JPH0250184B2 - - Google Patents
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- JPH0250184B2 JPH0250184B2 JP20983987A JP20983987A JPH0250184B2 JP H0250184 B2 JPH0250184 B2 JP H0250184B2 JP 20983987 A JP20983987 A JP 20983987A JP 20983987 A JP20983987 A JP 20983987A JP H0250184 B2 JPH0250184 B2 JP H0250184B2
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- plating
- bending
- alloy
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- spring
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Description
〔産業上の利用分野〕
本発明は、例えば自動車の電気配線等に使用す
る信号用微小電流コネクター材として好適なバネ
性と成形加工性に優れたコネクター用銅基合金に
関する。
〔従来の技術と問題点〕
自動車の電気配線等に使用する信号用微小電流
コネクター材、特にコネクターのメス端子は、バ
ネ性が高く且つ複雑な成形加工が可能なこと、接
点部の接触抵抗を低くするための部分Auメツキ
性に優れること、材料表面の変色防止やハンダ付
性を良好に保つためのSnメツキ処理性等に優れ
ていることが必要である。
しかし、従来において上記の特性を同時に満足
する材料が存在しないため、かような用途に供す
る場合には、バネ特性の良いバネ材料と成形加工
性の良いフレーム材料とを組み合わせて加工を行
なつているのが通常である。そのさい、バネ材と
してはベリリウム銅(C−1720)やCu−9Ni−
6Sn合金等が使用され、フレーム材としては、成
形加工性の良い黄銅(C−2600)或いはCu−
0.1Fe−0.03P合金等が主に使用されていた。
しかし、このような従来技術においては、次の
ような問題があつた。
(1) バネ材の接点部に対しては接触抵抗を下げる
ためにAuメツキを、その他の部分については
耐食性やハンダ付性を考慮してSnメツキを行
なつているが、バネ材として使用される材料
は、プレス成形後に315〜450℃の温度範囲で時
効硬化処理を行つてバネ性を発現させるもので
あり、このため、メツキ処理は、プレス後に行
う後メツキ処理を採用している。このため、プ
レス前にメツキを行う先メツキ処理に比べて製
造コストが大巾に高くなる。
(2) ベリリウム銅は、硬化処理前は成形加工性が
優れているが、価格が高く、これをメス端子部
の一体成形加工品に使用するには不経済であ
る。
(3) バネ部材とフレーム部材を別々の合金で製造
し、最終工程で組み立てる場合には工数が多く
なり加工コストが高くなる。
(4) 自動車の電気配線等に使用するコネクター材
の使用環境が厳しくなり、約150〜200℃の雰囲
気に長時間さらされても接触圧が変化しないこ
とが要求されるようになつたが、従来の2種類
の材料を組み合せて製造したコネクターでは、
この条件を満足できなくなつた。
(5) この組み合わせ品ではスクラツプとして再利
用する場合に分別に費用が嵩み、経済的でな
い。
〔発明の目的〕
本発明の目的とするところは、上記の問題点を
解決し、以下のような特性を備えながらバネ部と
フレーム部を一体成形加工できる経済的なコネク
ター用材料を提供することである。かような材料
に要求される具体的な特性値としては、
導電率:%IACS10〜20の範囲、
バネ限界値:45Kgf/mm2以上、
プレス成形性:90°W曲げ試験(CES−M−0002
−6)で代用し曲げ半径Rと板厚tの比R/t
=1.0で良好な曲げ表面が得られること、
バネが安定した接触圧を維持するか否かの指標と
なる応力緩和特性:200℃×500Hrの雰囲気にさ
らされた後でも応力緩和率が10%以下、
メツキ信頼性:AuメツキやSnメツキ処理後150
℃×500Hrの雰囲気にさらされた後90°W曲げ
試験を行つてもメツキが剥れないこと、
等である。
本発明の目的は、かような諸特性を具備する材
料の開発することにあり、且つこのような特性を
具備したうえで、更に結晶粒度の適正な調整(微
細化)によつて、曲げ加工や絞り加工時の肌荒れ
現象を防止し且つメツキ品の加工時のメツキ剥離
を防止することにある。
〔発明の要旨〕
前記の目的を達成せんとする本発明に係るコネ
クター用材料は、Ni:7〜15wt.%、Al:1.0〜
2.0wt.%、O2:0.0050wt.%以下の基本化学成分
に加え、さらにB:0.01〜0.1wt.%を含有し、残
部がCuおよび不可避的不純物からなるコネクタ
ー用銅基合金である。
〔発明の詳述〕
本発明合金において、Niは強度の向上および
耐食性の向上のために有益に機能する必須の元素
である。特に共添元素のAlと共にNiXAlYの微細
な金属間化合物を形成し、これを銅マトリツクス
中に析出することにより、強度とバネ限界値を向
上させることができる。しかし、Niが15wt%を
越えると導電率の低下およびNi含有量が多くな
るために材料価格が上昇する。また、Niが7%
未満では、Al量を増加させれば強度、バネ限界
値を向上させることはできるが、曲げ加工性が悪
化する。したがつて、本発明の銅基合金において
Niは7〜15wt.%含有させる。
Alは、本発明の銅基合金において強度および
バネ限界値の向上に寄与する必須の元素である。
しかし、2.0wt.%を越えると曲げ加工性が悪くな
り、コネクターの一体形成が不可能となる。また
1.0wt.%未満では、強度およびバネ限界値の向上
が十分には望めないので、1.0/〜2.0wt.%の範囲
でAlを含有させる。
O2は50ppmを超えると合金中でAlと反応して
Al2O3を形成し強度向上のためのAl量が減少す
る。また、組織中にAl2O3が分散することにより
プレス金型の短寿命化の問題がおこる。したがつ
てO2は50ppm未満に規制することが必要である。
このように本発明の銅合金は、Ni:7〜15wt.
%、Al:1.0〜2.0wt.%、O2:0.0050wt.%以下を
基本化学成分として含有させるが、この基本成分
系に対してさらにB:0.01〜0.1wt.%を含有させ
る点に特徴がある。すなわちBは、本発明合金の
溶体化処理時において、結晶粒の粗大化を防止す
る作用を果たす。本発明合金では溶体化処理し、
必要な加工を施した後、時効処理を施すことによ
つて、前述のNi−Al系の金属間化合物を微細に
