JPH0258334B2 - - Google Patents
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- Publication number
- JPH0258334B2 JPH0258334B2 JP3787681A JP3787681A JPH0258334B2 JP H0258334 B2 JPH0258334 B2 JP H0258334B2 JP 3787681 A JP3787681 A JP 3787681A JP 3787681 A JP3787681 A JP 3787681A JP H0258334 B2 JPH0258334 B2 JP H0258334B2
- Authority
- JP
- Japan
- Prior art keywords
- subcomponents
- temperature
- alloy
- less
- hexagonal lattice
- 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
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- 229910045601 alloy Inorganic materials 0.000 claims description 46
- 239000000956 alloy Substances 0.000 claims description 46
- 229910001374 Invar Inorganic materials 0.000 claims description 21
- 229910052782 aluminium Inorganic materials 0.000 claims description 15
- 229910052804 chromium Inorganic materials 0.000 claims description 15
- 230000005291 magnetic effect Effects 0.000 claims description 15
- 229910052710 silicon Inorganic materials 0.000 claims description 15
- 230000005290 antiferromagnetic effect Effects 0.000 claims description 13
- 238000010438 heat treatment Methods 0.000 claims description 13
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical group [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 claims description 13
- 229910052721 tungsten Inorganic materials 0.000 claims description 13
- 229910052725 zinc Inorganic materials 0.000 claims description 13
- 229910052787 antimony Inorganic materials 0.000 claims description 12
- 229910052785 arsenic Inorganic materials 0.000 claims description 12
- 229910052793 cadmium Inorganic materials 0.000 claims description 12
- 229910052733 gallium Inorganic materials 0.000 claims description 12
- 229910052737 gold Inorganic materials 0.000 claims description 12
- 229910052738 indium Inorganic materials 0.000 claims description 12
- 229910052745 lead Inorganic materials 0.000 claims description 12
- 229910052758 niobium Inorganic materials 0.000 claims description 12
- 229910052698 phosphorus Inorganic materials 0.000 claims description 12
- 229910052761 rare earth metal Inorganic materials 0.000 claims description 12
- 229910052716 thallium Inorganic materials 0.000 claims description 12
- 229910052718 tin Inorganic materials 0.000 claims description 12
- 229910052719 titanium Inorganic materials 0.000 claims description 12
- 229910052726 zirconium Inorganic materials 0.000 claims description 12
- 229910052790 beryllium Inorganic materials 0.000 claims description 11
- 229910052791 calcium Inorganic materials 0.000 claims description 11
- 229910052802 copper Inorganic materials 0.000 claims description 11
- 229910052749 magnesium Inorganic materials 0.000 claims description 11
- 238000002844 melting Methods 0.000 claims description 11
- 230000008018 melting Effects 0.000 claims description 11
- 229910052759 nickel Inorganic materials 0.000 claims description 11
- 229910052702 rhenium Inorganic materials 0.000 claims description 11
- 229910052717 sulfur Inorganic materials 0.000 claims description 11
- 229910052750 molybdenum Inorganic materials 0.000 claims description 10
- 229910052714 tellurium Inorganic materials 0.000 claims description 10
- 229910052796 boron Inorganic materials 0.000 claims description 8
- 229910052799 carbon Inorganic materials 0.000 claims description 8
- 238000001816 cooling Methods 0.000 claims description 7
- 239000012535 impurity Substances 0.000 claims description 7
- 238000011282 treatment Methods 0.000 claims description 7
- 238000004519 manufacturing process Methods 0.000 claims description 6
- 239000000203 mixture Substances 0.000 claims description 6
- 229910052720 vanadium Inorganic materials 0.000 claims description 6
- 239000013078 crystal Substances 0.000 claims description 3
- 238000000265 homogenisation Methods 0.000 claims description 3
- 230000004907 flux Effects 0.000 claims 2
- 230000001747 exhibiting effect Effects 0.000 claims 1
- 229910052732 germanium Inorganic materials 0.000 description 10
- 230000005294 ferromagnetic effect Effects 0.000 description 8
- 239000002994 raw material Substances 0.000 description 8
- 238000003303 reheating Methods 0.000 description 7
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 6
- 238000000691 measurement method Methods 0.000 description 6
- 238000000034 method Methods 0.000 description 6
- 229910000927 Ge alloy Inorganic materials 0.000 description 4
- 229910000914 Mn alloy Inorganic materials 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- 229910052748 manganese Inorganic materials 0.000 description 4
- 229910052786 argon Inorganic materials 0.000 description 3
