JPS6133892B2 - - Google Patents
Info
- Publication number
- JPS6133892B2 JPS6133892B2 JP54040293A JP4029379A JPS6133892B2 JP S6133892 B2 JPS6133892 B2 JP S6133892B2 JP 54040293 A JP54040293 A JP 54040293A JP 4029379 A JP4029379 A JP 4029379A JP S6133892 B2 JPS6133892 B2 JP S6133892B2
- Authority
- JP
- Japan
- Prior art keywords
- terbium
- disprosium
- alloy
- magnetostrictive
- properties
- 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
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 49
- 229910045601 alloy Inorganic materials 0.000 claims description 48
- 239000000956 alloy Substances 0.000 claims description 48
- 229910052771 Terbium Inorganic materials 0.000 claims description 31
- GZCRRIHWUXGPOV-UHFFFAOYSA-N terbium atom Chemical compound [Tb] GZCRRIHWUXGPOV-UHFFFAOYSA-N 0.000 claims description 30
- 229910052761 rare earth metal Inorganic materials 0.000 claims description 24
- 229910000765 intermetallic Inorganic materials 0.000 claims description 20
- 150000002910 rare earth metals Chemical class 0.000 claims description 18
- 229910052742 iron Inorganic materials 0.000 claims description 17
- 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 3
- 239000012535 impurity Substances 0.000 claims description 2
- 239000011572 manganese Substances 0.000 description 25
- 229910052748 manganese Inorganic materials 0.000 description 20
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 18
- 238000006073 displacement reaction Methods 0.000 description 16
- 239000000463 material Substances 0.000 description 15
- 230000005291 magnetic effect Effects 0.000 description 14
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 12
- 238000005275 alloying Methods 0.000 description 10
- 239000000203 mixture Substances 0.000 description 8
- 230000006872 improvement Effects 0.000 description 7
- 150000003624 transition metals Chemical class 0.000 description 7
- 230000000052 comparative effect Effects 0.000 description 6
- 229910052759 nickel Inorganic materials 0.000 description 6
- 238000010587 phase diagram Methods 0.000 description 6
- 238000012360 testing method Methods 0.000 description 6
- 229910052723 transition metal Inorganic materials 0.000 description 6
- 229910000531 Co alloy Inorganic materials 0.000 description 4
- 238000006243 chemical reaction Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- QVYYOKWPCQYKEY-UHFFFAOYSA-N [Fe].[Co] Chemical compound [Fe].[Co] QVYYOKWPCQYKEY-UHFFFAOYSA-N 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- -1 iron and nickel Chemical class 0.000 description 3
- 238000002844 melting Methods 0.000 description 3
- 230000008018 melting Effects 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- NIPNSKYNPDTRPC-UHFFFAOYSA-N N-[2-oxo-2-(2,4,6,7-tetrahydrotriazolo[4,5-c]pyridin-5-yl)ethyl]-2-[[3-(trifluoromethoxy)phenyl]methylamino]pyrimidine-5-carboxamide Chemical compound O=C(CNC(=O)C=1C=NC(=NC=1)NCC1=CC(=CC=C1)OC(F)(F)F)N1CC2=C(CC1)NN=N2 NIPNSKYNPDTRPC-UHFFFAOYSA-N 0.000 description 2
- AFCARXCZXQIEQB-UHFFFAOYSA-N N-[3-oxo-3-(2,4,6,7-tetrahydrotriazolo[4,5-c]pyridin-5-yl)propyl]-2-[[3-(trifluoromethoxy)phenyl]methylamino]pyrimidine-5-carboxamide Chemical compound O=C(CCNC(=O)C=1C=NC(=NC=1)NCC1=CC(=CC=C1)OC(F)(F)F)N1CC2=C(CC1)NN=N2 AFCARXCZXQIEQB-UHFFFAOYSA-N 0.000 description 2
- 229910001252 Pd alloy Inorganic materials 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 239000006185 dispersion Substances 0.000 description 2
- 230000005294 ferromagnetic effect Effects 0.000 description 2
- SORXVYYPMXPIFD-UHFFFAOYSA-N iron palladium Chemical compound [Fe].[Pd] SORXVYYPMXPIFD-UHFFFAOYSA-N 0.000 description 2
- 229910052747 lanthanoid Inorganic materials 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 238000007254 oxidation reaction Methods 0.000 description 2
- 229910000914 Mn alloy Inorganic materials 0.000 description 1
