KR0128137B1 - Producing method of al-ni-co complex magnetic powder - Google Patents
Producing method of al-ni-co complex magnetic powderInfo
- Publication number
- KR0128137B1 KR0128137B1 KR1019940040092A KR19940040092A KR0128137B1 KR 0128137 B1 KR0128137 B1 KR 0128137B1 KR 1019940040092 A KR1019940040092 A KR 1019940040092A KR 19940040092 A KR19940040092 A KR 19940040092A KR 0128137 B1 KR0128137 B1 KR 0128137B1
- Authority
- KR
- South Korea
- Prior art keywords
- powder
- weight
- magnetic powder
- thermosetting resin
- alnico
- Prior art date
Links
- 239000006247 magnetic powder Substances 0.000 title claims abstract description 35
- 238000000034 method Methods 0.000 title claims description 13
- 229920005989 resin Polymers 0.000 claims abstract description 39
- 239000011347 resin Substances 0.000 claims abstract description 39
- 239000000843 powder Substances 0.000 claims abstract description 29
- 230000005291 magnetic effect Effects 0.000 claims abstract description 24
- 229910000828 alnico Inorganic materials 0.000 claims abstract description 22
- 229920001187 thermosetting polymer Polymers 0.000 claims abstract description 21
- 239000000956 alloy Substances 0.000 claims abstract description 10
- 238000010791 quenching Methods 0.000 claims abstract description 10
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 9
- 230000000171 quenching effect Effects 0.000 claims abstract description 8
- 239000006087 Silane Coupling Agent Substances 0.000 claims abstract description 6
- 239000002131 composite material Substances 0.000 claims description 10
- 238000004519 manufacturing process Methods 0.000 claims description 7
- WYTZZXDRDKSJID-UHFFFAOYSA-N (3-aminopropyl)triethoxysilane Chemical group CCO[Si](OCC)(OCC)CCCN WYTZZXDRDKSJID-UHFFFAOYSA-N 0.000 claims description 4
- 150000007933 aliphatic carboxylic acids Chemical class 0.000 claims description 4
- 229910017827 Cu—Fe Inorganic materials 0.000 claims description 3
- 229910011212 Ti—Fe Inorganic materials 0.000 claims description 3
- 238000011068 loading method Methods 0.000 claims description 3
- XDLMVUHYZWKMMD-UHFFFAOYSA-N 3-trimethoxysilylpropyl 2-methylprop-2-enoate Chemical compound CO[Si](OC)(OC)CCCOC(=O)C(C)=C XDLMVUHYZWKMMD-UHFFFAOYSA-N 0.000 claims description 2
- BPSIOYPQMFLKFR-UHFFFAOYSA-N trimethoxy-[3-(oxiran-2-ylmethoxy)propyl]silane Chemical compound CO[Si](OC)(OC)CCCOCC1CO1 BPSIOYPQMFLKFR-UHFFFAOYSA-N 0.000 claims description 2
- 229910000077 silane Inorganic materials 0.000 claims 2
- 238000004381 surface treatment Methods 0.000 abstract description 5
- 238000010298 pulverizing process Methods 0.000 abstract description 4
- -1 carbon ester Chemical class 0.000 abstract description 3
- 238000002156 mixing Methods 0.000 abstract description 3
- 238000000137 annealing Methods 0.000 abstract 2
- 229910052799 carbon Inorganic materials 0.000 abstract 1
- 239000013078 crystal Substances 0.000 abstract 1
- 239000007822 coupling agent Substances 0.000 description 12
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 10
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 10
- 238000001816 cooling Methods 0.000 description 10
- 238000010438 heat treatment Methods 0.000 description 9
- 239000000203 mixture Substances 0.000 description 9
- 235000019441 ethanol Nutrition 0.000 description 8
- 238000000465 moulding Methods 0.000 description 7
- MVLVMROFTAUDAG-UHFFFAOYSA-N ethyl octadecanoate Chemical compound CCCCCCCCCCCCCCCCCC(=O)OCC MVLVMROFTAUDAG-UHFFFAOYSA-N 0.000 description 6
- 230000032683 aging Effects 0.000 description 5
- 229910052782 aluminium Inorganic materials 0.000 description 5
- 229910052786 argon Inorganic materials 0.000 description 5
- 230000000694 effects Effects 0.000 description 5
- 239000003822 epoxy resin Substances 0.000 description 5
- 229920000647 polyepoxide Polymers 0.000 description 5
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 4
- 239000007789 gas Substances 0.000 description 4
- 238000000227 grinding Methods 0.000 description 4
- 239000002244 precipitate Substances 0.000 description 4
