JPH0798210B2 - Amorphous alloy coated body and method for producing the same - Google Patents
Amorphous alloy coated body and method for producing the sameInfo
- Publication number
- JPH0798210B2 JPH0798210B2 JP28621886A JP28621886A JPH0798210B2 JP H0798210 B2 JPH0798210 B2 JP H0798210B2 JP 28621886 A JP28621886 A JP 28621886A JP 28621886 A JP28621886 A JP 28621886A JP H0798210 B2 JPH0798210 B2 JP H0798210B2
- Authority
- JP
- Japan
- Prior art keywords
- amorphous alloy
- core material
- coated body
- container
- body according
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 229910000808 amorphous metal alloy Inorganic materials 0.000 title claims description 104
- 238000004519 manufacturing process Methods 0.000 title claims description 13
- 239000011162 core material Substances 0.000 claims description 55
- 239000004033 plastic Substances 0.000 claims description 25
- 239000011247 coating layer Substances 0.000 claims description 22
- 238000001125 extrusion Methods 0.000 claims description 18
- 229910045601 alloy Inorganic materials 0.000 claims description 17
- 239000000956 alloy Substances 0.000 claims description 17
- 238000002425 crystallisation Methods 0.000 claims description 13
- 230000008025 crystallization Effects 0.000 claims description 13
- 238000000465 moulding Methods 0.000 claims description 12
- 230000007704 transition Effects 0.000 claims description 10
- 239000002184 metal Substances 0.000 claims description 8
- 238000010438 heat treatment Methods 0.000 claims description 6
- 238000011049 filling Methods 0.000 claims description 5
- 230000009467 reduction Effects 0.000 claims description 5
- 238000003754 machining Methods 0.000 claims description 3
- 239000011261 inert gas Substances 0.000 claims 1
- 238000000034 method Methods 0.000 description 30
- 239000000463 material Substances 0.000 description 16
- 238000012545 processing Methods 0.000 description 11
- 238000005304 joining Methods 0.000 description 7
- 239000000843 powder Substances 0.000 description 7
- 230000000052 comparative effect Effects 0.000 description 6
- 239000011248 coating agent Substances 0.000 description 5
- 238000000576 coating method Methods 0.000 description 5
- 230000008569 process Effects 0.000 description 5
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical class [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- 239000005300 metallic glass Substances 0.000 description 4
- 238000003466 welding Methods 0.000 description 4
- 239000000853 adhesive Substances 0.000 description 3
- 230000001070 adhesive effect Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 239000007788 liquid Substances 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical class N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 229910052786 argon Inorganic materials 0.000 description 2
- 239000000919 ceramic Substances 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 239000013078 crystal Substances 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 238000001514 detection method Methods 0.000 description 2
- 230000005284 excitation Effects 0.000 description 2
- 230000020169 heat generation Effects 0.000 description 2
- 238000007747 plating Methods 0.000 description 2
- 238000010791 quenching Methods 0.000 description 2
- 230000000171 quenching effect Effects 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- CDBYLPFSWZWCQE-UHFFFAOYSA-L Sodium Carbonate Chemical compound [Na+].[Na+].[O-]C([O-])=O CDBYLPFSWZWCQE-UHFFFAOYSA-L 0.000 description 1
- 238000002441 X-ray diffraction Methods 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 238000005219 brazing Methods 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 239000007772 electrode material Substances 0.000 description 1
- 238000005868 electrolysis reaction Methods 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 239000010408 film Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 238000001192 hot extrusion Methods 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 239000012770 industrial material Substances 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 239000000696 magnetic material Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000001000 micrograph Methods 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 229910000889 permalloy Inorganic materials 0.000 description 1
- 230000035699 permeability Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- -1 ribbons Substances 0.000 description 1
- 102220259718 rs34120878 Human genes 0.000 description 1
- 102200082816 rs34868397 Human genes 0.000 description 1
- 238000005070 sampling Methods 0.000 description 1
- 230000035945 sensitivity Effects 0.000 description 1
- 238000010008 shearing Methods 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 238000004544 sputter deposition Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 238000004781 supercooling Methods 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
- 238000007740 vapor deposition Methods 0.000 description 1
Landscapes
- Extrusion Of Metal (AREA)
- Metal Extraction Processes (AREA)
Description
【発明の詳細な説明】 [産業上の利用分野] 本発明は非晶質合金被覆体を芯材の表面に塑性加工によ
って形成する非晶質合金被覆体およびその製造方法に関
する。TECHNICAL FIELD The present invention relates to an amorphous alloy coated body in which an amorphous alloy coated body is formed on the surface of a core material by plastic working, and a method for producing the same.
[従来の技術] 非晶質合金は、一般にアモルファス合金とも呼ばれ、金
属のように結晶構造を有せず原子配列の周期性がなく無
秩序の状態にある。そのため、X線回折試験において
も、金属のようにはっきりしたピークを示さず、その原
子配列は液体状態に近いものである。[Prior Art] An amorphous alloy is generally called an amorphous alloy, and does not have a crystal structure like a metal and has no atomic arrangement periodicity and is in a disordered state. Therefore, even in the X-ray diffraction test, it does not show a clear peak like a metal, and its atomic arrangement is close to that in a liquid state.
非晶質合金は、機械的強度が大きく、熱膨張係数、放射
線損傷が小さく、化学的耐食性および耐摩耗性に優れて
いる。また、磁性体としての非晶質材は、非晶質合金に
見られるような結晶異方性、格子欠陥および粒界などの
組織不均一性がないために、保磁力、非透磁率に極めて
優れた特性を示す。このため非晶質合金は、電磁コア、
各種センサ、電磁クラッチ、など極めて広範囲の用途が
期待される。Amorphous alloys have high mechanical strength, low coefficient of thermal expansion, low radiation damage, and excellent chemical corrosion resistance and wear resistance. In addition, since an amorphous material as a magnetic material does not have the structure anisotropy such as crystal anisotropy, lattice defects and grain boundaries as seen in an amorphous alloy, the coercive force and the non-permeability are extremely high. It exhibits excellent properties. Therefore, the amorphous alloy has an electromagnetic core,
A wide range of applications such as various sensors and electromagnetic clutches are expected.
