JP2004100042A - Method for producing copper alloy stock - Google Patents

Method for producing copper alloy stock Download PDF

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Publication number
JP2004100042A
JP2004100042A JP2003198394A JP2003198394A JP2004100042A JP 2004100042 A JP2004100042 A JP 2004100042A JP 2003198394 A JP2003198394 A JP 2003198394A JP 2003198394 A JP2003198394 A JP 2003198394A JP 2004100042 A JP2004100042 A JP 2004100042A
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Japan
Prior art keywords
copper alloy
strain
alloy material
producing
conductivity
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JP2003198394A
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Japanese (ja)
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JP4014542B2 (en
Inventor
Mitsuhiro Funaki
船木 光弘
Daiki Baba
馬場 大樹
Masaya Oyama
大山 真哉
Toshiyuki Horimuki
堀向 俊之
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Honda Motor Co Ltd
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Honda Motor Co Ltd
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Priority to CN200910262569A priority Critical patent/CN101760663A/en
Priority to GB0601625A priority patent/GB2419605B/en
Priority to US10/521,333 priority patent/US7544259B2/en
Priority to GB0601627A priority patent/GB2419603B/en
Priority to GB0601624A priority patent/GB2419604B/en
Priority to CN03822284A priority patent/CN100591784C/en
Priority to CA002492925A priority patent/CA2492925A1/en
Priority to JP2003198394A priority patent/JP4014542B2/en
Application filed by Honda Motor Co Ltd filed Critical Honda Motor Co Ltd
Priority to GB0503149A priority patent/GB2406579B/en
Priority to PCT/JP2003/009102 priority patent/WO2004009859A1/en
Priority to AU2003252210A priority patent/AU2003252210A1/en
Publication of JP2004100042A publication Critical patent/JP2004100042A/en
Application granted granted Critical
Publication of JP4014542B2 publication Critical patent/JP4014542B2/en
Priority to US12/387,608 priority patent/US20100021334A1/en
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Abstract

<P>PROBLEM TO BE SOLVED: To provide a method for imparting excellent mechanical strength and thermal and electric properties to a copper alloy. <P>SOLUTION: Secondary elements which hardly enter into a solid solution such as Cr (chromium), zirconium (Zr), beryllium (Be), titanium (Ti) and boron (B) are dissolved into a solid solution with a base material metal (Cu) by solution heat treatment, and thereafter rapid cooling is performed to obtain a stock in a supersaturated state. If required, aging treatment is subsequently performed. Then, strain equivalent to an elongation of ≥200%, preferably of 220%, is applied to the stock to attain the fining of crystals (to a mean crystal grain size of ≤20 μm). Simultaneously with the application of the strain or thereafter, aging treatment is applied to promote the precipitation of the secondary elements between the crystal grains. <P>COPYRIGHT: (C)2004,JPO

