WO2012032961A1 - 磁性材料およびその製造方法 - Google Patents
磁性材料およびその製造方法 Download PDFInfo
- Publication number
- WO2012032961A1 WO2012032961A1 PCT/JP2011/069494 JP2011069494W WO2012032961A1 WO 2012032961 A1 WO2012032961 A1 WO 2012032961A1 JP 2011069494 W JP2011069494 W JP 2011069494W WO 2012032961 A1 WO2012032961 A1 WO 2012032961A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- amorphous metal
- magnetic material
- magnetic
- temperature
- magnet
- Prior art date
Links
- 239000000696 magnetic material Substances 0.000 title claims abstract description 85
- 238000004519 manufacturing process Methods 0.000 title claims description 36
- 239000005300 metallic glass Substances 0.000 claims abstract description 145
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 73
- 238000010438 heat treatment Methods 0.000 claims abstract description 39
- 229910052761 rare earth metal Inorganic materials 0.000 claims abstract description 35
- 238000002425 crystallisation Methods 0.000 claims abstract description 31
- 230000008025 crystallization Effects 0.000 claims abstract description 31
- 239000000203 mixture Substances 0.000 claims abstract description 23
- 229910052742 iron Inorganic materials 0.000 claims abstract description 22
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims abstract description 14
- 229910052796 boron Inorganic materials 0.000 claims abstract description 14
- 230000009477 glass transition Effects 0.000 claims abstract description 12
- 239000000843 powder Substances 0.000 claims description 80
- 239000000654 additive Substances 0.000 claims description 28
- 230000000996 additive effect Effects 0.000 claims description 24
- 229910017052 cobalt Inorganic materials 0.000 claims description 23
- 239000010941 cobalt Substances 0.000 claims description 23
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 19
- 238000002156 mixing Methods 0.000 claims description 13
- 239000011812 mixed powder Substances 0.000 claims description 12
- 238000002490 spark plasma sintering Methods 0.000 claims description 6
- 239000000463 material Substances 0.000 claims description 5
- 230000000977 initiatory effect Effects 0.000 claims 1
- 238000000034 method Methods 0.000 abstract description 40
- 239000006247 magnetic powder Substances 0.000 abstract description 8
- 229910045601 alloy Inorganic materials 0.000 description 51
- 239000000956 alloy Substances 0.000 description 51
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 49
- 229910052757 nitrogen Inorganic materials 0.000 description 26
- 238000005245 sintering Methods 0.000 description 24
- 239000002114 nanocomposite Substances 0.000 description 18
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 17
- 239000002245 particle Substances 0.000 description 16
- 239000013078 crystal Substances 0.000 description 13
- 238000000465 moulding Methods 0.000 description 13
- 238000001816 cooling Methods 0.000 description 12
- 230000004907 flux Effects 0.000 description 11
- 229910052782 aluminium Inorganic materials 0.000 description 10
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 10
- 239000010936 titanium Substances 0.000 description 10
- 239000007789 gas Substances 0.000 description 9
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 8
- 239000011651 chromium Substances 0.000 description 8
- 239000010949 copper Substances 0.000 description 8
- 238000002844 melting Methods 0.000 description 8
- 230000008018 melting Effects 0.000 description 8
- 239000010955 niobium Substances 0.000 description 8
- 239000012298 atmosphere Substances 0.000 description 7
- 238000003825 pressing Methods 0.000 description 7
- 229910052719 titanium Inorganic materials 0.000 description 7
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 7
- 229910052721 tungsten Inorganic materials 0.000 description 7
- 239000010937 tungsten Substances 0.000 description 7
- 238000000354 decomposition reaction Methods 0.000 description 6
- 238000000113 differential scanning calorimetry Methods 0.000 description 6
- 229910052751 metal Inorganic materials 0.000 description 6
- 239000002184 metal Substances 0.000 description 6
- 229910052759 nickel Inorganic materials 0.000 description 6
- 239000011701 zinc Substances 0.000 description 6
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 5
- 150000002500 ions Chemical class 0.000 description 5
- 230000005415 magnetization Effects 0.000 description 5
- 230000002093 peripheral effect Effects 0.000 description 5
- 150000002910 rare earth metals Chemical class 0.000 description 5
- 230000007704 transition Effects 0.000 description 5
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 4
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 4
- 229910052779 Neodymium Inorganic materials 0.000 description 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 4
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 4
- 229910052786 argon Inorganic materials 0.000 description 4
- 229910052804 chromium Inorganic materials 0.000 description 4
- 230000000052 comparative effect Effects 0.000 description 4
- 229910052802 copper Inorganic materials 0.000 description 4
- 230000007423 decrease Effects 0.000 description 4
- 238000009689 gas atomisation Methods 0.000 description 4
- 229910002804 graphite Inorganic materials 0.000 description 4
- 239000010439 graphite Substances 0.000 description 4
- QEFYFXOXNSNQGX-UHFFFAOYSA-N neodymium atom Chemical compound [Nd] QEFYFXOXNSNQGX-UHFFFAOYSA-N 0.000 description 4
- 229910001172 neodymium magnet Inorganic materials 0.000 description 4
- 229910052758 niobium Inorganic materials 0.000 description 4
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 4
- 239000002994 raw material Substances 0.000 description 4
- 238000005096 rolling process Methods 0.000 description 4
- 229910052710 silicon Inorganic materials 0.000 description 4
- 239000010703 silicon Substances 0.000 description 4
- 229910052726 zirconium Inorganic materials 0.000 description 4
- 229910052772 Samarium Inorganic materials 0.000 description 3
- 229910001297 Zn alloy Inorganic materials 0.000 description 3
- 229910000808 amorphous metal alloy Inorganic materials 0.000 description 3
- 150000001875 compounds Chemical class 0.000 description 3
- 229910001873 dinitrogen Inorganic materials 0.000 description 3
- 239000003822 epoxy resin Substances 0.000 description 3
- 238000010304 firing Methods 0.000 description 3
- 239000008187 granular material Substances 0.000 description 3
- KDLHZDBZIXYQEI-UHFFFAOYSA-N palladium Substances [Pd] KDLHZDBZIXYQEI-UHFFFAOYSA-N 0.000 description 3
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Substances [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 3
- 229920000647 polyepoxide Polymers 0.000 description 3
- 229920005989 resin Polymers 0.000 description 3
- 239000011347 resin Substances 0.000 description 3
- 229910052715 tantalum Inorganic materials 0.000 description 3
- 229910052725 zinc Inorganic materials 0.000 description 3
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 2
- XDTMQSROBMDMFD-UHFFFAOYSA-N Cyclohexane Chemical compound C1CCCCC1 XDTMQSROBMDMFD-UHFFFAOYSA-N 0.000 description 2
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 2
- 229910018487 Ni—Cr Inorganic materials 0.000 description 2
