JPS625972B2 - - Google Patents
Info
- Publication number
- JPS625972B2 JPS625972B2 JP56139766A JP13976681A JPS625972B2 JP S625972 B2 JPS625972 B2 JP S625972B2 JP 56139766 A JP56139766 A JP 56139766A JP 13976681 A JP13976681 A JP 13976681A JP S625972 B2 JPS625972 B2 JP S625972B2
- Authority
- JP
- Japan
- Prior art keywords
- less
- nitrogen
- alloy
- composition
- niobium
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 63
- 229910045601 alloy Inorganic materials 0.000 claims description 48
- 239000000956 alloy Substances 0.000 claims description 48
- 229910052757 nitrogen Inorganic materials 0.000 claims description 34
- 230000035699 permeability Effects 0.000 claims description 34
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 31
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 30
- 239000010955 niobium Substances 0.000 claims description 27
- 229910052758 niobium Inorganic materials 0.000 claims description 23
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims description 21
- 230000004907 flux Effects 0.000 claims description 18
- 239000000203 mixture Substances 0.000 claims description 18
- 230000009466 transformation Effects 0.000 claims description 16
- 238000001816 cooling Methods 0.000 claims description 15
- 238000010438 heat treatment Methods 0.000 claims description 15
- 229910052742 iron Inorganic materials 0.000 claims description 14
- 229910052759 nickel Inorganic materials 0.000 claims description 14
- 239000012535 impurity Substances 0.000 claims description 11
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical group [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 claims description 11
- 229910052761 rare earth metal Inorganic materials 0.000 claims description 11
- 229910052782 aluminium Inorganic materials 0.000 claims description 10
- 229910052787 antimony Inorganic materials 0.000 claims description 10
- 229910052796 boron Inorganic materials 0.000 claims description 10
- 229910052804 chromium Inorganic materials 0.000 claims description 10
- 239000011651 chromium Substances 0.000 claims description 10
- 229910052733 gallium Inorganic materials 0.000 claims description 10
- 229910052732 germanium Inorganic materials 0.000 claims description 10
- 229910052735 hafnium Inorganic materials 0.000 claims description 10
- 229910052738 indium Inorganic materials 0.000 claims description 10
- 229910052750 molybdenum Inorganic materials 0.000 claims description 10
- 229910052710 silicon Inorganic materials 0.000 claims description 10
- 229910052715 tantalum Inorganic materials 0.000 claims description 10
- 229910052716 thallium Inorganic materials 0.000 claims description 10
- 229910052718 tin Inorganic materials 0.000 claims description 10
- 229910052719 titanium Inorganic materials 0.000 claims description 10
- 239000010936 titanium Substances 0.000 claims description 10
- 229910052721 tungsten Inorganic materials 0.000 claims description 10
- 229910052720 vanadium Inorganic materials 0.000 claims description 10
- 229910052790 beryllium Inorganic materials 0.000 claims description 9
- 229910052802 copper Inorganic materials 0.000 claims description 9
- 239000010949 copper Substances 0.000 claims description 9
- 238000004519 manufacturing process Methods 0.000 claims description 9
- 229910052726 zirconium Inorganic materials 0.000 claims description 9
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 8
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 8
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 8
- GYHNNYVSQQEPJS-UHFFFAOYSA-N Gallium Chemical compound [Ga] GYHNNYVSQQEPJS-UHFFFAOYSA-N 0.000 claims description 8
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 8
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 8
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 8
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 8
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 8
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 claims description 8
- GNPVGFCGXDBREM-UHFFFAOYSA-N germanium atom Chemical compound [Ge] GNPVGFCGXDBREM-UHFFFAOYSA-N 0.000 claims description 8
- VBJZVLUMGGDVMO-UHFFFAOYSA-N hafnium atom Chemical compound [Hf] VBJZVLUMGGDVMO-UHFFFAOYSA-N 0.000 claims description 8
- APFVFJFRJDLVQX-UHFFFAOYSA-N indium atom Chemical compound [In] APFVFJFRJDLVQX-UHFFFAOYSA-N 0.000 claims description 8
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 claims description 8
- 239000011733 molybdenum Substances 0.000 claims description 8
- 230000001590 oxidative effect Effects 0.000 claims description 8
- 239000010703 silicon Substances 0.000 claims description 8
- BKVIYDNLLOSFOA-UHFFFAOYSA-N thallium Chemical compound [Tl] BKVIYDNLLOSFOA-UHFFFAOYSA-N 0.000 claims description 8
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 8
- 239000010937 tungsten Substances 0.000 claims description 8
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims description 8
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 7
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 claims description 7
- 229910017052 cobalt Inorganic materials 0.000 claims description 7
- 239000010941 cobalt Substances 0.000 claims description 7
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 7
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 claims description 7
- 238000002844 melting Methods 0.000 claims description 6
- 230000008018 melting Effects 0.000 claims description 6
- 238000003303 reheating Methods 0.000 claims description 6
- 239000000463 material Substances 0.000 claims description 3
- 229910001361 White metal Inorganic materials 0.000 claims description 2
- 239000010969 white metal Substances 0.000 claims description 2
- 230000001788 irregular Effects 0.000 claims 1
- 230000000694 effects Effects 0.000 description 11
- 229910001257 Nb alloy Inorganic materials 0.000 description 8