- 238000005266 casting Methods 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 230000009466 transformation Effects 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 239000012298 atmosphere Substances 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 238000002474 experimental method Methods 0.000 description 2
- 238000000227 grinding Methods 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 230000001590 oxidative effect Effects 0.000 description 2
- 239000004576 sand Substances 0.000 description 2
- 229910052709 silver Inorganic materials 0.000 description 2
- 229910052715 tantalum Inorganic materials 0.000 description 2
- 238000005496 tempering Methods 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 1
- 239000002885 antiferromagnetic material Substances 0.000 description 1
- 239000012300 argon atmosphere Substances 0.000 description 1
- 229910002056 binary alloy Inorganic materials 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000005868 electrolysis reaction Methods 0.000 description 1
- 230000005293 ferrimagnetic effect Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 125000004435 hydrogen atom Chemical class [H]* 0.000 description 1
- 229910052741 iridium Inorganic materials 0.000 description 1
- 229910052742 iron Inorganic materials 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
- 230000005389 magnetism Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 229910052762 osmium Inorganic materials 0.000 description 1
- 229910052697 platinum Inorganic materials 0.000 description 1
- 238000003672 processing method Methods 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 229910052703 rhodium Inorganic materials 0.000 description 1
- 229910052707 ruthenium Inorganic materials 0.000 description 1
- 229910052706 scandium Inorganic materials 0.000 description 1
- 230000002269 spontaneous effect Effects 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 229910052727 yttrium Inorganic materials 0.000 description 1
Landscapes
- Heat Treatment Of Nonferrous Metals Or Alloys (AREA)
Description
本発明は−50℃〜+100℃における線熱膨脹係
数が−8×10-6〜+8×10-6と小さいMn−Ge基
多元系六方格子型反強磁性インバー型合金に関す
るものである。
従来、インバー型合金としては、鉄を基とする
多数の強磁性面心立方格子合金が見出されてい
る。しかし、これら合金は磁気変態点以下で正の
大きな自発体積磁歪をもつため、その熱膨脹係数
が一般の合金に比し数分の1以下であり、また強
磁性であるため、その用途には制限がある。特
に、これらインバー型合金を例えばビデオテープ
レコーダのヘツド支持部、テレビ受像器のシヤド
ウマスク、電子顕微鏡の試料支持台、電動化のた
め発生する不均一磁界中での振動を要求される時
計の天府輪、ガンギ、アンクル等あるいは重力振
子桿、原子炉、各種の制御機器などへ適用するこ
とは困難で、これら用途には非強磁性インバー型
合金が要求される。
非強磁性インバー型合金としては、すでに本発
明者等の発明になる六方格子型のMn−Ge系合金
があるが、この合金は優秀なインバー型特性を示
すにも拘わらず、硬くかつ脆いため、成形するに
は一般には砥石による研削加工を採用している。
従つてその加工性の改善が要求されていた。
本発明者等はインバー型特性を損うことなく上
記Mn−Ge系合金の加工性を改善するため幾多の
実験、研究を行つた結果、重量比にて主成分とし
てGe20〜33%、好ましくは23〜32%、副成分と
してCr、W、Vの何れか0.01〜11%、Mo、Ti、
Zr、Nb、Ta、Ag、Au、Re、白金族元素(Pd、
Pt、Rh、Ir、Ru、Os)の何れか0.01〜10%、
Zn、Cd、Al、Ga、In、Tl、Sn、Pbの何れか
0.01〜9%、Co、Ni、Si、As、Sb、Bi、Se、
Te、希土類元素(Sc、Yおよびランタン系元素)
の何れか0.01〜8%、Be、Mg、Ca、Bの何れか
0.01〜6%、C、P、Sの何れか0.01〜1%の何
れか1種または2種以上の全量0.01〜11%と不可
避の不純物1%以下と残部Mn(但し副成分がCo、
Niだけの場合を除く)とからなる合金に特定の
熱処理を施すことにより、−50℃〜+100℃におけ
る線熱膨脹係数が−8×10-6〜+8×10-6以内
で、研削加工が容易な六方格子型の反強磁性イン
バー型合金が得られることを見出したものであ
る。
本発明に係わるMn−Ge基多元系合金は約500
℃を境界として高温相が六方構造のε相、低温相
が面心正方構造のε1相であり、インバー特性はε
相の構造をもつ合金において発揮される。そして
ε相よりε1相への変態の速度が非常に遅いことが
一つの特長である。
本発明者等は上述のような反強磁性(非強磁
性)インバー型合金の特殊性を確認し、これを製
造する方法を幾多研究の結果、通常の電解で得ら
れた純度のMnと99〜99.9%程度の純度を有する
Geとからなる合金に上述した副成分から選択し
た第3ないし第4の元素を加えることによつて反
強磁性のインバー型合金の製造に成功したもの
で、本発明は重量比にて主成分としてGe20〜33
%、副成分としてCr、W、Vの何れか0.01〜11
%、Mo、Ti、Zr、Nb、Ta、Ag、Au、Re、白
金族元素の何れか0.01〜10%、Zn、Cd、Al、
Ga、In、Tl、Sn、Pbの何れか0.01〜9%、Co、
Ni、Cu、Si、As、Sb、Bi、Se、Te、希土類元
素の何れか0.01〜8%、Be、Mg、Ca、Bの何れ
か0.01〜6%、C、P、Sの何れか0.01〜1%の
何れか1種または2種以上の全量0.01〜11%と不
可避の不純物1%以下と残りMnとからなる組成
物(但し副成分がCo、Niだけの場合を除く)を
870℃(液相線)以上の高温で溶解した後、鋳造
して所定形状の成品となし、少くとも500℃以上
融点未満の温度で適当時間(例えば1分ないし
500時間)加熱して均質化処理し、ついで(A)の温
度より0.7℃/時間以上の速度で冷却するかある
いは、(B)その温度より0.7℃/時間以上の冷却速
度で急冷した後、さらに500℃以下300℃以上の適
当温度に適当時間(例えば1分ないし500時間)
再加熱し、0.7℃/時間より速い速度で冷却する
か、いずれかの熱処理方法により、これに六方格
子型結晶構造をもたせ−50℃〜+100℃における
線熱膨脹係数が−8×10-6〜+8×10-6の範囲内
にある高性能のインバー型合金を製造するもので
ある。
次に本発明合金の製造方法について詳細に説明
する。
本発明の合金を造るには、まず主成分として
Ge20〜33%、副成分としてCr、W、Vの何れか
0.01〜11%、Mo、Ti、Zr、Nb、Ta、Ag、Au、
Re、白金族元素の何れか0.01〜10%、Zn、Cd、
Al、Ga、In、Tl、Sn、Pbの何れか0.01〜9%、
Co、Ni、Cu、Si、As、Sb、Bi、Se、Te、希土
類元素の何れか0.01〜8%、Be、Mg、Ca、Bの
何れか0.01〜6%、C、P、Sの何れか0.01〜1
%の何れか1種または2種以上の全量0.01〜11%
と残部Mn(但し副成分がCo、Niだけの場合を除
く)との適当量を空気中もしくは非酸化性雰囲気
(例えば水素、窒素、アルゴンなど)中または真
空中において、適当な溶解炉中て少くとも870℃
(液相線)以上の温度に加熱し、充分撹拌しなが
ら溶解して、組成的に均一な溶融合金を造る。
次にこれを砂型や金型などの適当な鋳型に注入
して、所要の用途に適合する形状の鋳塊を得る
か、あるいはこの鋳塊より切断、研削、切削等の
適当な加工法によつて所要の形状の物品を切り出
す。このようにして得た成形体を六方構造の反強
磁性体とするために、該成形体に通常のアルゴン
中、その他の非酸化性雰囲気中あるいは真空中で
少くとも500℃以上融点未満の適当な温度に適当
時間(例えば1分以上500時間以下)加熱するこ
とよりなる均質化処理を施す。このようにして均
質化処理された合金を組成の如何に拘わらず500
℃以上融点未満の温度より0.7℃/時間以上の速
い速度で冷却すれば、ε相よりε1相への変態速度
が極めて遅いため、常温においてε相の反強磁性
のインバー型合金が得られる。
また、鋳造した成形体を500℃以上融点未満の
温度で均質化処理した後急冷した場合、急冷歪が
残る可能性があり、この場合500℃未満の温度で
再加熱する必要がある。この際、再加熱の保持時
間は、再加熱温度が450℃では50時間以下、400℃
