JPS6050141A - Hard aluminum alloy sheet for can end and its production - Google Patents

Hard aluminum alloy sheet for can end and its production

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Publication number
JPS6050141A
JPS6050141A JP15675883A JP15675883A JPS6050141A JP S6050141 A JPS6050141 A JP S6050141A JP 15675883 A JP15675883 A JP 15675883A JP 15675883 A JP15675883 A JP 15675883A JP S6050141 A JPS6050141 A JP S6050141A
Authority
JP
Japan
Prior art keywords
aluminum alloy
heating
cold rolling
hard
alloy
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
JP15675883A
Other languages
Japanese (ja)
Other versions
JPH0331779B2 (en
Inventor
Takashi Inaba
隆 稲葉
Hideyoshi Usui
碓井 栄喜
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.)
Kobe Steel Ltd
Original Assignee
Kobe Steel Ltd
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 Kobe Steel Ltd filed Critical Kobe Steel Ltd
Priority to JP15675883A priority Critical patent/JPS6050141A/en
Publication of JPS6050141A publication Critical patent/JPS6050141A/en
Publication of JPH0331779B2 publication Critical patent/JPH0331779B2/ja
Granted legal-status Critical Current

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Abstract

PURPOSE:To produce a hard Al alloy sheet for a can end which permits reduction in thickness by subjecting an Al alloy casting ingot contg. a specific ratio of Mg and Cu to a specific treatment and specifying the average crystal grain size prior to final cold rolling. CONSTITUTION:An Al alloy casting ingot contg., by wt% 2.0-5.0% Mg and 0.05-0.50% Cu, contg. if necessary 0.05-0.50% Mn and 0.10-0.40% Cr and consisting of the balance substantially Al is subjected to soaking and hot rolling at 450-550 deg.C. The hot-rolled Al alloy is then heated to 400-600 deg.C at a heating rate of >=100 deg.C/min with or without cold rolling. The heated Al alloy sheet is cooled to <=200 deg.C at a cooling rate of >=100 deg.C/hr right after heating or after holding within 10min so that the average crystal grain size is made <=25mu and that the component incorporated therein to make contribution to prevention of conversion is made into a solid soln. state. The sheet is further subjected to the cold rolling at >=10% and the hard Al alloy sheet having an excellent bulging property, high strength and formability is obtd.

Description

【発明の詳細な説明】 本発明はキャンエンド用アルミニウl、合金硬質板およ
びその製造法に関し、さらに詳しくは、キャンエンド等
塗装印刷後加工を施す用途に使用するキャンエンド用ア
ルミニウl、合金硬質板によびぞの製造法に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an aluminum plate for can ends, a hard alloy plate, and a method for manufacturing the same, and more specifically, the present invention relates to an aluminum plate for can ends, a hard alloy plate, and a method for manufacturing the same. Concerning the manufacturing method of the board.

一般に、キャンエンド用アルミニウム合金板はアルミニ
ウム合金板に塗装印刷を施した後、(1)シェル加工 (2)多段張出加工 (3)スコアー加に (4)リベントカI」 (5)シームj用二I− 笠の加工が1jなわれるが、この加−1゛の中で最いB
要視される加工は多段張出加」二であり、(1(械的性
質(特に伸び)、盆属間化合物の分イli j’i 、
i ヒX+’i +il’+ #:j径等に影響を受け
る。
In general, aluminum alloy plates for can ends are made by painting and printing on the aluminum alloy plate, and then (1) shell processing, (2) multi-stage overhang processing, (3) scoring, (4) reventing, and (5) seam j. 2I- The processing of the hat is done in 1j, but the most B in this addition 1.
The processing that is considered important is multi-stage elongation.
i HiX+'i +il'+ #: Affected by j diameter, etc.

また、成形されたキャンエンドには、 (1)耐圧性 (2)聞出性 に))タフ抜げ性 (4)而J fill性 笠が要求され、特に、素材の薄肉化には耐圧性の向−1
頁高強度化)か必要である。
In addition, the molded can end is required to have (1) pressure resistance, (2) readability,)) tough removal resistance, and (4) fillability. Nomu-1
(higher page strength) is required.