- 239000000243 solution Substances 0.000 description 4
- 230000008018 melting Effects 0.000 description 3
- 238000002844 melting Methods 0.000 description 3
- VLKZOEOYAKHREP-UHFFFAOYSA-N n-Hexane Chemical compound CCCCCC VLKZOEOYAKHREP-UHFFFAOYSA-N 0.000 description 3
- 239000002245 particle Substances 0.000 description 3
- 239000010453 quartz Substances 0.000 description 3
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N silicon dioxide Inorganic materials O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 3
- 239000002904 solvent Substances 0.000 description 3
- 238000002441 X-ray diffraction Methods 0.000 description 2
- 230000002411 adverse Effects 0.000 description 2
- 238000005266 casting Methods 0.000 description 2
- 238000001035 drying Methods 0.000 description 2
- 229910001004 magnetic alloy Inorganic materials 0.000 description 2
- 238000004663 powder metallurgy Methods 0.000 description 2
- 239000000047 product Substances 0.000 description 2
- 239000001149 (9Z,12Z)-octadeca-9,12-dienoate Substances 0.000 description 1
- WTTJVINHCBCLGX-UHFFFAOYSA-N (9trans,12cis)-methyl linoleate Natural products CCCCCC=CCC=CCCCCCCCC(=O)OC WTTJVINHCBCLGX-UHFFFAOYSA-N 0.000 description 1
- LNJCGNRKWOHFFV-UHFFFAOYSA-N 3-(2-hydroxyethylsulfanyl)propanenitrile Chemical compound OCCSCCC#N LNJCGNRKWOHFFV-UHFFFAOYSA-N 0.000 description 1
- 229910001158 Alnico 8 Inorganic materials 0.000 description 1
- LVGKNOAMLMIIKO-UHFFFAOYSA-N Elaidinsaeure-aethylester Natural products CCCCCCCCC=CCCCCCCCC(=O)OCC LVGKNOAMLMIIKO-UHFFFAOYSA-N 0.000 description 1
- 229910017061 Fe Co Inorganic materials 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- PKIXXJPMNDDDOS-UHFFFAOYSA-N Methyl linoleate Natural products CCCCC=CCCC=CCCCCCCCC(=O)OC PKIXXJPMNDDDOS-UHFFFAOYSA-N 0.000 description 1
- 239000004677 Nylon Substances 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- LVGKNOAMLMIIKO-QXMHVHEDSA-N ethyl oleate Chemical compound CCCCCCCC\C=C/CCCCCCCC(=O)OCC LVGKNOAMLMIIKO-QXMHVHEDSA-N 0.000 description 1
- 229940093471 ethyl oleate Drugs 0.000 description 1
- 230000005294 ferromagnetic effect Effects 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 230000004907 flux Effects 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 238000001746 injection moulding Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 229920001778 nylon Polymers 0.000 description 1
- 239000003960 organic solvent Substances 0.000 description 1
- 239000005011 phenolic resin Substances 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 229920005992 thermoplastic resin Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F1/00—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties
- H01F1/44—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of magnetic liquids, e.g. ferrofluids
- H01F1/442—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of magnetic liquids, e.g. ferrofluids the magnetic component being a metal or alloy, e.g. Fe
-
- 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
- H01F1/012—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials adapted for magnetic entropy change by magnetocaloric effect, e.g. used as magnetic refrigerating material
- H01F1/015—Metals or alloys
-
- 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
-
- 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
- H01F1/06—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 in the form of particles, e.g. powder
-
- 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
- H01F1/42—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of organic or organo-metallic materials, e.g. graphene
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Hard Magnetic Materials (AREA)
Abstract
Description
본 발명은 열경화성 수지자석용 알니코계 복합자성분말 제조방법에 관한 것으로, 보다 상세하게는 급속냉각법을 이용한 열경화성 수지자석용 알니코계 복합자성 분말 제조방법에 관한 것이다.The present invention relates to a method for producing alnico composite magnetic powder for thermosetting resin magnet, and more particularly, to a method for preparing alnico composite magnetic powder for thermosetting resin magnet using rapid cooling method.
