JPH045738B2 - - Google Patents

Info

Publication number
JPH045738B2
JPH045738B2 JP58161627A JP16162783A JPH045738B2 JP H045738 B2 JPH045738 B2 JP H045738B2 JP 58161627 A JP58161627 A JP 58161627A JP 16162783 A JP16162783 A JP 16162783A JP H045738 B2 JPH045738 B2 JP H045738B2
Authority
JP
Japan
Prior art keywords
less
composition
sintering
permanent magnet
magnet material
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
Application number
JP58161627A
Other languages
Japanese (ja)
Other versions
JPS6052556A (en
Inventor
Hitoshi Yamamoto
Masato Sagawa
Setsuo Fujimura
Yutaka Matsura
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Proterial Ltd
Original Assignee
Sumitomo Special Metals Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Sumitomo Special Metals Co Ltd filed Critical Sumitomo Special Metals Co Ltd
Priority to JP58161627A priority Critical patent/JPS6052556A/en
Priority to US06/532,471 priority patent/US4601875A/en
Priority to CA000436891A priority patent/CA1287509C/en
Priority to EP83109508A priority patent/EP0126802B2/en
Priority to DE8383109508T priority patent/DE3378707D1/en
Publication of JPS6052556A publication Critical patent/JPS6052556A/en
Priority to SG594/90A priority patent/SG59490G/en
Priority to HK753/90A priority patent/HK75390A/en
Publication of JPH045738B2 publication Critical patent/JPH045738B2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Powder Metallurgy (AREA)
  • Hard Magnetic Materials (AREA)

Description

【発明の詳細な説明】[Detailed description of the invention]

