JPS62250144A - Aluminum-alloy foil for package - Google Patents
Aluminum-alloy foil for packageInfo
- Publication number
- JPS62250144A JPS62250144A JP9284286A JP9284286A JPS62250144A JP S62250144 A JPS62250144 A JP S62250144A JP 9284286 A JP9284286 A JP 9284286A JP 9284286 A JP9284286 A JP 9284286A JP S62250144 A JPS62250144 A JP S62250144A
- Authority
- JP
- Japan
- Prior art keywords
- foil
- aluminum
- alloy foil
- package
- strength
- 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
- 239000011888 foil Substances 0.000 title claims abstract description 40
- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 17
- 238000000137 annealing Methods 0.000 claims abstract description 12
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 10
- 239000012535 impurity Substances 0.000 claims abstract description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 9
- 238000004806 packaging method and process Methods 0.000 claims description 7
- 239000013078 crystal Substances 0.000 claims description 4
- 230000009172 bursting Effects 0.000 abstract description 10
- 239000000203 mixture Substances 0.000 abstract description 6
- 229910045601 alloy Inorganic materials 0.000 abstract description 4
- 239000000956 alloy Substances 0.000 abstract description 4
- 238000004519 manufacturing process Methods 0.000 abstract description 4
- 238000000465 moulding Methods 0.000 description 8
- 230000007423 decrease Effects 0.000 description 7
- 238000005096 rolling process Methods 0.000 description 6
- 238000005097 cold rolling Methods 0.000 description 5
- 238000005098 hot rolling Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 4
- 150000001875 compounds Chemical class 0.000 description 3
- 239000002648 laminated material Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- -1 polyethylene Polymers 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 238000011160 research Methods 0.000 description 2
- 239000006104 solid solution Substances 0.000 description 2
- 238000005482 strain hardening Methods 0.000 description 2
- 229920003002 synthetic resin Polymers 0.000 description 2
- 239000000057 synthetic resin Substances 0.000 description 2
- 241000219112 Cucumis Species 0.000 description 1
- 235000015510 Cucumis melo subsp melo Nutrition 0.000 description 1
- 229910002551 Fe-Mn Inorganic materials 0.000 description 1
- 239000004698 Polyethylene Substances 0.000 description 1
- FJJCIZWZNKZHII-UHFFFAOYSA-N [4,6-bis(cyanoamino)-1,3,5-triazin-2-yl]cyanamide Chemical compound N#CNC1=NC(NC#N)=NC(NC#N)=N1 FJJCIZWZNKZHII-UHFFFAOYSA-N 0.000 description 1
- 235000013361 beverage Nutrition 0.000 description 1
- 230000005489 elastic deformation Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 235000013305 food Nutrition 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000005022 packaging material Substances 0.000 description 1
- 229920000573 polyethylene Polymers 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 238000001953 recrystallisation Methods 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 230000003746 surface roughness Effects 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
Abstract
Description
【発明の詳細な説明】
産業上の利用分野
この発明は飲食容器のキャップシール等に使用される包
装用アルミニウム合金箔に関する。DETAILED DESCRIPTION OF THE INVENTION Field of Industrial Application This invention relates to an aluminum alloy foil for packaging used as cap seals for food and beverage containers.
従来技術及び問題点
この種包装用のアルミニウム箔には、その性質として、
破裂強度が高く容易に破断しないこと、及びせん固成形
(打抜き)後や絞り成形後の弾性変形(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。Prior art and problems Aluminum foil for this type of packaging has the following properties:
In particular, it is required to have high bursting strength and not break easily, and to have little elastic deformation (so-called springback) after solidification forming (punching) or drawing forming.
面して、従来かかる包装用アルミニウム箔にはlN30
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。ところがこのよう
な従来箔はスプリングバックは小さい反面破裂強度が低
いため、必然的に箔厚を30〜100μm程度の厚いも
のにせざるを得ず、コストアップの原因となっていた。On the other hand, conventionally, such packaging aluminum foil has lN30
A soft foil (so-called 0 material) obtained by annealing a pure aluminum alloy such as an alloy was used. However, since such conventional foils have low springback but low bursting strength, the foil must necessarily be thick, on the order of 30 to 100 μm, leading to increased costs.
