JP6196757B2 - Corson alloy and manufacturing method thereof - Google Patents

Corson alloy and manufacturing method thereof Download PDF

Info

Publication number
JP6196757B2
JP6196757B2 JP2012156835A JP2012156835A JP6196757B2 JP 6196757 B2 JP6196757 B2 JP 6196757B2 JP 2012156835 A JP2012156835 A JP 2012156835A JP 2012156835 A JP2012156835 A JP 2012156835A JP 6196757 B2 JP6196757 B2 JP 6196757B2
Authority
JP
Japan
Prior art keywords
rolling
annealing
corson alloy
area ratio
cold rolling
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.)
Active
Application number
JP2012156835A
Other languages
Japanese (ja)
Other versions
JP2014019880A (en
Inventor
波多野 隆紹
隆紹 波多野
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.)
JX Nippon Mining and Metals Corp
Original Assignee
JX Nippon Mining and Metals 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 JX Nippon Mining and Metals Corp filed Critical JX Nippon Mining and Metals Corp
Priority to JP2012156835A priority Critical patent/JP6196757B2/en
Publication of JP2014019880A publication Critical patent/JP2014019880A/en
Application granted granted Critical
Publication of JP6196757B2 publication Critical patent/JP6196757B2/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Conductive Materials (AREA)

Description

本発明は、コネクタ、端子、リレー、スイッチ等の導電性ばね材やトランジスタ、集積回路(IC)等の半導体機器のリ−ドフレーム材として好適な、優れた強度、曲げ加工性、耐応力緩和特性、導電性等を備えたコルソン合金及びその製造方法に関する。   The present invention is excellent in strength, bending workability, stress relaxation suitable as a lead frame material for semiconductor devices such as conductive spring materials such as connectors, terminals, relays and switches, and transistors and integrated circuits (ICs). The present invention relates to a Corson alloy having characteristics, conductivity, and the like, and a manufacturing method thereof.

近年、電気・電子部品の小型化が進み、これら部品に使用される銅合金に良好な強度、導電率及び曲げ加工性が要求されている。この要求に応じ、従来のりん青銅や黄銅といった固溶強化型銅合金に替わり、高い強度及び導電率を有するコルソン合金等の析出強化型銅合金の需要が増加している。コルソン合金はCuマトリックス中にNi−Si、Co−Si、Ni−Co−Si等の金属間化合物を析出させた合金であり、高強度、高い導電率、良好な曲げ加工性を兼ね備えている。一般に、強度と曲げ加工性とは相反する性質であり、コルソン合金においても高強度を維持しつつ曲げ加工性を改善することが望まれている。   In recent years, electrical and electronic parts have been miniaturized, and copper alloys used for these parts are required to have good strength, electrical conductivity, and bending workability. In response to this demand, demand for precipitation strengthened copper alloys such as Corson alloys having high strength and conductivity is increasing instead of conventional solid solution strengthened copper alloys such as phosphor bronze and brass. A Corson alloy is an alloy in which an intermetallic compound such as Ni—Si, Co—Si, or Ni—Co—Si is precipitated in a Cu matrix, and has high strength, high electrical conductivity, and good bending workability. Generally, strength and bending workability are contradictory properties, and it is desired to improve bending workability while maintaining high strength even in a Corson alloy.

ここでコルソン合金には、曲げ軸を圧延方向と直交直角にとった場合(Good Way)の曲げ加工性が、曲げ軸を圧延方向と平行にとった場合(Bad Way)の曲げ加工性より劣るという性質があり、Good Wayの曲げ加工性の改善が特に求められている。   Here, in the Corson alloy, the bending workability when the bending axis is perpendicular to the rolling direction (Good Way) is inferior to the bending workability when the bending axis is parallel to the rolling direction (Bad Way). There is a particular need for improving the good workability of Good Way.

近年、コルソン合金の曲げ加工性を改善する技術として、{001}<100>方位(Cube方位)を発達させる方策が提唱されている。例えば、特許文献1(特開2006−283059号)では、(1)鋳造、(2)熱間圧延、(3)冷間圧延(加工度95%以上)、(4)溶体化処理、(5)冷間圧延(加工度20%以下)、(6)時効処理、(7)冷間圧延(加工度1〜20%)、(8)短時間焼鈍、の工程を順次行うことにより、Cube方位の面積率を50%以上に制御し、曲げ加工性を改善している。   In recent years, as a technique for improving the bending workability of the Corson alloy, a strategy for developing the {001} <100> orientation (Cube orientation) has been proposed. For example, in patent document 1 (Unexamined-Japanese-Patent No. 2006-283059), (1) Casting, (2) Hot rolling, (3) Cold rolling (working degree 95% or more), (4) Solution treatment, (5 Cube orientation by performing the steps of cold rolling (working degree 20% or less), (6) aging treatment, (7) cold rolling (working degree 1-20%), and (8) short-time annealing. Is controlled to 50% or more to improve the bending workability.

特許文献2(特開2010−275622号)では、(1)鋳造、(2)熱間圧延(950℃から400℃に温度を下げながら行う)、(3)冷間圧延(加工度50%以上)、(4)中間焼鈍(450〜600℃、導電率を1.5倍以上に硬さを0.8倍以下に調整する)、(5)冷間圧延(加工度70%以上)、(6)溶体化処理、(7)冷間圧延(加工度0〜50%)、(8)時効処理を順次行うことにより、(200)({001}と同義)のX線回折強度を銅粉標準試料のX線回折強度以上に制御し曲げ加工性を改善している。   In Patent Document 2 (Japanese Patent Laid-Open No. 2010-275622), (1) casting, (2) hot rolling (performed while lowering the temperature from 950 ° C to 400 ° C), (3) cold rolling (working degree of 50% or more) ), (4) Intermediate annealing (450 to 600 ° C., adjusting conductivity to 1.5 times or more and hardness to 0.8 times or less), (5) cold rolling (working degree 70% or more), ( 6) Solution treatment, (7) Cold rolling (working degree 0 to 50%), (8) Aging treatment is carried out in order, and the X-ray diffraction intensity of (200) (synonymous with {001}) is reduced to copper powder. Bending workability is improved by controlling the X-ray diffraction intensity of the standard sample.

特許文献3(特開2011−17072号)では、Cube方位の面積率を5〜60%に制御すると同時に、Brass方位及びCopper方位の面積率をともに20%以下に制御し、曲げ加工性を改善している。そのための製造方法としては、(1)鋳造、(2)熱間圧延、(3)冷間圧延(加工度85〜99%)、(4)熱処理(300〜700℃、5分〜20時間)、(5)冷間圧延(加工度5〜35%)、(6)溶体化処理(昇温速度2〜50℃/秒)、(7)時効処理、(8)冷間圧延(加工度2〜30%)、(9)調質焼鈍、の工程を順次行う場合に最も良好な曲げ性が得られている。   In Patent Document 3 (Japanese Patent Laid-Open No. 2011-17072), the area ratio of the Cube orientation is controlled to 5 to 60%, and at the same time, the area ratios of the Brass orientation and Copper orientation are both controlled to 20% or less to improve bending workability. doing. Production methods for this purpose include (1) casting, (2) hot rolling, (3) cold rolling (working degree 85 to 99%), and (4) heat treatment (300 to 700 ° C, 5 minutes to 20 hours). (5) Cold rolling (working degree 5 to 35%), (6) Solution treatment (temperature increase rate 2 to 50 ° C./second), (7) Aging treatment, (8) Cold rolling (working degree 2) ~ 30%) and (9) temper annealing are performed in order to obtain the best bendability.

特許文献4(特許第4857395号公報)では、板厚方向の中央部において、Cube方位の面積率を10〜80%に制御すると同時に、Brass方位及びCopper方位の面積率をともに20%以下に制御し、ノッチ曲げ性を改善している。ノッチ曲げを可能とする製造方法として、(1)鋳造、(2)熱間圧延、(3)冷間圧延(30〜99%)、(4)予備焼鈍(軟化度0.25〜0.75、導電率20〜45%IACS)、(5)冷間圧延(7〜50%)、(6)溶体化処理、(7)時効、なる工程を提唱している。   In Patent Document 4 (Japanese Patent No. 4857395), the area ratio of the Cube orientation is controlled to 10 to 80% at the center in the thickness direction, and at the same time, the area ratios of the Brass orientation and Copper orientation are both controlled to 20% or less. And notch bendability is improved. Manufacturing methods that enable notch bending include (1) casting, (2) hot rolling, (3) cold rolling (30 to 99%), and (4) pre-annealing (softening degree of 0.25 to 0.75). , Conductivity 20-45% IACS), (5) cold rolling (7-50%), (6) solution treatment, (7) aging.

特許文献5(WO2011/068121公報)では、材料の表層および深さ位置で全体の1/4の位置でのCube方位面積率をそれぞれW0およびW4とし、W0/W4を0.8〜1.5、W0を5〜48%に制御し、さらに平均結晶粒径を12〜100μmに調整することで、180度密着曲げ性および耐応力緩和性を改善している。そのための製造方法として、(1)鋳造、(2)熱間圧延、(1パスの加工率を30%以下とし各パス間の保持時間を20〜100秒とする)、(3)冷間圧延(加工度90〜99%)、(4)熱処理(300〜700℃、10秒〜5時間)、(5)冷間圧延(加工度5〜50%)、(6)溶体化処理(800〜1000℃)、(7)時効処理、(8)冷間圧延、(9)調質焼鈍、なる工程を提唱している。   In Patent Document 5 (WO2011 / 068121), the Cube azimuth area ratios at 1/4 positions of the entire surface layer and depth position of the material are W0 and W4, respectively, and W0 / W4 is 0.8 to 1.5. , W0 is controlled to 5 to 48%, and the average crystal grain size is adjusted to 12 to 100 μm, thereby improving 180-degree adhesion bendability and stress relaxation resistance. Production methods therefor include (1) casting, (2) hot rolling, (the processing rate of one pass is 30% or less and the holding time between each pass is 20 to 100 seconds), (3) cold rolling (Working degree 90 to 99%), (4) heat treatment (300 to 700 ° C., 10 seconds to 5 hours), (5) cold rolling (working degree 5 to 50%), (6) solution treatment (800 to 1000 ° C), (7) aging treatment, (8) cold rolling, and (9) temper annealing are proposed.

曲げ性を改善する技術ではないが、特許文献6(WO2011/068134公報)では、圧延方向に向く(100)面の面積率を30%以上に制御することにより、ヤング率を110GPa以下、曲げたわみ係数を105GPa以下に調整している。また、そのための製造方法として、(1)鋳造、(2)熱間圧延(徐冷)、(3)冷間圧延(加工度70%以上)、(4)熱処理(300〜800℃、5秒〜2時間)、(5)冷間圧延(加工度3〜60%)、(6)溶体化処理、(7)時効処理、(8)冷間圧延(加工度50%以下)、(9)調質焼鈍、なる工程を提唱している。   Although it is not a technique for improving bendability, in Patent Document 6 (WO2011 / 068134), the Young's modulus is bent to 110 GPa or less by controlling the area ratio of the (100) plane facing the rolling direction to 30% or more. The coefficient is adjusted to 105 GPa or less. As manufacturing methods therefor, (1) casting, (2) hot rolling (slow cooling), (3) cold rolling (working degree of 70% or more), (4) heat treatment (300 to 800 ° C., 5 seconds) ~ 2 hours), (5) cold rolling (working degree 3 to 60%), (6) solution treatment, (7) aging treatment, (8) cold rolling (working degree 50% or less), (9) The process of temper annealing is proposed.

