WO2021238867A1 - 一种钕铁硼磁体及其制备方法和应用 - Google Patents
一种钕铁硼磁体及其制备方法和应用 Download PDFInfo
- Publication number
- WO2021238867A1 WO2021238867A1 PCT/CN2021/095528 CN2021095528W WO2021238867A1 WO 2021238867 A1 WO2021238867 A1 WO 2021238867A1 CN 2021095528 W CN2021095528 W CN 2021095528W WO 2021238867 A1 WO2021238867 A1 WO 2021238867A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- magnet
- iron boron
- neodymium iron
- boron magnet
- content
- Prior art date
Links
- 238000002360 preparation method Methods 0.000 title claims abstract description 9
- 229910001172 neodymium magnet Inorganic materials 0.000 claims abstract description 62
- 229910052761 rare earth metal Inorganic materials 0.000 claims abstract description 24
- 238000000034 method Methods 0.000 claims abstract description 18
- 229910052723 transition metal Inorganic materials 0.000 claims abstract description 5
- 239000002131 composite material Substances 0.000 claims abstract description 3
- 239000000126 substance Substances 0.000 claims abstract description 3
- 238000009792 diffusion process Methods 0.000 claims description 54
- 238000011282 treatment Methods 0.000 claims description 15
- 229910000831 Steel Inorganic materials 0.000 claims description 13
- 238000003825 pressing Methods 0.000 claims description 13
- 239000010959 steel Substances 0.000 claims description 13
- 239000002344 surface layer Substances 0.000 claims description 9
- 238000000576 coating method Methods 0.000 claims description 7
- 238000009826 distribution Methods 0.000 claims description 6
- 239000012535 impurity Substances 0.000 claims description 6
- 238000001755 magnetron sputter deposition Methods 0.000 claims description 6
- 238000004321 preservation Methods 0.000 claims description 6
- 229910052782 aluminium Inorganic materials 0.000 claims description 5
- 239000011248 coating agent Substances 0.000 claims description 5
- 229910052802 copper Inorganic materials 0.000 claims description 5
- 229910052733 gallium Inorganic materials 0.000 claims description 4
- 238000007738 vacuum evaporation Methods 0.000 claims description 4
- 229910052684 Cerium Inorganic materials 0.000 claims description 2
- 229910052691 Erbium Inorganic materials 0.000 claims description 2
- 229910052693 Europium Inorganic materials 0.000 claims description 2
- 229910052688 Gadolinium Inorganic materials 0.000 claims description 2
- 229910052689 Holmium Inorganic materials 0.000 claims description 2
- 229910052765 Lutetium Inorganic materials 0.000 claims description 2
- 229910052777 Praseodymium Inorganic materials 0.000 claims description 2
- 229910052773 Promethium Inorganic materials 0.000 claims description 2
- 229910052772 Samarium Inorganic materials 0.000 claims description 2
- 229910052775 Thulium Inorganic materials 0.000 claims description 2
- 229910052769 Ytterbium Inorganic materials 0.000 claims description 2
- GWXLDORMOJMVQZ-UHFFFAOYSA-N cerium Chemical compound [Ce] GWXLDORMOJMVQZ-UHFFFAOYSA-N 0.000 claims description 2
- UYAHIZSMUZPPFV-UHFFFAOYSA-N erbium Chemical compound [Er] UYAHIZSMUZPPFV-UHFFFAOYSA-N 0.000 claims description 2
- OGPBJKLSAFTDLK-UHFFFAOYSA-N europium atom Chemical compound [Eu] OGPBJKLSAFTDLK-UHFFFAOYSA-N 0.000 claims description 2
- UIWYJDYFSGRHKR-UHFFFAOYSA-N gadolinium atom Chemical compound [Gd] UIWYJDYFSGRHKR-UHFFFAOYSA-N 0.000 claims description 2
- KJZYNXUDTRRSPN-UHFFFAOYSA-N holmium atom Chemical compound [Ho] KJZYNXUDTRRSPN-UHFFFAOYSA-N 0.000 claims description 2
- 229910052746 lanthanum Inorganic materials 0.000 claims description 2
- FZLIPJUXYLNCLC-UHFFFAOYSA-N lanthanum atom Chemical compound [La] FZLIPJUXYLNCLC-UHFFFAOYSA-N 0.000 claims description 2
- OHSVLFRHMCKCQY-UHFFFAOYSA-N lutetium atom Chemical compound [Lu] OHSVLFRHMCKCQY-UHFFFAOYSA-N 0.000 claims description 2
- 229910052748 manganese Inorganic materials 0.000 claims description 2
- PUDIUYLPXJFUGB-UHFFFAOYSA-N praseodymium atom Chemical compound [Pr] PUDIUYLPXJFUGB-UHFFFAOYSA-N 0.000 claims description 2
- VQMWBBYLQSCNPO-UHFFFAOYSA-N promethium atom Chemical compound [Pm] VQMWBBYLQSCNPO-UHFFFAOYSA-N 0.000 claims description 2
- KZUNJOHGWZRPMI-UHFFFAOYSA-N samarium atom Chemical compound [Sm] KZUNJOHGWZRPMI-UHFFFAOYSA-N 0.000 claims description 2
- 229910052706 scandium Inorganic materials 0.000 claims description 2
- SIXSYDAISGFNSX-UHFFFAOYSA-N scandium atom Chemical compound [Sc] SIXSYDAISGFNSX-UHFFFAOYSA-N 0.000 claims description 2
- FRNOGLGSGLTDKL-UHFFFAOYSA-N thulium atom Chemical compound [Tm] FRNOGLGSGLTDKL-UHFFFAOYSA-N 0.000 claims description 2
- 229910052719 titanium Inorganic materials 0.000 claims description 2
- 229910052721 tungsten Inorganic materials 0.000 claims description 2
- NAWDYIZEMPQZHO-UHFFFAOYSA-N ytterbium Chemical compound [Yb] NAWDYIZEMPQZHO-UHFFFAOYSA-N 0.000 claims description 2
- 229910052727 yttrium Inorganic materials 0.000 claims description 2
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 claims description 2
- 229910052725 zinc Inorganic materials 0.000 claims description 2
- 229910052726 zirconium Inorganic materials 0.000 claims description 2
- 230000005347 demagnetization Effects 0.000 abstract description 26
- 239000000463 material Substances 0.000 abstract description 13
- 238000004519 manufacturing process Methods 0.000 abstract description 9
- 230000009467 reduction Effects 0.000 abstract description 8
- 230000004907 flux Effects 0.000 abstract description 7
- 239000012071 phase Substances 0.000 description 26
- 238000002474 experimental method Methods 0.000 description 15
- 238000005516 engineering process Methods 0.000 description 11
- 238000012360 testing method Methods 0.000 description 11
- 239000013078 crystal Substances 0.000 description 10
- 230000000694 effects Effects 0.000 description 9
- 230000005415 magnetization Effects 0.000 description 8
- 239000000203 mixture Substances 0.000 description 8
- 239000000843 powder Substances 0.000 description 8
- QJVKUMXDEUEQLH-UHFFFAOYSA-N [B].[Fe].[Nd] Chemical compound [B].[Fe].[Nd] QJVKUMXDEUEQLH-UHFFFAOYSA-N 0.000 description 7
- 229910045601 alloy Inorganic materials 0.000 description 7
- 239000000956 alloy Substances 0.000 description 7
- 238000001816 cooling Methods 0.000 description 7
- 239000002994 raw material Substances 0.000 description 7
- 230000007423 decrease Effects 0.000 description 6
- 239000010410 layer Substances 0.000 description 6
- 238000005245 sintering Methods 0.000 description 6
- 230000009471 action Effects 0.000 description 5
- 238000005324 grain boundary diffusion Methods 0.000 description 5
- 238000002844 melting Methods 0.000 description 5
- 230000008018 melting Effects 0.000 description 5
- 229910052751 metal Inorganic materials 0.000 description 5
- 239000002184 metal Substances 0.000 description 5
- 150000002910 rare earth metals Chemical class 0.000 description 5
- 229910052771 Terbium Inorganic materials 0.000 description 4
- 238000010902 jet-milling Methods 0.000 description 4
- 238000000465 moulding Methods 0.000 description 4
- 239000000758 substrate Substances 0.000 description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 239000000314 lubricant Substances 0.000 description 3
- 239000002245 particle Substances 0.000 description 3
- 229910052692 Dysprosium Inorganic materials 0.000 description 2
- 229910000976 Electrical steel Inorganic materials 0.000 description 2
- 238000003723 Smelting Methods 0.000 description 2
- 239000002253 acid Substances 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 238000000227 grinding Methods 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 230000006698 induction Effects 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 238000010298 pulverizing process Methods 0.000 description 2