析出させることによつて所要の特性を発揮するの
であるが、結晶粒を均一微細化することもこれら
の特性を発揮するうえで有利となり、且つ結晶粒
の微細化によつて曲げ加工性や絞り加工時の表面
の肌荒れ現象を防止できると共にメツキ処理後の
曲げ加工時におけるメツキの剥離を防止すること
ができる。また、Bの添加によつて溶体化処理時
の結晶粒の粗大化が抑制されることは、溶体化処
理の処理条件の最適範囲が拡がるので溶体化処理
自身が容易な処理となる。B添加量が0.1wt.%を
超えて含有させてもこのような効果は飽和し経済
的に無駄となるし、また0.01wt.%未満のBの添
加ではこのような効果は少ないので、Bの添加量
は0.01〜0.1wt.%とするのがよい。
以上のような成分組成の本発明に係る銅基合金
からなるコネクター用素材を製造するには、前記
成分組成の鋳片を熱間圧延して熱延板を作り、こ
の熱延板を最終厚みまで冷間圧延して板材とする
のが実際的である。そして、この過程で溶体化処
理を行なうのがよい。溶体化処理は熱延板に対し
て行なうこともできるが、熱延板から数回の冷間
圧延を行なつて板厚減少を行なうさいに冷間圧延
と冷間圧延との間で中間焼鈍を兼ねる溶体化処理
を行なうこともできる。この溶体化処理条件とし
ては、800〜1000℃に1〜120分間の加熱処理、好
ましくは900〜950℃に1〜30分間の条件で加熱処
理を施せばよい。また、時効処理は最終冷間圧延
の後に行なうのがよく、最終製品に加工後に時効
処理を行つてもよい。この時効処理は350〜600℃
に10〜200分間、好ましくは400〜500℃に約30分
間の条件で行なうのがよい。
以下に実施例によつて本発明合金の特徴を具体
的に示す。
例 1
表1にその成分分析値を示す基本成分系の合金
を高周波真空溶解炉にて溶解し、40mm(巾)×40
mm(厚)×150mm(長さ)のインゴツトに鋳造し
た。この鋳塊を面削したあと、900℃に加熱して
均一化処理して熱間圧延を行い、熱延後直ちに急
冷した。ついでこの熱延板を冷間圧延と900℃で
の溶体化処理を繰り返して厚さ0.8mmの板材とし
た。この0.8mm冷延板を900℃で20分間の溶体化処
理後ただちに水冷したうえ、0.4mmまで50%の加
工率で最終冷間圧延し、500℃で30分間の時効処
理を実施した。
得られた各板材から試験片を採取して機械的強
度、伸び、硬度、バネ限界値、導電率および曲げ
加工性を調べた。その結果を表1に併記して示し
た。
なお、機械的強度と伸びの測定はJIS−Z−
2241に、導電率の測定はJIS−H−0505に、硬度
の測定はJIS−Z−2244に、そしてバネ限界値の
測定はJIS−H−3130に従つた。曲げ加工性は
CES−M−0002−6に従つた90°W曲げ試験によ
つて評価した。曲げ半径R=0.4mm、板厚=0.4
mm、R/t=1.0である。表中のG.W.は曲げ軸が
圧延方向に垂直、B.W.は曲げ軸が圧延方向に平
行な場合の試験結果であり、表面状態を観察し、
曲げ表面が良好なものを○、曲げ表面にしわが発
生したものを△、曲げ表面に割れが発生したもの
を×として評価した。
表1の結果に見られるように、本発明の基本成
分系合金のNo.1〜5はいずれも本文に記載したバ
ネ限界値、導電率、曲げ加工性等の目標特性を同
時に満足することが明らかである。これに対して
Alを本発明で規定する量より多量に添加した比
較例No.6やNo.7では、Niが多くても(比較例No.
6)、また少なくても(比較例No.7)曲げ加工性
が悪い。またAl量が本発明で規定する量よりも
少ない比較例8では強度やバネ限界値さらには硬
さも低く、導電率や曲げ加工性も十分ではない。
さらにO2が本発明で規定する量より多い比較例
No.9ではAlが本発明で規定する範囲(Niも本発
明で規定する範囲)でも曲げ加工性が悪くなつて
いる。
[Industrial Application Field] The present invention relates to a copper-based alloy for connectors that has excellent spring properties and moldability and is suitable as a signal microcurrent connector material used, for example, in electrical wiring for automobiles. [Conventional technology and problems] Signal microcurrent connector materials used for automotive electrical wiring, etc., especially the female terminals of the connector, have high springiness and can be processed into complex molding processes. It is necessary to have excellent partial Au plating properties in order to lower the soldering temperature, and excellent Sn plating properties in order to prevent discoloration of the material surface and maintain good solderability. However, there is currently no material that satisfies all of the above characteristics at the same time, so when used for such purposes, a spring material with good spring characteristics and a frame material with good moldability are combined and processed. There is usually one. At that time, beryllium copper (C-1720) and Cu-9Ni- are used as spring materials.
6Sn alloy etc. are used, and the frame material is brass (C-2600) with good moldability or Cu-