特開2006−283059号JP 2006-283059 A 特開2010−275622号JP 2010-275622 A 特開2011−17072号JP 2011-17072 A 特許第4857395号公報Japanese Patent No. 4857395 WO2011/068121公報WO2011 / 068121 WO2011/068134公報WO2011 / 068134

本発明者は、従来技術に従いCube方位を発達させ曲げ性を改善したコルソン合金につき、コネクタに加工後のばね特性を検討した。その結果、図1に模式的に示すように、圧延方向と直交する方向(以下、圧延直交方向とする)にばね部が採取される端面接触型端子として用いた場合に、ばね接点において充分な接触力が得られず接触電気抵抗が増大することがあった。また、この接触力の低下が圧延直交方向のヤング率が低いことと関係することを知見した。ここでいうヤング率とは、圧延直交方向に引張試験を行って応力歪曲線を採取し、応力歪曲線における弾性範囲の直線の傾きから求めるヤング率であり、曲げたわみ係数として求めるヤング率(日本伸銅協会(JACBA)技術標準「銅及び銅合金板条の片持ち梁による曲げたわみ係数測定方法」)は上記接触力との相関を示さなかった。以下、単に「ヤング率」と表記する場合は、引張試験から求めるヤング率を指す。   This inventor examined the spring characteristic after processing a connector about the Corson alloy which developed Cube orientation and improved bendability according to the prior art. As a result, as schematically shown in FIG. 1, when used as an end face contact type terminal in which the spring portion is taken in a direction orthogonal to the rolling direction (hereinafter referred to as the rolling orthogonal direction), the spring contact is sufficient. The contact force could not be obtained, and the contact electrical resistance sometimes increased. It was also found that this decrease in contact force is related to a low Young's modulus in the direction perpendicular to rolling. The Young's modulus here refers to the Young's modulus obtained from a stress-strain curve obtained by conducting a tensile test in the direction perpendicular to the rolling direction, and obtained from the slope of the straight line of the elastic range in the stress-strain curve. The copper standard association (JACBA) technical standard “Method of measuring bending deflection coefficient by cantilever of copper and copper alloy strips”) showed no correlation with the contact force. Hereinafter, the simple expression “Young's modulus” refers to the Young's modulus obtained from a tensile test.

そこで本発明は、優れた曲げ加工性と有すると同時に、高い圧延直交方向のヤング率をも有する、コルソン合金及びその製造方法を提供することを課題とする。   Then, this invention makes it a subject to provide the Corson alloy which has the high Young's modulus of a rolling orthogonal direction, and its manufacturing method while having the outstanding bending workability.

本発明者は、コルソン合金の結晶方位をEBSD法で解析し、表面および板厚中央の断面のそれぞれに対し、結晶方位を最適化することにより、曲げ加工性が良好でありながら、圧延直交方向のヤング率も充分に高いコルソン合金が得られることを見出し、また、この結晶方位を得るための製造方法を明らかにした。   The present inventor analyzed the crystal orientation of the Corson alloy by the EBSD method, and optimized the crystal orientation for each of the surface and the cross-section at the center of the plate thickness, so that the bendability is good, but the orthogonal direction of rolling It was found that a Corson alloy having a sufficiently high Young's modulus can be obtained, and a manufacturing method for obtaining this crystal orientation was clarified.

以上の知見を基礎として完成した本発明は一側面において、Ni及びCoのうち一種以上を0.8〜5.0質量%、Siを0.2〜1.5質量%含有し、残部が銅及び不可避的不純物からなる圧延材であり、該圧延材の表面においてCube方位から10°以内の方位を持つ領域の面積率であるCube方位{001}<100>の面積率が5〜80%であり、板厚に対し45〜55%の深さの断面において、<100>方向がTDと成す角度が10°以内である領域の面積率である<100>方向が圧延材の幅方向(TD)に配向する結晶の面積率が50%以下であるコルソン合金である。

The present invention completed on the basis of the above knowledge, in one aspect, contains 0.8 to 5.0 mass% of one or more of Ni and Co, 0.2 to 1.5 mass% of Si, and the balance is copper. And an area ratio of a Cube orientation {001} <100> that is an area ratio of a region having an orientation within 10 ° from the Cube orientation on the surface of the rolled material is 5 to 80%. Yes, in a cross section having a depth of 45 to 55% with respect to the plate thickness, the <100> direction which is the area ratio of the region where the angle formed by the <100> direction and TD is within 10 ° is the width direction of the rolled material (TD ) Is a Corson alloy having an area ratio of crystals oriented to 50% or less.

本発明に係るコルソン合金の一実施形態においては、Sn、Zn、Mg、Fe、Ti、Zr、Cr、Al、P、Mn及びAgのうち1種以上を総量で0.005〜3.0質量%含有する。   In one embodiment of the Corson alloy according to the present invention, a total amount of one or more of Sn, Zn, Mg, Fe, Ti, Zr, Cr, Al, P, Mn, and Ag is 0.005 to 3.0 mass. %contains.

本発明に係るコルソン合金の別の一実施形態においては、圧延方向と直交する方向の引張試験から求めたヤング率が106GPa以上である。   In another embodiment of the Corson alloy according to the present invention, the Young's modulus obtained from a tensile test in a direction orthogonal to the rolling direction is 106 GPa or more.

本発明に係るコルソン合金の更に別の一実施形態においては、圧延方向と直交する方向に採取される端面接触型端子の素材として用いられる。   In yet another embodiment of the Corson alloy according to the present invention, it is used as a material for an end face contact type terminal sampled in a direction orthogonal to the rolling direction.

本発明は別の一側面において、Ni及びCoのうち一種以上を0.8〜5.0質量%、Siを0.2〜1.5質量%含有し、残部が銅及び不可避的不純物からなるインゴットを作製し、前記インゴットを800〜1000℃の温度から厚み3〜20mmまで熱間圧延し、加工度90〜99.8%の冷間圧延を、1パスあたりの加工度の最大値および平均値をそれぞれ20%以下および15%以下として行った後、軟化度0.20〜0.80の予備焼鈍、加工度3〜50%の冷間圧延、700〜950℃で5〜300秒間の溶体化処理、加工度0〜60%の冷間圧延、350〜600℃で2〜20時間の時効処理、加工度0〜50%の冷間圧延を順次行う方法であり、
前記軟化度は軟化度をSとして、
S=(σ0−σ)/(σ0−σ950
で示される、本発明に係るコルソン合金の製造方法である。
ここで、σ0は予備焼鈍前の引張強さであり、σ及びσ950はそれぞれ予備焼鈍後及び950℃で焼鈍後の引張強さである。
In another aspect of the present invention, at least one of Ni and Co is contained in an amount of 0.8 to 5.0 mass%, Si is contained in an amount of 0.2 to 1.5 mass%, and the balance is made of copper and inevitable impurities. An ingot was produced, the ingot was hot-rolled from a temperature of 800 to 1000 ° C. to a thickness of 3 to 20 mm, and cold rolling with a workability of 90 to 99.8% was performed. After setting the values to 20% or less and 15% or less, respectively, pre-annealing with a softening degree of 0.20 to 0.80, cold rolling with a working degree of 3 to 50%, and a solution at 700 to 950 ° C. for 5 to 300 seconds. Is a method of sequentially performing a chemical treatment, cold rolling at a working degree of 0 to 60%, an aging treatment at 350 to 600 ° C. for 2 to 20 hours, and a cold rolling at a working degree of 0 to 50%.
The softening degree is defined as S,
S = (σ 0 −σ) / (σ 0 −σ 950 )
It is a manufacturing method of the Corson alloy based on this invention shown by these.
Here, σ 0 is the tensile strength before pre-annealing, and σ and σ 950 are the tensile strength after pre-annealing and after annealing at 950 ° C., respectively.

本発明に係るコルソン合金の製造方法の一実施形態においては、前記インゴットが、Sn、Zn、Mg、Fe、Ti、Zr、Cr、Al、P、Mn及びAgのうち1種以上を総量で0.005〜3.0質量%含有する。   In one embodiment of the method for producing a Corson alloy according to the present invention, the ingot contains one or more of Sn, Zn, Mg, Fe, Ti, Zr, Cr, Al, P, Mn, and Ag in a total amount of 0. 0.005 to 3.0 mass%.

本発明は更に別の一側面において、本発明のコルソン合金を備えた伸銅品である。   In yet another aspect, the present invention is a copper-stretched product provided with the Corson alloy of the present invention.

本発明は更に別の一側面において、本発明のコルソン合金を備えた電子機器部品である。   In still another aspect, the present invention is an electronic device component including the Corson alloy of the present invention.

本発明によれば、優れた曲げ加工性と圧延直交方向の高いヤング率を兼備したコルソン合金及びその製造方法を提供することができる。   ADVANTAGE OF THE INVENTION According to this invention, the Corson alloy which has the outstanding bending workability and the high Young's modulus of a rolling orthogonal direction, and its manufacturing method can be provided.

圧延直交方向に採取される端面接触型端子を説明するための模式図である。It is a schematic diagram for demonstrating the end surface contact type | mold terminal extract | collected in a rolling orthogonal direction. 本発明に係る合金を種々の温度で焼鈍したときの焼鈍温度と引張強さとの関係を示すグラフである。It is a graph which shows the relationship between the annealing temperature when the alloy which concerns on this invention is annealed at various temperatures, and tensile strength.

(Ni、Co及びSiの添加量)
Ni、Co及びSiは、適当な時効処理を行うことにより、Ni−Si、Co−Si、Ni−Co−Si等の金属間化合物として析出する。この析出物の作用により強度が向上し、析出によりCuマトリックス中に固溶したNi、Co及びSiが減少するため導電率が向上する。しかしながら、NiとCoの合計量が0.8質量%未満又はSiが0.2質量%未満になると所望の強度が得られず、反対にNiとCoの合計量が5.0質量%を超えると又はSiが1.5質量%を超えると曲げ加工性が著しく劣化する。このため、本発明に係るコルソン合金では、NiとCoのうち一種以上の添加量は0.8〜5.0質量%とし、Siの添加量は0.2〜1.5質量%としている。NiとCoのうち一種以上の添加量は1.0〜4.0質量%がより好ましく、Siの添加量は0.25〜0.90質量%がより好ましい。
(Addition amount of Ni, Co and Si)
Ni, Co, and Si are precipitated as intermetallic compounds such as Ni—Si, Co—Si, and Ni—Co—Si by performing an appropriate aging treatment. The strength of the precipitate is improved by the action of the precipitate, and Ni, Co, and Si dissolved in the Cu matrix are reduced by the precipitation, so that the conductivity is improved. However, when the total amount of Ni and Co is less than 0.8% by mass or Si is less than 0.2% by mass, the desired strength cannot be obtained. Conversely, the total amount of Ni and Co exceeds 5.0% by mass. When Si exceeds 1.5% by mass, the bending workability is remarkably deteriorated. For this reason, in the Corson alloy which concerns on this invention, the addition amount of 1 or more types is set to 0.8-5.0 mass% among Si and Ni, and the addition amount of Si is 0.2-1.5 mass%. The addition amount of one or more of Ni and Co is more preferably 1.0 to 4.0% by mass, and the addition amount of Si is more preferably 0.25 to 0.90% by mass.

