JPS648455B2 - - Google Patents
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- Publication number
- JPS648455B2 JPS648455B2 JP55181751A JP18175180A JPS648455B2 JP S648455 B2 JPS648455 B2 JP S648455B2 JP 55181751 A JP55181751 A JP 55181751A JP 18175180 A JP18175180 A JP 18175180A JP S648455 B2 JPS648455 B2 JP S648455B2
- Authority
- JP
- Japan
- Prior art keywords
- crystals
- alloy
- magnet
- columnar
- crystal
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 239000013078 crystal Substances 0.000 claims description 75
- 229910045601 alloy Inorganic materials 0.000 claims description 33
- 239000000956 alloy Substances 0.000 claims description 33
- 239000000203 mixture Substances 0.000 claims description 20
- 239000000843 powder Substances 0.000 claims description 6
- 229910052761 rare earth metal Inorganic materials 0.000 claims description 5
- 150000002910 rare earth metals Chemical class 0.000 claims description 4
- 239000011230 binding agent Substances 0.000 claims description 3
- 229910052735 hafnium Inorganic materials 0.000 claims description 2
- 238000004898 kneading Methods 0.000 claims description 2
- 238000000465 moulding Methods 0.000 claims description 2
- 229910052758 niobium Inorganic materials 0.000 claims description 2
- 229910052715 tantalum Inorganic materials 0.000 claims description 2
- 229910052719 titanium Inorganic materials 0.000 claims description 2
- 229910052720 vanadium Inorganic materials 0.000 claims description 2
- 229910052726 zirconium Inorganic materials 0.000 claims description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 19
- 238000004519 manufacturing process Methods 0.000 description 12
- 238000005266 casting Methods 0.000 description 10
- 230000007423 decrease Effects 0.000 description 10
- 238000000034 method Methods 0.000 description 8
- 150000001875 compounds Chemical class 0.000 description 6
- 229910052751 metal Inorganic materials 0.000 description 6
- 239000002184 metal Substances 0.000 description 6
- 229920005989 resin Polymers 0.000 description 5
- 239000011347 resin Substances 0.000 description 5
- 229910017086 Fe-M Inorganic materials 0.000 description 4
- 229910052742 iron Inorganic materials 0.000 description 4
- 230000005415 magnetization Effects 0.000 description 4
- 238000002425 crystallisation Methods 0.000 description 3
- 230000008025 crystallization Effects 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- 229910052777 Praseodymium Inorganic materials 0.000 description 2
- 230000032683 aging Effects 0.000 description 2
- 210000002257 embryonic structure Anatomy 0.000 description 2
- 239000003822 epoxy resin Substances 0.000 description 2
- 239000006247 magnetic powder Substances 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 229920000647 polyepoxide Polymers 0.000 description 2
- 239000002244 precipitate Substances 0.000 description 2
- 239000000047 product Substances 0.000 description 2
- 238000007711 solidification Methods 0.000 description 2
- 230000008023 solidification Effects 0.000 description 2
- WZFUQSJFWNHZHM-UHFFFAOYSA-N 2-[4-[2-(2,3-dihydro-1H-inden-2-ylamino)pyrimidin-5-yl]piperazin-1-yl]-1-(2,4,6,7-tetrahydrotriazolo[4,5-c]pyridin-5-yl)ethanone Chemical compound C1C(CC2=CC=CC=C12)NC1=NC=C(C=N1)N1CCN(CC1)CC(=O)N1CC2=C(CC1)NN=N2 WZFUQSJFWNHZHM-UHFFFAOYSA-N 0.000 description 1
- 229910000531 Co alloy Inorganic materials 0.000 description 1
