise werden als Beschichtungsmaterial Siliziumverbindungen ausgewählt aus der Gruppe bestehend aus binären Wasserstoffverbindungen des Siliziums, Polydialkylsilanen, Carbosilanen, Polysilazanen, Alkoxyalkylsilanen, Alkylpolysiloxanen, Alkylsilanolen und Verbindungen von Alkylsilanolen mit Elementen der ersten Hauptgruppe verwendet. Damit ist gewährleistet, daß eine breite Verbindungsklasse von molekularen Vorläuferverbindungen des Siliziums eingesetzt werden kann, welches bei Pyrolyse zu verschiedenen Keramiken, sowohl auf Silizium-Sauerstoffbasis, beziehungsweise ebenso auf Silizium-Stickstoff oder Silizium-Stickstoff-Sauerstoff-Basis zur Verfügung gestellt werden können und je nach erwünschtem Anforderungsprofil optimiert sind. Entsprechend den Anwendungen des herzustellenden Bauteiles kann so die entsprechende Keramik, die auch einen Einfluß auf die magnetische Feldstärke und die Schaltzeit der weichmagnetischen Verbindungen hat, gewählt werden. Ebenso ist es dadurch möglich, den Temperaturbereich für die Anwendung entsprechend zu wählen.In a particularly preferred manner, are used as coating material Silicon compounds selected from the group consisting of from binary hydrogen compounds of silicon, polydialkylsilanes, Carbosilanes, polysilazanes, alkoxyalkylsilanes, Alkyl polysiloxanes, alkyl silanols and compounds of alkylsilanols with elements of the first main group. This ensures that a wide connection class of molecular precursor compounds of silicon can be used, which in pyrolysis to different Ceramics, both based on silicon-oxygen, or also on a silicon-nitrogen or silicon-nitrogen-oxygen basis to provide can and optimized according to the desired requirement profile are. According to the applications of the component to be manufactured so can the corresponding ceramics that also one Influence on the magnetic field strength and the switching time which has soft magnetic connections. It is also possible to change the temperature range for the Choose application accordingly.
In ebenso bevorzugter Weise können zum Beschichten des Weichmagnetpulvers Borverbindungen ausgewählt aus der Gruppe bestehend aus Borazol, Pyridin- oder sonstige π-Donor-Boranaddukte, beispielsweise Boran-Phosphan, Boran-Phosphinit, Boran-Schwefel oder Boran-Stickstoff-Addukte, Borsilazane und Polyborazane eingesetzt werden, so daß in einfacher Weise nach der Thermolyse verschiedene Borhaltige Keramiken in einfacher Weise zur Verfügung gestellt werden könnenIn a likewise preferred manner, for coating the Soft magnetic powder boron compounds selected from the group consisting of borazole, pyridine or other π-donor borane adducts, for example borane-phosphine, borane-phosphinite, Borane-sulfur or borane-nitrogen adducts, Borosilazanes and polyborazanes are used, so that in simple way after the thermolysis different boron-containing Ceramics can be made available in a simple manner can
Ebenso ist es bevorzugt möglich, ein Polyazalan als Aluminiumvorläuferverbindung zu verwenden, welches in Kleinstmengen von 0,2-2 Gew.%, bezogen auf die Gesamteinwaage, eingesetzt werden kann. Damit werden Aluminium-Stickstoff-Keramiken als Beschichtung für das weichmagnetische Pulver erzeugt, wobei der Gewichtsanteil des weichmagnetischen Pulvers besonders hoch ist.It is also preferably possible to use a polyazalane as an aluminum precursor compound to use, which in very small quantities of 0.2-2% by weight, based on the total weight can be. This makes aluminum-nitrogen ceramics as Coating for the soft magnetic powder produced, wherein the weight fraction of the soft magnetic powder especially is high.