(その他の添加元素)
Sn、Zn、Mg、Fe、Ti、Zr、Cr、Al、P、Mn、Agは強度上昇に寄与する。さらにZnはSnめっきの耐熱剥離性の向上に、Mgは応力緩和特性の向上に、Zr、Cr、Mnは熱間加工性の向上に効果がある。Sn、Zn、Mg、Fe、Ti、Zr、Cr、Al、P、Mn、Agが総量で0.005質量%未満であると上記の効果は得られず、3.0質量%を超えると曲げ加工性が著しく低下する。このため、本発明に係るコルソン合金では、これらの元素を総量で0.005〜3.0質量%含有することが好ましく、0.01〜2.5質量%含有することがより好ましい。
(Other additive elements)
Sn, Zn, Mg, Fe, Ti, Zr, Cr, Al, P, Mn, and Ag contribute to an increase in strength. Furthermore, Zn is effective in improving the heat-resistant peelability of Sn plating, Mg is effective in improving stress relaxation characteristics, and Zr, Cr, and Mn are effective in improving hot workability. If the total amount of Sn, Zn, Mg, Fe, Ti, Zr, Cr, Al, P, Mn, and Ag is less than 0.005% by mass, the above effect cannot be obtained. Workability is significantly reduced. For this reason, in the Corson alloy which concerns on this invention, it is preferable to contain 0.005-3.0 mass% of these elements in a total amount, and it is more preferable to contain 0.01-2.5 mass%.

(ヤング率)
ばね部が圧延方向と直交する端面接触型端子において、ばね接点での充分な接触力を得るために、圧延直交方向のヤング率を106GPa以上に調整することが好ましく、111GPa以上に調整することがより好ましい。
ヤング率の上限値は接触力の点からは規制されないものの、本発明のコルソン合金のヤング率は典型的には130GPa以下、より典型的には120GPa以下である。
なお、前記特許文献4、5においても、発明合金のヤング率が評価されているが、文献4のヤング率は圧延方向と平行に測定された曲げたわみ係数であり、また、文献5では引張試験によりヤング率を求めているものの、その引張試験は圧延方向と平行に行われている。
(Young's modulus)
In the end face contact type terminal where the spring part is orthogonal to the rolling direction, in order to obtain a sufficient contact force at the spring contact, it is preferable to adjust the Young's modulus in the rolling orthogonal direction to 106 GPa or more, and to 111 GPa or more. More preferred.
Although the upper limit of the Young's modulus is not restricted in terms of contact force, the Young's modulus of the Corson alloy of the present invention is typically 130 GPa or less, more typically 120 GPa or less.
The Young's modulus of the invention alloy is also evaluated in Patent Documents 4 and 5, but the Young's modulus of Document 4 is a bending deflection coefficient measured in parallel with the rolling direction. Although the Young's modulus is obtained by this, the tensile test is performed in parallel with the rolling direction.

(結晶方位)
本発明では、EBSD(Electron Back Scatter Diffraction:電子後方散乱回折)による測定値に基づき結晶方位を調整する。ここで、EBSDとは、SEM(Scanning Electron Microscope:走査電子顕微鏡)内で試料に電子線を照射したときに生じる反射電子菊池線回折(菊池パターン)を利用して結晶方位を解析する技術である。電子線は試料表面に照射され、このとき得られる情報は電子線が侵入する数10nmの深さまでの方位情報、すなわち極表層の方位情報である。
コルソン合金の圧延材では、その表面において、Cube方位に配向する結晶の面積率(以下、Cube方位面積率)が増加すると、不均一な変形が抑制され曲げ加工性が向上する。ここで、Cube方位とは、圧延面法線方向(ND)に(001)面が、圧延方向(RD)に(100)面が向いている状態であり、{001}<100>の指数で示される。そこで、良好な曲げ加工性を得るために、表面におけるCube方位面積率を5%以上、好ましくは10%以上、さらに好ましくは20%以上に制御する。
Cube方位面積率の上限値は、曲げ加工性改善の点からは規制されないものの、本発明のコルソン合金のCube方位面積率は典型的には80%以下である。
表面におけるCube方位面積率を高め曲げ加工性を改善した従来のコルソン合金の場合、圧延直交方向のヤング率が106GPaに満たなかった。このヤング率を高めるために、板厚中央部における結晶方位をEBSDによる測定値に基づき調整する。ここで、板厚中央部の結晶方位は、試料の一方の表面からエッチング、機械研磨等により厚み方向に試料を削って板厚中央部の断面を露出させ、この断面に対しEBSB測定を行うことで測定する。板厚中央部とは、板厚に対し45〜55%の位置を指す。
板厚中央部において、<100>方向が圧延材の幅方向(TD)に配向する結晶の面積率を50%以下に制御すると、圧延直交方向のヤング率が106GPa以上になる。<100>方向が圧延材の幅方向(TD)に配向する結晶としては、Cube方位の他、Cube方位がTDを中心軸として回転した方位(例えば{011}<011>、{012}<021>等)が含まれる。
板厚中央部における<100>方向が圧延材の幅方向(TD)に配向する結晶の面積率の下限値は、圧延直交方向のヤング率を高める点からは規制されないものの、本発明のコルソン合金の該合計値は典型的には5%以上である。
(Crystal orientation)
In the present invention, the crystal orientation is adjusted based on a measurement value by EBSD (Electron Back Scatter Diffraction). Here, EBSD is a technique for analyzing crystal orientation using reflected electron Kikuchi line diffraction (Kikuchi pattern) generated when a sample is irradiated with an electron beam in a SEM (Scanning Electron Microscope). . The electron beam is irradiated onto the sample surface, and information obtained at this time is orientation information up to a depth of several tens of nanometers in which the electron beam penetrates, that is, orientation information of the polar surface layer.
In the rolled material of the Corson alloy, when the area ratio of crystals oriented in the Cube orientation on the surface (hereinafter referred to as Cube orientation area ratio) increases, non-uniform deformation is suppressed and bending workability is improved. Here, the Cube orientation is a state in which the (001) plane faces the rolling surface normal direction (ND) and the (100) plane faces the rolling direction (RD), and is an index of {001} <100>. Indicated. Therefore, in order to obtain good bending workability, the Cube orientation area ratio on the surface is controlled to 5% or more, preferably 10% or more, and more preferably 20% or more.
Although the upper limit of the Cube orientation area ratio is not restricted from the viewpoint of improving the bending workability, the Cube orientation area ratio of the Corson alloy of the present invention is typically 80% or less.
In the case of a conventional Corson alloy in which the Cube orientation area ratio on the surface is increased to improve the bending workability, the Young's modulus in the direction perpendicular to the rolling is less than 106 GPa. In order to increase the Young's modulus, the crystal orientation at the center of the plate thickness is adjusted based on the measured value by EBSD. Here, the crystal orientation of the central portion of the plate thickness is determined by etching the sample from one surface of the sample by etching, mechanical polishing, etc. to expose the cross section of the central portion of the plate thickness and performing EBSB measurement on this cross section. Measure with A plate | board thickness center part points out the position of 45 to 55% with respect to plate | board thickness.
When the area ratio of the crystals in which the <100> direction is oriented in the width direction (TD) of the rolled material is controlled to 50% or less in the center portion of the plate thickness, the Young's modulus in the direction perpendicular to the rolling becomes 106 GPa or more. As a crystal in which the <100> direction is oriented in the width direction (TD) of the rolled material, in addition to the Cube orientation, the Cube orientation is an orientation rotated about TD (for example, {011} <011>, {012} <021 > Etc.).
Although the lower limit value of the area ratio of the crystal in which the <100> direction in the central portion of the plate thickness is oriented in the width direction (TD) of the rolled material is not restricted in terms of increasing the Young's modulus in the direction perpendicular to the rolling direction, the Corson alloy of the present invention The total value of is typically 5% or more.

(製造方法)
コルソン合金の一般的な製造プロセスでは、まず溶解炉で電気銅、Ni、Co、Si等の原料を溶解し、所望の組成の溶湯を得る。そして、この溶湯をインゴットに鋳造する。その後、熱間圧延、冷間圧延、溶体化処理、時効処理の順で所望の厚みおよび特性を有する条や箔に仕上げる。熱処理後には、熱処理時に生成した表面酸化膜を除去するために、表面の酸洗や研磨等を行ってもよい。また、高強度化のために、溶体化処理と時効の間や時効後に冷間圧延を行ってもよい。
本発明では、上述の結晶方位を得るために、溶体化処理の前に、熱処理(以下、予備焼鈍ともいう)及び比較的低加工度の冷間圧延(以下、軽圧延ともいう)を行い、さらに熱間圧延と予備焼鈍前との間の冷間圧延の条件を調整する。
予備焼鈍は、熱間圧延後の冷間圧延により形成された圧延組織中に、部分的に再結晶粒を生成させることを目的に行う。圧延組織中の再結晶粒の割合には最適値があり、少なすぎてもまた多すぎても上述の結晶方位が得られない。最適な割合の再結晶粒は、下記に定義する軟化度Sが0.20〜0.80、より好ましくは0.25〜0.75になるよう、予備焼鈍条件を調整することにより得られる。
図2に本発明に係る合金を種々の温度で焼鈍したときの焼鈍温度と引張強さとの関係を例示する。熱電対を取り付けた試料を1000℃の管状炉に挿入し、熱電対で測定される試料温度が所定温度に到達したときに、試料を炉から取り出して水冷し、引張強さを測定したものである。試料到達温度が500〜700℃の間で再結晶が進行し、引張強さが急激に低下している。高温側での引張強さの緩やかな低下は、再結晶粒の成長によるものである。
(Production method)
In a general manufacturing process of a Corson alloy, first, raw materials such as electrolytic copper, Ni, Co, and Si are melted in a melting furnace to obtain a molten metal having a desired composition. Then, this molten metal is cast into an ingot. Thereafter, the strips and foils having desired thickness and characteristics are finished in the order of hot rolling, cold rolling, solution treatment, and aging treatment. After the heat treatment, surface pickling, polishing, or the like may be performed in order to remove the surface oxide film generated during the heat treatment. In order to increase the strength, cold rolling may be performed between the solution treatment and aging or after aging.
In the present invention, in order to obtain the above crystal orientation, before the solution treatment, heat treatment (hereinafter also referred to as pre-annealing) and relatively low work cold rolling (hereinafter also referred to as light rolling), Furthermore, conditions for cold rolling between hot rolling and pre-annealing are adjusted.
The preliminary annealing is performed for the purpose of partially generating recrystallized grains in a rolled structure formed by cold rolling after hot rolling. There is an optimum value for the ratio of recrystallized grains in the rolled structure, and the above-mentioned crystal orientation cannot be obtained if the amount is too small or too large. The optimum proportion of recrystallized grains can be obtained by adjusting the pre-annealing conditions so that the softening degree S defined below is 0.20 to 0.80, more preferably 0.25 to 0.75.
FIG. 2 illustrates the relationship between the annealing temperature and the tensile strength when the alloy according to the present invention is annealed at various temperatures. A sample with a thermocouple attached was inserted into a 1000 ° C. tubular furnace, and when the sample temperature measured by the thermocouple reached a predetermined temperature, the sample was taken out of the furnace, cooled with water, and the tensile strength was measured. is there. Recrystallization proceeds when the sample arrival temperature is 500 to 700 ° C., and the tensile strength is drastically decreased. The gradual decrease in tensile strength on the high temperature side is due to the growth of recrystallized grains.