Description

【0001】
【発明の属する技術分野】
本発明は、溶接の電極材料や電気自動車のコネクタの材料等に好適する銅合金の製造方法に関する。
【0002】
【従来の技術】
自動車のEV(電気自動車)化に伴い、ハーネス、ワイヤーの接続部品であるコネクタの使用量が増加傾向にある。またEV化では電子制御技術で安全性、燃費を確保することも目的に挙げられる。
自動車に組み込まれるコネクタは高温、振動という過激な環境下で使用されるため、接続信頼性、接触安定性が求められる。またEV化が進むにつれてエネルギー損失が少ない、つまり高導電率な銅系ばね材料が望まれている。
また、溶接の電極材料に関しても機械的強度、熱的特性及び電気的特性の全てにおいて所定値以上の特性が要求される。
【0003】
金属材料の機械的強度を向上せしめる手段として結晶組織の微細化を図ることが、ホール・ペッチの法則として知られている。
例えば、金属や合金材料を変形すると、加工硬化によって材料強度が上昇する。これは加工(塑性変形)によって、材料中に種々の欠陥(点欠陥、転位、積層欠陥など)が蓄積し、これら欠陥の相互作用の結果、新しい欠陥の導入・移動が困難になり、外力に対する抵抗を持つことになるからと理解されている。
【0004】
金属材料に塑性変形(歪)を与えるには、従来から、押し出し、引き抜き、せん断、圧延、鍛造などが行われている。
具体的には、材料に高圧をかけながらねじるHPT(High Pressure Torsion)法、括れのついたパイプの中を繰り返し通すCEC(Cyclic Extrusion Compression)法、圧延で薄くなった金属板を切断して重ね合わせ繰り返し圧延するARB(Accumulative Roll Bonding)法が提案され、特にアルミニウム合金に対しての微細化の具体的方法として、特許文献1、特許文献2、特許文献3、特許文献4などに開示される材料の断面減少を伴わない側方押し出しで、せん断変形を与えるECAE法が提案されている。
【0005】
一方、銅合金については特許文献5、特許文献6などに開示される方法が提案されている。この先行技術は銅合金のうちでも、水栓金具などの材料として使用される黄銅(Cu−Zn)の特性(切削性と脱亜鉛腐食)を改善するために、熱間押し出しによって動的再結晶を起こさせ、結晶の微細化と特定の結晶組織割合(α相、β相、γ相の割合)が得られるようにしたものである。
【0006】
また、クロム(Cr)、ジルコニウム(Zr)、ベリリウム(Be)、ホウ素(B)、チタン(Ti)などの室温で固溶しないか殆んど固溶しない元素を添加した時効硬化型の銅合金に対して所定の特性を引き出すには、先ず、溶体化処理によって、前記元素を高温で十分に固溶させた後、急冷して過飽和状態とし、この後所定の温度で時効処理することで過飽和状態となっていた添加元素を析出せしめるようにしている。
【0007】
【特許文献】
特許文献1:特開平9−137244号公報
特許文献2:特開平10−258334号公報
特許文献3:特開平11−114618号公報
特許文献4:特開2000−271621号公報
特許文献5:特開平11−140568号公報
特許文献6:特開2000−355746号公報
【0008】
【発明が解決しようとする課題】
上述したアルミニウム合金や銅合金に対する加工硬化或いは時効処理をそのままクロム(Cr)、ジルコニウム(Zr)、ベリリウム(Be)、チタン(Ti)或いはホウ素(B)など添加した時効硬化型の銅合金に対して適用しても、機械的強度と熱的特性及び電気的特性の全てを両立させることができない。
【0009】
即ち、例えば電極材料として要求される熱的特性及び電気的特性を銅合金に発現せしめるには、固溶している添加元素をできるだけ多量に析出する必要がある。そして、多量に析出せしめるには時効温度を高める必要があるが、温度を高めると粒成長が進み機械的特性が低下してしまう。即ち、機械的強度と熱的・電気的特性とはトレードオフの関係にある。
【0010】
【課題を解決するための手段】
上記課題を解決するため、本発明に係る銅合金素材の製造方法は、先ず、溶体化処理によって、母材金属(Cu)にCr(クロム)、ジルコニウム(Zr)、ベリリウム(Be)、チタン(Ti)、ホウ素(B)等の固溶しにくい第2の元素を固溶させ、この後必要に応じて時効処理を施す。歪を与える前の素材としては、溶体化処理したままのものでも所望する性能は得られるが、溶体化処理後に時効を施し、結晶粒子間に第2の元素が析出しているものがより好ましい。
そして、上記の素材に200%以上、好ましくは220%の伸びに相当する歪を与えて結晶の微細化(平均結晶粒径20μm以下)を図るとともに、この歪を与えるのと同時またはその後に時効処理を施して結晶粒子間に前記第2の元素が析出するのを助長せしめる。
【0011】
上記の方法により、スポット溶接、アーク溶接、プラズマ溶接などの電極材料或いは電気自動車に組み込まれるコネクタとして好ましい特性を有する銅合金が得られる。好適な特性としては硬度が30(HRB)以上好ましくは40(HRB)以上、導電率が85(IACS%)以上好ましくは90(IACS%)以上、熱伝導率が350(W/(m・K))以上好ましくは360(W/(m・K))以上である。
硬度が30(HRB)以上であると、電極材料の先端が変形して発熱してしまうことが防止でき、導電率が85(IACS%)以上であると、鋼板と反応してくっついてしまうことを防止でき、熱伝導率が350(W/(m・K))以上であると冷却効率が高まり溶接時の電極材料の溶着を防止できる。
【0012】
前記素材に歪を与える手段としては、押出し、引き抜き、せん断、圧延または鍛造などが考えられる。特に側方押出し場合には、素材温度を400〜1000℃、金型温度を400〜500℃、押出し速度を0.5〜2.0mm/secとすることで、同時に時効処理を施すことも可能になる。
【0013】
【発明の実施の形態】
以下に本発明の実施の形態を添付図面に基づいて説明する。図1は本発明に係る銅合金を得る工程を説明した図であり、先ず、母材(Cu)にCr:0.1〜1.4wt%溶融し、これを急冷してCuにCrが過飽和に固溶した素材を得る。次いでこの素材に200%以上の伸びに相当する歪を与える。尚、素材としては溶体化処理の後に時効処理がなされているものが好ましい。
添加元素がZrの場合は、0.15〜0.5wt%、Beの場合は、0.1〜3.0wt%、Tiの場合は0.1〜6.0wt%、Bの場合は0.01〜0.5wt%、とする。
【0014】