では50時間以上120時間以下にする必要があり、
この時間は再加熱温度の降下とともに急に長くな
る。従つて調質処理の再加熱温度は500℃未満300
℃以上とした方がよい。以上の調質処理を施して
所望の製品が得られる。
次に本発明を実施例について説明する。
実施例 1
合金番号1(Ge27%、Cr1%、残部Mn)
原料としては99.9%の純度のGe、電解Crおよ
び99.8%純度の電解Mnを用いた。試料を造るに
は、まず全重量30gの原料をアルミナルツボ中
で、表面にアルゴンガスを吹きつけながらタンマ
ン炉により溶解した後、溶湯をよく撹拌し300℃
に加熱した砂型に鋳込んで直径3mmの丸棒を得
た。このとき、鋳造物の冷却速度を0.7℃/時間
以上に制御した。次にこれから長さ10cmの合金棒
と500mgの合金塊を切りとり、それぞれ熱膨脹お
よび帯磁率の測定用試料とした。最後にこれらを
850℃に10時間加熱後、100℃/時間および0.3
℃/時間の速度で冷却した焼鈍状態と850℃から
水中冷却した状態とについて実験を行つた。熱膨
脹係数は精密縦型膨脹計および横型熱膨脹計によ
り、帯磁率は磁気天秤により10KOeの磁場中で
アルゴン雰囲気中で求めた。測定結果は第1表に
示すとおりである。
The present invention relates to an Mn-Ge based multi-component hexagonal lattice type antiferromagnetic invar alloy with a small linear thermal expansion coefficient of -8x10 -6 to +8x10 -6 at -50°C to +100°C. Conventionally, many iron-based ferromagnetic face-centered cubic lattice alloys have been found as invar-type alloys. However, since these alloys have a large positive spontaneous bulk magnetostriction below their magnetic transformation point, their coefficient of thermal expansion is less than a fraction of that of general alloys, and they are ferromagnetic, so their applications are limited. There is. In particular, these invar-type alloys can be used, for example, in the head support of video tape recorders, the shadow mask of television receivers, the specimen support of electron microscopes, and the balance wheel of watches that are required to vibrate in a non-uniform magnetic field generated due to motorization. It is difficult to apply it to , escapes, pallets, etc., gravity pendulums, nuclear reactors, and various control equipment, and non-ferromagnetic invar type alloys are required for these applications. As a non-ferromagnetic invar type alloy, there is already a hexagonal lattice type Mn-Ge alloy invented by the present inventors, but although this alloy exhibits excellent invar type properties, it is hard and brittle. In general, grinding with a whetstone is used to form the material.
Therefore, there has been a demand for improvement in its workability. The present inventors have conducted numerous experiments and studies to improve the workability of the above Mn-Ge alloy without impairing the invar-type characteristics, and have found that Ge is the main component in a weight ratio of 20 to 33%, preferably 23 to 32%, 0.01 to 11% of any of Cr, W, or V as subcomponents, Mo, Ti,
Zr, Nb, Ta, Ag, Au, Re, platinum group elements (Pd,
Pt, Rh, Ir, Ru, Os) 0.01 to 10%,
Any of Zn, Cd, Al, Ga, In, Tl, Sn, Pb
0.01~9%, Co, Ni, Si, As, Sb, Bi, Se,
Te, rare earth elements (Sc, Y and lanthanum elements)
Any of 0.01 to 8%, Be, Mg, Ca, B
0.01 to 6%, 0.01 to 1% of C, P, and S, total amount of 0.01 to 11% of one or more of them, unavoidable impurities of 1% or less, and the balance Mn (however, the subcomponents are Co,
By applying a specific heat treatment to the alloy consisting of It was discovered that a hexagonal lattice type antiferromagnetic invar type alloy can be obtained. The Mn-Ge based multi-component alloy according to the present invention has approximately 500
The high temperature phase is the ε phase with a hexagonal structure, and the low temperature phase is the ε 1 phase with a face-centered square structure, and the invar characteristics are ε
It is exhibited in alloys with a phase structure. One of its features is that the rate of transformation to the ε 1 phase is much slower than that of the ε phase. The present inventors confirmed the special characteristics of the antiferromagnetic (non-ferromagnetic) invar type alloy as described above, and as a result of numerous studies on how to manufacture it, they found that it is possible to combine Mn with purity of 99% obtained by ordinary electrolysis. Has a purity of ~99.9%
By adding a third or fourth element selected from the above-mentioned subcomponents to an alloy consisting of Ge, an antiferromagnetic invar type alloy was successfully manufactured. As Ge20~33
%, any of Cr, W, or V as subcomponents 0.01 to 11
%, Mo, Ti, Zr, Nb, Ta, Ag, Au, Re, any of the platinum group elements 0.01-10%, Zn, Cd, Al,
0.01 to 9% of Ga, In, Tl, Sn, Pb, Co,
0.01-8% of any of Ni, Cu, Si, As, Sb, Bi, Se, Te, rare earth elements, 0.01-6% of any of Be, Mg, Ca, B, 0.01 of any of C, P, S A composition consisting of one or more of ~1% in a total amount of 0.01 to 11%, unavoidable impurities of 1% or less, and the remainder Mn (excluding cases where the only subsidiary components are Co and Ni).
After melting at a high temperature of 870°C (liquidus) or higher, it is cast to form a product in a specified shape, and then heated at a temperature of at least 500°C or higher and below the melting point for an appropriate period of time (for example, 1 minute or more).