本発明は新規な希土類石材料の製造方法に係
り、FeBRをベースとして添加元素M1を含み特
にSmなどの希少希土類金属を必ずしも必要とせ
ず資源的に豊富でかつ用途が少ないNdやPrを中
心とする軽希土類とFeを主成分とする高性能な
永久磁石材料の製造方法に関する。 永久磁石材料は一般家庭の各種電気製品から大
型コンピユーターの周辺端末機器まで巾広い分野
で使用されている極めて重要な電気・電子材料の
一つである。近年電気機器の小型化、高効率化の
要求にともない、永久磁石材料はますます高性能
化が求められている。また実用的にはモーター用
発電機用磁気カツプリング用など極めて大きい逆
磁界のかかる用途も多く高保磁力を有する磁石材
料も求められている。 現在使用されている永久磁石のうち代表的なも
のはアルニコ、ハードフエライト、および希土類
コバルト磁石である。最近の高い磁石特性を満た
す永久磁石としては希土類コバルト磁石である。
しかし希土類コバルト磁石は資源的に希少なSm
を必要とし供給が不安定なCoを多量に使用する
ため非常に高価である。 希土類磁石材料がもつと広い分野でかつ多量に
使用されるようになるためには高価なコバルトを
多量に含まず希土類金属として鉱石中に多量に含
まれている軽希土類を主成分とすることが必要で
ある。そのような永久磁石材料への一つの試みと
してRFe2系化合物(但しRは希土類金属の少な
くとも1種)が提案された。クラーク(A.E.
Clark)はスパツタリングにより得られた非晶質
TbFe2は4.2°Kで29.5MGOeのエネルギー積をも
ち、これを300〜500℃で熱処理すると室温で保磁
力は3.4kOe,最大エネルギー積は7MGOeを示す
ことを見い出した。同様な研究はSmFe2につい
ても行われ77°Kで9.2MGOeを示すことが報告さ
れている。 しかしこれらのものはどれもスパツタリングに
より作成された薄膜であり一般のスピーカーやモ
ーターに使用できる磁石ではない。またPrFe系
合金の超急冷により作製したリボンが2.8kOeの
高保磁力を示すことが報告されている。さらにク
ーン等は(Fe.B)0.9Tb0.05La0.05の超急冷により得
られた非晶質リボンを627℃で焼鈍すると保磁力
が9kOeにも達することを見い出した(Brは
5kG)。しかしこの場合磁化曲線の角形性が悪い
ため最大エネルギー積は低い(N.C.Koon他
Appl.Phys.Lett.39(10)1981,840〜842頁)。 またカバコフ(L.Kabacoff)等は(FeB)1-X
Prx(x=0〜0.3原子比)の組成の超急冷で作製
したリボンはFe・Pr2成分系で室温でkOeレベル
の保磁力をもつものがあると報告している。これ
らの超急冷でのリボン又はスパツタリングによる
薄膜はそれ自体として使用可能な実用永久磁石
(体)ではなく、これらのリボンや薄膜から実用
永久磁石を得ることは出来ない。即ち従来提案さ
れているFeBR系のリボン又はRFe系の薄膜から
は任意の形状・寸法を有するバルク永久磁石体を
得ることは出来ない。又これまでに報告された
FeBR系のリボンの磁化曲線は角形性が悪く従来
慣用されている磁石に対抗できる実用永久磁石材
料とはみなされない。更に超急冷でのリボン、ス
パツタリングによる薄膜はいずれも本質上等方性
であり、これから磁気異方性の実用永久磁石を得
ることは事実上不可能であつた。 本発明の目的は従来の欠点を除去したSm等の
希少な希土類を必ずしも用いる必要がなくCo等
資源的に問題のある成分を多く含まない新規な永
久磁石材料を得ることを基本目的とする。さら
に、本発明は、室温で良好な磁石特性を有し任意
の形状・実用寸法に成形でき、磁化曲線の角形性
が高いものであり、資源的に豊富な軽希土類元素
を有効に使用可能な永久磁石材料を簡便に得るた
めの製造方法を提供せんとするものである。 本発明者等は先にSm,Coを必ずしも用いる必
要のないFeBR系永久磁石材料を発明した(特願
昭57−145072)。このFeBR系永久磁石材料は、
従来知られているRCo5やR2Co17化合物とは異な
る新しい化合物を基礎とし、特にボロンBは、従
来の、たとえば非晶質合金作成時の非晶質促進元
素又は粉末治金法における焼結促進元素として添
加されるものではなく、このFeBR系永久磁石材
料の実体的内容を構成する磁気的に安定で高い磁
気異方性定数を有するR−Fe−B化合物の必須
構成元素であることを明らかにした(なお、上記
FeBR系永久磁石材料に基づき、適当なミクロ組
織を形成することによつて磁気異方性焼結永久磁
石が得られることも明らかにした)。更に、こう
したFeBR系永久磁石材料が、所定の組成を有す
る平均粒度0.3〜80μmの合金粉末(組成物)を成
形し、非酸化性雰囲気において900〜1200℃で焼
結することによつて製造できることも発明し、別
途出願した(特願昭58−88372)。 本発明者らは前記目的を達成するため更にこう
したFeBR三元化合物に基づく結晶質の永久磁石
材料の製法について鋭意研究したところFeBR系
をベースとしFeの一部をCoで置換し、添加元素
M1(Ti,Zr,Hf,HN,Ni,Ge,Sn,Bi,Sb)
を含むFeCoBRM1系の一定の組成範囲の合金粉
末を成形し、焼結し、更に熱処理することにより
磁石特性、特に保磁力と角形性が著しく優れた永
久磁石材料が得られることを見い出し本願発明に
至つたものである。 即ち、本発明によれば、原子百分率で8〜30%
のR(但しRはYを包含する希土類元素の少なく
とも1種)、2〜28%のB、所定%以下の添加元
素M1の1種又は2種以上 (但しM10%を除き、M1は Ti 4.5%以下、 Zr 5.5%以下、 Hf 5.5%以下、 Mn 8.0%以下、 Ni 8.0%以下、 Ge 7.0%以下、 Sn 3.5%以下、 Bi 5.0%以下、 及びSb 2.5%以下であり、 2種以上のMを含む場合M1の合量は含有する
M1の当該各元素のうち最大値を有するものの所
定%以下)、及び残部実質上Fe(製造上不可避の
不純物を含む)からなるFeBRM1系組成のうち
Feの一部を全組成に対して50%以下のCo(0%を
除く)で置換してなる組成(FeCOBRM1組成)
を有し、900〜1200℃で焼結してなる焼結体を、
350℃〜当該焼結温度以下で熱処理することを特
徴とする永久磁石材料の製造方法によつて、上記
目的を達成できる。 上記熱処理によつて、同一組成の焼結体に対し
他の磁気特性を劣化させることなく保磁力の顕著
な増大が得られる。この点は、例えば希土類元素
Rの増加による保磁力の増大の場合残留磁化の減
少をもたらすこと(特願昭57−145072号参照)に
対比するとその意義は極めて大きい。所定量の
M1の存在はこの熱処理による保磁力増大の効果
をさらに高めると共に、Coの存在により実用上
十分高いキユリー点を実現している。 又、このFeCoBRM1系組成にさらに所定%以
下の元素X(Cu3.5%以下、S2.0%以下、C4.0%以
下及びP3.5%以下)の一種又は二種以上を含有し
てなるFeCoBRM1系組成についても同様な焼結
後の熱処理の効果が達成できる。 なおかかる焼結体を前記先願におけるように所
定の組成を有する平均粒度0.3〜80μmの合金粉末
組成物を成形、特に非酸化性雰囲気で焼結するこ
とによつて得ることが好ましい。こうして得られ
る永久磁石材料は、上記FeCoBRM1系組成にお
いて磁気異方性の場合特に優れた磁気特性を示
す。 本発明製法は、従来のFeBR系アモルフアスリ
ボンと異なり磁気異方性の永久磁石材料が得られ
る点で特徴的であるが、等方性のものも従来の等
方性永久磁石材料に比して優れたものが得られ
る。以下、まず主として磁気異方性永久磁石材料
を製造する場合を基本として説明する。 本発明の永久磁石材料の製法において、FeBR
系組成においてFeをCoにより一部置換すること
により磁石材料の温度特性を改善すると共に添加
元素M1の添加及び時効処理により保磁力及び角
形性を改善するものであるが、更には希土類元素
Rとして資源的に豊富なNdやPrなどの軽希土類
を用いて高い磁気特性を発現させるものである。 一般にFe合金へのCoの添加は添加量の増大に
よりキユリー点Tcが上昇するものと下降するも
のがあり、一般的に添加効果を予測することは困
難である。本発明においてFeのCoによる置換の
結果はCoの置換量の増大に伴いTcは徐々に増大
することが明らかとなつた。又磁石材料組成のR
の種類によらず同様な傾向が確認される。Coの
置換量はわずかでも(例えば1%でも)Tc増大
に有効であり、Coの置換量により約310〜約750
℃の任意のTcをもつ合金が得られるがCo量は50
%(以下%は合金中の原子百分率を示す)以下で
十分効果が得られ、CoはiHc 1kOe以上とするた
め50%以下とする(以下%は合金中の原子百分率
を示す)。 Bは保磁力が1kOe以上を満たすために2%以
上とし、ハードフエライトの残留磁束密度Br約
4kG以上とするためには28%以下である。希土類
元素Rは保磁力1kOe以上とするため8%以上必
要であり、また燃え易く工業的取扱・製造上の困
難のため、また高価であることから30%以下とす
る。Bとしては純ボロン又はフエロボロンを用い
ることが出来、不純物としてAl,Si,Cなどを
含むものを用いることが出来る。 Rとしては資源的に豊富な軽希土類を用いるこ
とができ必ずしもSmを必要とせず或いはSmを主
体とする必要もないので原料が安価でありきわめ
て有用である。本発明の永久磁石材料は従来の
RCo磁石材料に比べて資源的、価格的いずれの点
においても有利であり磁気特性の上からも一層優
れたものが得られる。本発明で明るい希土類元素
RはYを含有し、軽希土類及び重希土類を包含す
る希土類元素であり、そのうち一種以上を用い
る。即ちこのRとしてはNd,Pr,La,Ce,Tb,
Dy,Ho,Er,Eu,Sm,Gd,Pm,Tm,Yb,
Lu及びYが包含される。Rとしては軽希土類を
もつて足り、特にNd,Prが好ましい。また通例
Rとして一種をもつて足りるが実用上は2種以上
の混合物(ミツシユメタル、ジジム等)を入手上
の便宜等の理由により用いることができ、Sm,
Y,La,Ce,Gd等は他のR、特にNd,Pr等と
の混合物として用いることができる。なおRとし
ては純希土類元素でなくともよく工業上入手可能
な範囲で製造上不可避な不純物を含有するもので
も用いることが出来る。 本発明によつて製造される永久磁石材料におい
て添加元素M1は保磁力を増大させる効果をもつ
ている。保磁力の増大は磁石の安定性を増し、そ
の用途が拡大される。しかしM1はその増大につ
れてBrが低下していき、そのため最大エネルギ
ー積(BH)maxが減少する。(BH)maxは少し
低くなつても高い保磁力Hcが必要とされる用途
は最近ことに多くなつてきたためM1を含む合金
は大変有用であるが(BH)maxは4MGOe以上
の範囲で有用である。 添加元素M1の夫々の添加によるBrへの及ぼ
す効果を明らかにするためその添加量を変化させ
てBrの変化を測定しハードフエライトのBr約
4kGと同等以上をその範囲とする。またハードフ
エライトの(BH)max約4MGOeと同等以上の
範囲を考慮しM1の添加量の上限は Ti 4.5%以下、 Zr 5.5%以下、 Hf 5.5%以下、 Mn 8.0%以下、 Ni 8.0%以下、 Ge 7.0%以下、 Sn 3.5%以下、 Bi 5.0%以下、 及びSb 2.5%以下である。 M1は0%を含まずまた1種もしくは2種以上
を添加することが出来る。2種以上含有する場合
には各添加元素の特性の中間の値を一般に示し
夫々の元素の含有量は上記%の範囲内でかつその
合量が各元素に対する上記%の最大値以下とす
る。 前記FeCoBRM1組成の範囲内の場合、最大エ
ネルギー積(BH)maxはハードフエライト磁石
(〜4MGOe)と同等あるいはそれ以上となる。
また軽希土類元素(特にNd,Pr)を全R中の50
%以上含有し、かつ12〜24%のR,3〜27%の
B,Co50%以下(但しCo0%を除く)、添加元素
M1はTi4.0%以下、Zr4.5%以下、Hf4.5%以下、
Mn6.0%以下、Ni3.5%以下、Ge5.5%以下、
Sn2.5%以下、Bi4.0%以下、及びSb1.5%以下で
あり、M1の合量は含有するM1の当該各含有元素
のうち最大値を有するものの原子百分率以下、残
部は実質的にFeの組成範囲の場合、(BH)max
は7MGOe以上と好ましい範囲となる。さらに最
も好ましい範囲は軽希土類元素(特にNd,Pr)
を全R中の50%以上含有し、かつ12〜20%のR、
4〜24%のB,Co50%以下(但しCo0%を除く)、
添加元素M1はTi3.5%以下、Zr3.5%以下、Hf3.5
%以下、Mn4.0%以下、Ni2.0%以下、Ge4.0%以
下、Sn1.0%以下、Bi3.0%以下、及びSb0.5%以
下であり、M1の合量は含有するM1の当該各含有
元素のうち最大値を有するものの原子百分率以
下、残部は実質的にFeの組成範囲の場合、(BH)
maxは10MGOe以上十分可能であり、最高の最
大エネルギー積は33MGOe以上に達する。また
本発明のFe−Co−B−R−M1合金はCo5%以上
で残留磁束密度(Br)の温度係数(α)はα≦
0.1%/℃となり、温度特性が良好となり、Coを
含有しないFe−B−R合金に比較して良好な温
度特性を有するのみならず、Co添加により減磁
曲線の各形性が改善されるため、最大エネルギー
積の向上がはかれる。Co25%以下において、他
の磁気特性(特にエネルギー積)は実質上悪影響
を受けない。Coが25%をこえると、(BH)max
は減少する。また、CoはFeに比べて耐蝕性を有
するので、Fe−B−R合金にCoを添加すること
により耐蝕性を付与することが可能である。 本発明によつて製造されるFeCoBRM1系焼結
体から成る永久磁石材料は、Fe,Co,B,R,
M1の外Cu,C,S,P,Ca,Mg,O,Si等を
少量含有することも可能であり、製造性改善、低
価格化が可能となる。特に、Cu3.5%以下、S2.0
%以下、C4.0%以下、P3.5%以下(但しその合量
は当該各元素の最大値以下)が実用上好ましい。
こうした元素の含有によつても、なおハードフエ
ライトと同程度のBr(4kG程度)以上であり、有
用である。さらにCa,Mgについては夫々4%以
下、O,Sについては夫々2%以下(但しその合
量は当該各元素の最大値以下)とすることが好ま
しい。なお、Cu,Pは安価な原料から、Cは有
機成形助剤等から、Sは製造工程から混入するこ
ともある。また、合金粉末の状態においては、処
理工程、空気からの吸着成分(水分、酸素等)が
含まれ易いが、これらは焼結時に除去することが
できる。但し、必要に応じて工程、保存に注意す
る。その他、工業的製造上不可避な不純物の存在
を許容できる点で本発明は実用的である。 以下本発明の製造方法を磁気異方性永久磁石材
料を製造する場合について更に説明する。 まず出発原料となる前記FeCoBRM1組成の合
金粉末(組成物)を得る。これは通常の合金溶
解・鋳造で得た合金鋳塊を粉砕して分級、配合等
により供してもよく、あるいはCa等の還元剤を
用いて酸化物から還元法によつて得てもよいが、
FeCoBRM1合金粉末の平均粒度0.3〜80μmのも
のを用いることが好ましい。平均粒度80μmをこ
えるとすぐれた磁石特性が得られない。平均粒度
0.3μmより下では、微粉砕中ないしその後の製造
工程において、粉末の酸化が著しくなり、焼結後
の密度が上がらず得られる磁石特性も低い。平均
粒度40〜80μmの範囲では磁石特性のうち保磁力
がやや低い。優れた磁石特性を得るためには合金
粉末の平均粒度として、1.0〜20μmが最も望まし
い。 粉砕は通常の方法でよく、不活性ガス雰囲気中
で行なう乾式粉砕又は有機溶媒中で行なう湿気粉
砕のいずれでもよい。湿気で行なう場合、アルコ
ール系溶媒、ヘキサン、トリクロルエタン、トリ
クロルエチレン、キシレン、トルエン、フツ素系
溶媒、パラフイン系溶媒などを用いることができ
る。 次に合金粉末を成形する。成形は通例の粉末治
金法と同様に行うことができ、加圧成形が好まし
く、異方性とするためには、磁界中でプレスす
る。例えば、合金粉末を5k0e以上の磁界中で0.5
〜3.0Ton/cm2の圧力で加圧することにより成形
体と成す。この磁界中加圧成形は粉末をそのまま
成形する方法、アセトン、トルエン等有機溶媒中
成形する方法いずれも可能である。 次に、この成形体を還元性ないし非酸化性雰囲
気中で所定温度(900〜1200℃)にて焼結する。
例えば、この成形体を10-2Torr以下の真空中な
いし、1〜760Torr、純度99.9%以上の不活性ガ
スないし還元性ガス雰囲気中で900〜1200℃の温
度範囲で0.5〜4時間焼結する。焼結温度900℃よ
り下では十分な焼結密度が得られず、高い残留磁
束密度も得られない。また1200℃より上では焼結
体が変形し結晶粒の配向がくずれるため残留磁束
密度の低下と減磁曲線の角形性が低下する。また
焼結時間は5分以上あればよいが余り長時間にな
ると量産性に問題があるので、磁石特性の再現性
を考慮すると、0.5〜4時間の焼結時間が望まし
い。なお、焼結工程は、焼結の進行と共に密度が
増大し、十分な密度に達するまでの加熱工程と考
えられる。 焼結雰囲気は本合金中の成分であるRが高温で
極めて酸化しやすいので、非酸化性雰囲気である
高真空中あるいは不活性ガス、還元性ガス雰囲気
中にて行うが、不活性ガス、還元性ガスの純度は
高い方がよい。不活性ガスを用いる場合は高い焼
結密度を得る方法として1〜760Torr未満の減圧
雰囲気中で行うことも可能である。 焼結時の昇温速度は特に規定しないが、前記式
気プレス方式の場合には有機溶媒の溶媒除去をお
こなうため昇温速度30℃/min以下で昇温を行う
か或いは昇温途中で200〜800℃の温度範囲で約1
時間以上保持して溶媒除去をおこなうことが望ま
しい。 焼結後、室温までの冷却速度は30℃/min以上
が製品のバラツキを少なくするために好ましく、
引続く熱処理(時効処理)により磁石特性を高め
るためには冷却速度として150℃/min以上が望
ましい(但し、焼結に続いて直ちに熱処理工程に
入れることもできる。)。 時効処理は真空ないし不活性ガスないし還元性
ガス雰囲気中で350℃から焼結温度以下の温度範
囲で、凡そ5分から70時間おこなう。時効処理の
雰囲気としては合金中の主成分のRが高温で酸素
或いは水分と急激に反応するので、真空の場合は
真空度10-3Torr以下、不活性ガス、還元性ガス
雰囲気の場合は雰囲気の純度99.99%以上が望ま
しい。 本発明合金の最適焼結温度は組成により
異なり、時効処理は本発明磁石材料の各焼結温度
以下で行う必要がある。例えば
71Fe5Co8B14Nd2Ti合金、
52Fe25Co5B17Nd1Mn合金では時効処理の上限
温度は各々950℃、1000℃である。一般にFeに富
むあるいはBが少ない、あるいはRが少ない組成
ほど上限時効処理温度を高くできる。しかし、時
効処理温度が高すぎると、本発明合金の結晶粒が
過剰成長し、磁石特性とりわけ保磁力の低下をも
たらすとともに、最適時効処理時間が極めて短時
間となり製造条件の制御が困難となり実用的でな
い。また350℃より下では時効処理時間に極めて
長時間を要するため実用的でなく、かつ減磁曲線
の角形性が低下し優れた永久磁石にならない。本
発明で得られる永久磁石材料の結晶粒の過剰成長
を起さずに優れた磁石特性を実用的に得るには時
効処理温度として450℃から800℃が最も望まし
い。時効処理は5分から70時間おこなうが、時効
処理時間が5分未満では時効処理の効果はほとん
ど現れず、また得られる磁石特性のバラツキも大
きい。一方、時効処理が70時間をこえると工業的
に長時間を要しすぎるため実用的とはいいがた
い。優れた磁石特性を実用的に再現性良く得るに
は時効処理時間として30分から8時間が最も望ま
しい。 また本発明製法において磁石合金の時効処理の
手法として2段以上の多段時効処理も有効であ
り、例えば1100℃で焼結した68Fe−5Co−7B−
18Nd−2Ge合金では1段目として800℃〜900℃
の温度範囲で30分から8時間の初段時効処理を行
つたのち、2段目以降は400〜800℃の温度範囲で
2時間から70時間の1回以上の時効処理を行うこ
とにより、残留磁束密度、保磁力、減磁曲線の角
形性のともに高い優れた磁石特性が得られる。と
しわけ2段目以降の時効処理は保磁力の著しい向
上に効果がある。また時効処理の別手法として多
段時効処理の代りに時効処理時350℃から950℃の
温度範囲を空冷・水冷等の冷却方法により一定の
冷却速度で冷却を行つても同等の磁石特性が得ら
れるが、その際の冷却速度は0.2℃/min〜20
℃/secであることが必要である。なおこれら時
効処理は焼結後そのまま行つても、焼結後一旦室
温まで冷却後再び昇温して行つても同等の磁石特
性が得られる。 また本発明の製造方法は磁気異方性永久磁石材
料のみならず、等方性永久磁石材料にも適用でき
る。なお等方性永久磁石材料の製造方法において
は合金粉末を磁界中でなく成形するほか他工程は
そのまま利用することが出来る。 等方性の場合には、R10〜25%、B3〜23%、
50%以下のCo、所定%のM1、残部Fe及び不可
避の不純物から成る組成において、(BH)
max2MGOe以上が得られる。等方性磁石材料は
元来異方性磁石材料の磁気特性の1/4〜1/6の低い
特性のものであるが、本発明によれば、それにも
かかわらず、等方性としては極めて有用な高い特
性が得られる。 等方性の場合も、R量が増加するに従つてiHc
は増加するが、Brは最大値を経た後減少する。
かくて(BH)max2MGOe以上を満足するR量
は10%以上でかつ25%以下である。 またB量が増大するに従いiHcは増大するがBr
は最大値を経た後減少する。かくて(BH)
max2MGOe以上を得るにはB3〜23%の範囲でな
ければならない。 好ましくは軽希土類(特にNd,Pr)をRの主
成分(全R中希土類が50原子%以上)とし12〜20
%のR、5〜18%のB、残部Feの組成で(BH)
max4MGOe以上の高い磁気特性を示す。最も好
ましい範囲としてNd,Pr等の軽希土類をRの主
成分とし12〜16%のR、6〜18%のB残部Feの
組成では(BH)maxが7MGOe以上で等方性永
久磁石材料ではかつて無い特性が得られる。 M1としては、下記の外は異方性の場合と同じ
範囲が好ましい(Ti4.7%以下、Ni4.7%以下、
Ge6.0%以下)。いずれのM1成分も等方性の場
合、その添加量の増大と共にBrは減少傾向を示
し、Br3kG以上(等方性ハードフエライトの
(BH)max2MGOeのレベルと同等以上とするた
め)をこの範囲内で示す。 結合剤、滑剤は、異方性の場合には、成形の際
の配向を妨げるため一般には用いられないが、等
方性磁石材料の場合には、結合剤、滑剤等を含む
ことによりプレス効率の改善、成形体の強度増大
等が可能である。 等方性の場合もR,B,Fe,Co,M1の他に所
定範囲内でC,P,S,Cu,Ca,Mg,O,Siが
含有されることもでき、C4.0%以下、P3.3%以
下、S2.5%以下、Cu3.3%以下、Ca4%以下、
Mg4%以下、O2%以下、Si2%以下(但しこれら
の合計は、各成分のうち最大値以下)が実用上好
ましい。なお、その他工業的製造上不可避な不純
物の存在を許容できる点も異方性材料におけるも
のと同様である。 以上詳述の通り本発明の永久磁石材料の製造方
法は新規なFeCoBRM1系の高保磁力・高エネル
ギー積を備える優れた磁石特性を有し、又Rとし
てNd,Pr等の軽希土類元素を用いることにより
資源的・価格的などの点においても優れた永久磁
石材料を簡便に製造でき、工業的利用性の高いも
のである。特に、Feの一部をCoで置換すること
によつてより実用的なキユリー温度を有するもの
を得ることができ、又所定の元素M1を含有させ
ると共に所定の時効処理を施すことによつて、結
晶質のFeCoBRM1系永久磁石材料について、よ
り一層の保磁力の向上及び減磁曲線の角形性の向
上を実現したものである。 以上本発明の態様及び効果について、さらに実
施例に従つて説明する。但し実施例及び記載の態
様は、本発明をこれらに限定するものではない。 表1〜4は、つぎの工程によつて作製した種々
のFeCoBRM1系組成から成る永久磁石材料の特
