JPH0361350A - Manufacture of aluminum alloy for drawing having high strength and low directional property - Google Patents
Manufacture of aluminum alloy for drawing having high strength and low directional propertyInfo
- Publication number
- JPH0361350A JPH0361350A JP19461589A JP19461589A JPH0361350A JP H0361350 A JPH0361350 A JP H0361350A JP 19461589 A JP19461589 A JP 19461589A JP 19461589 A JP19461589 A JP 19461589A JP H0361350 A JPH0361350 A JP H0361350A
- Authority
- JP
- Japan
- Prior art keywords
- subjected
- less
- aluminum alloy
- heat treatment
- 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.)
- Granted
Links
- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 24
- 238000004519 manufacturing process Methods 0.000 title claims description 12
- 229910000765 intermetallic Inorganic materials 0.000 claims abstract description 19
- 238000005097 cold rolling Methods 0.000 claims abstract description 18
- 238000010438 heat treatment Methods 0.000 claims abstract description 18
- 238000000034 method Methods 0.000 claims abstract description 16
- 238000000265 homogenisation Methods 0.000 claims abstract description 12
- 238000000137 annealing Methods 0.000 claims abstract description 11
- 238000005098 hot rolling Methods 0.000 claims abstract description 9
- 238000005096 rolling process Methods 0.000 claims abstract description 6
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 5
- 229910052725 zinc Inorganic materials 0.000 claims abstract description 4
- 229910052802 copper Inorganic materials 0.000 claims abstract description 3
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 3
- 229910052782 aluminium Inorganic materials 0.000 claims description 6
- 239000012535 impurity Substances 0.000 claims description 2
- 229910052748 manganese Inorganic materials 0.000 abstract description 9
- 229910052742 iron Inorganic materials 0.000 abstract description 8
- 239000000126 substance Substances 0.000 abstract description 8
- 229910052719 titanium Inorganic materials 0.000 abstract description 3
- 230000015572 biosynthetic process Effects 0.000 abstract description 2
- 238000005204 segregation Methods 0.000 abstract 1
- 239000000463 material Substances 0.000 description 21
- 239000000203 mixture Substances 0.000 description 5
- 238000000465 moulding Methods 0.000 description 5
- 238000005482 strain hardening Methods 0.000 description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 239000000047 product Substances 0.000 description 4
- 238000012545 processing Methods 0.000 description 3
- 230000001105 regulatory effect Effects 0.000 description 3
- 239000007779 soft material Substances 0.000 description 3
- 239000011324 bead Substances 0.000 description 2
- 238000005266 casting Methods 0.000 description 2
- 230000000052 comparative effect Effects 0.000 description 2
- 238000007796 conventional method Methods 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 230000000573 anti-seizure effect Effects 0.000 description 1