500 hours)) and then subjected to homogenization treatment and then cooled at a rate of 0.7°C/hour or more from the temperature of (A), or (B) rapidly cooled from that temperature at a cooling rate of 0.7°C/hour or more, Furthermore, at an appropriate temperature of 500℃ or less and 300℃ or more for an appropriate time (for example, 1 minute to 500 hours)
By reheating and cooling at a rate faster than 0.7°C/hour, or by any heat treatment method, it is given a hexagonal lattice crystal structure and the linear thermal expansion coefficient at -50°C to +100°C is -8 × 10 -6 ~ The purpose is to produce a high-performance invar-type alloy within the range of +8×10 -6 . Next, the method for producing the alloy of the present invention will be explained in detail. In order to make the alloy of the present invention, first the main component is
Ge20~33%, any of Cr, W, or V as subcomponents
0.01~11%, Mo, Ti, Zr, Nb, Ta, Ag, Au,
Re, 0.01-10% of any platinum group element, Zn, Cd,
0.01 to 9% of Al, Ga, In, Tl, Sn, Pb,
Co, Ni, Cu, Si, As, Sb, Bi, Se, Te, any rare earth element 0.01-8%, Be, Mg, Ca, B any 0.01-6%, any C, P, S or 0.01~1
Total amount of any one or two or more of the following: 0.01 to 11%
and the remaining Mn (excluding when the subcomponents are only Co and Ni) in air or in a non-oxidizing atmosphere (e.g. hydrogen, nitrogen, argon, etc.) or in vacuum in a suitable melting furnace. at least 870℃
(liquidus line) or higher and melted with sufficient stirring to create a compositionally uniform molten alloy. Next, this is poured into a suitable mold such as a sand mold or a metal mold to obtain an ingot with a shape suitable for the desired use, or this ingot is processed by an appropriate processing method such as cutting, grinding, or cutting. Then cut out the desired shape. In order to make the thus obtained molded body an antiferromagnetic material with a hexagonal structure, the molded body must be heated at a temperature of at least 500°C or higher and lower than its melting point in normal argon, other non-oxidizing atmosphere, or vacuum. Homogenization treatment is performed by heating at a temperature for an appropriate time (for example, 1 minute or more and 500 hours or less). Alloys homogenized in this way, regardless of their composition, are
If it is cooled at a faster rate of 0.7°C/hour or more than the temperature above ℃ or below the melting point, an antiferromagnetic invar-type alloy in the ε phase can be obtained at room temperature because the transformation rate from the ε phase to the ε 1 phase is extremely slow. . Furthermore, if a cast compact is homogenized at a temperature of 500°C or higher and lower than its melting point and then rapidly cooled, quenching distortion may remain, and in this case, it is necessary to reheat the product at a temperature below 500°C. At this time, the holding time for reheating is 50 hours or less when the reheating temperature is 450℃, and 400℃
Then, it must be more than 50 hours and less than 120 hours.
This time increases rapidly as the reheating temperature decreases. Therefore, the reheating temperature for tempering treatment is less than 500℃.
It is better to keep it above ℃. A desired product can be obtained by performing the above tempering treatment. Next, the present invention will be explained with reference to examples. Example 1 Alloy No. 1 (27% Ge, 1% Cr, remainder Mn) As raw materials, 99.9% pure Ge, electrolytic Cr, and 99.8% pure electrolytic Mn were used. To make the sample, first, raw materials with a total weight of 30 g were melted in an alumina crucible in a Tammann furnace while blowing argon gas onto the surface, and the molten metal was stirred well and heated to 300℃.
A round bar with a diameter of 3 mm was obtained by casting into a sand mold heated to . At this time, the cooling rate of the casting was controlled to 0.7° C./hour or more. Next, an alloy rod with a length of 10 cm and an alloy ingot of 500 mg were cut out from this and used as samples for measuring thermal expansion and magnetic susceptibility. Finally these
After heating to 850℃ for 10 hours, 100℃/hour and 0.3
Experiments were conducted for an annealed state cooled at a rate of °C/hour and a state cooled in water from 850°C. The coefficient of thermal expansion was determined using a precision vertical dilatometer and a horizontal dilatometer, and the magnetic susceptibility was determined using a magnetic balance in a magnetic field of 10 KOe in an argon atmosphere. The measurement results are shown in Table 1.
【表】
第1表から明らかな如く、Ge27%、Cr1%を含
むMn合金は、ε相を得るための限界冷却速度
0.7/時間を越える速度で冷却すれば、その目的
とする小さな熱膨脹係数が得られることがわか
る。また帯磁率も4.5×10-5emu/g程度と小さ
く反強磁性である。第1図には第1表に示した
種々の状態における熱膨脹曲線が示してある。第
1図から、0.7℃/時間を越える速度で冷却され
た曲線AおよびBは広い温度範囲でインバー特性
を示すが、0.7℃/時間より遅い0.3/時間で冷却
された曲線Cはインバー特性を示さないことがわ
かる。
実施例 2
合金番号4(Ge27%、Mo2%、残部Mn)
原料は実施例1と同じ純度のGeおよびMnと
99.8%純度の電解Moを用いた。試料の製造法、
熱処理法および測定法は実施例1と同じである。
次に得られた結果を第2表に示す。なお帯磁率は
3.9×10-5emu/gである。[Table] As is clear from Table 1, the Mn alloy containing 27% Ge and 1% Cr has the critical cooling rate to obtain the ε phase.
It can be seen that the desired small coefficient of thermal expansion can be obtained by cooling at a rate exceeding 0.7/hour. It also has a small magnetic susceptibility of about 4.5×10 -5 emu/g and is antiferromagnetic. FIG. 1 shows thermal expansion curves under various conditions shown in Table 1. From Figure 1, curves A and B cooled at a rate exceeding 0.7°C/hour exhibit invar characteristics over a wide temperature range, while curve C cooled at a rate of 0.3/hour, which is slower than 0.7°C/hour, exhibits invar characteristics. You can see that it is not shown. Example 2 Alloy number 4 (Ge27%, Mo2%, balance Mn) The raw materials were Ge and Mn of the same purity as in Example 1.
Electrolytic Mo with a purity of 99.8% was used. sample manufacturing method;
The heat treatment method and measurement method are the same as in Example 1.
The results obtained are shown in Table 2. The magnetic susceptibility is
It is 3.9×10 −5 emu/g.
【表】
実施例 3
合金番号17(Ge27%、Zn1%、残部Mn)
原料は実施例1と同じ純度のGeおよびMnと
99.9%純度のZnを用いた。試料は実施例1の方法
で溶解した後、溶湯をよく撹拌し、15℃に冷却し
た鋳型に鋳込んで直径3mmの丸棒を得、これから
長さ10cm、直径2.5mmの合金棒と500mgの合金塊を
切りとり、チル鋳造状態のものとした。次にこれ
を400℃で110および130時間、450℃で45および55
時間それぞれ加熱して100℃/時間の速度で冷却
し、500未満の温度において再加熱処理した状態
のものとした。測定方法は前記実施例1と同様で
ある。得られた成形体の特性は第3表に示すとお
りである。[Table] Example 3 Alloy number 17 (27% Ge, 1% Zn, balance Mn) The raw materials were Ge and Mn of the same purity as in Example 1.