性を示す。 (1) 出発原料はFeとして純度99.9%(重量%、以
下原料純度について同じ)の電解鉄、Bとして
フエロボロン合金(19.38%B、5.32%Al、0.74
%Si、0.03%C、残部Fe)、Rとして純度99%
以上(不純物は主として他の希土類金属)を使
用。 Coは純度99.9%の電解Coを使用した。M1と
しては純度99%のTi,Bi,Mn,Sb,Ni,Sn,
Ge、95%のHf、及びZrとして77.5%のZrを含
むフエロジルコニウムを使用した。 (2) 磁石原料を高周波誘導を用いて溶解を行つ
た。その際ルツボとしてはアルミナルツボを用
い水冷銅鋳型中に鋳込みインゴツトを作つた。 (3) 溶解で得られたインゴツトを搗砕し−
35meshにしたのち更にボールミルにより所定
の平均粒度のものが得られるように粉砕を行つ
た。 (4) 粉末を磁界中で所定の圧力で成形した(但し
等方性磁石材料を製造する場合は磁界をかけな
いで成形した。)。 (5) 成形体は900〜1200℃の範囲内の所定の雰囲
気焼結を行い、その後所定の熱処理を行つた。 実施例 1 原子百分率組成57Fe・15Co・9B・17Nd・2Ti
なる平均粒度4μmの合金粉末を15kOe磁界中で
1.0Ton/cm2の圧力で加圧成形した後、99.99%純
度の150Torr Ar中で1120℃、2時間焼結し、焼
結後は冷却速度500℃/minで室温まで冷却した。
さらに時効処理を700℃で20分、120分、240分、
3000分行い、本発明製法に係る磁石材料を得た。
磁石特性結果および本合金磁石の残留磁束密度
(Br)の温度係数α(%/℃)を比較例(焼結後)
とともに表1に示す。
The present invention relates to a method for producing a novel rare earth stone material, which is based on FeBR and contains an additive element M1, and in particular does not necessarily require rare rare earth metals such as Sm, and is mainly made of Nd and Pr, which are rich in resources and have few uses. The present invention relates to a method for producing high-performance permanent magnet materials whose main components are light rare earth elements and Fe. Permanent magnetic materials are one of the extremely important electrical and electronic materials used in a wide range of fields, from various household appliances to peripheral terminal equipment for large computers. In recent years, with the demand for smaller and more efficient electrical equipment, permanent magnet materials are required to have even higher performance. Furthermore, there is a need for magnetic materials with high coercive force in many practical applications where extremely large reverse magnetic fields are applied, such as magnetic couplings for motor generators. Representative permanent magnets currently in use are alnico, hard ferrite, and rare earth cobalt magnets. A recent permanent magnet that satisfies high magnetic properties is a rare earth cobalt magnet.
However, rare earth cobalt magnets are Sm
It is very expensive because it uses a large amount of Co, which is unstable in supply. In order for rare earth magnet materials to be used in large quantities in a wide range of fields, it is necessary to use light rare earth metals, which are found in large amounts in ores as rare earth metals, as the main component, without containing large amounts of expensive cobalt. is necessary. As an attempt to develop such a permanent magnet material, an RFe 2 compound (where R is at least one kind of rare earth metal) has been proposed. Clark (AE
Clark) is an amorphous material obtained by sputtering.
We found that TbFe 2 has an energy product of 29.5 MGOe at 4.2°K, and when it is heat-treated at 300-500°C, it exhibits a coercive force of 3.4 kOe and a maximum energy product of 7 MGOe at room temperature. A similar study was conducted on SmFe 2 , which was reported to exhibit 9.2 MGOe at 77°K. However, all of these are thin films created by sputtering and are not magnets that can be used in general speakers or motors. It has also been reported that ribbons made by ultra-rapid cooling of PrFe-based alloys exhibit a high coercive force of 2.8 kOe. Furthermore, Kuhn et al. found that when an amorphous ribbon obtained by ultra-quenching of (Fe.B) 0.9 Tb 0.05 La 0.05 was annealed at 627°C, the coercive force reached as high as 9 kOe (Br
5kG). However, in this case, the maximum energy product is low due to poor squareness of the magnetization curve (NCKoon et al.
Appl. Phys. Lett. 39 (10) 1981, pp. 840-842). Also, L.Kabacoff et al. (FeB) 1-X
It has been reported that ribbons fabricated by ultra-quenching with a composition of Pr x (x = 0 to 0.3 atomic ratio) have a coercive force of kOe level at room temperature due to the Fe/Pr two component system. These ultra-quenched ribbons or thin films produced by sputtering are not practical permanent magnets (bodies) that can be used as such, and practical permanent magnets cannot be obtained from these ribbons or thin films. That is, it is not possible to obtain a bulk permanent magnet body having arbitrary shapes and dimensions from the FeBR-based ribbons or RFe-based thin films that have been proposed so far. Also reported so far
The magnetization curve of FeBR-based ribbons has poor squareness and is not considered a practical permanent magnet material that can compete with conventionally used magnets. Furthermore, ribbons produced by ultra-quench cooling and thin films produced by sputtering are essentially isotropic, and it has been virtually impossible to obtain practical permanent magnets with magnetic anisotropy from them. The basic object of the present invention is to obtain a new permanent magnet material that eliminates the drawbacks of conventional materials, does not necessarily require the use of rare rare earths such as Sm, and does not contain many components that are problematic in terms of resources such as Co. Furthermore, the present invention has good magnetic properties at room temperature, can be formed into any shape and practical size, has a highly square magnetization curve, and can effectively use light rare earth elements, which are abundant in resources. The present invention aims to provide a manufacturing method for easily obtaining a permanent magnet material. The present inventors previously invented a FeBR-based permanent magnet material that does not necessarily require the use of Sm and Co (Japanese Patent Application No. 145072/1982). This FeBR-based permanent magnet material is
It is based on a new compound different from the conventionally known RCo 5 and R 2 Co 17 compounds, and in particular boron B can be used as an amorphous promoting element in the production of amorphous alloys or as an sintering agent in powder metallurgy. It is not added as a crystallization promoting element, but is an essential constituent element of the R-Fe-B compound that is magnetically stable and has a high magnetic anisotropy constant, which constitutes the substantial content of this FeBR-based permanent magnet material. (In addition, the above
It was also revealed that magnetically anisotropic sintered permanent magnets can be obtained by forming an appropriate microstructure based on FeBR-based permanent magnet materials). Furthermore, such FeBR-based permanent magnet materials can be manufactured by molding alloy powder (composition) with a predetermined composition and an average particle size of 0.3 to 80 μm, and sintering it at 900 to 1200°C in a non-oxidizing atmosphere. He also invented the invention and filed a separate application (Patent Application 1988-88372). In order to achieve the above object, the present inventors further conducted intensive research on the production method of crystalline permanent magnet materials based on such FeBR ternary compounds.
M1 (Ti, Zr, Hf, HN, Ni, Ge, Sn, Bi, Sb)
It was discovered that a permanent magnet material with extremely excellent magnetic properties, particularly coercive force and squareness, could be obtained by molding FeCoBRM1 alloy powder with a certain composition range, sintering it, and further heat-treating it. It has been reached. That is, according to the present invention, 8 to 30% in atomic percentage
R (where R is at least one kind of rare earth element including Y), 2 to 28% B, and one or more of the following additive elements M1 at a predetermined % or less (However, except for M10%, M1 is Ti 4.5 % or less, Zr 5.5% or less, Hf 5.5% or less, Mn 8.0% or less, Ni 8.0% or less, Ge 7.0% or less, Sn 3.5% or less, Bi 5.0% or less, and Sb 2.5% or less, and two or more If M is included, the total amount of M1 is included.
Among the FeBRM1 compositions, the FeBRM1 composition consists of M1 (within a predetermined percentage of the maximum value of each element in M1), and the remainder substantially consists of Fe (including impurities unavoidable in manufacturing).
A composition in which a portion of Fe is replaced with 50% or less of Co (excluding 0%) in the total composition (FeCOBRM1 composition)
A sintered body that is sintered at 900 to 1200℃,
The above object can be achieved by a method for producing a permanent magnet material, which is characterized by heat treatment at 350° C. to the sintering temperature or lower. By the above heat treatment, a significant increase in coercive force can be obtained for a sintered body of the same composition without deteriorating other magnetic properties. This point is extremely significant when compared with the fact that, for example, an increase in coercive force due to an increase in the rare earth element R results in a decrease in residual magnetization (see Japanese Patent Application No. 145072/1982). predetermined amount
The presence of M1 further enhances the effect of increasing the coercive force by this heat treatment, and the presence of Co achieves a sufficiently high Kurie point for practical use. In addition, this FeCoBRM1-based composition further contains one or more of the elements Similar post-sintering heat treatment effects can be achieved for FeCoBRM1-based compositions. It is preferable to obtain such a sintered body by molding an alloy powder composition having a predetermined composition and an average particle size of 0.3 to 80 μm, particularly by sintering it in a non-oxidizing atmosphere, as in the previous application. The permanent magnet material thus obtained exhibits particularly excellent magnetic properties when it has magnetic anisotropy in the FeCoBRM1 composition described above. The manufacturing method of the present invention is unique in that it can produce magnetically anisotropic permanent magnet materials, unlike conventional FeBR-based amorphous ribbons, but isotropic materials are also different from conventional isotropic permanent magnet materials. You can get better products. Hereinafter, a case will be mainly explained based on the production of a magnetically anisotropic permanent magnet material. In the method for producing a permanent magnet material of the present invention, FeBR
The temperature characteristics of the magnet material are improved by partially replacing Fe with Co in the system composition, and the coercive force and squareness are improved by adding the additive element M1 and aging treatment. It uses light rare earth elements such as Nd and Pr, which are abundant in resources, to exhibit high magnetic properties. Generally, when Co is added to an Fe alloy, the Curie point Tc may rise or fall depending on the amount added, and it is generally difficult to predict the effect of the addition. In the present invention, as a result of replacing Fe with Co, it was revealed that Tc gradually increases as the amount of Co substitution increases. Also, R of the magnet material composition