非晶質合金を得る方法としては、真空蒸着法、スパッタ
法、メツキ法などがあるが、これらはいずれも得られる
合金組織に制限があり、非晶質合金の薄膜を作るには適
するものの、大量の非晶質合金を得ることは出来ない。
その他に大量にしかも大きな非晶質合金を得る方法とし
ては、液体急冷法があり、この方法は溶融した金属・合
金を急速に冷却して過冷させその構造を凍結させてアモ
ルファスとするものである。As a method for obtaining an amorphous alloy, there are a vacuum vapor deposition method, a sputtering method, a plating method, etc., but these are all limited in the alloy structure that can be obtained, and although suitable for forming a thin film of an amorphous alloy, It is not possible to obtain a large amount of amorphous alloy.
In addition, as a method for obtaining a large amount of large amorphous alloy, there is a liquid quenching method, which is a method of rapidly cooling and supercooling a molten metal or alloy to freeze its structure to make it amorphous. is there.
かくして得られた非晶質合金を利用するに際しては、次
のような問題点がある。第1に、液体急冷法で得られる
非晶質合金であっても、せいぜい0.01cmの厚さの繊維
状、リボン状またはフレーク状のものしか得られず、こ
れ以上の厚さのものは冷却速度の関係から得ることが困
難であること、第2に、これら非晶質合金が結晶化を起
こす結晶化温度が比較的低く、非晶質合金の繊維、リボ
ン、粉末等から大きな成形体を得たりあるいは他の結晶
質の基材に接合するための加熱や機械加工によって、す
ぐに結晶化してしまうことがある このように非晶質合金の場合、通常の焼結法や溶接法
は、アモルファスの特徴であるランダムな原子配列を、
熱によって結晶化させてしまうため、繊維状、リボン状
またはフレーク状の非晶質合金から肉厚のあるものを製
作するための種々の提案がなされている。これら提案に
は、レーザ法(特開昭59−101287号公報)、接合材使用
法(特開昭60−102706号公報)、衝撃法(特開昭59−74
33号公報)、高温高圧法(特開昭60−24346号公報)お
よび高温押し出し法(H.H.Liebermann,Materials Scien
ce and Engineering,46(1980)241−248)がある。前
記方法の内レーザ法は、薄板枚数が接合限度であり、部
分接合となるため接合部分が弱く、整合材使用法は接合
部が弱く磁気特性も悪いといった欠点がある。また、衝
撃法は高価な爆薬を使用するためコストが高く、高温高
圧法は、試料寸法に限度があるといった問題点がある。
一方、工業材料の非晶質合金の整合も前記のレーザ法、
接合材使用法、衝撃法によって可能であるが、いずれも
接合部の強度不足の問題がある。The use of the amorphous alloy thus obtained has the following problems. First, even amorphous alloys obtained by the liquid quenching method can only obtain fibrous, ribbon-like or flake-like substances with a thickness of 0.01 cm at most, and those with a thickness greater than this can be cooled. Secondly, it is difficult to obtain it due to the relation of speed. Secondly, the crystallization temperature at which these amorphous alloys are crystallized is relatively low, and a large compact is formed from fibers, ribbons, powders, etc. of the amorphous alloy. It may be crystallized immediately by heating or machining to obtain or bond it to another crystalline base material.In this way, in the case of an amorphous alloy, the usual sintering method or welding method is Random atomic arrangement that is characteristic of amorphous,
Since it is crystallized by heat, various proposals have been made for producing a thick alloy from a fibrous, ribbon-shaped or flake-shaped amorphous alloy. These proposals include a laser method (JP-A-59-101287), a method of using a bonding material (JP-A-60-102706), and an impact method (JP-A-59-74).
33), high temperature and high pressure method (JP-A-60-24346) and high temperature extrusion method (HHLiebermann, Materials Scien)
ce and Engineering, 46 (1980) 241-248). Among the above methods, the laser method has a drawback that the number of thin plates is the joining limit and the joining is weak because the joining is partial, and the method of using the matching material has the drawback that the joining portion is weak and the magnetic characteristics are also poor. Further, the impact method is expensive because it uses an expensive explosive, and the high temperature and high pressure method has a problem that the sample size is limited.
On the other hand, the matching of amorphous alloys of industrial materials is also performed by the laser method,
Although it is possible to use the bonding material and the impact method, both have a problem of insufficient strength of the bonding portion.
ところで、非晶質合金の磁気的特性を利用した機器とし
て、トルクセンサがある。トルクセンサは駆動軸の表面
に磁歪材料を接着させ、駆動軸に加わる応力に供なって
磁歪材料の磁気特性の変化を検出するセンサで、この磁
歪材料に非晶質合金が利用されるものである。このトル
クセンサに非晶質合金を利用するに際して要求されるこ
とは、円筒状の非晶質合金ブロックを得ることと、この
円筒状の非晶質合金ブロックをいかに強固に駆動軸表面
に固着するかである。非晶質合金は前述のように高強度
・高高度でしかも400〜500℃という低い温度で結晶化し
てしまうため、普通の金属材料のように溶接やろう付け
といった一般的な接合方法が使えず、駆動軸と非晶質合
金との接合が非晶質合金トルクセンサの鍵となってい
る。By the way, there is a torque sensor as a device utilizing the magnetic characteristics of an amorphous alloy. A torque sensor is a sensor that adheres a magnetostrictive material to the surface of the drive shaft and detects the change in the magnetic characteristics of the magnetostrictive material by subjecting it to the stress applied to the drive shaft.This magnetostrictive material uses an amorphous alloy. is there. When using an amorphous alloy for this torque sensor, what is required is to obtain a cylindrical amorphous alloy block and how to firmly fix this cylindrical amorphous alloy block to the drive shaft surface. It is. As mentioned above, amorphous alloys have high strength and high altitude, and they crystallize at a low temperature of 400 to 500 ° C, so common welding methods such as welding and brazing cannot be used like ordinary metal materials. The joining of the drive shaft and the amorphous alloy is the key to the amorphous alloy torque sensor.