0.1Fe−0.03P alloy etc. were mainly used. However, such conventional technology has the following problems. (1) The contact parts of the spring material are plated with Au to reduce contact resistance, and the other parts are plated with Sn in consideration of corrosion resistance and solderability. The material is subjected to age hardening treatment at a temperature range of 315 to 450° C. after press molding to develop spring properties, and for this reason, the plating treatment is a post-plating treatment performed after pressing. For this reason, the manufacturing cost is significantly higher than the tip plating process in which plating is performed before pressing. (2) Beryllium copper has excellent moldability before hardening, but it is expensive and uneconomical to use in integrally molded products for female terminals. (3) If the spring member and frame member are manufactured from different alloys and assembled in the final process, the number of man-hours increases and the processing cost increases. (4) The operating environment for connector materials used in automobile electrical wiring, etc. has become more severe, and it is now required that the contact pressure does not change even when exposed to an atmosphere of about 150 to 200 degrees Celsius for a long time. In conventional connectors manufactured by combining two types of materials,
This condition could no longer be satisfied. (5) This combination product is not economical because the cost of separating it increases when it is reused as scrap. [Object of the Invention] The object of the present invention is to solve the above-mentioned problems and provide an economical material for a connector that has the following characteristics and can integrally mold a spring part and a frame part. It is. Specific characteristic values required for such materials include: Electrical conductivity: %IACS10-20 range, Spring limit value: 45Kgf/mm2 or more , Press formability: 90°W bending test (CES-M- 0002
-6) and the ratio of bending radius R to plate thickness t R/t
= 1.0, a good bending surface can be obtained. Stress relaxation property, which is an indicator of whether or not the spring maintains stable contact pressure: Stress relaxation rate is 10% even after being exposed to an atmosphere of 200℃ x 500 hours. Below, plating reliability: 150 after Au plating and Sn plating processing
The plating does not peel off even after being subjected to a 90°W bending test after being exposed to an atmosphere of ℃ x 500 hours. The purpose of the present invention is to develop a material that has the above-mentioned properties, and furthermore, by appropriately adjusting the crystal grain size (refining), it is possible to bend the material. The object of the present invention is to prevent surface roughness during drawing or drawing processing, and to prevent plating peeling during processing of plated products. [Summary of the Invention] The connector material according to the present invention, which aims to achieve the above object, contains Ni: 7-15 wt.%, Al: 1.0-1.
