JPS648454B2 - - Google Patents
Info
- Publication number
- JPS648454B2 JPS648454B2 JP55179989A JP17998980A JPS648454B2 JP S648454 B2 JPS648454 B2 JP S648454B2 JP 55179989 A JP55179989 A JP 55179989A JP 17998980 A JP17998980 A JP 17998980A JP S648454 B2 JPS648454 B2 JP S648454B2
- Authority
- JP
- Japan
- Prior art keywords
- crystals
- alloy
- columnar
- crystal
- magnet
- 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.)
- Expired
Links
- 239000013078 crystal Substances 0.000 claims description 65
- 229910045601 alloy Inorganic materials 0.000 claims description 28
- 239000000956 alloy Substances 0.000 claims description 28
- 239000000203 mixture Substances 0.000 claims description 16
- 229910052761 rare earth metal Inorganic materials 0.000 claims description 7
- 239000000843 powder Substances 0.000 claims description 5
- 150000002910 rare earth metals Chemical class 0.000 claims description 5
- 239000011230 binding agent Substances 0.000 claims description 4
- 229910052782 aluminium Inorganic materials 0.000 claims description 3
- 229910052804 chromium Inorganic materials 0.000 claims description 3
- 229910052737 gold Inorganic materials 0.000 claims description 3
- 229910052735 hafnium Inorganic materials 0.000 claims description 3
- 229910052748 manganese Inorganic materials 0.000 claims description 3
- 229910052750 molybdenum Inorganic materials 0.000 claims description 3
- 229910052759 nickel Inorganic materials 0.000 claims description 3
- 229910052758 niobium Inorganic materials 0.000 claims description 3
- 229910052709 silver Inorganic materials 0.000 claims description 3
- 229910052719 titanium Inorganic materials 0.000 claims description 3
- 229910052721 tungsten Inorganic materials 0.000 claims description 3
- 229910052720 vanadium Inorganic materials 0.000 claims description 3
- 229910052726 zirconium Inorganic materials 0.000 claims description 3
- 238000000465 moulding Methods 0.000 claims description 2
- 229910052715 tantalum Inorganic materials 0.000 claims description 2
- 238000004898 kneading Methods 0.000 claims 1
- 238000004519 manufacturing process Methods 0.000 description 8
- 150000001875 compounds Chemical class 0.000 description 6
- 230000007423 decrease Effects 0.000 description 6
- 238000005266 casting Methods 0.000 description 5
- 230000005415 magnetization Effects 0.000 description 5
- 239000002184 metal Substances 0.000 description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- 238000002425 crystallisation Methods 0.000 description 4
- 230000008025 crystallization Effects 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 239000000047 product Substances 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- 230000032683 aging Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 210000002257 embryonic structure Anatomy 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 239000002244 precipitate Substances 0.000 description 2
- 239000011347 resin Substances 0.000 description 2
- 229920005989 resin Polymers 0.000 description 2
- 238000007711 solidification Methods 0.000 description 2
- 230000008023 solidification Effects 0.000 description 2
- 229910052727 yttrium Inorganic materials 0.000 description 2
- 229910000531 Co alloy Inorganic materials 0.000 description 1
- 229910020637 Co-Cu Inorganic materials 0.000 description 1
- 229910052772 Samarium Inorganic materials 0.000 description 1
- 229910052786 argon Inorganic materials 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
- 229910052802 copper Inorganic materials 0.000 description 1