円筒状の非晶質合金ブロックを得る提案として特開昭60
−204804号公報の発明がある。この発明は、中空部を有
するアモルファス粉末成形体を製造するに際し、前記中
空部にほぼ対応する部分を別種の粉末とした予備成形体
を成形したのち、前記予備成形体を衝撃波成形法により
圧縮固化成形し、その後得られた固化成形体の別種の粉
末固化部分を除去して中空部となすものである。しか
し、この発明では衝撃波を与えるための方法が簡便でな
いという問題点がある。As a proposal to obtain a cylindrical amorphous alloy block, JP-A-60
There is an invention of -204804 publication. According to the present invention, when an amorphous powder compact having a hollow portion is manufactured, a preform having a portion substantially corresponding to the hollow portion is made of another kind of powder, and then the preform is compression-solidified by a shock wave molding method. It is formed into a hollow portion by molding and then removing the powder solidified portion of another kind of the solidified molded body obtained. However, the present invention has a problem that the method for applying a shock wave is not simple.
また、駆動軸を母材とし、その母材表面に直接アモルフ
ァス金属被覆層を形成する提案として、特開昭60−1940
85号公報の発明がある。この発明は、母材とアモルファ
ス金属とを金属製の容器に入れ、高エネルギー加工する
ことにより、アモルファス金属の被覆層を母材表面に形
成したものである。この発明で高エネルギー加工とは、
爆発成形加工であり、母材とアモルファス金属の被覆層
の接合は強固であり、被覆層の磁気特性も優れたもので
あるが、爆発加工であるため危険性が大きくかつ加工費
も非常に高価であるという欠点がある。Further, as a proposal for forming a drive shaft as a base material and forming an amorphous metal coating layer directly on the surface of the base material, Japanese Patent Laid-Open No. 60-1940
There is an invention of Japanese Patent No. 85. According to the present invention, a base material and an amorphous metal are placed in a metal container and subjected to high energy processing to form a coating layer of the amorphous metal on the surface of the base material. In this invention, high energy processing means
It is an explosion-molding process, the bond between the base material and the coating layer of amorphous metal is strong, and the magnetic properties of the coating layer are excellent, but since it is an explosion-processing process, there is a great risk and the processing cost is very expensive. There is a drawback that
高温押し出し成形により非晶質合金ブロックを得る方法
として米国特許第4,377,622号明細書の発明がある。こ
の発明は金属製の容器に細線状の非晶質合金を理論密度
の約50〜60%になるように充填し、容器を栓で密閉して
押し出し用ビレットとし、このビレットを塑性遷移温度
と結晶化温度の間の加工温度に加熱し、この加工温度で
断面減少率を少なくとも3.5対1(約70%)の割合で押
し出し加工をし、円柱状の非晶質合金ブロックを得るも
のである。また、この発明の他の実施態様では、容器の
中心に芯材を据え容器と芯材の間に非晶質合金を充填
し、容器を密閉後同じように塑性遷移温度と結晶化温度
の間の加工温度で押し出し加工し、芯材を機械加工で除
去して円筒状の非晶質合金ブロックを得る方法が開示さ
れている。There is an invention of US Pat. No. 4,377,622 as a method for obtaining an amorphous alloy block by hot extrusion. According to the invention, a metal container is filled with a thin wire amorphous alloy so as to have a theoretical density of about 50 to 60%, and the container is sealed with a stopper to form a billet for extrusion. A columnar amorphous alloy block is obtained by heating to a processing temperature between crystallization temperatures and extruding at this processing temperature at a cross-section reduction rate of at least 3.5 to 1 (about 70%). . Further, in another embodiment of the present invention, a core material is installed in the center of the container, an amorphous alloy is filled between the container and the core material, and after the container is closed, a plastic transition temperature and a crystallization temperature are similarly set. A method of obtaining a cylindrical amorphous alloy block by extruding at a processing temperature of 10 and removing the core material by machining is disclosed.
この発明では芯材と非晶質合金被覆層とを良好に接合す
るためには、押し出し加工における断面減少率を約70%
以上必要とする。これは相当な押し出し荷重を付与する
ための大掛かりな装置を必要とする。また、押し出し加
工時に、芯材と非晶質合金との押し出し速度の差を生
じ、両者の境界で滑りを発生して非晶質合金の側にクラ
ックが入り、両者の結合が悪くなるなどの問題を招く。In this invention, in order to satisfactorily bond the core material and the amorphous alloy coating layer, the cross-section reduction rate in the extrusion process is about 70%.
More than required. This requires extensive equipment to apply a significant extrusion load. In addition, during extrusion processing, a difference in extrusion speed between the core material and the amorphous alloy occurs, slippage occurs at the boundary between the two, and a crack is formed on the amorphous alloy side, resulting in poor bonding between the two. Cause problems.