- 238000010791 quenching Methods 0.000 description 2
- 238000002791 soaking Methods 0.000 description 2
- 238000004611 spectroscopical analysis Methods 0.000 description 2
- 238000004804 winding Methods 0.000 description 2
- 229910052779 Neodymium Inorganic materials 0.000 description 1
- 230000010718 Oxidation Activity Effects 0.000 description 1
- 238000004378 air conditioning Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000003153 chemical reaction reagent Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000007598 dipping method Methods 0.000 description 1
- KBQHZAAAGSGFKK-UHFFFAOYSA-N dysprosium atom Chemical compound [Dy] KBQHZAAAGSGFKK-UHFFFAOYSA-N 0.000 description 1
- 238000011049 filling Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000009776 industrial production Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- 230000005381 magnetic domain Effects 0.000 description 1
- 238000000691 measurement method Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- QEFYFXOXNSNQGX-UHFFFAOYSA-N neodymium atom Chemical compound [Nd] QEFYFXOXNSNQGX-UHFFFAOYSA-N 0.000 description 1
- 230000010287 polarization Effects 0.000 description 1
- 238000007780 powder milling Methods 0.000 description 1
- 229910001404 rare earth metal oxide Inorganic materials 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000004544 sputter deposition Methods 0.000 description 1
- GZCRRIHWUXGPOV-UHFFFAOYSA-N terbium atom Chemical compound [Tb] GZCRRIHWUXGPOV-UHFFFAOYSA-N 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Images
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
- H01F1/032—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 hard-magnetic materials
- H01F1/04—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 hard-magnetic materials metals or alloys
- H01F1/047—Alloys characterised by their composition
- H01F1/053—Alloys characterised by their composition containing rare earth metals
- H01F1/055—Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5
- H01F1/057—Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5 and IIIa elements, e.g. Nd2Fe14B
-
- 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
- H01F1/032—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 hard-magnetic materials
- H01F1/04—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 hard-magnetic materials metals or alloys
- H01F1/047—Alloys characterised by their composition
- H01F1/053—Alloys characterised by their composition containing rare earth metals
- H01F1/055—Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5
- H01F1/057—Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5 and IIIa elements, e.g. Nd2Fe14B
- H01F1/0571—Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5 and IIIa elements, e.g. Nd2Fe14B in the form of particles, e.g. rapid quenched powders or ribbon flakes
- H01F1/0575—Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5 and IIIa elements, e.g. Nd2Fe14B in the form of particles, e.g. rapid quenched powders or ribbon flakes pressed, sintered or bonded together
- H01F1/0576—Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5 and IIIa elements, e.g. Nd2Fe14B in the form of particles, e.g. rapid quenched powders or ribbon flakes pressed, sintered or bonded together pressed, e.g. hot working
-
- 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
- C22C38/002—Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
-
- 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
- C22C38/005—Ferrous alloys, e.g. steel alloys containing rare earths, i.e. Sc, Y, Lanthanides
-
- 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
- C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
-
- 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
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
-
- 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
- C22C38/10—Ferrous alloys, e.g. steel alloys containing cobalt
-
- 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
- C22C38/12—Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
-
- 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
- C22C38/14—Ferrous alloys, e.g. steel alloys containing titanium or zirconium
-
- 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
- C22C38/16—Ferrous alloys, e.g. steel alloys containing copper
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
- C23C14/14—Metallic material, boron or silicon
- C23C14/16—Metallic material, boron or silicon on metallic substrates or on substrates of boron or silicon
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
- C23C14/14—Metallic material, boron or silicon
- C23C14/16—Metallic material, boron or silicon on metallic substrates or on substrates of boron or silicon
- C23C14/165—Metallic material, boron or silicon on metallic substrates or on substrates of boron or silicon by cathodic sputtering
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
- C23C14/24—Vacuum evaporation
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
- C23C14/34—Sputtering
- C23C14/35—Sputtering by application of a magnetic field, e.g. magnetron sputtering
-
- 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
- H01F1/032—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 hard-magnetic materials
- H01F1/04—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 hard-magnetic materials metals or alloys
- H01F1/047—Alloys characterised by their composition
- H01F1/053—Alloys characterised by their composition containing rare earth metals
- H01F1/055—Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5
- H01F1/057—Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5 and IIIa elements, e.g. Nd2Fe14B
- H01F1/0571—Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5 and IIIa elements, e.g. Nd2Fe14B in the form of particles, e.g. rapid quenched powders or ribbon flakes
- H01F1/0575—Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5 and IIIa elements, e.g. Nd2Fe14B in the form of particles, e.g. rapid quenched powders or ribbon flakes pressed, sintered or bonded together
- H01F1/0577—Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5 and IIIa elements, e.g. Nd2Fe14B in the form of particles, e.g. rapid quenched powders or ribbon flakes pressed, sintered or bonded together sintered
-
- 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
- H01F41/0253—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 for manufacturing permanent magnets
-
- 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
- H01F41/0253—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 for manufacturing permanent magnets
- H01F41/0266—Moulding; Pressing
-
- 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
- H01F41/0253—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 for manufacturing permanent magnets
- H01F41/0293—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 for manufacturing permanent magnets diffusion of rare earth elements, e.g. Tb, Dy or Ho, into permanent magnets
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F7/00—Magnets
- H01F7/02—Permanent magnets [PM]
- H01F7/0205—Magnetic circuits with PM in general
- H01F7/021—Construction of PM
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F38/00—Adaptations of transformers or inductances for specific applications or functions
Definitions
- the invention belongs to the field of neodymium iron boron magnets, and specifically relates to a neodymium iron boron magnet and a preparation method and application thereof.
