JPH0231483B2 - - Google Patents
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- Publication number
- JPH0231483B2 JPH0231483B2 JP62037343A JP3734387A JPH0231483B2 JP H0231483 B2 JPH0231483 B2 JP H0231483B2 JP 62037343 A JP62037343 A JP 62037343A JP 3734387 A JP3734387 A JP 3734387A JP H0231483 B2 JPH0231483 B2 JP H0231483B2
- Authority
- JP
- Japan
- Prior art keywords
- temperature
- molded magnet
- magnet according
- heat treatment
- powder
- 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 - Lifetime
Links
- 238000001816 cooling Methods 0.000 claims description 38
- 238000011282 treatment Methods 0.000 claims description 38
- 238000010438 heat treatment Methods 0.000 claims description 26
- 239000000843 powder Substances 0.000 claims description 22
- 238000000034 method Methods 0.000 claims description 21
- 238000004519 manufacturing process Methods 0.000 claims description 19
- 229910052761 rare earth metal Inorganic materials 0.000 claims description 15
- 239000000203 mixture Substances 0.000 claims description 12
- 239000011230 binding agent Substances 0.000 claims description 10
- 229910017052 cobalt Inorganic materials 0.000 claims description 10
- 239000010941 cobalt Substances 0.000 claims description 10
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 10
- 150000002910 rare earth metals Chemical class 0.000 claims description 10
- 229910000765 intermetallic Inorganic materials 0.000 claims description 8
- 238000000465 moulding Methods 0.000 claims description 7
- 229910052804 chromium Inorganic materials 0.000 claims description 6
- 229910052748 manganese Inorganic materials 0.000 claims description 6
- 229910052759 nickel Inorganic materials 0.000 claims description 6
- 229910052742 iron Inorganic materials 0.000 claims description 5
- 229910052726 zirconium Inorganic materials 0.000 claims description 5
- 229910052802 copper Inorganic materials 0.000 claims description 4
- 229910052735 hafnium Inorganic materials 0.000 claims description 4
- 238000002156 mixing Methods 0.000 claims description 4
- 229910052758 niobium Inorganic materials 0.000 claims description 4
- 238000010298 pulverizing process Methods 0.000 claims description 4
- 229910052719 titanium Inorganic materials 0.000 claims description 4
- 229910052720 vanadium Inorganic materials 0.000 claims description 4
- 238000010791 quenching Methods 0.000 claims description 2
- 230000000171 quenching effect Effects 0.000 claims description 2
- 230000032683 aging Effects 0.000 description 31
- 239000000243 solution Substances 0.000 description 9
- 239000000463 material Substances 0.000 description 8
- 239000000047 product Substances 0.000 description 6
- 230000000694 effects Effects 0.000 description 5
- 101000993059 Homo sapiens Hereditary hemochromatosis protein Proteins 0.000 description 4
- 229910045601 alloy Inorganic materials 0.000 description 4
- 239000000956 alloy Substances 0.000 description 4
- 230000004907 flux Effects 0.000 description 4
- -1 polypropylene Polymers 0.000 description 4
- 238000004881 precipitation hardening Methods 0.000 description 4
- 238000005245 sintering Methods 0.000 description 4
- GWXLDORMOJMVQZ-UHFFFAOYSA-N cerium Chemical group [Ce] GWXLDORMOJMVQZ-UHFFFAOYSA-N 0.000 description 3
- 150000001875 compounds Chemical class 0.000 description 3
- 229920001971 elastomer Polymers 0.000 description 3
- 238000002347 injection Methods 0.000 description 3
- 239000007924 injection Substances 0.000 description 3
- 230000005415 magnetization Effects 0.000 description 3
- 229920005989 resin Polymers 0.000 description 3
- 239000011347 resin Substances 0.000 description 3
- 238000006467 substitution reaction Methods 0.000 description 3
- 229910052715 tantalum Inorganic materials 0.000 description 3
- 229910052684 Cerium Inorganic materials 0.000 description 2
- 239000004698 Polyethylene Substances 0.000 description 2