Zn with a purity of 99.9% was used. After the sample was melted using the method of Example 1, the molten metal was thoroughly stirred and poured into a mold cooled to 15°C to obtain a round bar with a diameter of 3 mm. From this, an alloy bar with a length of 10 cm and a diameter of 2.5 mm and a 500 mg The alloy ingot was cut out and made into a chill cast state. This was then heated at 400°C for 110 and 130 hours, and at 450°C for 45 and 55 hours.
It was heated for each time and cooled at a rate of 100° C./hour to obtain a reheated state at a temperature of less than 500° C. The measurement method was the same as in Example 1 above. The properties of the obtained molded product are shown in Table 3.
【表】
第3表から27%Ge−1%Zn−Mn合金は500℃
未満の温度に再加熱する場合、そのインバー特性
を保持するためには加熱温度によつて加熱時間に
おのずから限度があることがわかる。また、帯磁
率は400℃で110時間および450℃で45時間再加熱
した合金においてほとんど同じ値の2.9×
10-5emu/gで、これを400℃で130時間および
450℃で55時間再加熱した場合には18×
10-2emu/gとなる。すなわち前者は反強磁性で
あるが、後者は強いフエリ磁性である。
第2図には第3表に示した種々の加熱状態のう
ち400℃で110時間および130時間再時間したもの
の膨脹曲線をチル鋳造状態のものと対比して示し
てある。第2図において、曲線Fに示すとおり
400℃で130時間加熱したものはインバー特性を示
さないが、その他の処理をした状態のもの(曲線
DおよびE)では優れたインバー特性が現われて
いることが認められる。
実施例 4
合金番号56(Ge27%、Si1%、Al1%、残部Mn)
原料は実施例1と同じ純度のGeおよびMnと、
99.9%純度のSiおよびAlを用いた。試料は実施例
1および実施例3の方法によつて製造し、熱処理
を施した。測定法は前記実施例1と同様である。
得られた成形体の特性は第4表に示すとおりであ
る。なお帯磁率は3.6×10-5emu/gである。[Table] From Table 3, 27%Ge-1%Zn-Mn alloy is heated to 500℃.
It can be seen that when reheating to a temperature lower than that, there is a natural limit to the heating time depending on the heating temperature in order to maintain the Invar characteristics. In addition, the magnetic susceptibility was 2.9
10 -5 emu/g at 400℃ for 130 hours and
18× when reheated at 450°C for 55 hours
10 -2 emu/g. That is, the former is antiferromagnetic, while the latter is strongly ferrimagnetic. FIG. 2 shows the expansion curves of the various heating conditions shown in Table 3 after reheating at 400 DEG C. for 110 hours and 130 hours, in comparison with the chill casting condition. As shown in curve F in Figure 2,
It can be seen that those heated at 400° C. for 130 hours do not exhibit Invar properties, but those subjected to other treatments (curves D and E) exhibit excellent Invar properties. Example 4 Alloy number 56 (27% Ge, 1% Si, 1% Al, balance Mn) The raw materials are Ge and Mn of the same purity as in Example 1,
99.9% pure Si and Al were used. Samples were manufactured by the methods of Examples 1 and 3 and were heat treated. The measurement method was the same as in Example 1 above.
The properties of the obtained molded product are shown in Table 4. The magnetic susceptibility is 3.6×10 −5 emu/g.
【表】
実施例 5
Geを27%と一定にしたMn−27%Ge二元合金
に種々の副成分を加えた場合の線熱膨脹の測定結
果を第3図ないし第8図に示す。この場合、原料
は実施例1と同じ純度のGe、Mn、99.8%純度の
Cr、W、V、Mo、Ti、Zr、Nb、Taと99.9%純
度のAg、Au、Re、白金族元素、Zn、Cd、Al、
Ga、In、Tl、Sn、Pb、Cu、Si、As、Sb、Bi、
Se、Te、希土類元素、Be、Mg、Ca、B、C、
PおよびSを用い、実施例1と同じ方法によつて
試料を製造した。次にこれを850℃で10時間加熱
した後100℃/時間の速度で徐冷して焼鈍状態の
ものとした。測定方法は前記実施例1に記載した
とおりである。第3図ないし第8図には−50℃〜
+100℃における熱膨脹係数α(10-6)を添加元素
濃度(%)に対して描いてある。各図に示すよう
に線熱膨脹係数αは広い組成範囲において−8×
10-6〜+8×10-6の値をとることがわかつた。し
かしながら、特許請求の範囲に記載した上限値
(図中の点線)を越えると線熱膨脹係数は急激に
大きくなり好ましくないことが確められた。
実施例 6
次に第9図〜第35図には線熱膨脹の測定例と
して、副成分のうちCr、W、V、Al、In、Coお
よびSiを1%に固定した場合のMn−Ge基多元合
金の線熱膨脹係数が−8×10-6〜+8×10-6を示
す範囲を描いてある。この場合の原料、製造方
法、熱処理方法、測定方法は実施例1と同様であ
る。各図にみるように線熱膨脹係数は種々の元素
の組み合わせにおいて、広い組成範囲で優れたイ
ンバー領域を形成することがわかつた。
最後に本発明合金の代表的な特性を第5表に示
す。この場合、原料は実施例1と同じ純度のGe、
Mn、99.8℃の純度のCo、Ni、Cr、W、V、Mo、
Ti、Zr、Nb、Taと99.9%純度のAg、Au、Re、
白金族元素、Zn、Cd、Al、Ga、In、Tl、Sn、
Pb、Cu、Si、As、Sb、Bi、Se、Te、希土類元
素、Bi、Mg、Ca、B、C、PおよびSを用い、
実施例1と同じ方法によつて試料を製造した。次
にこれを850℃で10時間加熱した後100℃/時間の
速度で冷却して焼鈍状態のものとした。測定方法
は前記実施例1に記載したとおりで、硬度はビツ
カース硬度計により、切削性は通常の施盤により
調べた。[Table] Example 5 Figures 3 to 8 show the measurement results of linear thermal expansion when various subcomponents were added to a Mn-27%Ge binary alloy with Ge constant at 27%. In this case, the raw materials are Ge and Mn with the same purity as in Example 1, and 99.8% purity.