もっとも、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、該箔の薄肉化に伴う強度低下
を補う包装用素材として、アルミニウム箔にポリエチレ
ン等の合成樹脂フィルムを積層貼合したアルミニウムラ
ミネート材も使用されている。しかしかかるアルミニウ
ムラミネート材では、合成樹脂フィルムの弾性係数が低
いため成形後のスプリングバックが概して大きいものと
なり、次工程における処理上問題を生ずる虞れがあると
いう欠点を派生するものであった。However, in recent years, aluminum foil itself has been made thinner to reduce costs, and aluminum laminate materials, which are aluminum foil laminated with synthetic resin films such as polyethylene, have been used as packaging materials to compensate for the decrease in strength due to the thinner aluminum foil. is also used. However, in such aluminum laminate materials, since the elastic modulus of the synthetic resin film is low, the springback after molding is generally large, resulting in a drawback that there is a risk of problems in processing in the next step.
この発明はこのような事情に鑑みてなされたものであっ
て、破裂強度が高くかつ成形後のスプリングバックが小
さい包装用アルミニウム合金箔の提供を目的とするもの
である。The present invention was made in view of the above circumstances, and it is an object of the present invention to provide an aluminum alloy foil for packaging that has high bursting strength and low springback after forming.
問題点を解決するための手段
この目的において発明者は種々実験と研究を重ねた結果
、破裂強度向上のためには引張り強度及び伸びを大きく
する必要があり、かつ成形後のスプリングバックを少な
くするためには降伏強度(0,2%耐力)が低い方が好
ましいことを知見し、この観点から合金組成について更
なる研究の結果完成したものである。Means for Solving the Problems For this purpose, the inventor conducted various experiments and research, and found that in order to improve bursting strength, it is necessary to increase tensile strength and elongation, and to reduce springback after molding. It was discovered that a lower yield strength (0.2% yield strength) is preferable for this purpose, and from this point of view, this was completed as a result of further research on the alloy composition.
即ちこの発明に係る包装用アルミニウム合金箔は、Fe
: 0.7〜1.8vt%、Mn : 0゜1〜1.
5wt%、S i : 0. 2〜0. 5wt%を含
み、残部アルミニウム及び不可避不純物からなることを
特徴とするものである。That is, the aluminum alloy foil for packaging according to the present invention is made of Fe.
: 0.7~1.8vt%, Mn: 0°1~1.
5wt%, Si: 0. 2-0. 5 wt%, with the remainder consisting of aluminum and unavoidable impurities.
アルミニウム合金箔の組成において、Feは箔の結晶粒
を小さくし強度、伸びを向上させるものである。しかし
θ、7vt%未満ではその効果に乏しく、逆に1.8ν
j96を超えて含自°されてもAfi−F e−3i−
Mnの粗大化合物を形成し、強度、伸び、箔圧延性の低
下を来たす。In the composition of aluminum alloy foil, Fe makes the crystal grains of the foil smaller and improves its strength and elongation. However, when θ is less than 7vt%, the effect is poor, and on the contrary 1.8ν
Even if it contains more than j96, Afi-F e-3i-
A coarse compound of Mn is formed, resulting in a decrease in strength, elongation, and foil rollability.
好適には1,0〜1.671%の範囲の含自゛瓜とする
のが良い。Preferably, the content of melon is in the range of 1.0 to 1.671%.