A similar trend is confirmed regardless of the type. Even a small amount of Co substitution (for example, 1%) is effective in increasing Tc, and depending on the amount of Co substitution, it is about 310 to about 750.
An alloy with any Tc of °C can be obtained, but the Co amount is 50
% (hereinafter, % indicates the atomic percentage in the alloy) or less, a sufficient effect can be obtained, and Co is set to 50% or less in order to achieve iHc of 1 kOe or more (hereinafter, % indicates the atomic percentage in the alloy). B should be 2% or more to satisfy the coercive force of 1 kOe or more, and the residual magnetic flux density Br of hard ferrite should be approximately
In order to achieve 4kG or more, it must be 28% or less. The rare earth element R is required to be 8% or more in order to obtain a coercive force of 1 kOe or more, and is set to 30% or less because it is easily flammable, difficult to handle and manufacture industrially, and is expensive. As B, pure boron or ferroboron can be used, and a material containing Al, Si, C, etc. as an impurity can be used. As R, a light rare earth element which is abundant in resources can be used, and Sm is not necessarily required or Sm does not need to be the main component, so the raw material is inexpensive and extremely useful. The permanent magnet material of the present invention is
Compared to RCo magnet materials, it is advantageous in terms of resources and cost, and even better magnetic properties can be obtained. The bright rare earth element R in the present invention is a rare earth element containing Y and including light rare earths and heavy rare earths, of which one or more are used. That is, this R includes Nd, Pr, La, Ce, Tb,
Dy, Ho, Er, Eu, Sm, Gd, Pm, Tm, Yb,
Lu and Y are included. As R, a light rare earth element is sufficient, and Nd and Pr are particularly preferred. In addition, it is usually sufficient to have one type of R, but in practice, a mixture of two or more types (Mitsushimetal, dididim, etc.) can be used for reasons such as convenience of availability, Sm,
Y, La, Ce, Gd, etc. can be used as a mixture with other R, especially Nd, Pr, etc. Note that R does not have to be a pure rare earth element, and it is also possible to use an element containing impurities that are unavoidable in production as long as it is industrially available. In the permanent magnet material produced according to the present invention, the additive element M1 has the effect of increasing the coercive force. Increasing the coercive force increases the stability of the magnet and expands its applications. However, as M1 increases, Br decreases, and therefore the maximum energy product (BH) max decreases. Recently, there have been many applications that require high coercive force Hc even if (BH)max is slightly lower, so alloys containing M1 are very useful, but (BH)max is useful in the range of 4MGOe or higher. be. In order to clarify the effect on Br caused by the addition of each additive element M1, we measured the change in Br by varying the amount added, and calculated the Br value of hard ferrite.
The range is equal to or greater than 4kG. In addition, considering the range equivalent to or higher than the (BH) max of hard ferrite of about 4MGOe, the upper limit of the amount of M1 added is Ti 4.5% or less, Zr 5.5% or less, Hf 5.5% or less, Mn 8.0% or less, Ni 8.0% or less, Ge is 7.0% or less, Sn 3.5% or less, Bi 5.0% or less, and Sb 2.5% or less. M1 does not contain 0%, and one or more types can be added. When two or more kinds of additive elements are contained, the intermediate value of the characteristics of each additive element is generally indicated, and the content of each element is within the range of the above percentages, and the total amount is not more than the maximum value of the percentages for each element. When the FeCoBRM1 composition is within the above range, the maximum energy product (BH) max is equal to or greater than that of a hard ferrite magnet (~4MGOe).
In addition, light rare earth elements (especially Nd, Pr) account for 50% of the total R.
% or more, and 12 to 24% R, 3 to 27% B, Co 50% or less (excluding Co 0%), and additional elements
M1 is Ti4.0% or less, Zr4.5% or less, Hf4.5% or less,
Mn 6.0% or less, Ni 3.5% or less, Ge 5.5% or less,
Sn2.5% or less, Bi4.0% or less, and Sb1.5% or less, the total amount of M1 is less than the atomic percentage of the maximum value of each element contained in M1, and the remainder is substantially For Fe composition range, (BH)max
is in a preferable range of 7MGOe or more. Furthermore, the most preferable range is light rare earth elements (especially Nd, Pr)
containing 50% or more of the total R, and 12 to 20% of R,
4-24% B, Co50% or less (excluding Co0%),
Additive element M1 is Ti3.5% or less, Zr3.5% or less, Hf3.5
% or less, Mn4.0% or less, Ni2.0% or less, Ge4.0% or less, Sn1.0% or less, Bi3.0% or less, and Sb0.5% or less, and the total amount of M1 is the M1 contained (BH)
The max can be more than 10MGOe, and the highest maximum energy product can reach more than 33MGOe. In addition, the Fe-Co-B-R-M1 alloy of the present invention has a temperature coefficient (α) of residual magnetic flux density (Br) of 5% or more of Co and α≦
0.1%/℃, resulting in good temperature characteristics. Not only does it have better temperature characteristics than Fe-BR-R alloys that do not contain Co, but the addition of Co improves each shape of the demagnetization curve. Therefore, the maximum energy product can be improved. Below 25% Co, other magnetic properties (especially the energy product) are not substantially adversely affected. When Co exceeds 25%, (BH)max
decreases. Further, since Co has more corrosion resistance than Fe, it is possible to impart corrosion resistance to the Fe-BR alloy by adding Co. Permanent magnet materials made of FeCoBRM1-based sintered bodies manufactured by the present invention include Fe, Co, B, R,
It is also possible to contain a small amount of Cu, C, S, P, Ca, Mg, O, Si, etc. in addition to M1, making it possible to improve manufacturability and reduce costs. In particular, Cu3.5% or less, S2.0
% or less, C4.0% or less, and P3.5% or less (however, the total amount is below the maximum value of each element).
Even with the inclusion of these elements, it still has Br (about 4 kG) or higher, which is the same level as hard ferrite, and is useful. Further, it is preferable that Ca and Mg are each 4% or less, and O and S are each 2% or less (however, the total amount is below the maximum value of each element). Note that Cu and P may be mixed in from inexpensive raw materials, C may be mixed in from organic molding aids, etc., and S may be mixed in during the manufacturing process. In addition, in the state of alloy powder, adsorbed components (moisture, oxygen, etc.) from air during processing are likely to be included, but these can be removed during sintering. However, care should be taken in processing and storage as necessary. In addition, the present invention is practical in that it can tolerate the presence of impurities that are inevitable in industrial production. The manufacturing method of the present invention will be further explained below regarding the case of manufacturing a magnetically anisotropic permanent magnet material. First, an alloy powder (composition) having the FeCoBRM1 composition is obtained as a starting material. This may be obtained by crushing an alloy ingot obtained by ordinary alloy melting and casting, classification, blending, etc., or it may be obtained by a reduction method from an oxide using a reducing agent such as Ca. ,
It is preferable to use FeCoBRM1 alloy powder with an average particle size of 0.3 to 80 μm. If the average particle size exceeds 80 μm, excellent magnetic properties cannot be obtained. average particle size
If the diameter is less than 0.3 μm, the oxidation of the powder becomes significant during pulverization or the subsequent manufacturing process, and the density after sintering does not increase, resulting in poor magnetic properties. In the average particle size range of 40 to 80 μm, the coercive force among the magnetic properties is somewhat low. In order to obtain excellent magnetic properties, the average particle size of the alloy powder is most preferably 1.0 to 20 μm. The pulverization may be carried out by a conventional method, and may be either dry pulverization carried out in an inert gas atmosphere or wet pulverization carried out in an organic solvent. In the case of using moisture, alcohol solvents, hexane, trichloroethane, trichloroethylene, xylene, toluene, fluorine solvents, paraffin solvents, etc. can be used. Next, the alloy powder is shaped. The molding can be carried out in the same manner as the usual powder metallurgy method, preferably pressure molding, and in order to obtain anisotropy, pressing in a magnetic field. For example, when alloy powder is 0.5
A molded body is formed by applying a pressure of ~3.0Ton/cm 2 . This pressure molding in a magnetic field can be performed either by molding the powder as it is or by molding it in an organic solvent such as acetone or toluene. Next, this molded body is sintered at a predetermined temperature (900 to 1200°C) in a reducing or non-oxidizing atmosphere.
For example, this compact is sintered for 0.5 to 4 hours at a temperature range of 900 to 1200°C in a vacuum of 10 -2 Torr or less or in an inert gas or reducing gas atmosphere of 1 to 760 Torr and a purity of 99.9% or more. . If the sintering temperature is lower than 900°C, sufficient sintered density and high residual magnetic flux density cannot be obtained. Moreover, above 1200°C, the sintered body is deformed and the orientation of crystal grains is disrupted, resulting in a decrease in residual magnetic flux density and a decrease in the squareness of the demagnetization curve. Further, the sintering time may be at least 5 minutes, but if it is too long, there will be a problem in mass productivity, so in consideration of the reproducibility of the magnetic properties, the sintering time is preferably 0.5 to 4 hours. Note that the sintering process is considered to be a heating process in which the density increases as the sintering progresses and reaches a sufficient density. The sintering atmosphere is a non-oxidizing atmosphere, such as a high vacuum or an inert gas or reducing gas atmosphere, since R, which is a component in this alloy, is extremely susceptible to oxidation at high temperatures. The higher the purity of the sexual gas, the better. When using an inert gas, it is also possible to carry out the sintering in a reduced pressure atmosphere of 1 to less than 760 Torr as a method of obtaining high sintering density. The temperature increase rate during sintering is not particularly specified, but in the case of the above-mentioned air press method, in order to remove the organic solvent, the temperature increase rate is 30 °C/min or less, or the temperature is increased to 200 °C during the temperature rise. Approximately 1 in the temperature range of ~800℃