- 229910001117 Tb alloy Inorganic materials 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 230000000996 additive effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- 238000010835 comparative analysis Methods 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 238000000265 homogenisation Methods 0.000 description 1
- 150000002602 lanthanoids Chemical class 0.000 description 1
- 239000002075 main ingredient Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000005381 potential energy Methods 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 229910000859 α-Fe Inorganic materials 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10N—ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10N35/00—Magnetostrictive devices
- H10N35/80—Constructional details
- H10N35/85—Magnetostrictive active materials
Landscapes
- Hard Magnetic Materials (AREA)
Description
本発明はすぐれた磁歪特性を示し、かつ靭性に
すぐれたテルビウム―デイスプロジウム基巨大磁
歪合金に関するものである。従来より磁性体を磁
化した場合、内部磁気配列の変化に応じ、磁性体
の長さが変化すること、すなわち外部磁場を作用
させた場合、磁歪が生ずることが知られていた。
この磁歪は磁歪フイルタ,磁歪センサ,超音波遅
延線,磁歪振動子等に応用されている。これらの
デバイスを構成する磁歪物質としては、ニツケル
基合金,鉄―コバルト合金,フエライト等が用い
られている。
近年、計測工学の進歩および精密機械分野の発
展に伴い、ミクロンオーダーの微小変位制御に不
可欠の変位駆動部の開発が必要とされている。の
変位駆動部の駆動機構の一つとして磁歪物質を用
いた磁気―機械変換デバイスが有力である。しか
しながら従来知られている磁歪物質では変位の絶
対量が充分でなく、ミクロンオーダーの精密変位
制御駆動部材料としては絶対駆動変位量のみなら
ず、精密制御の点からも満足し得るものではなか
つた。
また上記磁歪物質の変位量のみに着目すれば、
稀土類と鉄の金属間化合物がニツケル基合金の
100倍近い磁歪を示すことが知られているが、電
気入力エネルギーの機械的変位への変換効率が極
めて悪いことおよび材質的に脆弱であることのた
め駆動部材料としては満足し得るものでなかつ
た。
本発明者等はこのような点に対拠して検討を進
めた結果8重量%〜38重量%の鉄および0.01重量
%〜25重量%のマンガン,0.1重量%〜35重量%
のテルビウム並びに残部のデイスプロシウムおよ
び不随的不純物から成り、かつテルビウムとデイ
スプロシウムの重量比((テルビウム重量)/
(デイスプロシウム重量))が0.001以上0.5以下の
範囲内にあり、かつ50体積%以上のラーベス型金
属間化合物相と残部テルビウムおよびデイスプロ
シウムを主成分とした稀土類金属α相より構成さ
れる2相合金組織よりなるテルビウム−デイスプ
ロシウム基巨大磁歪合金を見い出したものであ
る。
即ち本発明は優れた磁歪特性および靭性を有
し、特に精密変位制御駆動部用磁気―機械変位変
換デバイスの主要部材である磁歪物質に適したテ
ルビウム―デイスプロシウム基巨大磁歪合金を提
供する事を目的とする。
以下本発明を詳細に説明すると、本発明に係る
合金において、テルビウム,デイスプロシウムは
稀土類(ランタナイド)に属し、鉄,ニツケル等
の3d遷移金属と異なり、4f電子の強い軌道角運動
量のため極めて大きい結晶異方性を有し、すぐれ
た磁歪特性を得るための必須成分であると同時に
すぐれた靭性を付与する合金主成分でもある。し
かしながらテルビウム,デイスプロシウム単体、
あるいはテルビウム―デイスプロシウム合金で
は、低温領域では優れた磁歪特性を示すものの、
室温以上の温度領域では磁歪を示さず、満足した
特性を得ることが不可能である。
本発明合金の主要合金(添加)元素である鉄お
よびマンガンはテルビウムおよびデイスプロシウ
ムとラーベス型金属間化合物を形成し、テルビウ
ムおよびデイスプロシウム,テルビウム―デイス
プロシウム合金における室温以上の温度領域にお
ける磁歪特性を著しく向上せしめ、満足し得る特
性に至らしめるものである。鉄およびマンガンの
合金成分範囲をそれぞれ8重量%以上38重量%以
下の鉄,0.01重量%以上25重量%以下のマンガン
と限定する理由は、鉄,マンガンともにそれぞれ
8重量%未満の鉄,0.01重量%未満のマンガンで
は十分な磁歪特性の向上が得られず、38重量%を
超える鉄では靭性が著しく劣下し、脆弱になり、
25重量%を超えるマンガンでは磁歪特性が劣下す
るため上記合金成分範囲に限定する。さらにテル
ビウムの合金成分範囲を0.1重量%以上35重量%
以下でかつテルビウムとデイスプロシウムの重量
比((テルビウム重量)/(デイスプロシウム重
量))が0.001以上0.5以下の範囲内と限定する理
由はテルビウムの合金化によりデイスプロシウム
のみの場合に較べ、鉄およびマンガンによる磁歪
特性の向上が一層高められ、優れた磁歪特性を示
すテルビウム―デイスプロシウム基合金が実現さ
れるわけであるが、0.1重量%未満のテルビウム
では磁歪特性の向上が得られず、35重量%を越え
るテルビウムにおいては、かえつて磁歪特性の劣
化が認められることから、0.1重量%以上35重量
%以下の範囲に限定した。さらに上記テルビウム
限定範囲内においてもテルビウムとデイスプロシ
ウムの重量比が0.001以上0.5以下の範囲に含まれ
ない場合、磁歪特性の向上が得られないので、限
定範囲につけ加えた。
加えて本発明合金中に認められるラーベス型金
属間化合物の体積%としては50%を満たさない場
合、靭性その他の機械的性質はすぐれるものの満
足し得る磁歪特性が得られないので、50%以上の
ラーベス型金属間化合物を含むことを限定する。
次に本発明合金において遷移金属添加元素とし
て鉄およびマンガンに限定した理由を実験データ
に基づき説明する。デイスプロシウムおよびテル
ビウム金属は鉄およびマンガン等の遷移金属とラ
ーベス型金属間化合物を作る。ラーベス型金属間
化合物を作ることにより、テルビウム―デイスプ
ロシウム合金等の稀土類金属・合金のすぐれた磁
歪特性は室温以上に持ち来たされる。これは広義
の意味での強磁性相が室温以上の温度まで安定化
されるためである。強磁性相の消失する温度は稀
土類金属において一例を挙げるならば、デイスプ
ロシウムにおいて、179K(−94℃)である。一
方ラーベス型金属間化合物においてDyFe2の場合
635K(358℃)である。以上のごとく遷移金属は
稀土類金属の合金化においてラーベス型金属間化
合物を形成し、すぐれた磁歪特性を室温以上の温
度に持ち来たすわけである。ラーベス型金属間化
合物の室温における飽和磁歪値を第1表に示す。
The present invention relates to a terbium-disprodium-based giant magnetostrictive alloy that exhibits excellent magnetostrictive properties and excellent toughness. It has been known that when a magnetic body is magnetized, the length of the magnetic body changes in response to changes in the internal magnetic arrangement, that is, when an external magnetic field is applied, magnetostriction occurs.