종래 Al,Ni,Co,Cu,Fe 또는 Al,Ni,Co,Cu,Ti,Fe을 주요 성분으로 하는 알니코계 자성합금은 일반적으로 용해주조법(일본특허공개공보(소) 41-9284 및 (소)39-24213)으로 제조되어 왔으나, 경하고 취약한 알코니계 자석의 특성 때문에 절삭가공이 매우 곤란함으로, 소형의 복잡한 형상을 갖는 자석등은 분말야금법(일본특허공개공보(소)57-207101 및 (소) 61-127848)으로 제조하여 왔다. 그러나, 분말야금법도 아주 얇은 칫수나 복잡한 형상의 자석을 제조하는데는 한계가 있으며, 가격이 비싼 단점이 있는 것이다. 따라서 이러한 단점을 보완하기 위해 알니코계 자성분말을 바인더로 유기물 수지(이하 수지라 한다.)를 사용하여 원하는 형상으로 성형하는 알니코계 수지자석이 사용된다.Conventional alnico magnetic alloys containing Al, Ni, Co, Cu, Fe or Al, Ni, Co, Cu, Ti, Fe as the main components are generally melt casting methods (Japanese Patent Laid-Open No. 41-9284 and ( 39-24213), but the cutting process is very difficult due to the characteristics of the hard and fragile aluminum magnets. Therefore, the magnets having a small and complicated shape are made of powder metallurgy (Japanese Patent Laid-Open No. 57-24). 207101 and (small) 61-127848). However, powder metallurgy also has limitations in producing magnets of very thin dimensions or complex shapes, and has the disadvantage of being expensive. Therefore, to compensate for these disadvantages, an alnico resin magnet is used in which the alnico magnetic powder is molded into a desired shape using an organic resin (hereinafter referred to as a resin) as a binder.
상기 알니코계 수지자석(또는 본드자석이라 한다.)은 에폭시(epoxy)수지, 페놀(Phenol)수지등의 열경화성 수지를 사용하여 압축성형하거나, 나일론(Nylon)등의 열가소성 수지를 사용하여 사출성형함으로써 제조되고 있다.The alnico resin magnet (or bond magnet) is compression molded using a thermosetting resin such as epoxy resin or phenol resin, or injection molding using a thermoplastic resin such as nylon. It is manufactured by.
종래, 수지자석용 알니코계 자성분말은 원하는 조성의 배합원료를 유도용해하여 인곳트(ingot)를 제조한 후, 제조된 인곳트를 900-1300oC로 30-60분간 용체화 처리한 다음 650-950oC에서 자장중 연속냉각한다. 그후 다시 500-700oC에서 시효한 후 얻어진 열처리물을 조분쇄 및 미분쇄하여 제조하였다. 그러나 이 방법은 복잡하고 특히, 인곳트를 900-1300oC온도로 용체화 처리하여야 할 뿐만 아니라 분쇄하여 미분말로 제조하는 공정이 요구됨으로 비경제적이다.Conventionally, alnico-based magnetic powder for resin magnets is prepared by inducing and melting an ingredient of a desired composition to ingot (ingot), and then ingot-treated at 900-1300 o C for 30-60 minutes. Continuous cooling in a magnetic field at 650-950 ° C. After the aging at 500-700 o C again, the obtained heat-treated product was prepared by coarsely pulverizing and pulverizing. However, this method is complicated and economical, in particular, because the ingot must not only be solution-treated at 900-1300 ° C. but also needs to be pulverized and manufactured into fine powder.
이에, 본 발명의 목적은 저렴하고, 제조공정이 간단한(즉, 인곳트제조, 용체화처리 및 인곳트 분쇄공정을 필요로하지 않는) 수지자석용 알니코계 열가소성 복합자성분말 제조방법을 제공하는 것이다.Accordingly, an object of the present invention is to provide an alnico-based thermoplastic composite powder production method for resin magnets which is inexpensive and has a simple manufacturing process (that is, does not require ingot production, solution treatment, and ingot grinding process). will be.
