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JPH0123526B2 - - Google Patents
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JPH0123526B2 - - Google Patents

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Publication number
JPH0123526B2
JPH0123526B2 JP5514787A JP5514787A JPH0123526B2 JP H0123526 B2 JPH0123526 B2 JP H0123526B2 JP 5514787 A JP5514787 A JP 5514787A JP 5514787 A JP5514787 A JP 5514787A JP H0123526 B2 JPH0123526 B2 JP H0123526B2
Authority
JP
Japan
Prior art keywords
annealing
formability
aging
solution treatment
treatment
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
Application number
JP5514787A
Other languages
Japanese (ja)
Other versions
JPS63223151A (en
Inventor
Yosuke Matsui
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
NGK Insulators Ltd
Original Assignee
NGK Insulators Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by NGK Insulators Ltd filed Critical NGK Insulators Ltd
Priority to JP5514787A priority Critical patent/JPS63223151A/en
Priority to EP88301618A priority patent/EP0282204B1/en
Priority to DE19883884239 priority patent/DE3884239T2/en
Publication of JPS63223151A publication Critical patent/JPS63223151A/en
Publication of JPH0123526B2 publication Critical patent/JPH0123526B2/ja
Granted legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/08Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of copper or alloys based thereon

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  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Conductive Materials (AREA)
  • Heat Treatment Of Steel (AREA)
  • Metal Rolling (AREA)

Description

【発明の詳細な説明】[Detailed description of the invention]