- Sintered NdFeB magnets as the fourth-generation permanent magnet materials, are called "magnet kings" with their excellent magnetic properties. They are widely used in many fields such as automobiles, wind power, compressors, elevators, and industrial automation.
- the sintered NdFeB magnets in the motor are exposed to a high-temperature environment due to the heat generated by the windings and iron cores, and thermal demagnetization is prone to occur due to the action of the opposite direction magnetic field from the windings.
- Dy and/or Tb instead of Nd (neodymium) to form Dy-Fe-B or Tb-Fe-B
- the magnetic polarization of the two is significantly lower than that of Nd-Fe-B, resulting in a decrease in the remanence of the magnet That is, the final magnetic field strength that the magnet can provide is reduced, resulting in a decrease in the power of the motor or the need to increase the use of magnets in the motor to ensure the power output of the motor; at the same time, heavy rare earths are very expensive due to their reserves and excellent characteristics. The cost of magnets will also increase substantially as the amount of heavy rare earths used increases.
- the fine-grain technology is to reduce the size of the crystal grains to form single domain crystals as much as possible, reduce the number of magnetic domains inside a single magnet crystal grain, reduce internal defects of the crystal grain, and achieve the purpose of improving the coercive force of the magnet.
- Diffusion technology is to accurately put in heavy rare earth elements such as Dy and/or Tb to diffuse from the surface of the magnet into the inside of the magnet and enrich it at the grain boundary to improve the coercive force of the magnet.
- the grain boundary diffusion technology can use a small amount of heavy rare earths, the coercive force can be greatly improved, and the remanence will not drop significantly, and it has been widely recognized and applied in the industry.
- the grain boundary diffusion technology is another innovative development of the classic diffusion theory in the NdFeB industry. Its main principle is that under high temperature conditions, heavy rare earth elements such as Dy and/or Tb move along the grain boundary phase from the surface of the magnet to the center of the magnet.
- Diffusion and enrichment on the grain boundary phase replacing the Nd in the outer edge layer of the main phase grains, forming a layer of Dy or Tb enriched shell-like structure on the outer edge of the main phase grains, improving the outer edge of the grains Anisotropic field, so as to achieve the effect of greatly improving the coercivity.
- the concentration difference of Dy and/or Tb after it penetrates into the magnet, the concentration difference of Dy and/or Tb will be formed from the surface to the inside of the magnet, which will lead to the Hcj from the magnet. From the surface to the inside, there is also a phenomenon of gradient distribution.
- the embedded assembly of magnets for high-speed running motors such as the magnets used in automobile drive motors or the magnets used in air-conditioning compressor motors, does not occur uniformly throughout the entire motor due to the increase in the temperature of the entire motor during actual use. It often occurs at the corners, especially the four edges in contact with the silicon steel sheet of the motor. However, other areas of the magnet are less prone to demagnetization. Grain boundary diffusion technology has been widely recognized and applied in high-speed embedded assembly motors due to its unique Hcj distribution law.
- Nd-Fe-B sintered magnet records that Nd-Fe-B magnets are diffused in different directions, and their diffusion effects are inconsistent. Among them, diffusion along the magnetizing direction has the best effect. The material can diffuse deeper into the magnet; instead of the magnetization direction, the diffusion depth of the diffused material is limited, mainly concentrated on the surface of the material. Correspondingly, this also determines that the magnet uses the magnetizing direction to diffuse. When its Hcj increases significantly, its Br will decrease slightly. When using the non-magnetized direction to diffuse, because the diffusion material is mostly concentrated on the surface of the magnet, The internal structure of the magnet is uneven and the squareness is poor, which in turn affects the magnet's ability to withstand demagnetization.
- the patent document CN 101939804A describes that the magnet surface is coated with 4 surfaces parallel to the magnetizing direction.
- the magnet can obtain a high coercive force. Especially at the edge of the magnet, it is not easy to demagnetize even at high temperature. It is suitable for permanent magnet type. Rotating motor.
- This patent document effectively combines the actual operating state of the motor with the special law of the diffused magnet, and effectively maintains the magnetic flux of the magnet on the basis of ensuring the magnet's ability to withstand demagnetization.
- the four surfaces of the magnet parallel to the magnetizing direction are coated with diffusion materials, the internal structure of the magnet is not uniform, and the problem of poor squareness has not been solved. Although its resistance to demagnetization has been improved, the improvement is limited.
- Coating 4 surfaces parallel to the magnetizing direction When using the dipping method, it is necessary to isolate the two opposite surfaces perpendicular to the magnetizing direction, and the diffusion material will be unevenly distributed on the magnet surface due to gravity; magnetron sputtering is required
- the diffusion material can be attached to all 4 surfaces after multiple treatments, which results in low production efficiency and high mass production costs.
- the present invention provides a neodymium iron boron magnet and a preparation method and application thereof in order to improve the above technical problems and difficulties in actual mass production.
- a neodymium iron boron magnet which is represented by the chemical formula R1-R2-Fe-M-B, the neodymium iron boron magnet has a composite structure of a high coercivity region and a high remanence region;
- R1 is a rare earth element containing at least Nd
- R2 is a heavy rare earth element containing at least Dy and/or Tb
- M is a transition metal element containing at least Co.
- the content of R2 in the neodymium iron boron magnet is less than or equal to 1.0 wt%, for example, less than or equal to 0.8 wt%, preferably less than or equal to 0.5 wt%.