- 229910020637 Co-Cu Inorganic materials 0.000 description 1
- 229910003321 CoFe Inorganic materials 0.000 description 1
- 229910052772 Samarium Inorganic materials 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 239000012300 argon atmosphere Substances 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 230000002860 competitive effect Effects 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000005347 demagnetization Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- -1 heat treatment Substances 0.000 description 1
- 229910001004 magnetic alloy Inorganic materials 0.000 description 1
- 239000000696 magnetic material Substances 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000006911 nucleation Effects 0.000 description 1
- 238000010899 nucleation Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 238000005191 phase separation Methods 0.000 description 1
- 238000004881 precipitation hardening Methods 0.000 description 1
- 229910000938 samarium–cobalt magnet Inorganic materials 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 229910002058 ternary alloy Inorganic materials 0.000 description 1
- 238000009827 uniform distribution Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F1/00—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties
- H01F1/01—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials
- H01F1/03—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity
- H01F1/032—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
- H01F1/0555—Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5 pressed, sintered or bonded together
- H01F1/0558—Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5 pressed, sintered or bonded together bonded together
Landscapes
- Chemical & Material Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Inorganic Chemistry (AREA)
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Hard Magnetic Materials (AREA)
Description
本発明は、微粉末結合型の希土類永久磁石に関
する。
本発明の希土類永久磁石の製造方法を第1図に
示す。この磁石の磁気性能は、合金組成、熱処
理、粉末の粒度ならびに形状、バインダーの種
類、成形法などにより左右されることが以前から
知られていたが、今回新たに鋳造インゴツトのマ
クロ組織により、磁気性能が大きく変化すること
を見出した。
Sm−Pr−Co−Cu−Fe−M合金を使用した磁
石は、析出硬化型あるいは、2相分離型磁石の範
ちゆうに入る。これは、マトリツクス中に異相を
析出させて、磁気硬化させるためである。本系統
の磁石は、最初Sm−Co−Cuの3元系合金で、主
にSm2Co17結晶を用いた組成で磁石化されて以
来、今日広く発展してきたものである。CoをFe
と置換してゆくと、ある量まで飽和磁化4πIsが増
加することが知られている。4πIsが増大する範囲
でしかも、結晶が一軸異方性を示すのは、Sm2
(Co1-xFex)17で示すと、Xが0〜0.6の範囲であ
る。この事実はCoにCuをある程度の量を置換し
ても変らない。Sm2(CoCuFe)17にさらに、Mを
加えるとMの量は微量でもたいへん磁気性能の向
上がはかれる。すなわち、Mを加えると、Cuの
量が少くなつてもまた鉄の量が多くなつても、実
用磁石として充分なiHcが得られ高エネルギー積
の磁石の作製が可能になつた。Smの一部をPrで
置換すると、Pr2Co17結晶はSm2Co17G結晶より、
4πIsが高いので、高エネルギー積の磁石を得るこ
とが可能になる。また、希土類元素の資源の確保
の観点から言つても、SmとPrの両方を使用する
ことができるので、利点になる。しかしながら、
Smの一部をPrで置換してゆくと、4πIsは上昇す
るけれど結晶異方性が減少するので、異方性磁場
Haは小さくなる。Haが低下すれば、保磁力iHc
も必然的に低下する。それ故、本発明の目的の一
つは、Sm−Co−Cu−Fe−M系合金のSmをPrで
置換したことによるiHcの低下を、インゴツトを
柱状晶化することにより防ぐことにある。他の目
的は、Cuをさらに少くし、Feをさらに高めても
実用磁石として充分なiHcを柱状晶化することに
より得ることにある。
一般に溶融金属が、るつぼから鋳型に注入され
ると、鋳壁から凝固が開始する。これは、固体異
物質と接触したエンブリオ(晶芽)は、接触しな
いで溶液中に漂つているものに比べて、安定核生
成に対するエネルギー障壁が小さくなるからと説
明されている。鋳壁に生成した結晶は、隣の結晶
と相互に競争しつつ溶湯中に成長する。第3図に
示すような、鋳塊最外層の結晶の競争成長領域を
チル晶帯と呼んでいる。結晶は成長速度に異方性
があるため、最大成長速度をもつ方向が熱流の方
向に平行であるような結晶が、隣接の結晶成長を
抑えて優先的に成長する。結晶の成長中、優先方
位が熱流に近い程長く生き残り、他の結晶は淘汰
される結果、結晶の数は鋳塊内部にゆくに従つて
少くなり、柱状晶帯が形成される。条件が整えば
柱状晶帯がぶつかり合い凝固は完了するが、通常
第3図に示すように、柱状晶の内部に等軸晶が生
成する。等軸晶の生因については、以前はよく知
られていなかつたが、現在では鋳壁とか冷却され
た湯面で形成された結晶が遊離して自由晶とな
り、この自由晶が等軸晶帯を形成することが明ら
かになつている(A.Ohno、T.Motegi and H.