図2はCu管を用いて歪を与える金型を示し、Cu管に上記混合物を充填し、金型温度を400〜500℃とし、押し出し速度を約1mm/secとして、4回繰り返して押し出す(EACE処理)。このようにCrが過飽和に固溶した銅合金素材に歪を与える。この操作で、結晶粒径は200μmが20μm以下となる。
【0015】
ここで、Δe:歪量、ψ:接合内角の1/2、ERR:加工前後の面積比、A0:加工前の断面積、A:加工後の断面積、EAR:加工前後の相当断面積減少率、EE:相当歪(伸び)とすると、以下の関係が成立する。
Δe=2/√3cotanψ
ERR=A0/A=exp(Δe)
EAR=(1−1/ERR)×100
EE=(ERR−1)×100
【0016】
上記の側方押出し(EACE処理)によって結晶組織が微細化する。そして押出し条件が時効処理と重なるため、微細化と同時に第2元素の析出も助長される。
このEACE処理によって得られた銅合金の結晶組織を図3(a)の顕微鏡写真に示す。またEACE処理前の結晶組織を同図(b)の顕微鏡写真に示す。これら顕微鏡写真から、EACE処理によって微細な結晶粒子間に添加元素が析出(写真の黒い点)していることが分る。
【0017】
図4はEACE処理の際の金型温度と硬度との関係を示すグラフ、図5は金型温度と導電率との関係を示すグラフ、図6は金型温度と熱伝導率との関係を示すグラフであり、これらのグラフから本発明にかかる方法によって得られた銅合金は、溶接チップなどの電極材料として要求される特性、即ち、硬度30(HRB)以上、導電率85(IACS%)以上、熱伝導率350(W/(m・K))以上であることが分る。
【0018】
即ち、図4〜6からは、EACE処理を施していない素材(溶体化処理+時効処理)は硬度は高いが、導電率と熱伝導率に劣り、溶体化処理のみを施した素材にEACE処理を施した素材は硬度は低くなるものの、導電率と熱伝導率に優れ、更に溶体化処理後に時効処理を施した素材にEACE処理を施した素材は、硬度、導電率、熱伝導率の全てに優れることが分る。
【0019】
従来のように単に時効処理を行っていたものより、写真からも明らかなように、歪を与えて時効すると、第2の元素が成分中のC、O、B、N等の不純物と反応し、炭化物、酸化物、硼化物、窒化物といった形で析出する。時効析出物が従来より増すことで、成分中の銅以外の元素が減少し、マトリックスは純銅に近い成分となり上記の特性が向上すると考えられる。同様の理由で、硬度が低下する現象も理解できる。
【0020】
図7は本発明に係る方法によって得られた銅合金と従来の銅合金の溶接性をスパッタ発生、張り付きの有無で比較したグラフであり、本発明にかかる銅合金はアルミナ分散銅および時効処理前の銅合金に比較して、適正な電流条件は同等であり、また張り付きが生じない。
【0021】
図8は本発明に係る銅合金と従来の銅合金の溶接性を連続打点数で比較したグラフであり、本発明にかかる銅合金を溶接チップとした場合には、1475打点が可能であった。
【0022】
次に、添加元素としてチタン(Ti)を選定し、上記と同様の方法で銅合金を得た。得られた結果を図9乃至図12に示す。
図9はTi添加量と導電率の関係を示すグラフであり、元々Tiの最大固溶度は8wt%程度とあまり大きくないが、図9から時効処理しても約0.5wt%は固溶状態として残っている。この固溶しているTiが銅合金の導電率を低下させている原因と考えられる。
【0023】
図10は、銅合金を470℃で2時間時効処理した後に、強加工(200%の伸びに相当する歪を付与)した銅合金と時効処理しただけの銅合金の導電率を示すグラフである。このグラフから、強加工した銅合金の導電率が大幅に向上していることが分る。この原因は、強加工によって固溶していたTiが析出したためと考えられる。
【0024】
図11は、強加工した銅合金と時効処理しただけの銅合金の硬度を比較したグラフである。このグラフから、強加工した銅合金の硬度は時効処理しただけの銅合金の硬度よりも低くなっている。これは、固溶強化に寄与していたTiが強加工によって析出したためと考えられる。
【0025】
図12は、硬度、導電率と強加工の温度との関係を示したフラフである。このグラフから、強加工しない場合には導電率に劣り、強加工の温度を上げるに従って硬度は低下するが導電率は向上することが分る。この原因も上記したように固溶強化に寄与していたTiが強加工によって析出したためと考えられる。
【0026】
このように、時効処理では析出せしめることができなかった固溶状態のTiを強加工することを組み合わせることで、固溶しているTiを銅マトリクスから析出せしめることができ、しかも強加工の度合いを制御することで析出するTiの量を制御することができるので、目的に合致した特性の銅合金を作り出すことができる。
【0027】
次に、添加元素としてホウ素(B)を選定し、各種方法で銅合金を製造した。得られた銅合金のホウ素(TiB)と導電率の関係を図13に示す。ここで、銅合金を得る方法として、▲1▼溶体化処理した溶製材を調製、▲2▼銅に化合物(セラミック)としてTiB粉末を添加、▲3▼銅にTi粉末とB粉末を単独で添加する方法を採用した。
図13から、製法として溶製材を選定した場合が最も導電率が高いことが判明した。尚、何れの製法でもTiBの添加割合の増加に伴って導電率は低下し、また強加工を行うことで導電率は向上する。
【0028】
【発明の効果】
以上に説明したように本発明に係る銅合金の製造方法によれば、銅合金の結晶組織を微細した上で、結晶粒子間に添加元素を多量に析出せしめることができるため、従来トレードオフの関係にあった機械的強度と熱的・電気的特性を両立させることができる。
特に、溶接チップなどの電極材料として要求される特性、具体的には硬度30(HRB)以上、導電率85(IACS%)以上、熱伝導率350(W/(m・K))以上の銅合金を得ることができる。
また、電気自動車のコネクタなどの部品としての特性に優れた銅合金をえることができる。
【図面の簡単な説明】
【図1】本発明に係る銅合金の製造方法を説明した図
【図2】EACE処理に用いる金型を説明した図
【図3】(a)は本発明に係る製造方法で得られた銅合金の結晶組織を示す顕微鏡写真
(b)はEACE処理前の結晶組織を示す顕微鏡写真
【図4】金型温度と硬度との関係を示すグラフ
【図5】金型温度と導電率との関係を示すグラフ
【図6】金型温度と熱伝導率との関係を示すグラフ
【図7】本発明に係る製造方法で得られた銅合金と従来の銅合金の溶接性をスパッタ発生、張り付きの有無で比較したグラフ
【図8】本発明に係る製造方法で得られた銅合金と従来の銅合金の溶接性を連続打点数で比較したグラフ
【図9】Ti添加量と導電率の関係を示すグラフ
【図10】強加工した銅合金と時効処理しただけの銅合金の導電率を示すグラフ
【図11】強加工した銅合金と時効処理しただけの銅合金の硬度を比較したグラフ