In addition to the basic chemical components of 2.0 wt.% and O2 : 0.0050 wt.% or less, this is a copper-based alloy for connectors that further contains B: 0.01 to 0.1 wt.%, with the balance consisting of Cu and inevitable impurities. [Detailed Description of the Invention] In the alloy of the present invention, Ni is an essential element that functions beneficially to improve strength and corrosion resistance. In particular, by forming a fine intermetallic compound of Ni x Al Y with the co-added element Al and precipitating this in the copper matrix, the strength and spring limit value can be improved. However, when Ni exceeds 15 wt%, the electrical conductivity decreases and the Ni content increases, leading to an increase in material price. In addition, Ni is 7%
If the Al content is less than that, the strength and spring limit value can be improved by increasing the amount of Al, but the bending workability deteriorates. Therefore, in the copper-based alloy of the present invention
Ni is contained in a range of 7 to 15 wt.%. Al is an essential element that contributes to improving the strength and spring limit value in the copper-based alloy of the present invention.
However, if it exceeds 2.0 wt.%, bending workability deteriorates, making it impossible to form a connector integrally. Also
If it is less than 1.0 wt.%, sufficient improvement in strength and spring limit value cannot be expected, so Al is contained in a range of 1.0/-2.0 wt.%. When O 2 exceeds 50 ppm, it reacts with Al in the alloy.
The amount of Al required to form Al 2 O 3 and improve strength decreases. Furthermore, the dispersion of Al 2 O 3 in the structure causes the problem of shortening the life of the press die. Therefore, it is necessary to regulate O 2 to less than 50 ppm. As described above, the copper alloy of the present invention contains Ni: 7 to 15 wt.
%, Al: 1.0 to 2.0 wt.%, O 2 : 0.0050 wt.% or less as basic chemical components, and the feature is that B: 0.01 to 0.1 wt.% is further included in this basic component system. There is. That is, B functions to prevent coarsening of crystal grains during solution treatment of the alloy of the present invention. The alloy of the present invention is solution-treated,
After the necessary processing, aging treatment is performed to finely precipitate the Ni-Al intermetallic compound mentioned above, thereby achieving the desired characteristics. Refinement is also advantageous in exhibiting these properties, and by making the crystal grains finer, it is possible to improve bending workability and prevent surface roughness during drawing, and it also improves plating during bending after plating. peeling can be prevented. Furthermore, since coarsening of crystal grains during solution treatment is suppressed by the addition of B, the optimum range of treatment conditions for solution treatment is expanded, making the solution treatment itself easier. Even if the amount of B added exceeds 0.1wt.%, this effect will be saturated and it will be economically wasteful, and if the amount of B added is less than 0.01wt.%, this effect will be small. The amount of addition is preferably 0.01 to 0.1 wt.