Soda:Trans.ISIJ.11(1971)18)。
本系のSm−Pr−Co−Cu−Fe−M合金でも、
前述したように、チル晶帯、柱状晶帯、等軸晶帯
のうちでは柱状晶帯が磁石にするのに最もすぐれ
ていることが明らかになつた。チル晶も等軸チル
晶と柱状チル晶では、柱状チル晶の方がすぐれて
いる。今、例を樹脂結合型希土類コバルト磁石に
とつて説明する。この磁石は第1図に示すような
方法で磁石合金を磁石にする。製法を全く同じに
して、等軸晶合金と柱状晶合金そしてチル晶合金
を磁石にしてみると、柱状晶合金が、飽和磁化
4πIs、保磁力iHc、bHcあるいはヒステリシスル
ープの角形性にと、全ての性能にわたつてすぐれ
ていることが分つた。逆に、等軸晶合金および等
軸チル晶合金が性能的に一番劣つている。柱状チ
ル晶合金からは、これらのものの中間の値の磁石
ができる。これは、柱状晶組成が、該合金を熱処
理(溶体化処理および時効処理)する時に有効に
作用するためであると考えられる。すなわち、柱
状晶によつてマトリツクス中に析出する異相の析
出物の分布の均一化を促進するものと考えられ、
そのためにヒステリシスの角形性がよくなる。ま
た同時に析出物の結晶構造、形態もiHcを高める
方向に形成する作用も及ぼすものと考えられ、そ
のためiHcも向上する。
このため、本合金を鋳壁近傍のチル晶体は柱状
チル晶にして、他の部分は柱状晶にする製造法が
よい磁石を得るために大切である。チル晶帯は合
金全体では量が少いので、製造上最も大切なこと
は、等軸晶帯を防ぎ柱状晶帯の比率を大きくする
ことにあるのである。また、組成的には柱状晶化
によつて最も効果が期待されるのは、原子比を用
いた組成が、
Sm1-xPrx(Co1-u-v-wCuuFevMw)z
(但し、0<x<0.5
0<u<0.2
0<v<0.5
0<w<0.1
6.5≦z<9.0
MはTi、Zr、Hf、V、Nb、Taのうちの少な
くとも1種からなる元素を示す。)
で表わされる合金である。
それでは以下に成分と組成域を限定した理由を
述べる。
本合金系およびその組成域においては、Sm−
Co系が基本である。CuはSm2Co17型合金で保磁
力を得るために加えられるものであり、Cuを入
れることでiHcは向上する。しかし、4πIは低下
する。このため、実用磁石材料としては、組成式
中のuの値はu<0.2が望ましい。またFeを加え
ることにより、4πIsが向上するが、あまり多くな
るとiHcが著しく低下するため、組成式中のvの
値はv<0.5が望ましい。zの値が5z8.5の
間にある時には、Sm−Co合金はSmCo5型化合物
とSm2Co17型化合物に分離する。4πIsの値は、
Sm2Co17の方が20%高い。依つて、高4πIsを実現
するためには、zは6.5以上が望ましい。一方z
が9.0以上になると、iHcは著しく低下するととも
に、Co−Fe相が多く出て来てしまいヒステリシ
スループの角形性を悪くするので好ましくない。
また、Pr2Co17化合物は、Sm2Co17化合物よりも
4πIsの値は大きいけれど、結晶磁気異方性定数
K1は負であり、Pr2Co17のままでは一軸異方性を
利用した磁石は作製できない。ゆえに、K1が正
で大きいSm2Co17型化合物と4πIsの大きい
Pr2Co17型化合物を複合させて磁石にすることは、
4πIsが大きくてしかもある程度iHcの高い磁石を
得るのに有効な方法である。このためにはSm1-x
Prx(CoCuFe)z組成において、x<0.5が実用材料
としては望ましい。それ以上xの値が大きいと、
iHcが足らなくなる。wを0.1未満にしたのは、M
は著しく合金の4πIsを低下させるので、0.1以上
入れると、Feを増やし、Cuを低減し、Prを入れ
たりして4πIsを高めた意味がなくなるからであ
る。Mは単独で用いるだけでなく、2種以上を複
合して加えても良い。
前述のように、鋳造時の結晶状態によりインゴ
ツトの磁気的性能は著しく変る。この事実を最も
よく利用することのできる磁石製造法は、微粉末
結合型磁石である。何故ならば、該磁石を製造す
るのには第1図に示すような工程を取るので、熱
処理は全てインゴツト状態で行い、磁気硬化させ
た後で粉砕してバインダーで結合する。それ故、
磁気硬化後のインゴツトを切り出して所望の形の
磁石を作製することもできる。粉砕前までの工程
は、鋳造磁石と変らない。このような製造工程を
用いるため、焼結法と較べてインゴツトの結晶状
態が大いに磁気性能に影響を及ぼすのである。そ
のため逆に、樹脂結合法では鋳造時の結晶状態を
コントロールすればすぐれた磁気性能を有する磁
石の作製が可能になるわけである。
以下、実施例に従い本発明を詳細に説明してゆ
く。
実施例 1
高周波溶解炉を用いて、アルゴンガス中で合金
を1Kg溶解した、溶湯は第2図に示される円筒の
鉄製鋳型に鋳造された。鋳造インゴツトの断面の
マクロ組織は、第3図のようであつた。すなわち
A部はチル晶帯、B部は柱状晶帯、C部は等軸晶
帯を示す。鋳造された合金の組成は、Sm0.9Pr0.1
(Co0.6Cu0.08Fe0.3Zr0.02)8.3である。A部、B部、
C部より、それぞれインゴツトを切り出し、第1
図に示す製法1に従い樹脂結合磁石を作製した。
溶体化処理は、1150℃で10時間、時効は800℃で
20時間アルゴン雰囲気中で行つた。樹脂にはエポ
キシ樹脂を用い、磁気粉末に対して2.0wt%混合
した。結果を第1表に示す。表より分るように、
B部の柱状晶帯より得た値は、C部の等軸晶帯よ
り得たものより、たいへんすぐれている。A部の
チル晶帯は、4πIsとSQの値がB部のものに比べ
て低いとはいえ、C部よりもかなりすぐれてい
る。
The present invention relates to a fine powder bonded rare earth permanent magnet. A method for manufacturing a rare earth permanent magnet according to the present invention is shown in FIG. It has long been known that the magnetic performance of this magnet is influenced by alloy composition, heat treatment, powder particle size and shape, binder type, molding method, etc. We found that the performance changed significantly. Magnets using Sm-Pr-Co-Cu-Fe-M alloys fall into the category of precipitation hardening type or two-phase separation type magnets. This is because a different phase is precipitated in the matrix and magnetically hardened. This system of magnets has been widely developed since it was first made into a magnet using a ternary alloy of Sm-Co-Cu, mainly using Sm 2 Co 17 crystals. CoFe
It is known that the saturation magnetization 4πIs increases up to a certain amount by replacing it with . In the range where 4πIs increases, the crystal exhibits uniaxial anisotropy because Sm 2