- 150000004767 nitrides Chemical class 0.000 description 8
- 229910001199 N alloy Inorganic materials 0.000 description 7
- 229910001004 magnetic alloy Inorganic materials 0.000 description 7
- 238000010586 diagram Methods 0.000 description 6
- 230000007423 decrease Effects 0.000 description 5
- 238000005242 forging Methods 0.000 description 5
- 230000005389 magnetism Effects 0.000 description 5
- 238000000034 method Methods 0.000 description 4
- 229910003271 Ni-Fe Inorganic materials 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- KDLHZDBZIXYQEI-UHFFFAOYSA-N Palladium Chemical compound [Pd] KDLHZDBZIXYQEI-UHFFFAOYSA-N 0.000 description 2
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 2
- 239000003795 chemical substances by application Substances 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 239000001257 hydrogen Substances 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- 230000006698 induction Effects 0.000 description 2
- 229910052748 manganese Inorganic materials 0.000 description 2
- 239000011572 manganese Substances 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 229910000702 sendust Inorganic materials 0.000 description 2
- 229910000859 α-Fe Inorganic materials 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910017082 Fe-Si Inorganic materials 0.000 description 1
- 229910017133 Fe—Si Inorganic materials 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- KJTLSVCANCCWHF-UHFFFAOYSA-N Ruthenium Chemical compound [Ru] KJTLSVCANCCWHF-UHFFFAOYSA-N 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 230000000996 additive effect Effects 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- RBVYPNHAAJQXIW-UHFFFAOYSA-N azanylidynemanganese Chemical compound [N].[Mn] RBVYPNHAAJQXIW-UHFFFAOYSA-N 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000005097 cold rolling Methods 0.000 description 1
- 230000003009 desulfurizing effect Effects 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 230000002542 deteriorative effect Effects 0.000 description 1
- 229910001873 dinitrogen Inorganic materials 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 150000002431 hydrogen Chemical class 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 229910052741 iridium Inorganic materials 0.000 description 1
- GKOZUEZYRPOHIO-UHFFFAOYSA-N iridium atom Chemical compound [Ir] GKOZUEZYRPOHIO-UHFFFAOYSA-N 0.000 description 1
- 229910052746 lanthanum Inorganic materials 0.000 description 1
- FZLIPJUXYLNCLC-UHFFFAOYSA-N lanthanum atom Chemical compound [La] FZLIPJUXYLNCLC-UHFFFAOYSA-N 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 230000005381 magnetic domain Effects 0.000 description 1
- 239000000696 magnetic material Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 125000004433 nitrogen atom Chemical group N* 0.000 description 1
- 229910052762 osmium Inorganic materials 0.000 description 1
- SYQBFIAQOQZEGI-UHFFFAOYSA-N osmium atom Chemical compound [Os] SYQBFIAQOQZEGI-UHFFFAOYSA-N 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 229910052763 palladium Inorganic materials 0.000 description 1
- 229910000889 permalloy Inorganic materials 0.000 description 1
- 229910052697 platinum Inorganic materials 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 238000001953 recrystallisation Methods 0.000 description 1
- 229910052703 rhodium Inorganic materials 0.000 description 1
- 239000010948 rhodium Substances 0.000 description 1
- MHOVAHRLVXNVSD-UHFFFAOYSA-N rhodium atom Chemical compound [Rh] MHOVAHRLVXNVSD-UHFFFAOYSA-N 0.000 description 1
- 229910052707 ruthenium Inorganic materials 0.000 description 1
- 229910052706 scandium Inorganic materials 0.000 description 1
- SIXSYDAISGFNSX-UHFFFAOYSA-N scandium atom Chemical compound [Sc] SIXSYDAISGFNSX-UHFFFAOYSA-N 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 230000002195 synergetic effect Effects 0.000 description 1
- 229910052727 yttrium Inorganic materials 0.000 description 1
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 description 1
Landscapes
- Heat Treatment Of Nonferrous Metals Or Alloys (AREA)
- Magnetic Heads (AREA)
- Soft Magnetic Materials (AREA)
Description
本発明は交流磁界における磁気特性および耐摩
耗性がすぐれ、鍛造および加工が容易で磁気記録
再生ヘツドに好適な高透磁率合金およびその製造
法ならびに磁気記録再生ヘツドに関するものであ
る。
テープレコーダーなどの磁気記録再生ヘツドは
交流磁界において作動するものであるから、これ
に用いられる磁性合金は高周波磁界における実効
透磁率が高いことが必要とされ、また磁気テープ
が接触して摺動するため耐摩耗性が良好であるこ
とが望まれている。現在耐摩耗性にすぐれた磁気
ヘツド用磁性合金としてはセンダスト(Fe―Si
―Al系合金)およびフエライト(MnO―ZnO―
Fe2O3)があるが、これらは非常に硬く脆いた
め、鍛造,圧延加工が不可能で、ヘツドコアの製
造には研削,研磨の方法が用いられており、従つ
てその成品は高価である。またセンダストは飽和
磁束密度は大きいが、薄板にできないので高周波
磁界における実効透磁率が比較的小さく、フエラ
イトは実効透磁率は大きいが、飽和磁束密度が
5000G以下で小さいのが欠点である。他方パーマ
ロイ(Ni―Fe系合金)は鍛造,圧延加工および
打抜きは容易で量産性にすぐれているが、軟く摩
耗しやすいのが大きな欠点である。
本願人らはNi―Fe系合金の耐摩耗性について
の研究を行い、先に特公昭47―29690号において
Ni―Fe―Nb系合金は、鍛造加工が容易で耐摩耗
性にすぐれ、磁気記録再生ヘツドに適した磁性合
金であることを記述しておいたが、その後、磁気
記録再生機において記録密度を高めるため高保磁
力の磁気テープが採用されるようになり、それに
伴つて磁気ヘツド用磁性合金としては高い飽和磁
束密度を有することが必要とされるようになつて
きた。このため、Ni―Fe―Nb系合金において
も、飽和磁束密度を高めるため非磁性添加物であ
るNb量を減ずる傾向になつてきた。しかし、Nb
量の減少はNi―Fe―Nb系合金の硬度および電気
抵抗の低下をきたし、それによつて耐摩耗性およ
び高周波磁界における実効透磁率を劣化させるこ
とになり、適切な方法とは考えられない。したが
つて目下何等かの改善策が強く要望されている。
本発明はNi―Fe―Nb系合金の鍛造加工性を損
わずに、また飽和磁束密度をできるだけ低下させ
ずに、耐摩耗性および実効透磁率を優位に保持し
ようとするもので、Ni―Fe―Nb系合金に窒素を
少量添加するとニオブと窒素の相乗効果により、
その目的が達成されたのである。
すなわち、一般に高透磁率合金では窒化物など
の非金属介在物は磁気特性を劣化させるものとし
て、これを極力除去することに努めているが、本
発明では微量のNb系窒化物を積極的に利用し
て、Ni―Fe―Nb系合金の耐摩耗性および実効透
磁率を改善しようとするものである。
本発明は重量比にてニツケル70〜86%、ニオブ
0.5〜10%、窒素0.0003〜0.3%、少量の不純物と
残部鉄からなるか、または重量比にて主成分とし
てニツケル70〜86%、ニオブ0.5〜14%、窒素
0.0003〜0.3%、副成分としてモリブデン,タン
グステン,タンタル,マンガン,銅,コバルトの
それぞれ7%以下、クロム,バナジウム,チタ
ン,ゲルマニウム,ガリウム,インジウム,タリ
ウムのそれぞれ5%以下、アルミニウム,ケイ
素,ジルコニウム,ハフニウム,希土類元素,白
金属元素のそれぞれ3%以下、ベリリウム,錫,
アンチモンのそれぞれ2%以下、ホウ素の1%以
下の1種または2種以上の合計0.01〜7%、少量
の不純物と残部鉄からなり、飽和磁束密度5000G
以上を有し、耐摩耗性および実効透磁率がすぐ
れ、鍛造加工が容易な磁気記録再生ヘツド等に使
用し得る高透磁率磁性合金に関するものである。
さらに本発明は上記の高透磁率合金をケースおよ
びコアに用いて製造した耐摩耗性にすぐれた磁気
記録再生ヘツドに関するものである。
以下本発明を詳細に説明する。