【図12】硬度、導電率と強加工の温度との関係を示したフラフ
【図13】TiBの添加方法と導電率の関係を示すグラフ
[0001]
TECHNICAL FIELD OF THE INVENTION
The present invention relates to a method for producing a copper alloy suitable for a welding electrode material, a connector material of an electric vehicle, and the like.
[0002]
[Prior art]
As automobiles become EVs (electric vehicles), the amount of connectors used as connecting parts for harnesses and wires tends to increase. In addition, the purpose of EV is to secure safety and fuel efficiency with electronic control technology.
Connectors used in automobiles are used under extreme conditions of high temperature and vibration, and therefore, connection reliability and contact stability are required. Further, as the use of EVs progresses, a copper-based spring material having a small energy loss, that is, a high conductivity is desired.
Further, as for the electrode material for welding, all of mechanical strength, thermal properties and electrical properties are required to be equal to or higher than a predetermined value.
[0003]
As means for improving the mechanical strength of a metal material, miniaturization of the crystal structure is known as Hall-Petch's law.
For example, when a metal or alloy material is deformed, the material strength increases due to work hardening. This is because various defects (point defects, dislocations, stacking faults, etc.) accumulate in the material due to processing (plastic deformation), and as a result of the interaction of these defects, the introduction and movement of new defects becomes difficult. It is understood that it will have resistance.
[0004]
In order to apply plastic deformation (strain) to a metal material, extrusion, drawing, shearing, rolling, forging, and the like have been conventionally performed.
More specifically, the material is thinned by rolling, a high pressure torsion (HPT) method, a CEC (Cyclic Extrusion Compression) method of repeatedly passing through a constricted pipe, and a metal sheet thinned by rolling is cut and stacked. An ARB (Accumulative Roll Bonding) method of performing repetitive rolling is proposed, and specific methods for miniaturization of an aluminum alloy are disclosed in Patent Document 1, Patent Document 2, Patent Document 3, Patent Document 4, and the like. An ECAE method has been proposed in which shear deformation is provided by lateral extrusion without reducing the cross section of a material.
[0005]
On the other hand, for copper alloys, methods disclosed in Patent Literature 5, Patent Literature 6, and the like have been proposed. In this prior art, among copper alloys, dynamic recrystallization by hot extrusion is used to improve the properties (cutting properties and dezincification corrosion) of brass (Cu-Zn) used as a material for faucet fittings and the like. Is caused to obtain a finer crystal and a specific crystal structure ratio (the ratio of α phase, β phase, and γ phase).