(Co 1-x F x ) 17 , where X is in the range of 0 to 0.6. This fact does not change even if a certain amount of Cu is substituted for Co. When M is further added to Sm 2 (CoCuFe) 17 , the magnetic performance can be greatly improved even if the amount of M is very small. That is, when M is added, even if the amount of Cu is reduced or the amount of iron is increased, an iHc sufficient for a practical magnet can be obtained and a magnet with a high energy product can be manufactured. When a part of Sm is replaced with Pr, the Pr 2 Co 17 crystal becomes smaller than the Sm 2 Co 17 G crystal,
The high 4πIs makes it possible to obtain a magnet with a high energy product. Also, from the viewpoint of securing rare earth element resources, it is advantageous because both Sm and Pr can be used. however,
When a part of Sm is replaced with Pr, 4πIs increases but the crystal anisotropy decreases, so the anisotropic magnetic field
Ha becomes smaller. If Ha decreases, coercive force iHc
will also inevitably decline. Therefore, one of the objects of the present invention is to prevent the decrease in iHc caused by replacing Sm with Pr in a Sm-Co-Cu-Fe-M alloy by converting the ingot into columnar crystals. Another objective is to obtain enough iHc for a practical magnet by columnar crystallization, even if the Cu content is further reduced and the Fe content is further increased. Generally, when molten metal is poured from a crucible into a mold, solidification begins at the casting walls. This is explained by the fact that the energy barrier for stable nucleation of embryos (crystal buds) that have come into contact with a solid foreign material is smaller than that of embryos that are floating in solution without contact. Crystals formed on the casting wall grow into the molten metal while competing with neighboring crystals. The competitive growth region of crystals in the outermost layer of the ingot, as shown in FIG. 3, is called the chill crystal zone. Since crystals have anisotropy in growth rate, crystals whose direction of maximum growth rate is parallel to the direction of heat flow grow preferentially, suppressing the growth of adjacent crystals. During crystal growth, the closer the preferential orientation is to the heat flow, the longer the crystals survive, and other crystals are weeded out.As a result, the number of crystals decreases toward the inside of the ingot, forming columnar crystal zones. When the conditions are right, the columnar crystal bands collide and solidification is completed, but as shown in FIG. 3, equiaxed crystals are usually formed inside the columnar crystals. The origin of equiaxed crystals was not well known in the past, but it is now known that crystals formed on the casting wall or on the cooled surface of the molten metal are liberated and become free crystals, and these free crystals form the equiaxed crystal zone. (A. Ohno, T. Motegi and H.
Soda: Trans.ISIJ.11 (1971) 18). Even with this Sm-Pr-Co-Cu-Fe-M alloy,
As mentioned above, it has become clear that among the chill crystal zone, columnar crystal zone, and equiaxed crystal zone, the columnar crystal zone is the most suitable for making into a magnet. Regarding chill crystals, between equiaxed chill crystals and columnar chill crystals, columnar chill crystals are superior. An example will now be explained using a resin bonded rare earth cobalt magnet. This magnet is made from a magnetic alloy by the method shown in FIG. If we use exactly the same manufacturing method to make magnets from equiaxed crystal alloys, columnar crystal alloys, and chill crystal alloys, we find that the columnar crystal alloys exhibit saturation magnetization.