본 발명에 의하면, Al-Ni-Co-Cu-Fe 또는 Al-Ni-Co-Cu-Ti-Fe을 주요 성분으로 수지자석용 알니코계 복합자성분말 제조방법에 있어서, 알니코계 합금을 미세결정질의 급냉형 분말로 형성되도록 급냉시킨 다음 미세분말로 분쇄하고 650-950oC온도에서 1-10KOe의 외부자장을 부여하면서 자장중에서 2-30분간 열처리한 후, 500-700oC에서 1-10시간동안 시효열처리하는 단계 상기 제조된 자성분말을 자성분말의 중량기준으로 0.5-2.0 중량%의 실란계 커플링제로 표면처리하는 단계 및 상기 표면처리된 자성분말에 지방족 카본산 에스테르 5-30중량%가 함유된 열경화성수지를 1-5중량%을 혼합하는 단계로 구성됨을 특징으로 하는 열경화성 수지자석용 알니코계 복합자성분말 제조방법이 제공된다.According to the present invention, Al-Ni-Co-Cu-Fe or Al-Ni-Co-Cu-Ti-Fe as the main component in the manufacturing method of alnico composite magnetic powder for resin magnets, the alnico alloy is fine and then ground to a fine powder and then quenched by rapid cooling to form a crystalline powder of the type and 650-950 o C and a temperature giving an external magnetic field of 1-10KOe from 2-30 minutes in a magnetic field heat treatment at 500-700 o C l Aging heat treatment for 10 hours Surface treatment of the prepared magnetic powder with 0.5-2.0% by weight of silane coupling agent based on the weight of the magnetic powder and 5-30 weight of aliphatic carboxylic acid ester in the surface-treated magnetic powder Provided is a method for preparing alnico composite powder for thermosetting resin magnets, characterized in that the composition comprises 1-5% by weight of thermosetting resin containing%.
이하, 본 발명에 대하여 상세히 설명한다.EMBODIMENT OF THE INVENTION Hereinafter, this invention is demonstrated in detail.
본 발명의 방법에 의하면 Al-Ni-Co-Cu-Fe 또는 Al-Ni-Co-Cu-Ti-Fe을 주요 성분으로 하는 알니코계 합금을 급냉함으로써 종래방법에서 요구되는 인곳트 제조, 용체화처리 및 인곳트 분쇄공정을 거치지 않고 직접 알니코계 합금분말을 제조할 수 있다.According to the method of the present invention, the ingot preparation and solution, which are required in the conventional method, are rapidly cooled by quenching an alnico alloy containing Al-Ni-Co-Cu-Fe or Al-Ni-Co-Cu-Ti-Fe as a main component. Alnico alloy powder can be produced directly without treatment and ingot grinding process.
상기 분말제조시에는 대한민국 특허 제 48371에 개시된 급속냉각기를 사용하여 축출형 용융 회전법에 따라 용융상태의 알니코계 합금을 급냉시켜 미세결정질(1-30um)의 급속냉각형 분말로 제조할 수 있다.When the powder is manufactured, by using the rapid cooler disclosed in Korean Patent No. 48371, rapid cooling of the molten alnico alloy in a molten state according to the ejection type melt rotation method may be made into a microcrystalline (1-30um) rapid cooling powder. .
이때 상기 급속 냉각기의 회전체 선속도가 6m/sec 이하인 경우에는 용융상태의 합금을 축출해주는 힘이 약하여 분말을 얻기 어렵고 선속도가 40m/sec 이상이 되어도 무관하지만, 작업상 문제로 인하여 회전체 속도를 6-40m/sec로 하는 것이 바람직하다.At this time, when the linear velocity of the rotor of the rapid cooler is 6 m / sec or less, the force for discharging the alloy in the molten state is weak, so that it is difficult to obtain powder and the linear velocity may be higher than 40 m / sec. It is preferable to make 6-40 m / sec.
상기한 바와같이 급냉하여 제조된 분말은 단섬유(flake)형태로 취성이 매우 커 쉽게 분쇄된다. 따라서 헥산, 아세톤, 알코올 등과 같은 유기용매나 공기중에서 통상의 분쇄과정에 의해 용이하게 250메쉬이하의 입도로 제조할 수 있다.As described above, the powder prepared by quenching is easily pulverized in the form of flakes and very brittle. Therefore, it can be easily prepared to a particle size of less than 250 mesh by a conventional grinding process in an organic solvent such as hexane, acetone, alcohol or the like.