- 235000013405 beer Nutrition 0.000 description 1
- 235000013361 beverage Nutrition 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 235000014171 carbonated beverage Nutrition 0.000 description 1
- 239000011362 coarse particle Substances 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 230000002542 deteriorative effect Effects 0.000 description 1
- 210000005069 ears Anatomy 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000005496 eutectics Effects 0.000 description 1
- 235000013305 food Nutrition 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000010422 painting Methods 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000009966 trimming Methods 0.000 description 1
Landscapes
- Metal Rolling (AREA)
Abstract
Description
(産業上の利用分野)
本発明は主としてDRD缶に適する絞り加工用アルミニ
ウム合金の製造方法に関するものである。
(従来の技術及び解決しようとする課題)ビール、炭酸
飲料等の飲料缶或いは食缶等に用いられるアルミニウム
缶は、D RD (Drawn andRedratz
n :絞り・再絞り)加工或いは[) I (Draw
nand I roned:絞り・しごき)加工のいず
れかによって作られており、前者の加工方式により得ら
れたものをDRD缶、後者の加工方式により得られたも
のをDI缶と称されている。
DRD缶は、通常、板厚0.20”0.25mmの缶で
あり、これを製造する代表的な工程としては、塗装コイ
ル−ドロープレス(抜絞り加工)→リドロープレス−ビ
ーディングプレス(必要に応じて、サイドビード、ネッ
クビード加工)からなる工程である。この際、素材のア
ルミニウム合金としては、以下(1)〜(4)の特性を
備えていることが特に重要である。
(1) 必要な缶底強度を得るための素材強度、(2
)表面外観を損なう歪模様(「アルミニウムの基礎と工
業技術」軽金属協会発行(1986)P、139参照)
が発生しないこと、
(3)再絞り後の耳の発生が小さいこと、すなわち、方
向性が小さいこと、
(4) エンドとの巻き締め部のフランジ加工性に優
れること。
ところが、従来、要件(1)のために多量のMgを添加
したアルミニウム合金は(2)の欠点が現れてしまい、
冷間圧延率を高くすると耳の高い材料となって要件(3
)を満足しないという欠点があった。
このため、DRD缶として必要な要件(1)〜(4)を
同時に満足する材料が強く要求されていた。
これに対し、本発明者等は、先に特願昭63−0223
11号にて、これらの要件を同時に満足し得る方法を提
案した。この方法は、化学成分の調整と共に均質化熱処
理、熱間圧延、中間焼鈍の各条件を規制して特定サイズ
、量の金属間化合物を有する組織とし、これに適正な仕
上冷延(40〜50%)を行うものである。
しかしながら、より絞り加工度の大きいDRD缶材では
より低い耳率の材料の要求が出てきており、また材料の
製造の面からすると、仕上冷延率を大きくしても低耳率
の材料が開発されることが望ましく、より一層の材料の
開発が要望されていた。
本発明は、か\る要請に応えるべくなされたものであっ
て、主としてDRD缶としての上記要件。
特に高強度で且つより低方向性の絞り加工用アルミニウ
ム合金を製造する方法を提供することを目的とするもの
である。
(課題を解決するための手段)
上記目的を達成するため、本発明者は、先の提案を踏ま
え、更にアルミニウム素材の製造条件について鋭意研究
を重ねた結果、Mn含有量を少なくする等により化学成
分を調整すると共に均質化熱処理、熱間圧延、中間焼鈍
の各条件を規制して特定サイズ、量の金属間化合物を有
する組織とするならば、これに大きな冷延率の仕上冷延
を施しても、−層低耳率の材料が得られることを見出し
たものである。
すなわち、本発明は、Mg:0.8〜1.5%、Mn:
0.30〜0.50%及びCu:0.05〜0.80%
を必須成分として含有し、更にFe:0.7%以下、S
i:0,4%以下、Zn:0.5%以下、Cr:0.0
5%以下及びTi:0.05%以下のうちの1種又は2
種以上を含有し、残部がAl及び不純物からなるアルミ
ニウム合金鋳塊に500〜600℃で均質化熱処理を施
し、270〜600℃で熱間圧延を行った後、中間圧延
と350〜550℃の中間焼鈍を施して、直径が5 X
10”〜I X ]−04人の金属間化合物を体積分
率で0.5〜3%有する組織とし、その後冷間圧延率4
0〜70%の仕上冷延を施すことを特徴とする高強度で
且つ低方向性を有する絞り加工用アルミニウム合金の製
造方法を要旨とするものである。
以下に本発明を更に詳細に説明する。
(作用)
まず1本発明における化学成分の限定理由を説明する。
Mg:
Mgは強度を付与する元素であるが、0.8%未満では
十分な強度が得られず、また、1.5%を超えると成形
中に缶表面に歪模様が発生し易くなり、かつ、仕上冷延
量を大きくする際の加工硬化が大きくなり、材料の成形
性を損ねる。したがって、Mgff1は0.8〜1.5
%の範囲とする。
Mn:
Mnは強度の付与とAlとの金属間化合物(Mn、Fe
)Al、の形成に必要な元素であるが、0.30%未満
では十分な強度を付与できず、体積分率で0.5%以上
の金属間化合物を形成できない。また、Mnが0.50
%を超えると、冷間加工による集合組織が発達し易くな
り、耳率が高くなる。また、所望のサイズ(5x i
o2〜I X 10’人)の金属間化合物の割合が多く
なり、フランジ加工性が低下する。したがって、Mn量
は0.30〜0.50%の範囲とする。
Cu:
Cuは強度を付与するために必要な元素であるが、0.