- 239000004743 Polypropylene Substances 0.000 description 2
- 229910052772 Samarium Inorganic materials 0.000 description 2
- 238000001746 injection moulding Methods 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 238000005191 phase separation Methods 0.000 description 2
- 229920001707 polybutylene terephthalate Polymers 0.000 description 2
- 229920000573 polyethylene Polymers 0.000 description 2
- 229920001155 polypropylene Polymers 0.000 description 2
- 239000002244 precipitate Substances 0.000 description 2
- 238000001556 precipitation Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 229920005992 thermoplastic resin Polymers 0.000 description 2
- 229920001187 thermosetting polymer Polymers 0.000 description 2
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical group [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 description 2
- 239000004593 Epoxy Substances 0.000 description 1
- JHWNWJKBPDFINM-UHFFFAOYSA-N Laurolactam Chemical compound O=C1CCCCCCCCCCCN1 JHWNWJKBPDFINM-UHFFFAOYSA-N 0.000 description 1
- 229920000571 Nylon 11 Polymers 0.000 description 1
- 229920000299 Nylon 12 Polymers 0.000 description 1
- 229920000265 Polyparaphenylene Polymers 0.000 description 1
- 239000006087 Silane Coupling Agent Substances 0.000 description 1
- 239000003963 antioxidant agent Substances 0.000 description 1
- 230000003078 antioxidant effect Effects 0.000 description 1
- 238000000748 compression moulding Methods 0.000 description 1
- 239000007822 coupling agent Substances 0.000 description 1
- 230000005347 demagnetization Effects 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000011978 dissolution method Methods 0.000 description 1
- 239000000806 elastomer Substances 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 230000002431 foraging effect Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 239000000088 plastic resin Substances 0.000 description 1
- 238000012805 post-processing Methods 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- KZUNJOHGWZRPMI-UHFFFAOYSA-N samarium atom Chemical compound [Sm] KZUNJOHGWZRPMI-UHFFFAOYSA-N 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
- 238000001330 spinodal decomposition reaction Methods 0.000 description 1
- BDHFUVZGWQCTTF-UHFFFAOYSA-M sulfonate Chemical compound [O-]S(=O)=O BDHFUVZGWQCTTF-UHFFFAOYSA-M 0.000 description 1
- 229920006305 unsaturated polyester Polymers 0.000 description 1
- 229910052727 yttrium Inorganic materials 0.000 description 1
- 229910000859 α-Fe Inorganic materials 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
- H01F1/057—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
- H01F1/0578—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 bonded together
Landscapes
- Chemical & Material Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Inorganic Chemistry (AREA)
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Powder Metallurgy (AREA)
- Hard Magnetic Materials (AREA)
Description
【発明の詳細な説明】
発明の背景
技術分野
本発明は、セリウム族、イツトリウム族の1種
以上からなる希土類元素RとCoとの金属間化合
物を主体としたR2Co17系Cu置換析出効果型の永
久磁石材料を熱処理して粉末とし、この粉末を用
いた粉末成型磁石の製造方法に関する。
先行技術とその問題点
重量百分比で、22〜28%のR(Rは希土類元素
の一種以上)と、Coと、Cuと、Fe、Ni、Mnお
よびCrのうちの1種以上と、Zr、Ti、Hf、Nb、
VおよびTaのうちの1種以上とからなる組成を
有する希土類コバルト系のR2Co17系Cu置換析出
硬化型の永久磁石が知られている。
この磁石は、残留磁束密度(Br)、保持力
(bHc、iHc)が大きく、エネルギー積(B.H)
maxが大きく、しかもキユリー温度が高く、温
度特性のすぐれた永久磁石である。
このような永久磁石を製造するには、公知のい
わゆる還元拡散法あるいは溶解法によつて化合物
を作製したのち、これに溶体化処理、時効処理を
施して粉砕し、磁場配向を施して、ゴムやプラス
チツク樹脂をバインダーとして粉末成型磁石とし
たり、あるいは、化合物を粉砕後、磁場成型し、
その後焼結と溶体処理化を行い、次いで時効処理
を施して焼結磁石としたりしている。
このうち特に粉末成型磁石としては、従来の粉
末成型磁石にない高い磁気特性が期待され、しか
も従来の焼結フエライトと比べ、機器の小型化が
可能で、成型後の後加工が不要で複雑形状品が得
られるなどのすぐれた利点をもつ。
このような場合、R2Co17系のCu置換型磁石の
時効処理は、スピノーダル分解を利用して、マト
リツクス中に微細な析出物を分散析出させ、この
相分離を制御して保磁力を高めるための熱処理で
ある。そして、この析出および相分離の状態が磁
石の性能を大きく左右するため、この時効処理を
最適な条件下で実施することが、製造上きわめて
重要なポイントとなるものである。
従来、R2Co17系のCu置換析出硬化型磁石の時
効処理としては、700〜900℃の温度から400℃近
傍まで多段時効する方法(特開昭50−133106号公
報)や、700〜900℃の温度から400℃近傍まで徐
冷する方法(特開昭53−106624号公報)が知られ
ている。