(産業上の利用分野) 本発明はベリリウム銅合金材料よりなる部品成
形体の製造技術に関するものである。 (従来の技術) ベリリウム銅合金は、高強度および高導電性を
有する優れた素材として、コネクター、リレー等
の多くの製品に広く用いられている。そして、近
年では製品の小型化が益々要求されるに至つてい
るので、ベリリウム銅合金材料にも厳しい加工に
十分に耐えられる成形性が求められているのが現
状である。 従来より、部品成形体として加工するベリリウ
ム銅合金の圧延板は、原料の鋳造および熱間圧延
後に冷間圧延および焼鈍を繰返して施し、引続い
て溶体化処理を行つてから冷間圧延して製造する
のが普通である。さらに、ベリリウム銅合金の上
記圧延板は、次のいずれかの態様で所要の部品成
形体に加工されるものである。 第1の態様は、ベリリウム銅合金の上記圧延板
に引続いて時効硬化処理を行ない、いわゆるミル
ハードン材としてユーザに引渡し、ユーザ側の工
場で曲げを含む加工によつて所要の部品形状に成
形するものである。この場合、得られた成形体は
多くの場合にはそのまま部品として製品に組込む
ことになる。 第2の態様は、ベリリウム銅合金の上記圧延板
をそのままユーザに引渡し、前記同様にユーザ側
の工場で所要の部品形状に成形した後、ユーザ側
の工場で又は素材の製造工場に戻して時効硬化処
理を行ない、所要の強度を有する部品として完成
させるものである。 いずれの場合においても溶体化処理に引続いて
行なわれる冷間圧延板処理は、材料特性に大きな
影響を及ぼす因子であつて、製品強度の向上、時
効後の変形防止および時効析出の促進等を意図す
るものである。 (発明が解決しようとする問題点) 上述のごとく溶体化処理に引続いて冷間圧延処
理を施すにあたり、圧下率を高目に設定すると圧
延方向と平行な曲げ軸線を中心とする圧延板の
90゜方向曲げ特性が劣化し、時効硬化に先立つて
所要の部品形状に成形する場合であつても成形の
自由度が著しく損なわれるものである。それ故
に、特に顕著な加工硬化傾向を呈する材料では圧
下率60%以上の冷間圧延は通常は行なわれていな
い。換言すれば、溶体化処理前に行なわれる冷間
圧延および焼鈍の繰返しの回数を大とせざるを得
ず、製造コストの低減が困難となるものである。 他方、ミルハードン材として時効硬化処理を施
した材料は、時効後の強度が高いものほど伸びが
減少し、成形性が劣化するために部品形状への成
形、特に曲げ加工の自由度が著しく損なわれるこ
とになる。そして、所要の成形性を確保するため
にはベリリウム銅合金の本来的機能である高強度
を犠牲にせざるを得なかつたのである。 (発明が解決しようとする問題点) 本発明の目的は、圧下率20%以上の冷間加工を
施すことによつて成形性の劣化した材料を、部品
の加工成形時に曲率半径の小さな曲げ加工に耐え
るように改善することのできるベリリウム銅合金
材料を、所要の部品形状に加工した後、時効処理
によつて容易に最高強度を実現可能とすることに
ある。 (問題点を解決するための手段) この目的を達成するために本発明は、Be:0.2
〜0.8wt%、並びにNi及び/又はCo:0.3〜4.0wt
%を含み、残部が実質的にCuよりなるBe―Cu合
金の圧延板に溶体化処理を施した後、圧下率20%
以上の冷間加工を行ない、引続いて250℃〜550℃
の温度下で焼鈍を行なうことによりBe―Cu合金
材料の成形性を回復させ、かくして得られたBe
―Cu合金材料を、曲げを含む加工によつて所要
の部品形状に成形した後、350℃〜550℃の温度下
で時効させて所要の製品強度を達成するものであ
る。 第1図は前述した従来技術と本発明とを対比し
て示す製造工程のフローチヤートである。従来技
術においてはベリリウム銅合金の溶体化処理後の
冷間圧延板そのものにつき、所要の成形加工を行
なつてから時効硬化処理を施し、または先に時効
硬化処理を施して得られたミルハードン材に所要
の成形処理を行つて製品としている。かかる製造
プロセスが種々の問題点を伴うものであること
は、前述したとおりである。 これに対して、本発明においては、溶体化処理
後の冷間圧延に引続いて所定の温度下で焼鈍を行
なうことにより加工歪みの一部を解放して成形性
の回復を図り、成形性に優れたベリリウム銅合金
材料を、所要の部品形状に成形した後、時効硬化
処理を施すことにより所要の高強度を有する製品
を製造することが可能となるものである。 (作用および限定理由) 本発明においては、前述したとおり、Be:0.2
〜0.8wt%、並びにNi及び/又はCo:0.3〜4.0wt
%を含み、残部が実質的にCuよりなるBe―Cu合
金を用いている。各成分の限定理由は、次のとお
りである。 先ず、Beの添加量が0.2wt%未満の場合におい
ては十分な析出硬化が達成されず、また、0.8wt
%を越えると添加量の増加に応じた強度の向上が
認められなくなることを確認したので、Beの添
加量を0.2〜0.8wt%と限定したものである。 次に、Ni及び/又はCoの添加量も0.3wt%未満
であれば十分な析出硬化が達成されず、また、
4.0wt%を越える場合には成形性が劣化すること
を確認したので、Ni及び/又はCoの添加量を0.3
〜4.0wt%としたものである。 本発明において、上述のごとき組成のBe―Cu
合金の圧延板に、その溶体化処理後に施す冷間加
工の圧下率を20%以上とするのは、次の理由によ
るものである。すなわち、圧下率が20%未満であ
れば成形性がさほど劣化せず、あえて焼鈍によつ
て成形性を回復させる必要性が認められず、他
方、圧下率を高目に設定するほど、溶体化処理前
の冷間加工および焼鈍の繰返しの回数を減少する
ことが可能となるからでもある。 また、本発明において、溶体化処理後の冷間圧
延と、所要の部品形状への成形との間に行なう焼
鈍の温度範囲を250℃〜550℃とする理由は、250
℃未満の場合には成形性を十分に回復させること
ができず、550℃を超えると過時効状態となり、
加工成形後の時効硬化処理によつて十分な強度を
得ることができなくなるからである。 さらに、本発明において、所定の部品形状への
成形後に行なう時効硬化処理の温度範囲を350℃
〜500℃とする理由は、350℃未満では析出硬化が
得られず、500℃を超える場合には導電率は向上
するものの、過時効状態となり、十分な強度が得
られなくなるからである。 (実施例) 本発明の実施例(1)〜(16)および比較例(17)
〜(24)における成分組成、製造条件および機械
的特性は、第1表に示すとおりである。
(Industrial Application Field) The present invention relates to a technology for manufacturing a molded part made of a beryllium copper alloy material. (Prior Art) Beryllium copper alloy is an excellent material having high strength and high conductivity, and is widely used in many products such as connectors and relays. In recent years, there has been an increasing demand for smaller products, and therefore beryllium-copper alloy materials are also required to have formability sufficient to withstand severe processing. Conventionally, rolled plates of beryllium copper alloys processed into molded parts have been repeatedly cold rolled and annealed after casting and hot rolling of raw materials, followed by solution treatment and then cold rolling. It is common to manufacture Furthermore, the above-mentioned rolled plate of beryllium copper alloy is processed into a required part molded body in one of the following ways. In the first aspect, the rolled sheet of beryllium copper alloy is subsequently subjected to age hardening treatment, delivered to the user as a so-called mill-hardened material, and formed into the required part shape by processing including bending at the user's factory. It is something. In this case, the obtained molded body is often incorporated into a product as a part as it is. The second aspect is to deliver the rolled sheet of beryllium copper alloy to the user as is, form it into the required part shape at the user's factory in the same way as above, and then return it to the user's factory or the material manufacturing factory for aging. A hardening process is performed to complete the part as having the required strength. In either case, the cold-rolled sheet treatment that follows the solution treatment is a factor that has a large effect on the material properties, and is responsible for improving product strength, preventing deformation after aging, and promoting aging precipitation. It is intended. (Problems to be Solved by the Invention) As mentioned above, when performing cold rolling treatment following solution treatment, if the reduction rate is set to a high value, the rolled plate centering on the bending axis parallel to the rolling direction will