05%未満では十分な効果が得られず、また0、80%
を超えると強度が高くなって、強度の調整が難しくなる
と共に耐食性が劣化するので好ましくない。したがって
、Cu量は0.05〜0.80%の範囲とする。
以上の各元素を必須成分として含有するが、本発明では
以下の元素Fe、Si、Zn、Cr及びTiのうちの1
種又は2種以上を適量含有させる。
Fe量
Faは強度の付与に効果があるほか+ (Fe、 Mn
)Si、Al12の晶出物として成形時の焼き付き防止
の効果をもたらすと同時に前述のMnと(Mn、 Fe
)Al、の金属間化合物を形成する元素である。しかし
、0.7%を超えると粗大な金属間化合物(Mn、 F
e) A Q 、が形成し、所望のサイズ(5X10
”〜I X 10’入)で、かつ所望の体積分率(1〜
3%)のものが得られない。したがって、Fe量は0.
7%以下とする。
Si:
Sjは前述の(Fe、Mn) S L A Q izの
晶出物として成形時の焼付防止効果をもたらす元素であ
るが、0.4%を超えると粗大な晶出物が発生し、成形
性を損なうことになる。したがって、Si量は0.4%
以下とする。
Zn:
Znは強度をもたらす元素であるが、0.5%を超える
と耐食性が劣化するので、Zn量は0.5%以下とする
。
Cr、 ’ri:
Cr、Tiはともに組織を微細に制御するために添加さ
れる元素であるが、それぞれ0.05%を超えると粗大
な金属間化合物が発生し、成形性を損なうので、Cr量
、Ti量は各々0.05%以下とする。
次に本発明の製造方法について説明する。
上述の化学成分を有するアルミニウム合金は常法により
溶解、鋳造して鋳塊とする。鋳塊は例えばDC鋳造法に
より造塊される。
得られた鋳塊には500〜600℃の温度で均質化熱処
理を施す必要がある。この均質化熱処理はミクロ偏析の
均質化と所望の金属間化合物の形成を目的とするもので
ある。しかし、500℃未満では十分なる均質化熱処理
(ミクロ偏析の均質化)と所望の金属間化合物(Mn、
Fe)A I2.(直径5 X 102〜I X 1
0’人、体積分率0.5〜3%)の形成ができず、また
600℃を超えると共晶融解等の恐れがあるので、好ま
しくない。なお、加熱時間は特に制限しないが、上記温
度で3〜24時間の範囲が望ましい。
次いで、出炉後、600〜270℃の温度で熱間圧延を
行い、約2〜5mmの熱間圧延板とする。
この際、270℃未満の温度で圧延が実施されると冷間
歪が導入され、十分均一な熱間未再結晶組織が得られな
い。なお、上限温度600℃は均質化熱処理温度の上限
値600℃により規定される値である。
その後、中間圧延(冷間圧延)を行い、350〜550
℃の温度で中間焼鈍を実施し、軟質材とする。中間焼鈍
温度は、350℃未満では十分な軟質材が得られず、5
50℃を超えると異常粗大粒の発生を招くので、350
〜550℃の範囲とする。なお、中間焼鈍の加熱時間は
350〜400℃の温度域では2〜4時間必要であるが
、連続焼鈍炉を使用する高温処理の場合は、例えば50
0℃で0.5〜10秒の加熱時間を目安とするのがよい
。
上記製造工程により、本発明の特徴とする所望の金属間
化合物を有する組織が得られる。
主な金属間化合物としては(Mn、Fe)Al、であり
、冶金学的には析出物(D 1spersoids)に
属するものが中心であり、前述のように、■化学成分(
特にMn、Fe量)、■均質化熱処理、及び■熱間圧延
温度の最適な組合せにより、平均直径5×102〜I
X 10’八で且つ体積分率0.5〜3%のものが得ら
れる。サイズが5 X 102人未満では材料の強度が
高くなりすぎ、成形性を低下させることになり、またI
X 10’人より大きいものが多くなると成形加工中
に割れ等が発生する恐れがあるので好ましくない。また
5体積分率がO05%未満では組織を十分細かくするこ
とができず。
3%を超えると成形加工性を低下させるので好ましくな
い。
また、本発明によれば、Mn量を0.30−0゜50%
と規制したため、(M n 、 F e) A Q s
の生成量が従来よりも少なくなり、冷間加工時の集合組
織の発達が小さくなり1次工程での40〜70%もの冷
間加工を施しても、比較的低耳の材料が得られるという
効果を同時にもたらしている。
最後に、以上の所望の金属間化合物を有する軟質材に冷
間加工を付与して硬質材とするのであるが、40%未満
の冷間圧延率では十分な強度が得られない。一方、70
%を超える冷間圧延率では、冷間圧延により優先方向に
結晶粒が配向する集合組織が発達し、材料に方向性が生
じることとなり、缶に成形する時に約3%以上の耳高と
なり、成形後のトリミングの増加が必要となって製品価
値を著しく低下させる。よって、仕上圧延の冷間圧延率
は40〜70%の範囲とする。
以上の工程により、厚さ約0.20〜0.25m+sの
板材が得られる。この板材は、通常の方法により、塗装