MnはFeの固溶量を減少させ、再結晶核となるへρ−
Fe−Mn化合物の数を増加させ、箔の結晶粒微細化を
助長するとともに、微細析出物および固溶Mnによる強
度の向上に寄与するものである。しかし0.1wt%未
満ではこれらの効果に乏しく、逆に1.5wt%を超え
て含をされると粗大化合物を生成するとともに、加工硬
化が大きくなり箔圧延性が低下し、かつ降伏強度が高く
なり過ぎてスプリングバックが大となる欠点を派生する
。好適には0. 3〜1゜0vt96の範囲の含有量と
するのが良い。Mn reduces the amount of solid solution of Fe and becomes recrystallization nuclei ρ-
This increases the number of Fe-Mn compounds, promotes grain refinement of the foil, and contributes to improvement in strength due to fine precipitates and solid solution Mn. However, if it is less than 0.1 wt%, these effects are poor, and on the other hand, if it is added more than 1.5 wt%, coarse compounds are formed, work hardening increases, foil rollability decreases, and yield strength decreases. If the height is too high, the springback will be large. Preferably 0. The content is preferably in the range of 3 to 1°0vt96.
Siは箔の強度向上に寄与するものである。Si contributes to improving the strength of the foil.
しかし0.2vt%未満ではその効果に乏しく、逆に0
.5wt%を超えて含有されると加工硬化が大きくなり
箔圧延性を低下させるとともに、降伏強度が高くなり過
ぎスプリングバックが大となる欠点を派生する。好適に
は0. 2〜0゜35wt%の範囲の含有量とするのが
良い。However, if it is less than 0.2vt%, the effect is poor;
.. If the content exceeds 5 wt%, work hardening increases and foil rollability decreases, and yield strength becomes too high, resulting in large springback. Preferably 0. The content is preferably in the range of 2 to 0.35 wt%.
上記成分のほか、好ましくは鋳造時の凝固結晶粒微細化
のために、Ti:0.005〜0゜05wt%程度、B
:0.005〜0.05wt%程度の含有が許容される
。In addition to the above components, Ti: about 0.005 to 0.05 wt%, B
: Content of about 0.005 to 0.05 wt% is allowed.
ところでアルミニウム合金箔の一般的な既知の製造方法
は、アルミニウム合金鋳塊に熱間圧延、冷間圧延、箔圧
延、最終焼鈍の各必須工程を順次的に実施するが、この
発明に係るアルミニウム合金箔は、最終焼鈍後の平均結
晶粒径が15〜60μmの範囲に規定されてなるもので
あることが望ましい。すなわち平均結晶粒径が15μm
未満では、箔の降伏強度が高くなり過ぎ、成形後のスプ
リングバックが大となる虞れがある。また結晶粒径が6
0μmを超えて大きくなると、引張り強度、伸びが低下
し破裂強度が低くなるのみならず、成形加工後表面荒れ
が大きくなり、外観上問題となる虞れがある。より好ま
しくは15〜40umとするのが良い。By the way, in a generally known manufacturing method for aluminum alloy foil, each essential step of hot rolling, cold rolling, foil rolling, and final annealing is sequentially performed on an aluminum alloy ingot, but the aluminum alloy according to the present invention It is desirable that the foil has an average grain size after final annealing within a range of 15 to 60 μm. That is, the average crystal grain size is 15 μm
If it is less than that, the yield strength of the foil will become too high, and there is a risk that the springback after molding will become large. Also, the crystal grain size is 6
When the diameter exceeds 0 μm, not only the tensile strength and elongation decrease and the bursting strength decreases, but also the surface roughness becomes large after molding, which may cause problems in terms of appearance. More preferably, the thickness is 15 to 40 um.
なお、最終焼鈍後の平均結晶粒径は、前述した既知の製
造工程における各種条件、例えば熱間圧延温度、冷間圧
延や箔圧延の圧延率、最終焼鈍の温度、時間、昇温速度
などを変えることにより多様に変化させることができ、
またスラブの均質化処理の有無や、熱間圧延後あるいは
冷間圧延途中や箔圧延前に中間焼鈍を施すことによって
も変化させることができる。The average grain size after final annealing is determined by various conditions in the known manufacturing process described above, such as hot rolling temperature, rolling ratio of cold rolling or foil rolling, final annealing temperature, time, temperature increase rate, etc. By changing it, you can make various changes,
It can also be changed by whether or not the slab is homogenized or by performing intermediate annealing after hot rolling, during cold rolling, or before foil rolling.