Die zum Beschichten der weichmagnetischen Pulver eingesetzten anorganischen, beziehungsweise silizium-, bor und aluminiumorganischen Verbindungen mit vorwiegend polymeren Charakter weisen gute Gleit-, beziehungsweise Schmiereigenschaften auf. Nach der Aushärtung stellen sie somit ein duroplastisches Bindemittel dar, welches durch anschließende thermische Zersetzung (Pyrolyse) in eine Keramik oder in Legierungszusätze für Eisenmetalle umgewandelt wird. In Verbindung mit oxidationsempfindlichen magnetischen Materialien, wie beispielsweise Reineisen oder Reinnickel, erfolgt die Pyrolyse unter Schutzgas. Um Verbundkörper mit geringem Porenanteil zu erhalten, muß der bei der Pyrolyse auftretende Volumenschwund gering sein, was durch die eingesetzten Verbindungen gewährleistet ist. Ein Beispiel stellen Silizium-Wasserstoffverbindungen (Siliziumhydride) dar. Siliziumhydride mit mehren Si-Atomen sind schmelzbar und dienen somit zugleich als Gleitmittel für die beschichteten magnetischen Pulver. Sie zerfallen bei höheren Temperaturen je nach eingesetztem Hydrid in Si und H2. Bei weiterer Temperaturerhöhung legiert das Si in einer Oberflächenschicht, beispielsweise mit Reineisenpulver. Die Fe-Si-Legierungsschicht weist einen höheren elektrischen Widerstand und einen niedrigen Schmelzpunkt auf als Reineisen. Die mit Fe-Si beschichteten Eisenpulverteilchen sintern zu Verbundkörpern mit einem im Vergleich zu Reineisen höheren elektrischen Widerstand zusammen. Eine Alternative dazu ist die Abscheidung von Reinstsilizium auf Eisenpulverteilchen durch thermische Zersetzung von SiH4 . Das Verfahren ist bei der Halbleiterfertigung zum Aufbau von Siliziumschichten und beim Vergüten von Gläsern üblich. Niedermolekulare Siliziumhydride sind selbstentzündlich, so daß alle Verfahrensschritte unter Schutzgas erfolgen.The inorganic, or silicon, boron and organoaluminium compounds used for coating the soft magnetic powders, which are predominantly polymeric in character, have good sliding or lubricating properties. After hardening, they thus represent a thermosetting binder, which is converted into a ceramic or into alloy additives for ferrous metals by subsequent thermal decomposition (pyrolysis). In connection with oxidation-sensitive magnetic materials, such as pure iron or pure nickel, the pyrolysis takes place under protective gas. In order to obtain composite bodies with a small proportion of pores, the volume shrinkage occurring during the pyrolysis must be small, which is ensured by the compounds used. Silicon hydrogen compounds (silicon hydrides) are one example. Silicon hydrides with multiple Si atoms can be melted and thus also serve as lubricants for the coated magnetic powders. Depending on the hydride used, they decompose into Si and H 2 at higher temperatures. When the temperature increases further, the Si alloys in a surface layer, for example with pure iron powder. The Fe-Si alloy layer has a higher electrical resistance and a lower melting point than pure iron. The iron powder particles coated with Fe-Si sinter together to form composite bodies with a higher electrical resistance than pure iron. An alternative to this is the deposition of high-purity silicon on iron powder particles by thermal decomposition of SiH 4 . The method is common in semiconductor manufacturing for the build-up of silicon layers and in the tempering of glasses. Low molecular weight silicon hydrides are self-igniting, so that all process steps take place under protective gas.
Eine erfindungsgemäße Siliciumcarbidkeramik wird beispielsweise durch Pyrolyse von Polydialkylsilanen hergestellt. In Verbindung mit Pulvern aus der Reihe der Eisenmetalle führt die Abspaltung von kohlenstoffhaltigen Verbindungen bei der Pyrolyse zu Aufkohlen. Durch Glühbehandlungen in wasserstoffhaltiger Atmosphäre wird anschließend dem Metall der Kohlenstoffanteil wieder entzogen.A silicon carbide ceramic according to the invention is used, for example prepared by pyrolysis of polydialkylsilanes. In Connection with powders from the series of ferrous metals the elimination of carbon-containing compounds in the Pyrolysis to carburize. Through annealing treatments in hydrogen-containing The atmosphere then becomes the metal of the Carbon content withdrawn again.