[0006]
Also, an age hardening type copper alloy to which an element which does not form a solid solution or hardly forms a solid solution at room temperature, such as chromium (Cr), zirconium (Zr), beryllium (Be), boron (B) and titanium (Ti) is added. In order to bring out the predetermined characteristics, the element is first solid-dissolved at a high temperature by solution treatment, then rapidly cooled to a supersaturated state, and then supersaturated by aging at a predetermined temperature. The additive element in the state is precipitated.
[0007]
[Patent Document]
Patent Document 1: JP-A-9-137244 Patent Document 2: JP-A-10-258334 Patent Document 3: JP-A-11-114618 Patent Document 4: JP-A-2000-271621 Patent Document 5: JP-A-Hei Patent Document 6: JP-A-2000-355746
[Problems to be solved by the invention]
The above-mentioned work hardening or aging treatment for aluminum alloys and copper alloys is directly applied to age hardening type copper alloys added with chromium (Cr), zirconium (Zr), beryllium (Be), titanium (Ti) or boron (B). Even if it is applied, all of the mechanical strength, thermal characteristics and electrical characteristics cannot be compatible.
[0009]
That is, for example, in order to make the copper alloy exhibit the thermal and electrical properties required as an electrode material, it is necessary to deposit as much as possible of the solid solution additive element. It is necessary to raise the aging temperature in order to precipitate a large amount. However, when the temperature is increased, the grain growth proceeds and the mechanical properties are reduced. That is, there is a trade-off relationship between mechanical strength and thermal / electrical characteristics.
[0010]
[Means for Solving the Problems]
In order to solve the above-mentioned problems, a method for producing a copper alloy material according to the present invention comprises: first, a solution treatment is performed to convert a base metal (Cu) into Cr (chromium), zirconium (Zr), beryllium (Be), titanium ( A second element that hardly forms a solid solution, such as Ti) and boron (B), is dissolved, and then aging treatment is performed as necessary. As the material before applying strain, the desired performance can be obtained even after the solution treatment, but it is more preferable that the material is subjected to aging after the solution treatment and the second element is precipitated between crystal grains. .
Then, a strain corresponding to elongation of 200% or more, preferably 220% is given to the above-mentioned material to refine the crystal (average crystal grain size is 20 μm or less), and aging is performed simultaneously with or after applying the strain. A treatment is performed to promote the precipitation of the second element between the crystal grains.
[0011]
According to the above method, a copper alloy having preferable characteristics as an electrode material such as spot welding, arc welding, or plasma welding or a connector incorporated in an electric vehicle can be obtained. Suitable properties are a hardness of 30 (HRB) or more, preferably 40 (HRB) or more, a conductivity of 85 (IACS%) or more, preferably 90 (IACS%) or more, and a thermal conductivity of 350 (W / (m · K). )) Or more, preferably 360 (W / (m · K)) or more.
When the hardness is 30 (HRB) or more, the tip of the electrode material can be prevented from being deformed and generating heat, and when the conductivity is 85 (IACS%) or more, it reacts with the steel sheet and sticks. When the thermal conductivity is 350 (W / (m · K)) or more, the cooling efficiency is increased, and welding of the electrode material during welding can be prevented.
[0012]
Extrusion, drawing, shearing, rolling, forging, and the like can be considered as means for imparting strain to the material. Particularly in the case of lateral extrusion, aging treatment can be performed simultaneously by setting the material temperature to 400 to 1000 ° C, the mold temperature to 400 to 500 ° C, and the extrusion speed to 0.5 to 2.0 mm / sec. become.
[0013]
BEST MODE FOR CARRYING OUT THE INVENTION
Hereinafter, embodiments of the present invention will be described with reference to the accompanying drawings. FIG. 1 is a diagram for explaining a process for obtaining a copper alloy according to the present invention. First, Cr: 0.1 to 1.4 wt% is melted in a base material (Cu), and this is rapidly cooled to supersaturate Cr in Cu. To obtain a solid solution material. Next, a strain corresponding to elongation of 200% or more is given to this material. It is preferable that the material be subjected to an aging treatment after the solution treatment.
When the additive element is Zr, it is 0.15 to 0.5 wt%, when it is Be, it is 0.1 to 3.0 wt%, when it is Ti, it is 0.1 to 6.0 wt%, and when it is B, it is 0.1 to 0.5 wt%. 01 to 0.5 wt%.
[0014]
FIG. 2 shows a mold for giving strain using a Cu tube. The mixture is filled in a Cu tube, the mold temperature is set to 400 to 500 ° C., and the extrusion speed is about 1 mm / sec. EACE processing). Thus, a strain is given to the copper alloy material in which Cr is dissolved in supersaturation. By this operation, the crystal grain size becomes 200 μm or less from 200 μm.