本発明の合金を製造するには、まず主成分のニ
ツケル70〜86%、ニオブ0.5〜10%および残部鉄
の適当量を非酸化性雰囲気中あるいは真空中にお
いて適当な溶解炉を用いて溶解した後、適当な脱
酸剤,脱硫剤を少量添加してできるだけ不純物を
取り除き、そのままか、更にこれにモリブデン,
タングステン,タンタル,マンガン,銅,コバル
トのそれぞれ7%以下、クロム,バナジウム,チ
タン,ゲルマニウム,ガリウム,インジウム,タ
リウムのそれぞれ5%以下、アルミニウム,ケイ
素,ジルコニウム,ハフニウム,希土類元素,白
金属元素のそれぞれ3%以下、ベリリウム,錫,
アンチモンのそれぞれ2%以下、ホウ素の1%以
下の1種または2種以上の合計0.01〜7%の定量
を添加して充分に撹拌し、組成的に均一な溶融合
金を造る。ついでN2およびN3H等のガスを炉内に
注入して調圧するか、あるいは合金成分の窒化物
を適当量添加することにより、溶融合金に適当量
の窒素を添加する。その後、これを適当な形およ
び大きさの鋳型に注入して健全な鋳塊を得、さら
にこれを高温において熱間鍛造および冷間圧延な
どの成形加工を施して目的の形状のもの、例えば
厚さ0.1mmの薄板を造る。次にその薄板から目的
の形状,寸法のものを打抜き、これを水素中、そ
の他適当な非酸化性雰囲気中あるいは真空中で再
結晶温度以上、すなわち約600℃以上、特に800℃
以上融点以下の温度に1分間以上加熱し、ついで
組成に対応した適当な速度、例えば100℃/秒〜
1℃/時で冷却する。合金の組成によつてはこれ
をさらに約600℃以下の温度(規則格子―不規則
格子変態点以下の温度)、特に200〜600℃に1分
間以上再加熱し、冷却することにより、飽和磁束
密度5000G以上を有し、耐摩耗性にすぐれた高透
磁率磁性合金を得ることができる。
上記の溶体化温度から規則―不規則格子変態点
(約600℃)以上の温度までの冷却は、急冷しても
徐冷しても得られる磁性には大した変りはない
が、この変態点以下の冷却速度は磁性に大きな影
響を及ぼす。すなわちこの変態点以上の温度より
100℃/秒〜1℃/時の組成に対応した適当な速
度で常温迄冷却することにより、地の規則度が適
度に調整され、すぐれた磁性が得られる。そして
上記の冷却速度の内100℃/秒に近い速度で急冷
すると、規則度が小さくなり、これ以上速く冷却
すると規則化が進まず、規則度はさらに小さくな
り磁性は劣化する。しかしその規則度の小さい合
金をその変態点以下の200℃〜600℃に再加熱し冷
却すると、規則化が進んで適度な規則度となり磁
性は向上する。他方、上記の変態点以上の温度か
ら、例えば1℃/時以下の速度で徐冷すると、規
則化は進みすぎ、磁性は低下する。
次に本発明の実施例について述べる。
実施例 1
合金番号13(組成Ni=80.3%,Nb=5.0%,N
=0.010%,残部Fe)
試料を造るには、まず全重量800gをアルミナ
坩堝に入れ、真空中で高周波誘導炉によつて溶か
した後、よく撹拌して均質な溶融合金とした。つ
いで窒素ガスを炉内に注入し、1×10-1Torrに
調圧して10分間保持した後、これを直径25mm、高
さ170mmの孔をもつ鋳型に注入し、得られた鋳塊
を約1000℃で鍛造して厚さ約7mmの板とした。さ
らに約600〜900℃の間で厚さ1mmまで熱間圧延
し、ついで常温で冷間圧延を施して0.1mmの薄板
とし、それから外径45mm、内径33mmの環状板およ
び磁気ヘツドのコアを打ち抜いた。つぎにこれら
に第1表に示す種々な熱処理を施し、環状板で磁
気特性および硬度を、またコアを用いて磁気ヘツ
ドを製造し、タリサーフ表面粗さ計で磁気テープ
(CrO2)による200時間走行後の摩耗量を測定して
第1表のような結果を得た。
The present invention relates to a high magnetic permeability alloy that has excellent magnetic properties and wear resistance in an alternating magnetic field, is easy to forge and process, and is suitable for a magnetic recording/reproducing head, a method for producing the same, and a magnetic recording/reproducing head. Since magnetic recording/reproducing heads such as tape recorders operate in alternating magnetic fields, the magnetic alloys used therein must have high effective magnetic permeability in high-frequency magnetic fields, and magnetic tapes must slide in contact with each other. Therefore, it is desired that the wear resistance be good. Currently, Sendust (Fe-Si
-Al-based alloy) and ferrite (MnO-ZnO-
Fe 2 O 3 ), but these are extremely hard and brittle and cannot be forged or rolled. Grinding and polishing methods are used to manufacture head cores, and the finished product is therefore expensive. . Sendust has a high saturation magnetic flux density, but since it cannot be made into a thin plate, its effective permeability in a high-frequency magnetic field is relatively small. Ferrite has a high effective permeability, but its saturation magnetic flux density is relatively low.
The disadvantage is that it is small, less than 5000G. On the other hand, permalloy (Ni-Fe alloy) is easy to forge, roll, and punch, making it suitable for mass production, but its major drawback is that it is soft and easily wears out. The applicants conducted research on the wear resistance of Ni-Fe alloys, and previously published
As mentioned above, Ni-Fe-Nb alloy is a magnetic alloy that is easy to forge, has excellent wear resistance, and is suitable for magnetic recording/reproducing heads. In order to increase the coercivity, magnetic tapes with high coercivity have come to be used, and along with this, magnetic alloys for magnetic heads are required to have a high saturation magnetic flux density. For this reason, even in Ni--Fe--Nb alloys, there has been a trend to reduce the amount of Nb, which is a non-magnetic additive, in order to increase the saturation magnetic flux density. However, Nb
Reducing the amount will lead to a decrease in the hardness and electrical resistance of the Ni--Fe--Nb alloy, thereby deteriorating its wear resistance and effective magnetic permeability in high-frequency magnetic fields, and is not considered a suitable method. Therefore, there is a strong demand for some improvement measures. The present invention aims to maintain superior wear resistance and effective magnetic permeability without impairing the forging workability of Ni-Fe-Nb alloys or reducing the saturation magnetic flux density as much as possible. When a small amount of nitrogen is added to Fe-Nb alloy, due to the synergistic effect of niobium and nitrogen,
That purpose was achieved. In other words, generally in high permeability alloys, non-metallic inclusions such as nitrides deteriorate the magnetic properties, and efforts are made to remove them as much as possible, but in the present invention, we actively remove trace amounts of Nb-based nitrides. The aim is to improve the wear resistance and effective magnetic permeability of Ni-Fe-Nb alloys. The present invention has a weight ratio of 70 to 86% nickel and niobium.
0.5-10%, nitrogen 0.0003-0.3%, a small amount of impurities and the balance iron, or the main components by weight are nickel 70-86%, niobium 0.5-14%, nitrogen
0.0003 to 0.3%, as subcomponents molybdenum, tungsten, tantalum, manganese, copper, cobalt each up to 7%, chromium, vanadium, titanium, germanium, gallium, indium, thallium each up to 5%, aluminum, silicon, zirconium, Less than 3% each of hafnium, rare earth elements, and white metal elements, beryllium, tin,
Consists of less than 2% each of antimony, less than 1% of boron, a total of 0.01 to 7% of one or more types, a small amount of impurities and the balance iron, saturation magnetic flux density 5000G
The present invention relates to a high permeability magnetic alloy that has the above properties, has excellent wear resistance and effective magnetic permeability, and can be easily forged and used for magnetic recording/reproducing heads and the like.