Vorläuferverbindungen für BN-Keramiken als Beschichtungsmaterial werden unter Ammoniakatmosphäre pyrolysiert. (R.C.P. Cubbon, RAPRA Review Report Nr. 76, Polymeric Precursors for Ceramic Materials, Vol. 7, No. 4, 1994). Als besonders geeignet für weichmagnetische Verbundwerkstoffe mit einer keramischen Beschichtung erwies sich Borazol (B3N3H6), welches unter vermindertem Druck bereits bei 90 °C H2 abspaltet und in ein zu Polyphenylen analoges Polymer übergeht. Bei höheren Temperaturen schreitet die Abspaltung von H2 fort, bis bei ca. 750 °C die Stufe der hexagonalen Modifikation von BN erreicht ist. In diesem besonderen Falle erfolgt die Pyrolyse lediglich unter Schutzgas, beispielsweise Argon oder Stickstoff, und nicht in Ammoniakatmosphäre. Der dabei auftretende geringe Gewichtsverlust von 5,1 % hat eine geringe Schwindung und damit ein geringes Porenvolumen im Verbund aus BN und dem Magnetpulver zur Folge.Precursor compounds for BN ceramics as coating material are pyrolyzed under an ammonia atmosphere. (RCP Cubbon, RAPRA Review Report No. 76, Polymeric Precursors for Ceramic Materials, Vol. 7, No. 4, 1994). Borazole (B 3 N 3 H 6 ), which splits off under reduced pressure at 90 ° CH 2 and turns into a polymer analogous to polyphenylene, has proven to be particularly suitable for soft-magnetic composite materials with a ceramic coating. At higher temperatures, the elimination of H 2 continues until the hexagonal modification of BN is reached at approx. 750 ° C. In this particular case, the pyrolysis takes place only under protective gas, for example argon or nitrogen, and not in an ammonia atmosphere. The resulting slight weight loss of 5.1% results in low shrinkage and thus a small pore volume in the combination of BN and the magnetic powder.
Als geeigneter Ausgangstoff für die Beschichtung von Magnetpulvern mit einer Aluminiumnitrid-Keramik erwiesen sich Polyazalane. Diese wurden durch thermische Kondensation von Diisobutylaluminiumhydrid mit ungesättigten Nitrilen synthetisiert, was zu aushärtbarem flüssigen Polyazalanen führt. Damit wurden die magnetischen Pulver beschichtet. Die Polyazalane dienen dabei gleichzeitig als duroplastisches Gleit und Bindemittel, welches nach sich anschließender Pyrolyse bei 200 °C zu einem nichtschmelzenden Feststoff vernetzt und in nächsten Verfahrensschritt vollständig unter inerter Atmosphäre zu AlN pyrolysiert.As a suitable starting material for the coating of magnetic powders with an aluminum nitride ceramic, polyazalanes were found. These were by thermal condensation of Diisobutylaluminum hydride synthesized with unsaturated nitriles, which leads to curable liquid polyazalanes. This was used to coat the magnetic powders. The polyazalans also serve as a thermoset glide and binder, which after subsequent pyrolysis crosslinked to a non-melting solid at 200 ° C. and in the next process step completely under an inert atmosphere pyrolyzed to AlN.
Als geeigneter Ausgangstoff für die Beschichtung von Magnetpulvern mit einer Siliziumnitrid-Keramik erwiesen sich Carbosilane und Polysilazane. Siliziumnitrid Si3N4 entsteht dabei durch Pyrolyse dieser Verbindungen in Ammoniakatmosphäre. Die Pyrolyse unter Schutzgas erbrachte eine Beschichtung mit Siliziumcarbonitriden der Formel SiNxCy.Carbosilanes and polysilazanes have proven to be a suitable starting material for coating magnetic powders with a silicon nitride ceramic. Silicon nitride Si 3 N 4 is formed by pyrolysis of these compounds in an ammonia atmosphere. Pyrolysis under protective gas produced a coating with silicon carbonitrides of the formula SiN x C y .