- 230000005347 demagnetization Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- -1 heat treatment Substances 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 229910001004 magnetic alloy Inorganic materials 0.000 description 1
- 239000000696 magnetic material Substances 0.000 description 1
- 230000005389 magnetism Effects 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 150000002739 metals Chemical class 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
- 238000001556 precipitation Methods 0.000 description 1
- 238000004881 precipitation hardening Methods 0.000 description 1
- 229910000938 samarium–cobalt magnet Inorganic materials 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
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、希土類元素と遷都金属を主成分とす
る析出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−Y−Co−M合金を使用した磁石は、析出
硬化型あるいは、2相分離型磁石の範疇に入る。
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−Cu3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。Cuの代りに、Mn、Cr、Mo、
W、Ni、Ag、Au、Al、Ti、Zr、Hf、V、Nb、
Taのうちの1種あるいは2種以上を複合させて、
Sm−Co−Mとして用いれば、合金は同様に磁気
硬化する。Smの一部をYで置き換えると、
Sm2Co17よりY2Co17の方が飽和磁化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。又、希土類金属の資源確保の観点から言つて
もSmとYの両方を使うことができるので、都合
がよい。しかしながら、Smの一部をYで置き換
えてゆくと、4πIsは上昇するが、異方性磁場Ha
が低下する。Haが低下すれば、保磁力iHcも必
然的に低くなる。それ故本発明の一つの目的は、
このYを入れたことによるiHcの低下を、インゴ
ツトを柱状晶化することによつて防ぐことにあ
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
いで融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
少なくなり、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体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)。
本系の合金でも、前述したように、チル晶帯、
柱状晶帯、そして等軸晶帯のうちで柱状晶帯が磁
石にするのに最も優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
チル晶の方が優れている。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、柱状晶組織が、該合金を熱処理(溶体
化処理及び時効処理)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。
本合金の製造は、鋳壁近傍のチル晶帯域は柱状
チル晶として、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
金全体では量が少ないので、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-xYx(Co1-uMu)z
(但し、0<x<0.5
0<u<0.2
6.5≦z<9.0
MはMn、Cr、Mo、W、Ni、Ag、Au、Al、
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。中でもSm2Co17型結晶が主
体をなす。MはSm2Co17型合金の保磁力を得るた
めに加えられるものであり、Mを入れることで
iHcは向上するが、4πIsは低下する。このため実
用磁性材料としては、組成式中のuの値はu<
0.2が望ましい。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。Zの値が、5
z8.5の間にある時は、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の方が高い。よつて、高い
4πIsを実現するためには、Zは6.5以上が望まし
い。またZが9.0以上になると、Co相が多くなる
のでヒステリシスループの角形性が悪くなり好ま
しくない。またY2Co17化合物は、Sm2Co17化合
物よりも4πIsの値は大きいが、結晶磁気異方性定
数K1は負であり、Y2Co17のままでは、一軸異方
性を利用した磁石は作れない。よつてK1が正で
大きいSm2Co17型化合物と4πIsの大きいY2CO17
型化合物を複合させて、磁石にすることは飽和磁
化が大きくてしかもある程度高い保磁力を有する
磁石を得るに有効な方法である。このためには
Sm1-xYx(Co1-uMu)zも組成において、x<0.5で
あることが望ましい。それ以上xの値が大きい
と、iHcが足らなくなる。
鋳造時のマクロ組織でインゴツトの性能が改善
されることは前述したが、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、該磁石を製造するには第
1図で示すような工程を取るので、熱処理は全て
インゴツトのまま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、インゴツト
の状態で磁石化することもでき、この点では鋳造
磁石と少しも変わらない。バインダーで結合する
のは結晶を揃えるためと、実際の製品を作るとき
の成形性を上げ、コストを低くするためであり、
磁性の本質は、鋳造磁石と同じである。このため
焼結磁石では、鋳造のインゴツトの金属組織に磁
石の性能は左右されないが、微粉末結合磁石で
は、大いに影響される。逆に言うと、これを利用
して、微粉末結合型磁石の性能は高められるので
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、第1表に示
すとおりである。
The present invention relates to a precipitation type rare earth permanent magnet whose main components are rare earth elements and metals. 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-Y-Co-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 was initially
It is an Sm-Co-Cu ternary alloy that has been widely developed since it was first made into a magnet with a composition mainly using Sm 2 CO 17 crystals. Instead of Cu, Mn, Cr, Mo,
W, Ni, Ag, Au, Al, Ti, Zr, Hf, V, Nb,
By combining one or more of Ta,