The bending properties in the 90° direction deteriorate, and even when molding into a desired part shape prior to age hardening, the degree of freedom in molding is significantly impaired. Therefore, cold rolling at a reduction rate of 60% or more is not normally performed for materials exhibiting a particularly marked tendency to work hardening. In other words, the number of repetitions of cold rolling and annealing performed before solution treatment must be increased, making it difficult to reduce manufacturing costs. On the other hand, for materials subjected to age-hardening treatment as mill-hardened materials, the higher the strength after aging, the lower the elongation and the worse the formability, which significantly impairs the freedom of forming into part shapes, especially bending. It turns out. In order to secure the required formability, it was necessary to sacrifice the high strength that is the original function of beryllium-copper alloys. (Problems to be Solved by the Invention) The purpose of the present invention is to bend a material whose formability has deteriorated due to cold working at a reduction rate of 20% or more to a small radius of curvature during processing and forming of parts. The object of the present invention is to make it possible to easily achieve maximum strength by aging a beryllium-copper alloy material that can be improved to withstand stress after being processed into a desired part shape. (Means for solving the problem) To achieve this objective, the present invention provides Be: 0.2
~0.8wt%, and Ni and/or Co: 0.3~4.0wt
After applying solution treatment to a rolled sheet of Be-Cu alloy containing % and the remainder being substantially Cu, the rolling reduction rate is 20%.
After the above cold working, the temperature is 250℃~550℃.
The formability of the Be-Cu alloy material is restored by annealing at a temperature of
- Cu alloy material is formed into the required part shape through processing including bending, and then aged at a temperature of 350℃ to 550℃ to achieve the required product strength. FIG. 1 is a flowchart of a manufacturing process comparing the prior art described above and the present invention. In the conventional technology, the cold-rolled plate itself after solution treatment of beryllium copper alloy is subjected to the required forming processing and then subjected to age hardening treatment, or the mill-hardened material obtained by applying age hardening treatment first is used. The product is made by performing the necessary molding processing. As mentioned above, such a manufacturing process is accompanied by various problems. In contrast, in the present invention, cold rolling after solution treatment is followed by annealing at a predetermined temperature to release part of the processing strain and restore formability. By molding a beryllium copper alloy material with excellent properties into a desired part shape and then subjecting it to an age hardening treatment, it is possible to manufacture a product with the desired high strength. (Operation and Reason for Limitation) In the present invention, as described above, Be: 0.2
~0.8wt%, and Ni and/or Co: 0.3~4.0wt
% and the remainder is substantially Cu. The reasons for limiting each component are as follows. First, if the amount of Be added is less than 0.2wt%, sufficient precipitation hardening cannot be achieved;
It was confirmed that if the amount of Be added exceeds 0.2 to 0.8 wt%, the strength could not be improved in accordance with the increase in the amount of Be added. Next, if the amount of Ni and/or Co added is less than 0.3wt%, sufficient precipitation hardening will not be achieved;
It was confirmed that formability deteriorates when the amount exceeds 4.0wt%, so the amount of Ni and/or Co added was reduced to 0.3%.
~4.0wt%. In the present invention, Be--Cu having the composition as described above is used.
The reason why the rolling reduction ratio of cold working applied to a rolled alloy plate after solution treatment is set to 20% or more is as follows. In other words, if the rolling reduction is less than 20%, the formability will not deteriorate significantly, and there is no need to recover the formability through annealing.On the other hand, the higher the rolling reduction, the more the solution This is also because it becomes possible to reduce the number of repetitions of cold working and annealing before treatment. In addition, in the present invention, the reason why the temperature range of annealing performed between cold rolling after solution treatment and forming into the required part shape is set to 250 ° C to 550 ° C.
If the temperature is below ℃, the formability cannot be recovered sufficiently, and if it exceeds 550℃, it will become over-aged.
This is because sufficient strength cannot be obtained by age hardening treatment after processing and forming. Furthermore, in the present invention, the temperature range of the age hardening treatment performed after molding into a predetermined part shape is 350°C.
The reason for setting the temperature to 500°C is that precipitation hardening cannot be obtained at temperatures below 350°C, while electrical conductivity improves when the temperature exceeds 500°C, but an over-aged state occurs and sufficient strength cannot be obtained. (Example) Examples (1) to (16) of the present invention and comparative example (17)
The component compositions, manufacturing conditions, and mechanical properties of (24) are as shown in Table 1.