It is desirable to remove the solvent by holding it for a period of time or more. After sintering, the cooling rate to room temperature is preferably 30°C/min or more to reduce product variation.
In order to improve the magnetic properties through subsequent heat treatment (aging treatment), a cooling rate of 150°C/min or higher is desirable (however, it is also possible to immediately start the heat treatment process following sintering). The aging treatment is performed in a vacuum, inert gas, or reducing gas atmosphere at a temperature range from 350°C to below the sintering temperature for approximately 5 minutes to 70 hours. The aging treatment atmosphere should be a vacuum of 10 -3 Torr or less, or an inert gas or reducing gas atmosphere, since R, the main component in the alloy, reacts rapidly with oxygen or moisture at high temperatures. A purity of 99.99% or higher is desirable. The optimum sintering temperature of the alloy of the present invention varies depending on the composition, and the aging treatment must be performed at a temperature below each sintering temperature of the magnet material of the present invention. for example
71Fe5Co8B14Nd2Ti alloy,
For 52Fe25Co5B17Nd1Mn alloy, the upper limit temperature for aging treatment is 950℃ and 1000℃, respectively. In general, the upper limit aging temperature can be increased as the composition is richer in Fe, less B, or less R. However, if the aging temperature is too high, the crystal grains of the alloy of the present invention will grow excessively, leading to a decrease in magnetic properties, especially the coercive force, and the optimum aging treatment time will be extremely short, making it difficult to control the manufacturing conditions and making it difficult to put into practical use. Not. Furthermore, if the temperature is lower than 350°C, the aging treatment time will take an extremely long time, making it impractical, and the squareness of the demagnetization curve will deteriorate, making it impossible to obtain an excellent permanent magnet. In order to practically obtain excellent magnetic properties without causing excessive growth of crystal grains in the permanent magnet material obtained by the present invention, the aging treatment temperature is most preferably 450°C to 800°C. The aging treatment is carried out for 5 minutes to 70 hours, but if the aging treatment time is less than 5 minutes, the effect of the aging treatment will hardly appear, and the obtained magnet properties will vary widely. On the other hand, if the aging treatment exceeds 70 hours, it is difficult to say that it is practical because it takes too long for industrial purposes. In order to practically obtain excellent magnetic properties with good reproducibility, the most desirable aging treatment time is 30 minutes to 8 hours. In addition, in the manufacturing method of the present invention, multi-stage aging treatment of two or more stages is also effective as a method for aging the magnetic alloy. For example, 68Fe-5Co-7B-
For 18Nd-2Ge alloy, the first stage is 800℃~900℃
After the first stage aging treatment for 30 minutes to 8 hours at a temperature range of , excellent magnetic properties with high coercive force and high squareness of demagnetization curve can be obtained. The aging treatment after the second stage is effective in significantly improving the coercive force. In addition, as an alternative method of aging treatment, instead of multi-stage aging treatment, the same magnetic properties can be obtained by cooling the temperature range from 350℃ to 950℃ during aging treatment at a constant cooling rate using a cooling method such as air cooling or water cooling. However, the cooling rate at that time is 0.2℃/min ~ 20℃
It needs to be ℃/sec. Note that the same magnetic characteristics can be obtained even if these aging treatments are performed as is after sintering, or if the temperature is raised again after cooling to room temperature after sintering. Further, the manufacturing method of the present invention can be applied not only to magnetically anisotropic permanent magnet materials but also to isotropic permanent magnet materials. In addition, in the method for producing an isotropic permanent magnet material, the alloy powder is molded without being placed in a magnetic field, and other steps can be used as they are. For isotropic case, R10~25%, B3~23%,
In a composition consisting of 50% or less Co, a certain % M1, the balance Fe and unavoidable impurities, (BH)
You can get more than max2MGOe. Isotropic magnet materials originally have low magnetic properties that are 1/4 to 1/6 of the magnetic properties of anisotropic magnet materials, but according to the present invention, they are nevertheless extremely isotropic. High useful properties are obtained. Even in the case of isotropy, as the amount of R increases, iHc
increases, but Br decreases after reaching its maximum value.
Thus, the amount of R that satisfies (BH)max2MGOe or more is 10% or more and 25% or less. Also, as the amount of B increases, iHc increases, but Br
decreases after reaching its maximum value. Thus (BH)
Must be in the range of B3-23% to obtain max2MGOe or higher. Preferably, light rare earths (particularly Nd, Pr) are the main components of R (rare earths are 50 at% or more in all R) and 12 to 20
With a composition of % R, 5-18% B, and the balance Fe (BH)
Shows high magnetic properties exceeding max4MGOe. The most preferable range is a composition in which light rare earth elements such as Nd and Pr are the main components of R, and 12 to 16% R, 6 to 18% B with the balance Fe, and (BH)max is 7MGOe or more, and isotropic permanent magnet materials. You can obtain characteristics never seen before. For M1, the same range as in the case of anisotropy is preferable except for the following (Ti: 4.7% or less, Ni: 4.7% or less,
Ge6.0% or less). When any M1 component is isotropic, Br shows a decreasing tendency as the amount added increases, and Br3kG or more (to be equal to or higher than the level of (BH)max2MGOe of isotropic hard ferrite) is within this range. Indicated by Binders and lubricants are generally not used in the case of anisotropic materials because they interfere with orientation during molding, but in the case of isotropic magnet materials, containing binders and lubricants improves press efficiency. It is possible to improve the properties of the molded product and increase the strength of the molded product. Even in the case of isotropy, in addition to R, B, Fe, Co, and M1, C, P, S, Cu, Ca, Mg, O, and Si can be contained within a specified range, and C4.0% or less. , P3.3% or less, S2.5% or less, Cu3.3% or less, Ca4% or less,
It is practically preferable that Mg is 4% or less, O2% or less, and Si2% or less (however, the total of these is the maximum value or less of each component). Note that the presence of other impurities that are unavoidable in industrial production can be tolerated, as in the case of anisotropic materials. As detailed above, the method for manufacturing the permanent magnet material of the present invention has excellent magnetic properties with a novel FeCoBRM1 system having high coercive force and high energy product, and also uses light rare earth elements such as Nd and Pr as R. This makes it possible to easily produce a permanent magnet material that is excellent in terms of resources and cost, and has high industrial applicability. In particular, by substituting a part of Fe with Co, it is possible to obtain a material having a more practical Curie temperature, and by incorporating a predetermined element M1 and subjecting it to a predetermined aging treatment, This is a crystalline FeCoBRM1-based permanent magnet material that has further improved the coercive force and the squareness of the demagnetization curve. The aspects and effects of the present invention will be further explained based on Examples. However, the present invention is not limited to the examples and described aspects. Tables 1 to 4 show the characteristics of permanent magnet materials having various FeCoBRM1 compositions produced by the following steps. (1) The starting raw materials are electrolytic iron with a purity of 99.9% (weight%, the same applies to raw material purity below) as Fe, and feroboron alloy (19.38% B, 5.32% Al, 0.74% B) as B.
%Si, 0.03%C, balance Fe), purity 99% as R
The above (impurities are mainly other rare earth metals) are used. As Co, electrolytic Co with a purity of 99.9% was used. M1 includes 99% purity Ti, Bi, Mn, Sb, Ni, Sn,
Ferrozirconium containing 77.5% Zr as Ge, 95% Hf, and Zr was used. (2) Magnet raw materials were melted using high-frequency induction. At that time, an aluminum crucible was used as the crucible, and an ingot was made by casting into a water-cooled copper mold. (3) Crush the ingot obtained by melting.
After making the powder into 35 mesh, it was further pulverized using a ball mill to obtain a predetermined average particle size. (4) The powder was molded under a predetermined pressure in a magnetic field (however, when manufacturing an isotropic magnet material, molding was performed without applying a magnetic field). (5) The compact was sintered in a predetermined atmosphere within the range of 900 to 1200°C, and then subjected to a predetermined heat treatment. Example 1 Atomic percentage composition 57Fe・15Co・9B・17Nd・2Ti
An alloy powder with an average particle size of 4 μm is heated in a 15 kOe magnetic field.
After pressure molding at a pressure of 1.0Ton/cm 2 , it was sintered at 1120°C for 2 hours in 150 Torr Ar with a purity of 99.99%, and after sintering, it was cooled to room temperature at a cooling rate of 500°C/min.
Furthermore, aging treatment was performed at 700℃ for 20 minutes, 120 minutes, and 240 minutes.
This was carried out for 3000 minutes to obtain a magnet material according to the manufacturing method of the present invention.
Comparative example of magnet characteristics results and temperature coefficient α (%/℃) of residual magnetic flux density (Br) of this alloy magnet (after sintering)
They are shown in Table 1.