When used as Sm-Co-M, the alloy similarly hardens magnetically. If we replace part of Sm with Y, we get
Since Y 2 Co 17 has a higher saturation magnetization 4πIs than Sm 2 Co 17 , it becomes possible to obtain a magnet with a high energy product. Also, from the viewpoint of securing rare earth metal resources, it is convenient because both Sm and Y can be used. However, when a part of Sm is replaced by Y, 4πIs increases, but the anisotropic magnetic field Ha
decreases. If Ha decreases, coercive force iHc will also inevitably decrease. Therefore, one object of the present invention is to
The purpose is to prevent the decrease in iHc due to the addition of Y by forming the ingot into columnar crystals. 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 to stable nucleation of embryos (crystal buds) that come into contact with solid foreign matter is smaller than that of embryos that float in the melt 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 preferred 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 as they move inside 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. Although the origin of equiaxed crystals was not well known before, it is now known that crystals formed on the casting wall or on the cooled surface of the liquid become free crystals, and these free crystals form equiaxed crystals. (A. Ohno, T. Motegi and H.
Soda: Trans.ISIJ.11 (1971) 18). Even in this alloy, as mentioned above, chill crystal bands,
It has become clear that among columnar crystal bands and equiaxed crystal bands, columnar crystal bands are the most suitable for making into magnets. 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 make magnets using equiaxed crystal alloys, columnar crystal alloys, and chill crystal alloys using exactly the same manufacturing method, we find that the columnar crystal alloys have all the same characteristics in terms of saturation magnetization 4πIs, coercivity iHc, bHc, and hysteresis loop squareness. It was found that the performance was excellent across the board. vice versa,
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 structure acts effectively when the alloy is heat treated (solution treatment and aging treatment). That is, it is thought that the columnar crystals promote uniform distribution of different phase precipitates precipitated in the matrix, thereby improving the squareness of the hysteresis. At the same time, the crystal structure and morphology of the precipitates are thought to have the effect of forming in the direction of increasing iHc, and therefore, iHc
It also improves. In the production of this alloy, it is important to produce a good magnet by forming columnar chill crystals in the chill crystal zone near the casting wall and forming columnar crystals in other parts. Since the amount of chill crystal bands is small in the entire 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 effect of columnar crystallization is expected when the composition using atomic ratio is Sm 1-x Y x (Co 1-u M u ) z (where 0<x <0.5 0<u<0.2 6.5≦z<9.0 M is Mn, Cr, Mo, W, Ni, Ag, Au, Al,
Indicates 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. Among them, Sm 2 Co 17 type crystals are the main type. M is added to obtain the coercive force of the Sm 2 Co 17 type alloy, and by adding M,
iHc improves, but 4πIs decreases. Therefore, as a practical magnetic material, the value of u in the composition formula is u<
0.2 is desirable. M is not only used alone, but also
Two or more types may be added in combination. The value of Z is 5
When between z8.5, the Sm-Co alloy is
Separates into SmCo type 5 compound and Sm 2 Co type 17 compound.