It was found that all performances were excellent, including 4πIs, coercive force iHc, bHc, and the squareness of the hysteresis loop. On the contrary, equiaxed crystal alloys and equiaxed chill crystal alloys have the poorest performance. Columnar chill crystal alloys produce magnets with values intermediate between these. This is thought to be because the columnar crystal composition acts effectively when the alloy is heat treated (solution treatment and aging treatment). In other words, it is thought that the columnar crystals promote uniform distribution of different phase precipitates precipitated in the matrix.
This improves the squareness of the hysteresis. At the same time, it is thought that the crystal structure and morphology of the precipitate also act to increase iHc, and therefore iHc also improves. Therefore, in order to obtain a good magnet, it is important to manufacture this alloy in such a way that the chill crystals near the casting wall are made into columnar chill crystals, and the other parts are made into columnar crystals. Since the amount of chill crystal bands is small in the overall alloy, the most important thing in manufacturing is to prevent equiaxed crystal bands and increase the ratio of columnar crystal bands. In addition, in terms of composition, the most effective columnar crystallization is expected to be the composition using the atomic ratio, Sm 1-x Pr x (Co 1-uvw Cu u Fe v M w ) z (However, , 0<x<0.5 0<u<0.2 0<v<0.5 0<w<0.1 6.5≦z<9.0 M represents an element consisting of at least one of Ti, Zr, Hf, V, Nb, and Ta ) is an alloy represented by The reason for limiting the components and composition range will be explained below. In this alloy system and its composition range, Sm-
Co type is the basic type. Cu is added to the Sm 2 Co 17 type alloy to obtain coercive force, and adding Cu improves iHc. However, 4πI decreases. Therefore, as a practical magnetic material, the value of u in the composition formula is preferably u<0.2. Although 4πIs is improved by adding Fe, if the amount is too large, iHc decreases significantly, so the value of v in the composition formula is preferably v<0.5. When the value of z is between 5z8.5, the Sm-Co alloy separates into SmCo 5 type compounds and Sm 2 Co 17 type compounds. The value of 4πIs is
Sm 2 Co 17 is 20% more expensive. Therefore, in order to realize a high 4πIs, it is desirable that z be 6.5 or more. On the other hand z
If it becomes 9.0 or more, iHc decreases significantly and a large amount of Co--Fe phase comes out, which impairs the squareness of the hysteresis loop, which is not preferable.
Also, the Pr 2 Co 17 compound is more effective than the Sm 2 Co 17 compound.
Although the value of 4πIs is large, the magnetocrystalline anisotropy constant
K 1 is negative, and a magnet utilizing uniaxial anisotropy cannot be produced using Pr 2 Co 17 as it is. Therefore, Sm 2 Co 17 type compounds with positive and large K 1 and large 4πIs
Making a magnet by combining Pr 2 Co 17 type compound is
This is an effective method for obtaining a magnet with a large 4πIs and a somewhat high iHc. For this Sm 1-x
Pr x (CoCuFe) In the z composition, x < 0.5 is desirable as a practical material. If the value of x is larger than that,
I don't have enough iHc. What made w less than 0.1 was M
This is because if 0.1 or more is added, there is no point in increasing 4πIs by increasing Fe, reducing Cu, or adding Pr, as it significantly lowers the 4πIs of the alloy. M may be used not only alone, but also in combination of two or more. As mentioned above, the magnetic performance of the ingot changes significantly depending on the crystalline state at the time of casting. The magnet manufacturing method that can best utilize this fact is a fine powder bonded magnet. This is because manufacturing the magnet involves the steps shown in FIG. 1, so all heat treatment is performed in the ingot state, and after magnetic hardening, it is crushed and bonded with a binder. Therefore,
A magnet of a desired shape can also be produced by cutting out the ingot after magnetic hardening. The process before crushing is the same as for cast magnets. Because such a manufacturing process is used, the crystalline state of the ingot has a greater effect on magnetic performance than in the sintering method. Therefore, in contrast, with the resin bonding method, it is possible to produce a magnet with excellent magnetic performance by controlling the crystalline state during casting. Hereinafter, the present invention will be explained in detail according to examples. Example 1 Using a high frequency melting furnace, 1 kg of alloy was melted in argon gas, and the molten metal was cast into a cylindrical iron mold shown in FIG. The macrostructure of the cross section of the cast ingot was as shown in FIG. That is, part A shows a chill crystal zone, part B shows a columnar crystal band, and part C shows an equiaxed crystal band. The composition of the cast alloy is Sm 0.9 Pr 0.1
(Co 0.6 Cu 0.08 Fe 0.3 Zr 0.02 ) 8.3 . A part, B part,
Cut out an ingot from part C, and
A resin-bonded magnet was manufactured according to Manufacturing Method 1 shown in the figure.