Cr, W, V, Mo, Ti, Zr, Nb, Ta and 99.9% purity Ag, Au, Re, platinum group elements, Zn, Cd, Al,
Ga, In, Tl, Sn, Pb, Cu, Si, As, Sb, Bi,
Se, Te, rare earth elements, Be, Mg, Ca, B, C,
A sample was produced using P and S in the same manner as in Example 1. Next, this was heated at 850°C for 10 hours and then gradually cooled at a rate of 100°C/hour to obtain an annealed state. The measurement method was as described in Example 1 above. Figures 3 to 8 show -50℃~
The coefficient of thermal expansion α (10 −6 ) at +100°C is plotted against the concentration of added elements (%). As shown in each figure, the coefficient of linear thermal expansion α is -8×
It was found that it takes a value of 10 -6 to +8×10 -6 . However, it has been confirmed that when the upper limit (dotted line in the figure) described in the claims is exceeded, the coefficient of linear thermal expansion suddenly increases, which is not preferable. Example 6 Next, FIGS. 9 to 35 show examples of measuring linear thermal expansion of Mn-Ge groups when Cr, W, V, Al, In, Co, and Si among the subcomponents are fixed at 1%. A range in which the linear thermal expansion coefficient of the multi-component alloy is −8×10 −6 to +8×10 −6 is depicted. The raw materials, manufacturing method, heat treatment method, and measurement method in this case are the same as in Example 1. As shown in each figure, it was found that the linear thermal expansion coefficient formed an excellent invar region over a wide composition range in various combinations of elements. Finally, typical properties of the alloy of the present invention are shown in Table 5. In this case, the raw materials are Ge of the same purity as in Example 1,
Mn, 99.8℃ purity Co, Ni, Cr, W, V, Mo,
Ti, Zr, Nb, Ta and 99.9% purity Ag, Au, Re,
Platinum group elements, Zn, Cd, Al, Ga, In, Tl, Sn,
Using Pb, Cu, Si, As, Sb, Bi, Se, Te, rare earth elements, Bi, Mg, Ca, B, C, P and S,
Samples were manufactured by the same method as in Example 1. Next, this was heated at 850°C for 10 hours and then cooled at a rate of 100°C/hour to obtain an annealed state. The measurement method was as described in Example 1 above, and the hardness was measured using a Vickers hardness meter, and the machinability was measured using a normal lathe.
【表】【table】
【表】【table】
【表】
註:◎非常に良好、○良好
第5表から明らかなように本発明合金は広い組
成範囲および温度範囲で線熱膨脹係数が小さく、
従来の非強磁性インバー合金に比較して、はるか
に優つていることがわかる。帯磁率は高磁場中に
おいても2.5〜5.9×10-5emu/gの程度の値であ
り、磁性は無視し得る程小さい。さらに多元合金
としたことにより硬度が減少し、これに伴ない切
削性が良好になつていることがわかる。
要するに本発明合金は、主成分としてGe20〜
33%、副成分としてCr、W、Vの何れか0.01〜11
%、Mo、Ti、Zr、Nb、Ta、Ag、Au、Re、白
金族元素の何れか0.01〜10%、Zn、Cd、Al、
Ga、In、Tl、Sn、Pbの何れか0.01〜9%、Co、
Ni、Cu、Si、As、Sb、Bi、Se、Te、希土類元
素の何れか0.01〜8%、Be、Mg、Ca、Bの何れ
か0.01〜6%、C、P、Sの何れか0.01〜1%の
何れか1種または2種以上の全量0.01〜11%と不
可避の不純物1%以下と残部Mn(但し副成分が
Co、Niだけの場合を除く)とからなる多元合金
で、簡易な熱処理を施すことによつて六方格子型
の反(非)強磁性となり、−8×10-6〜+8×
10-6の範囲の任意の線熱膨脹係数を有する優れた
非強磁性インバー型合金である。従つて本発明は
精密機器或は制御機器の部材として非常に好適で
ある。
最後に本発明合金において、Ge量を20〜33%、
Cr、W、Vの何れか0.01〜11%、Mo、Ti、Zr、
Nb、Ta、Ag、Au、Re、白金族元素の何れか
0.01〜10%、Zn、Cd、Al、Ga、In、Tl、Sn、
Pbの何れか0.01〜9%、Co、Ni、Cu、Si、As、
Sb、Bi、Se、希土類元素の何れか0.01〜8%、
Be、Mg、Ca、Bの何れか0.01〜6%、C、P、
Sの何れか0.01〜1%(但し副成分全量0.01〜11
%)と限定した理由は、Ge量が33%を越えるか
20%未満および副成分のCr、W、Vが11%を越
え、Mo、Ti、Zr、Nb、Ta、Ag、Au、Re、白
金族元素が10%を越え、Zn、Cd、Al、Ga、In、
Tl、Sn、Pbが9%を越え、Co、Ni、Cu、Si、
As、Sb、Bi、Se、Te希土類元素が8%を越え、
Be、Mg、Ca、Bが6%を越え、C、P、Sが
1%を越えると如何なる処理によつても本発明合
金が必要とする反強磁性の六方構造が得られなく
なり、また線熱膨脹係数が±8×10-6を越えるか
らである。また副成分として添加元素が0.01%以
上含まれると、切削性が著しく改善されるが、
0.01%未満では切削性が何等改善されていないの
で、その下限を0.01%以上と限定した。[Table] Note: ◎Very good, ○Good As is clear from Table 5, the present alloy has a small coefficient of linear thermal expansion over a wide composition and temperature range;
It can be seen that it is far superior to conventional non-ferromagnetic Invar alloys. The magnetic susceptibility is on the order of 2.5 to 5.9×10 −5 emu/g even in a high magnetic field, and the magnetism is so small that it can be ignored. Furthermore, it can be seen that by using a multi-component alloy, the hardness is reduced and the machinability is improved accordingly. In short, the alloy of the present invention has Ge20~
33%, any of Cr, W, or V as subcomponents 0.01 to 11
%, Mo, Ti, Zr, Nb, Ta, Ag, Au, Re, any of the platinum group elements 0.01-10%, Zn, Cd, Al,
0.01 to 9% of Ga, In, Tl, Sn, Pb, Co,
0.01-8% of any of Ni, Cu, Si, As, Sb, Bi, Se, Te, rare earth elements, 0.01-6% of any of Be, Mg, Ca, B, 0.01 of any of C, P, S ~1% of the total amount of any one or two or more types of 0.01~11%, unavoidable impurities of 1% or less, and the balance Mn (however, the subcomponent is
It is a multi-component alloy consisting of (excluding cases where only Co and Ni are used), and by simple heat treatment, it becomes hexagonal lattice type anti(non)ferromagnetic, and has a magnetic field of -8×10 -6 to +8×
It is an excellent non-ferromagnetic invar type alloy with a coefficient of linear thermal expansion anywhere in the range of 10-6 . Therefore, the present invention is very suitable as a member of precision equipment or control equipment. Finally, in the alloy of the present invention, the amount of Ge is 20 to 33%,
0.01 to 11% of Cr, W, V, Mo, Ti, Zr,
Nb, Ta, Ag, Au, Re, any platinum group element
0.01~10%, Zn, Cd, Al, Ga, In, Tl, Sn,
Any 0.01 to 9% of Pb, Co, Ni, Cu, Si, As,
0.01 to 8% of Sb, Bi, Se, or rare earth elements,
0.01-6% of Be, Mg, Ca, B, C, P,
0.01 to 1% of any S (however, the total amount of subcomponents is 0.01 to 11
The reason for limiting it to %) is whether the Ge amount exceeds 33%.