Gläser, Emails und Lasuren stellen Kombinationen von Metallund Nichtmetalloxiden unterschiedlicher Zusammensetzung dar. Ein Ausführungsbeispiel zur Herstellung von glasartigen Beschichtungen von weichmagnetischen Pulvern ist die Verwendung von Silanen mit mehreren Silanolgruppen, die bei Zugabe von Wasser unter Abspaltung von Alkohol Polymere bilden. Das von der Fa. Hüls hergestellten Produkt NH 2100 ist ein noch nicht vollständig vernetztes, lösliches und schmelzbares Polykondensat des Trimethoxymethylsilan (CH3Si(OCH3)3)x und stellt ein ausgezeichnetes Vorläufermaterial für eine glasartige Beschichtung magnetischer Pulver dar. NH 2100 läßt sich unter Abspaltung von Wasser und Alkohol weiter kondensieren und geht bei einer anschließenden Pyrolyse mit einer keramischen Ausbeute von ca. 90 Gew.-% in ein Glas der Zusammensetzung SiOxCy (x = 1,9-2,1, y = 0,6-3,0) über.Glasses, enamels and glazes are combinations of metal and non-metal oxides of different compositions. An embodiment for the production of glass-like coatings of soft magnetic powders is the use of silanes with several silanol groups which form polymers when water is added with the elimination of alcohol. The product NH 2100 manufactured by Hüls is a not yet fully cross-linked, soluble and meltable polycondensate of trimethoxymethylsilane (CH 3 Si (OCH 3 ) 3 ) x and is an excellent precursor material for a glass-like coating of magnetic powders. NH 2100 leaves condense further with elimination of water and alcohol and, in the case of subsequent pyrolysis, goes into a glass of the composition SiO x C y (x = 1.9-2.1, y = 0) with a ceramic yield of approximately 90% by weight , 6-3.0) above.
99,9 Gew.-% Weicheisenpulver ABM 100,32 (oberflächenphosphatiert, Fa. Höganäs) werden mit 0,6 Gew.-% NH 2100 gecoatet, welches in einer Lösung in Aceton erfolgt. Bei Raumtemperatur wird diese Mischung unter 6 to/cm2 zu Probestäben verpreßt und das Harz bei 220 °C vernetzt. Die derart hergestellte Probe weist eine Festigkeit von 26 N/mm2 und einen spezifischen elektrischen Widerstand von 20000 µOhm auf. Das Polymer wird anschließend bei 700 °C unter Schutzgas pyrolysiert und geht in ein kohlenstoffhaltiges Glas SiOxCy über. Zusätzlich bilden sich erste Sinterhälse zwischen den Eisenteilchen. Dadurch sinkt der elektrische Widerstand auf 5 µΩm (Reineisen weist 0,1 µΩm auf), während die Biegefestigkeit auf 80 N/mm2 ansteigt. Bei weiterer Temperaturerhöhung nehmen die Eisen-Eisen-Sinterbrücken und die Festigkeit zu, während der spezifische elektrische Widerstand weiter abnimmt.99.9% by weight of soft iron powder ABM 100.32 (surface-phosphated, from Höganäs) are coated with 0.6% by weight of NH 2100, which is carried out in a solution in acetone. At room temperature, this mixture is pressed under 6 to / cm2 to test rods and the resin is crosslinked at 220 ° C. The sample produced in this way has a strength of 26 N / mm 2 and a specific electrical resistance of 20,000 μOhm. The polymer is then pyrolyzed at 700 ° C under a protective gas and passes into a carbon-containing glass SiO x C y . In addition, first sinter necks form between the iron particles. As a result, the electrical resistance drops to 5 µΩm (pure iron has 0.1 µΩm), while the bending strength increases to 80 N / mm 2 . As the temperature increases further, the iron-iron sintered bridges and the strength increase, while the specific electrical resistance continues to decrease.