[発明が解決しようとする問題点] 本発明は上述の問題を解決して芯材と非晶質合金との結
合に優れた非晶質合金被覆体およびその製造方法を提供
することを目的とする。[Problems to be Solved by the Invention] An object of the present invention is to solve the above problems and provide an amorphous alloy coated body excellent in bonding between a core material and an amorphous alloy and a method for producing the same. To do.
[問題点を解決するための手段] 本発明の非晶質合金被覆体は、表面に凹凸を備えた芯材
と、その芯材の表面に被覆される非晶質合金とから成
り、前記非晶質合金の塑性遷移温度と結晶化温度の間の
成形温度において前記芯材と前記非晶質合金とを塑性加
工することにより非晶質合金の被覆層が前記芯材の表面
に形成されたことを要旨とする。[Means for Solving the Problems] The amorphous alloy coated body of the present invention comprises a core material having irregularities on the surface and an amorphous alloy coated on the surface of the core material. A coating layer of an amorphous alloy was formed on the surface of the core material by plastically working the core material and the amorphous alloy at a forming temperature between the plastic transition temperature and the crystallization temperature of the crystalline alloy. That is the summary.
また、本発明の非晶質合金被覆体の製造方法は、次の工
程から成ることを要旨とする。Further, the gist of the method for producing an amorphous alloy coated body of the present invention is that it comprises the following steps.
a) 一端が開放された金属製容器の中心に、表面に凹
凸を備えた芯材を固定し、前記容器と芯材の間に非晶質
合金を充填する工程、 b) 前記容器の開放端に栓を嵌挿して容器を密閉し成
形ビレットとする工程、 c) 前記成形ビレットを前記非晶質合金の塑性遷移温
度と結晶化温度の間の成形温度に加熱し、該成形温度に
おいて塑性加工する工程。a) a step of fixing a core material having irregularities on the surface at the center of a metal container with one end open, and filling an amorphous alloy between the container and the core material, b) the open end of the container A step of inserting a stopper into the container to seal the container to form a forming billet, c) heating the forming billet to a forming temperature between the plastic transition temperature and the crystallization temperature of the amorphous alloy, and performing plastic forming at the forming temperature The process of doing.
[作用] 本発明で使用させる非晶質合金は、例えばFe系とCo系で
優れた磁気特性を有するもので、その形態は粉末、細線
あるいは薄帯のいずれでもよい。先ず一端が開放された
金属製容器の中心に、表面の凹凸を備えた芯材を固定す
る。芯材の表面の凹凸は芯材と非晶質合金が塑性変形を
受けた際、非晶質合金が芯材の表面を滑らない程度のも
のでよく、例えば芯材の表面をローレット加工を施した
ものでよい。次に、非晶質合金を容器と芯材の間の空間
に充填する。粉末である場合は、冷間予備圧縮を繰り返
しながら充填し、細線や薄帯の場合は芯材の回りに高密
度で巻き付ける。非晶質合金の充填密度は理論密度の約
40%程度で充分である。非晶質合金の充填が終わったな
らば、容器を10-3Torr程度以上に真空引きし、アルゴ
ン、窒素等の不活性置換を行う。これにより容器中の空
気が排除され、非晶質合金の酸化が防止される。次いで
容器の開放端に栓を嵌挿し密閉して成形ビレットとす
る。栓のシールには溶接または高温型接着剤例えばセラ
ミックス系接着剤を使用すると良い。[Operation] The amorphous alloy used in the present invention has excellent magnetic characteristics in, for example, Fe-based and Co-based, and may be in the form of powder, fine wire or ribbon. First, a core material having surface irregularities is fixed to the center of a metal container whose one end is open. The unevenness of the surface of the core material may be such that the amorphous alloy does not slip on the surface of the core material when the core material and the amorphous alloy undergo plastic deformation.For example, the surface of the core material is knurled. You can use what you did. Next, the amorphous alloy is filled into the space between the container and the core material. If it is a powder, it is filled while repeatedly performing cold precompression, and if it is a thin wire or a thin strip, it is wrapped around the core material at a high density. The packing density of an amorphous alloy is about the theoretical density.
About 40% is sufficient. After the filling of the amorphous alloy is completed, the container is evacuated to about 10 −3 Torr or more and inert substitution of argon, nitrogen, etc. is performed. This eliminates the air in the container and prevents the oxidation of the amorphous alloy. Next, a plug is inserted into the open end of the container and hermetically sealed to form a molded billet. Welding or high temperature type adhesives such as ceramics type adhesives may be used to seal the plugs.
成形ビレットは塑性遷移温度と結晶化温度の間の成形温
度に加熱する。ここで塑性遷移温度とは、非晶質合金を
種々の温度で応力を加えた場合、ある温度以下では不均
一変形挙動を示すが、それ以上の温度では均一変形挙動
を示し、その温度をいうのである。従って非晶質合金は
この塑性遷移温度と結晶化温度の間の成形温度で塑性変
形を与えると、非晶質合金全体が均一に変形する塑性変
形をするのである。The forming billet is heated to a forming temperature between the plastic transition temperature and the crystallization temperature. Here, the plastic transition temperature refers to the temperature at which, when stress is applied to an amorphous alloy at various temperatures, it exhibits a non-uniform deformation behavior at a certain temperature or lower, but shows a uniform deformation behavior at a temperature higher than that. Of. Therefore, when the amorphous alloy is plastically deformed at a forming temperature between the plastic transition temperature and the crystallization temperature, the amorphous alloy is deformed uniformly as a whole.