그후, 상기 분쇄된 급냉분말을 진공 석영관에 충진한 다음 아르곤 또는 수소 분위기하에서, 650-950oC의 온도구간에서 1-10KOe의 외부자장을 부하하면서 2-30분간 자장내에서 열처리한다.Thereafter, the pulverized quench powder was filled in a vacuum quartz tube and then heat-treated in a magnetic field under an argon or hydrogen atmosphere for 2-30 minutes while loading an external magnetic field of 1-10 KOe at a temperature range of 650-950 ° C.
위와같이 자장중에서 열처리함으로써 열처리도중 알니코계 자성합금재료내에서 석출되는 Fe-Co계 조성의 석출물(강자기 특성을 나타낸다.)의 양이 증대되고, 석출되는 동안 방향성 있게 일정한 배열로 성장된다.By heat treatment in the magnetic field as described above, the amount of the Fe-Co-based precipitate (which exhibits the ferromagnetic property) precipitated in the alnico magnetic alloy material during the heat treatment is increased and grows in a directionally constant arrangement during precipitation.
자장중에서 2분 이하로 열처리하면 석출물이 완전히 생성되지 않아 자기특성이 저하되고, 30분 이상 열처리하면 석출물이 조대해져 자기특성이 저하됨으로 2-30분간 자장처리하는 것이 바람직하다.If the heat treatment for 2 minutes or less in the magnetic field does not completely produce a precipitate, the magnetic properties are lowered. If the heat treatment for 30 minutes or more, the precipitate is coarse and the magnetic properties are lowered.
상기 열처리 후, 500-700oC로 1-10시간동안 시효처리한다. 시효처리시 온도가 500oC이하인 경우에는 그 효과가 충분하지 않고, 700oC이상인 경우에는 석출물이 성장하여 자장처리 효과가 감소함으로 500-700℃에서 시효처리하는 것이 바람직하다.After the heat treatment, aged at 500-700 o C for 1-10 hours. When the temperature is less than 500 o C at the time of aging treatment, the effect is not sufficient, and when it is above 700 o C, it is preferable that the aging treatment is performed at 500-700 ° C. as the precipitate grows and the magnetic field treatment effect is reduced.
그후, 상기 제조된 자성분말을 커플링제(Coupling agent)로 표면처리한다. 표면처리함으로써, 자성분말에 윤활성이 부여되고, 분산성 및 성형가공성이 향상되며, 수지자석의 자기적 특성 및 기계적강도가 개선된다.Thereafter, the prepared magnetic powder is surface treated with a coupling agent. By surface treatment, lubricity is imparted to the magnetic powder, dispersibility and molding processability are improved, and magnetic properties and mechanical strength of the resin magnet are improved.
상기 커플링제로는 통상의 커플링제를 사용할 수 있으나 γ-아미노프로필트리에톡시실란(gamma-amino propyltriethoxy silane), γ-글리시톡시프로필트리메톡시실란(gamma-glycidoxypropyl trimethoxy silane), 및 γ-메타크릴옥시프로필트리메톡시실란(gamma-methacryloxypropyl trimethoxy silane)으로 구성되는 그룹으로부터 선택된 실란계 커플링제를 사용하는 것이 바람직하다.As the coupling agent, a conventional coupling agent may be used, but gamma-amino propyltriethoxy silane, gamma-glycidoxypropyl trimethoxy silane, and gamma- Preference is given to using a silane coupling agent selected from the group consisting of methacryloxypropyl trimethoxy silane.
상기 커플링제는 자성분말에 자성분말의 중량기준으로 0.5-2.0중량%으로 첨가된다.The coupling agent is added to the magnetic powder at 0.5 to 2.0% by weight based on the weight of the magnetic powder.
첨가량이 0.5중량%이하인 경우에는 커플링제 처리효과가 불충분하고, 2.0중량% 이상인 경우에는 미반응 커플링제가 남게되어 잔류자속밀도를 감소시키는 등의 악영향을 나타내기 때문이다.This is because when the added amount is 0.5% by weight or less, the effect of treating the coupling agent is insufficient, and when it is 2.0% by weight or more, the unreacted coupling agent is left, resulting in adverse effects such as reducing the residual magnetic flux density.
살란계 커플링제로 자성분말을 표면처리하는 경우, 실란계 커플링제가 액상이므로 그대로 직접 혼합할 수 있으나, 알코올 및 아세톤과 같은 용매를 사용하여 혼합하는 것이 자성분말에 균일하게 피복되므로 바람직하며, 상기 표면처리는 실온 혹은 100℃미만에서 행하는 것이 보통이다.In the case of surface treatment of the magnetic powder with a sallan-based coupling agent, since the silane coupling agent is liquid, it can be directly mixed as it is, but mixing using a solvent such as alcohol and acetone is preferable since it is uniformly coated on the magnetic powder. Surface treatment is usually carried out at room temperature or below 100 ° C.