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 2
- 239000011575 calcium Substances 0.000 description 2
- 230000006866 deterioration Effects 0.000 description 2
- 238000011156 evaluation Methods 0.000 description 2
- 238000011049 filling Methods 0.000 description 2
- 239000010408 film Substances 0.000 description 2
- 239000011521 glass Substances 0.000 description 2
- 239000010931 gold Substances 0.000 description 2
- -1 hydroxide ions Chemical class 0.000 description 2
- 230000006698 induction Effects 0.000 description 2
- 239000011261 inert gas Substances 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 239000012212 insulator Substances 0.000 description 2
- 239000011572 manganese Substances 0.000 description 2
- 229910044991 metal oxide Inorganic materials 0.000 description 2
- 150000004706 metal oxides Chemical class 0.000 description 2
- QJGQUHMNIGDVPM-UHFFFAOYSA-N nitrogen group Chemical group [N] QJGQUHMNIGDVPM-UHFFFAOYSA-N 0.000 description 2
- 230000000737 periodic effect Effects 0.000 description 2
- 239000002244 precipitate Substances 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 238000010791 quenching Methods 0.000 description 2
- 239000010948 rhodium Substances 0.000 description 2
- 230000000630 rising effect Effects 0.000 description 2
- 150000003839 salts Chemical class 0.000 description 2
- 238000004781 supercooling Methods 0.000 description 2
- 229910052718 tin Inorganic materials 0.000 description 2
- 238000012546 transfer Methods 0.000 description 2
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 description 2
- 229910017980 Ag—Sn Inorganic materials 0.000 description 1
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910021364 Al-Si alloy Inorganic materials 0.000 description 1
- 229910018140 Al-Sn Inorganic materials 0.000 description 1
- 229910018137 Al-Zn Inorganic materials 0.000 description 1
- 229910018170 Al—Au Inorganic materials 0.000 description 1
- 229910018182 Al—Cu Inorganic materials 0.000 description 1
- 229910018564 Al—Sn Inorganic materials 0.000 description 1
- 229910018573 Al—Zn Inorganic materials 0.000 description 1
- 229910015363 Au—Sn Inorganic materials 0.000 description 1
- 229910004261 CaF 2 Inorganic materials 0.000 description 1
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 1
- 239000004215 Carbon black (E152) Substances 0.000 description 1
- BVKZGUZCCUSVTD-UHFFFAOYSA-L Carbonate Chemical compound [O-]C([O-])=O BVKZGUZCCUSVTD-UHFFFAOYSA-L 0.000 description 1
- 229910052684 Cerium Inorganic materials 0.000 description 1
- 229910020521 Co—Zn Inorganic materials 0.000 description 1
- 229910017518 Cu Zn Inorganic materials 0.000 description 1
- 229910017755 Cu-Sn Inorganic materials 0.000 description 1
- 229910017752 Cu-Zn Inorganic materials 0.000 description 1
- 229910017818 Cu—Mg Inorganic materials 0.000 description 1
- 229910017927 Cu—Sn Inorganic materials 0.000 description 1
- 229910017943 Cu—Zn Inorganic materials 0.000 description 1
- 229910052692 Dysprosium Inorganic materials 0.000 description 1
- 229910052691 Erbium Inorganic materials 0.000 description 1
- 229910052693 Europium Inorganic materials 0.000 description 1
- 229910052688 Gadolinium Inorganic materials 0.000 description 1
- GYHNNYVSQQEPJS-UHFFFAOYSA-N Gallium Chemical compound [Ga] GYHNNYVSQQEPJS-UHFFFAOYSA-N 0.000 description 1
- 229910052689 Holmium Inorganic materials 0.000 description 1
- 229910000846 In alloy Inorganic materials 0.000 description 1
- 229910052765 Lutetium Inorganic materials 0.000 description 1
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 1
- 229910000861 Mg alloy Inorganic materials 0.000 description 1
- 229910018648 Mn—N Inorganic materials 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- 229910018605 Ni—Zn Inorganic materials 0.000 description 1
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 1
- 229910052777 Praseodymium Inorganic materials 0.000 description 1
- 229910052773 Promethium Inorganic materials 0.000 description 1
- KJTLSVCANCCWHF-UHFFFAOYSA-N Ruthenium Chemical compound [Ru] KJTLSVCANCCWHF-UHFFFAOYSA-N 0.000 description 1
- 229910020994 Sn-Zn Inorganic materials 0.000 description 1
- 229910009069 Sn—Zn Inorganic materials 0.000 description 1
- 229910052771 Terbium Inorganic materials 0.000 description 1
- 229910052775 Thulium Inorganic materials 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- 229910009043 WC-Co Inorganic materials 0.000 description 1
- 229910052769 Ytterbium Inorganic materials 0.000 description 1
- 239000002253 acid Substances 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
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- ZMIGMASIKSOYAM-UHFFFAOYSA-N cerium Chemical compound [Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce] ZMIGMASIKSOYAM-UHFFFAOYSA-N 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 1
- TVZPLCNGKSPOJA-UHFFFAOYSA-N copper zinc Chemical compound [Cu].[Zn] TVZPLCNGKSPOJA-UHFFFAOYSA-N 0.000 description 1
- 230000005347 demagnetization Effects 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- KBQHZAAAGSGFKK-UHFFFAOYSA-N dysprosium atom Chemical compound [Dy] KBQHZAAAGSGFKK-UHFFFAOYSA-N 0.000 description 1
- UYAHIZSMUZPPFV-UHFFFAOYSA-N erbium Chemical compound [Er] UYAHIZSMUZPPFV-UHFFFAOYSA-N 0.000 description 1
- OGPBJKLSAFTDLK-UHFFFAOYSA-N europium atom Chemical compound [Eu] OGPBJKLSAFTDLK-UHFFFAOYSA-N 0.000 description 1
- UIWYJDYFSGRHKR-UHFFFAOYSA-N gadolinium atom Chemical compound [Gd] UIWYJDYFSGRHKR-UHFFFAOYSA-N 0.000 description 1
- 229910052733 gallium Inorganic materials 0.000 description 1
- 229910052732 germanium Inorganic materials 0.000 description 1
- GNPVGFCGXDBREM-UHFFFAOYSA-N germanium atom Chemical compound [Ge] GNPVGFCGXDBREM-UHFFFAOYSA-N 0.000 description 1
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 1
- 229910052737 gold Inorganic materials 0.000 description 1
- 229910052735 hafnium Inorganic materials 0.000 description 1
- VBJZVLUMGGDVMO-UHFFFAOYSA-N hafnium atom Chemical compound [Hf] VBJZVLUMGGDVMO-UHFFFAOYSA-N 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- KJZYNXUDTRRSPN-UHFFFAOYSA-N holmium atom Chemical compound [Ho] KJZYNXUDTRRSPN-UHFFFAOYSA-N 0.000 description 1
- 229930195733 hydrocarbon Natural products 0.000 description 1
- 150000002430 hydrocarbons Chemical class 0.000 description 1
- 229910052738 indium Inorganic materials 0.000 description 1
- 229910052741 iridium Inorganic materials 0.000 description 1
- GKOZUEZYRPOHIO-UHFFFAOYSA-N iridium atom Chemical compound [Ir] GKOZUEZYRPOHIO-UHFFFAOYSA-N 0.000 description 1
- BWHLPLXXIDYSNW-UHFFFAOYSA-N ketorolac tromethamine Chemical compound OCC(N)(CO)CO.OC(=O)C1CCN2C1=CC=C2C(=O)C1=CC=CC=C1 BWHLPLXXIDYSNW-UHFFFAOYSA-N 0.000 description 1
- 229910052746 lanthanum Inorganic materials 0.000 description 1
- FZLIPJUXYLNCLC-UHFFFAOYSA-N lanthanum atom Chemical compound [La] FZLIPJUXYLNCLC-UHFFFAOYSA-N 0.000 description 1
- OHSVLFRHMCKCQY-UHFFFAOYSA-N lutetium atom Chemical compound [Lu] OHSVLFRHMCKCQY-UHFFFAOYSA-N 0.000 description 1
- 239000006249 magnetic particle Substances 0.000 description 1
- 230000005389 magnetism Effects 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 239000004570 mortar (masonry) Substances 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 239000012299 nitrogen atmosphere Substances 0.000 description 1