本発明では成形ビレットはその非晶質合金の塑性遷移温
度と結晶化温度の間の成形温度に加熱されたまま、塑性
加工を受ける。塑性加工とは具体的には押し出しあるい
は引き抜き等の加工であって、この塑性加工によって非
晶質合金は剪断力を受ける。非晶質合金は単なる圧縮で
は結合は起こらないが、剪断応力成分が働くと隣接する
非晶質合金同志の接触が助長され、塑性変形の流れがこ
の接触面積を増大させると共に表面の酸化物や不純物の
皮膜を破壊するので、非晶質合金同志の接合が起こる。In the present invention, the forming billet undergoes plastic working while being heated to the forming temperature between the plastic transition temperature and the crystallization temperature of the amorphous alloy. Specifically, the plastic working is working such as extrusion or drawing, and the amorphous working receives shearing force by the plastic working. Bonding does not occur in an amorphous alloy by mere compression, but when a shear stress component acts, contact between adjacent amorphous alloys is promoted, and the flow of plastic deformation increases this contact area and the oxides on the surface and Since the film of impurities is destroyed, the joining of amorphous alloys takes place.
塑性変形に使用する押し出し型は予め加熱コイル等によ
り成形温度に加熱しておく。また、成形温度は加工発熱
による温度上昇により成形ビレットが結晶化温度以上に
ならないよう、結晶化温度から加工発熱温度を差し引い
た温度以下で加工する必要がある。押し出し加工の断面
減少率は40%程度で充分である。The extrusion die used for plastic deformation is preheated to the forming temperature by a heating coil or the like. Further, it is necessary to process the molding temperature at a temperature below the crystallization temperature minus the processing heat generation temperature so that the molding billet does not exceed the crystallization temperature due to the temperature rise due to the processing heat generation. A cross-section reduction rate of about 40% is sufficient for extrusion processing.
成形ビレットの塑性加工においては、芯材と非晶質合金
の密度が異なるため、成形中において芯材が先に伸びよ
うとする。このため、非晶質合金と芯材の摩擦が少ない
と両者の境界ですべりが生じ非晶質合金の側にクラック
が入ってしまうし、非晶質合金同志の接合に大きく寄与
する剪断が非晶質合金に十分加わらなくなる。しかし、
本発明では芯材の表面には凹凸が設けられているので、
芯材と非晶質合金の間の摩擦が大きく、非晶質合金と芯
材とが同じように伸び、境界ですべりが起こらず、非晶
質合金の被覆層にクラックが入らない。また、すべりに
よって生じる剪断のロスがなく、効果的に非晶質合金に
剪断を加えることができる。さらに、芯材の表面の凹凸
により、芯材と非晶質合金が機械的に強固に接合された
非晶質合金被覆体が一体成形できる。In the plastic working of a forming billet, the core material and the amorphous alloy have different densities, so that the core material tends to stretch first during forming. Therefore, if there is little friction between the amorphous alloy and the core material, slippage will occur at the boundary between the amorphous alloy and cracks on the side of the amorphous alloy, and the shear that greatly contributes to the joining of the amorphous alloys will not occur. It does not add enough to the crystalline alloy. But,
In the present invention, since the surface of the core material is provided with irregularities,
The friction between the core material and the amorphous alloy is large, the amorphous alloy and the core material are stretched similarly, slippage does not occur at the boundary, and the coating layer of the amorphous alloy is not cracked. Further, there is no shear loss caused by slippage, and shear can be effectively added to the amorphous alloy. Further, due to the unevenness of the surface of the core material, an amorphous alloy coated body in which the core material and the amorphous alloy are mechanically strongly bonded can be integrally molded.
[実施例] 本発明の実施例について詳細に説明し、本発明の効果を
明らかにする。Example An example of the present invention will be described in detail to clarify the effect of the present invention.
(実施例1) 第1図の断面図の示すような外径29mm、内径26mm、S45C
製の円筒形の容器10を用意し、この容器10の中心に14mm
φのS55C製の表面に軸心に対し45゜でかつ90゜で交差
し、ピッチ1mm、深さ0.5mmの直線溝を多数もつローレッ
ト加工12を施した芯材14を固定した。なお、芯材14の固
定端にはローレット加工をしていない。また、容器10の
先端16は90゜の角度に加工した。次いで容器10と芯材14
との間に、非晶質合金粉末(成分;Fe78B13Si9、粒径;74
〜105μm)18を冷間予備圧縮を繰り返しながら密度約4
0%になるように充填した。非晶質合金18を充填後、容
器10を10-3Torrに真空引きし、アルゴン置換を行い、直
ちに栓20を嵌挿しセラミック系接着剤でシールして容器
10を密閉し成形ビレット22とした。なお、比較のために
芯材14の表面にローレット加工12を施さない研摩状態の
芯材14を別に用意し、同じように非晶質合金18を充填し
て成形ビレット22とした。(Example 1) As shown in the sectional view of FIG. 1, outer diameter 29 mm, inner diameter 26 mm, S45C
Prepare a cylindrical container 10 made of 14 mm in the center of this container 10.
A knurled core 14 having a large number of linear grooves with a pitch of 1 mm and a depth of 0.5 mm was fixed to the surface of φ55 mm S55C, intersecting at 45 ° and 90 ° with respect to the shaft center. Note that the fixed end of the core material 14 is not knurled. Further, the tip 16 of the container 10 was processed at an angle of 90 °. Then the container 10 and core 14
Between the amorphous alloy powder (component; Fe 78 B 13 Si 9 , grain size; 74
~ 105 μm) 18 while repeatedly cold pre-compressing the density of about 4
It was filled to 0%. After filling the amorphous alloy 18, the container 10 was evacuated to 10 -3 Torr, and the atmosphere was replaced with argon. Immediately, the plug 20 was inserted and sealed with a ceramic adhesive to make the container.
10 was closed to form a molding billet 22. For comparison, a polished core material 14 in which the knurling 12 was not applied to the surface of the core material 14 was separately prepared and similarly filled with an amorphous alloy 18 to form a molding billet 22.
