Deprecated: The each() function is deprecated. This message will be suppressed on further calls in /home/zhenxiangba/zhenxiangba.com/public_html/phproxy-improved-master/index.php on line 456
JPS6013418B2 - High strength copper alloy - Google Patents
[go: Go Back, main page]

JPS6013418B2 - High strength copper alloy - Google Patents

High strength copper alloy

Info

Publication number
JPS6013418B2
JPS6013418B2 JP55145314A JP14531480A JPS6013418B2 JP S6013418 B2 JPS6013418 B2 JP S6013418B2 JP 55145314 A JP55145314 A JP 55145314A JP 14531480 A JP14531480 A JP 14531480A JP S6013418 B2 JPS6013418 B2 JP S6013418B2
Authority
JP
Japan
Prior art keywords
high strength
copper alloy
strength copper
manganese
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
JP55145314A
Other languages
Japanese (ja)
Other versions
JPS5770248A (en
Inventor
健治 久保薗
俊彦 森
輝雄 中西
公男 橋爪
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric Corp
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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP55145314A priority Critical patent/JPS6013418B2/en
Publication of JPS5770248A publication Critical patent/JPS5770248A/en
Publication of JPS6013418B2 publication Critical patent/JPS6013418B2/en
Expired legal-status Critical Current

Links

Landscapes

  • Conductive Materials (AREA)
  • Springs (AREA)

Description

【発明の詳細な説明】 この発明は、時効硬化性を有する高強度ばね材料に関す
るものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a high strength spring material having age hardenability.

従来、高強度ばね材料として使用されている代表例とし
てベリリウム鋼合金があるが、この合金の場合原材料費
が高価であるためおのずと用途が制限されている。
Beryllium steel alloy is a typical example of a material that has been conventionally used as a high-strength spring material, but the high cost of raw materials naturally limits its uses.

この発明はコスト的に優位な原材料を使用し高強度ばね
材の要求に答えたものである。
This invention meets the demand for high-strength spring materials using cost-effective raw materials.

一般に鋼一ニッケルースズ系の合金についてはある成分
比、あるいは加工率において、時効処理を施すことによ
り、スピノーダル分解が認められ、材料が硬化すること
が一部報告されている。しかし、この銅−ニッケルース
ズのみの成分では、時効硬化をさせるための素材の溶体
化処理において、結晶粒度が非常に大きく成長しやすく
、実用合金としては部品の曲げ加工や絞りにおいて肌あ
れを生じるという欠点が認められる。又上記鋼ーニッケ
ルースズ合金を得る場合にある墨比でマンガンを希釈剤
として存在させる方法もあるが、かかる方法はその製造
工程が複雑化するばかりでなくその温度管理に厳しい条
件が要求される等の問題がある。
In general, it has been reported that spinodal decomposition is observed in steel-nickel-tin alloys and the material hardens when subjected to aging treatment at a certain component ratio or processing rate. However, with this copper-nickel-tin component alone, the crystal grain size tends to grow very large during the solution treatment of the material for age hardening, and it is said that when used as a practical alloy, it will cause roughness during bending and drawing of parts. Defects are recognized. There is also a method in which manganese is present as a diluent at a certain black ratio when obtaining the above-mentioned steel-nickel-tin alloy, but such a method not only complicates the manufacturing process but also requires strict conditions for temperature control. There's a problem.

この発明はこの欠点を補うために徴量のマンガンを添加
し工程を複雑化することなく結晶粒の粗大化を抑えたも
のである。
In order to compensate for this drawback, the present invention adds a certain amount of manganese to suppress the coarsening of crystal grains without complicating the process.

この発明における添加元素中、ニッケル及びスズは時効
硬化が得られる最小成分量を下限としそれぞれ8%、3
%とした。
Among the additive elements in this invention, nickel and tin have a lower limit of 8% and 3%, respectively, with the minimum component amount that provides age hardening.
%.

また上限については、加工性よりそれぞれ30%、8%
とした。マンガンについては結晶粒の粗大化を抑える効
果が認められる量の0.2%を下限とし、上限について
はニッケル、スズと同様加工性の点で0.8%とした。
Also, the upper limits are 30% and 8%, respectively, based on workability.
And so. Regarding manganese, the lower limit was set at 0.2%, which is the amount at which the effect of suppressing coarsening of crystal grains is recognized, and the upper limit was set at 0.8% from the viewpoint of workability, similar to nickel and tin.

またマンガンについては他に脱酸剤としての効果も含ま
れている。以下、この発明の一実施例について説明する
Manganese also has other effects as a deoxidizing agent. An embodiment of the present invention will be described below.

試料の作成は前加工率60%で0.3肋厚さの試料を用
い、それぞれの組成材について溶体化処理を行い結晶粒
度の測定と更に加工を施した後の特性を確認した。表は
試験に供した一実施例の組成と代表特性を示したもので
ある。
Samples were prepared with a pre-processing rate of 60% and a thickness of 0.3 ribs, and each composition material was subjected to solution treatment, and the grain size was measured and the properties after further processing were confirmed. The table shows the composition and typical characteristics of one example tested.

表 表における引張強さはそれぞれの試料を850qoで1
股ご間の溶体化処理を施した後で40%の加工を行なっ
たものと更に250〜5000○で各々100分間の均
熱を行ったときの強度が最高となった値である。
The tensile strength in the table is 1 at 850qo for each sample.
The strength was the highest when the crotch was subjected to 40% processing after solution treatment and when it was soaked for 100 minutes at 250 to 5000°.