そして、素利の高強度化および薄肉化は成形性の低下を
招来し、従って、素材の薄肉11−にIJ高成形性、か
つ、高強度が茨木される。しかし従来使用されている素
材で゛は、塗装印刷後のベーキングにおいて強度が、杵
しく低下するのて゛高強度とするrこめに、固)H元素
の含有(固溶体強化)および最終冷間圧延率の」二昇(
Lf、イ+史比)が必要て゛ある。、−の場合、機械的
性質(伸び)の低ト”および結晶粒の1(径比を招いて
張出性等の成形性を低トさせる。
Increasing the strength and reducing the thickness of the material leads to a decrease in formability, and therefore, the thin wall 11- of the material has high IJ formability and high strength. However, the strength of conventionally used materials deteriorates dramatically during baking after coating and printing, so in order to achieve high strength, it is necessary to incorporate H elements (solid solution strengthening) and increase the final cold rolling rate. ”Nishō(
Lf, A + Shihito) are necessary. In the case of , -, the mechanical properties (elongation) are low and the crystal grain size ratio is low, resulting in low formability such as extensibility.

本発明は、塗装印4:1llL%のベーヘンクににいて
強度が殆んど低下せず、11、冒、二は強度が向−1,
[るベークハード型であり、従って、最終冷間圧延率を
現在より小さくすることがlり能で゛あり、が−フ、最
終冷間圧延前の結晶粒が徽t111で・あるため、成形
f]、特に、張出性が優れ′(にす、1:’、+J強度
および高成形性であり、薄肉化をi+J能としたキャン
エンド用アルミニウム合金硬質板によびその製造法を提
fJ1.−4−るもので゛ある。
The strength of the present invention hardly decreases when the paint mark is 4:1llL%, and the strength is almost -1,
It is a bake-hard type, so it is possible to make the final cold rolling rate smaller than the current one. We present an aluminum alloy hard plate for can ends, which has particularly excellent elongation properties'(Nisu, 1:', +J strength and high formability, and has i+J ability to reduce the wall thickness), and a method for manufacturing the same.fJ1 There are .-4- things.

本発明に係るキャンエンド゛用アルミニウム合金硬質板
およびその製造法1,1、(1)へ1署+ 2.(1−
5,(ltu1%、CuO,05〜0.50田195を
含有し残部′):、t′!的にノ\1からなるアルミニ
ラ1.f針盆で′、がン、最1f6冷開圧延前の平均結
晶粒仔が25μmn以1・C゛あることを特徴とするキ
ャンエンI・月jアルミニウl、合金硬板を第1の発明
とし、(2)M+; 2,0・・5.軸1%、Cu O
,05−0,50u+t%を3イJ腰 さらに、M+1
0.05□−Q、50u+t%、Cr (1,10=0
.40u+t%を含有し、残?1b実質白男こ)\1か
らなる“?ルミニ・ンムr針断で゛、かつ、最終冷間圧
延+iijの・IL均粘品村径か25/I m以下で゛
あることを特徴とするキャンエンド用アルミニウム合金
硬質板を第2の発明と腰(:()h1シ、2.+1〜5
.Ou+L%、C++ 0.05へ・0.50帆%を含
イ1し、必蟹に応じて、Mn (1,05〜0.50t
llL%、Cr (1,10ヘ(1,4(1+u1%を
含有し、残部天質的にノ\1からなるアルミニウム合金
ffJJ塊を、450〜550℃の温度で均熱によび熱
間)圧延を施し、その後冷間圧延を行ないまたは行なわ
ず、400−600’Cの温度に]00’C/min以
−にの加熱速度で加熱し、加熱直後または10分以内保
持した後、1.oO’c/Hr以]ユノ冷却速度c21
10℃以下に冷却して・1ノ・均結晶粒径を25μ以1
・にし、が−ノ、軟化11眉旨こ寄与する含有成分を固
iF(状(jととし、次いで、10%以4−の冷間圧延
を施すことを1、′1′徴と1−るキャンエンド用アル
ミニウム合金硬質板を第;)の発明とする3つの発明よ
りなるしのC゛ある。
An aluminum alloy hard plate for can ends and its manufacturing method according to the present invention 1, 1, (1) + 2. (1-
5, (ltu1%, CuO, 05-0.50% containing 195%, balance'):, t'! Aluminum 1. The first invention is an aluminum alloy hard plate characterized by an average crystal grain size of 25 μm or more before cold open rolling. , (2) M+; 2,0...5. Axial 1%, CuO
,05-0,50u+t% 3i J waist Furthermore, M+1
0.05□-Q, 50u+t%, Cr (1,10=0
.. Contains 40u+t% and the rest? 1b (substantially white male) \1 is characterized by having a diameter of 25/I m or less, which is made of \1, and has a final cold-rolled + IJ uniform viscous product diameter of 25/I m or less. The aluminum alloy hard plate for the can end is the second invention and the waist (: () h1 shi, 2. +1 ~ 5
.. Ou+L%, C++ to 0.05, including 0.50 sail%, depending on the required crab, Mn (1,05 to 0.50t
llL%, Cr (1,10he (1,4 (1+u1%), the balance is naturally composed of \1 aluminum alloy ffJJ lump is soaked at a temperature of 450 to 550°C) Rolling, then cold rolling or no cold rolling, heating to a temperature of 400-600'C] at a heating rate of 00'C/min or less, immediately after heating or after holding for within 10 minutes, 1. oO'c/Hr] Yuno cooling rate c21
Cool to below 10°C to reduce the uniform grain size to 25μ or more.
・Ingredients that contribute to softening and softening are defined as hard iF(j), and then subjected to cold rolling of 10% or more. The present invention consists of three inventions, the first invention being an aluminum alloy hard plate for a can end.