Furthermore, the present invention relates to a magnetic recording/reproducing head with excellent wear resistance manufactured using the above-mentioned high magnetic permeability alloy for the case and core. The present invention will be explained in detail below. To produce the alloy of the present invention, the main components, 70 to 86% nickel, 0.5 to 10% niobium, and an appropriate amount of the balance iron, were first melted in a non-oxidizing atmosphere or in a vacuum using a suitable melting furnace. After that, add a small amount of a suitable deoxidizing agent or desulfurizing agent to remove as much impurity as possible, and then add molybdenum,
7% or less each of tungsten, tantalum, manganese, copper, and cobalt; 5% or less each of chromium, vanadium, titanium, germanium, gallium, indium, and thallium; each of aluminum, silicon, zirconium, hafnium, rare earth elements, and platinum metal elements 3% or less, beryllium, tin,
A total amount of 0.01 to 7% of one or more types of antimony (2% or less) and boron (1% or less) are added and sufficiently stirred to produce a compositionally uniform molten alloy. Next, an appropriate amount of nitrogen is added to the molten alloy by injecting gases such as N 2 and N 3 H into the furnace to adjust the pressure, or by adding an appropriate amount of nitride as an alloy component. Thereafter, this is poured into a mold of an appropriate shape and size to obtain a sound ingot, which is then subjected to forming processes such as hot forging and cold rolling at high temperatures to obtain the desired shape, such as thickness. Build a thin plate with a thickness of 0.1mm. Next, punch out a piece of the desired shape and size from the thin plate, and heat it in hydrogen, other suitable non-oxidizing atmosphere, or vacuum at a temperature higher than the recrystallization temperature, that is, about 600℃ or higher, especially 800℃.
Heating for 1 minute or more at a temperature below the melting point, then at an appropriate rate depending on the composition, e.g. 100°C/sec.
Cool at 1°C/hour. Depending on the composition of the alloy, this may be further reheated to a temperature of approximately 600°C or below (temperature below the ordered lattice-irregular lattice transformation point), particularly 200 to 600°C for 1 minute or more, and then cooled to reduce the saturation magnetic flux. A high permeability magnetic alloy with a density of 5000G or more and excellent wear resistance can be obtained. Cooling from the above solution temperature to a temperature above the ordered-irregular lattice transformation point (approximately 600°C) shows that there is no significant difference in the magnetic properties obtained whether the cooling is rapid or gradual; The following cooling rates have a significant effect on magnetism. In other words, from the temperature above this transformation point
By cooling to room temperature at an appropriate rate corresponding to the composition of 100° C./sec to 1° C./hour, the regularity of the ground can be appropriately adjusted and excellent magnetism can be obtained. If the material is rapidly cooled at a rate close to 100° C./second among the above cooling rates, the degree of order decreases, and if it is cooled any faster, the degree of order does not proceed, and the degree of order decreases further, resulting in deterioration of magnetism. However, when an alloy with a low degree of order is reheated to 200 to 600 degrees Celsius, below its transformation point, and cooled, ordering progresses and the degree of order becomes moderate, improving magnetism. On the other hand, if it is slowly cooled from a temperature above the above-mentioned transformation point at a rate of, for example, 1° C./hour or less, ordering will proceed too much and the magnetism will decrease. Next, examples of the present invention will be described. Example 1 Alloy number 13 (composition Ni=80.3%, Nb=5.0%, N
= 0.010%, remainder Fe) To prepare the sample, first, a total weight of 800 g was placed in an alumina crucible, melted in a high frequency induction furnace in a vacuum, and then thoroughly stirred to form a homogeneous molten alloy. Next, nitrogen gas was injected into the furnace, the pressure was adjusted to 1 × 10 -1 Torr, and the pressure was maintained for 10 minutes. This was then injected into a mold with holes of 25 mm in diameter and 170 mm in height, and the resulting ingot was It was forged at 1000℃ into a plate approximately 7mm thick. Further, it is hot-rolled to a thickness of 1 mm between approximately 600 and 900°C, then cold-rolled at room temperature to form a thin plate of 0.1 mm. Then, an annular plate with an outer diameter of 45 mm and an inner diameter of 33 mm and the core of the magnetic head are punched out. Ta. Next, these were subjected to various heat treatments shown in Table 1, and the annular plate was used to check the magnetic properties and hardness, and the core was used to manufacture a magnetic head. The amount of wear after running was measured and the results shown in Table 1 were obtained.
【表】
実施例 2
合金番号74(組成Ni=79.8%,Nb=7.0%,Mn
=2.5%,N=0.013%,残部Fe)
試料を造るにはまずニツケル,鉄,ニオブの
780gをアルミナ坩堝に入れ、真空中で高周波誘
導電気炉によつて溶かし、ついで炉内にアルゴン
ガスを充填した後マンガン―窒素合金(窒素8%
含有)20gを添加し、よく撹拌して均質な溶融合
金とした。その後の製造工程は実施例1と同じで
ある。試料に種々の熱処理を施して第2表に示す
ような特性が得られた。[Table] Example 2 Alloy number 74 (composition Ni=79.8%, Nb=7.0%, Mn
= 2.5%, N = 0.013%, balance Fe) To make the sample, first nickel, iron, and niobium were used.
780g was placed in an alumina crucible and melted in a high-frequency induction electric furnace in a vacuum. After filling the furnace with argon gas, a manganese-nitrogen alloy (8% nitrogen) was melted.
(containing) was added and stirred well to obtain a homogeneous molten alloy. The subsequent manufacturing steps are the same as in Example 1. The samples were subjected to various heat treatments and the properties shown in Table 2 were obtained.
【表】
つぎに第3表には1150℃の水素中で2時間加熱
した後、600℃から種々な速度で常温まで冷却す
るか、あるいはこれをさらに600℃以下の温度で
再加熱して、常温で測定された代表的な合金の諸
特性が示してある。[Table] Next, Table 3 shows that after heating in hydrogen at 1150°C for 2 hours, cooling from 600°C to room temperature at various rates, or further heating at a temperature below 600°C, The properties of representative alloys measured at room temperature are shown.