%. In order to manufacture a connector material made of the copper-based alloy according to the present invention having the above-mentioned composition, a slab having the above-mentioned composition is hot-rolled to form a hot-rolled plate, and the hot-rolled plate is It is practical to cold-roll the material to form a plate material. Then, it is preferable to perform solution treatment during this process. Solution treatment can also be applied to hot-rolled sheets, but when cold-rolling a hot-rolled sheet several times to reduce its thickness, intermediate annealing is performed between cold-rolling. It is also possible to perform a solution treatment that also serves as a solution treatment. The solution treatment conditions include heat treatment at 800 to 1000°C for 1 to 120 minutes, preferably heat treatment at 900 to 950°C for 1 to 30 minutes. Further, the aging treatment is preferably performed after the final cold rolling, and the aging treatment may be performed after processing into the final product. This aging treatment is performed at 350-600℃
The temperature is preferably 400 to 500°C for about 30 minutes. The characteristics of the alloy of the present invention will be specifically shown below by way of Examples. Example 1 An alloy with the basic composition shown in Table 1 is melted in a high-frequency vacuum melting furnace, and a 40 mm (width) × 40
It was cast into an ingot of mm (thickness) x 150 mm (length). After face-cutting this ingot, it was heated to 900°C, homogenized, hot-rolled, and immediately after hot-rolling, it was rapidly cooled. This hot-rolled plate was then repeatedly subjected to cold rolling and solution treatment at 900°C to obtain a plate material with a thickness of 0.8 mm. This 0.8 mm cold rolled sheet was solution treated at 900°C for 20 minutes, immediately cooled in water, final cold rolled to 0.4 mm at a processing rate of 50%, and aged at 500°C for 30 minutes. Test pieces were taken from each of the obtained plates and examined for mechanical strength, elongation, hardness, spring limit value, electrical conductivity, and bending workability. The results are also shown in Table 1. In addition, the measurement of mechanical strength and elongation is based on JIS-Z-
2241, conductivity was measured in accordance with JIS-H-0505, hardness was measured in accordance with JIS-Z-2244, and spring limit value was measured in accordance with JIS-H-3130. The bendability is
It was evaluated by a 90°W bending test according to CES-M-0002-6. Bending radius R = 0.4mm, plate thickness = 0.4
mm, R/t=1.0. In the table, GW is the test result when the bending axis is perpendicular to the rolling direction, and BW is the test result when the bending axis is parallel to the rolling direction.
A good bending surface was evaluated as ◯, a case with wrinkles on the bending surface as △, and a case with cracks on the bending surface as ×. As can be seen from the results in Table 1, all of the basic composition alloys No. 1 to 5 of the present invention simultaneously satisfy the target properties such as spring limit value, electrical conductivity, and bending workability described in the text. it is obvious. On the contrary
In Comparative Examples No. 6 and No. 7, in which Al was added in a larger amount than the amount stipulated in the present invention, even if Ni was added (Comparative Example No.
6), and at least (Comparative Example No. 7) the bending workability is poor. Further, in Comparative Example 8, in which the amount of Al is smaller than the amount specified in the present invention, the strength, spring limit value, and hardness are low, and the conductivity and bending workability are also insufficient.
Furthermore, a comparative example in which O 2 is greater than the amount specified in the present invention
In No. 9, the bending workability was poor even though Al was within the range specified by the present invention (Ni was also within the range specified by the present invention).
【表】【table】
【表】
例 2
Ni:11wt.%、Al:1.7wt.%、02:0.0050wt.%
以下で残部がCuおよび不可避的不純物からなる
本発明の基本成分系の銅基合金を高周波溶解炉で
溶解し横型連続鋳造法により10mm(厚)×50mm
(巾)×L(長さ)のインゴツトを鋳造した。得ら
れたインゴツトから例1と同様の方法で0.4mm厚
の板材を製造し、例1と同様にこれを500℃×30