しかし、これら従来の方法による時効処理で
は、保磁力、残留磁束密度、エネルギー積、履歴
曲線の角形化、着磁特性等の磁気特性の点で、末
だ十分満足のできる特性が得られるには至つてお
らず、特に、10wt%以下、とりわけ8wt%以下の
低Cu量、および6wt%以上、とりわけ10wt%以
上の高Fe量の低価格の実用磁石材料組成におい
ての、磁気特性の改良が望まれている。すなわ
ち、より具体的に説明するならば、これら低Cu
量、高Fe量の実用磁石材料組成では、従来公知
の時効処理を施すことにより、12KG程度のBrが
えられ、30MGOe以上の(B・H)max値が期
待されるにもかかわらず、角形性が悪く、所期の
(B・H)max値がえられない。この場合、10wt
%よりわずかに小さいCu量の組成では、所期の
(B・H)maxより1〜2MGOe程度小さいのみ
の(B・H)max値はえられるが、従来の時効
処理では、この1〜2MGOeのエネルギー積の増
大を実現することができず、実用上大きな不都合
を生じている。
なお、Cu量を2〜3wt%程度にまで減少させた
ときには、従来の時効処理方法では、Brもきわ
めて低下してしまい、まつたく実用に耐える磁石
は実現しない。
さらには、従来の希土類コバルト系材料の時効
処理は、時効の開始温度および終了温度における
保持時間を長くとる必要があり、時効所要時間が
長いという欠点もある。
なお、従来の希土類コバルト系材料の時効処理
では、冷却の制御のしかたのみが着目されてお
り、くりかえし複数回の加熱冷却を行う例はな
い。
さらには、特開昭57−161044号公報には、1次
焼結および2次焼結を施し、等温処理後それより
高い温度から冷却する旨が開示されている。しか
し、この方法は、2回の焼結を行わなければなら
ない点できわめて煩雑であり、製造へのコストア
ツプにつながるものである。また減磁曲線の角形
化が十分でない。
さらに時効処理方法も、低温での等温処理の
後、温度を上げて次の時効処理を行なう点で本発
明の時効処理方法とは異なるものである。
また、本発明における粉末成型磁石については
開示されていない。
発明の目的
本発明は、このような実状に鑑みてなされたも
のであつて、その主たる目的は、保磁力、残留磁
束密度、エネルギー積、角形比、着磁特性等の磁
気特性が、高Fe量、低Cu量において、従来の時
効処理と比較して格段と向上し、実用上十分満足
できる磁石特性をもつ実用磁石が実現し、しか
も、時効処理時間も短縮できる熱処理方法を用い
たR2Co17系Cu置換型の粉末成型磁石の製造方法
を提供することにある。
このような目的は、下記の本発明によつて達成
される。
すなわち本発明は、重量百分比で、22〜28%
R(Rは希土類元素の一種以上)、2〜10% Cu、
6〜35% T(TはFe、Ni、MnおよびCrのう
ちの1種以上)、0.5〜6% M(MはZr、Ti、
Hf、Nb、VおよびTaのうちの1種以上)、残部
Coを主体とする組成を有する希土類コバルト系
金属間化合物を溶体化処理して急冷し、次いで、
750〜950℃の温度から700℃以下の温度まで冷却
する熱処理を2回以上くりかえし施した後、粉砕
してバインダーと混合し、磁場配向および成型を
行うことを特徴とする粉末成型磁石の製造方法で
ある。
なお、本出願の先願である特開昭58−219704号
に記載された永久磁石の製造方法は本発明と同種
の多段時効を行うものであるが、開示されている
ものは焼結磁石についてのみであり、粉末成型磁
石については開示されておらず、本発明とは異な
るものである。
発明の具体的構成
以下、本発明の具体的構成について詳細に説明
する。
本発明の粉末成型磁石は、後に詳述する組成を
有する希土類コバルト系金属間化合物を得、これ
を溶体化処理して急冷し、次いで、下記に示す熱
処理を施した後、粉砕して磁場配向と成型を行
い、バインダーに分散して製造している。
本発明の粉末成型磁石を製造するために用いる
熱処理方法においては、時効のための複数回の熱
処理に先だつて、上記のように、溶体化処理が施
される。
溶体化処理は、1000℃以上行うことが好まし
い。これは、1000℃未満では、履歴曲線の角形性
と保磁力とが低下するからである。
このような場合、溶体化処理は、通常、1000℃
〜1200℃にて、0.5〜10時間程度施される。
溶体化処理ののち、材料は急冷される。
この急冷は、一般に1〜300℃/min程度の冷
却速度で行われる。そして、急冷は、第1回目の
750〜950℃の冷却開始温度以下の任意の温度まで
行えばよい。
この後、必要に応じ所定の熱処理の冷却開始温
度までの加熱を行つたのち、複数回の熱処理が施
される。
すなわち、複数回施される各回の熱処理は、
750〜950℃の冷却開始温度から、700℃以下の冷
却終了温度までの冷却工程からなる。
そして、このような熱処理を2回以上くりかえ
すことによつて、本発明所定の効果が実現するも
のである。
この場合、くりかえし回数は、2回以上であれ
ば任意の回数であつてよいが、時効処理時間を短
縮化する上では、2〜4回であることが好まし
い。
各回の冷却開始温度は、それぞれ互いに異なつ
ていてもよいが、750〜950℃、好ましくは780〜
920℃である。
冷却開始温度が75℃未満となると析出硬化が不
十分となり、また950℃をこえると析出粒子が粗
大化して、ともに保磁力が低下してしまい不適当
である。
各回の冷却終了温度は、それぞれ異なつていて
もよいが、700℃以下である。
冷却終了温度が700℃をこえると、析出粒子が
粗大化したり、あるいは析出硬化が不十分とな
り、保磁力が低下してしまい、好ましくない。
この場合、冷却終了温度は、600℃から室温ま
での範囲、特に500℃から室温までの範囲とする
と、磁気特性向上の点で、より好ましい結果をう
る。なお、このような特性向上は、冷却終了温度
を下げるほど大きくなるが、400℃以下ではほと
んど効果はかわらない。
各回の冷却速度については特に制限はないが、
通常は、0.05〜15℃/min、より好ましくは2〜
10℃/min程度とする。
この場合、冷却プロフイールは、一旦温度を保
持する多段冷却としてもよく、必要に応じ途中で
冷却速度を変える連続冷却であつてもよい。た
だ、時効処理時間を短縮する上では、連続冷却で
あることが好ましく、特に、初期より終期の冷却
速度を減少させることが好ましい。
なお、冷却プロフイールの最適条件は、組成等
の違いに応じ、実験から容易に求めることができ
る。
さらに、各回の熱処理時間の加熱プロフイール
は任意であるが、通常は2〜10℃/min程度とす
る。
なお、冷却開始温度においては、保持時間を設
けることが好ましい。保持時間は、通常、5分〜
20時間程度であるが、好ましくは10分〜6時間が
よい。この保持時間は、くりかえしの回数、冷却
速度等の組合わせにより経験的に定める。
一方、冷却終了温度では、必ずしも保持時間を
設ける必要はない。
本発明の粉末成型磁石を製造するために上記の
ような複数回の熱処理を施す希土類コバルト系金
属間化合物の組成は、上記のものである。
この場合、22〜28wt%含有される希土類元素
Rは、セリウム系、イツトリウム系いずれの1種
以上であつてもよいが、特に好ましいのは、サマ
リウムまたはセリウムを含む場合である。
また、Cuの含有量は2〜10wt%である。
これ以外では、本発明の実効が小さくなる。
この場合、Cu含有量が、2.5〜8wt%、特に3
〜7.5wt%となると、従来の時効処理に対する磁
気特性の増大率はきわめて大きいものとなる。そ
して、きわめて良好な磁気特性をもつ磁石が実現
する。さらに、Fe、Ni、Mn、Crの1種以上の
Tは、6〜35wt%含有される。Tが、これ以外
の含有量となると、本発明の実効が小さくなる。
この場合、Tは必須元素としてFeを含み、必
要に応じ、Ni、Mn、Crの1種以上を含有する
と、より好ましい結果をうる。そして、Fe含有
量が10〜25wt%、特に14〜25wt%となると、従
来の時効処理に対する磁気特性の増大率はきわめ
て大きいものとなり、きわめて良好な磁気特性を
もつ磁石が実現する。
加えて、本発明における永久磁石材料中には、
Zr、Ti、Hf、Nb、VおよびTaのうちの少なく
とも1種以上のMが0.5〜6wt%含有される。Mが
これ以外の含有量となると、磁気特性が劣化して
しまう。
本発明の粉末成型磁石を製造するために使用す
るバインダーとしては、公知の種々の樹脂が挙げ
られる。具体的には、ゴム・エラストマー、ポリ
プロピレン(PP)、ポリエチレン(PE)、ナイロ
ン−11、12、6(PA)、ポリブチレンテレフタレ
ート(PBT)、ポリフエニレンスルホネート
(PPS)等の熱可塑性樹脂、不飽和ポリエステル、
エポキシ等の熱硬化性樹脂である。
希土類コバルト系金属間化合物を粉砕したもの
(以下金属粉末という場合がある)とそれを分散
するバインダーとの混合割合はバインダーが全体