次ぎに成形ビレット22に黒鉛潤滑剤を塗布し、第1表に
示すような種々の成形温度に加熱し、それを第2図に示
す押し出し型24に挿入し、押し出し成形を行って第3図
に示すように芯材14の表面に非晶質合金の被覆層26の形
成された非晶質合金被覆体28を得た。押し出し型24は予
め加熱コイル30で成形温度に加熱した。また、押し出し
型24の断面減少率は40%、進入角度は90゜であった。Next, a graphite lubricant is applied to the forming billet 22 and heated to various forming temperatures as shown in Table 1, which is inserted into the extrusion die 24 shown in FIG. As shown in FIG. 5, an amorphous alloy coating 28 having an amorphous alloy coating layer 26 formed on the surface of the core material 14 was obtained. The extrusion mold 24 was previously heated to the molding temperature by the heating coil 30. The cross-section reduction rate of the extrusion mold 24 was 40%, and the approach angle was 90 °.
得られた非晶質合金被覆体を切断し、被覆層の密度、ク
ラックの有無、磁気特性および非晶質合金含有量につい
て検査し結果を第1表に示した。The obtained amorphous alloy coated body was cut, and the density of the coating layer, the presence or absence of cracks, the magnetic properties and the amorphous alloy content were inspected and the results are shown in Table 1.
第1表から知られるように、500℃で成形したものは、
いずれの場合も結晶化していたが、それ以外のものは非
晶質状態で維持していることが確認できた。300℃以下
ではいずれの試料もクラックが多く、また非常にポーラ
スであった。しかし、350℃以上ではち密なものが得ら
れたが、表面研摩状態のものでは依然としてクラックが
消えなかったのに対し、表面ローレット加工を施したも
のはクラックがなく、しかもち密で良好な被覆層26が得
られ、その密度は理論密度の98.5%以上であった。な
お、表面研摩状態のものを400℃で成形した試料の断面
写真を第4図に、表面ローレット加工したものを400℃
で成形した試料の断面写真を第5図に、第5図のさらに
拡大写真を第6図に示した。第4図、第5図および第6
図から明らかなように、第4図の表面研摩状態のものは
押し出し方向に対して斜めのクラックが多数観察される
のに対し、第5図および第6図のローレット加工のもの
はクラックが全く観察されずち密な被覆層が形成されて
いることをが判る。 As known from Table 1, those molded at 500 ° C
Although it was crystallized in all cases, it was confirmed that the others were kept in an amorphous state. Below 300 ° C, all the samples had many cracks and were very porous. However, at 350 ° C or higher, a dense coating was obtained, but cracks did not disappear in the surface-polished state, whereas those subjected to surface knurling had no cracks and a dense and good coating layer. 26 was obtained, and its density was 98.5% or more of the theoretical density. A cross-sectional photograph of a sample obtained by molding the surface-polished state at 400 ° C is shown in Fig. 4, and the surface knurled at 400 ° C.
A cross-sectional photograph of the sample molded in step 1 is shown in FIG. 5, and a further enlarged photograph of FIG. 5 is shown in FIG. 4, 5, and 6
As is clear from the figure, many cracks oblique to the extrusion direction are observed in the surface-polished state shown in FIG. 4, whereas no cracks are observed in the knurled ones shown in FIGS. 5 and 6. It can be seen that a dense coating layer is formed without being observed.
なお、非晶質合金18が細線であるかまたは薄帯である場
合は、第7図および第8図に示すように、芯材12に細線
や薄帯を高密度に巻き付けてから容器10に挿入し栓20を
して成形ビレット22とすれば良い。When the amorphous alloy 18 is a thin wire or a thin strip, as shown in FIGS. 7 and 8, the thin wire or the thin strip is wound around the core material 12 at a high density before being placed in the container 10. The billet 22 may be formed by inserting it and plugging it 20.
(実施例2) 実施例1で400℃で成形加工した本発明例の試料と比較
例の試料を第9図の断面図にしめすようなトルクセンサ
シャフト32に加工し、第10図のトルクセンサ模式図に示
すように駆動軸4として接続し、トルクを検出した。Example 2 The sample of the present invention and the sample of the comparative example, which were molded at 400 ° C. in Example 1, were processed into a torque sensor shaft 32 as shown in the sectional view of FIG. 9, and the torque sensor of FIG. As shown in the schematic diagram, the drive shaft 4 was connected and the torque was detected.
第10図に示したトルクセンサの作動を説明すると、被覆
層26を形成した駆動軸4の表面近傍に、被覆層26を励磁
するコイル2と、被覆層26の磁歪特性を検出するコイル
3を設置すると、駆動軸4に伝達するトルクによる歪に
起因する起電力が測定できる。この起電力は増幅された
電気信号として取り出される。検出回路としては発信機
6から出された信号を駆動回路7にて方形波にし、励磁
コイル2に電流を付加する。検出コイル3にて駆動によ
り生じた歪にて発生する起電力を交流増幅器8にて増幅
し、サンプリング回路9にてサンプリングし、さらに励
磁方形波と比較することによりトルクを検出する。な
お、本実施例においては励磁周波数1,1khz、ギャップ0.
5mmとしてトルクを検出した。The operation of the torque sensor shown in FIG. 10 will be described. A coil 2 for exciting the coating layer 26 and a coil 3 for detecting the magnetostrictive characteristic of the coating layer 26 are provided near the surface of the drive shaft 4 on which the coating layer 26 is formed. When installed, the electromotive force caused by the distortion due to the torque transmitted to the drive shaft 4 can be measured. This electromotive force is extracted as an amplified electric signal. As a detection circuit, a signal output from the transmitter 6 is converted into a square wave by the drive circuit 7, and a current is added to the exciting coil 2. The electromotive force generated by the distortion generated by driving the detection coil 3 is amplified by the AC amplifier 8, sampled by the sampling circuit 9, and further compared with the excitation square wave to detect the torque. In this embodiment, the excitation frequency is 1,1khz and the gap is 0.