発明の効果
この発明に係る特定組成のアルミニウム合金箔は実施例
の参酌によっても明らかなように、破裂強度が高くしか
も成形後のスプリングバックの少ないものとなしつる。Effects of the Invention As is clear from the examples, the aluminum alloy foil having a specific composition according to the present invention has high bursting strength and less springback after forming.
従って箔の薄肉化が可能となりコストダウンを実現しろ
るとともに、成形後の次工程での処理に際しても問題を
生じ、ることがな(、包装用箔として好適なものとなし
うる。Therefore, it is possible to make the foil thinner, which reduces costs, and also prevents problems from occurring during processing in the next step after molding, making it suitable as a packaging foil.
実施例 次にこの発明の詳細な説明する。Example Next, this invention will be explained in detail.
第1表に示す組成のA Q−F e−Mn−3i合金と
、下記■〜■に示す製造方法とを組合わせて各種のアル
ミニウム合金箔を製作した。Various aluminum alloy foils were manufactured by combining the AQ-F e-Mn-3i alloy having the composition shown in Table 1 with the manufacturing methods shown in (1) to (2) below.
■ アルミニウム合金スラブに610°C×20時間の
均質化処理を施したのち、530°Cで厚さ4 mtn
まで熱間圧延し、続いて0 、 6 nunまで冷間圧
延したのち厚さ25μmまで箔圧延を施し、その後37
0℃×2時間の最終焼鈍を施したもの。■ After homogenizing the aluminum alloy slab at 610°C for 20 hours, it was heated to 530°C to a thickness of 4 mtn.
After hot rolling to 0,6 nun, foil rolling to a thickness of 25 μm, then 37
Final annealing at 0°C for 2 hours.
■ 上記■の工程において、冷間圧延後箔圧延前に40
0°C×1時間の中間焼鈍を施したもの。■ In the process of ■ above, after cold rolling and before foil rolling,
Intermediately annealed at 0°C for 1 hour.
■ 上記■の工程において、熱間圧延後400℃×1時
間の1次中間焼鈍を施し、さらに冷間圧延後400°C
×1時間の2次中間焼鈍を施したもの。■ In the step (■) above, first intermediate annealing is performed at 400°C for 1 hour after hot rolling, and then at 400°C after cold rolling.
×1 hour secondary intermediate annealing.
■ 」二足■の工程において、2次中間焼鈍を20℃/
s e cの昇温速成にて400℃X20秒行ったも
の。■ In the process of "Two feet■", the secondary intermediate annealing is carried out at 20℃/
The test was conducted at 400°C for 20 seconds at a rapid heating rate of sec.
そして上記により得られたアルミニウム合金箔の・I−
均結晶粒径を測定した。And ・I- of the aluminum alloy foil obtained above
The uniform grain size was measured.
第1表
次に」二足6箔の破裂強度を測定するとともに、ポンチ
径33tnm%ブランク径49 tntaで浅綬り成形
して成形後のスプリングバックのはを測定した。なおス
プリングバック量は、成形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。Table 1: Next, the bursting strength of two 6 foils was measured, and the springback after forming was measured by shallow rippling molding with a punch diameter of 33 tnm and a blank diameter of 49 tnta. The amount of springback was evaluated based on the difference between the maximum outer diameter of the molded product and the punch diameter after molding.
その結果を第2表に示す。The results are shown in Table 2.
第2表
第2表の結果から明らかなように、本発明に係るアルミ
ニウム合金箔は、破裂強度がいずれも2.oXy/mを
超えて高いものであるとともに、成形後のスプリングバ
ックが少ないものであることを確認しえた。As is clear from the results in Table 2, the aluminum alloy foils according to the present invention have a bursting strength of 2.2. It was confirmed that the value exceeds oXy/m and that the springback after molding is small.