[0015]
Here, Δe: strain amount, Δ: 1 / of the joining inner angle, ERR: area ratio before and after processing, A0: cross-sectional area before processing, A: cross-sectional area after processing, EAR: equivalent cross-sectional area before and after processing Rate, EE: Assuming equivalent strain (elongation), the following relationship is established.
Δe = 2 / {3 cotan}
ERR = A0 / A = exp (Δe)
EAR = (1-1 / ERR) × 100
EE = (ERR-1) × 100
[0016]
The crystal structure is refined by the lateral extrusion (EACE treatment). Since the extrusion conditions overlap with the aging treatment, the precipitation of the second element is promoted simultaneously with the refinement.
The microstructure of the copper alloy obtained by this EACE treatment is shown in the micrograph of FIG. The microstructure before the EACE treatment is shown in the micrograph of FIG. From these micrographs, it can be seen that the added element is precipitated between the fine crystal particles by the EACE treatment (black dots in the photograph).
[0017]
FIG. 4 is a graph showing the relationship between mold temperature and hardness during the EACE process, FIG. 5 is a graph showing the relationship between mold temperature and electrical conductivity, and FIG. 6 is a diagram showing the relationship between mold temperature and thermal conductivity. It is a graph showing that the copper alloy obtained by the method according to the present invention from these graphs has characteristics required for an electrode material such as a welding tip, that is, a hardness of 30 (HRB) or more and a conductivity of 85 (IACS%). As described above, it is understood that the thermal conductivity is 350 (W / (m · K)) or more.
[0018]
That is, from FIGS. 4 to 6, the material not subjected to the EACE treatment (solution treatment + aging treatment) has a high hardness, but is inferior in electric conductivity and thermal conductivity, and the material subjected to only the solution treatment is subjected to the EACE treatment. Although the hardness of the material which has been treated is low, it has excellent electrical conductivity and thermal conductivity, and the material which has been subjected to the aging treatment after the solution treatment has been subjected to the EACE treatment. You can see that it is excellent.
[0019]
As can be seen from the photograph, when aging is performed by applying strain, the second element reacts with impurities such as C, O, B, and N in the components, as is apparent from the photograph, compared to the conventional method in which the aging treatment was simply performed. , Carbides, oxides, borides and nitrides. It is considered that the element other than copper in the component is reduced by increasing the aging precipitate compared to the conventional one, and the matrix becomes a component close to pure copper, and the above-mentioned characteristics are considered to be improved. For the same reason, a phenomenon in which the hardness is reduced can be understood.
[0020]
FIG. 7 is a graph comparing the weldability of the copper alloy obtained by the method according to the present invention and the conventional copper alloy with or without spatter generation and sticking. The copper alloy according to the present invention is alumina-dispersed copper and before aging treatment. The appropriate current conditions are the same as those of the copper alloy, and no sticking occurs.
[0021]
FIG. 8 is a graph comparing the weldability of the copper alloy according to the present invention and the conventional copper alloy by the number of continuous hit points. When the copper alloy according to the present invention was used as a welding tip, 1475 hit points were possible. .
[0022]
Next, titanium (Ti) was selected as an additive element, and a copper alloy was obtained in the same manner as described above. The obtained results are shown in FIGS.
FIG. 9 is a graph showing the relationship between the amount of Ti added and the conductivity. The maximum solid solubility of Ti is not so large as about 8 wt% from the beginning, but from FIG. It remains as a state. This is considered to be the cause of the solid solution of Ti lowering the conductivity of the copper alloy.
[0023]
FIG. 10 is a graph showing the electrical conductivity of a copper alloy that has been subjected to aging treatment at 470 ° C. for 2 hours, and then subjected to heavy working (giving a strain equivalent to 200% elongation) and a copper alloy that has just been subjected to aging treatment. . From this graph, it can be seen that the conductivity of the strongly worked copper alloy has been greatly improved. This is considered to be due to the precipitation of Ti, which was dissolved as a solid solution, by heavy working.
[0024]
FIG. 11 is a graph comparing the hardness of a copper alloy that has been subjected to heavy working and a copper alloy that has only been subjected to aging treatment. From this graph, the hardness of the hardened copper alloy is lower than the hardness of the copper alloy which has just been aged. This is considered to be because Ti that had contributed to solid solution strengthening was precipitated by strong working.
[0025]
FIG. 12 is a fluff showing the relationship between hardness, electrical conductivity, and the temperature of heavy working. From this graph, it can be seen that the conductivity is inferior when the hard working is not performed, and the hardness decreases but the conductivity increases as the temperature of the strong working increases. It is considered that this was also due to the fact that Ti, which contributed to solid solution strengthening as described above, was precipitated by strong working.