【表】【table】
【表】
つぎに本発明合金の窒素添加効果について図面
によつて詳細に述べる。第1図には80.3%Ni―
Fe―5%Nb―N合金についてN量と飽和磁束密
度,実効透磁率,硬度および摩耗量との関係が示
してある。一般に窒素量の増加とともに硬度は著
しく増大し、同時に摩耗量は著しく減少するが、
特に窒素の微量添加で極めてその効果が大きい。
また、一般に窒素の添加は磁気記録再生ヘツド
を作動させる交流磁界、特に高周波磁界において
実効透磁率を高める効果が大きい。しかし窒素が
0.3%以上では鍛造,加工が困難となり、また磁
気特性も磁気ヘツド用磁性合金として不適当にな
ることがわかる。
第2図は80.3%Ni―Fe―Nb合金と窒素を0.010
%含んだ80.3%Ni―Fe―Nb%―0.010%N合金に
ついて、ニオブ量と硬度および摩耗量との関係を
示したもので、ニオブ量の増加とともに窒素添加
の効果が著しく増大することがわかる。
第3図はNo.13(80.3%Ni―Fe―5.0%Nb―0.01
%N)、No.36(79.6%Ni―Fe―6.3%Nb―0.003%
N―2.0%Mo)、No.60(74.5%Ni―Fe―3.0%Nb―
0.009%N―5.0%Ta)およびNo.128(81.5%Ni―
Fe―3.5%Nb―0.013%N―3.0%Cr)の各合金を
1150℃において加熱した後400℃/時の速度で冷
却したときの加熱時間と実効透磁率との関係を示
したもので、各合金にはそれぞれ最適な加熱時間
が存在することがわかる。第4図はNo.13,No.36,
No.60及びNo.128の各合金を1150℃において適当時
間加熱した後規則―不規則格子変態点以上の温度
から冷却したときの冷却速度と実効透磁率との関
係を示したもので、各合金にはそれぞれ最適な冷
却速度が存在することがわかる。第5図はNo.13,
No.36,No.60及びNo.128の各合金を1150℃において
適当時間加熱した後規則―不規則格子変態点以上
の温度から400℃/時の速度で冷却し、さらに規
則―不規則格子変態点以下の適当な温度で再加熱
したときの再加熱時間と実効透磁率との関係を示
したもので、各合金にはそれぞれ最適な再加熱温
度および再加熱時間が存在することがわかる。
本発明合金のこのような高い硬度および耐摩耗
性の向上はニオブの効果により、Ni―Fe合金の
地が固溶体硬化するが、これに窒素を添加すると
格子間に窒素原子が侵入して地をさらに硬化する
とともに、強固なニオブ系窒化物その他ニツケル
系,鉄系窒化物などが地に微細に析出して、さら
に硬化が進むものと考えられる。また、これらの
窒化物の微細な析出は磁区を分割して磁壁を増加
させるので、交流磁界における磁壁の移動速度を
相対的に減少させ、そのため渦電流損失が小さく
なり、大きな実効透磁率が得られるものと考えら
れる。
さらに副成分として添加するMo,W,Ta,
Mn,Cu,Co,Cr,V,Ti,Ge,Ga,In,Tl,
Al,Si,Zr,Hf,希土類元素,白金族元素,
Be,Sn,SbおよびB等は本発明合金の比電気抵
抗を高める効果があり、またCoは飽和磁束密度
を高めるのに有効であり、さらにW,Ta,V,
Ti,Ge,Ga,In,Tl,Al,Si,Zr,Hf,希土類
元素,白金族元素,Be,Sn,SbおよびB等は本
発明合金の耐摩耗性を改善する効果が大きい。ま
たこれらの副成分も窒化物を生成し、上記のよう
に実効透磁率および耐摩耗性を改善する。
本発明合金は飽和磁束密度が5000G以上である
ので、磁気ヘツド用磁性合金として好適であるば
かりでなく、実効透磁率が大きく、硬度が高く、
耐摩耗性がすぐれ、且つ加工性が良好なので
VTRおよび電子計算機の磁気記録再生ヘツドな
らびに普通の電気機器などに用いる磁性材料とし
ても非常に好適である。
次に本発明において合金の組成をニツケル70〜
86%、ニオブ0.5〜10%、窒素0.0003〜0.3%およ
び残部鉄と限定し、またこれに添加する元素をモ
リブデン,タングステン,タンタル,マンガン,
銅,コバルトのそれぞれ7%以下、クロム,バナ
ジウム,チタン,ゲルマニウム,ガリウム,イン
ジウム,タリウムのそれぞれ5%以下、アルミニ
ウム,ケイ素,ジルコニウム,ハフニウム,希土
類元素,白金族元素のそれぞれ3%以下、ベリリ
ウム,錫,アンチモンのそれぞれ2%以下、ホウ
素の2%以下の1種または2種以上の合計0.01〜
7%と限定した理由は、実施例第3表第1図およ
び第2図で明らかなように、その組成範囲の飽和
磁束密度は5000G以上で、実効透磁率および硬度
が高く耐摩耗性にすぐれ、且つ加工性も良好であ
るが、組成がこの範囲をはずれると、飽和磁束密
度が5000G以下となり、実効透磁率および硬度が
低く摩耗が大きくなり、かつ加工が困難となり、
磁気記録再生ヘツドの材料として不適当となるか
らである。すなわち、ニオブが0.5%以下および
窒素が0.0003%未満では添加効果が小さく、ニオ
ブが10%を越えると飽和磁束密度が5000G以下と
なり、また窒素が0.3%を越えると鍛造加工が困
難となる。そしてこれに副成分としてモリブデン
7%、タングステン7%、マンガン7%、銅7
%、クロム5%、バナジウム5%、チタン5%、
ゲルマニウム5%、ガリウム5%、インジウム5
%、タリウム5%、アルミニウム3%、ケイ素3
%、ハフニウム3%、希土類元素3%、白金族元
素3%のそれぞれを越え添加すると飽和磁束密度
が5000G以下となるからであり、ベリリウム2
%、錫2%、アンチモン2%、ホウ素1%のそれ
ぞれを越えて添加すると鍛造あるいは加工が困難
となるからであり、Coを7%を越え添加すると
実効透磁率が小さくなるからである。
なお、第3表より明らかなように、Ni―Fe―
Nb―N系合金に副成分の何れかを入れると実効
透磁率は大きくなり、また、硬度も高くなり、耐
摩耗性が改善されるのでこれらの副成分の添加は
同一効果であり、同効成分と見做し得る。また希
土類元素はスカンジウム,イツトリウムおよびラ
ンタン系元素からなるものであるが、その効果は
全く同一であり、白金族元素は白金,イリジウ
ム,ルテニウム,ロジウム,パラジウム,オスミ
ウムからなるが、その効果も全く同一である。
なお、炭素および酸素は硬度を高め耐摩耗性を
改善するので、加工性および磁気特性を損なわな
い程度のそれぞれ0.1%添加までは有効であり、
本発明合金に含有されても差支えない。[Table] Next, the effect of adding nitrogen to the alloy of the present invention will be described in detail with reference to the drawings. Figure 1 shows 80.3%Ni-
The relationship between the amount of N, saturation magnetic flux density, effective magnetic permeability, hardness, and amount of wear is shown for the Fe-5%Nb-N alloy. Generally, as the amount of nitrogen increases, the hardness increases significantly, and at the same time the amount of wear decreases significantly.