本発明【こ係るキャンエンド用アルミニウム合金石XI
!質板およびその製造法について9Y細に説明する。
The present invention [This aluminum alloy stone for can end XI]
! The quality plate and its manufacturing method will be explained in detail.

先ず、キャンエンド用アルミニウ1.’N ’& 4便
′t¥根の含有成分J5よび成分開会について説1り目
−る。
First, aluminum for the can end 1. 'N'& 4th flight 't¥ Root's content component J5 and component opening are explained in the first place.

N旬は強度向1−に有効な元素であり、14+に、ベー
クハード効果を得るために必須のムのC゛あり、含有微
か2.01%未!:l:i C’は7(11肉化橿−る
ための高強度力慴られず、また、5.(1+++lJg
を越える合(r−tυで′は高強度は得られるか、ハ延
11,1に月割れ1°1の問題か発生し、かつ、製品に
おける加1.に際L !’i!lれの発生する原因にな
る。よって、へjHf (1’ jj’、は2.0−5
.Ou+t%とする。
N is an effective element for the strength direction of 1-, and 14+ has C, which is essential for obtaining the bake hard effect, and the content is only 2.01%. :l:i C' is 7(11), and 5.(1+++lJg
(at r-tυ'), is it possible to obtain high strength? However, the problem of lunar cracking of 1°1 occurs in the extension 11,1, and when the addition of 1. in the product is Therefore, jHf (1'jj', is 2.0-5
.. Let Ou+t%.

Cuはへ18と同じ様な効果を−fj1−る元素で゛あ
り、含有量か0.05u+t%末::eiではベークハ
ート効果は得られず、また、0.5w1.%を越える含
有量では含有させた程の効果は期待で・きす、かっ、耐
蝕性において問題かある。よって、(九λ(i jil
、は(1,05−0,50田りんとする。
Cu is an element that has the same effect as H18, and the Bekehardt effect cannot be obtained at a content of 0.05u+t%::ei, and at a content of 0.5w1. If the content exceeds %, the expected effect will not be as good as that of its inclusion, but there may be problems in terms of scratch, corrosion, and corrosion resistance. Therefore, (9λ(i jil
, is (1,05-0,50 fields).

M nはベークハード効果には1ti接彰響をりえない
が、強度の向」―、結晶粒の微細化j;、1びツノ向′
l′1の制御(45°方向耳を高める)に効果があり、
3fノ量が0.05u+t、%未満ではこの効果は少な
く、また、0.50u+L%を越えて含有されるとこの
効果は得られるが、金属間化合物[A I6(M+++
 Fe)1等のサイズの成長を招き、特にキャンエンド
の7Fうな多段張出加工により割Jzの発生の起点とな
る。よって、Mn含有量は(1,05〜0.50田1%
とする。
Although Mn cannot exceed the 1ti tangential effect for the bake-hard effect, the direction of strength is '-, the refinement of grains j;, 1 and the horn direction'.
It is effective in controlling l'1 (increasing the 45° direction ear),
This effect is small when the amount of 3f is less than 0.05u+t,%, and this effect is obtained when the content exceeds 0.50u+l%, but the intermetallic compound [A I6(M+++
This leads to the growth of the size of Fe) 1 grade, and becomes the starting point for the occurrence of cracking Jz, especially due to the multi-stage overhang processing of the 7F eel at the can end. Therefore, the Mn content is (1.05~0.50 1%
shall be.

