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JPH0141411B2 - - Google Patents
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JPH0141411B2 - - Google Patents

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Publication number
JPH0141411B2
JPH0141411B2 JP12877785A JP12877785A JPH0141411B2 JP H0141411 B2 JPH0141411 B2 JP H0141411B2 JP 12877785 A JP12877785 A JP 12877785A JP 12877785 A JP12877785 A JP 12877785A JP H0141411 B2 JPH0141411 B2 JP H0141411B2
Authority
JP
Japan
Prior art keywords
laminate material
cap seal
aluminum
warpage
resin film
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
JP12877785A
Other languages
Japanese (ja)
Other versions
JPS61286032A (en
Inventor
Hideo Kawai
Masashi Sakaguchi
Tomoaki Yamanoi
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 JP12877785A priority Critical patent/JPS61286032A/en
Publication of JPS61286032A publication Critical patent/JPS61286032A/en
Publication of JPH0141411B2 publication Critical patent/JPH0141411B2/ja
Granted legal-status Critical Current

Links

Description

【発明の詳細な説明】[Detailed description of the invention]

産業上の利用分野 この発明は、飲食容器などのキヤツプシール用
アルミニウムラミネート材の製造方法、特に反り
や成形後の弾性変型(いわゆるスプリングバツ
ク)の少ないキヤツプシールを製作するためのア
ルミニウムラミネート材の製造方法に関する。 なおこの明細書において、アルミニウムの語は
アルミニウム合金を含む意味において用いる。 従来の技術 飲食容器などのキヤツプシール用材としては、
従来より、1N30合金等を焼鈍した軟質状態の箔
(いわゆるO材)が用いられていたが、かかる軟
質箔は強度的に弱いため、箔厚を概ね30〜100μ
m程度の比較的厚いものにせざるを得ず、昨今の
コストダウンの要求に対処できなくなつてきた。 そこで最近では、アルミニウム箔自体を薄肉化
してコスト低減を図るとともに該箔の薄肉化に伴
なう強度低下を補うキヤツプシール用素材とし
て、アルミニウム箔に合成樹脂フイルムを積層貼
合したアルミニウムラミネート材が用いられるよ
うになつてきている。 発明が解決しようとする問題点 而してこのアルミニウムラミネート材を用いて
キヤツプシールを製作する場合、製造あがりの該
ラミネート材をキヤツプシール形状小片への打抜
き工程に付すのが通常であるが、この打抜き後の
打抜き片にフイルムを内側にしてカールする反り
が生じることが往々にしてあつた。このためこの
ような打抜き片をそのままキヤツプシールとして
使用する場合にはキヤツプシールに反りが残存し
た状態となり、また打抜き片をブランク材として
絞り成形した場合においてもこの反りが原因とな
つてスプリングバツクが大きくなり、甚しくは絞
りポンチの形状と異なつたものとなつて次工程に
おける処理上問題を生ずる虞れがあるというよう
な欠点を派生するものであつた。 この発明はかかる事情に鑑みてなされたもので
あつて、打抜き片の反りを減じることにより、キ
ヤツプシール自体の反りや絞り成形後のスプリン
グバツクを軽減しうるキヤツプシール用アルミニ
ウムラミネート材の提供を目的としてなされたも
のである。 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、発明者は種々実験
と研究を重ね、打抜き片の反りの原因を解明した
結果、該反りは、アルミニウムラミネート材の製
造工程におけるアルミニウムとラミネート材との
貼合の際、フイルムのしわを防止するため該フイ
ルムに一般に付与される引張力に基く残留応力の
偏りに起因していることを知見するに至り、さら
にこの残留応力の偏り、ひいては打抜き片の反り
は、打抜き前において、アルミニウムラミネート
材に、貼合の際樹脂フイルムに付与した引張力と
直交する方向に一定範囲内の引張歪を付与するこ
とにより軽減可能であることを見い出し、この発
明を完成しえたものである。 すなわちこの発明は、アルミニウム箔の少なく
とも片面に、合成樹脂フイルムを引張力を付与し
つつ積層貼合してアルミニウムラミネート材を形
成し、その後キヤツプシール形状への打抜き以前
に該ラミネート材に前記樹脂フイルムの引張力方
向と直交する方向において0.5〜1.5%の引張歪を
付与することを特徴とするキヤツプシール用アル
ミニウムラミネート材の製造方法を要旨とするも
のである。 アルミニウム箔としては、一般に1N30合金等
の純アルミニウム系合金を0処理した軟質箔が用
いられるが、これらに限定されるものではない。
またアルミニウム箔の厚さは、コスト低減効果の
点から25μm以下とするのが望ましい。 合成樹脂フイルムの一例としてはポリプロピレ
ン(PP)、ポリエステル(PET)、ポリエチレン
(PE)、ナイロン等をあげうる。合成樹脂フイル
ムとアルミニウム箔との貼合はアルミニウム箔の
片面のみに行われるものであつても、両面に行わ
れるものであつても良く、あるいは両面に行われ
る場合には片面毎にフイルムの種類を変えても良
く、あるいはさらにフイルムの上に同種、異種の
フイルムを複数層に積層したものであつても良
い。かかる合成樹脂フイルムとアルミニウム箔と
の貼合加工は、周知の湿式貼合せ法、乾式貼合せ
法、熱溶融式貼合せ法、あるいは押出し式貼合せ
法などを始めとする各種の方法によつて行われる
が、貼合に際してはフイルムのしわを防止するた
め、該フイルムに適度の引張力を付与するものと
なされる。貼合直後においては、合成樹脂フイル
ムは引張力を付与された結果、アルミニウム箔に
較べて残留応力が大となつている。 こうして製造されたアルミニウムラミネート材
は、その後所定のキヤツプシール形状小片への打
抜き工程に付されるが、この発明では打抜き以前
に、貼合時に樹脂フイルムに付与した引張力の方
向と直交する方向において、前記ラミネート材に
0.5〜1.5%の引張歪を付与することを条件とす
る。これは、貼合によつて生じた残留応力の偏り
をなくして打抜き片の反りを減じ、ひいてはキヤ
ツプシールとしての反りや絞り成形後のスプリン
グバツクを減少させるためである。ここで引張歪
が0.5%未満ではその効果に乏しく、また1.5%を
越えると逆に引張歪付与方向に大きな反りを生じ
好ましくない。このため、引張歪の範囲を上記に
限定したのである。なお引張歪の付与は、アルミ
ニウム箔と樹脂フイルムとの貼合後打抜き以前で
あればいつ行つても良く、貼合直後あるいは打抜
き直前でも良い。 キヤツプシールはこのアルミニウムラミネート
材の打抜き後、打抜き片をそのまま使用し、ある
いは打抜き片をブランク材として浅絞り成形する
ことにより製作される。なお打抜き片を絞り成形
する場合には、絞り比1.3〜2.0、シワ押え圧力0.5
〜8.0Kgf/cm2、ポンチとダイスのクリアランス
を素材厚さの1.0〜2.5倍の条件で絞り成形を行う
ことが成形後のスプリングバツクを一層抑制する
ことができる点で好ましい。 発明の効果 以上説明したように、この発明は、アルミニウ
ム箔の少なくとも片面に、合成樹脂フイルムを引
張力を付与しつつ積層貼合してアルミニウムラミ
ネート材を形成し、その後キヤツプシール形状へ
の打抜き以前に該ラミネート材に前記樹脂フイル
ムの引張力方向と直交する方向において所定の引
張歪を付与することを特徴とするものあるから、
該引張歪によつて貼合時に生じたアルミニウム箔
と樹脂フイルムとの残留応力の偏りをなくすこと
ができ、キヤツプシール形状に打抜いた際の反り
を軽減したキヤツプシール用アルミニウムラミネ
ート材を製造することができる。従つて、このラ
ミネート材を打抜き後そのままキヤツプシールと
して用いた場合にはキヤツプシール自体としての
反りを減少でき、一方打抜き後絞り成形した場合
にはスプリングバツクを減少でき、次工程の処理
上においても品質上においても全く問題のないキ
ヤツプシールを提供することができる。 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。 1N30合金を3材処理してある厚さ20μmのアル
ミニウム軟質箔の片面に、厚さ6μmのポリエス
テルフイルムを所定の引張力を付与しつつ積層貼
合してアルミニウムラミネート材を作製した。 次いでこのラミネート材に、引張力付与方向と
直角方向に下記表に示すような引張歪を付与した
のちあるいは付与することなく、該ラミネート材
を直径49mmのキヤツプシール形状に打抜いて各打
抜き片の反りの量(1/曲率半径)を測定した。
その結果を同表に示す。
Industrial Application Field This invention relates to a method for producing an aluminum laminate material for cap seals such as food and beverage containers, and in particular, a method for producing an aluminum laminate material for producing cap seals with less warpage and elastic deformation after molding (so-called spring back). Regarding the method. In this specification, the term aluminum is used to include aluminum alloys. Conventional technology As material for cap seals such as food and drink containers,
Conventionally, soft foil (so-called O material) made by annealing 1N30 alloy, etc., has been used, but such soft foil has low strength, so the foil thickness is generally 30 to 100 μm.
It has become impossible to meet the recent demands for cost reduction, as it has no choice but to be relatively thick. Therefore, recently, aluminum laminate material, which is made by laminating a synthetic resin film on aluminum foil, has been developed as a material for cap seals, which aims to reduce the cost by thinning the aluminum foil itself and compensate for the decrease in strength due to the thinning of the aluminum foil. It is starting to be used. Problems to be Solved by the Invention When producing a cap seal using this aluminum laminate material, the laminate material after production is usually subjected to a punching process into cap seal-shaped pieces. After punching, the punched pieces often curled with the film inside. Therefore, if such a punched piece is used as a cap seal as it is, the cap seal will remain warped, and even if the punched piece is drawn as a blank material, this warp will cause spring back. This leads to drawbacks such as the size of the punch and the shape of the punch which differs from that of the drawing punch, which may cause processing problems in the next step. The