The torque was detected as 5 mm.
第11図は本発明例と比較例に加えられるトルクとその出
力との関係を示す図である。比較例1はパーマロイを芯
材の回りに凹凸を設けずに結合したもので、比較例2は
芯材の回りにNiメッキを形成したものである。第11図か
ら明らかなように、駆動軸である非晶質被覆体に加えら
れるトルクと、その結果非晶質合金被覆層から得られる
出力は、本発明例は比較例に比較して良い比例関係が成
立している。また、印加トルクの上昇と下降とによるヒ
ステリシスの差も、比較例より本発明例の方が小さく感
度も良い。FIG. 11 is a diagram showing the relationship between the torque applied to the example of the present invention and the comparative example and its output. In Comparative Example 1, permalloy is bonded around the core material without providing irregularities, and in Comparative Example 2, Ni plating is formed around the core material. As is apparent from FIG. 11, the torque applied to the amorphous coating body that is the drive shaft and the output obtained from the amorphous alloy coating layer as a result of the invention are in good proportion as compared with the comparative example. The relationship is established. Further, the difference in hysteresis due to the rise and fall of the applied torque is smaller and the sensitivity is better in the example of the present invention than in the comparative example.
なお、本発明において、芯材の凹凸は第1図のようにロ
ーレット加工によるものの他に、芯材が円柱状であれば
その周方向に凹凸を設けてもよいし、不規則な形状で凹
凸を設けてもよい。このような凹凸の配置は、押し出し
加工あるいは引き抜き加工の際の芯材と非晶質合金との
押し出しあるいは引き抜き速度差をなくすことができ、
非晶質合金よりなる被覆層のクラック発生を防止でき
る。なお、凹凸の形状としては芯材が円柱状の場合、そ
の軸方向の凹凸と上記配置の凹凸との併用は場合によっ
て差し支えない。In addition, in the present invention, the unevenness of the core material is not limited to that obtained by knurling as shown in FIG. 1, but the unevenness may be provided in the circumferential direction if the core material has a cylindrical shape. May be provided. The arrangement of such irregularities can eliminate the difference in extrusion or drawing speed between the core material and the amorphous alloy during extrusion or drawing.
It is possible to prevent cracking of the coating layer made of an amorphous alloy. As for the shape of the unevenness, when the core material is cylindrical, the unevenness in the axial direction and the unevenness in the above arrangement may be used in some cases.
[発明の効果] 本発明の非晶質合金被覆体およびその製造方法は以上説
明したように、表面に凹凸を備えた芯材を容器の中心に
固定し、容器と芯材の間に非晶質合金を充填し、容器に
栓をして密閉し成形ビレツトを作り、この成形ビレツト
を非晶質合金の塑性遷移温度と結晶化温度の間の成形温
度で塑性加工し、芯材の表面に非晶質合金の被覆層を得
るものであり、本発明により得られた非晶質合金被覆体
は、被覆層にクラック等の欠陥がなく密度も充分に高
く、磁性特性にも優れていると共に、芯材との接合も極
めて強固である等の数々の優れた効果がある。本発明の
非晶質合金被覆体を用いればトルクセンサ等の磁性体、
磁気ヘッド、耐摩耗性の摺動部材、耐食性を有するフィ
ルタ材、ソーダ電解や燃料電池などの電極材料として多
くの部品に利用できる。[Effects of the Invention] As described above, the amorphous alloy coated body of the present invention and the method for producing the same are such that the core material having surface irregularities is fixed to the center of the container, and the amorphous material is provided between the container and the core material. The alloy is filled with a high-quality alloy, the container is capped and sealed to form a molded vitreto, and the molded vitreto is plastically worked at a molding temperature between the plastic transition temperature and the crystallization temperature of the amorphous alloy to form a core material surface. In order to obtain a coating layer of an amorphous alloy, the amorphous alloy coating obtained by the present invention has no defects such as cracks in the coating layer and has a sufficiently high density, and also has excellent magnetic properties. Also, it has a number of excellent effects such as extremely strong bonding with the core material. By using the amorphous alloy coated body of the present invention, a magnetic body such as a torque sensor,
It can be used for many parts as a magnetic head, a wear-resistant sliding member, a filter material having corrosion resistance, an electrode material for soda electrolysis and a fuel cell.
第1図は成形ビレットの断面図、第2図は押し出し型の
断面図、第3図は非晶質合金被覆体の断面図、第4図、
第5図および第6図は被覆層の断面の金属組織を表す顕
微鏡写真、第7図は薄帯状の非晶質合金を充填した成形
ビレットの断面図、第8図は細線状の非晶質合金を充填
した成形ビレットの断面図、第9図はトルクセンサシャ
フトの断面図、第10図はトルクセンサの模式図、第11図
はトルクとトルクセンサ出力の関係を表す図である。 10……容器、12……ローレット加工、14……芯材、18…
…非晶質合金、20……栓、22……成形ビレット、26……
非晶質合金被覆層、28…非晶質合金被覆体FIG. 1 is a sectional view of a forming billet, FIG. 2 is a sectional view of an extrusion die, FIG. 3 is a sectional view of an amorphous alloy coated body, FIG.