- 229910052762 osmium Inorganic materials 0.000 description 1
- SYQBFIAQOQZEGI-UHFFFAOYSA-N osmium atom Chemical compound [Os] SYQBFIAQOQZEGI-UHFFFAOYSA-N 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 229910052763 palladium Inorganic materials 0.000 description 1
- 229910052698 phosphorus Inorganic materials 0.000 description 1
- 239000011574 phosphorus Substances 0.000 description 1
- 229910052697 platinum Inorganic materials 0.000 description 1
- PUDIUYLPXJFUGB-UHFFFAOYSA-N praseodymium atom Chemical compound [Pr] PUDIUYLPXJFUGB-UHFFFAOYSA-N 0.000 description 1
- 238000002203 pretreatment Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- VQMWBBYLQSCNPO-UHFFFAOYSA-N promethium atom Chemical compound [Pm] VQMWBBYLQSCNPO-UHFFFAOYSA-N 0.000 description 1
- 238000010298 pulverizing process Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 229910052703 rhodium Inorganic materials 0.000 description 1
- MHOVAHRLVXNVSD-UHFFFAOYSA-N rhodium atom Chemical compound [Rh] MHOVAHRLVXNVSD-UHFFFAOYSA-N 0.000 description 1
- 229910052707 ruthenium Inorganic materials 0.000 description 1
- KZUNJOHGWZRPMI-UHFFFAOYSA-N samarium atom Chemical compound [Sm] KZUNJOHGWZRPMI-UHFFFAOYSA-N 0.000 description 1
- 229910001954 samarium oxide Inorganic materials 0.000 description 1
- 229940075630 samarium oxide Drugs 0.000 description 1
- FKTOIHSPIPYAPE-UHFFFAOYSA-N samarium(iii) oxide Chemical compound [O-2].[O-2].[O-2].[Sm+3].[Sm+3] FKTOIHSPIPYAPE-UHFFFAOYSA-N 0.000 description 1
- 229910052706 scandium Inorganic materials 0.000 description 1
- SIXSYDAISGFNSX-UHFFFAOYSA-N scandium atom Chemical compound [Sc] SIXSYDAISGFNSX-UHFFFAOYSA-N 0.000 description 1
- 229910052709 silver Inorganic materials 0.000 description 1
- 239000004332 silver Substances 0.000 description 1
- BSWGGJHLVUUXTL-UHFFFAOYSA-N silver zinc Chemical compound [Zn].[Ag] BSWGGJHLVUUXTL-UHFFFAOYSA-N 0.000 description 1
- 229910052708 sodium Inorganic materials 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 1
- 229910052714 tellurium Inorganic materials 0.000 description 1
- GZCRRIHWUXGPOV-UHFFFAOYSA-N terbium atom Chemical compound [Tb] GZCRRIHWUXGPOV-UHFFFAOYSA-N 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- GPPXJZIENCGNKB-UHFFFAOYSA-N vanadium Chemical compound [V]#[V] GPPXJZIENCGNKB-UHFFFAOYSA-N 0.000 description 1
- NAWDYIZEMPQZHO-UHFFFAOYSA-N ytterbium Chemical compound [Yb] NAWDYIZEMPQZHO-UHFFFAOYSA-N 0.000 description 1
- 229910052727 yttrium Inorganic materials 0.000 description 1
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C45/00—Amorphous alloys
- C22C45/02—Amorphous alloys with iron as the major constituent
-
- 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
- B22F3/02—Compacting only
- B22F3/087—Compacting only using high energy impulses, e.g. magnetic field impulses
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/10—Sintering only
- B22F3/105—Sintering only by using electric current other than for infrared radiant energy, laser radiation or plasma ; by ultrasonic bonding
-
- 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
-
- 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
- C22C1/11—Making amorphous alloys
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C28/00—Alloys based on a metal not provided for in groups C22C5/00 - C22C27/00
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C33/00—Making ferrous alloys
- C22C33/003—Making ferrous alloys making amorphous alloys
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C33/00—Making ferrous alloys
- C22C33/02—Making ferrous alloys by powder metallurgy
- C22C33/0257—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements
- C22C33/0278—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5%
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
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- C—CHEMISTRY; METALLURGY
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- H01F41/0273—Imparting anisotropy
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- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/10—Sintering only
- B22F3/105—Sintering only by using electric current other than for infrared radiant energy, laser radiation or plasma ; by ultrasonic bonding
- B22F2003/1051—Sintering only by using electric current other than for infrared radiant energy, laser radiation or plasma ; by ultrasonic bonding by electric discharge
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Definitions
- the present invention relates to a magnetic material and a manufacturing method thereof.
- Nd—Fe—B sintered magnet a sintered magnet having an Nd—Fe—B composition
- a magnet having high magnetic properties is known as a magnet having high magnetic properties.
- Such a magnet can be manufactured, for example, by magnetically pressing and orienting magnet powder to improve magnetic properties and then sintering.
- an anisotropic magnet powder having a composition of Nd 12.5 Fe bal Co 17.5 B 6.6 Ga 0.2 Zr 0.1 Si 0.1 is kneaded with paraffinic hydrocarbon. Further, the magnet powder and CaF 2 (insulator with high electrical resistance) are mixed and molded in a magnetic field, and then the resulting molded body is debindered to produce graphite for discharge plasma sintering.
- a method of manufacturing a high electric resistance rare earth permanent magnet by inserting into a mold and performing discharge plasma sintering see, for example, Patent Document 1 (Example 1) below).
- Nd—Fe—B sintered magnets are generally known to contain a rare earth such as Dy, which is a rare resource, in order to improve heat resistance. From the viewpoint of depletion, there is a need for an alternative magnet for the Nd—Fe—B sintered magnet that does not require a heavy rare earth such as Dy.
- a nitrogen-based magnet for example, a magnet having an Sm—Fe—N-based composition
- Nitrogen-based magnets have high potential and excellent magnetic properties, but are thermally unstable. Therefore, when sintered, the magnetic properties may deteriorate due to decomposition of the components of the nitrogen-based magnet.
- the manufacturing method of such a high electric resistance rare earth permanent magnet is complicated in operation, and further, the molded body may be damaged during the transfer.
- a magnetic press machine is equipped with a sintering machine, and a method of magnetic pressing and sintering with the same mold in the magnetic press machine is also considered.
- the magnet is affected by the influence of heat. Cannot be properly oriented, and further, there is a problem that the apparatus becomes larger.
- the resin bond magnet of the said patent document 2 contains an epoxy resin, although a molded object itself can be formed densely, the density of a magnet component cannot be improved and, therefore, sufficient magnetic properties can be obtained. There is a bug that cannot be done.
- An object of the present invention is to provide a magnetic material that can be easily manufactured and has excellent magnetic properties, and a method of manufacturing a magnetic material that can reliably manufacture magnetic materials having excellent magnetic properties by simple operations. There is to do.