마지막으로 상기 커플링제로 표면처리된 자성분말에 지방족 에스테르가 함유된 열경화성 수지를 첨가, 혼합하여 열경화성 수지자석용 알니코계 복합자성분말을 제조한다.Finally, a thermosetting resin containing an aliphatic ester is added to the magnetic powder surface-treated with the coupling agent and mixed to prepare an alnico composite powder for thermosetting resin magnets.
상기 열경화성 수지에 지방족 카본산 에스테르를 첨가함으로써 자성분말과 수지간의 마찰 및 수지내부의 극성기(dipole)간에 발생되는 상호작용이 감소됨으로 자성분말의 충진량이 증가되어 자기적 특성이 개선된다.By adding an aliphatic carboxylic acid ester to the thermosetting resin, friction between the magnetic powder and the resin and interaction between the polar groups in the resin are reduced, so that the amount of the magnetic powder is increased to improve the magnetic properties.
상기 열경화성 수지에 첨가되는 지방족 카본산 에스테르로는 스테아린산 에틸, 올레인산 에틸, 리놀산 메틸등이 사용되며, 열경화성수지 100중량%에 대한 첨가량이 5중량% 이하인 경우에는 그 효과가 미비하며, 30 중량% 이상인 경우에는 오히려 자기적 특성에 악영향을 끼침으로 5-30중량% 첨가하는 것이 바람직하다.As the aliphatic carboxylic acid ester added to the thermosetting resin, ethyl stearate, ethyl oleate, methyl linoleate, and the like are used. When the amount of the thermosetting resin is added in an amount of 5% by weight or less, the effect is insignificant, and 30% by weight or more. In this case, it is preferable to add 5-30% by weight, adversely affecting the magnetic properties.
상기 열경화성수지로는 통상 사용되는 열경화성 수지를 사용할 수 있으며, 에폭시 수지가 보편적으로 사용된다.As the thermosetting resin, a thermosetting resin generally used may be used, and an epoxy resin is generally used.
상기 표면처리된 사정분말에 대한 지방족 에스테르가 함유된 열경화성 수지의 첨가량이 자성분말의 중량기준으로 5중량% 이상인 경우에는 수지의 양이 너무 많아 자기적 특성이 감소되며, 1중량% 이하인 경우에는 수지자석의 강도가 저하됨으로 1-5중량% 첨가하는 것이 바람직하다.When the amount of the thermosetting resin containing the aliphatic ester to the surface-treated ejaculate powder is 5% by weight or more based on the weight of the magnetic powder, the amount of the resin is too large and the magnetic properties are reduced. It is preferable to add 1-5% by weight since the strength of the magnet is lowered.
상기한 바와같이 제조된 복합자성분말을 성형, 경화시켜 수지자석을 제조한다. 상기 성형시, 성형압이 1ton/cm2이하인 경우에는 성형압이 낮아 강도를 유지하기 어렵고, 10ton/cm2이상인 경우에는 성형압이 높아 금형이 심하게 손상됨으로 1-10ton/cm2의 성형압으로 성형하여 성형체를 제조하는 것이 바람직하며, 상기 성형체를 진공드라이 오븐에서 120-180oC로 1-4시간 가열함으로써 경화시켜 수지자석을 제조한다. 상기 제시된 경화온도 및 시간은 에폭시수지가 완전히 3차원적인 망상구조를 갖도록 적절한 범위로 조절가능한 것이다.The composite magnetic powder prepared as described above is molded and cured to produce a resin magnet. When the molding is severely damaged by the mold increase the molding pressure not less than the molding pressure is 1ton / cm 2, the molding pressure is low, it is difficult to maintain the strength, 10ton / cm 2 or less, the molding pressure of 1-10ton / cm 2 It is preferable to form a molded body by molding, and the molded body is cured by heating at 120-180 ° C. for 1-4 hours in a vacuum dry oven to prepare a resin magnet. The curing temperature and time set forth above are adjustable in an appropriate range so that the epoxy resin has a completely three-dimensional network.