Solution treatment is at 1150℃ for 10 hours and aging is at 800℃.
The test was carried out in an argon atmosphere for 20 hours. Epoxy resin was used as the resin, and was mixed at 2.0 wt% with respect to the magnetic powder. The results are shown in Table 1. As you can see from the table,
The values obtained from the columnar zones in section B are much better than those obtained from the equiaxed zones in section C. Although the chill crystal zone of part A has lower values of 4πIs and SQ than those of part B, it is considerably better than that of part C.
【表】
ただし、SQとはヒステリシスループの角形性
を示す指標で、
SQ=Hk/iHc
で与えられる。Hkは、4πI−H減磁曲線上で
0.9Brを与える磁場の大きさである。これらの結
果より、B部の柱状晶の部分が最も性能がすぐれ
ていることが判明した。A部のチル晶帯は、鋳壁
のごく近傍のみに生成するもので、本実施例のイ
ンゴツトでは、1mm以下である。よつて表1の結
果を得るに用いたA部のインゴツトには、かなり
の割合でB部の柱状晶の部分が入つていると思わ
れる。このように、A部はインゴツト全体ではご
くわずかなので、無視してよい。インゴツトを製
造するうえで重要な点は、いかにC部の等軸晶を
抑え、柱状晶を発達させるかにある。
実施例 2
実施例1と同様な方法で第2表に示される組成
の合金から樹脂結合磁石を製造した。ただし、溶
体化処理は、1150〜1180℃の間で最も最適な温度
で10時間行つた。[Table] However, SQ is an index indicating the squareness of the hysteresis loop, and is given by SQ = Hk/iHc. Hk is on the 4πI-H demagnetization curve
This is the magnitude of the magnetic field that gives 0.9Br. From these results, it was found that the columnar crystal part of part B had the best performance. The chill crystal zone in part A is generated only in the very vicinity of the casting wall, and in the ingot of this example, it is 1 mm or less. Therefore, it seems that the ingot of Part A used to obtain the results in Table 1 contains a considerable proportion of columnar crystals of Part B. In this way, since part A is very small in the whole ingot, it can be ignored. The important point in producing ingots is how to suppress equiaxed crystals in the C portion and develop columnar crystals. Example 2 A resin-bonded magnet was manufactured from an alloy having the composition shown in Table 2 in the same manner as in Example 1. However, the solution treatment was performed at the most optimal temperature between 1150 and 1180°C for 10 hours.
【表】
本実施例はまた、主にB、C部のみのインゴツ
トに対して行つた。結果を第4図に示す。Feの
量が増加していつても、柱状晶の方がよりよい磁
気性能が得られることが分る。これにより、ある
程度Feの量を高めても、iHcを得られることが明
らかになつた。
実施例 3
実施例2と全く同様な方法で、第3表の組成の
合金から樹脂結合磁石を製造した。結果を第5図
に示す。(SmPr)z(CoCuFeM)17型の合金では、
Cuの量が低くなると、iHcは低下するが、柱状晶
のものでは、等軸晶のものに比べ、低Cu組成ま
で、iHcは高い値が得られることが分る。また角
形性も柱状晶の方がすぐれている。[Table] This example was also carried out mainly on ingots of only parts B and C. The results are shown in Figure 4. It can be seen that columnar crystals provide better magnetic performance even as the amount of Fe increases. This revealed that iHc can be obtained even if the amount of Fe is increased to some extent. Example 3 In exactly the same manner as in Example 2, resin-bonded magnets were manufactured from alloys having the compositions shown in Table 3. The results are shown in Figure 5. (SmPr) z (CoCuFeM) For alloy type 17 ,
As the amount of Cu decreases, iHc decreases, but it can be seen that in columnar crystals, higher iHc values can be obtained up to low Cu compositions than in equiaxed crystals. Columnar crystals also have better squareness.