Crは強度の向上に有効な元素であり、含有量か0.1
(lu+t%未満ではこの効果が少なく、また、0.4
0+u1%を越えて含有されると金属間化合物のサイズ
の成長を招くようになる。よって、C「・含有量は0.
10−0.4(lu+L%とする。
Cr is an element effective in improving strength, and the content is 0.1
(If less than lu+t%, this effect is small, and 0.4
If the content exceeds 0+u1%, the size of the intermetallic compound will grow. Therefore, C' content is 0.
10-0.4 (lu+L%).

なお、その池含有される元素は通常市販の純アルミニウ
ムに含有されている不純物程度C゛あれば特に規制はし
ない。
The elements contained in the pond are not particularly regulated as long as they are at the level of impurities C' normally contained in commercially available pure aluminum.

次に、本発明に係る製造法について説明する。Next, the manufacturing method according to the present invention will be explained.

上記に説明した含有成分および成分割合のアルミニウム
合金を通常の方法により′t8解鋳造して鋳塊とし、こ
の鋳塊を450〜55[)’Cの7:j度にJ3いて均
熱処理するのであるが、この均熱処理は適11(な熱間
圧延および張出性(特に小径の多段張出性)を得るため
のもので・あり、45(1”(’;未γI4の均2屓品
度では熱間圧延時に耳割れが発’LL易く、がっ、微細
析出物が多く生成し張出性の低下を本腰55(1’cを
越える均熱温度ではバーニングおよび7クレを発生し、
製品特性の加1−性、表面品質の低下に一]ながる。よ
って、均熱ン晶度は450〜550’Cとする。
An aluminum alloy having the above-mentioned components and proportions is decasted by a normal method to form an ingot, and this ingot is soaked at 7:j degrees of 450 to 55 [)'C. However, this soaking treatment is to obtain suitable hot rolling and stretchability (especially small-diameter multi-step stretchability). If the heating temperature exceeds 55°C, edge cracking is likely to occur during hot rolling, and a large number of fine precipitates are formed, resulting in a decrease in elongation properties.
This leads to a decrease in product properties and surface quality. Therefore, the soaking crystallinity is set to 450 to 550'C.

その後の熱間圧延では特に限定的な条1′1はないが、
250℃以上の温度において熱間圧延を終了するのがよ
い。この熱間圧延後に冷間圧延は行なっても行なわなく
てもよいのである。
In the subsequent hot rolling, there is no particularly restrictive strip 1'1,
It is preferable to finish hot rolling at a temperature of 250° C. or higher. Cold rolling may or may not be performed after this hot rolling.

次に、行なう中間焼鈍であるが、これはベークハード効
果と成形性に優れた特性(微細結晶粒)を得るために重
要な工程であり、加熱温度を4()o・−600℃とす
るのはベークハードに必要なMgとCuを固溶するため
であり、400℃未11シ1の加熱温度では固溶が充分
に行なわれず、その後のベークハード効果が期待で′き
ず、また、600℃を越える加熱温度ではこの効果は飽
和してあまり期待できず、かえって、バーニング等を起
しこ特性の11(、l’につながる。よって、加熱温度
は40(1= [1(1(1’Cとする。
Next is intermediate annealing, which is an important step in order to obtain a bake-hard effect and excellent properties (fine crystal grains) in formability, and the heating temperature is 4 () o -600°C. This is to form a solid solution of Mg and Cu, which are necessary for bake-hardening, and heating temperatures below 400°C do not sufficiently form a solid-solution, and the subsequent bake-hardening effect is not expected. At a heating temperature exceeding ℃, this effect is saturated and cannot be expected much, and instead causes burning etc., which leads to the characteristic 11(, l'. Therefore, the heating temperature is 40(1=[1(1(1 'C.

この際の加熱速度100°C/ m聞易−1−および加
熱直後または10分以内保持後100℃/ l l r
以」−の冷却速度で200℃以下の温度まで冷却する必
決があり、これは、成形性に有効な微細結晶R(25μ
III以1・)とし、かつ、Mg、Cuを強制固溶さぜ
る、二とにあり、これらの範囲外においてはベークハー
ド効果および微細結晶粒による高成形性がイ:1られな
い。
At this time, the heating rate was 100°C/m, and 100°C/l l r immediately after heating or after being held for less than 10 minutes.
It is essential to cool down to a temperature of 200°C or less at a cooling rate of
III.1.) and Mg and Cu are forcibly mixed into solid solution. Outside these ranges, the bake-hard effect and the high formability due to fine crystal grains cannot be achieved.