【表】 第1表に記載した試料(1)〜(24)は、いずれも
第1図に示したプロセスにおける溶体化処理まで
を既知の態様で施した後、それぞれの異なる製造
条件下で作成したものである。 第1表において、成形性は、時効硬化処理前の
Be―Cu合金の圧延板につき、圧延方向と平行な
曲げ軸線を中心として180℃曲げを加えた後、曲
げ部における割れの有無に基づいて安全曲げ半径
Rを定め、その値を板厚tで除したR/t値を用
いており、値が小さいほど曲率半径の小さな曲げ
加工を含むより厳しい成形加工に耐えうるもので
あることを表している。 第1表から明らかなとおり、本発明の実施例に
よる試料(1)〜(16)はいずれも優れた成形性およ
び強度(JIS Z2241に準じて求めた時効硬化後の
0.2%耐力)を有している。比較例の試料につい
て説明すると、比較例試料(17),(19),(21)は
実施例試料(5)〜(8)と、また比較例試料(18),
(20),(22)は実施例試料(10),(11)と、それぞれ
同一組成のものである。 比較例試料(17),(18)は冷間加工の圧下率を
低く設定したものである。すなわち、圧下率15%
の場合には焼鈍を行なわなくても良好な成形性が
得られるが、時効後の0.2%耐力値は同一組成の
実施例試料による値よりも低いことが明らかであ
る。 比較例試料(19)は高温で焼鈍を行なつたもの
であるために析出核が粗大化し、時効後の0.2%
耐力値が低下したものであり、試料(20)は低温
で焼鈍を行なつたものであるために焼鈍後の成形
性の回復が不十分である。 比較例試料(21)は高温で時効処理を行なつた
ために過時効状態となり、また試料(22)は低温
で時効処理を行なつたために未時効状態となり、
いずれも0.2%耐力値が低下している。 さらに、比較例試料(23)はベリリウムの、ま
た試料(24)はコバルトの含有量がそれぞれ少な
すぎるために十分な強度が得られていないもので
ある。 次に、第2表は、上述した実施例試料(10),(11)
と同一組成の試料に圧下率20〜90%で冷間加工を
施し、引続いて400℃で焼鈍を行なつた後の成形
性と、さらに400℃で時効処理を行なつた後の0.2
%耐力値とを示すものである。
[Table] Samples (1) to (24) listed in Table 1 were prepared under different manufacturing conditions after being subjected to the solution treatment in the process shown in Figure 1 in a known manner. This is what I did. In Table 1, formability is shown before age hardening treatment.
After bending a rolled sheet of Be-Cu alloy at 180°C around the bending axis parallel to the rolling direction, the safe bending radius R is determined based on the presence or absence of cracks at the bent part, and this value is determined by the sheet thickness t. The smaller the value, the more severe the forming process including bending process with a small radius of curvature can be withstood. As is clear from Table 1, samples (1) to (16) according to the examples of the present invention all had excellent formability and strength (after age hardening determined according to JIS Z2241).
0.2% yield strength). To explain the comparative example samples, comparative example samples (17), (19), and (21) are the same as the example samples (5) to (8), and the comparative example samples (18),
Samples (20) and (22) have the same composition as Example samples (10) and (11), respectively. Comparative example samples (17) and (18) have a low rolling reduction ratio during cold working. In other words, the reduction rate is 15%
In the case of , good formability can be obtained without annealing, but it is clear that the 0.2% proof stress value after aging is lower than the value of the example sample with the same composition. Comparative example sample (19) was annealed at a high temperature, so the precipitate nuclei became coarser, and after aging it was 0.2%
The yield strength value has decreased, and since sample (20) was annealed at a low temperature, the recovery of formability after annealing is insufficient. Comparative example sample (21) was aged at a high temperature, resulting in an overaged state, and sample (22) was aged at a low temperature, resulting in an unaged state.
In both cases, the yield strength value decreased by 0.2%. Furthermore, Comparative Example Sample (23) and Sample (24) contain too little beryllium and cobalt, respectively, so that sufficient strength cannot be obtained. Next, Table 2 shows the example samples (10) and (11) mentioned above.
Formability after cold working a sample with the same composition as 20% to 90%, followed by annealing at 400℃, and 0.2 after aging treatment at 400℃.
% proof stress value.