予備焼鈍における軟化度Sを次式で定義する。
S=(σ0−σ)/(σ0−σ950
ここで、σ0は焼鈍前の引張強さであり、σおよびσ950はそれぞれ予備焼鈍後および950℃で焼鈍後の引張強さである。950℃という温度は、本発明に係る合金を950℃で焼鈍すると安定して完全再結晶することから、再結晶後の引張強さを知るための基準温度として採用している。
軟化度が0.2〜0.8の範囲から外れると、圧延材表面において、Cube方位の面積率が5%未満になる。予備焼鈍の温度および時間は特に制約されず、Sを上記範囲に調整することが重要である。一般的には、連続焼鈍炉を用いる場合には炉温400〜750℃で5秒間〜10分間の範囲、バッチ焼鈍炉を用いる場合には炉温350〜600℃で30分間〜20時間の範囲で行われる。
なお、予備焼鈍条件の設定は、次の手順により行うことができる。
(1)予備焼鈍前の材料の引張強さ(σ0)を測定する。
(2)予備焼鈍前の材料を950℃で焼鈍する。具体的には、熱電対を取り付けた材料を1000℃の管状炉に挿入し、熱電対で測定される試料温度が950℃に到達したときに、試料を炉から取り出して水冷する。
(3)上記950℃焼鈍後の材料の引張強さ(σ950)を求める。
(4)例えば、σ0が800MPa、σ950が300MPaの場合、軟化度0.20及び0.80に相当する引張強さは、それぞれ700MPa及び400MPaである。
(5)焼鈍後の引張強さが400〜700MPaとなるように、予備焼鈍の条件を求める。
The softening degree S in the pre-annealing is defined by the following equation.
S = (σ 0 −σ) / (σ 0 −σ 950 )
Here, σ 0 is the tensile strength before annealing, and σ and σ 950 are the tensile strength after preliminary annealing and after annealing at 950 ° C., respectively. The temperature of 950 ° C. is adopted as a reference temperature for knowing the tensile strength after recrystallization because the alloy according to the present invention is stably completely recrystallized when annealed at 950 ° C.
If the softening degree is out of the range of 0.2 to 0.8, the area ratio of the Cube orientation is less than 5% on the surface of the rolled material. The temperature and time of the pre-annealing are not particularly limited, and it is important to adjust S to the above range. Generally, when a continuous annealing furnace is used, the furnace temperature ranges from 400 to 750 ° C. for 5 seconds to 10 minutes, and when a batch annealing furnace is used, the furnace temperature ranges from 350 to 600 ° C. for 30 minutes to 20 hours. Done in
The pre-annealing conditions can be set by the following procedure.
(1) Measure the tensile strength (σ 0 ) of the material before pre-annealing.
(2) The material before preliminary annealing is annealed at 950 ° C. Specifically, the material to which the thermocouple is attached is inserted into a 1000 ° C. tubular furnace, and when the sample temperature measured by the thermocouple reaches 950 ° C., the sample is taken out of the furnace and water-cooled.
(3) Obtain the tensile strength (σ 950 ) of the material after annealing at 950 ° C.
(4) For example, when σ 0 is 800 MPa and σ 950 is 300 MPa, the tensile strengths corresponding to the softening degrees of 0.20 and 0.80 are 700 MPa and 400 MPa, respectively.
(5) Pre-annealing conditions are determined so that the tensile strength after annealing is 400 to 700 MPa.

上記予備焼鈍の後、溶体化処理に先立ち、加工度が3〜50%、より好ましくは7〜50%の軽圧延を行う。加工度R(%)は次式で定義する。
R=(t0−t)/t0×100(t0:圧延前の板厚,t:圧延後の板厚)
加工度が3〜50%の範囲から外れると、圧延材表面においてCube方位の面積率が5%未満になる。
上記予備焼鈍および軽圧延の実施に加え、熱間圧延と予備焼鈍との間の冷間圧延の条件を調整することにより、表面ではCube方位の面積率が5%以上で、板厚中央部では<100>方向が圧延材のTDに配向する結晶の面積率が50%以下である結晶方位の特徴を付与することができる。
該冷間圧延では、一対の圧延ロール間に材料を繰り返し通過させ、目標の板厚に仕上げてゆく。結晶方位には、該冷間圧延における総加工度と1パスあたりの加工度が影響を及ぼす。ここで、総加工度Rは、一般的にいう加工度を指し、上述したRと同じ式で定義される。また、1パスあたりの加工度r(%)とは、圧延ロールを1回通過したときの板厚減少率であり、r=(T0−T)/T0×100(T0:圧延ロール通過前の厚み、T:圧延ロール通過後の厚み)で与えられる。
総加工度Rは90〜99.8%とする。Rが90%未満になると、表面でのCube方位の面積率が5%未満になる。Rが99.8%を超えると、圧延材のエッジ等に割れが発生し、圧延中の材料が破断することがある。より好ましい加工度は95〜99%である。
1パスあたりの加工度rについては、全パスのうちの最大値(rmax)を20%以下とし、全パスの平均値(rave)を15%以下とする。この条件から外れると、板厚中央部において<100>方向が圧延材のTDに配向する結晶の面積率が50%を超える。raveの下限値については、結晶方位の点からは制限されないが、raveが小さくなると圧延に時間がかかり生産効率が低下するため、raveは10%以上にすることが好ましい。
After the pre-annealing, prior to the solution treatment, light rolling with a workability of 3 to 50%, more preferably 7 to 50% is performed. The processing degree R (%) is defined by the following equation.
R = (t 0 −t) / t 0 × 100 (t 0 : plate thickness before rolling, t: plate thickness after rolling)
When the workability is out of the range of 3 to 50%, the area ratio of the Cube orientation on the rolled material surface becomes less than 5%.
In addition to the pre-annealing and the light rolling, by adjusting the conditions of the cold rolling between the hot rolling and the pre-annealing, the area ratio of the Cube orientation is 5% or more on the surface, The crystal orientation characteristic in which the area ratio of crystals whose <100> direction is oriented to the TD of the rolled material is 50% or less can be imparted.
In the cold rolling, the material is repeatedly passed between a pair of rolling rolls to finish the target plate thickness. The crystal orientation is affected by the total degree of work in cold rolling and the degree of work per pass. Here, the total working degree R indicates a working degree in general and is defined by the same formula as R described above. Further, the processing degree r (%) per pass is a sheet thickness reduction rate when the rolling roll passes once, and r = (T 0 −T) / T 0 × 100 (T 0 : rolling roll) Thickness before passing, T: Thickness after passing the rolling roll).
The total processing degree R is 90 to 99.8%. When R is less than 90%, the area ratio of the Cube orientation on the surface is less than 5%. If R exceeds 99.8%, cracks may occur at the edges of the rolled material, and the material being rolled may break. A more preferable degree of processing is 95 to 99%.
Regarding the processing degree r per pass, the maximum value (r max ) of all passes is set to 20% or less, and the average value (r ave ) of all passes is set to 15% or less. If it deviates from this condition, the area ratio of the crystal in which the <100> direction is oriented to the TD of the rolled material in the central portion of the plate thickness exceeds 50%. The lower limit of r ave, but are not limited in terms of crystal orientation, since the time rolling and r ave becomes smaller consuming production efficiency decreases, r ave is preferably set to 10% or more.

本発明合金の製造方法を工程順に列記すると次のようになる。
(1)インゴットの鋳造(厚み20〜300mm)
(2)熱間圧延(温度800〜1000℃、厚み3〜20mmまで)
(3)冷間圧延(R=90〜99.8%、rmax≦20%、rave≦15%)
(4)予備焼鈍(軟化度:S=0.20〜0.80)
(5)軽圧延(加工度3〜50%)
(6)溶体化処理(700〜950℃で5〜300秒)
(7)冷間圧延(加工度0〜60%)
(8)時効処理(350〜600℃で2〜20時間)
(9)冷間圧延(加工度0〜50%)
(10)歪取り焼鈍(300〜700℃で5秒〜10時間)
It is as follows when the manufacturing method of this invention alloy is listed in order of a process.
(1) Ingot casting (thickness 20 to 300 mm)
(2) Hot rolling (temperature 800 to 1000 ° C., thickness 3 to 20 mm)
(3) Cold rolling (R = 90-99.8%, r max ≦ 20%, r ave ≦ 15%)
(4) Pre-annealing (degree of softening: S = 0.20 to 0.80)
(5) Light rolling (working degree 3-50%)
(6) Solution treatment (700 to 950 ° C. for 5 to 300 seconds)
(7) Cold rolling (working degree 0-60%)
(8) Aging treatment (2 to 20 hours at 350 to 600 ° C.)
(9) Cold rolling (working degree 0-50%)
(10) Strain relief annealing (at 300 to 700 ° C. for 5 seconds to 10 hours)

冷間圧延(7)及び(9)は高強度化のために任意に行うものである。ただし、圧延加工度の増加とともに強度が増加する反面、表面でのCube方位の面積率が減少する傾向にある。冷間圧延(7)及び(9)におけるそれぞれの加工度が上記上限値を超えると、表面でのCube方位の面積率が5%未満になり曲げ加工性が劣化する。
歪取り焼鈍(10)は、冷間圧延(9)を行う場合にこの冷間圧延で低下するばね限界値等を回復させるために任意に行うものである。歪取り焼鈍(10)の有無に関わらず、結晶方位制御により良好な曲げ加工性と圧延直交方向の高いヤング率とが両立するという本発明の効果は得られる。歪取り焼鈍(10)は行っても良いし行わなくても良い。
なお、工程(2)、(6)及び(8)については、コルソン合金の一般的な製造条件を選択すればよい。
Cold rolling (7) and (9) is optionally performed to increase the strength. However, while the strength increases as the rolling degree increases, the area ratio of the Cube orientation on the surface tends to decrease. If the respective working degrees in the cold rolling (7) and (9) exceed the upper limit, the area ratio of the Cube orientation on the surface becomes less than 5% and the bending workability deteriorates.
The strain relief annealing (10) is optionally performed in order to recover the spring limit value and the like which are lowered by the cold rolling when the cold rolling (9) is performed. Regardless of the presence or absence of strain relief annealing (10), the effect of the present invention that both good bending workability and high Young's modulus in the orthogonal direction of rolling can be achieved by controlling the crystal orientation. The strain relief annealing (10) may or may not be performed.
In addition, what is necessary is just to select the general manufacturing conditions of a Corson alloy about process (2), (6) and (8).