後、2〜3回の絞りを行なうDRD加工で所望の缶に成
形される。
(実施例)
次に本発明の実施例を示す。
叉部A±
第1表に示す化学成分を有する厚さ600n+mのアル
ミニウム合金鋳塊をDC鋳造法にて溶製し、面削後、5
75℃X6hrの均質化熱処理を施し、550〜300
℃の温度で熱間圧延を行って厚さ3.5mmのホットコ
イルとした。
次いで、中間圧延で0.50mmtのコイルとし、連続
焼鈍炉で500℃X3secの中間焼鈍を施し、仕上冷
延(冷間圧延率45%)にて0,22a+mt、の硬質
板とした。
得られた材料について、金属間化合物のサイズ及び量を
調べ、また製造まま及び塗装熱処理(200’CX20
m1n)後の機械的性質を調べると共に、耳率、表面歪
模様、フランジ加工性についても評価した。その結果を
第1表に併記する。
なお、耳率はポンチ径40m1lφ、絞り率40%にて
求めた。また表面歪模様とフランジ加工性はO(良)、
0、・(不良)の印を付して評価した。
第1表より、本発明例Ncl〜Ha 5のアルミニウム
合金板はいずれも、本発明範囲内のサイズ、量の金属間
化合物を有し、高強度で表面歪模様がなく、耳率及びフ
ランジ加工性に優れた特性を有していることがわかる。
一方、比較例は高強度を示すものの、表面歪模様が生じ
、殆どが耳率やフランジ加工性が劣っている。(Industrial Application Field) The present invention mainly relates to a method for manufacturing an aluminum alloy for drawing, which is suitable for DRD cans. (Prior art and problems to be solved) Aluminum cans used for beverage cans such as beer and carbonated drinks, food cans, etc.
n: Drawing/re-drawing) processing or [) I (Draw
Cans obtained by the former method are called DRD cans, and those obtained by the latter method are called DI cans. DRD cans are usually cans with a plate thickness of 0.20" and 0.25 mm, and the typical process for manufacturing them is: Coating coil - draw press (drawing process) -> redraw press - beading press (as necessary) This is a process consisting of side bead and neck bead processing depending on the process. At this time, it is particularly important that the aluminum alloy used as the material has the following characteristics (1) to (4). (1) Material strength to obtain the required can bottom strength, (2
) Distortion patterns that impair the surface appearance (see "Basics and Industrial Technology of Aluminum", published by the Light Metals Association (1986), p. 139)
(3) The occurrence of ears after redrawing is small, that is, the directionality is small. (4) The flange workability of the tightening part with the end is excellent. However, in the past, aluminum alloys to which a large amount of Mg was added due to requirement (1) had the drawback of (2),
If the cold rolling rate is increased, the material will have a high selvage and meet the requirements (3).