The value of 4πIs is higher for Sm 2 Co 17 . It's expensive
In order to realize 4πIs, Z is preferably 6.5 or more. Furthermore, if Z is 9.0 or more, the amount of Co phase increases, which deteriorates the squareness of the hysteresis loop, which is not preferable. In addition, the Y 2 Co 17 compound has a larger value of 4πIs than the Sm 2 Co 17 compound, but the magnetocrystalline anisotropy constant K 1 is negative. You can't make magnets. Therefore, Sm 2 Co 17 type compounds with positive and large K 1 and Y 2 CO 17 with large 4πIs
Combining type compounds to form a magnet is an effective method for obtaining a magnet with large saturation magnetization and a relatively high coercive force. For this purpose
In the composition of Sm 1-x Y x (Co 1-u M u ) z , it is also desirable that x<0.5. If the value of x is larger than that, iHc becomes insufficient. As mentioned above, the macrostructure during casting improves the performance of the ingot, and the magnet manufacturing method that can best utilize this fact is the fine powder bonded magnet. This is because the steps shown in FIG. 1 are used to manufacture the magnet, so all the heat treatment is performed on the ingot as it is, magnetically hardened, and then crushed and bonded with a binder. Therefore, it can be magnetized in the ingot state, and in this respect it is no different from cast magnets. The purpose of binding with a binder is to align the crystals, improve moldability and reduce costs when making actual products.
The essence of magnetism is the same as that of cast magnets. Therefore, in the case of a sintered magnet, the performance of the magnet is not affected by the metal structure of the cast ingot, but in the case of a fine powder bonded magnet, it is greatly affected. In other words, this can be used to improve the performance of fine powder bonded magnets. Hereinafter, the present invention will be explained in detail according to examples. Example 1 Using a high frequency melting furnace, 1 kg of an alloy was melted in argon gas. The molten metal was cast into the 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 as shown in Table 1.
【表】
鋳造インゴツトより、A部、B部そしてC部を
切り出し、第1図に示される磁石製造工程に従い
樹脂結合型磁石を製造した。容体化処理は、1100
〜1200℃の間の各組成に適した温度で、10時間行
い、時効処理は、800℃で24時間行つた。結果を
第2表に示す。表中のます目の中で、上段の数字
はB部の柱状晶帯を用いて得たものであり、下段
のものは、C部の等軸晶帯を用いて得たものであ
る。これにより、柱状晶帯の方が、iHc、4πIsと
もに大きいことがわかる。[Table] Parts A, B, and C were cut out from the cast ingot, and resin-bonded magnets were manufactured according to the magnet manufacturing process shown in FIG. Containment processing is 1100
The aging treatment was carried out for 10 hours at a temperature suitable for each composition between ~1200°C and 24 hours at 800°C. The results are shown in Table 2. Among the squares in the table, the numbers in the upper row are those obtained using the columnar crystal zone of section B, and those in the lower row are those obtained using the equiaxed crystal zone of section C. This shows that both iHc and 4πIs are larger in the columnar crystal zone.
【表】
実施例 2
実施例1と同様の方法で、第3表に示される組
成の合金を使用して樹脂結合型磁石を製造した。[Table] Example 2 A resin-bonded magnet was manufactured in the same manner as in Example 1 using an alloy having the composition shown in Table 3.
【表】
その結果を第4表に示す。表中のます目の中
で、上段の数字はB部の柱状晶帯を用いて得たも
のであり、下段のものは、C部の等軸晶帯を用い
て得たものである。[Table] The results are shown in Table 4. Among the squares in the table, the numbers in the upper row are those obtained using the columnar crystal zone of section B, and those in the lower row are those obtained using the equiaxed crystal zone of section C.
【表】
第4表より分かることは、柱状晶化することに
より、角形性(Hk/iHc)がたいへん上昇して
いることである。ただしHkは、4πI−H減磁曲線
上で0.9×Brを与える磁場の大きさである。また、
これらの合金組成でも、柱状晶の方が等軸晶より
もiHcがすぐれており、角形性がすぐれているこ
とと相まつて、柱状晶の方が、最大エネルギー積
がたいへん大きくなつている。
実施例 3
実施例1と同様の方法で、第5表、第6表に示
される組成の合金を使用して、樹脂結合型磁石を
製造した。[Table] It can be seen from Table 4 that the squareness (Hk/iHc) is greatly increased by columnar crystallization. However, Hk is the magnitude of the magnetic field that gives 0.9×Br on the 4πI-H demagnetization curve. Also,
Even in these alloy compositions, the columnar crystals have a better iHc than the equiaxed crystals, and together with their superior squareness, the columnar crystals have a much larger maximum energy product. Example 3 A resin-bonded magnet was manufactured in the same manner as in Example 1 using alloys having the compositions shown in Tables 5 and 6.