5 and 6 are micrographs showing the metallographic structure of the cross section of the coating layer, FIG. 7 is a cross section of a molded billet filled with a ribbon-shaped amorphous alloy, and FIG. 8 is a thin-line amorphous. 9 is a sectional view of a molded billet filled with an alloy, FIG. 9 is a sectional view of a torque sensor shaft, FIG. 10 is a schematic diagram of a torque sensor, and FIG. 11 is a diagram showing a relationship between torque and torque sensor output. 10 …… container, 12 …… knurling, 14 …… core material, 18…
… Amorphous alloy, 20 …… Stopper, 22 …… Molded billet, 26 ……
Amorphous alloy coating layer, 28 ... Amorphous alloy coating
フロントページの続き (72)発明者 赤井 正司 愛知県刈谷市昭和町1丁目1番地 日本電 装株式会社内 (56)参考文献 特開 昭53−57170(JP,A) 特開 昭61−69953(JP,A)Front page continuation (72) Inventor Shoji Akai 1-1, Showa-cho, Kariya city, Aichi Nihon Denso Co., Ltd. (56) Reference JP-A-53-57170 (JP, A) JP-A-61-69953 ( JP, A)
Claims (13)
面に被覆される非晶質合金とから成り、前記非晶質合金
の塑性遷移温度と結晶化温度の間の成形温度において前
記芯材と前記非晶質合金とを塑性加工することにより非
晶質合金の被覆層が前記芯材の表面に形成されたことを
特徴とする非晶質合金被覆体。1. A molding temperature comprising a core material having irregularities on its surface and an amorphous alloy coated on the surface of the core material, the molding temperature being between the plastic transition temperature and the crystallization temperature of the amorphous alloy. 2. An amorphous alloy coated body, wherein a coating layer of an amorphous alloy is formed on the surface of the core material by plastically working the core material and the amorphous alloy.
レット加工によって生じた凹凸である特許請求の範囲第
1項に記載の非晶質合金被覆体。2. The amorphous alloy coated body according to claim 1, wherein the irregularities on the surface of the core material are irregularities generated by knurling the surface of the core material.
請求の範囲第1項または第2項に記載の非晶質合金被覆
体。3. The amorphous alloy coated body according to claim 1 or 2, wherein the plastic working is extrusion working.
請求の範囲第1項または第2項に記載の非晶質合金被覆
体。4. The amorphous alloy coated body according to claim 1 or 2, wherein the plastic working is drawing.
の98%以上である特許請求の範囲第1項に記載の非晶質
合金被覆体。5. The amorphous alloy coated body according to claim 1, wherein the density of the coating layer of the amorphous alloy is 98% or more of the theoretical density.
合金被覆体の製造方法、 a) 一端が開放された金属製容器の中心に、表面に凹
凸を備えた芯材を固定し、前記容器と芯材の間に非晶質
合金を充填する工程、 b) 前記容器の開放端に栓を嵌挿して容器を密閉し成
形ビレットとする工程、 c) 前記成形ビレットを前記非晶質合金の塑性遷移温
度と結晶化温度の間の成形温度に加熱し、該成形温度に
おいて塑性加工する工程。6. A method for producing an amorphous alloy coated body, which comprises the steps of: a) fixing a core material having an uneven surface on the center of a metal container whose one end is open. Filling the amorphous alloy between the container and the core material, b) inserting a plug into the open end of the container to seal the container into a molded billet, c) the amorphous billet Heating to a forming temperature between the plastic transition temperature and the crystallization temperature of the fine alloy, and plastically working at the forming temperature.
真空引きした後不活性ガス置換を行う特許請求の範囲第
6項に記載の非晶質合金被覆体の製造方法。7. The method for producing an amorphous alloy-coated body according to claim 6, wherein the container is filled with an amorphous alloy, and then the container is evacuated and then replaced with an inert gas.
特許請求の範囲第6項に記載の非晶質合金被覆体の製造
方法。8. The method for producing an amorphous alloy coated body according to claim 6, wherein the evacuation is performed at least 10 −3 Torr.
である特許請求の範囲第6項に記載の非晶質合金被覆体
の製造方法。9. The filling rate of the amorphous alloy is at least 40%.
The method for producing an amorphous alloy coated body according to claim 6, wherein
請求の範囲第6項に記載の非晶質合金被覆体の製造方
法。10. The method for producing an amorphous alloy coated body according to claim 6, wherein the plastic working is extrusion molding.
請求の範囲第6項に記載の非晶質合金被覆体の製造方
法。11. The method for producing an amorphous alloy coated body according to claim 6, wherein the plastic working is drawing.
とも40%である特許請求の範囲第6項、第9項または第
10項のいずれかに記載の非晶質合金被覆体の製造方法。12. A cross-section reduction rate due to the plastic working is at least 40%.
11. The method for producing an amorphous alloy coated body according to any one of 10 items.
て除去する特許請求の範囲第6項に記載の非晶質合金被
覆体の製造方法。13. The method for producing an amorphous alloy coated body according to claim 6, wherein the container is removed by machining after the plastic working.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP28621886A JPH0798210B2 (en) | 1986-12-01 | 1986-12-01 | Amorphous alloy coated body and method for producing the same |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP28621886A JPH0798210B2 (en) | 1986-12-01 | 1986-12-01 | Amorphous alloy coated body and method for producing the same |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS63140723A JPS63140723A (en) | 1988-06-13 |
| JPH0798210B2 true JPH0798210B2 (en) | 1995-10-25 |
Family
ID=17701501
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP28621886A Expired - Lifetime JPH0798210B2 (en) | 1986-12-01 | 1986-12-01 | Amorphous alloy coated body and method for producing the same |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0798210B2 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20130140173A1 (en) * | 2011-06-10 | 2013-06-06 | Séverin Stéphane Gérard Tierce | Rotary sputter target assembly |
-
1986
- 1986-12-01 JP JP28621886A patent/JPH0798210B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JPS63140723A (en) | 1988-06-13 |
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