[0026]
As described above, the solid solution Ti, which could not be precipitated by the aging treatment, is combined with the strong working, so that the solid solution Ti can be precipitated from the copper matrix. By controlling the amount of Ti, the amount of precipitated Ti can be controlled, so that a copper alloy having characteristics suitable for the purpose can be produced.
[0027]
Next, boron (B) was selected as an additive element, and copper alloys were manufactured by various methods. FIG. 13 shows the relationship between boron (TiB) and conductivity of the obtained copper alloy. Here, as a method of obtaining a copper alloy, (1) a solution-treated ingot is prepared, ( 2 ) TiB 2 powder is added to copper as a compound (ceramic), and (3) Ti powder and B powder are used alone for copper. Was adopted.
From FIG. 13, it was found that the conductivity was highest when an ingot was selected as the manufacturing method. In any of the production methods, the conductivity decreases with an increase in the proportion of TiB added, and the conductivity increases by performing strong working.
[0028]
【The invention's effect】
As described above, according to the method for producing a copper alloy according to the present invention, since the crystal structure of the copper alloy is refined, it is possible to precipitate a large amount of additional elements between crystal grains. The related mechanical strength and thermal / electrical properties can be compatible.
In particular, characteristics required as an electrode material such as a welding tip, specifically, copper having a hardness of 30 (HRB) or more, a conductivity of 85 (IACS%) or more, and a thermal conductivity of 350 (W / (m · K)) or more An alloy can be obtained.
Further, it is possible to obtain a copper alloy having excellent characteristics as a component such as a connector of an electric vehicle.
[Brief description of the drawings]
FIG. 1 is a diagram illustrating a method for producing a copper alloy according to the present invention. FIG. 2 is a diagram illustrating a mold used for an EACE process. FIG. 3A is a diagram illustrating a copper obtained by a method according to the present invention. A micrograph (b) showing the crystal structure of the alloy is a micrograph showing the crystal structure before EACE treatment. [FIG. 4] A graph showing the relationship between mold temperature and hardness. [FIG. 5] The relationship between mold temperature and conductivity. FIG. 6 is a graph showing the relationship between the mold temperature and the thermal conductivity. FIG. 7 is a graph showing the weldability between the copper alloy obtained by the production method according to the present invention and the conventional copper alloy, which shows spatter generation and sticking. FIG. 8 is a graph comparing the weldability of a copper alloy obtained by the production method according to the present invention with a conventional copper alloy by the number of continuous dots. FIG. 9 is a graph showing the relationship between the amount of Ti added and the conductivity. Graph [Figure 10] shows the electrical conductivity of the copper alloy that was subjected to heavy working and the copper alloy that had just been aged. Rough [Fig. 11] A graph comparing the hardness of a hard-worked copper alloy with that of a copper alloy just subjected to aging [Fig. 12] A fluff showing the relationship between hardness, conductivity and the temperature of hard-working [Fig. 13] Graph showing the relationship between the addition method and conductivity

Claims (5)

室温で固溶しないか殆んど固溶しない第2の元素を母材金属(Cu)に固溶させ、この素材に200%以上の伸びに相当する歪を与えて結晶の微細化を図るとともに、この歪を与えるのと同時またはその後に時効処理を施して結晶粒子間に前記第2の元素が析出するのを助長せしめることを特徴とする銅合金素材の製造方法。A second element that does not form a solid solution or hardly forms a solid solution at room temperature is dissolved in a base metal (Cu), and a strain corresponding to elongation of 200% or more is given to this material to achieve crystal refinement. A method for producing a copper alloy material, wherein an aging treatment is performed simultaneously with or after the application of the strain to promote the precipitation of the second element between crystal grains. 請求項1に記載の銅合金素材の製造方法において、前記第2の元素はCr(クロム)、ジルコニウム(Zr)、ベリリウム(Be)、チタン(Ti)、ホウ素(B)のうちの何れかであることを特徴とする銅合金素材の製造方法。2. The method for manufacturing a copper alloy material according to claim 1, wherein the second element is any one of Cr (chromium), zirconium (Zr), beryllium (Be), titanium (Ti), and boron (B). A method for producing a copper alloy material, comprising: 請求項1または請求項2に記載の銅合金素材の製造方法において、前記素材に歪を与える手段は、押出し、引き抜き、せん断、圧延または鍛造のうちの何れかであることを特徴とする銅合金素材の製造方法。3. The method for producing a copper alloy material according to claim 1, wherein the means for giving a strain to the material is any one of extrusion, drawing, shearing, rolling, and forging. Material manufacturing method. 請求項3に記載の銅合金素材の製造方法において、前記押出しの条件は側方押出しとし、金型温度は400〜500℃、押出し速度は0.5〜2.0mm/secとすることを特徴とする銅合金素材の製造方法。4. The method for producing a copper alloy material according to claim 3, wherein the extrusion conditions are lateral extrusion, the mold temperature is 400 to 500 ° C., and the extrusion speed is 0.5 to 2.0 mm / sec. Method for producing copper alloy material. 請求項1乃至請求項4に記載の銅合金素材の製造方法において、前記素材に歪を与える前に予め素材に時効処理を施しておくことを特徴とする銅合金素材の製造方法。The method for manufacturing a copper alloy material according to claim 1, wherein the material is preliminarily subjected to an aging treatment before the material is strained.