なお、保持時間を10分以内とするのは10分を越える
時間保持してもベークハード効果は向−1−ぜず、かえ
っ−て、結晶粒の成長とエネルギーの無駄となり、また
、200°C以下の温度まで冷却するのはベーキングに
よる硬化を図るためである。
Note that holding the holding time within 10 minutes does not improve the bake-hard effect even if the holding time exceeds 10 minutes, and on the contrary causes crystal grain growth and wastes energy. The purpose of cooling to a temperature below C is to harden by baking.

本発明に係るキャンエンド用アルミニウム合金硬質板お
よびその製造法について実Mi例を説明す実施例1 第1表に示す含有成分および成分開会のアルミニウム合
金鋳塊を500’CX旧1rの均熱処理と熱間圧延によ
り4mmの熱間圧延板とした。その後、1mm厚まで冷
間圧延し、中間焼鈍は500 ’C’ X :(Os+
・(。
Example 1 to explain an actual example of the aluminum alloy hard plate for can ends and the manufacturing method thereof according to the present invention An aluminum alloy ingot with the contents and components shown in Table 1 was subjected to soaking treatment of 500'CX old 1r. A 4 mm hot rolled plate was obtained by hot rolling. Thereafter, it was cold rolled to a thickness of 1 mm, and intermediate annealing was performed at 500'C'
・(.

で加熱、冷却速度を500 ’C/+n i nとした
。これを冷間圧延し0.30+nm厚にした時の(幾械
的性賀(1,i:延のまま、ベーキング後)と中間焼鈍
後の結晶粒径を第2表に示す。結lit冒rt、t’f
、は切断法によりその・1′−均値をめたものである。
The heating and cooling rates were set at 500'C/+n i n. Table 2 shows the grain size when this was cold rolled to a thickness of 0.30+ nm (geometrical properties (1,i: as rolled, after baking) and after intermediate annealing. rt,t'f
, is the 1'-average value determined by the cutting method.

この第2表かられかる、1、うに、本発明(No、l、
No、2、No、4はAI Cu−へ旬系の微細イ11
出物により、ベーキングによる強度低1ζは比較例に比
して少なく、特に、NO,,1の場合には抗張力σは逆
に向」ニしており、また、結晶ネη径は本発明は全べて
25μm以下となっている。後述Yる第・1表に示すよ
うに、成形性は全て良brであるが、高強度高成形性に
ついては本発明が優れている。。
From this Table 2, Rekaru, 1, sea urchin, present invention (No, l,
No, 2, No, 4 are AI Cu-Heshun type micro-i 11
The low strength 1ζ due to baking is smaller than that of the comparative example, and especially in the case of NO,,1, the tensile strength σ is in the opposite direction, and the crystal diameter η is smaller than that of the comparative example. All of them are 25 μm or less. As shown in Table 1 below, all moldability was good, but the present invention was superior in terms of high strength and high moldability. .

実施例2 実施例1における中間焼鈍を:(Li(1’CX 2山
、加熱、冷却速度40℃/ Hrで実施した場jrの(
1,:tIIIIl+1’Iの(茂(成約性質および中
間焼鈍後のV晶1’i IJ、を・第3表に、また、成
形性については第・1表に大7ノ示す。
Example 2 When the intermediate annealing in Example 1 was carried out with: (Li (1'CX 2 peaks, heating and cooling rate of 40°C/Hr)
1,:tIIII+1'I (contract properties and V crystal 1'i IJ after intermediate annealing are shown in Table 3, and the formability is shown in Table 1.

この第3表および第4表かられ/J:るように、中間焼
鈍を従米条j!1(3GO°(:X211r、加熱、冷
ノJl速度40℃/11r)で実施した場合、本発明の
含(i成分およびrL分割合であるアルミニウムa金に
I5いても、ベーキングによる軟化が大きく、高強度が
iJられず、また、中間焼鈍後の結晶粒#J25 /l
 m l;月、どなり、現状の板厚では成形上問題はな
いが、薄肉化した場合1こは問題が生じる。
From Tables 3 and 4, intermediate annealing is performed as shown in Table 3 and Table 4. When carried out at 1 (3 GO° (: , high strength is not achieved, and grain #J25/l after intermediate annealing
ml; Moon, roar, there is no problem in forming with the current plate thickness, but if the thickness is made thinner, a problem will occur.