分の時効処理した。そして例1と同様にその特性
値を調べ、その結果を表2に示した。
比較のために、市販のバネ用リン青銅(C−
5210)EH材、およびベリリウム銅(C−1720)
1/4H材で315℃×2.5時間の熱処理を施した材
料についての特性値も併わせて表2に示した。
表2の結果より、本発明の基本成分系の合金は
リン青銅やベリリウム銅より曲げ加工性にすぐれ
ていることがわかる。
次に前記3種の合金の応力緩和特性を調べた。
応力緩和特性試験は、試験片に60Kgf/mm2の最大
曲げ応力が作用するように荷重をかけてわん曲さ
せ、200℃で所定時間(最大500時間まで)保持後
に荷重を解除し、試験片の変形量(%)を測定す
ることにより評価した。その結果を第1図に示し
た。
第1図の結果から明らかなように、リン青銅
(C−5210)EH材が最も応力緩和特性が悪く、
ベリリウム青銅(C−1720)1/4Hの熱処理材
も200℃×100Hr以降では応力緩和率は10%以上
になることがわかる。しかし、本発明の基本成分
系合金は、200℃×500Hr経過後も応力緩和特性
は5%程度であり、このような条件においてバネ
として使用された場合安定した接触圧を示すこと
が明らかである。
また、前記3種の合金のメツキ信頼性試験を行
つた。まず各3種の合金にAuメツキまたはSnメ
ツキ処理を施した。Auメツキは電解脱脂、酸洗
後、銅ストライクメツキを付けた上にワツト浴で
Niメツキをつけ、再度アルカリ脱脂、酸洗を行
つた後、酸性浴でAuメツキを0.2μ厚つけた。Sn
メツキは、電解脱脂、酸洗後、一部のものはCu
下地メツキを施し、もう一方のものはCu下地メ
ツキ無しとして、その上に硫酸浴で無光沢Snメ
ツキを2μ厚つけた。いずれのメツキにおいても
メツキ付性は3種の合金とも良好であつた。
次いで、得られた各メツキ品を150℃×500Hr
の熱処理に供したうえ90°W曲げ試験を行い、曲
げ面のメツキの密着性を調査し、その密着性の良
否を調べた。その結果を表3に示した。
表3の結果に見られるように、本発明の基本成
分系合金は、Cu下地メツキ処理を行つた上にSn
メツキを施したもを除いては密着性は良好であつ
た。Cu下地メツキ付きのSnメツキにおいてはメ
ツキ界面にCuとSnの金属間化合物が生成し、そ
こから剥離したものと推定され、メツキ自身の性
質に由来するものであると考えられる。これに対
して、リン青銅(C−5210)EH材とベリリウム
銅(C−1720)1/4Hの熱処理材はCu下地メツ
キの有無にかかわらずSnメツキはすべて剥離し
た。このように本発明の基本成分系合金のメツキ
性は非常に良好であることが判明した。[Table] Example 2 Ni: 11wt.%, Al: 1.7wt.%, 02 : 0.0050wt.%
Below, the copper-based alloy of the basic composition system of the present invention, the balance of which is Cu and unavoidable impurities, is melted in a high-frequency melting furnace and cast to 10 mm (thickness) x 50 mm by horizontal continuous casting method.
An ingot of (width) x L (length) was cast. A plate with a thickness of 0.4 mm was produced from the obtained ingot in the same manner as in Example 1, and heated at 500°C for 30
Aged for 1 minute. Then, the characteristic values were investigated in the same manner as in Example 1, and the results are shown in Table 2. For comparison, commercially available phosphor bronze for springs (C-
5210) EH material and beryllium copper (C-1720)
Table 2 also shows the characteristic values of the 1/4H material that was heat-treated at 315°C for 2.5 hours. From the results in Table 2, it can be seen that the basic component alloy of the present invention has better bending workability than phosphor bronze or beryllium copper. Next, the stress relaxation properties of the three types of alloys were investigated.
In the stress relaxation property test, a load is applied to the test piece so that a maximum bending stress of 60Kgf/ mm2 acts on it, the test piece is bent, and after being held at 200℃ for a specified period of time (up to 500 hours), the load is released and the test piece is The evaluation was made by measuring the amount of deformation (%). The results are shown in Figure 1. As is clear from the results in Figure 1, phosphor bronze (C-5210) EH material has the worst stress relaxation properties;
It can be seen that the stress relaxation rate of the heat treated material of beryllium bronze (C-1720) 1/4H becomes 10% or more after 200°C x 100 hours. However, the basic composition alloy of the present invention has stress relaxation properties of about 5% even after 500 hours at 200°C, and it is clear that it exhibits stable contact pressure when used as a spring under such conditions. . In addition, a plating reliability test was conducted on the three types of alloys. First, each of the three types of alloys was subjected to Au plating or Sn plating treatment. Au plating is electrolytically degreased and pickled, then copper strike plating is applied and a wax bath is applied.
After applying Ni plating, alkaline degreasing and pickling again, Au plating was applied to a thickness of 0.2μ in an acid bath. Sn
After electrolytic degreasing and pickling, some are made of Cu.