- the magnetic material of the present invention is a magnetic material made from magnet powder and amorphous metal, and the amorphous metal contains rare earth elements, iron and boron,
- the atomic ratio of the rare earth element is in the range of 22 to 44 atomic%
- the atomic ratio of the boron is in the range of 6 to 28 atomic%
- the magnet powder and the amorphous metal are mixed, and It is characterized by being obtained by heating to a temperature that is 30 ° C. lower than the crystallization temperature (Tx) of the amorphous metal or, if the amorphous metal is a metallic glass, to a temperature that is higher than the glass transition temperature (Tg). Yes.
- the amorphous metal further contains cobalt, and in the amorphous metal, the atomic ratio of cobalt to iron is 1.5 or less.
- the magnetic material of the present invention further contains an additive, and the content ratio of the additive is preferably less than 10 parts by mass with respect to 100 parts by mass of the magnetic material.
- a magnetic anisotropic magnet powder is used as the magnet powder, and a mixture with the amorphous metal is subjected to a magnetic field press treatment.
- the method for producing a magnetic material according to the present invention includes a step of mixing a magnetic powder and an amorphous metal having a softening start temperature of 600 ° C. or lower to obtain a mixed powder, filling the mixed powder into a mold, and in a magnetic field.
- the magnetic material of the present invention high magnetic properties can be ensured by simple manufacturing.
- the softening start temperature of the amorphous metal is 600 ° C. or lower, the sintering temperature in the discharge plasma sintering can be lowered. Therefore, after the magnetic powder and the amorphous metal are pressure-molded in a magnetic field in a mold, discharge plasma sintering can be performed in the same mold without transferring the molded body to a highly heat-resistant mold.
- a magnetic material having excellent magnetic properties can be reliably produced by a simple operation.
- the magnetic material of the present invention is made from magnet powder and amorphous metal.
- the magnet powder include nitrogen-based magnet powder (hereinafter referred to as nitrogen-based magnet), nitrogen-based nanocomposite magnet powder (hereinafter referred to as nitrogen-based nanocomposite magnet), and the like.
- the nitrogen-based magnet is not particularly limited, and examples thereof include rare earth-transition metal-nitrogen magnets and transition metal-nitrogen magnets.
- rare earth-transition metal-nitrogen based magnets examples include Sm—Fe—N based magnets and Sm—Fe—Mn—N based magnets, preferably Sm—Fe—N based magnets.
- the Sm—Fe—N-based magnet is a powder of a magnet having an Sm—Fe—N-based composition (hereinafter sometimes referred to as “SmFeN”).
- SmFeN obtained by a known method is pulverized. Can be manufactured.
- an SmFe alloy powder is produced from a samarium oxide and iron powder by a reduction diffusion method, and then the obtained SmFe alloy powder is obtained by, for example, N 2 gas or NH 3 gas. in an atmosphere such as N 2 and H 2 gas mixture, for example, by heating at 600 ° C. below the temperature to produce the SmFeN.
- the obtained SmFeN is finely pulverized by a known pulverizer such as a jet mill or a ball mill. Thereby, an Sm—Fe—N-based magnet can be obtained.
- the Sm—Fe—N magnet can be manufactured without pulverizing SmFeN.
- Sm and Fe are dissolved in an acid to obtain Sm ions and Fe ions, and then the solution is reacted with, for example, Sm ions and Fe ions to form an insoluble salt.
- Ions for example, hydroxide ions, carbonate ions, etc.
- the Sm—Fe—N magnet is not limited to the above method, and can be manufactured by other known methods.
- Sm—Fe—N magnets More specific examples include Sm 2 Fe 17 N 3 (Curie point: 474 ° C.).
- transition metal-nitrogen based magnet examples include an Fe—N based magnet and the like, and an Fe 16 N 2 based magnet is preferable.
- nitrogen-based magnets can be used alone or in combination of two or more.
- the decomposition temperature of the nitrogen-based magnet is, for example, 600 ° C. or higher. Furthermore, such a nitride magnet is gradually decomposed from, for example, 500 ° C. by heating to generate SmN, Fe, and the like.
- the volume average particle diameter of the nitrogen-based magnet (powder) is, for example, 1 to 20 ⁇ m, preferably 2 to 4 ⁇ m.
- the coercive force is good.
- a nitrogen-based magnet a commercially available one can be used.
- Z16 Sm—Fe—N-based magnet (Sm 2 Fe 17 N 3 ), decomposition temperature 600 ° C. , volume average particle diameter of 3 [mu] m, can be used Nichia Corporation) and the like.
- the nitrogen-based nanocomposite magnet is not particularly limited, and examples thereof include an Sm—Fe—N-based nanocomposite magnet.
- the Sm—Fe—N-based nanocomposite magnet is, for example, a powder of a nanocomposite magnet having a Fe / Sm—Fe—N-based structure, and is not particularly limited. And can be produced by applying pressure.
- an Sm—Fe—N magnet obtained by a known method is pressurized at a predetermined pressure and pulsed for a predetermined time.
- the Sm—Fe—N magnet can be partially decomposed, and the Fe crystal phase as the soft magnetic phase can be formed in the Sm—Fe—N single crystal phase as the high magnetic phase.
- an Sm—Fe—N-based nanocomposite magnet can be manufactured.
- the Sm—Fe—N-based nanocomposite magnet can be further pulverized and used as necessary.
- the Sm—Fe—N-based nanocomposite magnet is not limited to the above method, and can be manufactured by other known methods.
- Sm—Fe—N-based nanocomposite magnets include nanocomposite magnets of Fe and Sm 2 Fe 17 N 3 (Curie point: 474 ° C.).
- These nitrogen-based nanocomposite magnets can be used alone or in combination of two or more.
- the temperature at which the crystal of the nitrogen-based nanocomposite magnet becomes coarse is, for example, 600 ° C. or higher.
- the volume average particle diameter of the nitrogen-based nanocomposite magnet (powder) is, for example, 30 to 300 ⁇ m, preferably 50 to 150 ⁇ m.
- the volume average particle diameter of the nitrogen-based nanocomposite magnet (powder) is in the above range, the magnetic particle filling rate is improved and the residual magnetic flux density is improved.
- magnet powders are classified into magnetic isotropic magnet powders and magnetic anisotropic magnet powders.
- Magnetic isotropic magnet powder is defined as one in which individual alloy powders are composed of a large number of fine crystal grains, and the direction of easy axis of magnetization of each crystal grain is disordered.
- the magnetic anisotropic magnet powder is composed of a single crystal of each alloy powder or a large number of fine crystal grains, and the magnetization easy axis direction of each crystal grain is Defined as being aligned in a specific direction.
- These magnetic isotropic magnet powder and magnetic anisotropic magnet powder can be produced by a known method.
- magnet powders can be used alone or in combination of two or more.
- a magnetic isotropic magnet powder it can ensure the outstanding magnetic characteristic, without performing the magnetic field press process mentioned later, and uses a magnetic anisotropic magnet powder. In the case, from the viewpoint of improving the magnetic properties of the obtained magnetic material, preferably, magnetic field pressing is performed as described later.
- the amorphous metal is an amorphous alloy that starts deformation (softens) at a temperature lower than the crystallization temperature (Tx) and has excellent magnetic properties.
- Tx crystallization temperature
- Such an amorphous metal starts to deform (soften) by heating, and then crystallizes.
- the amorphous metal contains rare earth elements, Fe (iron) and B (boron).
- a rare earth element is contained in order to cause magnetocrystalline anisotropy and improve its magnetic properties (for example, coercive force) during firing.