In particular, the effect of adding a small amount of nitrogen is extremely large. Further, in general, the addition of nitrogen has a great effect of increasing the effective magnetic permeability in an alternating magnetic field that operates a magnetic recording/reproducing head, especially in a high frequency magnetic field. But nitrogen
It can be seen that if the content exceeds 0.3%, forging and processing become difficult, and the magnetic properties become unsuitable as a magnetic alloy for magnetic heads. Figure 2 shows 80.3%Ni-Fe-Nb alloy and nitrogen at 0.010%
This graph shows the relationship between the amount of niobium, hardness, and wear amount for the 80.3%Ni-Fe-Nb%-0.010%N alloy, which shows that the effect of nitrogen addition increases significantly as the amount of niobium increases. . Figure 3 shows No. 13 (80.3%Ni-Fe-5.0%Nb-0.01
%N), No.36 (79.6%Ni-Fe-6.3%Nb-0.003%
N-2.0%Mo), No.60 (74.5%Ni-Fe-3.0%Nb-
0.009%N-5.0%Ta) and No.128 (81.5%Ni-
Fe-3.5%Nb-0.013%N-3.0%Cr) alloys
This graph shows the relationship between heating time and effective magnetic permeability when heated at 1150°C and then cooled at a rate of 400°C/hour, showing that each alloy has its own optimal heating time. Figure 4 shows No.13, No.36,
This graph shows the relationship between the cooling rate and effective magnetic permeability when each alloy No. 60 and No. 128 is heated at 1150℃ for an appropriate time and then cooled from a temperature above the regular-irregular lattice transformation point. It can be seen that each alloy has its own optimal cooling rate. Figure 5 is No. 13,
After heating the alloys No. 36, No. 60 and No. 128 at 1150℃ for an appropriate time, they were cooled at a rate of 400℃/hour from a temperature above the ordered-irregular lattice transformation point, and then the ordered-irregular lattice alloys were heated at a rate of 400℃/hour. This shows the relationship between reheating time and effective magnetic permeability when reheated at an appropriate temperature below the transformation point, and it can be seen that each alloy has its own optimal reheating temperature and reheating time. Such high hardness and improved wear resistance of the alloy of the present invention are due to the effect of niobium, which causes solid solution hardening of the base of the Ni-Fe alloy, but when nitrogen is added to this, nitrogen atoms enter between the lattices and harden the base. It is thought that as it hardens further, strong niobium-based nitrides, nickel-based nitrides, iron-based nitrides, etc. are finely precipitated on the ground, causing further hardening. In addition, these fine nitride precipitations divide the magnetic domain and increase the domain wall, which relatively reduces the movement speed of the domain wall in an alternating magnetic field, which reduces eddy current loss and provides a large effective magnetic permeability. It is considered that the Furthermore, Mo, W, Ta, added as subcomponents,
Mn, Cu, Co, Cr, V, Ti, Ge, Ga, In, Tl,
Al, Si, Zr, Hf, rare earth elements, platinum group elements,
Be, Sn, Sb, B, etc. have the effect of increasing the specific electrical resistance of the alloy of the present invention, Co is effective in increasing the saturation magnetic flux density, and W, Ta, V,
Ti, Ge, Ga, In, Tl, Al, Si, Zr, Hf, rare earth elements, platinum group elements, Be, Sn, Sb, B, and the like are highly effective in improving the wear resistance of the alloy of the present invention. These subcomponents also form nitrides, which improve the effective permeability and wear resistance as described above. Since the alloy of the present invention has a saturation magnetic flux density of 5000G or more, it is not only suitable as a magnetic alloy for magnetic heads, but also has a large effective magnetic permeability, high hardness,
It has excellent wear resistance and good workability.
It is also very suitable as a magnetic material for use in magnetic recording/reproducing heads for VTRs and computers, as well as ordinary electrical equipment. Next, in the present invention, the composition of the alloy is changed from Nickel 70 to
86%, niobium 0.5-10%, nitrogen 0.0003-0.3%, and the balance iron, and the elements added to this are molybdenum, tungsten, tantalum, manganese,
7% or less each of copper and cobalt, 5% or less each of chromium, vanadium, titanium, germanium, gallium, indium, and thallium, 3% or less each of aluminum, silicon, zirconium, hafnium, rare earth elements, and platinum group elements, beryllium, 2% or less each of tin and antimony, and 2% or less of boron, total of 0.01 or more
The reason for limiting it to 7% is that, as is clear from Figures 1 and 2 of Table 3 of Examples, the saturation magnetic flux density in that composition range is 5000G or more, the effective magnetic permeability and hardness are high, and the wear resistance is excellent. , and has good workability, but if the composition is outside this range, the saturation magnetic flux density will be less than 5000G, the effective magnetic permeability and hardness will be low, wear will be large, and machining will be difficult.
This is because it is unsuitable as a material for magnetic recording/reproducing heads. That is, when niobium is less than 0.5% and nitrogen is less than 0.0003%, the effect of addition is small, when niobium exceeds 10%, the saturation magnetic flux density becomes 5000G or less, and when nitrogen exceeds 0.3%, forging becomes difficult. In addition to this, the subcomponents are 7% molybdenum, 7% tungsten, 7% manganese, and 7% copper.
%, chromium 5%, vanadium 5%, titanium 5%,
Germanium 5%, gallium 5%, indium 5
%, thallium 5%, aluminum 3%, silicon 3
%, hafnium 3%, rare earth elements 3%, and platinum group elements 3%.
This is because adding more than 2% Co, 2% tin, 2% antimony, and 1% boron makes forging or processing difficult, and adding more than 7% Co reduces the effective magnetic permeability. Furthermore, as is clear from Table 3, Ni―Fe―
Adding any of the subcomponents to the Nb-N alloy increases the effective magnetic permeability, increases the hardness, and improves the wear resistance, so the addition of these subcomponents has the same effect. It can be considered as an ingredient. Rare earth elements consist of scandium, yttrium, and lanthanum-based elements, but their effects are exactly the same; platinum group elements consist of platinum, iridium, ruthenium, rhodium, palladium, and osmium, and their effects are exactly the same. It is. Note that carbon and oxygen increase hardness and improve wear resistance, so it is effective to add up to 0.1% of each without impairing workability and magnetic properties.
It may be contained in the alloy of the present invention.
第1図は80.3%Ni―Fe―5%Nb―N合金の窒
素量と実効透磁率,飽和磁束密度,硬度および摩
耗量との関係を示す特性図、第2図は80.3%Ni―
Fe―Nb合金および80.3%Ni―Fe―Nb―0.010%
N合金のニオブ量と硬度および摩耗量との関係を
示す特性図、第3図はNo.13,No.36,No.60およびNo.
128の各合金を1150℃において加熱した後400℃/
時の速度で冷却したときの加熱時間と実効透磁率
との関係を示す特性図、第4図はNo.13,No.36,No.
60およびNo.128の各合金を1150℃において適当時
間加熱した後規則―不規則格子変態点以上の温度
から冷却したときの冷却速度と実効透磁率との関
係を示す特性図、第5図はNo.13,No.36,No.60およ
びNo.128の各合金を1150℃において適当時間加熱
した後規則―不規則格子変態点以上の温度から
400℃/時の速度で冷却し、さらに規則―不規則
格子変態点以下の適当な温度で再加熱したときの
再加熱時間と実効透磁率との関係を示した特性図
である。
Figure 1 is a characteristic diagram showing the relationship between nitrogen content, effective magnetic permeability, saturation magnetic flux density, hardness, and wear amount of 80.3%Ni-Fe-5%Nb-N alloy, and Figure 2 is a characteristic diagram showing the relationship between nitrogen content and effective magnetic permeability, saturation magnetic flux density, hardness, and wear amount of 80.3%Ni-Fe-5%Nb-N alloy.
Fe-Nb alloy and 80.3%Ni-Fe-Nb-0.010%
A characteristic diagram showing the relationship between the amount of niobium, hardness, and wear amount of N alloys. Figure 3 shows No. 13, No. 36, No. 60, and No. 3.
After heating each alloy of 128 at 1150℃, 400℃/
Figure 4 is a characteristic diagram showing the relationship between heating time and effective magnetic permeability when cooling at the same speed as No. 13, No. 36, and No. 36.
Figure 5 is a characteristic diagram showing the relationship between cooling rate and effective permeability when alloys No. 60 and No. 128 are heated at 1150°C for an appropriate time and then cooled from a temperature above the regular-irregular lattice transformation point. After heating No. 13, No. 36, No. 60 and No. 128 alloys at 1150℃ for an appropriate time,
FIG. 2 is a characteristic diagram showing the relationship between reheating time and effective magnetic permeability when cooled at a rate of 400° C./hour and then reheated at an appropriate temperature below the regular-irregular lattice transformation point.