) had the disadvantage of not satisfying the following. Therefore, there has been a strong demand for a material that simultaneously satisfies requirements (1) to (4) necessary for a DRD can. On the other hand, the inventors of the present invention previously applied for patent application No. 63-0223.
In No. 11, we proposed a method that can simultaneously satisfy these requirements. In this method, the chemical composition is adjusted and the conditions of homogenization heat treatment, hot rolling, and intermediate annealing are regulated to create a structure with a specific size and amount of intermetallic compounds. %). However, for DRD can stock with a higher degree of drawing, there is a demand for material with a lower selvage ratio, and from the perspective of material manufacturing, even if the finishing cold rolling ratio is increased, it is not possible to use a material with a lower selvage ratio. It is desirable that this material be developed, and further development of the material has been desired. The present invention was made to meet the above requirements, mainly for the DRD can. In particular, it is an object of the present invention to provide a method for producing an aluminum alloy for drawing that has high strength and low directionality. (Means for Solving the Problems) In order to achieve the above object, the inventor of the present invention, based on the previous proposal, further conducted intensive research on the manufacturing conditions of aluminum materials, and as a result, the present inventors have determined that by reducing the Mn content, etc. If the composition is adjusted and the conditions of homogenization heat treatment, hot rolling, and intermediate annealing are regulated to obtain a structure with a specific size and amount of intermetallic compounds, it is necessary to perform finish cold rolling at a large cold rolling rate. It has been found that a material with a low selvage ratio can be obtained even if That is, in the present invention, Mg: 0.8 to 1.5%, Mn:
0.30-0.50% and Cu: 0.05-0.80%
Contains as an essential component, Fe: 0.7% or less, S
i: 0.4% or less, Zn: 0.5% or less, Cr: 0.0
One or two of 5% or less and Ti: 0.05% or less
An aluminum alloy ingot containing at least 100% of aluminum with the remainder consisting of Al and impurities is subjected to homogenization heat treatment at 500 to 600°C, hot rolled at 270 to 600°C, and then subjected to intermediate rolling and 350 to 550°C. After intermediate annealing, the diameter is 5
10''~I
The gist of the present invention is a method for producing an aluminum alloy for drawing, which has high strength and low directionality, and is characterized by performing finish cold rolling of 0 to 70%. The present invention will be explained in more detail below. (Function) First, the reason for limiting the chemical components in the present invention will be explained. Mg: Mg is an element that imparts strength, but if it is less than 0.8%, sufficient strength cannot be obtained, and if it exceeds 1.5%, distortion patterns are likely to occur on the can surface during molding. Moreover, work hardening increases when the amount of finish cold rolling is increased, impairing the formability of the material. Therefore, Mgff1 is 0.8-1.5
% range. Mn: Mn provides strength and is an intermetallic compound with Al (Mn, Fe
)Al is an element necessary for the formation of Al, but if it is less than 0.30%, sufficient strength cannot be imparted, and an intermetallic compound with a volume fraction of 0.5% or more cannot be formed. Also, Mn is 0.50
%, texture due to cold working tends to develop and the selvage rate increases. Also, the desired size (5x i
The ratio of intermetallic compounds (o2 to I x 10') increases, and flange workability decreases. Therefore, the amount of Mn is set in the range of 0.30 to 0.50%. Cu: Cu is an element necessary to impart strength, but 0.
If it is less than 0.05%, sufficient effect cannot be obtained, and if it is less than 0.80%,
Exceeding this is not preferable because the strength increases, making it difficult to adjust the strength and deteriorating the corrosion resistance. Therefore, the amount of Cu is in the range of 0.05 to 0.80%. Each of the above elements is contained as an essential component, but in the present invention, one of the following elements Fe, Si, Zn, Cr and Ti is contained.
Contain an appropriate amount of one or more seeds. The amount of Fe (Fa) is effective in imparting strength and also + (Fe, Mn
)Si, Al12 as crystallized products, it has the effect of preventing seizure during molding, and at the same time, the above-mentioned Mn and (Mn, Fe
) Al is an element that forms an intermetallic compound. However, if it exceeds 0.7%, coarse intermetallic compounds (Mn, F
e) A Q, formed and of desired size (5X10
”~I
3%) cannot be obtained. Therefore, the amount of Fe is 0.