【表】 実施例 2 原子百分率組成55Fe−15Co−10B−16Nd・
2Pr−2Hf、平均粒度3μmなる合金粉末を15kOe
磁界中で1.0Ton/cm2の圧力で加圧成形した後、
99.999%純度の400Torr Ar中で1160℃、4時間
焼結し、焼結後は冷却速度450℃/minで室温ま
で冷却した。さらに3×10-5Torr真空中にて時
効処理を表2に示す各温度にて4時間行い、本発
明製法による磁石材料を得た。磁石特性結果およ
び残留磁束密度(Br)の温度係数α(%/℃)を
比較例(焼結後等)とともに表2に示す。
[Table] Example 2 Atomic percentage composition 55Fe−15Co−10B−16Nd・
2Pr−2Hf, 15kOe of alloy powder with average particle size of 3μm
After pressure molding in a magnetic field at a pressure of 1.0Ton/ cm2 ,
Sintering was performed at 1160°C for 4 hours in 400 Torr Ar with a purity of 99.999%, and after sintering, the material was cooled to room temperature at a cooling rate of 450°C/min. Further, aging treatment was performed in a vacuum of 3×10 −5 Torr at each temperature shown in Table 2 for 4 hours to obtain a magnet material according to the manufacturing method of the present invention. The magnet characteristic results and the temperature coefficient α (%/°C) of the residual magnetic flux density (Br) are shown in Table 2 together with comparative examples (after sintering, etc.).