本発明のコルソン合金は種々の伸銅品、例えば板、条及び箔に加工することができ、更に、本発明のコルソン合金は、リードフレーム、コネクタ、ピン、端子、リレー、スイッチ、二次電池用箔材等の電子機器部品等に使用することができる。特に、厳しいGood Wayの曲げ加工が施される部品、およびばね部が圧延直交方向に採取され端面接触で電気接点を得る部品(図1参照)として好適である。ここでいう直交する方向とは、圧延方向とばね部方向とが成す角度が60〜120度の場合を指す。当該角度が70〜110度であれば発明の効果がより発揮され、80〜100度であれば発明の効果がさらによく発揮される。   The Corson alloy of the present invention can be processed into various copper products, for example, plates, strips and foils. Further, the Corson alloy of the present invention is a lead frame, connector, pin, terminal, relay, switch, secondary battery. It can be used for electronic device parts such as foil materials. In particular, it is suitable as a part to be subjected to severe Good Way bending, and a part (see FIG. 1) in which a spring part is taken in a direction perpendicular to rolling to obtain an electrical contact by end face contact. The direction orthogonal here refers to the case where the angle formed by the rolling direction and the spring portion direction is 60 to 120 degrees. If the said angle is 70-110 degree | times, the effect of invention will be exhibited more, and if it is 80-100 degree | times, the effect of invention will be exhibited more fully.

以下に本発明の実施例を比較例と共に示すが、これらの実施例は本発明及びその利点をよりよく理解するために提供するものであり、発明が限定されることを意図するものではない。   Examples of the present invention will be described below together with comparative examples, but these examples are provided for better understanding of the present invention and its advantages, and are not intended to limit the invention.

(実施例1)
Ni:2.6質量%、Si:0.58質量%、Sn:0.5質量%、およびZn:0.4質量%を含有し残部が銅及び不可避的不純物からなる合金を実験材料とし、予備焼鈍条件、軽圧延条件及び予備焼鈍前の圧延条件と結晶方位との関係、さらに結晶方位が製品の曲げ性および機械的特性に及ぼす影響を検討した。
高周波溶解炉にてアルゴン雰囲気中で内径60mm、深さ200mmの黒鉛るつぼを用い電気銅2.5kgを溶解した。上記合金組成が得られるよう合金元素を添加し、溶湯温度を1300℃に調整した後、鋳鉄製の鋳型に鋳込み、厚さ30mm、幅60mm、長さ120mmのインゴットを製造した。このインゴットを、次の工程順で加工し、板厚0.15mmの製品試料を作製した。
(1)熱間圧延:950℃で3時間加熱したインゴットを所定の厚みまで圧延した。圧延後の材料は直ちに水冷した。
(2)研削:熱間圧延で生成した酸化スケールをグラインダーで除去した。研削量は片面あたり0.5mmとした。
(3)冷間圧延:種々の総加工度(R)および1パスあたりの加工度(r)で、所定の厚みまで冷間圧延した。
(4)予備焼鈍:所定温度に調整した電気炉に試料を挿入し、所定時間保持した後、試料を水槽に入れ冷却した。
(5)軽圧延:種々の圧延加工度で、厚み0.25mmまで冷間圧延を行った。
(6)溶体化処理:800℃に調整した電気炉に試料を挿入し、10秒間保持した後、試料を水槽に入れ冷却した。溶体化処理後の結晶粒径は約10μmであった。
(7)時効処理:電気炉を用い450℃で5時間、Ar雰囲気中で加熱した。
(8)冷間圧延:0.25mmから0.20mmまで加工度20%で冷間圧延した。
(9)歪取り焼鈍:400℃に調整した電気炉に試料を挿入し、10秒間保持した後、試料を大気中に放置し冷却した。
Example 1
An alloy containing Ni: 2.6% by mass, Si: 0.58% by mass, Sn: 0.5% by mass, and Zn: 0.4% by mass with the balance being copper and inevitable impurities is used as an experimental material. The relationship between pre-annealing conditions, light rolling conditions, rolling conditions before pre-annealing and crystal orientation, and the effect of crystal orientation on the bendability and mechanical properties of the products were investigated.
In a high frequency melting furnace, 2.5 kg of electrolytic copper was melted using a graphite crucible having an inner diameter of 60 mm and a depth of 200 mm in an argon atmosphere. Alloy elements were added to obtain the above alloy composition, the melt temperature was adjusted to 1300 ° C., and then cast into a cast iron mold to produce an ingot having a thickness of 30 mm, a width of 60 mm, and a length of 120 mm. The ingot was processed in the following process order to produce a product sample with a plate thickness of 0.15 mm.
(1) Hot rolling: An ingot heated at 950 ° C. for 3 hours was rolled to a predetermined thickness. The material after rolling was immediately cooled with water.
(2) Grinding: The oxide scale generated by hot rolling was removed with a grinder. The grinding amount was 0.5 mm per side.
(3) Cold rolling: Cold rolling was performed to a predetermined thickness at various total processing degrees (R) and processing degrees per pass (r).
(4) Pre-annealing: The sample was inserted into an electric furnace adjusted to a predetermined temperature and held for a predetermined time, and then the sample was placed in a water bath and cooled.
(5) Light rolling: Cold rolling was performed at various rolling degrees to a thickness of 0.25 mm.
(6) Solution treatment: The sample was inserted into an electric furnace adjusted to 800 ° C. and held for 10 seconds, and then the sample was placed in a water bath and cooled. The crystal grain size after the solution treatment was about 10 μm.
(7) Aging treatment: Heated in an Ar atmosphere at 450 ° C. for 5 hours using an electric furnace.
(8) Cold rolling: Cold rolling was performed at a workability of 20% from 0.25 mm to 0.20 mm.
(9) Strain relief annealing: The sample was inserted into an electric furnace adjusted to 400 ° C. and held for 10 seconds, and then the sample was left in the air and cooled.

予備焼鈍後の試料および製品試料(この場合は歪取り焼鈍上がり)について、次の評価を行った。
(予備焼鈍での軟化度評価)
予備焼鈍前および予備焼鈍後の試料につき、引張試験機を用いてJIS Z 2241に準拠し圧延方向と平行に引張強さを測定し、それぞれの値をσ0およびσとした。また、950℃焼鈍試料を前記手順(1000℃の炉に挿入し試料が950℃に到達したときに水冷)で作製し、圧延方向と平行に引張強さを同様に測定しσ950を求めた。σ0、σ、σ950から、軟化度Sを求めた。
S=(σ0−σ)/(σ0−σ950
なお、引張試験片はJIS Z 2201に規定する13B号試験片とした。
The following evaluation was performed on the sample after the pre-annealing and the product sample (in this case, the strain relief annealing was completed).
(Evaluation of softening degree in preliminary annealing)
About the sample before pre-annealing and after pre-annealing, the tensile strength was measured in parallel with the rolling direction according to JIS Z 2241 using a tensile tester, and the respective values were set to σ 0 and σ. Further, a 950 ° C. annealed sample was prepared by the above procedure (water cooling when the sample reached 950 ° C. when inserted into a 1000 ° C. furnace), and the tensile strength was measured in parallel with the rolling direction to obtain σ 950 . . The softening degree S was determined from σ 0 , σ, and σ 950 .
S = (σ 0 −σ) / (σ 0 −σ 950 )
The tensile test piece was a No. 13B test piece specified in JIS Z 2201.

(EBSD)
結晶粒を200個以上含む、500μm四方の試料面積に対し、0.5μmのステップでスキャンし、結晶方位分布を測定し、結晶方位密度関数解析を行った。
表層の結晶方位を解析するための試料として、試料表面を機械研摩して圧延模様等による微小凹凸を除去した後、コロイダルシリカ砥粒を使用し鏡面に仕上げた。これによる表面の研摩深さは2〜3μmの範囲であった。その後、Cube方位から10°以内の方位を持つ領域の面積を求め、この面積を全測定面積で除し、面積率とした。
板厚中央部の結晶方位を解析するための試料として、一方の表面から板厚中央部までを塩化第二鉄溶液を用いたエッチングにより除去し、次に、機械研摩と電解研磨により鏡面に仕上げた。仕上げ後の試料の厚みは、元の板厚に対し45〜55%の範囲であった。その後、結晶の<100>方向がTDと成す角度が10°以内である領域の面積を求め、この面積を全測定面積で除し、<100>方向がTDに配向する結晶の面積率とした。
なお、EBSDによる方位解析において得られる情報は、電子線が試料に侵入する数10nmの深さまでの方位情報を含んでいるが、測定している広さに対して充分に小さいため、面積率として記載した。
(EBSD)
A sample area of 500 μm square containing 200 or more crystal grains was scanned in steps of 0.5 μm, crystal orientation distribution was measured, and crystal orientation density function analysis was performed.
As a sample for analyzing the crystal orientation of the surface layer, the sample surface was mechanically polished to remove minute irregularities due to a rolling pattern or the like, and then finished to a mirror surface using colloidal silica abrasive grains. The surface polishing depth was in the range of 2 to 3 μm. Thereafter, the area of a region having an azimuth within 10 ° from the Cube azimuth was determined, and this area was divided by the total measurement area to obtain an area ratio.
As a sample for analyzing the crystal orientation at the center of the plate thickness, the part from one surface to the center of the plate thickness is removed by etching using a ferric chloride solution, and then mirror polished by mechanical polishing and electrolytic polishing. It was. The thickness of the sample after finishing was in the range of 45 to 55% with respect to the original plate thickness. Then, the area of the region where the angle formed by the <100> direction of the crystal and the TD is within 10 ° is obtained, and this area is divided by the total measurement area to obtain the area ratio of the crystal in which the <100> direction is oriented to TD. .
Note that the information obtained in the azimuth analysis by EBSD includes azimuth information up to a depth of several tens of nanometers at which the electron beam penetrates into the sample, but is sufficiently small with respect to the area being measured. Described.

(製品の引張り試験)
JIS Z 2201に規定する13B号試験片を引張方向が圧延方向と平行になるように採取し、JIS Z 2241に準拠して圧延方向と平行に引張試験を行い、引張強さを求めた。
(Product tensile test)
A specimen No. 13B specified in JIS Z 2201 was taken so that the tensile direction was parallel to the rolling direction, and a tensile test was performed in parallel with the rolling direction in accordance with JIS Z 2241 to determine the tensile strength.