7% or less. Si: Sj is an element that provides an anti-seizure effect during molding as a crystallized product of the above-mentioned (Fe, Mn) SLAQiz, but if it exceeds 0.4%, coarse crystallized products are generated. This will impair moldability. Therefore, the amount of Si is 0.4%
The following shall apply. Zn: Zn is an element that provides strength, but if it exceeds 0.5%, corrosion resistance deteriorates, so the amount of Zn is set to 0.5% or less. Cr, 'ri: Both Cr and Ti are elements added to finely control the structure, but if each exceeds 0.05%, coarse intermetallic compounds are generated and formability is impaired, so Cr The amount of Ti and the amount of Ti are each 0.05% or less. Next, the manufacturing method of the present invention will be explained. An aluminum alloy having the above-mentioned chemical components is melted and cast into an ingot using a conventional method. The ingot is formed by, for example, a DC casting method. The obtained ingot needs to be subjected to homogenization heat treatment at a temperature of 500 to 600°C. The purpose of this homogenization heat treatment is to homogenize microsegregation and form desired intermetallic compounds. However, below 500°C, sufficient homogenization heat treatment (homogenization of microsegregation) and desired intermetallic compounds (Mn,
Fe) A I2. (Diameter 5 x 102 ~ I x 1
If the temperature exceeds 600°C, there is a risk of eutectic melting, etc., which is not preferable. Note that the heating time is not particularly limited, but a range of 3 to 24 hours at the above temperature is desirable. Next, after being taken out of the furnace, hot rolling is performed at a temperature of 600 to 270°C to obtain a hot rolled plate of approximately 2 to 5 mm. At this time, if rolling is performed at a temperature below 270° C., cold strain will be introduced and a sufficiently uniform hot unrecrystallized structure will not be obtained. Note that the upper limit temperature of 600°C is a value defined by the upper limit of the homogenization heat treatment temperature of 600°C. After that, intermediate rolling (cold rolling) is performed, and the
Intermediate annealing is performed at a temperature of ℃ to make a soft material. If the intermediate annealing temperature is lower than 350°C, a sufficiently soft material cannot be obtained;
If the temperature exceeds 50℃, abnormally coarse particles will occur, so
The temperature should be in the range of ~550°C. Note that the heating time for intermediate annealing is 2 to 4 hours in the temperature range of 350 to 400°C, but in the case of high-temperature treatment using a continuous annealing furnace, for example,
It is best to aim for a heating time of 0.5 to 10 seconds at 0°C. Through the above manufacturing process, a structure having a desired intermetallic compound, which is a feature of the present invention, can be obtained. The main intermetallic compounds are (Mn, Fe)Al, and metallurgically speaking, they mainly belong to precipitates (D 1spersoids), and as mentioned above, chemical composition (
In particular, by optimal combinations of Mn, Fe content), homogenization heat treatment, and hot rolling temperature, the average diameter of
X 10'8 and a volume fraction of 0.5 to 3% can be obtained. If the size is less than 5 x 102, the strength of the material will be too high, reducing moldability, and I
If there are many pieces larger than X10', cracks may occur during the molding process, which is not preferable. Further, if the 5 volume fraction is less than 5%, the structure cannot be made sufficiently fine. If it exceeds 3%, it is not preferable because it reduces moldability. Further, according to the present invention, the amount of Mn is reduced to 0.30-0°50%.