Durch Zusatz weiterer Verbindungen, welche sich in glasbildende Oxide überführen lassen, entstehen die entsprechenden Gläser oder Emails. Ihre Zusammensetzung wird im Hinblick auf eine gute Haftung am Magnetpulver ausgewählt. So dient ein Zusatz von Aluminiumstearat sowohl als Gleitmittel zur Entformung aus dem Preßwerkzeug als auch nach seiner thermischen Zersetzung zu Al203 als Glasbildner.The corresponding glasses or enamels are formed by adding further compounds which can be converted into glass-forming oxides. Their composition is selected with a view to good adhesion to the magnetic powder. Thus, an addition of aluminum stearate serves both as a lubricant for removal from the press tool and after its thermal decomposition to Al 2 0 3 as a glass former.
946,5 g phosphatiertes Eisenpulver (AB 100.32,Fa. Höganäs) wird im Kneter mit einer Lösung von 2,4 g Methylpolysiloxan-Präpolymer (NH 2100, Chemiewerk Nünchritz) in Aceton benetzt. Nach Zugabe einer Lösung von 46,3 g Natrium-Trimethylsilanolat in Aceton bildet sich ein Gelmantel um die Eisenpartikel. Nach dem Verdampfen des Acetons im Kneter wird 5 g Aluminiumtristearat zugesetzt und dieses unter Kneten bei 140 °C aufgeschmolzen. Das Aluminiumtristearat wirkt beim anschließenden axialen Verpressen des Verbundwerkstoffes als Gleit- und Formtrennmittel. Beim Erhitzen der Preßlinge unter Schutzgas auf 200 °C härtet das Methylpolysiloxan-Präpolymer zunächst aus. Bei weiterer Temperaturerhöhung auf 800°C pyrolysieren alle eingesetzten Produkte und schmelzen zu ca. 40 g eines Glases mit der ungefähren Zusammensetzung 27 g Si02, 12.8 g Na2O und 0,3 g A1203 auf.946.5 g of phosphated iron powder (AB 100.32, Höganäs) is wetted in the kneader with a solution of 2.4 g of methylpolysiloxane prepolymer (NH 2100, Nünchritz chemical plant) in acetone. After adding a solution of 46.3 g sodium trimethylsilanolate in acetone, a gel coat forms around the iron particles. After the acetone has been evaporated in a kneader, 5 g of aluminum tristearate are added and this is melted at 140 ° C. while kneading. The aluminum tristearate acts as a lubricant and mold release agent during the subsequent axial pressing of the composite material. When the compacts are heated to 200 ° C under protective gas, the methylpolysiloxane prepolymer initially hardens. When the temperature is increased further to 800 ° C., all the products used pyrolyze and melt to about 40 g of a glass with the approximate composition 27 g Si0 2 , 12.8 g Na 2 O and 0.3 g A1 2 0 3 .