This magnetostriction is applied to magnetostrictive filters, magnetostrictive sensors, ultrasonic delay lines, magnetostrictive vibrators, etc. Nickel-based alloys, iron-cobalt alloys, ferrite, and the like are used as magnetostrictive materials constituting these devices. In recent years, with advances in measurement engineering and development in the field of precision machinery, there has been a need to develop a displacement drive unit that is indispensable for minute displacement control on the micron order. A magneto-mechanical conversion device using a magnetostrictive material is promising as one of the drive mechanisms for the displacement drive unit. However, conventionally known magnetostrictive materials do not have a sufficient absolute amount of displacement, and are not satisfactory as materials for drive parts for precise displacement control on the micron order, not only in terms of absolute drive displacement but also in terms of precision control. . Also, if we focus only on the amount of displacement of the magnetostrictive material,
Rare earth and iron intermetallic compounds form nickel-based alloys.
Although it is known to exhibit magnetostriction of nearly 100 times, it is not satisfactory as a drive part material because the conversion efficiency of electrical input energy into mechanical displacement is extremely poor and the material is brittle. Ta. The present inventors carried out studies based on these points, and as a result, iron of 8% to 38% by weight, manganese of 0.01% to 25% by weight, and 0.1% to 35% by weight
of terbium and the remainder disprosium and incidental impurities, and the weight ratio of terbium to disprosium ((terbium weight)/
(disprosium weight)) is in the range of 0.001 to 0.5, and is composed of 50% by volume or more of a Laves type intermetallic compound phase and the balance of rare earth metal α phase mainly composed of terbium and disprosium. We have discovered a terbium-disprosium-based giant magnetostrictive alloy consisting of a two-phase alloy structure. That is, the present invention provides a terbium-disprosium-based giant magnetostrictive alloy that has excellent magnetostrictive properties and toughness and is particularly suitable as a magnetostrictive material that is a main component of a magneto-mechanical displacement conversion device for a precision displacement control drive unit. With the goal. To explain the present invention in detail below, in the alloy according to the present invention, terbium and disprosium belong to rare earth elements (lanthanides), and unlike 3d transition metals such as iron and nickel, because of the strong orbital angular momentum of 4f electrons. It has extremely large crystal anisotropy and is an essential component for obtaining excellent magnetostriction properties, and at the same time is the main alloy component that provides excellent toughness. However, terbium, disprosium alone,
Alternatively, although the terbium-disprosium alloy exhibits excellent magnetostriction properties at low temperatures,
It does not exhibit magnetostriction in the temperature range above room temperature, making it impossible to obtain satisfactory characteristics. Iron and manganese, which are the main alloying (additional) elements of the alloy of the present invention, form a Laves type intermetallic compound with terbium and disprosium, and in the temperature range above room temperature in terbium, disprosium, and terbium-disprosium alloys. This significantly improves the magnetostrictive properties, leading to satisfactory properties. The reason for limiting the alloy composition ranges of iron and manganese to 8% to 38% by weight of iron and 0.01% to 25% by weight of manganese is that both iron and manganese must contain less than 8% by weight of iron and 0.01% by weight, respectively. If the amount of manganese is less than 38% by weight, sufficient improvement in magnetostrictive properties will not be obtained, and if the amount of iron is more than 38% by weight, the toughness will significantly deteriorate and the material will become brittle.
If manganese exceeds 25% by weight, the magnetostrictive properties deteriorate, so the alloy composition is limited to the above range. In addition, the range of terbium alloy composition has been increased from 0.1% by weight to 35% by weight.
The reason why the weight ratio of terbium and disprosium ((terbium weight)/(disprosium weight)) is limited to 0.001 or more and 0.5 or less is as follows: The magnetostrictive properties are further improved by iron and manganese, and a terbium-disprosium-based alloy exhibiting excellent magnetostrictive properties is realized, but with less than 0.1% by weight terbium, the magnetostrictive properties are not improved. First, if terbium exceeds 35% by weight, deterioration of the magnetostrictive properties is observed, so the content is limited to 0.1% by weight or more and 35% by weight or less. Furthermore, even within the above-mentioned limited range of terbium, if the weight ratio of terbium and disprosium is not within the range of 0.001 or more and 0.5 or less, no improvement in magnetostrictive properties can be obtained, so this was added to the limited range. In addition, if the volume percent of the Laves type intermetallic compound found in the alloy of the present invention is less than 50%, although the toughness and other mechanical properties are excellent, satisfactory magnetostriction properties cannot be obtained. It is limited to include Laves-type intermetallic compounds. Next, the reason why the transition metal additive elements in the alloy of the present invention are limited to iron and manganese will be explained based on experimental data. Disprosium and terbium metals form Laves-type intermetallic compounds with transition metals such as iron and manganese. By creating Laves-type intermetallic compounds, the excellent magnetostrictive properties of rare earth metals and alloys such as terbium-disprosium alloys can be brought to temperatures above room temperature. This is because the ferromagnetic phase in a broad sense is stabilized up to temperatures above room temperature. The temperature at which the ferromagnetic phase disappears is 179 K (-94° C.) in disprosium, to give an example of rare earth metals. On the other hand, in the case of DyFe 2 in the Laves type intermetallic compound
It is 635K (358℃). As described above, transition metals form Laves-type intermetallic compounds when rare earth metals are alloyed, and bring excellent magnetostrictive properties to temperatures above room temperature. Table 1 shows the saturation magnetostriction values of the Laves type intermetallic compounds at room temperature.