【表】【table】

【表】 第2表から明らかなとおり、冷間加工の圧下率
の増加に伴つて成形性が劣化するが、本発明によ
つて焼鈍を施すことにより実用性の高いR/t値
まで回復している。 (発明の効果) 本発明によれば、溶体化処理後の冷間加工に際
しての圧下率を高く設定することによつて時効後
の強度の向上、変形の防止等を効果的に達成する
と共に、圧下率が高い場合に従来は不可避的と考
えられていた成形性の劣化を所定温度下での焼鈍
によつて的確に防止することが可能となる利点が
得られるものである。 また、溶体化処理後の冷間加工の圧下率を高め
ることにより、例えば圧下率を80%とすれば最終
製品板厚が0.2mmである場合に板厚1.0mmの状態で
溶体化処理を行なうことが可能となり、従来のご
とく低圧下率で冷間加工を行なう場合と対比して
溶体化処理前の圧延および焼鈍の繰返し回数を減
少しうる等の経済的利点も得られるのである。 さらには、焼鈍を拘束状態で行なうことによつ
て材料形状が矯正され、同時に時効析出もある程
度促進されるため、部品形状への成形後の時効処
理時に生じる収縮変形を効果的に防止することも
可能となるものである。
[Table] As is clear from Table 2, formability deteriorates as the rolling reduction during cold working increases, but by annealing according to the present invention, it recovers to a highly practical R/t value. ing. (Effects of the Invention) According to the present invention, by setting a high rolling reduction rate during cold working after solution treatment, it is possible to effectively improve strength after aging, prevent deformation, etc. This provides the advantage that deterioration in formability, which was conventionally thought to be unavoidable when the reduction rate is high, can be accurately prevented by annealing at a predetermined temperature. In addition, by increasing the reduction rate during cold working after solution treatment, for example, if the reduction rate is 80%, if the final product plate thickness is 0.2 mm, solution treatment will be performed with the plate thickness being 1.0 mm. This makes it possible to achieve economical advantages such as the ability to reduce the number of repetitions of rolling and annealing before solution treatment compared to conventional cold working at a low reduction rate. Furthermore, by performing annealing in a restrained state, the material shape is corrected and at the same time aging precipitation is promoted to some extent, so shrinkage deformation that occurs during aging treatment after forming into a part shape can be effectively prevented. It is possible.

【図面の簡単な説明】[Brief explanation of drawings]

第1図は本発明の製造方法における各工程を従
来技術と対比して示すフローチヤートである。
FIG. 1 is a flowchart showing each step in the manufacturing method of the present invention in comparison with the prior art.

Claims (1)