- rare earth elements include Sc (scandium), Y (yttrium), La (lanthanum), Ce (cerium), Pr (praseodymium), Nd (neodymium), Pm (promethium), Sm (samarium), Eu (europium).
- Light rare earth elements such as Gd (gadolinium), Tb (terbium), Dy (dysprosium), Ho (holmium), Er (erbium), Tm (thulium), Yb (ytterbium), Lu (lutetium), etc. Heavy rare earth elements.
- These rare earth elements can be used alone or in combination of two or more.
- Such an amorphous metal can exhibit a sufficiently large coercive force without necessarily including a heavy rare earth element.
- the rare earth element is preferably a light rare earth element, more preferably Nd (neodymium).
- Nd neodymium
- the atomic ratio of rare earth elements (the total amount when they are used together) is 22 to 44 atomic%, preferably 23 to 40 atomic%, more preferably 24 to 37 atomic%. It is a range.
- the crystallization temperature (Tx) of the amorphous metal may be increased, so that a magnetic material is manufactured by heat-treating the magnet powder and the amorphous metal as described later. In this case, there is a problem that the energy cost of the heat treatment is increased and the workability and productivity are lowered.
- the atomic ratio of the rare earth element is in the above range, the remanent magnetization and coercive force of the magnetic material obtained using the amorphous metal can be improved, and further, the crystallization temperature (Tx) of the amorphous metal. Therefore, as will be described later, a magnetic material can be manufactured at low cost and with good workability and productivity without heat treatment at a high temperature.
- Fe is an element that contributes to magnetism, and is contained to improve the magnetic properties (for example, residual magnetic flux density) of the magnetic material.
- the atomic ratio of Fe (iron) is, for example, in the range of 15 to 65 atomic%, preferably 20 to 60 atomic%, and more preferably 25 to 55 atomic%.
- the atomic ratio of Fe (iron) is less than the above lower limit, the residual magnetic flux density of the magnetic material after heat treatment (crystallization) described later may decrease.
- the atomic ratio of Fe (iron) exceeds the above upper limit, the coercivity of the magnetic material after heat treatment (crystallization) described later may be reduced.
- B boron
- the atomic ratio of B (boron) is in the range of 6 to 28 atomic%, preferably 12 to 28 atomic%, more preferably 15 to 25 atomic%.
- a crystal phase may be generated during quenching, which will be described later.
- a discharge plasma sintering method, a hot press method, or the like is used. In the case of manufacturing a molded body, moldability and workability may be reduced.
- the atomic ratio of B (boron) exceeds the above upper limit, the residual magnetic flux density of the magnetic material after heat treatment (crystallization) described later may be lowered.
- the amorphous metal preferably contains Co (cobalt).
- Co cobalt
- the amorphous metal In the amorphous metal, Co (cobalt) is contained in order to improve the magnetic properties of the magnetic material obtained by using the amorphous metal and to improve the handleability by preventing oxidation.
- the amorphous metal is a metallic glass as described later
- Co cobalt
- the metallic glass in a softened state (glass transition state) described later, and improves its moldability. Contained.
- the atomic ratio of Co (cobalt) is, for example, in the range of 1 to 50 atomic%, preferably 2 to 45 atomic%, more preferably 4 to 40 atomic%.
- the residual magnetic flux density of the magnetic material obtained using amorphous metal may be lowered.
- the atomic ratio of Co (cobalt) is preferably 1.5 or less, preferably 1.44 or less, more preferably 0.6 or less. Can be mentioned.
- the handleability can be improved. On the other hand, if it exceeds 1.5, there is a problem that the cost is inferior.
- the amorphous metal further contains other elements such as Ti (titanium), Zr (zirconium), Hf (hafnium), V (vanadium), Nb (niobium), Ta (tantalum), Cr (additional elements).
- additive elements can be used alone or in combination of two or more.
- Preferred additive elements include Ti (titanium), Zr (zirconium), Nb (niobium), Cr (chromium), Ni (nickel), Cu (copper), Si (silicon), and Al (aluminum).
- the additive element is selected from the group consisting of Ti (titanium), Zr (zirconium), Nb (niobium), Cr (chromium), Ni (nickel), Cu (copper), Si (silicon), and Al (aluminum). If at least one kind is contained, the residual magnetic flux density and coercive force of the magnetic material can be improved.
- the atomic ratio of the additive element is, for example, 1 to 15 atomic%, preferably 1 to 10 atomic%. More preferably, it is 1 to 5 atomic%.
- Al aluminum
- Al aluminum
- the amorphous metal contains Al (aluminum) as an additive element, the crystallization temperature (Tx) of the amorphous metal, which will be described later, can be suppressed to a low level.
- a magnetic material can be manufactured at low cost and with good workability and productivity.
- the softening start temperature (deformation start temperature, glass transition temperature (Tg)) of the metal glass can be kept low, so that the formability can be further improved. it can.
- the atomic ratio of Al (aluminum) is, for example, less than 15 atomic%, preferably less than 5 atomic%, more preferably 3.5 atomic% or less, More preferably, it is 3 atomic% or less.
- the crystallization temperature (Tx) of the amorphous metal increases, which increases the cost of manufacturing the magnetic material, and decreases workability and productivity. There is a case to let you.
- the total amount of atomic ratios of rare earth elements and Fe (iron) (and Co (cobalt) contained if necessary) is, for example, 65 to 94 atomic%, preferably 70 to 90 atoms. %, More preferably 72 to 85 atomic%.
- the formability and workability of the amorphous metal can be improved.
- the residual magnetic flux density and coercive force of the magnetic material after the heat treatment (crystallization) can be improved.
- an element excluding rare earth elements and Fe (iron) (and Co (cobalt) contained if necessary) (including B (boron) as an essential component) and an additive element (for example, Ti (titanium) as an optional component) ), Zr (zirconium), Nb (niobium), Cr (chromium), Ni (nickel), Cu (copper), Si (silicon), Al (aluminum), and the like. It is in the range of 6 atomic% or more, preferably 10 to 30 atomic%, more preferably 15 to 28 atomic%, and particularly preferably 15 to 25 atomic%.
- the formability and workability of the amorphous metal can be improved, and further, heat treatment (crystal The residual magnetic flux density and coercive force of the magnetic material after the formation can be improved.
- An example of such an amorphous metal is an amorphous metal represented by the following formula (1).
- R 83-x Fex / 2 Co x / 2 Al 17-y B y (1) (Wherein, R represents a rare earth element. In addition, a 0 ⁇ x ⁇ 83, also a 0 ⁇ y ⁇ 17.) In the above formula (1), R represents the rare earth element described above (the same applies hereinafter).
- the range of x is 0 ⁇ x ⁇ 83, preferably 28 ⁇ x ⁇ 58, and more preferably 33 ⁇ x ⁇ 53.
- the value of x is in the above range, the formability and workability of the amorphous metal can be improved, and further, the residual magnetic flux density and coercive force of the magnetic material after heat treatment (crystallization) described later are improved. be able to.
- the range of y is 0 ⁇ y ⁇ 17, preferably 12 ⁇ y ⁇ 17, and more preferably 13.5 ⁇ y ⁇ 17.
- the formability and workability of the amorphous metal can be improved, and further, the residual magnetic flux density and coercive force of the magnetic material after heat treatment (crystallization) to be described later are improved. be able to.