の2〜50重量%となるようにするのがよい。
成型方法は、分散するバインダーの種類によつ
て異なり、熱可塑性樹脂の場合は射出成型、押出
成型、圧延成型等が用いられ、熱硬化性樹脂の場
合は圧縮成型等が用いられる。
一般に射出成型が用いられるが、通常射出中に
磁場を印加する。
本発明の粉末成型磁石を製造する場合、さら
に、カツプリング剤、滑剤、酸化防止剤などを添
加してもよい。
また、用いる金属粉末や磁石には表面コーテイ
ングを行つてもよい。
発明の具体的作用効果
本発明によれば、従来の時効処理を行うときと
比較して、保磁力、残留磁束密度、エネルギー
積、角形比、着磁特性等の磁気特性が向上する。
すなわち、10wt%以下の低Cu量、高Fe量の実
用磁石材料組成において、実用上十分満足できる
磁気特性がえられる。
この場合、比較的10wt%に近いCu量範囲、例
えば4〜10wt%、特に4〜8wt%においては、従
来の時効処理と比較して、Brを同等以上とした
上で、角形性が向上し、保磁力が向上するので、
所期の(B・H)max値がえられ、実用上十分
満足できる特性を示す。
このため、粉末成型磁石としての特性が優れ
る。
また、従来の時効処理ではまつたく実用に耐え
なかつた、より低Cu組成、例えば2〜4wt%、特
に2.5〜4wt%では、Bf、保磁力ともきわめて高
い増大率で増大する結果、やはり実用上十分満足
できる特性を示す。
また、各回の冷却過程において、冷却開始ない
し終了温度等での保持時間は従来より短くするこ
とができ、総体として時効処理時間は、従来より
短縮することができる。
発明の具体的実験例および実施例
以下、本発明を実験例および実施例により、さ
らに詳細に説明する。
実験例 1
重量百分比で、24.5%Sm、5%Cu、15%Fe、
2%Zr、残Coからなる合金を高周波誘導溶解に
より作製した。
これを溶体化処理し、室温まで冷却した。
これを、第1図のようなプロフイールにて、冷
却開始温度T1、冷却終了温度t1として、T1とt1を
変化させて熱処理を2回くりかえした。
第3図に、iHcとT1との関係、第4図にiHcと
t1との関係を実線にて示す。
なお、第3図、第4図には、第2図で示した従
来法である1回のみの多段時効処理のプロフイー
ルにおいて、保持時間をa=2Hr、b=1Hr、C
=1Hrとした場合の結果が破線で示される。
これらの結果から、2回以上の所定の時効熱処
理を施す本発明の効果があきらかである。
また、T1は750〜950℃、t1は700℃以下が好ま
しいこともわかる。
さらには、トータル時効処理時間も短縮されて
いることがわかる。
実施例 1
実験例1と同様に溶体化処理したのち、下記熱
処理A、B、Cを施して、表1に示すような合金
1A〜10Cを得た。
A:第1図のプロフイールにおいて、T1=850
℃、t1=400℃。
B:第5図の3回のプロフイールにおいて、T1
=900℃、T2=850℃、T3=800℃、t1=500℃、
t2=450℃、t3=400℃。
C:第2図の1回のみのプロフイールにおいて、
T1=850℃、t1=400℃、a=6Hr、b=1Hr、
c=4Hrとした場合。
このような合金1A〜10Cを粉砕し、分散す
るバインダーにナイロン12を用いて、サンプ
ル:バインダーの混合割合を重量比で94:6とし
て混合したものに、さらにシラン系のカツプリン
グ剤をそれぞれ、上記混合物に対し0.1wt%添加
して混合し、その後270℃で加熱混練した。
その後ペレツト化し、磁場中で射出成型した。
この場合射出中の印加磁場は15KOeとした。
このように成型した磁石を取出し、着磁を行つ
た。
上記のように作製した磁石を用いた合金1A〜
10Cに応じてサンプル1A〜7Cとする。
サンプル1A〜7Cの磁気特性、Br、iHc、
(B・H)maxを表2に示す。
また、表2には、これら各特性の、処理Cに対
する増大率が示される。[Detailed Description of the Invention] Background Technical Field of the Invention The present invention is directed to the R 2 Co 17 system Cu substitution precipitation effect, which is mainly composed of an intermetallic compound of Co and a rare earth element R consisting of one or more of the cerium group and the yttrium group. The present invention relates to a method of manufacturing a powder-molded magnet using a powder formed by heat-treating a permanent magnet material of a mold and using the powder. Prior art and its problems By weight percentage, 22 to 28% of R (R is one or more rare earth elements), Co, Cu, one or more of Fe, Ni, Mn and Cr, Zr, Ti, Hf, Nb,
A rare earth cobalt based R 2 Co 17 based Cu substitution precipitation hardening permanent magnet having a composition consisting of at least one of V and Ta is known. This magnet has large residual magnetic flux density (Br), coercive force (bHc, iHc), and energy product (BH)
It is a permanent magnet with a large max, a high Kyrie temperature, and excellent temperature characteristics. In order to manufacture such permanent magnets, a compound is prepared by a known reduction-diffusion method or dissolution method, and then subjected to solution treatment, aging treatment, pulverization, and magnetic field orientation to form a rubber compound. or plastic resin as a binder to make powder molded magnets, or after crushing the compound and molding it in a magnetic field,
After that, sintering and solution treatment are performed, followed by aging treatment to form a sintered magnet. Among these, powder molded magnets in particular are expected to have high magnetic properties not found in conventional powder molded magnets.In addition, compared to conventional sintered ferrite, they can be made smaller, require no post-processing after molding, and have complex shapes. It has excellent advantages such as being able to obtain high quality products. In such cases, the aging treatment of R2Co17 - based Cu-substituted magnets uses spinodal decomposition to disperse and precipitate fine precipitates in the matrix, and controls this phase separation to increase the coercive force. This is a heat treatment for Since