- the neodymium iron boron magnet has a high coercive force region with a high R2 content and a high remanence region with a low R2 content.
- the distribution of the high coercivity area and the high remanence area is basically as shown in FIG. 1.
- the R2 concentration difference between the surface layer of the high remanence region and the inside of the magnet at about 1mm is ⁇ 1 ⁇ 0.1%
- the R2 concentration difference between the surface layer of the high coercive force region and the interior of the neodymium iron boron magnet is about 1 mm ⁇ 2 ⁇ 0.15%.
- the width of the high coercivity area is 1-5 mm, preferably 1.5-4 mm, and the central area has a high remanence area, which can effectively avoid the reduction of the magnetic flux of the magnet.
- the high coercive force region is defined as extending from the surface layer to the inside of the magnet, and when the concentration difference of R2 is 1%, it is the width of the high coercive force region.
- the neodymium iron boron magnet has a structure basically as shown in FIG. 1.
- the R1 may also contain lanthanum (La), cerium (Ce), praseodymium (Pr), promethium (Pm), samarium (Sm), europium (Eu) and scandium. At least one of (Sc).
- the content of R1 in the neodymium iron boron magnet is 28-32wt%, for example 29-31wt%, exemplarily 28wt%, 29wt%, 30wt%, 31wt%, 32wt%.
- the R2 may also contain gadolinium (Gd), holmium (Ho), erbium (Er), thulium (Tm), ytterbium (Yb), lutetium ( At least one of Lu) and yttrium (Y).
- Gd gadolinium
- Ho holmium
- Er erbium
- Tm thulium
- Yb ytterbium
- Lu yttrium
- the M may also contain at least one of Cu, Ga, Zr, Ti, Al, Mn, Zn, and W; for example, M is selected from Co, Al, Cu And at least one of Ga.
- the content of Co in the neodymium iron boron magnet is 1-3wt%, for example 1.5-2.5wt%, exemplarily 1wt%, 1.5wt%, 2wt%, 2.5wt%, 3wt% .
- the content of the transition metal elements in the NdFeB magnet other than Co in M is ⁇ 2wt%, for example, ⁇ 1.5wt%, or ⁇ 1wt%, exemplarily 0.1wt%, 0.15wt%, 0.2wt%, 0.3wt%, 0.35wt%, 0.4wt%, 0.5wt%, 0.6wt%, 0.7wt%, 0.8wt%, 0.9wt%, 1.0wt%.
- the content of B in the neodymium iron boron magnet is 0.5-1.3wt%, for example 0.8-1.05wt%, exemplarily 0.8wt%, 0.9wt%, 0.98wt%, 1.0wt% , 1.05wt%.
- the neodymium iron boron magnet also contains inevitable impurities, such as at least one of C, N and the like.
- the neodymium iron boron magnet has excellent demagnetization resistance.
- the squareness of the neodymium iron boron magnet is ⁇ 0.9.
- the demagnetization resistance of the magnet mainly depends on the demagnetization resistance of the magnet itself and the working load point of the motor.
- the squareness of the magnet at the working temperature determines the matching relationship between the magnet's own demagnetization resistance and the motor's working load point. The higher the squareness, the higher the magnet's own demagnetization resistance, which is affected by the motor's working load point. The smaller.
- the present invention also provides a preparation method of the above-mentioned neodymium iron boron magnet, which includes the following steps:
- the base magnet of the R1-Fe-MB base structure make the heavy rare earth element R2 containing at least Dy and/or Tb form a film on the two opposite sides of the base magnet surface, and then carry out the diffusion treatment, the R2 element is along the base
- the grain boundary of the magnet diffuses from the surface of the magnet to the inside, and is enriched at the grain boundary to obtain the neodymium iron boron magnet;
- R1, R2, M and B all have the meaning and content as described above.
- the base magnet can be prepared by methods known in the art, for example, by smelting, powdering, pressing, and heat treatment.
- the raw material powder is prepared according to the above element content.
- the raw material powder is heated (for example, 1400-1520°C) and melted into molten steel. After rapid cooling, it nucleates and crystallizes, and gradually grows to form alloy flakes.
- the powder milling adopts a jet mill grinding method to obtain jet mill powder with an average particle size of 1-5 ⁇ m, preferably 2-4 ⁇ m.
- a lubricant known in the art is added to the jet mill powder, and after the materials are fully mixed, the powder is pressed into molding under the action of an external magnetic field.
- the temperature of the heat treatment is 1050-1100°C, exemplarily 1070°C and 1075°C; the heat preservation time of the heat treatment is 200-400min, exemplarily 270min, 300min.
- the base magnet is a regular hexahedron.
- the two opposite faces are two opposite faces that are not perpendicular to the magnetic direction of the base magnet and not perpendicular to the pressing direction (ie, the magnetizing direction) when the base magnet is formed.
- the details are shown in Figure 2.
- the R2 element is formed into a film on these two opposite surfaces, which can more effectively increase the effective utilization rate of diffused heavy rare earth elements, avoid the waste of heavy rare earth elements, and avoid the influence of the reduction of magnet remanence to the greatest extent.
- the method for forming a film of the R2 element on the surface of the base magnet can be a method known in the art, including but not limited to methods such as vacuum evaporation, magnetron sputtering, and coating.
- vacuum evaporation, magnetron sputtering or coating of the same amount of R2 element For example, on the two opposite sides of the base magnet, vacuum evaporation, magnetron sputtering or coating of the same amount of R2 element.
- the amount of R2 element is ⁇ 0.5wt%, such as 0.4wt%, 0.2wt%.
- the vacuum degree of the diffusion treatment is ⁇ 10 -2 Pa.
- the first temperature rise and then heat preservation are carried out, and then the temperature is rapidly cooled down, and then the second temperature rise and heat preservation are carried out to complete the diffusion treatment.
- the temperature to which the temperature is raised for the first time is 850-950°C, such as 880-930°C, exemplarily 900°C.
- the time for the first heat preservation is 500-700 min, such as 550-650 min, exemplarily 600 min.
- the temperature to which the rapid cooling is reached is 15-40°C, such as 20-35°C, exemplarily 25°C (room temperature).
- the rapid cooling rate is 5-30°C/min, such as 10-20°C/min, exemplarily 5°C/min, 10°C/min, 15°C/min, 20°C/min, 25°C/min min, 30°C/min.
- the temperature to which the temperature is raised for the second time is 500-600°C, such as 520-580°C, exemplarily 550°C.
- the time for the second heat preservation is 200-300 min, such as 220-270 min, exemplarily 240 min.