Less than 20% and subcomponents Cr, W, V more than 11%, Mo, Ti, Zr, Nb, Ta, Ag, Au, Re, platinum group elements more than 10%, Zn, Cd, Al, Ga ,In,
Tl, Sn, Pb exceeds 9%, Co, Ni, Cu, Si,
As, Sb, Bi, Se, Te rare earth elements exceed 8%,
If Be, Mg, Ca, and B exceed 6% and C, P, and S exceed 1%, the antiferromagnetic hexagonal structure required by the alloy of the present invention cannot be obtained no matter what treatment is performed, and the wire This is because the coefficient of thermal expansion exceeds ±8×10 -6 . Additionally, if 0.01% or more of additional elements are included as subcomponents, machinability will be significantly improved;
Since machinability is not improved at all if it is less than 0.01%, the lower limit is set to 0.01% or more.
第1図は27%Ge−1%Cr−Mn合金に種々の熱
処理を施した状態における線熱膨脹係数の温度変
化を示す特性曲線図、第2図は27%Ge−1%Zn
−Mn合金のチル鋳造状態とこれを400℃で110お
よび130時間加熱したときの線熱膨脹係数の温度
変化を示す特性曲線図、第3図ないし第8図は
Mn−27%Ge合金に種々の副成分を添加した場合
の−50℃〜+100℃における線熱膨脹係数αの温
度変化を示す特性曲線図、第9図ないし第35図
はMn−27%Ge合金に第3元素を1%加え固定
し、さらに第4元素を加えた場合の多元合金が線
熱膨脹係数α=+8×10-6以下となる範囲を示す
特性曲線図である。
Figure 1 is a characteristic curve diagram showing temperature changes in linear thermal expansion coefficient of 27%Ge-1%Cr-Mn alloy subjected to various heat treatments.
-Characteristic curve diagrams showing temperature changes in linear thermal expansion coefficient when Mn alloy is chilled cast and heated at 400℃ for 110 and 130 hours, Figures 3 to 8 are
Characteristic curve diagrams showing temperature changes in linear thermal expansion coefficient α from -50℃ to +100℃ when various subcomponents are added to Mn-27%Ge alloy, Figures 9 to 35 are Mn-27%Ge alloy It is a characteristic curve diagram showing a range in which a multi-component alloy has a coefficient of linear thermal expansion α=+8×10 −6 or less when 1% of a third element is added and fixed, and a fourth element is further added.
Claims (1)
分としてCr、W、Vの何れか0.01〜11%、Mo、
Ti、Zr、Nb、Ta、Ag、Au、Re、白金族元素
の何れか0.01〜10%、Zn、Cd、Al、Ga、In、
Tl、Sn、Pbの何れか0.01〜9%、Cu、Si、As、
Sb、Bi、Se、Te、希土類元素の何れか0.01〜8
%、Be、Mg、Ca、Bの何れか0.01〜6%、C、
P、Sの何れか0.01〜1%の何れか1種あるいは
2種以上の副成分全量0.01〜11%と不可避の不純
物1%以下と残部Mnとからなり、−50℃〜+100
℃における線熱膨脹係数が−8×10-6〜+8×
10-6の範囲であることを特徴とする六方格子型反
強磁性インバー型合金。 2 重量比にて主成分としてGe20〜33%、副成
分としてCo、Niの何れか0.01〜8%を含み、更
に、副成分としてCr、W、Vの何れか0.01〜11
%、Mo、Ti、Zr、Nb、Ta、Ag、Au、Re、白
金族元素の何れか0.01〜10%、Zn、Cd、Al、
Ga、In、Tl、Sn、Pbの何れか0.01〜9%、Cu、
Si、As、Sb、Bi、Se、Te、希土類元素の何れか
0.01〜8%、Be、Mg、Ca、Bの何れか0.01〜6
%、C、P、Sの何れか0.01〜1%の何れか1種
あるいは2種以上の副成分全量0.01〜11%と不可
避の不純物1%以下と残部Mnとからなり、−50
℃〜+100℃における線熱膨脹係数が−8×10-6
〜+8×10-6の範囲であることを特徴とする特許
請求の範囲第1項記載の六方格子型反強磁性イン
バー型合金。 3 重量比にて主成分としてGe20〜33%、副成
分としてCr、W、Vの何れか0.01〜11%、Mo、
Ti、Zr、Nb、Ta、Ag、Au、Re、白金族元素
の何れか0.01〜10%、Zn、Cd、Al、Ga、In、
Tl、Sn、Pbの何れか0.01〜9%、Cu、Si、As、
Sb、Bi、Se、Te、希土類元素の何れか0.01〜8
%、Be、Mg、Ca、Bの何れか0.01〜6%、C、
P、Sの何れか0.01〜1%の何れか1種あるいは
2種以上の副成分全量0.01〜11%と不可避の不純
物1%以下と残部Mnとからなる組成物を870℃
以上の高温で溶解し、鋳造し、所定形状の成形品
とし、500℃以上融点未満の温度で1分ないし500
時間の範囲の適当時間加熱して均質化処理を施し
た後、500℃以上融点未満の温度より0.7℃/時間
以上の速度で冷却して六方格子型結晶相となし、
−8×10-6〜+8×10-6の範囲の線熱膨脹係数を
発揮せしめることを特徴とする六方格子型反強磁
性インバー型合金の製造方法。 4 重量比にて主成分としてGe20〜33%、副成
分としてCr、W、Vの何れか0.01〜11%、Mo、
Ti、Zr、Nb、Ta、Ag、Au、Re、白金族元素
の何れか0.01〜10%、Zn、Cd、Al、Ga、In、
Tl、Sn、Pbの何れか0.01〜9%、Cu、Si、As、
Sb、Bi、Se、Te、希土類元素の何れか0.01〜8
%、Be、Mg、Ca、Bの何れか0.01〜6%、C、
P、Sの何れか0.01〜1%の何れか1種または2
種以上の副成分全量0.01〜11%と不可避の不純物
1%以下と残部Mnとからなる組成物を870℃以
上の高温で溶解し、鋳造し、所定形状の成形品と
し、500℃以上融点未満の温度で1分ないし500時
間の範囲の適当時間加熱して均質化処理を施した
後、500℃以上融点未満の温度より0.7℃/時間以
上の速度で冷却する工程と、得られた成形物を更
に300℃以上500℃未満の温度で1分ないし500時
間再加熱し、0.7℃/時間以上の速度で冷却して
六方格子型結晶相となし、−8×10-6〜+8×
10-6の範囲の線熱膨脹係数を発揮せしめることを
特徴とする六方格子型反強磁性インバー型合金の
製造方法。[Claims] 1 Ge as the main component 20 to 33% by weight, any of Cr, W, or V as subcomponents 0.01 to 11%, Mo,
Ti, Zr, Nb, Ta, Ag, Au, Re, 0.01-10% of any platinum group element, Zn, Cd, Al, Ga, In,
0.01 to 9% of Tl, Sn, Pb, Cu, Si, As,
Any of Sb, Bi, Se, Te, or rare earth elements 0.01 to 8
%, Be, Mg, Ca, 0.01 to 6% of any of B, C,
Consisting of 0.01 to 1% of either P or S, the total amount of one or more subcomponents of 0.01 to 11%, unavoidable impurities of 1% or less, and the balance Mn, -50℃ to +100℃
Linear thermal expansion coefficient at °C is -8×10 -6 ~+8×
A hexagonal lattice type antiferromagnetic invar alloy characterized by a magnetic flux in the range of 10 -6 . 2 Contains 20 to 33% of Ge as the main component, 0.01 to 8% of Co or Ni as a subcomponent, and further 0.01 to 11% of any of Cr, W, or V as a subcomponent by weight