One was plated with a base plating, and the other was without a Cu base plating, and a 2μ thick matte Sn plating was applied on top of it in a sulfuric acid bath. In all cases of plating, the plating properties of the three alloys were good. Next, each plated product obtained was heated at 150℃×500Hr.
After being subjected to heat treatment, a 90°W bending test was conducted to investigate the adhesion of the plating on the bent surface, and to determine whether the adhesion was good or bad. The results are shown in Table 3. As seen in the results in Table 3, the basic composition alloy of the present invention has been subjected to Cu underplating treatment and Sn
Adhesion was good except for those that were plated. In the case of Sn plating with a Cu base plating, an intermetallic compound of Cu and Sn was formed at the plating interface, and it is presumed that the intermetallic compound was peeled from there, and this is thought to be due to the properties of the plating itself. On the other hand, the Sn plating of the heat-treated phosphor bronze (C-5210) EH material and beryllium copper (C-1720) 1/4H material was completely peeled off regardless of the presence or absence of the Cu base plating. As described above, it has been found that the basic component alloy of the present invention has very good plating properties.
【表】【table】
【表】【table】
【表】
例 3
表4にその成分分析値を示すように、基本成分
系合金に対して適量のBを添加した合金を高周波
真空溶解炉にて溶解し、40mm(巾)×40mm(厚)×
150mm(長さ)のインゴツトに鋳造した。この鋳
塊を面削したあと、900℃に加熱して均一化処理
して熱間圧延を行い、熱延後直ちに急冷した。つ
いでこの熱延板を冷間圧延と900℃での溶体化処
理を繰り返して厚さ0.6mmの板材とした。
得られた0.6mmの冷延材から試験片を採取して
900℃×60分間の溶体化処理後ただちに水冷し、
各合金の硬度と結晶粒径を測定した。その結果を
表5に示した。
また、溶体化処理後の前記試験片を0.3mmまで
50%の加工率で冷間圧延し、500℃で30分間の時
効処理を実施し、得られた試料の曲げ加工性を調
べた。その結果も表5に併記した。曲げ加工性は
CES−M−0002−6に従つた90°W曲げ試験によ
つて評価した。曲げ半径R=0.3mm、板厚=0.3
mm、R/t=1.0である。表中のG.W.は曲げ軸が
圧延方向に垂直、B.W.は曲げ軸が圧延方向に平
行な場合の試験結果であり、表面状態を観察し、
曲げ表面が良好なものを○、曲げ表面にしわが発
生したものを△、曲げ表面に割れが発生したもの
を×として評価した。
表5の結果に見られるように、Bを添加した本
発明合金は、B添加量が増加するに従つて溶体化
処理後の硬度が高くなり且つ結晶粒径が小さくな
つていることがわかる。また、時効処理後の曲げ
加工性も、Bを添加して結晶粒度が微細なものは
これにともなつて良好となることがわかる。なお
No.13の比較合金は、溶体化処理工程の時間が過剰
の為、結晶粒径が大きく成長し曲げ加工性が劣化
したものである。[Table] Example 3 As shown in Table 4, an alloy with an appropriate amount of B added to the basic composition alloy was melted in a high-frequency vacuum melting furnace, and the resulting material was 40 mm (width) x 40 mm (thickness). ×
Cast into a 150mm (length) ingot. After face-cutting this ingot, it was heated to 900°C, homogenized, hot-rolled, and immediately after hot-rolling, it was rapidly cooled. This hot-rolled plate was then repeatedly subjected to cold rolling and solution treatment at 900°C to obtain a plate material with a thickness of 0.6 mm. A test piece was taken from the obtained 0.6 mm cold-rolled material.
After solution treatment at 900℃ for 60 minutes, immediately cool with water.
The hardness and grain size of each alloy were measured. The results are shown in Table 5. In addition, the test piece after solution treatment can be made up to 0.3 mm.
The samples were cold rolled at a processing rate of 50% and aged at 500°C for 30 minutes, and the bending workability of the obtained samples was investigated. The results are also listed in Table 5. The bendability is
It was evaluated by a 90°W bending test according to CES-M-0002-6. Bending radius R = 0.3mm, plate thickness = 0.3
mm, R/t=1.0. In the table, GW is the test result when the bending axis is perpendicular to the rolling direction, and BW is the test result when the bending axis is parallel to the rolling direction.