- the invention also provides the neodymium iron boron magnet prepared by the above method.
- the invention also provides the application of the above-mentioned neodymium iron boron magnets in embedded motors.
- the present invention also provides a magnetic steel containing the neodymium iron boron magnet.
- the present invention also provides an embedded motor, which contains the above-mentioned neodymium iron boron magnet and/or magnetic steel.
- the neodymium iron boron magnet and/or the magnetic steel are embedded in the motor.
- the neodymium iron boron magnet of the present invention can use a small amount of Dy/Tb, greatly improve the high-temperature resistance demagnetization ability of the magnet, and suppress the reduction of the magnetic flux of the magnet, and is suitable for embedded high-speed motors.
- the method for preparing the magnet can also greatly improve the utilization rate of the material and the production efficiency, and has the feasibility of mass production.
- the area that is prone to demagnetization is only on the outermost layer, and there is almost no demagnetization inside.
- the heavy rare earth elements diffused into the magnet are wasteful, and In the process of diffusion, it will inevitably diffuse into the main phase crystal grains, resulting in a reduction in the remanence of the magnet and affecting the output power of the motor.
- the inventor further found that when the heavy rare earth film is formed and diffused on the surface perpendicular to the pressing direction of the magnet, the diffusion depth is very shallow and the coercive force increase is lower than that of the magnetization direction.
- the squareness range at working temperature is less than 0.9, which greatly affects the magnet's ability to withstand demagnetization when the motor is running.
- the coercivity of the magnet is The force increase is between the diffusion in the compression direction of the magnet and the diffusion in the magnetization direction, and the squareness at the working temperature is ⁇ 0.9.
- the main phase crystal grains When it is pressed in magnetization, the main phase crystal grains are deflected under the action of a magnetic field, and then when it is pressed, it appears that there is no grain boundary phase or polarity between the crystal grains perpendicular to the pressing direction.
- the grain boundary phase is thin, and the grain boundary phase between the grains parallel to the pressing direction is thick.
- the thicker grain boundary phase will melt into the liquid phase, which acts as a flux to promote the growth of the main phase grains; or fills the adjacent two main phase grains to form the grain boundary through the principle of capillary tension Phase; or the formation of a larger triangular grain boundary phase or a thicker binary grain boundary phase, due to the active nature of RE elements, it is easy to form impurity compounds such as rare earth oxides in it. Therefore, the uniformity of the grain boundary phase parallel to the pressing direction is poor, and there are many impurities, and it is not easy to react with displacement diffusion, resulting in a small increase in the coercive force of the magnet diffused along the pressing direction and low squareness.
- the grain boundary phase is repaired by the liquefaction and filling of the grain boundary phase parallel to the pressing direction during sintering, and a continuous uniform fineness is formed.
- the thin grain boundary phase is prone to displacement diffusion reaction, but it is perpendicular to the magnet C axis, and its diffusion depth and effect are slightly inferior to the orientation direction diffusion.
- the diffusion depth and diffusion effect are highly coincident with the actual easy demagnetization area of the magnet when the motor is running, achieving the efficient application of heavy rare earths, and the squareness can be ensured ⁇ 0.9, ensuring the resistance of the magnet Demagnetization ability.
- the heavy rare earth film is not formed on the surface of the magnet perpendicular to the magnetizing direction, the content of heavy rare earth is relatively low in most of the surface perpendicular to the magnetizing direction, and the reduction of its remanence is significantly suppressed, effectively ensuring Maintain the magnetic flux of the magnet.
- the present invention only performs film formation and diffusion on the two opposite surfaces of the magnet, which not only simplifies
- the production process has been reduced, the use of heavy rare earths has been reduced, the feasibility of industrial production has been greatly improved, and it is suitable for embedded high-speed motor applications, because the embedded high-speed motor is operating at high temperature at high speed, its easy demagnetization area is the magnet
- the position of the edge in contact with the silicon steel sheet component of the motor When the edge has a high coercivity, it can effectively resist the high-temperature thermal demagnetization phenomenon of the magnetic steel.
- the magnetic steel in the embedded motor has a small surface area where demagnetization occurs; the high coercivity area obtained by its diffusion corresponds to the easy demagnetization area of the magnet (as shown in Figure 3).
- the embedded assembly method shown in Figure 3 can effectively improve the magnet's resistance to demagnetization and significantly suppress the reduction of the magnetic flux of the magnet.
- Fig. 1 is a schematic diagram of the high remanence area and the high coercive force area of the neodymium iron boron magnet of the present invention.
- Figure 2 is a schematic diagram of the diffusion surface of the neodymium iron boron magnet of the present invention.
- Figure 3 is a schematic diagram of the structure of the embedded motor (a) and the magnet (b).
- Figure 4 is a graph showing the relationship between coercivity and diffusion depth.
- the raw materials and reagents used in the following examples are all commercially available products, or can be prepared by known methods.
- High coercivity area define the side of this area away from the high remanence area as the surface layer, from the surface layer and extending into the inside of the magnet, each processing 1*1*1mm small test piece, after acid soaking and melting the whole, adopt the spectroscopic method to test
- the difference between R2 content and R2 content is ⁇ 2.
- the squareness involved in the present invention takes the final magnet as the standard size of the sample and is tested by a magnetic measuring instrument.
- the gradient distribution of the coercive force involved in the present invention is tested by processing a 1*1*1mm test piece on a magnet and using a strong pulse PFM06 equipment.
- R1-Fe-MB based magnets Prepare raw alloys according to the following composition ratios.
- R1 is Nd with a content of 30.5wt%; Co content is 1.5wt%; M is Al, Cu and Ga, with a content of 0.1wt. %, 0.1wt% and 0.15wt%; B content is 0.95%, the balance is Fe and unavoidable impurities, such as C, N and so on.
- the specific preparation process of the neodymium iron boron base magnet is as follows:
- a) Melting Using a vacuum induction melting furnace, put the above-equipped raw materials into a crucible and heat it to 1480°C. The raw materials are melted into molten steel, and the fully dissolved molten steel is poured onto the quench roll, and the temperature is rapidly reduced. It nucleates, crystallizes, and gradually grows to form alloy scales.
- Pulverization The alloy flakes are subjected to HD crushing treatment, and then subjected to jet milling to obtain jet milling powder with an average particle size of SMD of 3.0 ⁇ m.
- the substrate magnet was processed into small pieces of 10-10 mm to 10 mm, and the Dy metal sputter coating was performed on the surface of the substrate magnet according to Table 1 using the magnetron sputtering method.
- experiments 1, 2, 3, 4 comprehensively compare the coercive force, squareness and magnetic moment indicators.