Claims (1)
10%、窒素0.0003〜0.3%、少量の不純物と残部
鉄からなり、飽和磁束密度5000G以上を有するこ
とを特徴とする磁気記録再生ヘツド用耐摩耗性高
透磁率合金。 2 重量比にてニツケル70〜86%、ニオブ0.5〜
10%、窒素0.0003〜0.3%、少量の不純物と残部
鉄とを主成分とし、副成分としてモリブデン,タ
ングステン,タンタル,マンガン,銅,コバルト
のそれぞれ7%以下、クロム,バナジウム,チタ
ン,ゲルマニウム,ガリウム,インジウム,タリ
ウムのそれぞれ5%以下、アルミニウム,ケイ
素,ジルコニウム,ハフニウム,希土類元素,白
金族元素のそれぞれ3%以下、ベリリウム,錫,
アンチモンのそれぞれ2%以下、ホウ素の1%以
下の1種または2種以上の合計0.01〜7%を含有
した合金より成り飽和磁束密度5000G以上を有す
ることを特徴とする磁気記録再生ヘツド用耐摩耗
性高透磁率合金。 3 重量比にてニツケル70〜86%、ニオブ0.5〜
10%、窒素0.0003〜0.3%、少量の不純物と残部
鉄からなる合金を600℃以上融点以下の温度で非
酸化性雰囲気あるいは真空中において、少なくと
も1分間以上組成に対応した適当時間加熱した
後、規則―不規則格子変態点以上の温度から100
℃/秒〜1℃/時の組成に対応した適当な速度で
常温まで冷却することを特徴とする磁気記録再生
ヘツド用耐摩耗性高透磁率合金の製造法。 4 重量比にてニツケル70〜86%、ニオブ0.5〜
10%、窒素0.0003〜0.3%、少量の不純物と残部
鉄からなる合金を600℃以上融点以下の温度で非
酸化性雰囲気あるいは真空中において、少なくと
も1分間以上100時間以下の組成に対応した適当
時間加熱した後、規則―不規則格子変態点以上の
温度から100℃/秒〜1℃/時の組成に対応した
適当な速度で常温まで冷却し、これをさらに規則
―不規則格子変態点以下の温度で非酸化性雰囲気
あるいは真空中において、1分間以上組成に対応
した適当時間再加熱し、冷却することを特徴とす
る磁気記録再生ヘツド用耐摩耗性高透磁率合金の
製造法。 5 重量比にてニツケル70〜86%、ニオブ0.5〜
10%、窒素0.0003〜0.3%、少量の不純物と残部
鉄とを主成分とし、副成分としてモリブデン,タ
ングステン,タンタル,マンガン,銅,コバルト
のそれぞれ7%以下、クロム,バナジウム,チタ
ン,ゲルマニウム,ガリウム,インジウム,タリ
ウムのそれぞれ5%以下、アルミニウム,ケイ
素,ジルコニウム,ハフニウム,希土類元素,白
金族元素のそれぞれ3%以下、ベリリウム,錫,
アンチモン,ホウ素のそれぞれ2%以下の1種ま
たは2種以上の合計0.01〜7%を含有した合金を
600℃以上融点以下の温度で非酸化性雰囲気ある
いは真空中において、少なくとも1分間以上組成
に対応した適当時間加熱した後、規則―不規則格
子変態点以上の温度から100℃/秒〜1℃/時の
組成に対応した適当な速度で常温まで冷却するこ
とを特徴とする磁気記録再生ヘツド用耐摩耗性高
透磁率合金の製造法。 6 重量比にてニツケル70〜86%、ニオブ0.5〜
10%、窒素0.0003〜0.3%、少量の不純物と残部
鉄とを主成分とし、副成分としてモリブデン,タ
ングステン,タンタル,マンガン,銅,コバルト
のそれぞれ7%以下、クロム,バナジウム,チタ
ン,ゲルマニウム,ガリウム,インジウム,タリ
ウムのそれぞれ5%以下、アルミニウム,ケイ
素,ジルコニウム,ハフニウム,希土類元素,白
金属元素のそれぞれ3%以下、ベリリウム,錫,
アンチモンのそれぞれ2%以下、ホウ素の1%以
下の1種または2種以上の合計0.01〜7%を含有
した合金を600℃以上融点以下の温度で非酸化性
雰囲気あるいは真空中において、少なくとも1分
間以上100時間以下の組成に対応した適当時間加
熱した後、規則―不規則格子変態点以上の温度か
ら100℃/秒〜1℃/時の組成に対応した適当な
速度で常温まで冷却し、これをさらに規則―不規
則格子変態点以下の温度で非酸化性雰囲気あるい
は真空中において、1分間以上組成に対応した適
当時間再加熱し、冷却することを特徴とする磁気
記録再生ヘツド用耐摩耗性高透磁率合金の製造
法。 7 重量比にてニツケル70〜86%、ニオブ0.5〜
10%、窒素0.0003〜0.3%、少量の不純物と残部
鉄からなり、飽和磁束密度5000G以上を有する合
金より成ることを特徴とする磁気記録再生ヘツ
ド。 8 重量比にてニツケル70〜86%、ニオブ0.5〜
10%、窒素0.0003〜0.3%、少量の不純物と残部
鉄とを主成分とし、副成分としてモリブデン,タ
ングステン,タンタル,マンガン,銅,コバルト
のそれぞれ7%以下、クロム,バナジウム,チタ
ン,ゲルマニウム,ガリウム,インジウム,タリ
ウムのそれぞれ5%以下、アルミニウム,ケイ
素,ジルコニウム,ハフニウム,希土類元素,白
金族元素のそれぞれ3%以下、ベリリウム,錫,
アンチモンのそれぞれ2%以下、ホウ素の1%以
下の1種または2種以上の合計0.01〜7%を含有
した合金より成ることを特徴とする磁気記録再生
ヘツド。[Claims] 1. Nickel 70-86%, niobium 0.5-0.5% by weight
10% nitrogen, 0.0003 to 0.3% nitrogen, a small amount of impurities, and the balance iron, and is characterized by having a saturation magnetic flux density of 5000G or more. 2 Nickel 70~86%, niobium 0.5~
10%, nitrogen 0.0003 to 0.3%, a small amount of impurities and the balance iron as the main components, and minor components of molybdenum, tungsten, tantalum, manganese, copper, cobalt each of up to 7%, chromium, vanadium, titanium, germanium, gallium. , 5% or less each of indium, thallium, 3% or less each of aluminum, silicon, zirconium, hafnium, rare earth elements, platinum group elements, beryllium, tin,
A wear-resistant material for a magnetic recording/reproducing head characterized by being made of an alloy containing 0.01 to 7% of one or more types, each containing 2% or less of antimony and 1% or less of boron, and having a saturation magnetic flux density of 5000G or more. High magnetic permeability alloy. 3 Nickel 70~86%, niobium 0.5~ by weight
After heating an alloy consisting of 10% nitrogen, 0.0003 to 0.3% nitrogen, a small amount of impurities, and the balance iron in a non-oxidizing atmosphere or in a vacuum at a temperature of 600°C or higher and lower than the melting point for at least 1 minute or more depending on the composition, Rule - 100 from temperature above irregular lattice transformation point
A method for producing a wear-resistant high permeability alloy for a magnetic recording/reproducing head, which comprises cooling to room temperature at an appropriate rate corresponding to the composition of the alloy. 4 Nickel 70~86%, niobium 0.5~ by weight
An alloy consisting of 10% nitrogen, 0.0003 to 0.3% nitrogen, a small amount of impurities, and the balance iron is heated in a non-oxidizing atmosphere or in vacuum at a temperature above 600°C and below the melting point for an appropriate time corresponding to the composition for at least 1 minute and up to 100 hours. After heating, it is cooled from a temperature above the ordered-disordered lattice transformation point to room temperature at an appropriate rate corresponding to the composition of 100°C/sec to 1°C/hour, and then cooled to room temperature at a temperature below the ordered-disordered lattice transformation point. 1. A method for producing a wear-resistant high permeability alloy for a magnetic recording/reproducing head, which comprises reheating at a temperature in a non-oxidizing atmosphere or in a vacuum for at least one minute for an appropriate time corresponding to the composition, and cooling. 5 Nickel 70-86%, Niobium 0.5-0.5% by weight
10%, nitrogen 0.0003 to 0.3%, a small amount of impurities and the balance iron as the main components, and minor components of molybdenum, tungsten, tantalum, manganese, copper, cobalt each of up to 7%, chromium, vanadium, titanium, germanium, gallium. , 5% or less each of indium, thallium, 3% or less each of aluminum, silicon, zirconium, hafnium, rare earth elements, platinum group elements, beryllium, tin,
An alloy containing 0.01 to 7% of one or more of antimony and boron, each of which is 2% or less.