【表】
これらの値は従来の磁歪金属例えばニツケルの
飽和磁歪値30×10-6に比べ桁違いに大きいことが
一見できる。しかしラーベス型金属間化合物単相
の機械的性質は極めて悪く、特に加工性,靭性に
劣り、実用合金かはほど違い特性しか有していな
い。加えて第1表に示す飽和磁歪値を得るために
は、数十キロエルステツドという強磁場を必要と
し、1アンペア当り100エルステツド程度のソレ
ノイド型マグネツトを用い、電気―磁気変換を行
なうならば100アンペア以上の大電流を必要と
し、数十キロワツトの電力消費となり、実用上の
大きな障害となる。
加工性および靭性の改善策の一つとしては、ラ
ーベス型金属間化合物を構成する遷移金属を鉄と
マンガンとの合金にすることによつて達成され
る。またさらに加工性および靭性を向上せしめる
手段としてはラーベス型金属間化合物中に延性に
富む稀土類金属α相、特にα―デイスプロシウム
相を分散せしめ破壊靭性値を向上せしめることで
ある。しかしこのα―テルビウム―デイスプロシ
ウム相の分散による靭性,加工性の改善は熱平衡
状態図より上記鉄―マンガン―稀土類金属・合金
系に限定される。遷移金属―稀土類金属系状態図
は第1図に示すデイスプロシウム―マンガン系の
ごとき稀土類金属側においてDyMn2ラーベス型
金属間化合物より高稀土類金属元素濃度の化合物
が存在しない系と第2図に示すデイスプロシウム
―コバルト系のごとき稀土類金属側において
DyCo2ラーベス型金属間化合物より高稀土類元素
の化合物が存在する系とに大別される。本発明合
金製品に適用可能な合金系としてはデイスプロシ
ウム―マンガン系型の状態図を示す合金系に限定
されるわけであるが、これを満たす合金系として
は、鉄―マンガン稀土類合金系であるわけであ
る。
次にラーベス型金属間化合物中の稀土類金属お
よび遷移金属、特に稀土類金属としてはデイスプ
ロシウムのテルビウムによる合金化、遷移金属と
しては鉄のマンガンによる合金化に伴う磁歪特性
の変化及びα―テルビウム―デイスプロシウムに
より靭性を改善した場合の磁歪特性の変化につい
て説明する。
第3図および第4図に(TbyDy(1―y))1.33
(Fe1―xMnx)2系の各x値(マンガン濃度)、各y
値(テルビウム濃度)における磁歪特性を示す。
マンガンの合金化は室温、特に低磁場側(2kOe
以下)での磁歪特性において、yが0.2程度,テ
ルビウム濃度13重量%程度より低濃度側におい
て、鉄のマンガンによる合金化に伴い、顕著な磁
歪特性の向上が認められた。なお第3図において
磁歪特性はDy1.33Fe2の室温における磁歪特性を
10とした場合の相対値で示す。(Tb0.2Dy0.8)1.33
(Fe0.8Mn0.2)2においては、現在磁歪特性が明ら
かになつている物質中、最高の特性を示す
Tb0.3Dy0.7Fe2を上回るものである。加えて
Tb0.3Dy0.7Fe2は脆弱であることに較べ、
(Tb0.2Dy0.8)1.33(Fe0.8Mn0.2)2は著しく靭性の改
善が認められた。
一方テルビウムの合金化は、室温特に低磁場側
(2kOe以下)での磁歪特性において、x値,マン
ガン濃度の大小によらず、デイスプロシウムのテ
ルビウムによる合金金化に伴い、顕著な磁歪特性
の向上が認められた。加えてテルビウム合金化の
効果はxが0.1,0.2、特にx=0.2において顕著に
認められた。第4図における磁歪特性は
Dy1.33Fe2の室温における磁歪特性を10とした場
合の相対値で示す。この結果上記Tb0.3Dy0.7Fe2
に較べ低テルビウム濃度において、優れた磁歪特
性を示すものである。
稀土類金属は地球上に稀有な金属資源であり、
近年有限な資源の有効活用は、技術的問題の一つ
にまで高められている。この意味においても稀土
類ランタナイド中最も稀有で高価な金属の一つで
ある低テルビウム濃度化は、極めて実用上、技術
上意味が大きい。
また(Tb0.2Dy0.8)(Fe0.8Mn0.2)2―α(Tb―
Dy)系の磁歪特性を第5図に示す。なお磁歪特
性(Tb0.2Dy0.8)(Fe0.8Mn0.2)2の室温における磁
歪特性を10とした場合の相対値で示す。α―(テ
ルビウム―デイスプロシウム)体積パーセントが
50%を越えると急激に磁歪特性が劣下することが
判る。
以上のごとき実験事実に基づき本発明合金の組
成が限定された。
次に本発明の実施例について説明し、併せて本
発明の効果を確認するために比較例についても説
明する。
実施例 1
第2表,第3表,第4表のNo.2―1〜No.2―
14,No.3―1〜No.3―14,No.4―1〜No.4−14,
各14種類,合計42種類の合金を用意し、夫々アー
ク溶解後800℃で120時間均一化処理したのち切削
加工により厚さ3mm,幅6mm,長さ15mmの試験片
を作成した後、室温下において磁歪特性を測定し
た。[Table] At first glance, it can be seen that these values are orders of magnitude larger than the saturation magnetostriction value of 30×10 -6 for conventional magnetostrictive metals, such as nickel. However, the mechanical properties of single-phase Laves-type intermetallic compounds are extremely poor, especially in workability and toughness, and the properties are far different from those of practical alloys. In addition, in order to obtain the saturation magnetostriction values shown in Table 1, a strong magnetic field of tens of kilo Oersteds is required, and if a solenoid-type magnet with a per ampere of about 100 Oersteds is used and electric-magnetic conversion is performed, the magnetic field will exceed 100 Amps. This requires a large current of several tens of kilowatts, which poses a major obstacle in practical use. One of the measures to improve workability and toughness is to alloy the transition metal constituting the Laves-type intermetallic compound with iron and manganese. Furthermore, as a means to further improve workability and toughness, it is possible to improve the fracture toughness value by dispersing a highly ductile rare earth metal α phase, particularly an α-disprosium phase, in the Laves type intermetallic compound. However, improvements in toughness and workability due to the dispersion of this α-terbium-disprosium phase are limited to the above-mentioned iron-manganese-rare earth metal/alloy system based on the thermal equilibrium phase diagram. The phase diagram for the transition metal-rare earth metal system is shown in Figure 1, where there is no compound with a higher rare earth metal element concentration than the DyMn 2 Laves type intermetallic compound on the rare earth metal side, such as the disprosium-manganese system, and the phase diagram shown in Figure 1. On the rare earth metal side, such as the disprosium-cobalt system shown in Figure 2,
