JPS61250153A - Manufacture of aluminum alloy foil suitable for use as laminating material on plastic film for cap seal - Google Patents

Manufacture of aluminum alloy foil suitable for use as laminating material on plastic film for cap seal

Info

Publication number
JPS61250153A
JPS61250153A JP9174185A JP9174185A JPS61250153A JP S61250153 A JPS61250153 A JP S61250153A JP 9174185 A JP9174185 A JP 9174185A JP 9174185 A JP9174185 A JP 9174185A JP S61250153 A JPS61250153 A JP S61250153A
Authority
JP
Japan
Prior art keywords
alloy foil
foil
aluminum alloy
hard
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
Application number
JP9174185A
Other languages
Japanese (ja)
Other versions
JPH08952B2 (en
Inventor
Hideo Kawai
英夫 河合
Masashi Sakaguchi
雅司 坂口
Tomoaki Yamanoi
智明 山ノ井
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.)
Altemira Co Ltd
Original Assignee
Showa Aluminum 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 Showa Aluminum Corp filed Critical Showa Aluminum Corp
Priority to JP60091741A priority Critical patent/JPH08952B2/en
Publication of JPS61250153A publication Critical patent/JPS61250153A/en
Publication of JPH08952B2 publication Critical patent/JPH08952B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Abstract

PURPOSE:To manufacture the titled Al alloy foil causing hardly spring-back at a low cost by cold rolling an Al alloy ingot contg. a specified amount of Fe so as to provide a hard or semihard refined state. CONSTITUTION:An Al alloy ingot consisting of 0.1-1.2wt% Fe and the balance Al with inevitable impurities is essentially cold rolled and is optionally annealed at a low temp. or annealed and rolled at a low draft so as to provide a hard or semihard refined state. Thus, Al alloy foil suitable for use as a laminating material on a plastic film for a cap seal is obtd. The Al alloy foil has >=about 10.5kgf/mm<2>, preferably <=about 25kgf/mm<2> tensile strength and >=about 5.5kgf/ mm<2> offset yield stress strength at 0.2% permanent set and hardly causes spring- back.

Description

【発明の詳細な説明】 産業上の利用分野 この発明は、合成樹脂フィルムと貼合されて、飲食容器
などのキうップシール用うミネート材を形成するのに適
したアルミニウム合金箔の製造方法に関する。
DETAILED DESCRIPTION OF THE INVENTION Field of Industrial Application This invention relates to a method for producing an aluminum alloy foil suitable for laminating with a synthetic resin film to form a laminate material for use in lid seals for food and drink containers, etc. .

従来の技術及び問題点 周知のとおりアルミニウムないしアルミニウム合金箔は
食品や医薬品の包装容器などに広く用いられているが、
なかでも、飲食容器などのキャップシールの素材として
用いられる場合には、その性質として、強度に優れ容易
に破断しないこと及び成形後の弾性変形(いわゆるスプ
リングバック)が少ないことなどが特に要求される。
Conventional Technology and Problems As is well known, aluminum or aluminum alloy foil is widely used for food and pharmaceutical packaging containers, etc.
In particular, when used as a material for cap seals for food and drink containers, etc., the material is particularly required to have excellent strength, not to break easily, and to have little elastic deformation (so-called springback) after molding. .

而して、従来かかるキャップシール用アルミニウム箔に
は、1N30合金等の純アルミニウム系合金を焼鈍した
軟質状態の箔(いわゆる0材)が用いられていた。これ
は、箔が軟質化するにつれて箔のスプリングバックが小
さくなるという事実に基づいたものであるが、反面強度
が低下するため、必然的に箔厚を30〜100μm程度
の厚いものにせざるを得す、コストアップの原因となっ
ていた。
Conventionally, such aluminum foil for cap seals has been made of a soft foil (so-called 0 material) obtained by annealing a pure aluminum alloy such as 1N30 alloy. This is based on the fact that the springback of the foil decreases as the foil becomes softer, but on the other hand, the strength decreases, so the foil must be thicker, approximately 30 to 100 μm. This caused an increase in costs.