【表】
実施例 4
第4表に示される組成の合金を1Kgづつ、第2
図で示される鋳型と、柱状晶部分を多く得るため
に第6図に示される角形の鋳型に鋳造した。柱状
晶部分の割合は、前者の鋳型では約40%、後者の
鋳型では約80%であつた。インゴツトは鋳型から
取り出された後丸ごと熱処理され、1Kg全て粉砕
された。熱処理条件は実施例2と同じ。充分微粉
になつた粉はエポキシ樹脂と混練された。粉砕、
混練を通じて磁粉は全体に均一になつている。全
体から10gをサンプリングして、磁場中成形して
磁石を成形した。従つて製造工程は第1図の製法
1である。結果を第7図に示す。角型の鋳型に鋳
込んだ磁石の性能の方がすぐれていることが分
る。またPrをある程度多くしても、柱状晶化す
ることにより、実用的磁石に必要な位のiHcが得
られることが分る。[Table] Example 4 1 kg of the alloy having the composition shown in Table 4 was added to the second
In order to obtain a large number of columnar crystal portions, casting was performed in the mold shown in the figure and in a rectangular mold shown in FIG. 6. The proportion of columnar crystal portions was approximately 40% in the former mold and approximately 80% in the latter mold. After the ingot was removed from the mold, it was heat-treated in its entirety and pulverized to 1 kg. The heat treatment conditions are the same as in Example 2. The sufficiently finely divided powder was kneaded with epoxy resin. crushing,
Through kneading, the magnetic powder becomes uniform throughout. A 10g sample was taken from the whole sample and molded in a magnetic field to form a magnet. Therefore, the manufacturing process is Manufacturing Method 1 shown in FIG. The results are shown in FIG. It can be seen that the performance of the magnet cast in a square mold is superior. Furthermore, even if the Pr content is increased to a certain extent, the iHc required for a practical magnet can be obtained by forming columnar crystals.
【表】
実施例 5
第6図に示す鋳型に、第5表に示す組成の合金
を鋳造した。鋳造時の溶湯の温度は、1600℃であ
る。従来、溶湯温度は1450℃付近で行なわれてい
た。この位の温度であると、鋳造されたインゴツ
トは第3図に示すように等軸晶の割合が多い。柱
状晶を多く得るには、湯温を上昇するのが大切で
ある。従つて、本実施例で行つた鋳造では約90%
の柱状晶組織を得ることができた。[Table] Example 5 An alloy having the composition shown in Table 5 was cast into the mold shown in FIG. The temperature of the molten metal during casting was 1600°C. Conventionally, molten metal temperature was around 1450℃. At this temperature, the cast ingot has a large proportion of equiaxed crystals, as shown in FIG. In order to obtain a large amount of columnar crystals, it is important to raise the water temperature. Therefore, in the casting performed in this example, approximately 90%
A columnar crystal structure was obtained.
【表】
磁石製造法は、実施例5と同様に行つた。結果
を第6表に示す。各Mに対して、樹脂結合磁石と
しては高性能な値が得られていることが分る。[Table] The magnet manufacturing method was carried out in the same manner as in Example 5. The results are shown in Table 6. It can be seen that high performance values are obtained for each M as a resin bonded magnet.
【表】
実施例 6
第7表に示す組成の合金を、実施例5と全く同
様な工程を用いて樹脂結合型磁石を作製した。結
果を第8表に示す。[Table] Example 6 A resin-bonded magnet was produced using the alloy having the composition shown in Table 7 using the same process as in Example 5. The results are shown in Table 8.
【表】【table】
【表】
上記のごとく、zの値を変化させても充分高い
性能を有する磁石の作製が可能であつた。
このようにSm−Co−Cu−Fe−M合金にPrを
入れて飽和磁化を高め、さらに柱状晶化により保
磁力、角形性そして飽和磁化まで向上させた合金
を使用した微粉末結合型磁石は、磁気性能、成形
性、加工性、コスト面においてすぐれ、精密業界
のみならず各業界に与える効用は大きい。[Table] As shown above, it was possible to produce a magnet with sufficiently high performance even if the value of z was changed. In this way, a fine powder bonded magnet using an alloy that increases saturation magnetization by adding Pr to the Sm-Co-Cu-Fe-M alloy, and further improves coercive force, squareness, and saturation magnetization by columnar crystallization. It has excellent magnetic performance, moldability, workability, and cost, and has great utility not only in the precision industry but in other industries as well.
第1図は、樹脂結合型磁石の製造工程を示す。
第2図は、円筒状の鉄製鋳型を示す。寸法の単位
はmmである。第3図は、第2図で示される鋳型に
鋳込まれたときのインゴツトのマクロ組織を示
す。Aはチル晶帯、Bは柱状晶帯、Cは等軸晶
帯、Dは鋳型の側面の断面である。第4図は、
Sm0.9Pr0.1(Co0.9-vCu0.08FevZr0.02)8.3の組成にお
い
て、Vを変化させた時の樹脂結合磁石の磁気性能
を示す。第5図は、Sm0.8Pr0.2(Co0.676-uCuuFe0.3
Zr0.024)8.1の組成において、uを変化させた時の
樹脂結合磁石の磁気性能を示す。第6図は、角形
状の鉄製の鋳型を示す。寸法の単位はmmである。
第7図は、Sm1-xPrx(Co0.6Cu0.08Fe0.3Ti0.02)8.3の
組成を有する合金を、円筒型の鋳型と角型の鋳型
に鋳込み、磁気性能の変化をみたものである。
FIG. 1 shows the manufacturing process of a resin-bonded magnet.