present invention was made in view of the above circumstances, and an object of the present invention is to provide an aluminum laminate material for a cap seal that can reduce warpage of the cap seal itself and spring back after drawing by reducing the warpage of the punched piece. This was done as a. Means for Solving the Problems In order to achieve this objective, the inventor conducted various experiments and research, and as a result of elucidating the cause of the warpage of the punched pieces, the inventor found that the warpage was caused by aluminum in the manufacturing process of aluminum laminate materials. It has been discovered that this is due to the unevenness of residual stress based on the tensile force that is generally applied to the film to prevent wrinkles when laminated with a laminate material. Furthermore, it has been discovered that the warping of the punched pieces can be reduced by applying tensile strain within a certain range to the aluminum laminate material in a direction orthogonal to the tensile force applied to the resin film during lamination before punching. , this invention was completed. That is, this invention forms an aluminum laminate material by laminating and bonding a synthetic resin film on at least one side of an aluminum foil while applying a tensile force, and then, before punching into a cap seal shape, the resin film is attached to the laminate material before punching into a cap seal shape. The gist of this invention is a method for manufacturing an aluminum laminate material for a cap seal, which is characterized by imparting a tensile strain of 0.5 to 1.5% in a direction perpendicular to the direction of the tensile force. As the aluminum foil, a soft foil obtained by zero-treating a pure aluminum alloy such as 1N30 alloy is generally used, but the foil is not limited to these.
Further, the thickness of the aluminum foil is desirably 25 μm or less from the viewpoint of cost reduction effect. Examples of synthetic resin films include polypropylene (PP), polyester (PET), polyethylene (PE), and nylon. The synthetic resin film and aluminum foil may be laminated on only one side of the aluminum foil, or on both sides, or if laminated on both sides, the type of film is determined for each side. Alternatively, a plurality of films of the same type or different types may be laminated on top of the film. The lamination process of such a synthetic resin film and aluminum foil can be carried out by various methods including the well-known wet lamination method, dry lamination method, hot melt lamination method, or extrusion lamination method. However, in order to prevent the film from wrinkling during lamination, an appropriate tensile force is applied to the film. Immediately after lamination, the synthetic resin film has a larger residual stress than the aluminum foil as a result of being subjected to tensile force. The aluminum laminate material produced in this way is then subjected to a punching process into small pieces with a predetermined cap seal shape, but in this invention, before punching, the aluminum laminate material is , to the laminate material
The condition is to apply a tensile strain of 0.5 to 1.5%. This is to eliminate uneven residual stress caused by bonding and reduce warping of the punched piece, which in turn reduces warping as a cap seal and spring back after drawing. Here, if the tensile strain is less than 0.5%, the effect is poor, and if it exceeds 1.5%, conversely, large warpage occurs in the direction in which the tensile strain is applied, which is not preferable. For this reason, the range of tensile strain was limited to the above range. The tensile strain may be applied at any time after bonding the aluminum foil and the resin film before punching, or immediately after bonding or immediately before punching. The cap seal is manufactured by punching the aluminum laminate material and then using the punched piece as it is, or by shallow drawing the punched piece as a blank material. In addition, when drawing the punched piece, the drawing ratio is 1.3 to 2.0, and the wrinkle pressing pressure is 0.5.
It is preferable to carry out drawing forming under conditions of ~8.0 Kgf/cm 2 and a clearance between the punch and die of 1.0 to 2.5 times the thickness of the material, since spring back after forming can be further suppressed. Effects of the Invention As explained above, this invention forms an aluminum laminate material by laminating a synthetic resin film on at least one side of an aluminum foil while applying a tensile force, and then punching it into a cap seal shape. The laminate material is characterized in that a predetermined tensile strain is imparted to the laminate material in a direction orthogonal to the tensile force direction of the resin film.
To produce an aluminum laminate material for a cap seal that can eliminate the imbalance of residual stress between the aluminum foil and the resin film that occurs during lamination due to the tensile strain, and that reduces warping when punched into a cap seal shape. be able to. Therefore, if this laminate material is used as a cap seal as it is after punching, the warpage of the cap seal itself can be reduced, while if it is drawn and formed after punching, spring back can be reduced, and it can also be used in the next process. It is possible to provide a cap seal with no problems in terms of quality. Examples Next, examples of the present invention will be shown in comparison with comparative examples. An aluminum laminate material was prepared by laminating a 6 μm thick polyester film on one side of a 20 μm thick soft aluminum foil treated with 1N30 alloy while applying a predetermined tensile force. Next, after applying or not applying tensile strain to this laminate material as shown in the table below in a direction perpendicular to the direction in which the tensile force is applied, the laminate material was punched into a cap seal shape with a diameter of 49 mm, and each punched piece was The amount of warpage (1/radius of curvature) was measured.
The results are shown in the same table.