(製品の曲げ試験)
より厳しい曲げ加工を想定し、W曲げ等の90度曲げ試験ではなく、180度曲げ試験を行った。
幅が10mmで、長さが30mm以上の短冊形試料を、その長手方向が圧延方向と平行になるように採取した。JIS Z 2248の押し曲げ法に準拠し、内側半径をSとし、Good Way方向(曲げ軸が圧延方向と直交)に180度曲げ試験を行った。曲げ断面を機械研磨及びバフ研磨で鏡面に仕上げ、光学顕微鏡で割れの有無を観察した。Sが0.05、0.10、0.15、0.20、0.25、0.30、0.40、0.50、0.60、0.80、1.0mmの曲げを行うための試験ジグを準備し、割れが発生しない最小のS(Smin)を求めた。Sminを板厚(d)で割った値(Smin/d)を曲げ加工性の指標とした。Smin/dが1.0以下であれば、良好なGood Wayの曲げ加工性が得られたと判断した。
(Product bending test)
A 180 degree bending test was performed instead of a 90 degree bending test such as a W bending, assuming a more severe bending process.
A strip-shaped sample having a width of 10 mm and a length of 30 mm or more was collected so that the longitudinal direction thereof was parallel to the rolling direction. A 180 ° bending test was performed in the Good Way direction (the bending axis was perpendicular to the rolling direction) with the inner radius set to S in accordance with the JIS Z 2248 push bending method. The bent section was mirror-finished by mechanical polishing and buffing, and the presence or absence of cracks was observed with an optical microscope. For bending with S of 0.05, 0.10, 0.15, 0.20, 0.25, 0.30, 0.40, 0.50, 0.60, 0.80, 1.0 mm The minimum S (S min ) at which cracks do not occur was prepared. A value (S min / d) obtained by dividing S min by the plate thickness (d) was used as an index of bending workability. If S min / d was 1.0 or less, it was judged that good Good Way bending workability was obtained.

(製品のヤング率)
JIS Z 2201に規定する13B号試験片を引張方向が圧延方向と直交するように採取し、引張試験を行った。得られた応力歪曲線から、弾性範囲における直線部の傾きを求め、この値をヤング率とした。
評価結果を表1及び表2に示す。



(Young's modulus of the product)
A No. 13B specimen specified in JIS Z 2201 was sampled so that the tensile direction was perpendicular to the rolling direction, and a tensile test was performed. From the obtained stress-strain curve, the slope of the straight line portion in the elastic range was obtained, and this value was taken as the Young's modulus.
The evaluation results are shown in Tables 1 and 2.



Figure 0006196757
Figure 0006196757

Figure 0006196757
Figure 0006196757

発明例は、いずれも本発明が規定する条件で予備焼鈍前の冷間圧延、予備焼鈍および軽圧延を行ったものであり、板厚表面および中央部の結晶方位が本発明の規定を満たし、Good Wayの180度曲げのSmin/dが1.0以下となり、同時に106MPa以上の圧延直交方向のヤング率が得られた。
比較例1〜3は、予備焼鈍前の冷間圧延における1パス当たりの加工度(r)の条件が本発明の規定から外れたものである。比較例1ではraveが過大、比較例2ではrmaxが過大、比較例3ではrave、rmaxとも過大である。これらでは、板厚中央において<100>方向が圧延材のTDに配向する結晶の面積率が50%を超え、圧延直交方向のヤング率が106GPaに満たなかった。
Inventive examples are all subjected to cold rolling, pre-annealing and light rolling before pre-annealing under the conditions defined by the present invention, and the crystallographic orientation of the plate thickness surface and the central portion satisfies the provisions of the present invention, Good Way's 180 degree bend S min / d was 1.0 or less, and at the same time, Young's modulus in the orthogonal direction of rolling of 106 MPa or more was obtained.
In Comparative Examples 1 to 3, the condition of the degree of processing (r) per pass in cold rolling before pre-annealing deviates from the definition of the present invention. In comparative example 1, r ave is excessive, in comparative example 2, r max is excessive, and in comparative example 3, both r ave and r max are excessive. In these, the area ratio of the crystals in which the <100> direction is aligned with the TD of the rolled material at the center of the plate thickness exceeded 50%, and the Young's modulus in the rolling orthogonal direction was less than 106 GPa.

表3は、予備焼鈍の直前に、9.0mmから0.357mmまで総加工度(R)が96.0%の圧延を行った、発明例3および比較例1〜3について、各パスの上がりの板厚および各パスの加工度(r)を比較したものである。   Table 3 shows the increase in each pass for Invention Example 3 and Comparative Examples 1 to 3 in which rolling was performed at a total workability (R) of 96.0% from 9.0 mm to 0.357 mm immediately before the preliminary annealing. The plate thickness and the degree of processing (r) of each pass are compared.

Figure 0006196757
Figure 0006196757

従来のコルソン合金の冷間圧延(特に工程の前半に行なう粗圧延)では、生産性を重視し、比較例3のように各パスの加工度を高く設定し、少ないパス回数で圧延を行うことが通常であった。
比較例4は、予備焼鈍前の冷間圧延における総加工度(R)が90.0%を下回ったものである。表面でのCube方位の面積率が5%未満となったため、曲げ加工性が悪化し、Good Wayの180度曲げのSmin/dが1.0を超えた。
比較例5では予備焼鈍の軟化度が0.20を下回り、比較例6では予備焼鈍での軟化度が0.80を超えた。また、比較例7では軽圧延の加工度が3%を下回り、比較例8では軽圧延の加工度が50%を超えた。比較例5〜8では、表面でのCube方位面積率が5%未満となったため、曲げ加工性が悪化し、Good Wayの180度曲げのSmin/dが1.0を超えた。
比較例9は、従来の一般的なコルソン合金の製造方法に準じて製造されたものである。予備焼鈍および軽圧延は行わず、熱間圧延と溶体化処理との間の冷間圧延では、生産性を重視しraveを15%超、rmaxを20%超に設定している。表面においてCube方位の面積率が5%を下回り、板厚中央において<100>方向が圧延材のTDに配向する結晶の面積率が50%以下であった。Good Wayの180度曲げのSmin/dは2.5と曲げ加工性が悪く、反面、圧延直交方向のヤング率は140GPaを超える高い値であった。
比較例10〜14は、当該合金組成のコルソン合金を特許文献2〜5に記載された製造方法に準じて製造したものである。ここで、熱間圧延と予備焼鈍(中間焼鈍)との間の冷間圧延では、生産性を重視しraveを15%超、rmaxを20%超に設定している。
比較例10は、特許文献2に準じて製造したものであり、表2に記載した以外の条件として、熱間圧延は950℃から400℃に温度を下げながら行い、予備(中間)焼鈍では導電率を1.5倍以上に硬さを0.8倍以下に調整している。この条件で製造することで、表面においてCube方位の面積率が5%以上になったが、板厚中央において<100>方向が圧延材のTDに配向する結晶の面積率が50%を超えた。その結果、曲げ加工性は良好であったが、圧延直交方向のヤング率が106GPaに満たなかった。
比較例11は、特許文献3に準じて製造したものであり、表2に記載した以外の条件として、溶体化処理では400〜750℃の範囲の昇温速度を2〜50℃/秒とした。この条件で製造することで、Cube方位の面積率が5〜60%、Brass方位及びCopper方位の面積率が20%以下となった。一方、板厚中央において<100>方向が圧延材のTDに配向する結晶の面積率が50%を超えた。その結果、曲げ加工性は良好であったが、圧延直交方向のヤング率が106GPaに満たなかった。
比較例12は、特許文献4に準じて製造したものであり、表2に記載した以外の条件として、予備焼鈍において導電率を20〜45%IACSの範囲に調整した。この条件で製造することで、板厚方向の中央部において、Cube方位の面積率を10〜80%、Brass方位及びCopper方位の面積率をともに20%以下になり、ノッチ曲げが可能になった。一方、板厚中央において<100>方向が圧延材のTDに配向する結晶の面積率が50%を超えた。その結果、曲げ加工性は良好であったが、圧延直交方向のヤング率が106GPaに満たなかった。
比較例13は、特許文献5に準じて製造したものであり、表2に記載した以外の条件として、熱間圧延では1パスの加工率を30%以下とし各パス間の保持時間を20〜100秒とした。また、溶体化処理を900℃で行い、平均結晶粒径を12〜100μmの範囲に調整した。この条件で製造することで、W0/W4が0.8〜1.5、W0が5〜48%(W0およびW4は、それぞれ材料の表層および深さ位置で全体の1/4の位置でのCube方位面積率)となり、1.0mm幅の試験片による180度密着曲げが可能となり(試験片幅が細いほど曲げ加工は容易)、150℃で1000時間加熱したときの応力緩和値が30%以下になった。一方、板厚中央において<100>方向が圧延材のTDに配向する結晶の面積率が50%を超えた。その結果、曲げ加工性(試験片幅10mm)は良好であったが、圧延直交方向のヤング率が106GPaに満たなかった。
比較例14は、特許文献6に準じて製造したものであり、表2に記載した以外の条件として、熱間圧延後に350℃まで徐冷した。この条件で製造することで、圧延方向に向く(100)面の面積率が30%以上となり、圧延平行方向のヤング率が110GPa以下になった。一方、表面においてCube方位の面積率が5%をわずかに下回り、板厚中央において<100>方向が圧延材のTDに配向する結晶の面積率が50%を超えた。その結果、曲げ加工性は若干悪く、圧延直交方向のヤング率は106GPaに満たなかった。
In conventional cold rolling of Corson alloy (especially rough rolling performed in the first half of the process), emphasis is placed on productivity, the degree of processing of each pass is set high as in Comparative Example 3, and rolling is performed with a small number of passes. Was normal.
In Comparative Example 4, the total degree of work (R) in cold rolling before pre-annealing is less than 90.0%. Since the area ratio of the Cube orientation on the surface was less than 5%, the bending workability deteriorated, and the Smin / d of 180 degrees bending of Good Way exceeded 1.0.
In Comparative Example 5, the pre-annealing softening degree was less than 0.20, and in Comparative Example 6, the pre-annealing softening degree exceeded 0.80. In Comparative Example 7, the light rolling workability was less than 3%, and in Comparative Example 8, the light rolling workability exceeded 50%. In Comparative Examples 5 to 8, since the Cube orientation area ratio on the surface was less than 5%, the bending workability was deteriorated, and the S min / d of 180 degrees bending of Good Way exceeded 1.0.
The comparative example 9 is manufactured according to the manufacturing method of the conventional general Corson alloy. Pre-annealing and light rolling are not performed, and in cold rolling between hot rolling and solution treatment, productivity is emphasized and r ave is set to more than 15% and r max is set to more than 20%. The area ratio of the Cube orientation was less than 5% on the surface, and the area ratio of crystals with the <100> direction oriented to the TD of the rolled material was 50% or less at the center of the plate thickness. Good Way 180 degree bending Smin / d is 2.5, and bending workability is bad, On the other hand, the Young's modulus of a rolling orthogonal direction was a high value exceeding 140 GPa.
In Comparative Examples 10 to 14, Corson alloys having the alloy compositions are manufactured according to the manufacturing methods described in Patent Documents 2 to 5. Here, in cold rolling between hot rolling and pre-annealing (intermediate annealing), productivity is emphasized and r ave is set to more than 15% and r max is set to more than 20%.
Comparative Example 10 was manufactured according to Patent Document 2, and as conditions other than those described in Table 2, hot rolling was performed while lowering the temperature from 950 ° C. to 400 ° C., and conductive in the preliminary (intermediate) annealing. The rate is adjusted to 1.5 times or more and the hardness is adjusted to 0.8 times or less. By manufacturing under this condition, the area ratio of the Cube orientation on the surface became 5% or more, but the area ratio of the crystals in which the <100> direction was aligned with the TD of the rolled material exceeded 50% at the center of the plate thickness. . As a result, the bending workability was good, but the Young's modulus in the direction perpendicular to the rolling was less than 106 GPa.
Comparative Example 11 was manufactured according to Patent Document 3, and as a condition other than those described in Table 2, the temperature increase rate in the range of 400 to 750 ° C. was 2 to 50 ° C./second in the solution treatment. . By manufacturing under these conditions, the area ratio of Cube orientation was 5 to 60%, and the area ratio of Brass orientation and Copper orientation was 20% or less. On the other hand, the area ratio of crystals in which the <100> direction is aligned with the TD of the rolled material at the center of the plate thickness exceeded 50%. As a result, the bending workability was good, but the Young's modulus in the direction perpendicular to the rolling was less than 106 GPa.
The comparative example 12 was manufactured according to patent document 4, and the electrical conductivity was adjusted to the range of 20 to 45% IACS in pre-annealing as conditions other than those described in Table 2. By manufacturing under these conditions, the area ratio of the Cube orientation is 10 to 80%, the area ratios of the Brass orientation and the Copper orientation are both 20% or less, and notch bending is possible at the center in the thickness direction. . On the other hand, the area ratio of crystals in which the <100> direction is aligned with the TD of the rolled material at the center of the plate thickness exceeded 50%. As a result, the bending workability was good, but the Young's modulus in the direction perpendicular to the rolling was less than 106 GPa.
Comparative Example 13 was manufactured according to Patent Document 5, and as a condition other than those described in Table 2, in hot rolling, the processing rate of one pass was 30% or less, and the holding time between each pass was 20 to 20%. 100 seconds. Further, the solution treatment was performed at 900 ° C., and the average crystal grain size was adjusted to a range of 12 to 100 μm. By manufacturing under these conditions, W0 / W4 is 0.8 to 1.5, W0 is 5 to 48% (W0 and W4 are the surface layer and depth position of the material, respectively, at the 1/4 position of the whole. Cube orientation area ratio), and 180-degree contact bending with a 1.0 mm wide test piece is possible (the narrower the test piece width, the easier the bending process is), and the stress relaxation value when heated at 150 ° C. for 1000 hours is 30%. It became the following. On the other hand, the area ratio of crystals in which the <100> direction is aligned with the TD of the rolled material at the center of the plate thickness exceeded 50%. As a result, the bending workability (test specimen width 10 mm) was good, but the Young's modulus in the direction perpendicular to the rolling was less than 106 GPa.
The comparative example 14 was manufactured according to patent document 6, and it annealed to 350 degreeC after hot rolling as conditions other than having described in Table 2. FIG. By manufacturing under these conditions, the area ratio of the (100) plane facing the rolling direction was 30% or more, and the Young's modulus in the rolling parallel direction was 110 GPa or less. On the other hand, the area ratio of the Cube orientation on the surface was slightly less than 5%, and the area ratio of the crystals in which the <100> direction was aligned with the TD of the rolled material exceeded 50% at the center of the plate thickness. As a result, the bending workability was slightly poor and the Young's modulus in the direction perpendicular to the rolling was less than 106 GPa.