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Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
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DE19945619A1 (en) * | 1999-09-23 | 2001-04-19 | Bosch Gmbh Robert | Press compound and method for producing a soft magnetic composite material with the press compound |
DE60132314T2 (en) * | 2000-03-10 | 2009-01-02 | Höganäs Ab | METHOD FOR PRODUCING POWDER ON IRON BASE AND POWDER ON IRON BASIS |
DE10106172A1 (en) * | 2001-02-10 | 2002-08-29 | Bosch Gmbh Robert | Process for producing a molded part from a soft magnetic composite material |
US7153594B2 (en) * | 2002-12-23 | 2006-12-26 | Höganäs Ab | Iron-based powder |
DE10331339A1 (en) | 2003-07-10 | 2005-02-03 | Siemens Ag | Electromagnetic switching device |
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SE0303580D0 (en) * | 2003-12-29 | 2003-12-29 | Hoeganaes Ab | Composition for producing soft magnetic composites by powder metallurgy |
US7494600B2 (en) * | 2003-12-29 | 2009-02-24 | Höganäs Ab | Composition for producing soft magnetic composites by powder metallurgy |
SE0401644D0 (en) * | 2004-06-23 | 2004-06-23 | Hoeganaes Ab | Lubricants for insulated soft magnetic iron-based powder compositions |
KR100845392B1 (en) | 2004-06-23 | 2008-07-09 | 회가내스 아베 | Lubricants for insulated soft magnetic iron-based powder compositions |
US7416578B2 (en) * | 2004-09-17 | 2008-08-26 | Höganäs Ab | Powder metal composition |
JP4613622B2 (en) * | 2005-01-20 | 2011-01-19 | 住友電気工業株式会社 | Soft magnetic material and dust core |
DE102006032517B4 (en) * | 2006-07-12 | 2015-12-24 | Vaccumschmelze Gmbh & Co. Kg | Process for the preparation of powder composite cores and powder composite core |
JP5332408B2 (en) * | 2008-08-29 | 2013-11-06 | Tdk株式会社 | Powder magnetic core and manufacturing method thereof |
US8911663B2 (en) * | 2009-03-05 | 2014-12-16 | Quebec Metal Powders, Ltd. | Insulated iron-base powder for soft magnetic applications |
DE102013212866A1 (en) * | 2013-07-02 | 2015-01-08 | Robert Bosch Gmbh | Sintered soft magnetic composite material and process for its production |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4696725A (en) * | 1985-06-26 | 1987-09-29 | Kabushiki Kaisha Toshiba | Magnetic core and preparation thereof |
US4919734A (en) * | 1984-09-29 | 1990-04-24 | Kabushiki Kaisha Toshiba | Compressed magnetic powder core |
EP0406580A1 (en) * | 1989-06-09 | 1991-01-09 | Matsushita Electric Industrial Co., Ltd. | A composite material and a method for producing the same |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2068658A (en) * | 1934-06-20 | 1937-01-26 | Associated Electric Lab Inc | Inductance coil core |
DE667919C (en) * | 1934-08-16 | 1938-11-23 | Herbert Burchard | Process for the production of mass cores |
DE966314C (en) * | 1949-08-26 | 1957-07-25 | Standard Elek K Ag | Process for the production of mass cores from magnetizable powder particles raised with an insulating material of high softening temperature |
US3856582A (en) * | 1973-06-22 | 1974-12-24 | Gen Electric | Fabrication of matrix bonded transition metal-rare earth alloy magnets |
DE2501042B2 (en) * | 1974-01-23 | 1977-12-08 | Rilsan Corp, Glen Rock, N.J. (V.StA.) | POWDER, THE PARTICLES OF WHICH ARE PRACTICALLY UNIFORM COVERED WITH A NYLON, WHICH CAN BE TRAINED OR. LET FIBERS DRAW OUT |
JPS579802A (en) * | 1980-06-20 | 1982-01-19 | Dainippon Ink & Chem Inc | Metallic magnetic powder and its manufacture |
DE3026696A1 (en) * | 1980-07-15 | 1982-02-18 | Basf Ag, 6700 Ludwigshafen | FERROMAGNETIC, PARTICULARLY IRON METAL PARTICLES WITH A SURFACE COVER, METHOD FOR THE PRODUCTION THEREOF AND THEIR USE FOR THE PRODUCTION OF MAGNETIC RECORDING CARRIERS |