Claims (2)
.5wt%、Si:0.2〜0.5wt%を含み、残部
アルミニウム及び不可避不純物からなることを特徴とす
る包装用アルミニウム合金箔。(1) Fe: 0.7-1.8wt%, Mn: 0.1-1
.. 5 wt%, Si: 0.2 to 0.5 wt%, and the remainder consists of aluminum and inevitable impurities.
囲に規定されてなる特許請求の範囲第1項記載の包装用
アルミニウム合金箔。(2) The aluminum alloy foil for packaging according to claim 1, wherein the average crystal grain size after final annealing is defined in the range of 15 to 60 μm.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP61092842A JPH07820B2 (en) | 1986-04-21 | 1986-04-21 | Aluminum alloy foil for packaging with little springback after molding |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP61092842A JPH07820B2 (en) | 1986-04-21 | 1986-04-21 | Aluminum alloy foil for packaging with little springback after molding |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS62250144A true JPS62250144A (en) | 1987-10-31 |
JPH07820B2 JPH07820B2 (en) | 1995-01-11 |
Family
ID=14065686
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP61092842A Expired - Fee Related JPH07820B2 (en) | 1986-04-21 | 1986-04-21 | Aluminum alloy foil for packaging with little springback after molding |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH07820B2 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH01279725A (en) * | 1988-05-06 | 1989-11-10 | Kobe Steel Ltd | Aluminum alloy foil excellent in formability and its production |
US6531006B2 (en) | 2001-02-13 | 2003-03-11 | Alcan International Limited | Production of high strength aluminum alloy foils |
EP1902149B2 (en) † | 2005-06-29 | 2019-05-22 | Eurofoil Luxembourg S.A. | Process of producing a foil of an al-fe-si type aluminium alloy and foil thereof |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS58224142A (en) * | 1982-06-22 | 1983-12-26 | Sumitomo Light Metal Ind Ltd | Aluminum alloy plate with superior formability and its manufacture |
JPS59157265A (en) * | 1983-02-25 | 1984-09-06 | Showa Alum Corp | Production of aluminum alloy plate for forming |
JPS60145346A (en) * | 1984-01-09 | 1985-07-31 | Kobe Steel Ltd | Thin aluminum alloy plate having low tearing strength |
JPS60200943A (en) * | 1984-03-23 | 1985-10-11 | Sumitomo Light Metal Ind Ltd | Aluminum alloy having superior strength and workability |
-
1986
- 1986-04-21 JP JP61092842A patent/JPH07820B2/en not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS58224142A (en) * | 1982-06-22 | 1983-12-26 | Sumitomo Light Metal Ind Ltd | Aluminum alloy plate with superior formability and its manufacture |
JPS59157265A (en) * | 1983-02-25 | 1984-09-06 | Showa Alum Corp | Production of aluminum alloy plate for forming |
JPS60145346A (en) * | 1984-01-09 | 1985-07-31 | Kobe Steel Ltd | Thin aluminum alloy plate having low tearing strength |
JPS60200943A (en) * | 1984-03-23 | 1985-10-11 | Sumitomo Light Metal Ind Ltd | Aluminum alloy having superior strength and workability |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH01279725A (en) * | 1988-05-06 | 1989-11-10 | Kobe Steel Ltd | Aluminum alloy foil excellent in formability and its production |
US6531006B2 (en) | 2001-02-13 | 2003-03-11 | Alcan International Limited | Production of high strength aluminum alloy foils |
EP1902149B2 (en) † | 2005-06-29 | 2019-05-22 | Eurofoil Luxembourg S.A. | Process of producing a foil of an al-fe-si type aluminium alloy and foil thereof |
Also Published As
Publication number | Publication date |
---|---|
JPH07820B2 (en) | 1995-01-11 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
LAPS | Cancellation because of no payment of annual fees |