DyCo 2 It is broadly classified into systems in which compounds of higher rare earth elements exist than Laves type intermetallic compounds. The alloy systems that can be applied to the alloy products of the present invention are limited to alloy systems that exhibit a disprosium-manganese type phase diagram, but alloy systems that satisfy this include iron-manganese rare earth alloy systems. That is why. Next, we will discuss rare earth metals and transition metals in Laves-type intermetallic compounds, especially changes in magnetostrictive properties due to alloying of disprosium with terbium as a rare earth metal, and alloying of iron with manganese as a transition metal, and α- We will explain the change in magnetostrictive properties when toughness is improved by terbium-disprosium. In Figures 3 and 4 (TbyDy (1 - y) ) 1.33
(Fe 1 - x Mnx) Each x value (manganese concentration), each y of the 2 systems
Magnetostrictive properties at various values (terbium concentration) are shown.
Alloying of manganese is done at room temperature, especially on the low magnetic field side (2kOe
Regarding the magnetostrictive properties (below), when y is about 0.2 and the terbium concentration is lower than about 13% by weight, a remarkable improvement in the magnetostrictive properties was observed due to the alloying of iron with manganese. In addition, in Figure 3, the magnetostrictive properties are the magnetostrictive properties of Dy 1. 33 Fe 2 at room temperature.
Shown as a relative value when set to 10. ( Tb 0.2 Dy 0.8 ) 1.33
(Fe 0.8 Mn 0.2 ) 2 exhibits the best magnetostrictive properties among the materials whose magnetostrictive properties are currently known .
It exceeds Tb 0.3 Dy 0.7 Fe 2 . In addition
Compared to Tb 0 . 3 Dy 0 . 7 Fe 2 which is brittle,
(Tb 0.2 Dy 0.8 ) 1.33 ( Fe 0.8 Mn 0.2 ) 2 was found to have significantly improved toughness . On the other hand, when alloying terbium, the magnetostriction properties at room temperature, particularly in the low magnetic field (below 2 kOe), are significantly reduced, regardless of the x value or the manganese concentration, as disprosium becomes alloyed with terbium. Improvement was observed. In addition, the effect of terbium alloying was noticeable when x was 0.1 and 0.2, especially when x=0.2. The magnetostrictive characteristics in Figure 4 are
It is expressed as a relative value when the magnetostriction property of Dy 1 . 33 Fe 2 at room temperature is set to 10. As a result, the above Tb 0.3 Dy 0.7 Fe 2
It exhibits excellent magnetostrictive properties at low terbium concentrations compared to . Rare earth metals are rare metal resources on earth.
In recent years, effective utilization of limited resources has become a technical issue. In this sense as well, lowering the concentration of terbium, which is one of the rarest and most expensive metals among rare earth lanthanides, has great practical and technical significance. Also , (Tb 0.2 Dy 0.8 ) ( Fe 0.8 Mn 0.2 ) 2 ―α ( Tb―
Figure 5 shows the magnetostrictive characteristics of the Dy) system. The magnetostrictive properties (Tb 0.2 Dy 0.8 ) (Fe 0.8 Mn 0.2 ) 2 are expressed as relative values when the magnetostrictive properties at room temperature are taken as 10 . α-(terbium-disprosium) volume percent
It can be seen that when it exceeds 50%, the magnetostrictive properties deteriorate rapidly. Based on the above experimental facts, the composition of the alloy of the present invention was limited. Next, examples of the present invention will be described, and comparative examples will also be described in order to confirm the effects of the present invention. Example 1 No.2-1 to No.2- in Tables 2, 3, and 4
14, No. 3-1 ~ No. 3-14, No. 4-1 ~ No. 4-14,
A total of 42 types of alloys (14 types each) were prepared, and after arc melting each alloy was homogenized at 800℃ for 120 hours, a test piece with a thickness of 3 mm, width of 6 mm, and length of 15 mm was created by cutting. The magnetostrictive properties were measured.