JP2003198394A 2002-07-18 2003-07-17 Method for producing copper alloy material Expired - Lifetime JP4014542B2 (en)

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GB0601625A GB2419605B (en) 2002-07-18 2003-07-17 Method of manufacturing composite copper material
PCT/JP2003/009102 WO2004009859A1 (en) 2002-07-18 2003-07-17 Copper alloy, copper alloy producing method, copper complex material, and copper complex material producing method
GB0601624A GB2419604B (en) 2002-07-18 2003-07-17 Method of manufacturing composite copper material
CN03822284A CN100591784C (en) 2002-07-18 2003-07-17 Copper alloy, copper alloy producing method
CA002492925A CA2492925A1 (en) 2002-07-18 2003-07-17 Copper alloy, copper alloy producing method, copper complex material, and copper complex material producing method
JP2003198394A JP4014542B2 (en) 2002-07-18 2003-07-17 Method for producing copper alloy material
CN200910262569A CN101760663A (en) 2002-07-18 2003-07-17 Copper alloy, copper alloy producing method, copper complex material, and copper complex material producing method
US10/521,333 US7544259B2 (en) 2002-07-18 2003-07-17 Copper alloy, copper alloy producing method, copper complex material, and copper complex material producing method
GB0601627A GB2419603B (en) 2002-07-18 2003-07-17 Composite copper material
AU2003252210A AU2003252210A1 (en) 2002-07-18 2003-07-17 Copper alloy, copper alloy producing method, copper complex material, and copper complex material producing method
GB0503149A GB2406579B (en) 2002-07-18 2003-07-17 Copper alloy, method, of manufacturing copper alloy
US12/387,608 US20100021334A1 (en) 2002-07-18 2009-05-05 Method of manufacturing composite copper material

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JP2010007159A (en) * 2008-06-30 2010-01-14 Sumitomo Light Metal Ind Ltd Copper alloy material and electrode member of welding equipment
JP2011529677A (en) * 2008-07-29 2011-12-08 シーメンス アクチエンゲゼルシヤフト A rotor with a superconducting rotor winding and a single sleeve surrounding the rotor winding
JP2012097305A (en) * 2010-10-29 2012-05-24 Jx Nippon Mining & Metals Corp Titanium-copper for electronic component
JP2013209729A (en) * 2012-03-30 2013-10-10 Jx Nippon Mining & Metals Corp Hydrogen permeable copper alloy, hydrogen permeation membrane and steam reformer
US9303300B2 (en) 2005-09-30 2016-04-05 Mitsubishi Shindoh Co., Ltd. Melt-solidified substance, copper alloy for melt-solidification and method of manufacturing the same
US9328401B2 (en) 2004-08-10 2016-05-03 Mitsubishi Shindoh Co., Ltd. Copper alloy casting having excellent machinability, strength, wear resistance and corrosion resistance and method of casting the same

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US9328401B2 (en) 2004-08-10 2016-05-03 Mitsubishi Shindoh Co., Ltd. Copper alloy casting having excellent machinability, strength, wear resistance and corrosion resistance and method of casting the same
US10017841B2 (en) 2004-08-10 2018-07-10 Mitsubishi Shindoh Co., Ltd. Copper alloy casting and method of casting the same
US10570483B2 (en) 2004-08-10 2020-02-25 Mitsubishi Shindoh Co., Ltd. Copper-based alloy casting in which grains are refined
US9303300B2 (en) 2005-09-30 2016-04-05 Mitsubishi Shindoh Co., Ltd. Melt-solidified substance, copper alloy for melt-solidification and method of manufacturing the same
JP2010007159A (en) * 2008-06-30 2010-01-14 Sumitomo Light Metal Ind Ltd Copper alloy material and electrode member of welding equipment
JP2011529677A (en) * 2008-07-29 2011-12-08 シーメンス アクチエンゲゼルシヤフト A rotor with a superconducting rotor winding and a single sleeve surrounding the rotor winding
JP2012097305A (en) * 2010-10-29 2012-05-24 Jx Nippon Mining & Metals Corp Titanium-copper for electronic component
JP2013209729A (en) * 2012-03-30 2013-10-10 Jx Nippon Mining & Metals Corp Hydrogen permeable copper alloy, hydrogen permeation membrane and steam reformer

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