【表】【table】

【表】 実施例 3 平均粒度2〜10μm、表3に示す原子百分率組
成を有するFe−Co−B−R−M1合金粉末を
10kOe磁界中で1.5Ton/cm2の圧力で加圧成形し
た後、99.999%純度の200Torr Ar中で1060℃、
2時間焼結し、焼結後は冷却速度650℃/minで
室温まで急速冷却した。さらに600TorrのAr中
にて時効処理を650℃で4時間行い、本発明製法
による磁石材料を得た。磁石特性およびBrの温
度係数α(%/℃)の値をCoを含有しない比較例
とともに表3に示す。
[Table] Example 3 Fe-Co-B-R-M1 alloy powder having an average particle size of 2 to 10 μm and the atomic percentage composition shown in Table 3 was
After pressure molding at a pressure of 1.5Ton/ cm2 in a 10kOe magnetic field, 1060℃ in 200Torr Ar with 99.999% purity,
Sintering was carried out for 2 hours, and after sintering, it was rapidly cooled to room temperature at a cooling rate of 650°C/min. Furthermore, aging treatment was performed at 650° C. for 4 hours in Ar at 600 Torr to obtain a magnet material according to the manufacturing method of the present invention. The magnetic properties and the temperature coefficient α (%/°C) of Br are shown in Table 3 along with a comparative example that does not contain Co.

【表】 実施例 4 平均粒度2〜10μmを有する下記原子百分率組
成のFe−Co−B−R−M1合金粉末を無磁界中で
1.5Ton/cm2の圧力で加圧成形した後、99.9%純度
の150Torr Ar中で1040℃、1時間焼結し、焼結
後は冷却速度450℃/minで室温まで急速冷却し
た。さらに650Torr Ar中にて時効処理を650℃
で4時間行い、本発明製法による等方性磁石材料
を得た。磁石特性の結果を時効処理なしの焼結後
の試料(比較例)とともに表4に示す。
[Table] Example 4 Fe-Co-B-R-M1 alloy powder having the following atomic percentage composition and having an average particle size of 2 to 10 μm was prepared in a non-magnetic field.
After pressure molding at a pressure of 1.5Ton/cm 2 , it was sintered at 1040°C for 1 hour in 150Torr Ar with 99.9% purity, and after sintering, it was rapidly cooled to room temperature at a cooling rate of 450°C/min. Furthermore, aging treatment was performed at 650℃ in 650Torr Ar.
The process was carried out for 4 hours to obtain an isotropic magnet material according to the manufacturing method of the present invention. The results of the magnetic properties are shown in Table 4 together with the sample after sintering without aging treatment (comparative example).