the state of this precipitation and phase separation greatly influences the performance of the magnet, performing this aging treatment under optimal conditions is an extremely important point in manufacturing. Conventionally, aging treatments for R 2 Co 17 -based Cu substitution precipitation hardening magnets include multi-stage aging from 700 to 900°C to around 400°C (Japanese Patent Application Laid-open No. 133106/1983); A method of slowly cooling from a temperature of 10°C to around 400°C is known (Japanese Patent Application Laid-open No. 106624/1983). However, with these conventional aging treatments, it is difficult to obtain sufficiently satisfactory magnetic properties in terms of coercive force, residual magnetic flux density, energy product, hysteresis curve squaring, magnetization properties, etc. In particular, it is desirable to improve magnetic properties in low-cost practical magnet material compositions with low Cu contents of 10 wt% or less, especially 8 wt% or less, and high Fe contents of 6 wt% or more, especially 10 wt% or more. It is rare. In other words, to explain more specifically, these low Cu
In a practical magnet material composition with a high Fe content, approximately 12 KG of Br can be obtained by conventionally known aging treatment, and although a (B・H) max value of 30 MGOe or more is expected, the square shape The performance is poor and the expected (B・H) max value cannot be obtained. In this case, 10wt
%, a (B・H) max value that is only about 1 to 2 MGOe smaller than the expected (B・H) max can be obtained, but in conventional aging treatment, this 1 to 2 MGOe It is not possible to realize an increase in the energy product of , resulting in a major practical disadvantage. In addition, when the amount of Cu is reduced to about 2 to 3 wt%, Br is also extremely reduced by the conventional aging treatment method, and a magnet that can withstand practical use cannot be realized. Furthermore, the conventional aging treatment of rare earth cobalt-based materials requires a long holding time at the aging start temperature and end temperature, and has the disadvantage that the aging time is long. In addition, in the conventional aging treatment of rare earth cobalt-based materials, attention is focused only on the method of controlling cooling, and there is no example of repeated heating and cooling multiple times. Furthermore, JP-A-57-161044 discloses that primary sintering and secondary sintering are performed, and after isothermal treatment, cooling is performed from a higher temperature. However, this method is extremely complicated in that sintering must be performed twice, leading to increased manufacturing costs. Also, the demagnetization curve is not sufficiently squared. Furthermore, the aging treatment method is also different from the aging treatment method of the present invention in that after isothermal treatment at a low temperature, the next aging treatment is performed at a raised temperature. Further, the powder molded magnet in the present invention is not disclosed. Purpose of the Invention The present invention has been made in view of the above circumstances, and its main purpose is to improve magnetic properties such as coercive force, residual magnetic flux density, energy product, squareness ratio, and magnetization characteristics with high Fe. Using a heat treatment method that can reduce the aging treatment time, we have realized a practical magnet that has significantly improved Cu content and low Cu content compared to conventional aging treatment, and has magnetic properties that are sufficiently satisfactory for practical use . An object of the present invention is to provide a method for manufacturing a Co17 -based Cu-substituted powder molded magnet. These objects are achieved by the invention described below. That is, the present invention has a weight percentage of 22 to 28%.