Therefore, (M n , Fe) A Q s
The amount of carbon produced is smaller than before, and the development of texture during cold working is smaller, making it possible to obtain a material with relatively low selvage even if 40 to 70% of the cold working is performed in the primary process. effect at the same time. Finally, the soft material containing the desired intermetallic compound is subjected to cold working to form a hard material, but sufficient strength cannot be obtained at a cold rolling rate of less than 40%. On the other hand, 70
When the cold rolling rate exceeds 3%, the cold rolling develops a texture in which crystal grains are oriented in the preferential direction, resulting in directional properties of the material, resulting in an edge height of approximately 3% or more when forming into cans. Increased trimming after molding is required, significantly reducing product value. Therefore, the cold rolling rate in finish rolling is in the range of 40 to 70%. Through the above steps, a plate material having a thickness of approximately 0.20 to 0.25 m+s is obtained. After painting, this plate material is formed into a desired can by a DRD process in which drawing is performed two to three times using a conventional method. (Example) Next, an example of the present invention will be shown. Prong A ± An aluminum alloy ingot with a thickness of 600n+m having the chemical composition shown in Table 1 was melted using the DC casting method, and after surface cutting,
Homogenized heat treatment at 75℃ x 6hrs, 550~300℃
Hot rolling was performed at a temperature of 0.degree. C. to obtain a hot coil with a thickness of 3.5 mm. Next, it was intermediate rolled to form a 0.50 mmt coil, subjected to intermediate annealing at 500°C for 3 seconds in a continuous annealing furnace, and finished cold rolled (cold rolling ratio 45%) to form a 0.22a+mt hard plate. The obtained material was examined for the size and amount of intermetallic compounds, and also subjected to as-manufactured and painted heat treatment (200'CX20
In addition to examining the mechanical properties after m1n), the selvedge ratio, surface distortion pattern, and flange workability were also evaluated. The results are also listed in Table 1. Note that the selvage ratio was determined using a punch diameter of 40 ml φ and a drawing ratio of 40%. In addition, the surface distortion pattern and flange workability are O (good).
It was evaluated by marking it as 0 or . (defective). From Table 1, it can be seen that the aluminum alloy plates of Invention Examples Ncl to Ha 5 all have intermetallic compounds in the size and amount within the range of the invention, have high strength, have no surface distortion pattern, and have a high selvedge ratio and flange processing. It can be seen that it has excellent properties. On the other hand, although the comparative examples exhibit high strength, surface distortion patterns occur and most of them have poor selvage ratio and flange workability.
犬11先
第1表中のNa 1のアルミニウム合金について、第2
表に示す条件の種々の製造工程にて最終板厚0.22問
tのアルミニウム合金硬質板を製造した。
得られた材料について、実施例■の場合と同様に材料特
性を評価した。その結果を第2表に併記する。
同表より、本発明例恥11〜&17のアルミニウム合金
板はいずれも、高強度で表面歪模様がなく、低耳率で優
れた特性を有していることがわかる。一方、比較例は、
本発明範囲内の化学成分を有し、高強度ではあるものの
、耳率、表面歪模様、肌荒れ、フランジ加工性のいずれ
かが劣っている。Regarding the aluminum alloy with Na 1 in Table 1, the second
Aluminum alloy hard plates having a final plate thickness of 0.22 mm were manufactured using various manufacturing processes under the conditions shown in the table. The material properties of the obtained material were evaluated in the same manner as in Example (2). The results are also listed in Table 2. From the same table, it can be seen that the aluminum alloy plates of Invention Examples No. 11 to No. 17 all have high strength, no surface distortion pattern, and have excellent characteristics with a low selvage rate. On the other hand, the comparative example is
Although it has chemical components within the scope of the present invention and has high strength, it is poor in any of the selvedge ratio, surface distortion pattern, rough surface, and flangeability.
(発明の効果)
以上詳述したように、本発明によれば、特定の化学成分
のアルミニウム合金について均質化熱処理、熱間圧延の
各条件を規制して適用し、所定のサイズ、量の金属間化
合物を有する組織を得るので、高強度で表面歪模様がな
く、且つ仕上冷延率を高くしても方向性の低い優れた絞
り加工用アルミニウム合金硬質板を製造することができ
る。特にDRD缶の製造に好適である。(Effects of the Invention) As detailed above, according to the present invention, homogenization heat treatment and hot rolling conditions are regulated and applied to an aluminum alloy having a specific chemical composition, and metal of a predetermined size and amount is produced. Since a structure having intermediate compounds is obtained, it is possible to produce an excellent aluminum alloy hard plate for drawing that has high strength, has no surface distortion pattern, and has low directionality even at a high finishing cold rolling rate. It is particularly suitable for manufacturing DRD cans.
