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JPS5950740B2 - high strength copper alloy - Google Patents
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JPS5950740B2 - high strength copper alloy - Google Patents

high strength copper alloy

Info

Publication number
JPS5950740B2
JPS5950740B2 JP7442877A JP7442877A JPS5950740B2 JP S5950740 B2 JPS5950740 B2 JP S5950740B2 JP 7442877 A JP7442877 A JP 7442877A JP 7442877 A JP7442877 A JP 7442877A JP S5950740 B2 JPS5950740 B2 JP S5950740B2
Authority
JP
Japan
Prior art keywords
weight
strength
zirconium
chromium
copper alloy
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
JP7442877A
Other languages
Japanese (ja)
Other versions
JPS549117A (en
Inventor
光一 手島
晴香 待鳥
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.)
Toshiba Corp
Original Assignee
Tokyo Shibaura Electric Co 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 Tokyo Shibaura Electric Co Ltd filed Critical Tokyo Shibaura Electric Co Ltd
Priority to JP7442877A priority Critical patent/JPS5950740B2/en
Publication of JPS549117A publication Critical patent/JPS549117A/en
Publication of JPS5950740B2 publication Critical patent/JPS5950740B2/en
Expired legal-status Critical Current

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  • Conductive Materials (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)

Description

【発明の詳細な説明】 本発明はチタン−銅合金系の高力銅合金の改良に関する
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to improvements in high strength copper alloys based on titanium-copper alloys.

チタン−銅合金は析出硬化して硬さ、強さなどのすぐれ
た銅合金として使用されている。
Titanium-copper alloys are precipitation hardened and are used as copper alloys with excellent hardness and strength.

しかし、さらに硬さ、強度、バネ性などを向上させるこ
とが望まれる。
However, it is desired to further improve hardness, strength, springiness, etc.

このために、本発明はクロムやジルコニウムを添加する
とともに、けい素、マグネシウム、ゲルマニウム、はう
素などを添加して、結晶粒の微細化と肌荒れの防止を図
り、かつ強度等の特性向上を実現したものである。
To this end, the present invention adds chromium and zirconium, as well as silicon, magnesium, germanium, boron, etc., to refine crystal grains, prevent rough skin, and improve properties such as strength. This has been achieved.

本発明合金の第1の実施態様は、チタン1〜5重量%と
、クロム0.1〜3重量%と、けい素、マグネシウム、
ゲルマニウム、はう素のうち少くとも1種を0.005
〜0.1重量%と、残部銅とからなる合金である。
A first embodiment of the alloy of the present invention contains 1 to 5% by weight of titanium, 0.1 to 3% by weight of chromium, silicon, magnesium,
0.005 of at least one of germanium and borosilicate
It is an alloy consisting of ~0.1% by weight and the balance copper.

チタンは強度をある程度達成するために不可欠であり、
一方あまり多量に含有すると加工性が劣化するので上記
値とする。
Titanium is essential to achieve some degree of strength;
On the other hand, if the content is too large, the processability will deteriorate, so the above value is set.

好ましくは2〜4.5重量%、最も好ましくは3〜4重
量%である。
Preferably it is 2-4.5% by weight, most preferably 3-4% by weight.

クロムは加工性を劣化させずに、チタンによる強度向上
の効果をさらに高めるため添加されるが、あまり多くし
ても強度向上の効果はみられない。
Chromium is added to further enhance the strength improvement effect of titanium without deteriorating workability, but if it is added too much, no strength improvement effect will be seen.

よって上記値とする。硬さ、強度、バネ性のバランスの
ため好ましくは0.1〜2重量%、最も好ましくは0.
5〜1.5重量%である。
Therefore, the above value is used. In order to balance hardness, strength, and springiness, it is preferably 0.1 to 2% by weight, most preferably 0.1% by weight.
It is 5 to 1.5% by weight.

けい素、マグネシウム、ゲルマニウム、はう素は、結晶
粒の微細化や肌荒れ防止に役立ち、強度、延性等の向上
に効果を示す。
Silicon, magnesium, germanium, and boron are useful for refining crystal grains and preventing rough skin, and are effective in improving strength, ductility, etc.

あまり多く添加してもその割に強度等の向上がみられな
いので上記範囲とするが、これ等が最も効果的なのは好
ましくは0.01〜0.08重量%、最も好ましくは0
.02〜0.05重量%である。
Even if too much is added, no improvement in strength etc. is observed, so the above range is used, but the most effective range is preferably 0.01 to 0.08% by weight, most preferably 0.
.. 02 to 0.05% by weight.

本発明の第2の実施態様はチタン1〜5重量%、ジルコ
ニウム0.1〜3重量%、けい素、マグネシウム、ゲル
マニウム、はう素のうち少くとも1種0.05〜0.1
重量%、残部銅とからなるものである。
A second embodiment of the present invention includes 1 to 5% by weight of titanium, 0.1 to 3% by weight of zirconium, and 0.05 to 0.1% of at least one of silicon, magnesium, germanium, and boron.
% by weight, the balance being copper.

第1の実施態様とはクロムにかえジルコニウムを含有す
る点で異なるが、ジルコニウムの場合の方がクロムの場
合より添加量を少くしうる点で好ましい。
Although it differs from the first embodiment in that it contains zirconium instead of chromium, zirconium is preferable in that the amount added can be smaller than that of chromium.