【表】 上記結果から明らかなように、本発明によつて
製造されたアルミニウムラミネート材の打抜き片
(試料No.2〜4)は、引張歪を付与しないもの
(試料No.1)に較べて反りの量を減少しうること
がわかる。また引張歪を本発明範囲を越えて付与
すると(試料No.5)、逆に引張歪付与方向に大き
な反りを生ずることもわかる。 一方、打抜き片の反りの量と絞り加工後のスプ
リングバツク量とが比例関係にあることを確認す
るために、反りの量を種々に変えた打抜き片を用
意し、各打抜き片を同一条件で絞り成形し、その
ときのスプリングバツク量を調べた。なお、スプ
リンバツク量は成形後の成形体の最大径とポンチ
径との差で評価した。その結果を図面にグラフに
て示す。 グラフから明らかなように、反りの量が減少す
とキヤツプシールのスプリンバツクも減少するこ
とがわかる。従つてこの発明によつて製造された
アルミニウムラミネート材によれば、打抜き片を
絞り成形してキヤツプシールを製作した場合には
スプリンバツク量を軽減でき、また打抜き片をそ
のままキヤツプシールとして使用した場合には当
然にその反りを軽減しうるものであることを確認
しえた。
[Table] As is clear from the above results, the punched pieces of aluminum laminate materials manufactured according to the present invention (Samples No. 2 to 4) were more effective than those to which no tensile strain was applied (Sample No. 1). It can be seen that the amount of warpage can be reduced. Furthermore, it can be seen that when a tensile strain is applied beyond the range of the present invention (sample No. 5), a large warpage occurs in the direction in which the tensile strain is applied. On the other hand, in order to confirm that there is a proportional relationship between the amount of warpage of the punched piece and the amount of springback after drawing, we prepared punched pieces with various amounts of warpage, and tested each punched piece under the same conditions. It was drawn and formed, and the amount of spring back at that time was examined. The amount of springback was evaluated based on the difference between the maximum diameter of the molded product after molding and the punch diameter. The results are shown graphically in the drawing. As is clear from the graph, as the amount of warpage decreases, the springback of the cap seal also decreases. Therefore, according to the aluminum laminate material manufactured according to the present invention, when a cap seal is manufactured by drawing a punched piece, the amount of springback can be reduced, and when the punched piece is used as it is as a cap seal, the amount of springback can be reduced. It was confirmed that this can naturally reduce the warpage.