(実施例2)
実施例1で示した曲げ加工性の改善効果が、異なる成分および製造条件のコルソン合金でも得られるかについて検討した。
まず、実施例1と同様の方法で鋳造を行い、表4及び5の成分を有するインゴットを得た。
(1)熱間圧延:950℃で3時間加熱したインゴットを所定の厚みまで圧延した。圧延後の材料は直ちに水冷した。
(2)研削:熱間圧延で生成した酸化スケールをグラインダーで除去した。研削量は片面あたり0.5mmとした。
(3)冷間圧延:種々の総加工度(R)および1パスあたりの加工度(r)で、所定の厚みまで冷間圧延した。
(4)予備焼鈍:所定温度に調整した電気炉に試料を挿入し、所定時間保持した後、試料を水槽に入れ冷却した。
(5)軽圧延
(6)溶体化処理:所定温度に調整した電気炉に試料を挿入し、10秒間保持した後、試料を水槽に入れ冷却した。該温度は再結晶粒の平均直径が5〜25μmの範囲になる範囲で選択した。
(7)冷間圧延(圧延1)
(8)時効処理:電気炉を用い所定温度で5時間、Ar雰囲気中で加熱した。該温度は時効後の引張強さが最大になるように選択した。
(9)冷間圧延(圧延2)
(10)歪取り焼鈍:所定温度に調整した電気炉に試料を挿入し、10秒間保持した後、試料を大気中に放置し冷却した。
(Example 2)
It was examined whether the bending workability improving effect shown in Example 1 could be obtained even with a Corson alloy having different components and manufacturing conditions.
First, casting was performed in the same manner as in Example 1 to obtain ingots having the components shown in Tables 4 and 5.
(1) Hot rolling: An ingot heated at 950 ° C. for 3 hours was rolled to a predetermined thickness. The material after rolling was immediately cooled with water.
(2) Grinding: The oxide scale generated by hot rolling was removed with a grinder. The grinding amount was 0.5 mm per side.
(3) Cold rolling: Cold rolling was performed to a predetermined thickness at various total processing degrees (R) and processing degrees per pass (r).
(4) Pre-annealing: The sample was inserted into an electric furnace adjusted to a predetermined temperature and held for a predetermined time, and then the sample was placed in a water bath and cooled.
(5) Light rolling (6) Solution treatment: The sample was inserted into an electric furnace adjusted to a predetermined temperature and held for 10 seconds, and then the sample was placed in a water bath and cooled. The temperature was selected so that the average diameter of the recrystallized grains was in the range of 5 to 25 μm.
(7) Cold rolling (Rolling 1)
(8) Aging treatment: Heating was performed in an Ar atmosphere using an electric furnace at a predetermined temperature for 5 hours. The temperature was selected to maximize the tensile strength after aging.
(9) Cold rolling (Rolling 2)
(10) Strain relief annealing: The sample was inserted into an electric furnace adjusted to a predetermined temperature and held for 10 seconds, and then the sample was left in the air and cooled.

予備焼鈍後の試料および製品試料について、実施例1と同様の評価を行った。表6に評価結果を示す。圧延1または圧延2を行わなかった場合は、それぞれの加工度の欄に「0」と表記している。また、歪取り焼鈍か行わなかった場合は、温度の欄に「なし」と表記している。   Evaluation similar to Example 1 was performed about the sample after preliminary annealing, and a product sample. Table 6 shows the evaluation results. When rolling 1 or rolling 2 is not performed, “0” is written in the column of each degree of processing. In the case where the strain relief annealing is not performed, “none” is written in the temperature column.

Figure 0006196757
Figure 0006196757

Figure 0006196757
Figure 0006196757

Figure 0006196757
Figure 0006196757

発明例は、いずれも本発明が規定する条件で予備焼鈍前の冷間圧延、予備焼鈍および軽圧延を行ったものであり、板厚表面および中央部の結晶方位が本発明の規定を満たし、Good Wayの180度曲げのSmin/dが1.0以下となり、同時に106MPaを超える圧延直交方向のヤング率が得られた。また、650MPaを超える高い引張強さも得られた。
比較例15、21、22、23、25、27は、予備焼鈍前の冷間圧延における1パス当たりの加工度(r)の条件が本発明の規定から外れたものである。このため、板厚中央において<100>方向が圧延材のTDに配向する結晶の面積率が50%を超え、圧延直交方向のヤング率が106GPaに満たなかった。
比較例17は予備焼鈍前の冷間圧延における総加工度(R)が90.0%を下回ったものである。比較例18、26は軽圧延の加工度が本発明の規定を満足しなかったものである。比較例16、24は予備焼鈍の軟化度が本発明の規定を満足しなかったものである。これらでは、表面でのCube方位の面積率が5%未満となり、Smin/dが1.0を超えた。
比較例19、20、28は、本発明が規定する条件で予備焼鈍前の冷間圧延、予備焼鈍および軽圧延を行ったものであるが、比較例20では圧延1の加工度が60%を超え、比較例19、28では圧延2の加工度が50%を超えた。このため、表面でのCube方位の面積率が5%未満となり、Smin/dが1.0を超えた。
比較例29はNiとCoの合計濃度およびSi濃度が本発明の規定を下回ったものである。結晶方位が本発明の規定を満たし、1.0以下のSmin/dおよび106GPaを超える圧延直交方向のヤング率が得られたものの、引張強さが500MPaにも達しなかった。
比較例30はNiとCoの合計濃度が本発明の規定を超えたものである。表面でのCube方位の面積率が5%以上であったが、Smin/dが1.0を超えた。
比較例31は特許文献1が提唱する方法に準じ製造したものであり、予備焼鈍および軽圧延は行わず、表5に記載した以外の条件として、溶体化処理、時効処理および歪取り焼鈍(短時間焼鈍)の冷却速度をそれぞれ10℃/秒以上、10℃/秒未満および10℃/秒以上とし、短時間焼鈍における導電率低下を0.5〜3%IACSとし、平均結晶粒径を10μm以下とした。また、熱間圧延と溶体化処理との間の冷間圧延では、生産性を重視しraveを15%超、rmaxを20%超に設定した。その結果、導電率が35%IACS、耐力が700MPa以上となり、Bad Wayの90度W曲げ加工性は良好であったが、Good Wayの180度曲げ加工性は本発明例と比較し劣っていた。なお、特許文献1によれば上記方法で製造することにより表面のCube方位面積率は50%以上になるが、本実験で得られたCube方位面積率は5%にも満たなかった。この齟齬が生じた原因は、明らかにできなかった。
Inventive examples are all subjected to cold rolling, pre-annealing and light rolling before pre-annealing under the conditions defined by the present invention, and the crystallographic orientation of the plate thickness surface and the central portion satisfies the provisions of the present invention, Good Way's 180 degree bend S min / d was 1.0 or less, and at the same time, Young's modulus in the orthogonal direction of rolling exceeding 106 MPa was obtained. A high tensile strength exceeding 650 MPa was also obtained.
In Comparative Examples 15, 21, 22, 23, 25, and 27, the condition of the degree of work (r) per pass in cold rolling before pre-annealing deviates from the definition of the present invention. For this reason, the area ratio of the crystals in which the <100> direction is aligned with the TD of the rolled material at the center of the plate thickness exceeded 50%, and the Young's modulus in the direction perpendicular to the rolling was less than 106 GPa.
In Comparative Example 17, the total degree of work (R) in cold rolling before pre-annealing is less than 90.0%. In Comparative Examples 18 and 26, the light rolling workability did not satisfy the provisions of the present invention. In Comparative Examples 16 and 24, the degree of softening of the pre-annealing did not satisfy the definition of the present invention. In these, the area ratio of the Cube orientation on the surface was less than 5%, and S min / d exceeded 1.0.
Comparative Examples 19, 20, and 28 were obtained by performing cold rolling, pre-annealing, and light rolling before pre-annealing under the conditions specified by the present invention. In Comparative Example 20, the workability of rolling 1 was 60%. In Comparative Examples 19 and 28, the workability of rolling 2 exceeded 50%. For this reason, the area ratio of the Cube orientation on the surface was less than 5%, and S min / d exceeded 1.0.
In Comparative Example 29, the total concentration of Ni and Co and the Si concentration were lower than those specified in the present invention. Crystal orientation satisfies the requirements of the present invention, although less than 1.0 S min / d and rolling orthogonal direction Young's modulus greater than 106GPa were obtained, the tensile strength did not reach even 500 MPa.
In Comparative Example 30, the total concentration of Ni and Co exceeds the definition of the present invention. The area ratio of the Cube orientation on the surface was 5% or more, but S min / d exceeded 1.0.
Comparative Example 31 was produced according to the method proposed by Patent Document 1, and pre-annealing and light rolling were not performed. Conditions other than those described in Table 5 were solution treatment, aging treatment, and strain relief annealing (short). The cooling rate of time annealing is set to 10 ° C./second or more and less than 10 ° C./second and 10 ° C./second or more, the decrease in conductivity in short-time annealing is 0.5 to 3% IACS, and the average crystal grain size is 10 μm. It was as follows. Further, in the cold rolling between the hot rolling and solution treatment, more than 15% of the r ave emphasizes productivity, was set r max 20 percent. As a result, the electrical conductivity was 35% IACS, the proof stress was 700 MPa or more, and Bad Way 90 degree W bending workability was good, but Good Way 180 degree bending workability was inferior to that of the present invention example. . According to Patent Document 1, the Cube orientation area ratio of the surface becomes 50% or more by manufacturing by the above method, but the Cube orientation area ratio obtained in this experiment was less than 5%. The cause of this wrinkle could not be clarified.