もっとも軟質状態で箔自体の強度を高めるために、例え
ばMgやMn等の強′化元素を天下する方法も試みられ
たが、圧延抵抗が大となって大幅なコストダウンは望め
なかった。
In order to increase the strength of the foil itself in its softest state, attempts have been made to add reinforcing elements such as Mg and Mn, but rolling resistance increases and significant cost reductions cannot be expected.

そこで最近では、キャップシール用素材として要求され
る強度を維持しつつアルミニウム箔自体を薄肉化してコ
スト低減を図るため、上記の軟質部を合成樹脂フィルム
に貼り合わせたいわゆるAnラミネート材が用いられる
ようになってきている。
Therefore, in order to reduce costs by thinning the aluminum foil itself while maintaining the strength required as a material for cap seals, a so-called An laminate material, in which the above-mentioned soft part is bonded to a synthetic resin film, has recently been used. It is becoming.

しかしながら、この場合には合成樹脂フィルムの弾性係
数が低いため、絞り加工後におけるラミネート材のスプ
リングバックが概して大きくなり、甚しくは絞りポンチ
の形状と異なったものとなって次工程における処理上問
題を生じるおそれがあるというような欠点を派生するも
のであった。
However, in this case, since the elastic modulus of the synthetic resin film is low, the springback of the laminate material after drawing is generally large, and the shape of the laminate material is even different from that of the drawing punch, causing processing problems in the next process. This resulted in drawbacks such as the risk of causing problems.

この発明はかかる事情に鑑みてなされたものであって、
スプリングバックが少なくかつコストも安価なキャップ
シール用AQラミネート材を実現するためのアルミニウ
ム合金箔の提供を意図してなされたものである。
This invention was made in view of such circumstances, and
This was made with the intention of providing an aluminum alloy foil for realizing an AQ laminate material for cap seals that has less springback and is inexpensive.

問題点を解決するための手段 この目的を達成するために、発明者らは種々実験と研究
を重ねた結果、AQラミネート材のスプリングバックは
、合成樹脂フィルムに貼合されるアルミニウム箔の強度
と密接な関係があり、特に箔の引張強度が10.5Ng
f/−以上、望ましくは12.589f/−以上でかつ
0.2%耐力が5.5Ngf/−以上である場合には、
上記の目的を有効に達成しうろことを見出し、かかる知
見に基づきさらにこの条件を満足するアルミニウム合金
箔の製造方法について研究した結果この発明を完成しえ
たものである。
Means for solving the problem In order to achieve this objective, the inventors conducted various experiments and research, and found that the springback of AQ laminate material was determined by the strength of the aluminum foil laminated to the synthetic resin film. There is a close relationship, especially when the tensile strength of the foil is 10.5Ng.
f/- or more, preferably 12.589 f/- or more, and the 0.2% proof stress is 5.5 Ngf/- or more,
The present invention has been completed as a result of discovering how to effectively achieve the above object, and based on this knowledge, conducting further research on a method for producing aluminum alloy foil that satisfies this condition.

即ちこの発明は、l”e :0.1〜1.2wt%を含
み、残部がアルミニウム及び不可避不純物よりなるアル
ミニウム合金の鋳塊に、冷間圧延を必須工程として施し
、その後低温度での焼鈍(H2n)あるいは焼鈍機低圧
下率による圧延(H1n)を任意工程として実施し、硬
質ないし半硬質の調質状態に作製することを特徴とする
キャップシール用合成樹脂フィルムラミネート材に適し
たアルミニウム合金箔の製造方法を要旨とする。
That is, in this invention, an aluminum alloy ingot containing 0.1 to 1.2 wt% of l"e and the remainder consisting of aluminum and unavoidable impurities is cold rolled as an essential step, and then annealed at a low temperature. An aluminum alloy suitable for a synthetic resin film laminate material for cap seals, which is produced in a hard or semi-hard tempered state by performing (H2n) or rolling (H1n) at a low reduction rate in an annealing machine as an optional step. The gist is the method for manufacturing foil.