したがってこの第2の実施態様においてはジルコニウム
の好ましい範囲は硬さ、強度、バネ性のバランスの点か
らも合わせて0.1〜1.0重量%、最も好ましくは0
.3〜0.8重量%である。
Therefore, in this second embodiment, the preferable range of zirconium is 0.1 to 1.0% by weight, most preferably 0.0% by weight in terms of the balance between hardness, strength, and springiness.
.. It is 3 to 0.8% by weight.

第3の実施態様はチタン1〜5重量%、クロムとジルコ
ニウムを合量で0.1〜3重量%(但し、クロム、ジル
コニウムはいずれも必須元素)、けい素、マグネシウム
、ゲルマニウム、はう素のうち少くとも1種0.005
〜0.1重量%、残部銅からなる合金である。
The third embodiment contains 1 to 5% by weight of titanium, 0.1 to 3% by weight of chromium and zirconium in total (however, chromium and zirconium are both essential elements), silicon, magnesium, germanium, and boron. At least one of the following: 0.005
It is an alloy consisting of ~0.1% by weight, the balance being copper.

この実施態様の場合はクロムとジルコニウムを両方必ず
含むため相互作用により強度、硬度、バネ性の向上に効
果が大である点で上記2つの実施態様より有利である。
This embodiment is more advantageous than the above two embodiments in that since it necessarily contains both chromium and zirconium, the interaction has a great effect on improving strength, hardness, and springiness.

この場合好ましくはクロム0.5〜1.5重量%、ジル
コニウム0.3〜0.8重量%とするとよい。
In this case, it is preferable to use 0.5 to 1.5% by weight of chromium and 0.3 to 0.8% by weight of zirconium.

最も好ましくはクロム0.6〜1.0重量%、ジルコニ
ウム0.3〜0.5重量%とすることである。
Most preferably, the content is 0.6 to 1.0% by weight of chromium and 0.3 to 0.5% by weight of zirconium.

なお、第2、第3の実施態様ではけい素、マグネシウム
、ゲルマニウム、はう素の説明を特にしなかったが、第
1の実施態様の場合と同様である。
Note that in the second and third embodiments, silicon, magnesium, germanium, and boron were not particularly explained, but this is the same as in the first embodiment.

本発明合金は析出硬化型合金であるため、溶体化処理→
冷間加工→時効処理を必要とする。
Since the alloy of the present invention is a precipitation hardening alloy, solution treatment→
Requires cold working → aging treatment.

溶体化処理は850〜920℃で行い、急冷後80%以
下の加工率で冷間加工し、350〜500℃で1〜3時
間時間時効処理するとよい。
Solution treatment is preferably performed at 850 to 920°C, followed by cold working at a processing rate of 80% or less after quenching, and aging treatment at 350 to 500°C for 1 to 3 hours.

本発明合金を完成するにあたり行った実験の代表例を次
の第1表及び第2表に示す。
Representative examples of experiments conducted to complete the alloy of the present invention are shown in Tables 1 and 2 below.

これらの結果は析出硬化のために、900℃で溶体化処
理したのち、急冷し、さらに60%の冷間加工を施し、
425℃にて2時間の時効処理を施した場合である。
These results show that for precipitation hardening, after solution treatment at 900℃, quenching, and further cold working of 60%,
This is the case where aging treatment was performed at 425° C. for 2 hours.

本発明合金は以上のように優れた強度を有しておりバネ
材として有用であり、また熱伝導性も良好であるため金
型材料としても有用である。
As described above, the alloy of the present invention has excellent strength and is useful as a spring material, and also has good thermal conductivity, so it is useful as a mold material.

Claims (1)

【特許請求の範囲】[Claims] 1 チタン1〜5重量%と、クロム及びジルコニウムの
うち一方又は両方を0.1〜3重量%と、けい素、マグ
ネシウム、ゲルマニウム、はう素のうち少くとも1種を
0.005〜0.1%と、残部銅とからなる高力銅合金
1 1 to 5% by weight of titanium, 0.1 to 3% by weight of one or both of chromium and zirconium, and 0.005 to 0.0% of at least one of silicon, magnesium, germanium, and boron. A high-strength copper alloy consisting of 1% copper and the balance copper.
JP7442877A 1977-06-24 1977-06-24 high strength copper alloy Expired JPS5950740B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7442877A JPS5950740B2 (en) 1977-06-24 1977-06-24 high strength copper alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7442877A JPS5950740B2 (en) 1977-06-24 1977-06-24 high strength copper alloy

Publications (2)

Publication Number Publication Date
JPS549117A JPS549117A (en) 1979-01-23
JPS5950740B2 true JPS5950740B2 (en) 1984-12-10

Family

ID=13546921

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7442877A Expired JPS5950740B2 (en) 1977-06-24 1977-06-24 high strength copper alloy

Country Status (1)

Country Link
JP (1) JPS5950740B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01219520A (en) * 1988-02-26 1989-09-01 Canon Inc inkjet recording device

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59159243A (en) * 1983-03-02 1984-09-08 Hitachi Ltd Metallic mold for casting and its production
JPS60218440A (en) * 1984-04-13 1985-11-01 Furukawa Electric Co Ltd:The Copper alloy for lead frame

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01219520A (en) * 1988-02-26 1989-09-01 Canon Inc inkjet recording device

Also Published As

Publication number Publication date
JPS549117A (en) 1979-01-23

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