A good bending surface was evaluated as ◯, a case with wrinkles on the bending surface as △, and a case with cracks on the bending surface as ×. As seen in the results in Table 5, it can be seen that in the alloys of the present invention to which B is added, as the amount of B added increases, the hardness after solution treatment increases and the grain size decreases. Furthermore, it can be seen that the bending workability after aging treatment also becomes better when B is added and the crystal grain size is fine. In addition
Comparative alloy No. 13 had excessive time in the solution treatment process, so the crystal grain size grew large and the bending workability deteriorated.
【表】【table】
【表】
硬度および結晶粒径:溶体化処理後
曲げ加工性:時効処理後
以上の実施例から明らかなように、本発明合金
はコネクター用材料特に従来の自動車の微小電流
用コネクター材に要求される導電率やバネ限界値
を満たしながら優れた曲げ加工性を有しており、
従つて本発明によるとバネ部とフレーム部を一体
成形加工できる点で従来材(2ピース材)にはな
い有利な面を有するコネクター用材料を提供でき
る。またベリリウム銅合金のように高価元素を含
有しないでそれ以上の応力緩和特性を発現し得た
点で経済的にも特性的にも格段のものがあると共
にメツキ信頼性も十分なものであり、そのコネク
ターの使用環境を200℃まで引き上げることにも
成功したものであるから、このコネクター用材料
分野に安価な新規材料を提供するものである。[Table] Hardness and grain size: After solution treatment Bending workability: After aging treatment As is clear from the above examples, the alloy of the present invention is required for connector materials, especially conventional connector materials for microcurrents in automobiles. It has excellent bending workability while meeting the electrical conductivity and spring limit values.
Therefore, according to the present invention, it is possible to provide a material for a connector which has an advantage over conventional materials (two-piece materials) in that the spring portion and the frame portion can be integrally molded. Furthermore, unlike beryllium-copper alloys, it does not contain expensive elements and exhibits stress relaxation properties superior to those of other alloys, so it is economically and economically superior in terms of properties, and it also has sufficient plating reliability. Since we have succeeded in increasing the operating environment of the connector to 200°C, we will provide a new, inexpensive material for the field of connector materials.
第1図は、本発明の基本成分系合金と公知合金
の200℃×500時間までの応力緩和率の変化を示す
図である。
FIG. 1 is a diagram showing changes in stress relaxation rates of the basic composition alloy of the present invention and a known alloy at 200° C. for 500 hours.
Claims (1)
0.0050wt.%以下の基本化学成分に加え、さらに
B:0.01〜0.1wt.%を含有し、残部がCuおよび不
可避的不純物からなるコネクター用銅基合金。1 Ni: 7-15wt.%, Al: 1.0-2.0wt.%, O2 :
A copper-based alloy for connectors containing 0.01 to 0.1 wt.% of B in addition to 0.0050 wt.% or less of basic chemical components, with the remainder consisting of Cu and inevitable impurities.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP20983987A JPS6452035A (en) | 1987-08-24 | 1987-08-24 | Copper-base alloy for connector |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP20983987A JPS6452035A (en) | 1987-08-24 | 1987-08-24 | Copper-base alloy for connector |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6452035A JPS6452035A (en) | 1989-02-28 |
| JPH0250184B2 true JPH0250184B2 (en) | 1990-11-01 |
Family
ID=16579471
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP20983987A Granted JPS6452035A (en) | 1987-08-24 | 1987-08-24 | Copper-base alloy for connector |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6452035A (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2594249B2 (en) * | 1992-05-06 | 1997-03-26 | 同和鉱業株式会社 | Copper base alloy for connector and method of manufacturing the same |
| JP2594250B2 (en) * | 1992-05-13 | 1997-03-26 | 同和鉱業株式会社 | Copper base alloy for connector and method of manufacturing the same |
| JP2743342B2 (en) * | 1992-05-21 | 1998-04-22 | 同和鉱業株式会社 | Copper base alloy for connector and method of manufacturing the same |
| JP7126359B2 (en) * | 2018-02-28 | 2022-08-26 | 株式会社神戸製鋼所 | Copper alloy materials and terminals with excellent contact corrosion resistance to aluminum |
-
1987
- 1987-08-24 JP JP20983987A patent/JPS6452035A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6452035A (en) | 1989-02-28 |
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