【表】【table】
【表】【table】
【表】【table】
【表】
磁歪特性はコアマグネツトを用い、磁気回路の
一部に上記試料を挿入し、歪ゲージ法により測定
された。
なおNo.2シリーズは(テルビウム)/(デイス
プロシウム)重量比が0.1,No.3シリーズは(テ
ルビウム)/(デイスプロシウム)重量比が
0.2,No.4シリーズは(テルビウム)/(デイス
プロシウム)重量比が0.3である。
この測定結果は第5表,第6表,第7表に示す
通りである。[Table] Magnetostrictive properties were measured by the strain gauge method using a core magnet and inserting the above sample into a part of a magnetic circuit. The No. 2 series has a (terbium)/(disprosium) weight ratio of 0.1, and the No. 3 series has a (terbium)/(disprosium) weight ratio of 0.1.
The 0.2, No. 4 series has a (terbium)/(disprosium) weight ratio of 0.3. The measurement results are shown in Tables 5, 6, and 7.
【表】【table】
【表】【table】
【表】【table】
【表】
比較例 1
第8表のNo.5―1〜No.5―14に示す組成の14種
類の合金を用意し、実施例同様アーク溶解後800
℃で120時間均一化処理したのち切削加工により
厚さ3mm,幅6mm長さ15mmの試験片を作成した
後、実施例と同一条件下で磁歪特性を測定した。
また第8表のNo.5―15〜No.5―17に示す組成の従
来用いられているニツケル,鉄―コバルト系合金
および鉄―パラジウム系合金についても磁歪特性
を測定した。この結果を第9表に併記した。[Table] Comparative Example 1 Fourteen types of alloys with the compositions shown in No. 5-1 to No. 5-14 in Table 8 were prepared, and as in the example, after arc melting 800
After homogenizing at ℃ for 120 hours, a test piece with a thickness of 3 mm, width of 6 mm, and length of 15 mm was prepared by cutting, and then the magnetostrictive properties were measured under the same conditions as in the example.
The magnetostrictive properties were also measured for conventionally used nickel, iron-cobalt alloys, and iron-palladium alloys having the compositions shown in No. 5-15 to No. 5-17 in Table 8. The results are also listed in Table 9.
【表】
およびデイスプロシウムを主成分
としたα相ではない。(RT3相))
[Table] Main ingredients include and disprosium
It is not the α phase. (RT 3 phase))
【表】【table】
【表】
なお磁歪特性の比較にあたつては、低磁場側の
磁歪値に注目し、印加磁場2kOeにおける静的磁
気歪値を求め、No.5―5に示すDyFe2の磁歪特性
を10とし、これを基準として相対値で表示した。
上記実施例1の結果から明らかな如く、本発明
によるテルビウム―デイスプロシウム基巨大磁歪
合金は、DyFe2の磁歪特性に較べ、その室温,低
磁場(低電気入力)側での特性の大幅改善がなさ
れることが確認された。比較例1の5―17なるニ
ツケルに比べ本発明合金,実施例1―2の3―
9,実施例1―3の4―10においては約8倍から
9倍、すなわち従来最も用いられている磁歪材料
に比べ1桁近く磁歪特性が向上している。この事
実は、精密微小変位駆動用材料に例を取るなら
ば、従来1mで最大40μm程度の精密変位制御が
可能であつたところを同一長さ(1m)であれば
400μm程度の精密変位制御が可能となる以外に
同一変位(40μm)を精密変位制御するのであれ
ば10cm長さですみ、小型化できるとともに、この
サイズは実用化の可否を決める重要な因子でもあ
る。
更に本発明合金の磁歪特性は、比較例1の5―
15に示す鉄―コバルト合金,比較例5―16に示す
鉄―パラジウム合金の磁歪特性をも大幅に上回る
ものである。
加えて本発明合金はDyFe2の磁歪特性および靭
性の改善を検討した本発明者等が先に提案したデ
イスプロシウム基巨大磁歪合金の磁歪特性をさら
に3倍近く向上せしめた合金である。
第6図に本発明合金、実施例1−2の3―9,
実施例1―3の4―10および脆弱ではあるが磁歪
特性に優れたラーベス型金属間化合物
Tb0.3Dy0.7Fe2の低磁場(低電気入力エネルギ
ー)側の磁歪特性を示すが、本発明合金は低電気
入力側において、Tb0.3Dy0.7Fe2を上回る特性を
示し、かつ電気入力に対する直線性に優れ、高速
交流制御においては極めて有利な特性を有してい
る。
なお上記実施例では磁歪特性の向上のみについ
て示したが、実施例1に示したような巨大磁歪合
金を精密変位駆動部材あるいは強力超音波発生部
材に適用する場合、磁歪特性に加え靭性は実用上
大きな問題となる。以下実施例1,第2表,第3
表,第4表に示した本発明合金および比較例2,
第10表に示した合金について、靭性の改善の実施
例について説明する。[Table] When comparing the magnetostriction properties, we focused on the magnetostriction value on the low magnetic field side, calculated the static magnetostriction value at an applied magnetic field of 2 kOe, and compared the magnetostriction properties of DyFe 2 shown in No. 5-5 to 10 The value is expressed as a relative value using this as a standard. As is clear from the results of Example 1 above, the terbium-disprosium-based giant magnetostrictive alloy according to the present invention has significantly improved properties at room temperature and in a low magnetic field (low electrical input) compared to the magnetostrictive properties of DyFe 2 . It has been confirmed that this will be done. Compared to the nickel 5-17 of Comparative Example 1, the alloy of the present invention, 3- of Example 1-2
9. In Example 4-10 of Example 1-3, the magnetostrictive properties are improved by about 8 to 9 times, that is, by nearly one order of magnitude compared to the conventionally most used magnetostrictive material. Taking the example of materials for precision micro-displacement drives, this fact means that while conventionally it was possible to precisely control displacement up to 40 μm over 1 m, if the same length (1 m) is used,