- Experiment 4 has the highest comprehensive performance, and the width of the high coercive force area is 2.4mm, which can cover the high speed of the motor. The area is easy to demagnetize during operation.
- the test piece was processed according to the diffusion direction to test the relationship between the coercivity and the diffusion depth, as shown in FIG. 4.
- experiment 2 diffuses along the magnetizing direction, the average value of the coercive force is the highest, and the fluctuation along the diffusion depth is the smallest;
- experiment 3 diffuses along the pressing direction, its coercive force forms a sharp peak on the diffusion surface and enters the magnet At 1mm inside, the coercive force drops sharply, and the coercive force at the center position is almost equivalent to that of the undiffused magnet;
- Experiment 4 the coercive force decreases stepwise at 0-3mm on the surface of the magnet, the outermost layer
- the coercive force is due to the diffusion of the magnetizing direction in Experiment 2, that is, the demagnetization resistance of its outermost layer is better than that in Experiment 2, and it gradually becomes flat at> 3mm, and the coercive force is about 250kA/m higher than that of the non-diffused magnet. , Its resistance to demagnetization has also been improved.
- R1-Fe-MB based magnets Prepare R1-Fe-MB based magnets and prepare raw alloys according to the following composition ratios, where R1 is Nd with a content of 31wt%; Dy content is 0.5wt%, Co content is 2.0wt%; M is Al, Cu and Ga, The content is respectively 0.15wt%, 0.15wt% and 0.1wt%; the B content is 0.98%, the balance is Fe and inevitable impurities, such as C, N and so on.
- the specific preparation process of the neodymium iron boron base magnet is as follows:
- a) Melting Using a vacuum induction melting furnace, put the above-equipped raw materials into a crucible and heat it to 1460°C. The raw materials are melted into molten steel, and the fully dissolved molten steel is poured onto the quench roller, and the temperature is rapidly reduced. It nucleates, crystallizes, and gradually grows to form alloy scales.
- Pulverization The alloy flakes are subjected to HD crushing treatment, and then subjected to jet milling to obtain jet milling powder with an average particle size of SMD of 2.8 ⁇ m.
- the substrate magnet is processed into 40-8-20 and 40-8-2.5 square pieces (20 and 2.5 directions are the thickness in the magnetizing direction), and the surface of the substrate magnet is coated with Tb metal according to the coating method according to Table 3. .
- the coercivity at 3mm is slightly lower in experiment 6, but the coercivity of the outermost layer is 156kA/m higher than that in experiment 7, which can effectively resist the demagnetization effect of the external magnetic field on the magnet; at the same time, the magnetic moment is higher. 0.6%, effectively avoiding the reduction of the magnetic moment, and ensuring the high-efficiency output of the magnet's magnetic field.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Power Engineering (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Organic Chemistry (AREA)
- Metallurgy (AREA)
- Manufacturing & Machinery (AREA)
- Inorganic Chemistry (AREA)
- Crystallography & Structural Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Hard Magnetic Materials (AREA)
- Manufacturing Cores, Coils, And Magnets (AREA)
- Powder Metallurgy (AREA)
- Permanent Field Magnets Of Synchronous Machinery (AREA)
Abstract
Description
实验编号 | 磁体尺寸 | Tb金属施加位置 |
5 | 40-8-2.5 | 无 |
6 | 40-8-20 | 40*20的2个对面,每个单面均匀涂覆磁体0.2wt%的Tb |
7 | 40-8-2.5 | 40*8的2个对面,每个单面均匀涂覆磁体0.2wt%的Tb |
Claims (10)
- 一种钕铁硼磁体,其特征在于,所述钕铁硼磁体以化学式R1-R2-Fe-M-B表示,所述钕铁硼磁体具有高矫顽力区域和高剩磁区域的复合结构;其中,R1为至少含有Nd的稀土元素,R2为至少含有Dy和/或Tb的重稀土元素,M为至少含有Co的过渡金属元素。
- 根据权利要求1所述的钕铁硼磁体,其特征在于,R2在所述钕铁硼磁体中的含量≤1.0wt%,例如≤0.8wt%,优选≤0.5wt%。
- 根据权利要求1或2所述的钕铁硼磁体,其特征在于,所述钕铁硼磁体具有R2含量高的高矫顽力区域和具有R2含量低的高剩磁区域;优选地,所述高矫顽力区域和高剩磁区域的分布基本如图1所示。优选地,所述高剩磁区域的表层及磁体内部1mm处的R2浓度差△1≤0.1%,优选地,所述高矫顽力区域的表层及与所述钕铁硼磁体内部1mm处的R2浓度差△2≥0.15%。优选地,所述△2/△1≥1.5,优选△2/△1≥2。优选地,所述高矫顽力区域的宽度为1-5mm,优选1.5-4mm,且中心区域具有高剩磁区域;其中,所述高矫顽力区域定义为自表层至磁体内部延伸,R2的浓度差值为1%时,即为高矫顽力区域的宽度。