Claims (1)
n:0.30〜0.50%及びCu:0.05〜0.8
0%を必須成分として含有し、更にFe:0.7%以下
、Si:0.4%以下、Zn:0.5%以下、Cr:0
.05%以下及びTi:0.05%以下のうちの1種又
は2種以上を含有し、残部がAl及び不純物からなるア
ルミニウム合金鋳塊に500〜600℃で均質化熱処理
を施し、270〜600℃で熱間圧延を行った後、中間
圧延と350〜550℃の中間焼鈍を施して、直径が5
×10^2〜1×10^4Åの金属間化合物を体積分率
で0.5〜3%有する組織とし、その後冷間圧延率40
〜70%の仕上冷延を施すことを特徴とする高強度で且
つ低方向性を有する絞り加工用アルミニウム合金の製造
方法。In weight% (the same applies hereinafter), Mg: 0.8 to 1.5%, M
n: 0.30-0.50% and Cu: 0.05-0.8
Contains 0% as an essential component, and further contains Fe: 0.7% or less, Si: 0.4% or less, Zn: 0.5% or less, Cr: 0
.. An aluminum alloy ingot containing one or more of Ti: 0.05% or less and Ti: 0.05% or less, with the remainder consisting of Al and impurities, is subjected to homogenization heat treatment at 500 to 600 ° C. After hot rolling at ℃, intermediate rolling and intermediate annealing at 350 to 550℃ are performed to reduce the diameter to 5.
× 10^2 to 1 × 10^4 Å intermetallic compound in a volume fraction of 0.5 to 3%, and then a cold rolling rate of 40
A method for producing an aluminum alloy for drawing having high strength and low directionality, the method comprising performing finish cold rolling of ~70%.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19461589A JPH0651901B2 (en) | 1989-07-27 | 1989-07-27 | Method for producing aluminum alloy for drawing having high strength and low directionality |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19461589A JPH0651901B2 (en) | 1989-07-27 | 1989-07-27 | Method for producing aluminum alloy for drawing having high strength and low directionality |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH0361350A true JPH0361350A (en) | 1991-03-18 |
| JPH0651901B2 JPH0651901B2 (en) | 1994-07-06 |
Family
ID=16327485
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP19461589A Expired - Lifetime JPH0651901B2 (en) | 1989-07-27 | 1989-07-27 | Method for producing aluminum alloy for drawing having high strength and low directionality |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0651901B2 (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4326985A1 (en) * | 1992-09-04 | 1994-03-10 | Hitachi Ltd | Fluid-cooled electronic component - has transversal element in path of cooling medium flow ensuring distribution across rear of semiconductor element |
| CN106435297A (en) * | 2016-11-17 | 2017-02-22 | 东莞宜安科技股份有限公司 | Preparation method and product of a bending-resistant, corrosion-resistant high-strength aluminum-magnesium alloy |
| CN115584416A (en) * | 2022-10-09 | 2023-01-10 | 哈尔滨工程大学 | A kind of nano-intermetallic compound multiphase strengthened aluminum alloy and its preparation method |
-
1989
- 1989-07-27 JP JP19461589A patent/JPH0651901B2/en not_active Expired - Lifetime
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4326985A1 (en) * | 1992-09-04 | 1994-03-10 | Hitachi Ltd | Fluid-cooled electronic component - has transversal element in path of cooling medium flow ensuring distribution across rear of semiconductor element |
| DE4326985C2 (en) * | 1992-09-04 | 1998-07-02 | Hitachi Ltd | Liquid-cooled electronic component |
| US5959351A (en) * | 1992-09-04 | 1999-09-28 | Hitachi, Ltd. | Liquid-cooled electronic device |
| CN106435297A (en) * | 2016-11-17 | 2017-02-22 | 东莞宜安科技股份有限公司 | Preparation method and product of a bending-resistant, corrosion-resistant high-strength aluminum-magnesium alloy |
| CN115584416A (en) * | 2022-10-09 | 2023-01-10 | 哈尔滨工程大学 | A kind of nano-intermetallic compound multiphase strengthened aluminum alloy and its preparation method |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0651901B2 (en) | 1994-07-06 |
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