%, Mo, Ti, Zr, Nb, Ta, Ag, Au, Re, any of the platinum group elements 0.01-10%, Zn, Cd, Al,
0.01 to 9% of Ga, In, Tl, Sn, Pb, Cu,
Any of Si, As, Sb, Bi, Se, Te, rare earth elements
0.01~8%, any of Be, Mg, Ca, B 0.01~6
%, consisting of 0.01 to 1% of any one of C, P, and S, the total amount of any one or two or more subcomponents of 0.01 to 11%, unavoidable impurities of 1% or less, and the balance Mn, -50
Linear thermal expansion coefficient between ℃ and +100℃ is -8×10 -6
The hexagonal lattice type antiferromagnetic invar alloy according to claim 1, characterized in that the hexagonal lattice type antiferromagnetic invar type alloy has a magnetic flux in the range of ~+8×10 -6 . 3 Ge 20-33% as main component by weight, 0.01-11% of any of Cr, W, V as subcomponents, Mo,
Ti, Zr, Nb, Ta, Ag, Au, Re, 0.01-10% of any platinum group element, Zn, Cd, Al, Ga, In,
0.01 to 9% of Tl, Sn, Pb, Cu, Si, As,
Any of Sb, Bi, Se, Te, or rare earth elements 0.01 to 8
%, Be, Mg, Ca, 0.01 to 6% of any of B, C,
A composition consisting of 0.01 to 1% of either P or S in a total amount of 0.01 to 11% of one or more of the subcomponents, unavoidable impurities of 1% or less, and the balance Mn was heated at 870°C.
Melt at a high temperature of 500°C or higher, cast it to form a molded product in a specified shape, and heat it for 1 minute to 500°C at a temperature of 500°C or higher and lower than the melting point.
After applying homogenization treatment by heating for an appropriate period of time, cooling from a temperature of 500°C or more and less than the melting point at a rate of 0.7°C/hour or more to form a hexagonal lattice crystal phase,
A method for producing a hexagonal lattice type antiferromagnetic invar alloy, which exhibits a linear thermal expansion coefficient in the range of -8×10 -6 to +8×10 -6 . 4 Ge20 to 33% as main component by weight, 0.01 to 11% of any of Cr, W, or V as subcomponents, Mo,
Ti, Zr, Nb, Ta, Ag, Au, Re, 0.01-10% of any platinum group element, Zn, Cd, Al, Ga, In,
0.01 to 9% of Tl, Sn, Pb, Cu, Si, As,
Any of Sb, Bi, Se, Te, or rare earth elements 0.01 to 8
%, Be, Mg, Ca, 0.01 to 6% of any of B, C,
0.01 to 1% of either P or S, one or two
A composition consisting of a total amount of 0.01 to 11% of the total amount of subcomponents above, 1% or less of unavoidable impurities, and the balance Mn is melted and cast at a high temperature of 870°C or higher to form a molded product of a specified shape, and the melting point is 500°C or higher and below the melting point. A step of homogenizing the product by heating it at a temperature of 1 minute to 500 hours for an appropriate period of time, and then cooling it at a rate of 0.7 °C/hour or more from a temperature of 500 °C or more and below the melting point, and the obtained molded product. is further reheated at a temperature of 300°C or more and less than 500°C for 1 minute to 500 hours, and cooled at a rate of 0.7°C/hour or more to form a hexagonal lattice crystal phase, -8×10 -6 to +8×
A method for producing a hexagonal lattice antiferromagnetic invar alloy characterized by exhibiting a linear thermal expansion coefficient in the range of 10 -6 .
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3787681A JPS57155341A (en) | 1981-03-18 | 1981-03-18 | Antiferromagnetic invar type alloy having hexagonal lattice and method for producing the same |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3787681A JPS57155341A (en) | 1981-03-18 | 1981-03-18 | Antiferromagnetic invar type alloy having hexagonal lattice and method for producing the same |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP9543089A Division JPH01301833A (en) | 1989-04-17 | 1989-04-17 | Hexagonal lattice antiferromagnetic invar alloy and its manufacturing method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS57155341A JPS57155341A (en) | 1982-09-25 |
| JPH0258334B2 true JPH0258334B2 (en) | 1990-12-07 |
Family
ID=12509728
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP3787681A Granted JPS57155341A (en) | 1981-03-18 | 1981-03-18 | Antiferromagnetic invar type alloy having hexagonal lattice and method for producing the same |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS57155341A (en) |
-
1981
- 1981-03-18 JP JP3787681A patent/JPS57155341A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS57155341A (en) | 1982-09-25 |
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