先ず、アルミニウム合金箔の組成において、1”e量が
0.1〜1.2Tllt%に限定されるのは、下限値未
満では強度向上効果に乏しいうえ、地金コストも高価に
つき薄箔化によるコスト低減を期待できないからである
。逆に上限値を超えた場合には、II質処理の如何を問
わず最終筋の強度が大となってしまい、この発明を適用
する意味がなくなるからである。
First of all, in the composition of aluminum alloy foil, the 1"e content is limited to 0.1 to 1.2 Tllt%. If it is less than the lower limit, the strength improvement effect is poor, and the metal cost is high, so it is difficult to make the foil thinner. This is because cost reduction cannot be expected.On the other hand, if the upper limit is exceeded, the strength of the final streak becomes large regardless of the quality II treatment, and there is no point in applying this invention. .

次に製造方法について説明すれば、この発明では、上記
組成のアルミニウム合金の鋳塊に、必須工程として冷間
圧延を施すものとする。もつとも冷間圧延前において、
上記鋳塊に均質化処理、熱間圧延等を施すことを妨げる
ものではない。また冷間圧延を一次冷間圧延と二次冷間
圧延とに分け、その間に中間焼鈍を施すものとしても良
い。
Next, the manufacturing method will be described. In this invention, an aluminum alloy ingot having the above composition is subjected to cold rolling as an essential step. Before cold rolling,
This does not preclude subjecting the ingot to homogenization treatment, hot rolling, etc. Alternatively, cold rolling may be divided into primary cold rolling and secondary cold rolling, and intermediate annealing may be performed between them.

この冷間圧延を最終の箔圧延工程としだ場合には、得ら
れるアルミニウム箔は硬質(H)となるが、この発明で
は、任意工程として、冷間圧延後低温度での焼鈍を施し
、あるいは焼鈍機低圧下率による圧延を施すことにより
、半硬質(1/2H)以上の調質状態となされることが
許容される。冷開圧延後に施す焼鈍は、その後に圧延を
施さない場合にあっては約200〜250℃程度の温度
範囲で30分〜5時間行われるのが一般的であり、好適
には220〜230℃の範囲で1〜2時間行われる。
If this cold rolling is carried out as the final foil rolling process, the resulting aluminum foil will be hard (H), but in this invention, as an optional step, annealing at a low temperature is performed after cold rolling, or By rolling with a low reduction rate in an annealing machine, it is allowed to achieve a refining state of semi-hard (1/2H) or more. The annealing performed after cold-open rolling is generally carried out at a temperature of about 200 to 250°C for 30 minutes to 5 hours, preferably at 220 to 230°C, if rolling is not performed afterwards. It is carried out for 1 to 2 hours.

一方、圧延を施す場合にあっては、再結晶温度以上の温
度で完全焼鈍となされるのが望ましい。また焼鈍後論さ
れる前記圧延の圧下率は約10〜50%の範囲に設定す
るのが望ましく、より好適には20〜30%に設定する
のが良い。また調質状態を硬質ないし半硬質としたのは
、合金箔の引張強度を10.5紹f/−以上、0.2%
耐力を5.5に9f/ae1以上とするためである。尚
、引張強度が大きいと圧延変形抵抗の増大、取扱上の不
便を招くことなどから25Kgf/−以下とするのが望
ましい。またこの発明では、圧延後脱脂のための洗浄を
必要に応じて行うことも推奨される。
On the other hand, when rolling is performed, it is desirable that complete annealing be performed at a temperature equal to or higher than the recrystallization temperature. Further, the rolling reduction ratio in the rolling mentioned after annealing is desirably set in a range of about 10 to 50%, and more preferably in a range of 20 to 30%. In addition, the hard or semi-hard tempered state means that the tensile strength of the alloy foil is 10.5 inf/- or more, 0.2%
This is to make the yield strength 5.5 and 9f/ae1 or more. Incidentally, if the tensile strength is too high, the resistance to rolling deformation increases and handling becomes inconvenient, so it is desirable that the tensile strength is 25 Kgf/- or less. In the present invention, it is also recommended to perform cleaning for degreasing after rolling, if necessary.