- Such an amorphous metal is not particularly limited, and can be produced by a known method.
- first, simple powders, lumps, etc. of the above-mentioned respective elements (which may be partially alloyed if necessary) are prepared as raw material components, and these are set to the above atomic ratio. Mix like so.
- the obtained mixture of raw material components is dissolved in, for example, an inert gas (eg, nitrogen gas, argon gas) atmosphere.
- an inert gas eg, nitrogen gas, argon gas
- the method for dissolving the raw material components is not particularly limited as long as it is a method capable of dissolving each of the above elements, and examples thereof include arc melting.
- the obtained bulk alloy is pulverized by a known method to obtain alloy particles (particle size: 0.5 to 20 mm).
- the obtained alloy particles are melted to obtain a molten alloy.
- the method for melting the alloy granular material is not particularly limited as long as it is a method capable of melting the alloy granular material, and examples thereof include high-frequency induction heating.
- the obtained molten alloy is rapidly cooled by a known method such as a single roll method or a gas atomizing method to obtain an amorphous metal.
- the molten alloy is flowed down on the outer peripheral surface of the rotating cooling roll, and the molten alloy and the cooling roll are brought into contact with each other for a predetermined time to rapidly cool the molten alloy.
- Quench rate of the molten alloy (cooling rate) is, for example, 10 -2 ⁇ 10 3 °C / s .
- the rapid cooling rate (cooling rate) of the molten alloy is controlled, for example, by adjusting the rotational speed of the cooling roll.
- the rotation speed of the cooling roll is, for example, 1 to 60 m / s, preferably 20 to 50 m / s, and more preferably 30 to 40 m / s.
- a strip-shaped (including a thin film and a thick film) amorphous metal can be obtained on the outer peripheral surface of the cooling roll.
- the thickness of the obtained amorphous metal is, for example, 1 to 500 ⁇ m, preferably 5 to 300 ⁇ m, more preferably 10 to 100 ⁇ m.
- a high-pressure injection gas for example, helium gas, argon gas, nitrogen gas, etc.
- a high-pressure injection gas for example, helium gas, argon gas, nitrogen gas, etc.
- powdered amorphous metal can be obtained by rapidly cooling the molten alloy.
- the volume average particle diameter of the obtained amorphous metal is, for example, 1 to 200 ⁇ m, preferably 5 to 50 ⁇ m.
- the method for rapidly cooling the molten alloy is not limited to the single roll method and the gas atomizing method, and a known method can be employed. Preferably, a single roll method is employed.
- the crystallization temperature (Tx) of the amorphous metal (temperature at which crystallization starts) is, for example, 600 ° C. or less, preferably 550 ° C. or less, more preferably 500 ° C. or less.
- the crystallization temperature (Tx) of the amorphous metal can be measured by DSC (Differential Scanning Calorimetry), and is defined as a value measured at a heating rate of 40 ° C./min in the present invention.
- the lowest crystallization temperature (Tx) among the crystallization temperatures (Tx) is set as the crystallization temperature (Tx) of the amorphous metal.
- the amorphous metal obtained in this way contains metallic glass.
- Metallic glass is an amorphous alloy having a glass transition temperature (Tg) lower than the crystallization temperature (Tx), and has high formability.
- the softening start temperature (deformation start temperature, glass transition temperature (Tg)) is, for example, 600 ° C. or less, preferably 500 ° C. or less. More preferably, it is 450 ° C. or lower.
- the amorphous metal is not metallic glass, it may be softened by heating.
- the softening start temperature is, for example, 600 ° C. or lower, preferably 500 ° C. or lower, more preferably 450 ° C. or lower. It is.
- the softening start temperature of amorphous metal can be obtained by, for example, DSC (differential scanning calorimetry) or press displacement measurement of a discharge plasma sintering machine.
- amorphous metals can be used alone or in combination of two or more.
- the magnetic material of the present invention can further contain an additive.
- transition elements and typical elements having a melting point of 600 ° C. or lower and compounds adjusted to have a melting point of 600 ° C. or lower.
- transition elements and typical elements such as Zn, Sn, Bi, Cd, In, Li, P, Na, S, Te, for example, Ag—Al alloy, Ag—Sn alloy, Ag—Zn alloy Al-Au alloy, Al-Cu alloy, Al-Si alloy, Al-Sn alloy, Al-Zn alloy, Au-Mg alloy, Au-Sn alloy, Cu-In alloy, Cu-Mg alloy, Cu-Sn alloy , Cu—Zn alloys, Cu—Rare earth alloys, Co—Zn alloys, Fe—Zn alloys, Mg—Zn alloys, Ni—Zn alloys, Sn—Zn alloys and the like, and multi-component compounds having a melting point of 600 ° C. or less Is mentioned.
- additives can be used alone or in combination of two or more.
- Zn (zinc) is preferable.
- the volume average particle diameter of the additive is, for example, 5 nm to 100 ⁇ m, preferably 20 nm to 10 ⁇ m.
- the content of the additive is, for example, less than 10 parts by mass, preferably 5 parts by mass or less with respect to 100 parts by mass of the magnetic material.
- magnet powder and amorphous metal are mixed.
- the blending ratio of the magnet powder and the amorphous metal is, for example, 60 to 99 parts by weight, preferably 80 to 95 parts by weight of the magnet powder with respect to 100 parts by weight of the total amount of the magnet powder and the amorphous metal.
- the metal is, for example, 1 to 40 parts by mass, preferably 5 to 20 parts by mass.
- the blending ratio is adjusted so that the content of the additive in the magnetic material is within the above range.
- the mixing is not particularly limited as long as the magnetic powder and the amorphous metal (with additives added as necessary) can be sufficiently mixed.
- a known mixing device such as a ball mill can be used.
- either a dry method or a wet method can be employed.
- magnet powder and amorphous metal are mixed in an inert gas (for example, nitrogen gas, argon gas, etc.) atmosphere.
- an inert gas for example, nitrogen gas, argon gas, etc.
- the magnet powder and the amorphous metal are mixed in a solvent (for example, cyclohexane, acetone, ethanol, etc.).
- the mixing conditions are not particularly limited, but when a ball mill (capacity 0.3 L) is used, the rotation speed is, for example, 100 to 300 rpm, preferably 150 to 250 rpm, and the mixing time is, for example, 5 to 60 minutes, preferably 5 to 45 minutes.
- the mixture of the magnet powder and the amorphous metal (and the additive compounded as necessary) is heated to a temperature 30 ° C. lower than the crystallization temperature (Tx) of the amorphous metal while being pressurized, for example. .
- the mixture of the magnet powder and the amorphous metal is heated to a temperature equal to or higher than the glass transition temperature (Tg) while being pressurized, for example.
- a mixture of magnet powder and amorphous metal (added if necessary) is added, for example, 20 to Under a pressure condition of 1500 MPa, preferably 200 to 1000 MPa, a temperature that is 30 ° C. lower than the crystallization temperature (Tx) of the amorphous metal, or a glass transition temperature (Tg) if the amorphous metal is a metallic glass
- the amorphous metal is heated to a temperature equal to or higher than the crystallization temperature (Tx) of the amorphous metal, specifically 400 to 600 ° C., preferably 410 to 550 ° C., for example.
- ⁇ / RTI> By such pressure heating molding, the amorphous metal is deformed, whereby a high-density magnetic material can be obtained. Furthermore, since an amorphous metal becomes a hard magnetic phase, a magnetic material containing a magnet powder and a hard magnetic phase generated from the amorphous metal can be obtained.