- 根据权利要求1-3任一项所述的钕铁硼磁体,其特征在于,所述R1除含Nd元素外,还含有镧(La)、铈(Ce)、镨(Pr)、钷(Pm)、钐(Sm)、铕(Eu)和钪(Sc)中的至少一种。优选地,所述R1在钕铁硼磁体中的含量为28-32wt%。
- 根据权利要求1-4任一项所述的钕铁硼磁体,其特征在于,所述R2除含有Dy和/或Tb元素外,还含有钆(Gd)、钬(Ho)、铒(Er)、铥(Tm)、镱(Yb)、镥(Lu)和钇(Y)中的至少一种。优选地,所述M除含有Co外,还含有Cu、Ga、Zr、Ti、Al、Mn、Zn和W中的至少一种。优选地,所述Co在钕铁硼磁体中的含量为1-3wt%。优选地,除Co之外的M中其余过渡金属元素在钕铁硼磁体中的含量≤2wt%。优选地,所述B在钕铁硼磁体中的含量为0.5-1.3wt%。优选地,所述钕铁硼磁体中还含有不可避免的杂质。
- 权利要求1-5任一项所述钕铁硼磁体的制备方法,其特征在于,包括如下步骤:制备或准备R1-Fe-M-B基结构的基体磁体,使至少含有Dy和/或Tb的重稀土元素R2在所述基体磁体表面的2个对面上成膜,然后进行扩散处理,R2元素沿基体磁体晶界由磁体表面向内部扩散,并在晶界处富集,得到所述钕铁硼磁体。
- 根据权利要求6所述钕铁硼磁体的制备方法,其特征在于,所述基体磁体为规则的六面体。优选地,所述2个对面为非垂直于磁体充磁方向且非垂直于磁体成型时压制方向-的2个对面。优选地,所述R2元素在磁体表面成膜的方式包括但不限于真空蒸镀、磁控溅射或涂覆方法。优选地,在磁体的2个对面上,真空蒸镀、磁控溅射或涂覆等量的R2元素。优选地,所述扩散处理的真空度<10 -2Pa。优选地,所述扩散处理时先进行第一次升温后保温,然后急冷降温,再进行第二次升温和保温后,完成扩散处理。
- 权利要求1-5任一项所述钕铁硼磁体在嵌入式电机中的应用。
- 一种磁钢,其特征在于,所述磁钢中含有权利要求1-5任一项所述钕铁硼磁体。
- 一种嵌入式电机,其特征在于,所述电机含有权利要求1-5任一项钕铁 硼磁体和/或权利要求9所述的磁钢。
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP21814433.5A EP4156209A4 (en) | 2020-05-27 | 2021-05-24 | NDFEB MAGNET, PRODUCTION METHOD THEREOF AND APPLICATION THEREOF |
KR1020227042249A KR102670670B1 (ko) | 2020-05-27 | 2021-05-24 | NdFeB 자석 및 이의 제조 방법 및 응용 |
JP2022573291A JP7443570B2 (ja) | 2020-05-27 | 2021-05-24 | ネオジム鉄ボロン磁石及びその製造方法並びに応用 |
US17/999,989 US20230207165A1 (en) | 2020-05-27 | 2021-05-24 | Neodymium-iron-boron magnet, preparation method and use thereof |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202010464304.9 | 2020-05-27 | ||
CN202010464304.9A CN111653404B (zh) | 2020-05-27 | 2020-05-27 | 一种钕铁硼磁体及其制备方法和应用 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2021238867A1 true WO2021238867A1 (zh) | 2021-12-02 |
Family
ID=72348707
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/CN2021/095528 WO2021238867A1 (zh) | 2020-05-27 | 2021-05-24 | 一种钕铁硼磁体及其制备方法和应用 |
Country Status (6)
Country | Link |
---|---|
US (1) | US20230207165A1 (zh) |
EP (1) | EP4156209A4 (zh) |
JP (1) | JP7443570B2 (zh) |
KR (1) | KR102670670B1 (zh) |
CN (1) | CN111653404B (zh) |
WO (1) | WO2021238867A1 (zh) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2023216358A1 (zh) * | 2022-05-10 | 2023-11-16 | 江西金力永磁科技股份有限公司 | 一种低涡流损耗钕铁硼磁体 |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2023510819A (ja) * | 2020-01-21 | 2023-03-15 | 福建省長汀金龍希土有限公司 | R-Fe-B系焼結磁石及びその粒界拡散処理方法 |
CN111653404B (zh) * | 2020-05-27 | 2022-11-15 | 烟台正海磁性材料股份有限公司 | 一种钕铁硼磁体及其制备方法和应用 |
CN113035556B (zh) * | 2021-03-04 | 2022-12-20 | 江西金力永磁科技股份有限公司 | 一种磁体性能梯度分布的r-t-b磁体的制备方法 |
CN113096910B (zh) * | 2021-04-06 | 2022-11-25 | 江西金力永磁科技股份有限公司 | 一种性能呈梯度分布的片状磁体及其制备方法 |
CN113224862A (zh) * | 2021-06-11 | 2021-08-06 | 华域汽车电动系统有限公司 | 局部扩散电机磁钢 |
CN113593802A (zh) * | 2021-07-08 | 2021-11-02 | 烟台正海磁性材料股份有限公司 | 一种耐腐蚀、高性能钕铁硼烧结磁体及其制备方法和用途 |
CN115798853A (zh) * | 2022-11-30 | 2023-03-14 | 天津三环乐喜新材料有限公司 | 一种烧结钕铁硼磁体及其制备方法 |
CN117275928A (zh) * | 2023-11-23 | 2023-12-22 | 中科三环(赣州)新材料有限公司 | 一种多次增重多次扩散的晶界扩散方法 |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20040000359A1 (en) * | 2002-06-27 | 2004-01-01 | Nissan Motor Co., Ltd. | Rare earth magnet, method for manufacturing the same, and motor using rare earth magnet |
CN101939804A (zh) | 2008-12-04 | 2011-01-05 | 信越化学工业株式会社 | Nd基烧结磁体及其制造方法 |
CN105374486A (zh) * | 2015-12-08 | 2016-03-02 | 宁波韵升股份有限公司 | 一种高性能烧结钕铁硼磁体 |
CN105489369A (zh) * | 2015-12-29 | 2016-04-13 | 浙江东阳东磁稀土有限公司 | 一种提高钕铁硼磁体矫顽力的方法 |
CN106205992A (zh) * | 2016-06-28 | 2016-12-07 | 上海交通大学 | 高矫顽力及低剩磁温度敏感性的烧结钕铁硼磁体及制备 |
CN111653404A (zh) * | 2020-05-27 | 2020-09-11 | 烟台正海磁性材料股份有限公司 | 一种钕铁硼磁体及其制备方法和应用 |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP4702546B2 (ja) | 2005-03-23 | 2011-06-15 | 信越化学工業株式会社 | 希土類永久磁石 |
TWI413136B (zh) | 2005-03-23 | 2013-10-21 | Shinetsu Chemical Co | 稀土族永久磁體 |
JP2009088206A (ja) | 2007-09-28 | 2009-04-23 | Tdk Corp | 希土類磁石の製造方法 |
JP5209349B2 (ja) * | 2008-03-13 | 2013-06-12 | インターメタリックス株式会社 | NdFeB焼結磁石の製造方法 |
JP2010119190A (ja) | 2008-11-12 | 2010-05-27 | Toyota Motor Corp | 磁石埋め込み型モータ用ロータと磁石埋め込み型モータ |
JP2015228431A (ja) * | 2014-06-02 | 2015-12-17 | インターメタリックス株式会社 | RFeB系磁石及びRFeB系磁石の製造方法 |
CN109275334A (zh) | 2016-01-25 | 2019-01-25 | Ut巴特勒有限公司 | 具有选择性表面改性的钕-铁-硼磁体及其制造方法 |
CN106328367B (zh) | 2016-08-31 | 2017-11-24 | 烟台正海磁性材料股份有限公司 | 一种R‑Fe‑B系烧结磁体的制备方法 |