【特許請求の範囲】 1 Be:0.2〜0.8wt%、並びにNi及び/又は
Co:0.3〜4.0wt%を含み、残部が実質的にCuよ
りなるBe―Cu合金の圧延板に溶体化処理を施し
た後、圧下率20%以上の冷間加工を行ない、引続
いて250℃〜550℃の温度下で焼鈍を行なうことに
より得られたBe―Cu合金材料を、さらに曲げを
含む加工によつて所要の部品形状に成形した後、
350℃〜500℃の温度下で時効させて得られたもの
であることを特徴とする、ベリリウム銅合金材料
よりなる部品成形体。 2 Be:0.2〜0.8wt%、並びにNi及び/又は
Co:0.3〜4.0wt%を含み、残部が実質的にCuよ
りなるBe―Cu合金の圧延板に溶体化処理を施し
た後、圧下率20%以上の冷間加工を行ない、引続
いて250℃〜550℃の温度下で焼鈍を行なうことに
より得られたBe―Cu合金材料を、さらに曲げを
含む加工によつて所要の部品形状に成形した後、
350℃〜500℃の温度下で時効させることを特徴と
する、ベリリウム銅合金材料よりなる部品成形体
の製造方法。
[Claims] 1 Be: 0.2 to 0.8 wt%, and Ni and/or
A rolled sheet of Be-Cu alloy containing 0.3 to 4.0 wt% of Co, with the remainder being substantially Cu, is subjected to solution treatment, then cold worked at a reduction rate of 20% or more, and then The Be-Cu alloy material obtained by annealing at temperatures between ℃ and 550℃ is further formed into the desired part shape by processing including bending.
A molded part made of a beryllium copper alloy material, characterized in that it is obtained by aging at a temperature of 350°C to 500°C. 2 Be: 0.2 to 0.8wt%, and Ni and/or
A rolled sheet of Be-Cu alloy containing 0.3 to 4.0 wt% of Co, with the remainder being substantially Cu, is subjected to solution treatment, then cold worked at a reduction rate of 20% or more, and then The Be-Cu alloy material obtained by annealing at temperatures between ℃ and 550℃ is further formed into the desired part shape by processing including bending.
A method for producing a molded part made of a beryllium copper alloy material, characterized by aging at a temperature of 350°C to 500°C.
JP5514787A 1987-03-12 1987-03-12 Formed body for parts composed of berylium-copper alloy material and its production Granted JPS63223151A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
JP5514787A JPS63223151A (en) 1987-03-12 1987-03-12 Formed body for parts composed of berylium-copper alloy material and its production
EP88301618A EP0282204B1 (en) 1987-03-12 1988-02-25 Shaped body formed of copper-beryllium alloy and method of manufacturing same
DE19883884239 DE3884239T2 (en) 1987-03-12 1988-02-25 Shaped body made of copper-beryllium alloy and process for its manufacture.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5514787A JPS63223151A (en) 1987-03-12 1987-03-12 Formed body for parts composed of berylium-copper alloy material and its production

Publications (2)

Publication Number Publication Date
JPS63223151A JPS63223151A (en) 1988-09-16
JPH0123526B2 true JPH0123526B2 (en) 1989-05-02

Family

ID=12990650

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5514787A Granted JPS63223151A (en) 1987-03-12 1987-03-12 Formed body for parts composed of berylium-copper alloy material and its production

Country Status (3)

Country Link
EP (1) EP0282204B1 (en)
JP (1) JPS63223151A (en)
DE (1) DE3884239T2 (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0774420B2 (en) * 1991-02-21 1995-08-09 日本碍子株式会社 Method for producing beryllium copper alloy
US5486244A (en) * 1992-11-04 1996-01-23 Olin Corporation Process for improving the bend formability of copper alloys
US5824167A (en) * 1994-01-06 1998-10-20 Ngk Insulators, Ltd. Beryllium-copper alloy excellent in strength, workability and heat resistance and method for producing the same
EP0854200A1 (en) * 1996-10-28 1998-07-22 BRUSH WELLMAN Inc. Copper-beryllium alloy
US6001196A (en) * 1996-10-28 1999-12-14 Brush Wellman, Inc. Lean, high conductivity, relaxation-resistant beryllium-nickel-copper alloys
US6129795A (en) * 1997-08-04 2000-10-10 Integran Technologies Inc. Metallurgical method for processing nickel- and iron-based superalloys
DE102006018896B3 (en) * 2006-04-24 2007-12-13 Infineon Technologies Ag Local selective change of breaking strength and elongation in region of bending groove of electrical terminal clamp, includes strong cold deformation of the electrical terminal clamp by annealing under variable recrystallization temperature
JP5480688B2 (en) * 2010-03-26 2014-04-23 株式会社神戸製鋼所 Aluminum alloy plate for PP cap and method for producing the same
EP3208664B1 (en) * 2016-02-19 2023-08-16 Omega SA Timepiece mechanism or clock without magnetic signature

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4179314A (en) * 1978-12-11 1979-12-18 Kawecki Berylco Industries, Inc. Treatment of beryllium-copper alloy and articles made therefrom
US4394185A (en) * 1982-03-30 1983-07-19 Cabot Berylco, Inc. Processing for copper beryllium alloys
CA1237361A (en) * 1983-11-10 1988-05-31 Brush Wellman Inc. Thermomechanical processing of beryllium-copper alloys
US4579603A (en) * 1985-03-18 1986-04-01 Woodard Dudley H Controlling distortion in processed copper beryllium alloys

Also Published As

Publication number Publication date
JPS63223151A (en) 1988-09-16
EP0282204B1 (en) 1993-09-22
EP0282204A1 (en) 1988-09-14
DE3884239D1 (en) 1993-10-28
DE3884239T2 (en) 1994-03-31

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