尚、上記方法によって製造されたアルミニウム箔と貼合
される合成樹脂フィルムとしては、貼合がヒートシール
により行われることから比較的耐熱性のあるボリブOピ
レン、ポリエステル、ナイロン等を使用するのが望まし
い。
In addition, as the synthetic resin film to be laminated with the aluminum foil produced by the above method, it is recommended to use relatively heat-resistant materials such as boli-O-pyrene, polyester, and nylon since lamination is performed by heat sealing. desirable.

発明の詳細 な説明したように、この発明によれば、引張強度が10
.5幻f/j、0.2%耐力が5.5Kgf/−以上の
アルミニウム合金箔を製造することができ、この合金箔
を用いることによって、実施例の参酌によっても明らか
なようにスプリングバックの少ないキャップシール用と
して好適なAQラミネート材を実現することができる。
As described in detail, according to the present invention, the tensile strength is 10
.. 5 illusion f/j, 0.2% yield strength of 5.5 Kgf/- or more can be manufactured, and by using this alloy foil, springback can be reduced as is clear from consideration of the examples. It is possible to realize an AQ laminate material suitable for use in small cap seals.

もとより1〜30合金を0材処理した従来箔よりも強度
に優れるものであるから、従来箔を用いたラミネート材
に較べて箔単体としての薄肉化がさらに可能となり、コ
ストダウンを併せて実現することができる。
Since it is superior in strength to conventional foils made from 1-30 alloys treated with 0 material, it is possible to make the foil itself thinner than laminate materials using conventional foils, which also reduces costs. be able to.

実施例 次にこの発明の実施例を比較例との対比において示す。Example Next, examples of the present invention will be shown in comparison with comparative examples.

第1表に示す各種組成のアルミニウム合金の母屋スラブ
に、熱間圧延、−次冷間圧延、中間焼鈍、二次冷間圧延
(箔圧延)を順次的に施し、ついで実施例のうち試料N
α1〜4のものについては圧延のまま硬質箔(1−1)
とし、試料Nα5〜8のものについては200〜250
℃で焼鈍を施して半硬質箔(1/2H)に調質し、比較
例のものについては300℃以上で焼鈍を施して軟質箔
(0)とした。そしてこれらの箔の引張強度、0.2%
耐力をそれぞれ測定した。その結果を同表に示す。尚、
8箔は厚さ10μm、20μm、30μmの3種類を作
製し、引張強度、0.2%耐力はこれらの平均値で示し
た。
Purlin slabs of aluminum alloys with various compositions shown in Table 1 were sequentially subjected to hot rolling, secondary cold rolling, intermediate annealing, and secondary cold rolling (foil rolling), and then Sample N of Examples
For α1 to 4, hard foil (1-1) is used as rolled.
and 200 to 250 for samples Nα5 to 8.
The foils were annealed at 300° C. to become semi-hard foils (1/2H), and those of comparative examples were annealed at 300° C. or higher to become soft foils (0). and the tensile strength of these foils, 0.2%
The yield strength of each was measured. The results are shown in the same table. still,
Three types of 8 foils were produced with thicknesses of 10 μm, 20 μm, and 30 μm, and the tensile strength and 0.2% proof stress were shown as the average value of these.

第1表 次に上記の厚さ20μmの各合金箔について、箔の両面
に厚さ15μm、6μmのポリエステルフィルムを貼り
合せ、ポンチ径32履、ブランク径50s1クリアラン
ス0.5〜0.6履、シワ押え20kgf以下の加工条
件で絞り加工し、加工後のスプリングバックの量を調べ
た。スプリングバック量は、加工後における成形体の最
大外径とポンチ径の差で評価した。その結果を第2表に
示す。
Table 1 Next, for each of the above alloy foils with a thickness of 20 μm, polyester films with a thickness of 15 μm and 6 μm were laminated on both sides of the foil, a punch diameter of 32 mm, a blank diameter of 50 s, a clearance of 0.5 to 0.6 mm, Drawing processing was performed under processing conditions of a wrinkle presser of 20 kgf or less, and the amount of springback after processing was investigated. The amount of springback was evaluated by the difference between the maximum outer diameter of the molded body and the punch diameter after processing. The results are shown in Table 2.