JP2018056188A (ja) | 2016-09-26 | 2018-04-05 | 信越化学工業株式会社 | R−Fe−B系焼結磁石 |
JP7251917B2 (ja) | 2016-12-06 | 2023-04-04 | Tdk株式会社 | R-t-b系永久磁石 |
DE102017222062A1 (de) | 2016-12-06 | 2018-06-07 | Tdk Corporation | Permanentmagnet auf R-T-B-Basis |
JP2018107928A (ja) | 2016-12-27 | 2018-07-05 | トヨタ自動車株式会社 | Ipmモータ用ロータ |
US11152142B2 (en) * | 2018-03-29 | 2021-10-19 | Tdk Corporation | R-T-B based permanent magnet |
US11527340B2 (en) * | 2018-07-09 | 2022-12-13 | Daido Steel Co., Ltd. | RFeB-based sintered magnet |
CN108831655B (zh) * | 2018-07-20 | 2020-02-07 | 烟台首钢磁性材料股份有限公司 | 一种提高钕铁硼烧结永磁体矫顽力的方法 |
-
2020
- 2020-05-27 CN CN202010464304.9A patent/CN111653404B/zh active Active
-
2021
- 2021-05-24 KR KR1020227042249A patent/KR102670670B1/ko active IP Right Grant
- 2021-05-24 WO PCT/CN2021/095528 patent/WO2021238867A1/zh unknown
- 2021-05-24 US US17/999,989 patent/US20230207165A1/en active Pending
- 2021-05-24 EP EP21814433.5A patent/EP4156209A4/en active Pending
- 2021-05-24 JP JP2022573291A patent/JP7443570B2/ja active Active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20040000359A1 (en) * | 2002-06-27 | 2004-01-01 | Nissan Motor Co., Ltd. | Rare earth magnet, method for manufacturing the same, and motor using rare earth magnet |
CN101939804A (zh) | 2008-12-04 | 2011-01-05 | 信越化学工业株式会社 | Nd基烧结磁体及其制造方法 |
CN105374486A (zh) * | 2015-12-08 | 2016-03-02 | 宁波韵升股份有限公司 | 一种高性能烧结钕铁硼磁体 |
CN105489369A (zh) * | 2015-12-29 | 2016-04-13 | 浙江东阳东磁稀土有限公司 | 一种提高钕铁硼磁体矫顽力的方法 |
CN106205992A (zh) * | 2016-06-28 | 2016-12-07 | 上海交通大学 | 高矫顽力及低剩磁温度敏感性的烧结钕铁硼磁体及制备 |
CN111653404A (zh) * | 2020-05-27 | 2020-09-11 | 烟台正海磁性材料股份有限公司 | 一种钕铁硼磁体及其制备方法和应用 |
Non-Patent Citations (1)
Title |
---|
See also references of EP4156209A4 |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2023216358A1 (zh) * | 2022-05-10 | 2023-11-16 | 江西金力永磁科技股份有限公司 | 一种低涡流损耗钕铁硼磁体 |
Also Published As
Publication number | Publication date |
---|---|
US20230207165A1 (en) | 2023-06-29 |
EP4156209A1 (en) | 2023-03-29 |
KR20230006556A (ko) | 2023-01-10 |
KR102670670B1 (ko) | 2024-05-29 |
JP7443570B2 (ja) | 2024-03-05 |
EP4156209A4 (en) | 2023-12-06 |
CN111653404A (zh) | 2020-09-11 |
JP2023527854A (ja) | 2023-06-30 |
CN111653404B (zh) | 2022-11-15 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
WO2021238867A1 (zh) | 一种钕铁硼磁体及其制备方法和应用 | |
CN111223624B (zh) | 一种钕铁硼磁体材料、原料组合物及制备方法和应用 | |
WO2021249159A1 (zh) | 重稀土合金、钕铁硼永磁材料、原料和制备方法 | |
EP3355319B1 (en) | Corrosion-resistant sintered neodymium-iron-boron magnet rich in lanthanum and cerium, and manufacturing method | |
CN111223627B (zh) | 钕铁硼磁体材料、原料组合物、制备方法、应用 | |
CN109585113A (zh) | 一种烧结钕铁硼磁体的制备方法 | |
CN113593882B (zh) | 2-17型钐钴永磁材料及其制备方法和应用 | |
CN111243807A (zh) | 一种钕铁硼磁体材料、原料组合物及制备方法和应用 | |
WO2021169889A1 (zh) | 钕铁硼磁体材料、原料组合物、制备方法、应用 | |
WO2023124688A1 (zh) | 钕铁硼磁体及其制备方法和应用 | |
CN111312461A (zh) | 一种钕铁硼磁体材料、原料组合物及制备方法和应用 | |
CN111223626B (zh) | 钕铁硼磁体材料、原料组合物、制备方法、应用 | |
WO2023001189A1 (zh) | 一种高性能烧结钕铁硼磁体及其制备方法 | |
CN112768170B (zh) | 一种稀土永磁体及其制备方法 | |
CN113871123A (zh) | 低成本稀土磁体及制造方法 | |
CN111223628B (zh) | 钕铁硼磁体材料、原料组合物、制备方法、应用 | |
EP4394809A1 (en) | High-remanence neodymium-iron-boron magnet, and preparation method therefor and use thereof | |
CN109243746A (zh) | 一种低温延时烧结而成的超细晶烧结永磁体及其制备方法 | |
US20220005637A1 (en) | Method for preparing high-performance sintered NdFeB magnets and sintered NdFeB magnets | |
CN114927302A (zh) | 稀土磁体及其制备方法 | |
CN113539600A (zh) | 一种高磁能积和高矫顽力的含Dy稀土永磁体及制备方法 | |
CN111210961A (zh) | 一种铈铁铝合金、含铈稀土永磁体及其制备方法 | |
CN117059357A (zh) | 晶粒中具有重稀土元素偏聚结构的钕铁硼稀土永磁体及其制备方法和应用 | |
CN114360831A (zh) | 一种磁性能一致性高的r-t-b系烧结磁体及其制备方法和应用 | |
CN116631760A (zh) | 一种提高含铈钕铁硼磁体重稀土扩散效率的方法 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 21814433 Country of ref document: EP Kind code of ref document: A1 |
|
ENP | Entry into the national phase |
Ref document number: 2022573291 Country of ref document: JP Kind code of ref document: A |
|
ENP | Entry into the national phase |
Ref document number: 20227042249 Country of ref document: KR Kind code of ref document: A |
|
NENP | Non-entry into the national phase |
Ref country code: DE |
|
ENP | Entry into the national phase |
Ref document number: 2021814433 Country of ref document: EP Effective date: 20221223 |