- the heating is not particularly limited, but for example, heating can be performed from room temperature at a constant temperature increase rate.
- the temperature increase rate is, for example, 10 to 200 ° C./min, preferably 20 to 100 ° C./min.
- a molded body of magnet powder and an amorphous metal or a hard magnetic phase generated from an amorphous metal may be heated at a high temperature using the image furnace or the like. It can also be held for a predetermined time under the conditions.
- the above heat treatment for example, it is held at 400 to 600 ° C., preferably 410 to 550 ° C., for example, for 1 to 120 minutes, preferably 10 to 60 minutes.
- the above-described pressure heating molding and the subsequent heat treatment can be performed in a magnetic field.
- a mixture of magnet powder and amorphous metal can be pressurized (magnetic field press treatment) in a magnetic field.
- a magnetic anisotropic magnet powder is used as the magnet powder
- a mixture of the magnet powder and the amorphous metal is subjected to magnetic field press treatment.
- the magnetic powder When pressed in a magnetic field, the magnetic powder can be oriented in a predetermined direction, so that the magnetic properties of the obtained magnetic material can be further improved.
- the applied magnetic field is 10 kOe or more, preferably 20 kOe or more, and the pressure condition is, for example, 30 to 2000 MPa, preferably 100 to 1000 MPa.
- the magnetic material thus obtained, material deterioration caused by firing the magnet powder, more specifically, generation of SmN, Fe, etc. due to decomposition of the nitrogen-based magnet, and generation of the nitrogen-based nanocomposite magnet Crystal coarsening is suppressed, and gaps (voids) in the magnet powder are filled with amorphous metal having excellent magnetic properties.
- this magnetic material can improve its magnetic characteristics as compared with a resin bonded magnet containing a resin (for example, epoxy resin).
- the atomic ratio of the rare earth element in the amorphous metal is in the range of 22 to 44 atomic% and the atomic ratio of boron is in the range of 6 to 28 atomic%.
- the magnetic material can be manufactured at low cost and with good workability and productivity.
- an amorphous metal other than the above composition for example, Nd 60 Fe 30 Al 10 or the like
- an amorphous metal has insufficient magnetic properties and is thus obtained.
- the magnetic properties of the magnetic material may be inferior.
- the magnetic material of the present invention is obtained by mixing the amorphous metal and the magnet powder and heating to a temperature equal to or higher than the softening start temperature of the amorphous metal, the magnetic material can have excellent magnetic properties. .
- the magnetic material may be, for example, an amorphous metal having a softening start temperature of 600 ° C. or less, and after the pressure-molding of the mixed powder of the magnet powder and the amorphous metal in a magnetic field, the discharge plasma sintering is performed. By doing so, it can also be manufactured.
- a mixed powder of magnet powder and amorphous metal is filled in a mold and pressure-molded (magnetic field press treatment) in a magnetic field to obtain a compact.
- molds examples include cemented carbide molds.
- the cemented carbide is based on a periodic table (in accordance with IUPAC Periodic Table of the Elements (version date 22 June 2007)) carbides of group 4 to 6 metal atoms (for example, WC (tungsten carbide)), for example, Fe It is a composite material sintered with an iron-based metal such as (iron), Co (cobalt), or Ni (nickel).
- the cemented carbide is preferably a Ni-bonded alloy from the viewpoint of the orientation of the magnet powder in the magnetic field press.
- Ni-bonded alloy examples include a WC—Ni (tungsten carbide-nickel) based alloy and a WC—Ni—Cr (tungsten carbide-nickel-chromium) based alloy.
- cemented carbide other cemented carbide, more specifically, an iron-bonded alloy such as a WC—Fe (tungsten carbide-iron) based alloy, for example, WC—Co (tungsten carbide).
- Bite-cobalt) alloy WC-TiC-Co (tungsten carbide-titanium carbide-cobalt) alloy
- WC-TaC-Co tungsten carbide-tantalum carbide-cobalt
- WC-TiC-TaC Examples include Co-bonded alloys such as -Co (tungsten carbide-titanium carbide-tantalum carbide-cobalt) alloys.
- the applied magnetic field is 10 kOe or more, preferably 20 kOe or more, and the pressure condition is, for example, 30 to 2000 MPa, preferably 100 to 1000 MPa.
- the magnetic powder When the mixed powder is pressed in a magnetic field, the magnetic powder can be oriented in a predetermined direction, so that the magnetic properties of the obtained magnetic material can be further improved.
- the obtained molded body is subjected to discharge plasma sintering in the above-described mold, that is, the same mold used in the magnetic field press treatment.
- a molded body made of a mixture of magnet powder and amorphous metal is, for example, 20 to 1500 MPa, preferably 200 to 1000 MPa, under a pressure condition of 200 to 1000 MPa. Heating (heat treatment) to 200 ° C., preferably 10 to 150 ° C., specifically 400 to 600 ° C., preferably 410 to 500 ° C., for example.
- the heating is not particularly limited, but for example, heating can be performed from room temperature at a constant temperature increase rate.
- the temperature increase rate is, for example, 10 to 200 ° C./min, preferably 20 to 100 ° C./min.
- the mixture of the magnet powder and the amorphous metal can be maintained for a predetermined time under high temperature conditions, continuing from the above heat treatment.
- the above heat treatment for example, it is held at 400 to 600 ° C., preferably 410 to 500 ° C., for example, for 1 to 120 minutes, preferably 10 to 60 minutes.
- the molding pressure condition is, for example, 30 to 2000 MPa, preferably 100 to 1000 MPa, More preferably, it is 200 to 800 MPa.
- the above pressure molding can be performed in a magnetic field.
- the magnetic material thus obtained, material deterioration caused by firing of the magnet powder, more specifically, generation of SmN, Fe, etc. by decomposition of the nitrogen-based magnet, and coarsening of the crystal of the nanocomposite magnet
- the gap (gap) of the magnet powder is filled with an amorphous metal having excellent magnetic properties.
- the softening start temperature of the amorphous metal is 600 ° C. or lower, the sintering temperature in the discharge plasma sintering can be lowered. Therefore, after the magnetic powder and the amorphous metal are pressure-molded in a magnetic field in a mold, discharge plasma sintering can be performed in the same mold without transferring the molded body to a highly heat-resistant mold.
- alloy particles particle size: 0.5 to 10 mm.
- the obtained alloy granular material was melted by high-frequency induction heating in an Ar atmosphere to obtain a molten alloy, and then the obtained molten alloy was subjected to a peripheral speed of 40 m / m in a single roll apparatus in an Ar atmosphere. It flowed down on the outer peripheral surface of the cooling roll of s and rapidly cooled. Thereby, an amorphous metal was obtained.
- amorphous metal was finely pulverized to a volume average particle size of 1.5 ⁇ m by a planetary ball mill (LP-1 manufactured by Ito Seisakusho).
- Nd 60 Fe 30 Al 10 was produced by a gas atomizing method (injection gas: Ar), and then finely pulverized by a ball mill (LP-1 manufactured by Ito Seisakusho). Accordingly, the volume average particle diameter of 1 [mu] m, to obtain a powder of Nd 60 Fe 30 Al 10.