【表】【table】
【表】
結果を第4図、第5図に示す。この結果より、
SmをYで置換したいつた時にも、柱状晶化によ
り磁気性能は向上することが分かる。また第5図
から、zのどの値に対しても、柱状晶の方が磁気
性能がすぐれていることが分かる。
このようにSm−Co−M合金にY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
樹脂結合型磁石は、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] The results are shown in Figures 4 and 5. From this result,
It can be seen that even when Sm is replaced with Y, the magnetic performance is improved due to columnar crystallization. Furthermore, from FIG. 5, it can be seen that columnar crystals have better magnetic performance for any value of z. In this way, resin-bonded magnets using an alloy that increases saturation magnetization by adding Y to the Sm-Co-M alloy, and further improves coercive force, squareness, and saturation magnetization by columnar crystallization, have excellent magnetic performance and moldability. properties, processability,
It is superior in terms of cost and has great benefits not only to the precision industry but to 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
込ませ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、Dは鋳型の側面の
断面である。第4図は、Sm1-xYx(Co0.95Zr0.05)8.3
の組成において、x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、Sm0.8Y0.2
(Co0.95Ti0.05)zの組成において、zを変化させた
時の樹脂結合磁石の磁気性能を示す。
FIG. 1 shows the manufacturing process of a resin-bonded magnet.
FIG. 2 shows a cylindrical iron mold. FIG. 3, whose dimensions are in mm, 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, and D is a cross section of the side surface of the mold. Figure 4 shows Sm 1-x Y x (Co 0.95 Zr 0.05 ) 8.3
The magnetic performance of the resin-bonded magnet is shown when x is varied in the composition. Figure 5 shows Sm 0.8 Y 0.2
(Co 0.95 Ti 0.05 ) In the composition of z , the magnetic performance of the resin bonded magnet is shown when changing z.
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-xYx(Co1-uMu)z (但し、0<x<0.5 0<u<0.2 6.5≦z<9.0 MはMn、Cr、Mo、W、Ni、Ag、Au、Al、
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 Y x (Co 1-u M u ) z (However, 0<x<0.5 0<u<0.2 6.5≦z<9.0 M is Mn, Cr, Mo, W, Ni, Ag, Au, Al,
Indicates an element consisting of at least one of 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 |
|---|---|---|---|
| JP55179989A JPS57104202A (en) | 1980-12-19 | 1980-12-19 | Permanent magnet made of rare-earth cobalt |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP55179989A JPS57104202A (en) | 1980-12-19 | 1980-12-19 | Permanent magnet made of rare-earth cobalt |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS57104202A JPS57104202A (en) | 1982-06-29 |
| JPS648454B2 true JPS648454B2 (en) | 1989-02-14 |
Family
ID=16075506
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP55179989A Granted JPS57104202A (en) | 1980-12-19 | 1980-12-19 | Permanent magnet made of rare-earth cobalt |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS57104202A (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP3057448B2 (en) * | 1988-05-26 | 2000-06-26 | 信越化学工業株式会社 | Rare earth permanent magnet |
| JP6995542B2 (en) * | 2017-09-19 | 2022-02-04 | 株式会社東芝 | Magnet materials, permanent magnets, rotary machines, and vehicles |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5216444A (en) * | 1975-07-30 | 1977-02-07 | Matsushita Refrigeration | Automatic spot welding process |
| JPS6043900B2 (en) * | 1978-08-03 | 1985-10-01 | セイコーエプソン株式会社 | permanent magnet material |
-
1980
- 1980-12-19 JP JP55179989A patent/JPS57104202A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS57104202A (en) | 1982-06-29 |
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