具体的には試料No.1は425qoで100分間、N
o.2〜No.4は450℃で100分の熱処理を行っ
たときの値である。図はそれぞれの試料の熔体化処理と
結晶粒度の関係を示したものである。
Specifically, sample No. 1 is 425qo for 100 minutes, N
o. 2~No. 4 is the value obtained when heat treatment was performed at 450° C. for 100 minutes. The figure shows the relationship between melting treatment and crystal grain size for each sample.

表及び図の結果よりこの合金は非常に優れた時効硬化性
を有しているが結晶粒度に関してはマンガンの影響が大
きいことを示している。
The results shown in the table and figures show that this alloy has very good age hardenability, but the grain size is greatly influenced by manganese.

即ちマンガン量が0.2%未満においては結晶粒の粗大
化が著しく含有量が多い程抑制効果があることが分る。
以上のように、この発明合金は比較的低コストの原材料
の組成で高強度を得ることができ、また実用面で曲げや
絞りの加工を施した部分が接触部の場合に問題となる肌
あれが生じにくい、即ち結晶粒度の細かい材料をつくる
ことを可能にしたものである。
That is, it can be seen that when the amount of manganese is less than 0.2%, the crystal grains become coarser and the larger the content, the more suppressive effect there is.
As described above, this invention alloy can obtain high strength with a relatively low-cost raw material composition, and in practical use, it is possible to obtain surface roughness, which is a problem when the contact area is a bent or drawn part. This makes it possible to produce a material that is difficult to produce, that is, has a fine crystal grain size.

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

図は試料Nol〜No.4の組成合金について750〜
880つ○で各10分間の熱処理を行ったときの結晶粒
度と熱処理温度との関係を示す図である。
The figure shows samples No. 750~ for composition alloy 4
It is a figure which shows the relationship between the crystal grain size and heat treatment temperature when heat treatment was performed for 10 minutes each at 880 points.

Claims (1)

【特許請求の範囲】[Claims] 1 重量比でニツケル8〜30%、スズ3〜8%、とマ
ンガンを0.2〜0.8%含み及びそれに付随する不可
避の不純物と残部銅から成ることを特徴とする高強度銅
合金。
1. A high-strength copper alloy comprising, by weight, 8 to 30% of nickel, 3 to 8% of tin, and 0.2 to 0.8% of manganese, accompanied by inevitable impurities, and the balance being copper.
JP55145314A 1980-10-17 1980-10-17 High strength copper alloy Expired JPS6013418B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP55145314A JPS6013418B2 (en) 1980-10-17 1980-10-17 High strength copper alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP55145314A JPS6013418B2 (en) 1980-10-17 1980-10-17 High strength copper alloy

Publications (2)

Publication Number Publication Date
JPS5770248A JPS5770248A (en) 1982-04-30
JPS6013418B2 true JPS6013418B2 (en) 1985-04-06

Family

ID=15382285

Family Applications (1)

Application Number Title Priority Date Filing Date
JP55145314A Expired JPS6013418B2 (en) 1980-10-17 1980-10-17 High strength copper alloy

Country Status (1)

Country Link
JP (1) JPS6013418B2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0637680B2 (en) * 1987-06-15 1994-05-18 三菱電機株式会社 Cu-Ni-Sn alloy with excellent fatigue characteristics
JPH0736885B2 (en) * 1991-03-29 1995-04-26 川崎重工業株式会社 Exhaust gas cooling / purification method and device

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5430370A (en) * 1977-08-10 1979-03-06 Shimano Industrial Co Brake for use in vehicle

Also Published As

Publication number Publication date
JPS5770248A (en) 1982-04-30

Similar Documents

Publication Publication Date Title
KR930005073B1 (en) Cu-Ni-Sn Alloy with Excellent Fatigue Properties
US4052204A (en) Quaternary spinodal copper alloys
US1935897A (en) Precious metal alloy
KR101040909B1 (en) Brass
JP4154100B2 (en) Copper alloy for electronic materials having excellent surface characteristics and method for producing the same
US3901692A (en) Corrosion resistant copper alloy and the method of forming the alloy
JPH03162553A (en) Manufacture of high strength and high conductivity copper alloy having good bendability
JPH07258803A (en) Production of titanium-copper alloy excellent in bendability and stress relaxation property
US2048647A (en) Process of producing hard alloys
JPS6013418B2 (en) High strength copper alloy
US2804408A (en) Process of treating tin bronze
US4871399A (en) Copper alloy for use as wiring harness terminal material and process for producing the same
JP2009108392A (en) High-strength nickel silver superior in bendability, and manufacturing method therefor
JPS62156242A (en) Copper-base alloy
US2390775A (en) Brazing alloys
JPH0456755A (en) Manufacture of phosphor bronze excellent in bendability
JPS58213847A (en) Copper alloy for electric and electronic parts and its manufacture
JPH0469217B2 (en)
JP2918961B2 (en) High-strength copper alloy with high workability
JPS6141751A (en) Manufacture of copper alloy material for lead frame
JPH01189805A (en) Copper alloy for wire harness terminal
US3150969A (en) Beryllium-bronze alloy
JP3050763B2 (en) Heat resistant automotive terminal materials
JPS6260850A (en) Manufacture of copper alloy having superior stress relaxation resistance
JPS62243750A (en) Manufacture of copper alloy excellent in property of proof stress relaxation