FIG. 2 shows a cylindrical iron mold. The unit of dimension is mm. FIG. 3 shows the macrostructure of the ingot when it is cast into the mold shown in FIG. A is a chill crystal zone, B is a columnar crystal zone, C is an equiaxed crystal zone, and D is a cross section of the side surface of the mold. Figure 4 shows
The magnetic performance of the resin-bonded magnet is shown when V is varied at a composition of Sm 0.9 Pr 0.1 (Co 0.9-v Cu 0.08 Fe v Zr 0.02 ) 8.3 . Figure 5 shows Sm 0.8 Pr 0.2 (Co 0.676-u Cu u Fe 0.3
Zr 0.024 ) Magnetic performance of the resin bonded magnet when u is changed in the composition 8.1 is shown. FIG. 6 shows a rectangular iron mold. The unit of dimension is mm.
Figure 7 shows the changes in magnetic performance when an alloy with a composition of Sm 1-x Pr x (Co 0.6 Cu 0.08 Fe 0.3 Ti 0.02 ) 8.3 was cast into a cylindrical mold and a square mold. .
Claims (1)
インダーを混練して成形してなる希土類永久磁石
において、前記合金として原子比を用いた組成
が、 Sm1-xPrx(Co1-u-v-wCuuFevM w )z (但し、0<x<0.5 0<u<0.2 0<v<0.5 0<w<0.1 6.5≦z<9.0 MはTi、Zr、Hf、V、Nb、Taのうちの少な
くとも1種からなる元素を示す。) で表わされ、かつマクロ組織が主に柱状晶組織で
ある合金を使用したことを特徴とする希土類永久
磁石。[Claims] 1. A rare earth permanent magnet formed by kneading a binder into powder of an alloy mainly composed of Sm 2 Co 17 type crystals and molding the alloy, wherein the alloy has a composition using an atomic ratio of Sm 1-x Pr x (Co 1-uvw Cu u Fe v M w ) z (0<x<0.5 0<u<0.2 0<v<0.5 0<w<0.1 6.5≦z<9.0 M is Ti, Zr, Hf , V, Nb, and Ta), and is characterized by using an alloy whose macrostructure is mainly a columnar crystal structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP55181751A JPS57106007A (en) | 1980-12-22 | 1980-12-22 | Permanent magnet of rare earth cobalt |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP55181751A JPS57106007A (en) | 1980-12-22 | 1980-12-22 | Permanent magnet of rare earth cobalt |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS57106007A JPS57106007A (en) | 1982-07-01 |
| JPS648455B2 true JPS648455B2 (en) | 1989-02-14 |
Family
ID=16106242
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP55181751A Granted JPS57106007A (en) | 1980-12-22 | 1980-12-22 | Permanent magnet of rare earth cobalt |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS57106007A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS59169108A (en) * | 1983-03-16 | 1984-09-25 | Toshiba Corp | Permanent magnet |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5061699A (en) * | 1973-10-03 | 1975-05-27 | ||
| JPS5216444A (en) * | 1975-07-30 | 1977-02-07 | Matsushita Refrigeration | Automatic spot welding process |
| JPS5261123A (en) * | 1975-11-14 | 1977-05-20 | Namiki Precision Jewel Co Ltd | Permanent magnetic alloy |
| JPS6043900B2 (en) * | 1978-08-03 | 1985-10-01 | セイコーエプソン株式会社 | permanent magnet material |
| JPS55128502A (en) * | 1979-03-23 | 1980-10-04 | Tdk Corp | Permanent magnet material and its manufacture |
| JPS56102533A (en) * | 1980-01-16 | 1981-08-17 | Seiko Epson Corp | Manufacture of rare earth element-cobalt permanent magnet alloy |
| JPS56150146A (en) * | 1980-04-22 | 1981-11-20 | Seiko Epson Corp | Production of rare earth-cobalt permanent magnet alloy |
| JPS56166348A (en) * | 1980-05-26 | 1981-12-21 | Seiko Epson Corp | Manufacture of permanent magnet alloy of rare earth element and cobalt |
| JPS56166347A (en) * | 1980-05-26 | 1981-12-21 | Takagi Kogyo Kk | Manufacture of permanent magnet alloy of rare earth element and cobalt |
-
1980
- 1980-12-22 JP JP55181751A patent/JPS57106007A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS57106007A (en) | 1982-07-01 |