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

図面は打抜き片の反りの量とキヤツプシールの
スプリンバツク量との関係を示すグラフである。
The drawing is a graph showing the relationship between the amount of warpage of the punched piece and the amount of springback of the cap seal.

Claims (1)

【特許請求の範囲】[Claims] 1 アルミニウム箔の少なくとも片面に、合成樹
脂フイルムを引張力を付与しつつ積層貼合してア
ルミニウムラミネート材を形成し、その後キヤツ
プシール形状への打抜き以前に該ラミネート材に
前記樹脂フイルムの引張力方向と直交する方向に
おいて0.5〜1.5%の引張歪を付与することを特徴
とするキヤツプシール用アルミニウムラミネート
材の製造方法。
1. Form an aluminum laminate material by laminating and bonding a synthetic resin film on at least one side of an aluminum foil while applying a tensile force, and then apply the tensile force direction of the resin film to the laminate material before punching into a cap seal shape. A method for producing an aluminum laminate material for a cap seal, the method comprising applying a tensile strain of 0.5 to 1.5% in a direction perpendicular to the direction.
JP12877785A 1985-06-12 1985-06-12 Production of aluminum laminated material for cap seal Granted JPS61286032A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12877785A JPS61286032A (en) 1985-06-12 1985-06-12 Production of aluminum laminated material for cap seal

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12877785A JPS61286032A (en) 1985-06-12 1985-06-12 Production of aluminum laminated material for cap seal

Publications (2)

Publication Number Publication Date
JPS61286032A JPS61286032A (en) 1986-12-16
JPH0141411B2 true JPH0141411B2 (en) 1989-09-05

Family

ID=14993207

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12877785A Granted JPS61286032A (en) 1985-06-12 1985-06-12 Production of aluminum laminated material for cap seal

Country Status (1)

Country Link
JP (1) JPS61286032A (en)

Also Published As

Publication number Publication date
JPS61286032A (en) 1986-12-16

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