이하, 본 발명의 실시예에 대하여 상세히 설명한다.Hereinafter, embodiments of the present invention will be described in detail.
[실시예 1]Example 1
Al, Ni, Co, Cu, Fe 인곳트(ingot)를 8중량%(이하 %라 한다). Al-14%Ni-24%Co-3%Cu-51%Fe 조성의 알니코 5계 조성으로 칭량한후 아르곤(Ar) 가스 분위기하에서 플라즈마이크로 완전 용융한 다음 축출형 용융회전기로 단섬유(flake)형상의 급냉분말을 제조하였으며 이 때의 냉각속도, 즉 냉각회전체의 회전 선속도는 8.5-32.7 m/sec로 변화시켰다.Al, Ni, Co, Cu and Fe ingots are 8% by weight (hereinafter referred to as%). Al-14% Ni-24% Co-3% Cu-51% Fe composition is weighed in an Alnico 5-based composition and completely melted by plasma in an argon (Ar) gas atmosphere, followed by flakes with an ejection melting rotor. ) Quenching powder was prepared and the cooling speed at this time, that is, the linear linear velocity of the cooling rotor was changed to 8.5-32.7 m / sec.
상기와 같이 제조된 급냉분말에 대하여 x-선 회절분석 및 평균결정입도를 측정하였으며, 그 결과를 하기표1에 나타내었다.X-ray diffraction analysis and average grain size of the quench powder prepared as described above were measured, and the results are shown in Table 1 below.
하기 표 1에서 알 수 있는 바와 같이, 모두 결정질 조직으로 나타났다.As can be seen in Table 1 below, all appeared crystalline tissue.
상기와 같이 제조된 각각의 급냉분말을 알콜용매에서 아트리터(attritor)를 사용하여 분쇄한후 60메쉬(mesh)의 ASTM E11에서 규정한 체(sieve)를 사용하여 분급하여 입도가 250 마이크로미터 이하인 분말을 얻었다. 이들 분말을 석영관에 충진한 후 아르곤 가스 분위기하에서 650-900 C 온도구간에서 7KOe 의 외부자장을 부하하면서 냉각한 후, 600 C에서 4시간 시효처리하여 자성분말을 얻었다 커플링제로 γ-아미노프로필 트리에톡시실란 0.5중량%를 에틸 알코올에 희석시킨후, 이에 자성분말을 함침하고, 자성분말 표면에 골고루 묻도록 교반한 후, 건조시켜 알코올을 제거함으로써 자성분말 표면을 처리하였다.Each quenched powder prepared as described above was pulverized using an attritor in an alcohol solvent and classified using a sieve specified in ASTM E11 of 60 mesh to have a particle size of 250 micrometers or less. A powder was obtained. These powders were filled in quartz tubes and then 650-900 under argon gas atmosphere. After cooling with load of 7 KOe magnetic field in temperature range, 600 After aging at C for 4 hours to obtain a magnetic powder, 0.5 wt% of γ-aminopropyl triethoxysilane was diluted in ethyl alcohol as a coupling agent. The magnetic powder surface was treated by drying to remove alcohol.
상기 커플링제로 표면처리된 자성분말 97.5중량%와 스테아린산 에틸 20중량%가 함유된 에폭시수지 2.5중량%를 혼합한 다음, 혼함물을 8ton/㎠로 압축성형하고 제조된 성형체를 진공 드라이 오븐에서 150 C로 1시간 경화처리하여 수지자석을 제조하였다. 이들 수지자석에 대한 자기특성을 측정하고 그 결과를 하기 표 2에 나타내었다.After mixing 97.5% by weight of the magnetic powder surface treated with the coupling agent and 2.5% by weight of epoxy resin containing 20% by weight of ethyl stearate, the mixture was compression-molded at 8 ton / cm 2 and the produced molded product was dried in a vacuum dry oven. Curing treatment with C for 1 hour to prepare a resin magnet. Magnetic properties of these resin magnets were measured and the results are shown in Table 2 below.