R (R is one or more rare earth elements), 2-10% Cu, 6-35% T (T is one or more of Fe, Ni, Mn and Cr), 0.5-6% M (M is Zr, Ti,
one or more of Hf, Nb, V and Ta), remainder
A rare earth cobalt-based intermetallic compound having a composition mainly composed of Co is solution-treated and rapidly cooled, and then
A method for producing a powder molded magnet, which comprises repeating heat treatment twice or more to cool from a temperature of 750 to 950°C to a temperature of 700°C or less, followed by pulverization, mixing with a binder, magnetic field orientation, and molding. It is. The permanent magnet manufacturing method described in Japanese Patent Application Laid-Open No. 58-219704, which is an earlier application of the present application, involves multi-stage aging of the same type as the present invention, but the method disclosed is for sintered magnets. However, the powder molded magnet is not disclosed, and is different from the present invention. Specific Configuration of the Invention The specific configuration of the present invention will be described in detail below. The powder-molded magnet of the present invention is obtained by obtaining a rare earth cobalt-based intermetallic compound having a composition described in detail later, and then solution-treating and quenching it, then subjecting it to the heat treatment shown below, and then pulverizing it to align it in a magnetic field. It is manufactured by molding and dispersing it in a binder. In the heat treatment method used to manufacture the powder molded magnet of the present invention, solution treatment is performed as described above prior to multiple heat treatments for aging. The solution treatment is preferably performed at 1000°C or higher. This is because the squareness of the hysteresis curve and the coercive force decrease below 1000°C. In such cases, solution treatment is typically carried out at 1000°C.
It is applied at ~1200℃ for about 0.5 to 10 hours. After solution treatment, the material is rapidly cooled. This rapid cooling is generally performed at a cooling rate of about 1 to 300°C/min. Then, the first rapid cooling
The cooling may be carried out to any temperature below the cooling start temperature of 750 to 950°C. Thereafter, heating is performed to a cooling start temperature for a predetermined heat treatment, if necessary, and then heat treatment is performed a plurality of times. In other words, each heat treatment performed multiple times is
It consists of a cooling process from a cooling start temperature of 750 to 950°C to a cooling end temperature of 700°C or less. By repeating such heat treatment two or more times, the desired effects of the present invention can be achieved. In this case, the number of repetitions may be any number of times as long as it is two or more times, but from the viewpoint of shortening the aging treatment time, it is preferably 2 to 4 times. The cooling start temperature each time may be different from each other, but is preferably 750 to 950°C, preferably 780 to 950°C.
It is 920℃. If the cooling start temperature is less than 75°C, precipitation hardening will be insufficient, and if it exceeds 950°C, the precipitated particles will become coarse and the coercive force will decrease, which is unsuitable. The cooling end temperature for each round may be different, but is 700°C or less. If the cooling end temperature exceeds 700°C, the precipitated particles may become coarse or precipitation hardening may become insufficient, resulting in a decrease in coercive force, which is not preferable. In this case, when the cooling end temperature is set in the range from 600° C. to room temperature, particularly in the range from 500° C. to room temperature, more favorable results can be obtained in terms of improved magnetic properties. Note that such improvement in characteristics becomes greater as the cooling end temperature is lowered, but the effect remains almost unchanged below 400°C. There is no particular limit to the cooling rate each time, but
Usually 0.05-15℃/min, more preferably 2-15℃/min
The temperature should be approximately 10℃/min. In this case, the cooling profile may be multistage cooling in which the temperature is temporarily maintained, or continuous cooling in which the cooling rate is changed midway as necessary. However, in order to shorten the aging treatment time, continuous cooling is preferable, and it is particularly preferable to reduce the cooling rate in the final stage compared to the initial stage. Note that the optimum conditions for the cooling profile can be easily determined through experiments depending on the difference in composition and the like. Furthermore, although the heating profile for each heat treatment time is arbitrary, it is usually about 2 to 10°C/min. Note that it is preferable to provide a holding time at the cooling start temperature. Holding time is usually 5 minutes ~
The time is about 20 hours, but preferably 10 minutes to 6 hours. This holding time is determined empirically based on a combination of the number of repetitions, cooling rate, etc. On the other hand, at the cooling end temperature, it is not necessarily necessary to provide a holding time. The composition of the rare earth cobalt-based intermetallic compound to be subjected to the heat treatment multiple times as described above in order to produce the powder-molded magnet of the present invention is as described above. In this case, the rare earth element R contained in the range of 22 to 28 wt% may be one or more of cerium and yttrium, but it is particularly preferable to include samarium or cerium. Moreover, the content of Cu is 2 to 10 wt%. Otherwise, the effectiveness of the present invention will be reduced. In this case, the Cu content is 2.5 to 8 wt%, especially 3
When it becomes ~7.5 wt%, the rate of increase in magnetic properties compared to conventional aging treatment becomes extremely large. As a result, a magnet with extremely good magnetic properties is realized. Furthermore, T of one or more of Fe, Ni, Mn, and Cr is contained in an amount of 6 to 35 wt%. If the T content is other than this, the effectiveness of the present invention will be reduced. In this case, T contains Fe as an essential element, and if necessary, contains one or more of Ni, Mn, and Cr to obtain more preferable results. When the Fe content is 10 to 25 wt%, particularly 14 to 25 wt%, the rate of increase in magnetic properties compared to conventional aging treatment becomes extremely large, and a magnet with extremely good magnetic properties is realized. In addition, the permanent magnet material in the present invention includes:
At least one type of M selected from Zr, Ti, Hf, Nb, V, and Ta is contained in an amount of 0.5 to 6 wt%. If the M content is outside this range, the magnetic properties will deteriorate. As the binder used to manufacture the powder molded magnet of the present invention, various known resins can be mentioned. Specifically, rubber elastomers, thermoplastic resins such as polypropylene (PP), polyethylene (PE), nylon-11, 12, 6 (PA), polybutylene terephthalate (PBT), polyphenylene sulfonate (PPS), unsaturated polyester,
It is a thermosetting resin such as epoxy. The mixing ratio of the pulverized rare earth cobalt-based intermetallic compound (hereinafter sometimes referred to as metal powder) and the binder for dispersing it is preferably such that the binder accounts for 2 to 50% by weight of the total. The molding method differs depending on the type of binder to be dispersed, and in the case of a thermoplastic resin, injection molding, extrusion molding, rolling molding, etc. are used, and in the case of a thermosetting resin, compression molding, etc. are used. Injection molding is commonly used, and a magnetic field is usually applied during injection. When manufacturing the powder molded magnet of the present invention, a coupling agent, a lubricant, an antioxidant, etc. may be further added. Further, the metal powder and magnet used may be surface coated. Specific Effects of the Invention According to the present invention, magnetic properties such as coercive force, residual magnetic flux density, energy product, squareness ratio, and magnetization properties are improved compared to when conventional aging treatment is performed. That is, in a practical magnet material composition with a low Cu content of 10 wt% or less and a high Fe content, magnetic properties that are sufficiently satisfactory for practical use can be obtained. In this case, in a Cu content range relatively close to 10 wt%, for example 4 to 10 wt%, especially 4 to 8 wt%, squareness can be improved while keeping Br at the same level or higher compared to conventional aging treatment. , the coercive force improves, so
The desired (B·H)max value was obtained, and the characteristics were sufficiently satisfactory for practical use. Therefore, it has excellent characteristics as a powder molded magnet. Furthermore, at lower Cu compositions, such as 2 to 4 wt%, especially 2.5 to 4 wt%, which could not withstand practical use with conventional aging treatment, both Bf and coercive force increase at an extremely high rate, which is still impractical for practical use. Shows sufficiently satisfactory characteristics. Furthermore, in each cooling process, the holding time at the cooling start and end temperatures can be made shorter than before, and the aging treatment time as a whole can be made shorter than before. Specific Experimental Examples and Examples of the Invention Hereinafter, the present invention will be explained in more detail with reference to Experimental Examples and Examples. Experimental example 1 Weight percentage: 24.5% Sm, 5% Cu, 15% Fe,
An alloy consisting of 2% Zr and the remainder Co was produced by high frequency induction melting. This was solution treated and cooled to room temperature. The heat treatment was repeated twice by changing T 1 and t 1 with a cooling start temperature T 1 and a cooling end temperature t 1 in a profile as shown in FIG. 1. Figure 3 shows the relationship between iHc and T 1 , and Figure 4 shows the relationship between iHc and T 1.
The relationship with t 1 is shown by a solid line. In addition, in FIGS. 3 and 4, in the profile of the conventional multi-stage aging treatment shown in FIG. 2, the holding time is a=2Hr, b=1Hr,
The result when =1Hr is shown by the broken line. From these results, it is clear that the present invention is effective in performing predetermined aging heat treatment two or more times. It can also be seen that T 1 is preferably 750 to 950°C, and t 1 is preferably 700°C or less. Furthermore, it can be seen that the total aging treatment time is also shortened. Example 1 After solution treatment in the same manner as in Experimental Example 1, the following heat treatments A, B, and C were performed to obtain alloys 1A to 10C as shown in Table 1. A: In the profile shown in Figure 1, T 1 = 850
℃, t 1 = 400℃. B: In the three profiles in Figure 5, T 1
= 900℃, T 2 = 850℃, T 3 = 800℃, t 1 = 500℃,
t 2 = 450℃, t 3 = 400℃. C: In the one-time profile shown in Figure 2,
T 1 = 850℃, t 1 = 400℃, a = 6Hr, b = 1Hr,
When c=4Hr. Such alloys 1A to 10C were crushed and mixed using nylon 12 as a binder to be dispersed at a sample:binder mixing ratio of 94:6, and a silane coupling agent was added to the mixture as described above. It was added in an amount of 0.1 wt% to the mixture, mixed, and then heated and kneaded at 270°C. It was then pelletized and injection molded in a magnetic field. In this case, the applied magnetic field during injection was 15 KOe.
The magnet thus molded was taken out and magnetized. Alloy 1A using magnets prepared as above
Samples 1A to 7C correspond to 10C. Magnetic properties of samples 1A to 7C, Br, iHc,
(B・H)max is shown in Table 2. Further, Table 2 shows the increase rate of each of these characteristics with respect to treatment C.
【表】【table】
【表】
表2の結果から、本発明の効果があきらかであ
る。[Table] From the results in Table 2, the effects of the present invention are clear.
第1図は、本発明における熱処理方法の1例を
示す温度−時間プロフイールのグラフである。第
2図は、従来における熱処理方法の例を示す温度
−時間プロフイールのグラフである。第3図およ
び第4図は、それぞれ第1図および第2図のプロ
フイールのT1およびt1をかえたときの、保磁力−
T1および保磁力−t1のグラフである。この場合、
第3図および第4図において、実線が第1図のプ
ロフイールによる、破線が第2図のプロフイール
による場合である。第5図は、本発明における熱
処理方法の他の例を示す温度−時間プロフイール
のグラフである。
FIG. 1 is a temperature-time profile graph showing one example of the heat treatment method according to the present invention. FIG. 2 is a temperature-time profile graph showing an example of a conventional heat treatment method. Figures 3 and 4 show the coercive force - when T 1 and t 1 of the profiles in Figures 1 and 2 are changed, respectively.
It is a graph of T 1 and coercive force −t 1 . in this case,
In FIGS. 3 and 4, the solid line represents the profile shown in FIG. 1, and the broken line represents the profile shown in FIG. 2. FIG. 5 is a temperature-time profile graph showing another example of the heat treatment method according to the present invention.