After heating in a non-oxidizing atmosphere or vacuum at a temperature of 600℃ or higher and lower than the melting point for at least 1 minute or more for an appropriate time depending on the composition, it is heated at a temperature of 100℃/second to 1℃/second from the regular-irregular lattice transformation point or higher. A method for producing a wear-resistant high permeability alloy for magnetic recording/reproducing heads, which is characterized by cooling to room temperature at an appropriate rate corresponding to the composition at the time. 6 Nickel 70~86%, niobium 0.5~ by weight
10%, nitrogen 0.0003 to 0.3%, a small amount of impurities and the balance iron as the main components, and minor components of molybdenum, tungsten, tantalum, manganese, copper, cobalt each of up to 7%, chromium, vanadium, titanium, germanium, gallium. , 5% or less each of indium, thallium, 3% or less each of aluminum, silicon, zirconium, hafnium, rare earth elements, white metal elements, beryllium, tin,
An alloy containing a total of 0.01 to 7% of one or more types, each containing 2% or less of antimony and 1% or less of boron, is heated for at least 1 minute in a non-oxidizing atmosphere or in vacuum at a temperature of 600°C or higher and lower than the melting point. After heating for an appropriate time corresponding to the composition (100 hours or less), cooling from a temperature above the ordered-disorder lattice transformation point to room temperature at an appropriate rate corresponding to the composition between 100℃/sec and 1℃/hour. Wear resistance for magnetic recording and reproducing heads is further characterized by reheating the head at a temperature below the ordered-disorder lattice transformation point in a non-oxidizing atmosphere or in vacuum for at least 1 minute for an appropriate time corresponding to the composition, and cooling. Manufacturing method for high permeability alloys. 7 Nickel 70~86%, niobium 0.5~
1. A magnetic recording/reproducing head comprising an alloy comprising 10% nitrogen, 0.0003 to 0.3% nitrogen, a small amount of impurities, and the balance iron, and has a saturation magnetic flux density of 5000G or more. 8 Nickel 70~86%, niobium 0.5~ by weight
10%, nitrogen 0.0003 to 0.3%, a small amount of impurities and the balance iron as the main components, and minor components of molybdenum, tungsten, tantalum, manganese, copper, cobalt each of up to 7%, chromium, vanadium, titanium, germanium, gallium. , 5% or less each of indium, thallium, 3% or less each of aluminum, silicon, zirconium, hafnium, rare earth elements, platinum group elements, beryllium, tin,
1. A magnetic recording/reproducing head comprising an alloy containing 0.01 to 7% of one or more types, each containing 2% or less of antimony and 1% or less of boron.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP56139766A JPS5842741A (en) | 1981-09-07 | 1981-09-07 | Wear resistant alloy with high permeability for magnetic recording and reproducing head, its manufacture and magnetic recording and reproducing head |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP56139766A JPS5842741A (en) | 1981-09-07 | 1981-09-07 | Wear resistant alloy with high permeability for magnetic recording and reproducing head, its manufacture and magnetic recording and reproducing head |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5842741A JPS5842741A (en) | 1983-03-12 |
| JPS625972B2 true JPS625972B2 (en) | 1987-02-07 |
Family
ID=15252891
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP56139766A Granted JPS5842741A (en) | 1981-09-07 | 1981-09-07 | Wear resistant alloy with high permeability for magnetic recording and reproducing head, its manufacture and magnetic recording and reproducing head |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5842741A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0297583U (en) * | 1989-01-19 | 1990-08-03 |
Families Citing this family (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS60194051A (en) * | 1984-03-15 | 1985-10-02 | Daido Steel Co Ltd | Heat treatment method for magnetic alloys |
| JPS61174349A (en) * | 1985-01-30 | 1986-08-06 | Res Inst Electric Magnetic Alloys | Wear-resistant high permeability alloy and its manufacturing method, and magnetic recording/reproducing head |
| JPS61260420A (en) * | 1985-05-15 | 1986-11-18 | Hitachi Ltd | magnetic recording medium |
| JPS63149361A (en) * | 1986-12-11 | 1988-06-22 | Nippon Yakin Kogyo Co Ltd | Manufacture of iron-nickel alloy |
| JP2540374Y2 (en) * | 1992-02-06 | 1997-07-02 | 株式会社ニイクラ | Free album |
| JP2777319B2 (en) * | 1993-07-30 | 1998-07-16 | 財団法人電気磁気材料研究所 | Wear-resistant high-permeability alloy, method for producing the same, and magnetic recording / reproducing head |
| JP3294029B2 (en) * | 1994-11-16 | 2002-06-17 | 財団法人電気磁気材料研究所 | Wear-resistant high-permeability alloy, method for producing the same, and magnetic recording / reproducing head |
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| WO2020179082A1 (en) | 2019-03-07 | 2020-09-10 | 三菱日立パワーシステムズ株式会社 | Cobalt-based alloy powder, cobalt-based alloy sintered body, and method for producing cobalt-based alloy sintered body |
| EP3725902B1 (en) | 2019-03-07 | 2023-03-01 | Mitsubishi Heavy Industries, Ltd. | Cobalt-based alloy product and method for producing same |
| US11414728B2 (en) | 2019-03-07 | 2022-08-16 | Mitsubishi Heavy Industries, Ltd. | Cobalt based alloy product, method for manufacturing same, and cobalt based alloy article |
| SG11202012575WA (en) | 2019-03-07 | 2021-09-29 | Mitsubishi Power Ltd | Cobalt based alloy product |
| EP3733885A4 (en) | 2019-03-07 | 2020-12-30 | Mitsubishi Power, Ltd. | Heat exchanger |
-
1981
- 1981-09-07 JP JP56139766A patent/JPS5842741A/en active Granted
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0297583U (en) * | 1989-01-19 | 1990-08-03 |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5842741A (en) | 1983-03-12 |
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