[以下余白] 第2表 上記結果から明らかなように、この発明によって製造さ
れるアルミニウム合金箔は、引張強度が10.5kyf
/−を、0.2%耐力が5.5kyf/−をいずれも超
え、比較例のものに較べてラミネート材のスプリングバ
ックが少ないことを確認しえた。
[Margin below] As is clear from the above results in Table 2, the aluminum alloy foil manufactured by the present invention has a tensile strength of 10.5 kyf.
/- and the 0.2% proof stress exceeded 5.5 kyf/-, and it was confirmed that the springback of the laminate material was less than that of the comparative example.

以  上that's all

Claims (1)

【特許請求の範囲】[Claims] Fe:0.1〜1.2wt%を含み、残部がアルミニウ
ム及び不可避不純物よりなるアルミニウム合金の鋳塊に
、冷間圧延を必須工程として施し、その後低温度での焼
鈍あるいは焼鈍後低圧下率による圧延を任意工程として
実施し、硬質ないし半硬質の調質状態に作製することを
特徴とするキャップシール用合成樹脂フィルムラミネー
ト材に適したアルミニウム合金箔の製造方法。
An ingot of an aluminum alloy containing 0.1 to 1.2 wt% of Fe with the balance consisting of aluminum and unavoidable impurities is subjected to cold rolling as an essential step, and then annealed at a low temperature or by a low reduction rate after annealing. A method for producing an aluminum alloy foil suitable for a synthetic resin film laminate material for cap seals, characterized by performing rolling as an optional step and producing the foil in a hard or semi-hard tempered state.
JP60091741A 1985-04-26 1985-04-26 Laminate material for cap sealing of aluminum alloy foil and resin film with little springback during molding Expired - Lifetime JPH08952B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP60091741A JPH08952B2 (en) 1985-04-26 1985-04-26 Laminate material for cap sealing of aluminum alloy foil and resin film with little springback during molding

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP60091741A JPH08952B2 (en) 1985-04-26 1985-04-26 Laminate material for cap sealing of aluminum alloy foil and resin film with little springback during molding

Publications (2)

Publication Number Publication Date
JPS61250153A true JPS61250153A (en) 1986-11-07
JPH08952B2 JPH08952B2 (en) 1996-01-10

Family

ID=14034948

Family Applications (1)

Application Number Title Priority Date Filing Date
JP60091741A Expired - Lifetime JPH08952B2 (en) 1985-04-26 1985-04-26 Laminate material for cap sealing of aluminum alloy foil and resin film with little springback during molding

Country Status (1)

Country Link
JP (1) JPH08952B2 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015083657A1 (en) * 2013-12-02 2015-06-11 大日本印刷株式会社 Battery-packaging material
JP2016062805A (en) * 2014-09-19 2016-04-25 大日本印刷株式会社 Battery-packaging material
CN114959368A (en) * 2022-04-19 2022-08-30 山东意吉希精密制造有限公司 Al-Fe type motor rotor alloy and preparation method and application thereof

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5118362A (en) * 1974-08-07 1976-02-13 Sanyo Electric Co GYOSHUFUJOBUNRISOCHI

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5118362A (en) * 1974-08-07 1976-02-13 Sanyo Electric Co GYOSHUFUJOBUNRISOCHI

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015083657A1 (en) * 2013-12-02 2015-06-11 大日本印刷株式会社 Battery-packaging material
US10128471B2 (en) 2013-12-02 2018-11-13 Dai Nippon Printing Co., Ltd. Battery-packaging material
JP2016062805A (en) * 2014-09-19 2016-04-25 大日本印刷株式会社 Battery-packaging material
CN114959368A (en) * 2022-04-19 2022-08-30 山东意吉希精密制造有限公司 Al-Fe type motor rotor alloy and preparation method and application thereof

Also Published As

Publication number Publication date
JPH08952B2 (en) 1996-01-10

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