- DSC Denssion Chemical Vapor Deposition Method
- Tx crystallization temperature
- Example 1 Amorphous metal powder obtained in Production Example 1, Z16 (magnetic anisotropic magnet powder, Sm—Fe—N based magnet (Sm 2 Fe 17 N 3 ), decomposition temperature 600 ° C., volume average particle diameter 3 ⁇ m, (Asia Chemical Co., Ltd.) is blended in such a way that the amorphous metal is 10% by mass with respect to the total amount thereof, and in cyclohexane, an attritor (Primix film mix 40-40 type) is used to obtain a peripheral speed of 40 m / s for 5 minutes.
- Z16 magnetic anisotropic magnet powder, Sm—Fe—N based magnet (Sm 2 Fe 17 N 3 ), decomposition temperature 600 ° C., volume average particle diameter 3 ⁇ m, (Asia Chemical Co., Ltd.
- an attritor Principal film mix 40-40 type
- a discharge plasma sintering machine (SPS-515S manufactured by SPS Shintex Co., Ltd.) was used to pressurize to 800 MPa in vacuum and heated to 440 ° C. at a temperature rising rate of 40 ° C./min (temperature increase) And kept for 30 minutes, and then allowed to cool.
- SPS-515S manufactured by SPS Shintex Co., Ltd.
- Examples 2 to 22 and Comparative Examples 1 to 8 Magnet powder Z16 or SP14 (magnetic isotropic magnet powder, isotropic Sm—Fe—N-based magnet used for the manufacture of bonded magnet SP-14 (manufactured by Daido Electronics)), and the respective production examples.
- a magnetic material was obtained in the same manner as in Example 1 except that the amorphous metal was blended in the ratio shown in Table 2 and the discharge plasma sintering process was performed under the processing conditions shown in Table 2. In addition, except for Example 1 and Comparative Example 8, no magnetic field press treatment was performed.
- Examples 23-27 By mixing the magnetic powder Z16, the amorphous metal obtained in Production Example 1 and the additive Zn (volume average particle diameter 30 nm) in the proportions shown in Table 3, and mixing them in a mortar, the amorphous metal powder A mixed powder of magnet powder and additive was obtained.
- Br represents the residual magnetic flux density
- bHc represents the coercive force (B coercive force)
- iHc represents the coercive force (I coercive force)
- (BH) max represents the maximum energy product.
- the magnetic material of the present invention is suitably used in, for example, a motor incorporated in various equipment such as a drive motor of a hybrid vehicle or an electric vehicle, for example, a compressor of an air conditioner.
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Abstract
Description
(式中、Rは、希土類元素を示す。また、0<x<83であり、また、0<y≦17である。)
上記式(1)において、Rは、上記した希土類元素を示す(以下同様。)。
Nd(ネオジム)、Fe(鉄)、Co(コバルト)、Al(アルミニウム)およびB(ホウ素)の単体粉末または塊状物を、表1に示す組成となる配合割合で処方し、アーク溶解炉により、4kPa(30Torr)のAr(アルゴン)雰囲気下で溶解させ、表1に示す組成比の合金(インゴット)を作製した。
ガスアトマイズ法(噴射ガス:Ar)によりNd60Fe30Al10を製造した後、ボールミル(伊藤製作所製 LP-1)により微粉砕した。これにより、体積平均粒子径1μmの、Nd60Fe30Al10の粉末を得た。
[評価]
DSC(示差走査熱量測定:SII社製、DSC6300)を用いて、各製造例において得られたアモルファス金属の結晶化温度(Tx)、および、アモルファス金属が金属ガラスである場合には、そのガラス遷移温度(Tg)を測定した。
製造例1において得られたアモルファス金属の粉末と、Z16(磁気異方性磁石粉末、Sm-Fe-N系磁石(Sm2Fe17N3)、分解温度600℃、体積平均粒子径3μm、日亜化学工業社製)とを、それらの総量に対してアモルファス金属が10質量%となるように配合し、シクロヘキサン中において、アトライター(プライミクス製フィルミックス40-40型)によって、周速40m/sで5分間混合した。
磁石粉末Z16、または、SP14(磁気等方性磁石粉末、ボンド磁石SP-14(ダイドー電子製)の製造に用いられる等方性Sm-Fe-N系磁石)と、各製造例で得られたアモルファス金属とを、表2に示す割合で配合し、また、表2に示す処理条件で放電プラズマ焼結処理した以外は、実施例1と同様にして、磁性材料を得た。なお、実施例1および比較例8以外では、磁場プレス処理しなかった。
磁石粉末Z16と、製造例1で得られたアモルファス金属と、添加材Zn(体積平均粒子径30nm)とを、表3に示す割合で配合し、乳鉢中において混合することにより、アモルファス金属の粉末と磁石粉末と添加材との混合粉末を得た。
各実施例および比較例により得られた各磁性材料について、VSM(玉川製作所製)にて減磁曲線を測定し、それらの磁気特性を評価した。その結果を表4および5に示す。
Claims (5)
- 磁石粉末とアモルファス金属とを原料とする磁性材料であって、
前記アモルファス金属が、希土類元素、鉄およびホウ素を含有し、
前記アモルファス金属において、
前記希土類元素の原子割合が、22~44原子%の範囲であり、
前記ホウ素の原子割合が、6~28原子%の範囲であり、
前記磁石粉末と前記アモルファス金属とを混合するとともに、
前記アモルファス金属の結晶化温度(Tx)より30℃低い温度以上、または、アモルファス金属が金属ガラスである場合には、そのガラス遷移温度(Tg)以上の温度に加熱することにより得られることを特徴とする、磁性材料。 - 前記アモルファス金属が、さらに、コバルトを含有し、
前記アモルファス金属において、鉄に対するコバルトの原子比が、1.5以下である
ことを特徴とする、請求項1に記載の磁性材料。 - さらに、添加材を含有し、
前記添加材の含有割合が、磁性材料100質量部に対して、10質量部未満であることを特徴とする、請求項1に記載の磁性材料。 - 前記磁石粉末として、磁気異方性磁石粉末が用いられ、前記アモルファス金属との混合物が磁場プレス処理されていることを特徴とする、請求項1に記載の磁性材料。
- 磁石粉末と、軟化開始温度が600℃以下のアモルファス金属とを混合し、混合粉末を得る工程、
前記混合粉末を金型に充填するとともに、磁場中で圧力成形し、成形体を得る工程、および、
前記成形体を、同一の前記金型内において、放電プラズマ焼結することにより、前記アモルファス金属の前記軟化開始温度以上の温度に加熱する工程
を備えることを特徴とする、磁性材料の製造方法。
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CN113677457B (zh) * | 2019-03-14 | 2024-03-29 | 国立研究开发法人产业技术综合研究所 | 亚稳态单晶稀土磁体微粉以及其制造方法 |
CN110106454B (zh) * | 2019-05-27 | 2021-05-07 | 大连理工大学 | 一种硼基非晶合金及其制备方法 |
CN113496816A (zh) * | 2020-03-18 | 2021-10-12 | 中国科学院宁波材料技术与工程研究所 | 钐钴基永磁块体的生产方法及钐钴基永磁块体 |
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- 2011-08-29 CN CN201180042824XA patent/CN103081035A/zh active Pending
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Also Published As
Publication number | Publication date |
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CN103081035A (zh) | 2013-05-01 |
US20130280119A1 (en) | 2013-10-24 |
DE112011102958T5 (de) | 2013-06-20 |
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