【表】【table】

Claims (1)

【特許請求の範囲】 1 原子百分率で8〜30%のR(但しRはYを包
含する希土類元素の少なくとも1種)、2〜28%
のB、所定%以下の添加元素M1の1種又は2種
以上 (但しM1 0%を除き、M1は Ti 4.5%以下、 Zr 5.5%以下、 Hf 5.5%以下、 Mn 8.0%以下、 Ni 8.0%以下、 Ge 7.0%以下、 Sn 3.5%以下、 Bi 5.0%以下 及びSb 2.5%以下であり、 2種以上のM1を含む場合M1合量は含有する
M1の当該各元素のうち最大値を有するものの所
定%以下)、及び残部実質上FeからなるFeBRM1
系組成のうちFeの一部を全組成に対して50%以
下のCo(0%を除く)で置換してなる
FeCoBRM1系組成を有し、900〜1200℃で焼結し
てなる焼結体を350℃〜当該焼結温度以下で熱処
理することを特徴とする永久磁石材料の製造方
法。 2 前記焼結体は、前記FeCoBRM1組成を有し、
平均粒度0.3〜80μmの合金粉末組成物を成形、焼
結して得られる特許請求の範囲第1項記載の永久
磁石材料の製造方法。 3 原子百分率で8〜30%のR(但しRはYを包
含する希土類元素の少なくとも1種)、2〜28%
のB、所定%以下の添加元素M1の1種又は2種
以上 (但しM1 0%を除き、M1は Ti 4.5%以下、 Zr 5.5%以下、 Hf 5.5%以下、 Mn 8.0%以下、 Ni 8.0%以下、 Ge 7.0%以下、 Sn 3.5%以下、 Bi 5.0%以下、 及びSb 2.5%以下であり、 2種以上のM1を含む場合M1合量は含有する
M1の当該各元素のうち最大値を有するものの所
定%以下)、所定%以下の元素Xの一種又は二種
以上(所定%以下の元素XはCu3.5%以下、S2.0
%以下、C4.0%以下及びP3.5%以上であり、Xが
二種以上のときX合量は当該各元素のうち最大所
定%を有するものの当該所定%以下)、及び残部
実質上FeからなるFeBRM1系組成のうちFeの一
部を全組成に対して50%以下のCo(0%を除く)
で置換してなるFeCoBRM1系組成を有し、900〜
1200℃で焼結してなる焼結体を350℃〜当該焼結
温度以下で熱処理することを特徴とする永久磁石
材料の製造方法。
[Claims] 1. 8 to 30% R (wherein R is at least one rare earth element including Y), 2 to 28% in atomic percentage
B, one or more of the additive elements M1 in a specified percentage or less (excluding M1 0%, M1 is Ti 4.5% or less, Zr 5.5% or less, Hf 5.5% or less, Mn 8.0% or less, Ni 8.0%) Below, Ge is 7.0% or less, Sn 3.5% or less, Bi 5.0% or less, and Sb 2.5% or less, and if two or more types of M1 are included, the total amount of M1 is included.
FeBRM1 consisting of a specified percentage of the maximum value of each element in M1), and the remainder substantially consisting of Fe.
Part of the Fe in the system composition is replaced with 50% or less Co (excluding 0%) of the total composition.
1. A method for producing a permanent magnet material, which comprises heat-treating a sintered body having a FeCoBRM1 composition and sintered at 900 to 1200°C at 350°C to below the sintering temperature. 2 The sintered body has the FeCoBRM1 composition,
A method for producing a permanent magnet material according to claim 1, which is obtained by molding and sintering an alloy powder composition having an average particle size of 0.3 to 80 μm. 3 8 to 30% R in atomic percentage (however, R is at least one rare earth element including Y), 2 to 28%
B, one or more of the additive elements M1 in a specified percentage or less (excluding M1 0%, M1 is Ti 4.5% or less, Zr 5.5% or less, Hf 5.5% or less, Mn 8.0% or less, Ni 8.0%) Below, Ge is 7.0% or less, Sn 3.5% or less, Bi 5.0% or less, and Sb 2.5% or less, and if two or more types of M1 are included, the total amount of M1 is included.
The maximum value of each element in M1 is below a predetermined percentage), one or more of the elements X below a predetermined percentage (element
% or less, C4.0% or less, and P3.5% or more, and when X is two or more types, the total amount of A part of Fe in the FeBRM1 system composition consisting of 50% or less of Co (excluding 0%) in the total composition
It has a FeCoBRM1-based composition consisting of substitution with 900~
A method for producing a permanent magnet material, which comprises heat-treating a sintered body obtained by sintering at 1200°C at a temperature of 350°C to the sintering temperature.
JP58161627A 1983-05-25 1983-09-02 Permanent magnet and its production Granted JPS6052556A (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
JP58161627A JPS6052556A (en) 1983-09-02 1983-09-02 Permanent magnet and its production
US06/532,471 US4601875A (en) 1983-05-25 1983-09-15 Process for producing magnetic materials
CA000436891A CA1287509C (en) 1983-05-25 1983-09-16 Process for producing magnetic materials
EP83109508A EP0126802B2 (en) 1983-05-25 1983-09-23 Process for producing of a permanent magnet
DE8383109508T DE3378707D1 (en) 1983-05-25 1983-09-23 Process for producing of a permanent magnet
SG594/90A SG59490G (en) 1983-05-25 1990-07-18 Process for producing of a permanent magnet
HK753/90A HK75390A (en) 1983-05-25 1990-09-20 Process for producing of a permanent magnet

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58161627A JPS6052556A (en) 1983-09-02 1983-09-02 Permanent magnet and its production

Publications (2)

Publication Number Publication Date
JPS6052556A JPS6052556A (en) 1985-03-25
JPH045738B2 true JPH045738B2 (en) 1992-02-03

Family

ID=15738775

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58161627A Granted JPS6052556A (en) 1983-05-25 1983-09-02 Permanent magnet and its production

Country Status (1)

Country Link
JP (1) JPS6052556A (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60255941A (en) * 1984-05-30 1985-12-17 Tohoku Metal Ind Ltd Manufacture of rare earth element-transition metal element-semimetal alloy magnet
JPS61113736A (en) * 1984-11-09 1986-05-31 Agency Of Ind Science & Technol Manufacture of sintered magnet of rare earth-transition metal compound
JP2779794B2 (en) * 1986-05-17 1998-07-23 株式会社 トーキン Manufacturing method of rare earth permanent magnet
JPH0768561B2 (en) * 1987-09-22 1995-07-26 三菱マテリアル株式会社 Method for producing rare earth-Fe-B alloy magnet powder
JPH01232704A (en) * 1988-03-14 1989-09-18 Kawasaki Steel Corp Manufacture of rare-earth transition metal permanent magnet

Also Published As

Publication number Publication date
JPS6052556A (en) 1985-03-25

Similar Documents

Publication Publication Date Title
US5110377A (en) Process for producing permanent magnets and products thereof
JP3143156B2 (en) Manufacturing method of rare earth permanent magnet
JPH0510807B2 (en)
JP3254229B2 (en) Manufacturing method of rare earth permanent magnet
JPH04245403A (en) Rare earth-fe-co-b-based anisotropic magnet
JP2853838B2 (en) Manufacturing method of rare earth permanent magnet
JPH01219143A (en) Sintered permanent magnet material and its production
JP2948223B2 (en) High performance permanent magnet with excellent corrosion resistance and method of manufacturing the same
JPH045740B2 (en)
JPH0320046B2 (en)
JPH045739B2 (en)
JPH061726B2 (en) Method of manufacturing permanent magnet material
KR900006533B1 (en) Anisotropic magnetic powder, its magnet and manufacturing method thereof
JPH045737B2 (en)
JP3126199B2 (en) Manufacturing method of rare earth permanent magnet
JPH0320048B2 (en)
JPH0461042B2 (en)
JPS6052556A (en) Permanent magnet and its production
JP3143157B2 (en) Manufacturing method of rare earth permanent magnet
JPH0435547B2 (en)
JPH0320047B2 (en)
JPH0316766B2 (en)
JPH04246803A (en) Rare earth-fe-b anisotropic magnet
JPH0475303B2 (en)
JPH044384B2 (en)