[실시예 2]Example 2
Al, Ni, Co, Cu, Ti, Fe 인곳트를 하기 표3의 조성을 갖는 알니코 8계 합금 조성으로 칭량한 후 아르곤 가스 분위기하에서 플라즈마 아크로 완전 용융한 다음 축출형 용융회전기로 단섬유 형상의 급냉분말을 제조하였으며, 이때의 냉각속도, 즉 냉각회전체의 회전속도는 8.51 m/sec 로 하였다.Al, Ni, Co, Cu, Ti, Fe ingots were weighed with an Alnico 8-based alloy composition having the composition shown in Table 3, followed by complete melting with a plasma arc in an argon gas atmosphere, followed by quenching in a short fiber shape with an ejection melt rotor. Powder was prepared and the cooling speed at this time, that is, the rotation speed of the cooling rotor was 8.51 m / sec.
상기와 같이 제조된 급냉분말에 대하여 X-선 회절분석을 행한 결과 모두 결정질 조직으로 나타났으며 하기 표 3에 용해된 합금의 조성을 나타내었다.X-ray diffraction analysis of the quenched powder prepared as described above showed all crystalline structures, and the composition of the alloy dissolved in Table 3 below.
상기와 같이 제조된 각각의 급냉분말을 알콜용매에서 아트리터(attritor)를 사용하여 분쇄한 후 60 메쉬(mesh)의 ASTM E11에서 규정한 체(sieve)를 사용하여 분급함으로써 입도가 250um이하인 분말을 얻었다 이들 분말을 석영관에 충전한 후 아르곤 가스 분위기하에서 780-840 C 온도에서 7KOe의 외부자장을 부하하면서 10분간 등온자장 열처리한 후, 600 C에서 10시간 시효처리하여 자성분말을 얻었다. 커플링제로서 γ-아미노 프로필 트리에톡시실란 0.5중량%를 에틸알콜(ethyl alcohol)에 희석시킨후, 자성분말을 함침시켜 자성분말 표면에 골고루 묻도록 교반한 다음, 건조 시켜 알콜을 제거함으로써 자성분말을 표면 처리 하였다.Each quenched powder prepared as described above was pulverized in an alcohol solvent using an attritor and then classified using a sieve defined in ASTM E11 of 60 mesh to obtain a powder having a particle size of 250 μm or less. These powders were charged in a quartz tube and then 780-840 under argon gas atmosphere. After isothermal magnetic field heat treatment for 10 minutes while loading 7 KOe magnetic field at C temperature, 600 Aged at C for 10 hours to obtain magnetic powder. 0.5 wt% of γ-amino propyl triethoxysilane as a coupling agent was diluted in ethyl alcohol, and then impregnated with magnetic powder to stir evenly on the surface of the magnetic powder, followed by drying to remove alcohol. Was surface treated.
상기 커플링제로 표면처리된 각 자성분말 97.5중량%와 스테아린산 에틸 20중량%가 함유된 에폭시수지 2.5중량%를 혼합한 다음, 혼합물을 8ton/cm 로 압축성형하고 제조된 성형체를 진공 드라이 오븐에서 150 C로 1시간 경화처리하여 수지자석을 제조하였다. 이들 수지자석에 대한 자기적 특성을 측정하고 그 결과를 하기 표 4에 나타내었다.97.5% by weight of each magnetic powder surface-treated with the coupling agent and 2.5% by weight of epoxy resin containing 20% by weight of ethyl stearate were mixed, and then the mixture was 8 ton / cm. Molded and molded in a vacuum dry oven Curing treatment with C for 1 hour to prepare a resin magnet. Magnetic properties of these resin magnets were measured and the results are shown in Table 4 below.
상기 표 2와 4에 나타난 바와같이 본 발명에 따라 제조된 열경화성 수지자석이 종래의 주조법으로 제조한 인곳트를 분쇄한 분말을 사용한 열경화성 수지자석에 비하여 자기적 특성이 비슷하며, 용체화 처리가 불필요하고 분쇄가 용이하여 저렴하고 단순한 공정으로 열경화성 수지자석용 알니코계 복합자성분말을 제조할 수 있음을 알 수 있다.As shown in Tables 2 and 4, the thermosetting resin magnets prepared according to the present invention have similar magnetic properties as compared to the thermosetting resin magnets obtained by pulverizing the ingot prepared by the conventional casting method, and do not require solution treatment. And it can be seen that the alnico-based composite powder for thermosetting resin magnets can be manufactured in an inexpensive and simple process due to easy grinding.
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JP2000348918A (en) * | 1999-06-02 | 2000-12-15 | Seiko Epson Corp | Rare earth bonded magnet, composition for bonded rare earth magnet, and method for manufacturing rare earth bonded magnet |
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