In addition to enabling precise displacement control of about 400 μm, if the same displacement (40 μm) is to be precisely controlled, the length is only 10 cm, which allows for miniaturization, and this size is also an important factor in determining whether it can be put into practical use. . Furthermore, the magnetostrictive properties of the alloy of the present invention are as follows:
It also significantly exceeds the magnetostrictive properties of the iron-cobalt alloy shown in No. 15 and the iron-palladium alloy shown in Comparative Example 5-16. In addition, the alloy of the present invention is an alloy that further improves the magnetostrictive properties by nearly three times that of the disprosium-based giant magnetostrictive alloy previously proposed by the present inventors who investigated improvements in the magnetostrictive properties and toughness of DyFe 2 . Figure 6 shows the alloy of the present invention, 3-9 of Example 1-2,
4-10 of Example 1-3 and Laves-type intermetallic compound with excellent magnetostrictive properties although fragile
Tb 0.3 Dy 0.7 Fe 2 exhibits magnetostrictive properties on the low magnetic field ( low electrical input energy) side, but the alloy of the present invention has properties superior to Tb 0.3 Dy 0.7 Fe 2 on the low electrical input side. It exhibits excellent linearity with respect to electrical input, and has extremely advantageous characteristics in high-speed AC control. In addition, although the above example shows only the improvement of magnetostrictive properties, when applying a giant magnetostrictive alloy as shown in Example 1 to precision displacement drive members or powerful ultrasonic generation members, toughness in addition to magnetostrictive properties is practically important. It becomes a big problem. Below is Example 1, Table 2, and Table 3.
The present invention alloy and Comparative Example 2 shown in Tables 4 and 4,
Examples of improving the toughness of the alloys shown in Table 10 will be described.
【表】
実施例 2
第2表のNo.2―1〜No.2―14,第3表No.3―1
〜3―14,第4表No.4―1〜4―14,各14種類,
合計42種類の合金を用意し、夫々アーク溶解後
800℃で120時間均一化処理したのち切削加工によ
り、10〓mm×100mmの試験片を作成した。靭性
の比較評価方法としては凹凸を有する鉄製敷板へ
の落下試験を採用し、同一形状(ほぼ同一重量)
の試験片をA(0.5m),B(1m),C(2m),
D(3m)の4種類の異なる位置エネルギーの位
置より自然落下させ、破壊の有無を調べた。この
結果は第11表に示す通りである。なお靭性の表示
方法としては位置A以下の位置より落下させたと
き破壊したものは×印,位置A以上位置B以下の
位置より落下させたとき破壊したものは△印,位
置B以上位置C以下より落下させたとき破壊した
ものは〇印,位置C以上位置D以下より落下させ
たとき破壊したものは◎印,位置D以上より落下
させたとき破壊するものあるいは破壊をまつたく
おこさないものは↑印で示した。[Table] Example 2 No.2-1 to No.2-14 in Table 2, No.3-1 in Table 3
~3-14, Table 4 No.4-1 to 4-14, 14 types each,
A total of 42 types of alloys are prepared, and after arc melting each
After homogenization treatment at 800°C for 120 hours, a 10mm x 100mm test piece was created by cutting. As a comparative evaluation method for toughness, we adopted a drop test on an uneven iron plate, and tested the same shape (almost the same weight).
Test pieces A (0.5m), B (1m), C (2m),
D (3 m) was allowed to fall naturally from four different potential energy positions, and the presence or absence of breakage was examined. The results are shown in Table 11. In addition, the toughness is indicated by an X mark if the product was broken when dropped from a position A or below, a △ mark if a product was broken when dropped from a position A or above B or below, and a △ mark if the product was broken when dropped from a position B or above. Items that break when dropped from a higher position are marked with ○, items that are broken when dropped from position C or higher and lower than position D are marked with ◎, items that break when dropped from position D or higher, or those that do not cause destruction at all. Indicated by ↑.
【表】
比較例 2
本発明合金におけるマンガンの合金化および稀
土類金属濃度の靭性への効果を確認するために第
10表のNo.10―1〜No.10―5の合金を実施例2と同
一条件で作成した後、同一条件で試験した。この
試験結果は第12表に示す通りである。[Table] Comparative Example 2 In order to confirm the effect of manganese alloying and rare earth metal concentration on toughness in the alloy of the present invention,
Alloys No. 10-1 to No. 10-5 in Table 10 were prepared under the same conditions as in Example 2, and then tested under the same conditions. The test results are shown in Table 12.