US4601765A (en) * | 1983-05-05 | 1986-07-22 | General Electric Company | Powdered iron core magnetic devices |
JPH0611008B2 (en) * | 1983-11-16 | 1994-02-09 | 株式会社東芝 | Dust core |
US4731191A (en) * | 1985-12-31 | 1988-03-15 | Dow Corning Corporation | Method for protecting carbonyl iron powder and compositions therefrom |
JPH01164006A (en) * | 1987-09-02 | 1989-06-28 | Kao Corp | Ferromagnetic metal powder and manufacture thereof |
US4869964A (en) * | 1987-12-14 | 1989-09-26 | The B. F. Goodrich Company | Oxidation resistant compositions for use with rare earth magnets |
US5198137A (en) * | 1989-06-12 | 1993-03-30 | Hoeganaes Corporation | Thermoplastic coated magnetic powder compositions and methods of making same |
JPH03241705A (en) * | 1989-11-14 | 1991-10-28 | Hitachi Metals Ltd | Magnetically anisotropic magnet and manufacture thereof |
US5211896A (en) * | 1991-06-07 | 1993-05-18 | General Motors Corporation | Composite iron material |
JPH05109520A (en) * | 1991-08-19 | 1993-04-30 | Tdk Corp | Composite soft magnetic material |
US5206327A (en) * | 1991-10-07 | 1993-04-27 | Hercules Incorporated | Preceramic polymers incorporating boron and their application in the sintering of carbide ceramics |
EP0574856B1 (en) * | 1992-06-15 | 1996-12-11 | Kureha Kagaku Kogyo Kabushiki Kaisha | Resin magnetic compound and molded article thereof |
US5898253A (en) * | 1993-11-18 | 1999-04-27 | General Motors Corporation | Grain oriented composite soft magnetic structure |
US5798439A (en) * | 1996-07-26 | 1998-08-25 | National Research Council Of Canada | Composite insulating coatings for powders, especially for magnetic applications |
US5980603A (en) * | 1998-05-18 | 1999-11-09 | National Research Council Of Canada | Ferrous powder compositions containing a polymeric binder-lubricant blend |
US6410770B2 (en) | 2000-02-08 | 2002-06-25 | Gelest, Inc. | Chloride-free process for the production of alkylsilanes suitable for microelectronic applications |
-
1997
- 1997-08-14 DE DE19735271A patent/DE19735271C2/en not_active Expired - Fee Related
-
1998
- 1998-08-11 US US09/284,368 patent/US6537389B1/en not_active Expired - Fee Related
- 1998-08-11 EP EP98948761A patent/EP0931322B1/en not_active Expired - Lifetime
- 1998-08-11 WO PCT/DE1998/002297 patent/WO1999009565A1/en active IP Right Grant
- 1998-08-11 EP EP00119956A patent/EP1061534A3/en not_active Withdrawn
- 1998-08-11 JP JP51265599A patent/JP2001504283A/en active Pending
- 1998-08-11 DE DE59808444T patent/DE59808444D1/en not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4919734A (en) * | 1984-09-29 | 1990-04-24 | Kabushiki Kaisha Toshiba | Compressed magnetic powder core |
EP0434669A2 (en) * | 1984-09-29 | 1991-06-26 | Kabushiki Kaisha Toshiba | Method of making a coated magnetic powder and a compressed magnetic powder core |
US4696725A (en) * | 1985-06-26 | 1987-09-29 | Kabushiki Kaisha Toshiba | Magnetic core and preparation thereof |
EP0406580A1 (en) * | 1989-06-09 | 1991-01-09 | Matsushita Electric Industrial Co., Ltd. | A composite material and a method for producing the same |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2004033135A1 (en) * | 2002-09-27 | 2004-04-22 | Vacuumschmelze Gmbh & Co. Kg | Moulded soft magnetic part produced by metal powder processing technique and exhibiting high maximum permeability, related manufacturing methods and uses |
Also Published As
Publication number | Publication date |
---|---|
DE59808444D1 (en) | 2003-06-26 |
EP0931322A1 (en) | 1999-07-28 |
EP0931322B1 (en) | 2003-05-21 |
DE19735271C2 (en) | 2000-05-04 |
JP2001504283A (en) | 2001-03-27 |
US6537389B1 (en) | 2003-03-25 |
DE19735271A1 (en) | 1999-02-25 |
WO1999009565A1 (en) | 1999-02-25 |
EP1061534A3 (en) | 2000-12-27 |
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