Claims (8)

Ni及びCoのうち一種以上を0.8〜5.0質量%、Siを0.2〜1.5質量%含有し、残部が銅及び不可避的不純物からなる圧延材であり、
該圧延材の表面においてCube方位から10°以内の方位を持つ領域の面積率であるCube方位{001}<100>の面積率が5〜80%であり、
板厚に対し45〜55%の深さの断面において、<100>方向がTDと成す角度が10°以内である領域の面積率である<100>方向が圧延材の幅方向(TD)に配向する結晶の面積率が50%以下であるコルソン合金。
One or more of Ni and Co is 0.8 to 5.0 mass%, Si is 0.2 to 1.5 mass%, and the balance is a rolled material made of copper and inevitable impurities,
The area ratio of the Cube orientation {001} <100>, which is the area ratio of the region having an orientation within 10 ° from the Cube orientation on the surface of the rolled material, is 5 to 80%.
In a cross section having a depth of 45 to 55% with respect to the plate thickness, the <100> direction, which is the area ratio of the region where the angle formed by the <100> direction and TD is within 10 °, is the width direction (TD) of the rolled material. A Corson alloy having an area ratio of oriented crystals of 50% or less.
Sn、Zn、Mg、Fe、Ti、Zr、Cr、Al、P、Mn及びAgのうち1種以上を総量で0.005〜3.0質量%含有する請求項1に記載のコルソン合金。   The Corson alloy of Claim 1 which contains 0.005-3.0 mass% of 1 or more types in total in Sn, Zn, Mg, Fe, Ti, Zr, Cr, Al, P, Mn, and Ag. 圧延方向と直交する方向の引張試験から求めたヤング率が106GPa以上である請求項1又は2に記載のコルソン合金。   The Corson alloy according to claim 1 or 2, wherein the Young's modulus obtained from a tensile test in a direction orthogonal to the rolling direction is 106 GPa or more. 圧延方向と直交する方向に採取される端面接触型端子の素材として用いられる請求項1〜3のいずれかに記載のコルソン合金。   The Corson alloy in any one of Claims 1-3 used as a raw material of the end surface contact type terminal extract | collected in the direction orthogonal to a rolling direction. Ni及びCoのうち一種以上を0.8〜5.0質量%、Siを0.2〜1.5質量%含有し、残部が銅及び不可避的不純物からなるインゴットを作製し、前記インゴットを800〜1000℃の温度から厚み3〜20mmまで熱間圧延し、加工度90〜99.8%の冷間圧延を、1パスあたりの加工度の最大値および平均値をそれぞれ20%以下および15%以下として行った後、軟化度0.20〜0.80の予備焼鈍、加工度3〜50%の冷間圧延、700〜950℃で5〜300秒間の溶体化処理、加工度0〜60%の冷間圧延、350〜600℃で2〜20時間の時効処理、加工度0〜50%の冷間圧延を順次行う方法であり、
前記軟化度は軟化度をSとして、
S=(σ0−σ)/(σ0−σ950
〔ここで、σ0は予備焼鈍前の引張強さであり、σ及びσ950はそれぞれ予備焼鈍後及び950℃で焼鈍後の引張強さである。〕
で示される、請求項1〜4のいずれかに記載のコルソン合金の製造方法。
One or more of Ni and Co is contained in an amount of 0.8 to 5.0 mass%, Si is contained in an amount of 0.2 to 1.5 mass%, and the balance is made of copper and inevitable impurities. Hot rolling from a temperature of ˜1000 ° C. to a thickness of 3-20 mm, cold rolling with a workability of 90-99.8%, maximum value and average value of workability per pass of 20% or less and 15%, respectively After the following, pre-annealing with a softening degree of 0.20 to 0.80, cold rolling with a working degree of 3 to 50%, solution treatment at 700 to 950 ° C. for 5 to 300 seconds, working degree of 0 to 60% Cold rolling, aging treatment at 350 to 600 ° C. for 2 to 20 hours, cold rolling at a working degree of 0 to 50% is sequentially performed,
The softening degree is defined as S,
S = (σ 0 −σ) / (σ 0 −σ 950 )
[Where σ 0 is the tensile strength before pre-annealing, and σ and σ 950 are the tensile strength after pre-annealing and after annealing at 950 ° C., respectively. ]
The manufacturing method of the Corson alloy in any one of Claims 1-4 shown by these.
前記インゴットが、Sn、Zn、Mg、Fe、Ti、Zr、Cr、Al、P、Mn及びAgのうち1種以上を総量で0.005〜3.0質量%含有する請求項5に記載のコルソン合金の製造方法。   The said ingot contains 0.005-3.0 mass% of 1 or more types in total in Sn, Zn, Mg, Fe, Ti, Zr, Cr, Al, P, Mn, and Ag in total amount. Corson alloy manufacturing method. 請求項1〜4のいずれかに記載のコルソン合金を備えた伸銅品。   The copper-stretched article provided with the Corson alloy in any one of Claims 1-4. 請求項1〜4のいずれかに記載のコルソン合金を備えた電子機器部品。   The electronic device component provided with the Corson alloy in any one of Claims 1-4.
JP2012156835A 2012-07-12 2012-07-12 Corson alloy and manufacturing method thereof Active JP6196757B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2012156835A JP6196757B2 (en) 2012-07-12 2012-07-12 Corson alloy and manufacturing method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2012156835A JP6196757B2 (en) 2012-07-12 2012-07-12 Corson alloy and manufacturing method thereof

Related Child Applications (1)

Application Number Title Priority Date Filing Date
JP2016172836A Division JP2017014624A (en) 2016-09-05 2016-09-05 Corson alloy and manufacturing method therefor

Publications (2)

Publication Number Publication Date
JP2014019880A JP2014019880A (en) 2014-02-03
JP6196757B2 true JP6196757B2 (en) 2017-09-13

Family

ID=50195135

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2012156835A Active JP6196757B2 (en) 2012-07-12 2012-07-12 Corson alloy and manufacturing method thereof

Country Status (1)

Country Link
JP (1) JP6196757B2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105154714A (en) * 2015-09-02 2015-12-16 太仓顺如成建筑材料有限公司 Alloy copper bar
JP2017014624A (en) * 2016-09-05 2017-01-19 Jx金属株式会社 Corson alloy and manufacturing method therefor
DE102018122574B4 (en) * 2018-09-14 2020-11-26 Kme Special Products Gmbh Use of a copper alloy

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4556841B2 (en) * 2005-10-27 2010-10-06 日立電線株式会社 High strength copper alloy material excellent in bending workability and manufacturing method thereof
WO2011019042A1 (en) * 2009-08-10 2011-02-17 古河電気工業株式会社 Copper alloy material for electrical/electronic components
KR101419149B1 (en) * 2009-12-02 2014-07-11 후루카와 덴키 고교 가부시키가이샤 Copper alloy sheet
JP5961335B2 (en) * 2010-04-05 2016-08-02 Dowaメタルテック株式会社 Copper alloy sheet and electrical / electronic components
JP4976521B2 (en) * 2010-04-13 2012-07-18 三菱伸銅株式会社 Cu-Ni-Si-based copper alloy having excellent projection welding characteristics and method for producing the same
JP4857395B1 (en) * 2011-03-09 2012-01-18 Jx日鉱日石金属株式会社 Cu-Ni-Si alloy and method for producing the same

Also Published As

Publication number Publication date
JP2014019880A (en) 2014-02-03

Similar Documents

Publication Publication Date Title
JP4857395B1 (en) Cu-Ni-Si alloy and method for producing the same
KR101628583B1 (en) Cu-ni-si alloy and method for manufacturing same
JP6228725B2 (en) Cu-Co-Si alloy and method for producing the same
JP6111028B2 (en) Corson alloy and manufacturing method thereof
JP6345290B1 (en) Copper alloy strip with improved dimensional accuracy after press working
JP2013104082A (en) Cu-Co-Si-BASED ALLOY AND METHOD FOR PRODUCING THE SAME
JP6196757B2 (en) Corson alloy and manufacturing method thereof
TWI450986B (en) Cu-Co-Si alloy and a method for producing the same
JP5039863B1 (en) Corson alloy and manufacturing method thereof
JP2016199808A (en) Cu-Co-Si-BASED ALLOY AND PRODUCTION METHOD THEREFOR
JP6440760B2 (en) Copper alloy strip with improved dimensional accuracy after press working
JP6246454B2 (en) Cu-Ni-Si alloy and method for producing the same
JP4987155B1 (en) Cu-Ni-Si alloy and method for producing the same
JP2013100586A (en) Copper-titanium alloy and method of manufacturing the same
JP2017014624A (en) Corson alloy and manufacturing method therefor
JP2016211078A (en) Cu-Ni-Si-BASED ALLOY AND MANUFACTURING METHOD THEREFOR
JP2016084542A (en) Corson alloy and manufacturing method therefor

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20140401

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20150223

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20150317

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20150414

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20151027

A02 Decision of refusal

Free format text: JAPANESE INTERMEDIATE CODE: A02

Effective date: 20160607

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20170821

R150 Certificate of patent or registration of utility model

Ref document number: 6196757

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

S531 Written request for registration of change of domicile

Free format text: JAPANESE INTERMEDIATE CODE: R313531

R350 Written notification of registration of transfer

Free format text: JAPANESE INTERMEDIATE CODE: R350

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250