【表】
上記実施例2の結果から明らかなごとく、マン
ガンの合金化およびラーベス型金属間化合物化学
量論的組成の稀土類金属濃度以上の稀土類金属濃
度によつて著しく靭性の改善がなされている。す
なわち本発明合金であるテルビウム―デイスプロ
シウム―鉄―マンガン系よりなるテルビウム―デ
イスプロシウム基合金はマンガンの合金化延性に
富むα―(Tb―Dy)の分散により、金属間化合
物のもつ脆弱性を克服し、実用にたえうる靭性の
付与を可能ならしめたものである。加えて化学量
論的組成の稀土類金属濃度以上の稀土類金属濃度
により、室温における耐酸化性,耐食性をも向上
せしめることが可能である。
以上説明した如く本発明によるテルビウム―デ
イスプロシウム―鉄―マンガン系テルビウム―デ
イスプロシウム基合金は従来の磁歪材料の特性に
比べ、極めて優れた磁歪特性を有するとともに靭
性および耐酸化等の実用材料に不可欠な要因をも
満たし、特にミクロンオーダーの微小変位制御用
駆動部強力超音波発生用振動子,センサ等の構成
材料として極めて優れた特性を有するものであ
る。[Table] As is clear from the results of Example 2 above, toughness was significantly improved by alloying manganese and by increasing the rare earth metal concentration higher than the rare earth metal concentration in the Laves type intermetallic compound stoichiometric composition. There is. In other words, the terbium-disprosium-based alloy consisting of the terbium-disprosium-iron-manganese system, which is the alloy of the present invention, has a high resistance to the brittleness of intermetallic compounds due to the dispersion of α-(Tb-Dy), which is rich in alloying ductility of manganese. This has made it possible to overcome the toughness and provide toughness that is suitable for practical use. In addition, by having a rare earth metal concentration higher than the rare earth metal concentration in the stoichiometric composition, it is possible to improve oxidation resistance and corrosion resistance at room temperature. As explained above, the terbium-disprosium-iron-manganese terbium-disprosium-based alloy according to the present invention has extremely superior magnetostrictive properties compared to the properties of conventional magnetostrictive materials, and is a practical material with good toughness and oxidation resistance. It also satisfies the essential factors, and has extremely excellent properties especially as a constituent material for drive units for micron-order minute displacement control, vibrators for generating powerful ultrasonic waves, sensors, etc.
第1図はデイスプロシウム―マンガン合金状態
図、第2図はデイスプロシウム―コバルト合金状
態図、第3図は(TbyDy(1―y))1.33
(Fe1―xMnx)2におけるマンガン濃度と磁歪特性
との関係を示す曲線図、第4図は
(TbyDy(1―y))1.33(Fe1―xMnx)2におけるテル
ビウム濃度と磁歪特性との関係を示す曲線図、第
5図はα(Tb―Dy)―Tb0.2Dy0.8)
(Fe0.8Mn0.2)2におけるα―(Tb―Dy)体積パー
セントと磁歪特性との関係を示す曲線図、第6図
は本発明合金およびTb0.3Dy0.7Fe2の低磁場側の
磁歪特性を示す曲線図。
Figure 1 is a disprosium-manganese alloy phase diagram, Figure 2 is a disprosium-cobalt alloy phase diagram, and Figure 3 is (TbyDy (1 - y) ) 1.33
Figure 4 is a curve diagram showing the relationship between manganese concentration and magnetostriction properties at (Fe 1 - x Mnx) 2. Figure 4 shows the relationship between terbium concentration and magnetostriction at ( TbyDy ( 1 - y) ) 1 . A curve diagram showing the relationship with the characteristics , Figure 5 is α(Tb-Dy)-Tb 0.2 Dy 0.8 )
(Fe 0.8 Mn 0.2 ) 2 A curve diagram showing the relationship between α-(Tb - Dy) volume percentage and magnetostriction properties, Figure 6 shows the alloy of the present invention and Tb 0.3 Dy 0.7 Fe 2 A curve diagram showing the magnetostriction characteristics on the low magnetic field side of .
Claims (1)
25重量%のマンガン,0.1重量%〜35重量%のテ
ルビウム並びに残部のデイスプロジウムおよび不
随的不純物から成り、かつテルビウムとデイスプ
ロジウムの重量比((テルビウム/(デイスプロ
ジウム重量))が0.001以上0.5以下の範囲内にあ
り、かつ50体積%以上のラーベス型金属間化合物
相と残部テルビウムおよびデイスプロジウムを主
成分とした稀土類金属α相より構成される2相合
金組織より成るテルビウム―デイスプロジウム基
巨大磁歪合金。1 8wt%~38wt% iron and 0.01wt%~
Consists of 25% by weight of manganese, 0.1% to 35% by weight of terbium, and the remainder disprosium and incidental impurities, and the weight ratio of terbium to disprosium ((terbium/(disprosium weight)) is 0.001 or more and 0.5 or less A terbium-disprosium group consisting of a two-phase alloy structure consisting of a Laves-type intermetallic compound phase of 50% or more by volume and a rare earth metal α phase mainly composed of terbium and disprosium. Magnetostrictive alloy.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4029379A JPS55134150A (en) | 1979-04-05 | 1979-04-05 | Terbium- and dysprosium-base macro-magnetostrictive alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4029379A JPS55134150A (en) | 1979-04-05 | 1979-04-05 | Terbium- and dysprosium-base macro-magnetostrictive alloy |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS55134150A JPS55134150A (en) | 1980-10-18 |
| JPS6133892B2 true JPS6133892B2 (en) | 1986-08-05 |
Family
ID=12576548
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP4029379A Granted JPS55134150A (en) | 1979-04-05 | 1979-04-05 | Terbium- and dysprosium-base macro-magnetostrictive alloy |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS55134150A (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS59158574A (en) * | 1983-03-01 | 1984-09-08 | Toshiba Corp | Control element for minute displacement |
| DE68926768T2 (en) * | 1988-09-29 | 1996-12-12 | Toshiba Kawasaki Kk | Super magnetostrictive alloy |
| US5223046A (en) * | 1988-09-29 | 1993-06-29 | Kabushiki Kaisha Toshiba | Super-magnetostrictive alloy |
-
1979
- 1979-04-05 JP JP4029379A patent/JPS55134150A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS55134150A (en) | 1980-10-18 |
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