Claims (1)
素の一種以上)、2〜10% Cu、6〜35% T
(TはFe、Ni、MnおよびCrのうちの1種以上)、
0.5〜6% M(MはZr、Ti、Hf、Nb、Vおよび
Taのうちの1種以上)、残部Coを主体とする組
成を有する希土類コバルト系金属間化合物を溶体
化処理して急冷し、次いで、750〜950℃の温度か
ら700℃以下の温度まで冷却する熱処理を2回以
上くりかえし施した後、粉砕してバインダーと混
合し、磁場配向および成型を行うことを特徴とす
る粉末成型磁石の製造方法。 2 希土類コバルト系金属間化合物のCu含有量
が2.5〜8%である特許請求の範囲第1項に記載
の粉末成型磁石の製造方法。 3 希土類コバルト系金属間化合物のTがFe、
またはFeとNi、MnおよびCrのうちの1種以上
との組合わせからなり、Fe含有量が10〜25%で
ある特許請求の範囲第1項または第2項に記載の
粉末成型磁石の製造方法。 4 溶体化処理温度が1000℃以上である特許請求
の範囲第1項ないし第3項のいずれかに記載の粉
末成型磁石の製造方法。 5 溶体化処理後の急冷終了温度が、第1回目の
750〜950℃の冷却開始温度から室温までの温度範
囲内にある特許請求の範囲第1項ないし第4項の
いずれかに記載の粉末成型磁石の製造方法。 6 熱処理の各回の冷却終了温度が、650℃から
室温までの温度範囲内にある特許請求の範囲第1
項ないし第5項のいずれかに記載の粉末成型磁石
の製造方法。 7 熱処理のくりかえし回数が2〜4回である特
許請求の範囲第1項ないし第6項のいずれかに記
載の粉末成型磁石の製造方法。 8 熱処理での各回の冷却開始温度にて、5分〜
20時間の保持時間を設ける特許請求の範囲第1項
ないし第7項のいずれかに記載の粉末成型磁石の
製造方法。 9 熱処理の各回の冷却速度が0.05〜15℃/min
である特許請求の範囲第1項ないし第8項のいず
れかに記載の粉末成型磁石の製造方法。[Claims] 1 Weight percentage: 22-28% R (R is one or more rare earth elements), 2-10% Cu, 6-35% T
(T is one or more of Fe, Ni, Mn and Cr),
0.5-6% M (M is Zr, Ti, Hf, Nb, V and
A rare-earth cobalt-based intermetallic compound having a composition mainly consisting of one or more of Ta) and the remainder Co is solution-treated and rapidly cooled, and then cooled from a temperature of 750 to 950°C to a temperature of 700°C or less. A method for producing a powder molded magnet, which comprises repeating heat treatment two or more times, then pulverizing it, mixing it with a binder, and performing magnetic field orientation and molding. 2. The method for producing a powder molded magnet according to claim 1, wherein the rare earth cobalt-based intermetallic compound has a Cu content of 2.5 to 8%. 3 T of the rare earth cobalt-based intermetallic compound is Fe,
or manufacturing a powder-molded magnet according to claim 1 or 2, which is made of a combination of Fe and one or more of Ni, Mn, and Cr, and has an Fe content of 10 to 25%. Method. 4. The method for manufacturing a powder molded magnet according to any one of claims 1 to 3, wherein the solution treatment temperature is 1000°C or higher. 5 The end temperature of quenching after solution treatment is the same as that of the first
The method for manufacturing a powder molded magnet according to any one of claims 1 to 4, wherein the temperature range is from a cooling start temperature of 750 to 950°C to room temperature. 6. Claim 1 in which the cooling end temperature of each heat treatment is within the temperature range from 650°C to room temperature.
5. A method for producing a powder molded magnet according to any one of items 5 to 5. 7. The method for producing a powder molded magnet according to any one of claims 1 to 6, wherein the heat treatment is repeated 2 to 4 times. 8 At the cooling start temperature of each heat treatment, for 5 minutes or more
A method for manufacturing a powder-molded magnet according to any one of claims 1 to 7, in which a holding time of 20 hours is provided. 9 Cooling rate for each heat treatment is 0.05 to 15℃/min
A method for manufacturing a powder molded magnet according to any one of claims 1 to 8.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP62037343A JPS62216203A (en) | 1983-02-19 | 1987-02-20 | Manufacture of powder molding magnet |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP58026859A JPS59153873A (en) | 1983-02-19 | 1983-02-19 | Heat treatment of permanent magnet material |
| JP62037343A JPS62216203A (en) | 1983-02-19 | 1987-02-20 | Manufacture of powder molding magnet |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP58026859A Division JPS59153873A (en) | 1983-02-19 | 1983-02-19 | Heat treatment of permanent magnet material |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS62216203A JPS62216203A (en) | 1987-09-22 |
| JPH0231483B2 true JPH0231483B2 (en) | 1990-07-13 |
Family
ID=26364711
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP62037343A Granted JPS62216203A (en) | 1983-02-19 | 1987-02-20 | Manufacture of powder molding magnet |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS62216203A (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6136099A (en) * | 1985-08-13 | 2000-10-24 | Seiko Epson Corporation | Rare earth-iron series permanent magnets and method of preparation |
| US5538565A (en) * | 1985-08-13 | 1996-07-23 | Seiko Epson Corporation | Rare earth cast alloy permanent magnets and methods of preparation |
| US5213631A (en) * | 1987-03-02 | 1993-05-25 | Seiko Epson Corporation | Rare earth-iron system permanent magnet and process for producing the same |
-
1987
- 1987-02-20 JP JP62037343A patent/JPS62216203A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS62216203A (en) | 1987-09-22 |
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