実施例3 第1表に示すNo、1合金について、中間焼鈍をFSS
表に示す条件で実施し、0.:(囮0厚の時の1tlt
械的性質と申開焼鈍後の結晶粒を第11表に示す。なお
、到達温度(加熱温度)における保11時間は(lse
cである。
Example 3 For alloy No. 1 shown in Table 1, intermediate annealing was performed by FSS.
Conducted under the conditions shown in the table, 0. :(1tlt when the decoy is 0 thick
Table 11 shows the mechanical properties and grains after open annealing. In addition, the 11 hours of holding at the reached temperature (heating temperature) is (lse
It is c.

この第5表よりわかるように、加熱温度(到達温度)は
4(Xl’C以上が必要であり、バーニング等を考慮す
ると、400〜60(1’cの加熱?!a! 瓜としな
ければならず、また、加熱速度が100°C/ Ill
 i n以下では微細な結晶粒が得られず、冷却速度が
100’C/Hr(1,7°C/+n1u)以下ではベ
ークバー・ドに有効なCu、Mgが冷却時に析出してベ
ーキ、・グ時の硝化が11られない。
As can be seen from Table 5, the heating temperature (achieved temperature) needs to be 4 (Xl'C or higher), and considering burning, etc., it is 400 to 60 (1'C heating?!a! If it is not a melon) Also, the heating rate is 100°C/Ill
If the cooling rate is less than i n, fine crystal grains cannot be obtained, and if the cooling rate is less than 100'C/Hr (1,7°C/+n1u), Cu and Mg, which are effective in baking bars, will precipitate during cooling, resulting in baking,... Nitrification during cleaning is not possible.

1、フ、ト説明したように、本発明に1系るA−、ンJ
〜ンド用アルミニウム介金イi更質板JよJ、びくの製
造法は上記のI’+Vi成を有しているものであるから
、塗装印刷時のベーキング丁程でベークハード効果を利
用して高強度を保持し、がっ、結晶粒の徽、11+化に
ょリキVンエントの主要成形である多伐張出加IVIに
優れており、そして、薄肉化が「り能C゛あるという効
果を奏するものである。
1. As explained above, the present invention includes A-, NJ
The manufacturing method for the aluminum alloy plate J, J, and Biku has the above-mentioned I'+Vi composition, so the bake-hard effect is utilized in the baking stage during coating printing. It maintains high strength, has excellent crystal grain shape, and is excellent in multi-cut extension IVI, which is the main forming process of 11+ conversion liquid Vents. It is something that plays.

Claims (3)

【特許請求の範囲】[Claims] (1)Mg 2.0〜5.0IIIL%、Cu 000
5・−(1,5(lu+L%を含有し、残部実質的にA
1からなるアルミニウム合金で、かつ、最終冷間圧延前
の−I勺う珪11品粒径が25μ+n以下であることを
特徴とするキャンエンド用アルミニウム合金硬質板。
(1) Mg 2.0-5.0IIIL%, Cu 000
5・-(1,5(lu+L%), the remainder is substantially A
1. An aluminum alloy hard plate for can ends, which is made of an aluminum alloy comprising:
(2)Mg2.0−5.Ou+t%、Cu O,05−
0,50u+L%を含有し、さらに、 Mu 0.05−0.50ulL%、Cr O,10□
−(1,4(1+u1%を含有し、残部実質的にA1か
らなるアルミニウム合金で、かつ、最終冷間1王延前の
甲・均結晶粒iヤが25μm0以下であることを特徴と
するAnノンエンドアルミニウム合金硬質板。
(2) Mg2.0-5. Ou+t%, CuO,05-
Contains 0.50u+L%, and further contains Mu 0.05-0.50ulL%, CrO, 10□
- An aluminum alloy containing (1,4(1+u1%) and the remainder substantially consisting of A1, and characterized in that the A/uniform grain size before the final cold rolling is 25 μm or less. End aluminum alloy hard plate.
(3)M62.0−5.Ou+1%、Cu 0.05〜
0.50+n1%を含有し、必要に応じて、Mn 0.
05〜0.5(l四1%、0「0.10〜0.4(1w
t%を含有し、残部実質的にA1からなるアルミニウム
合金鋳塊を、450〜550°Cの温度で均熱および熱
間圧延を施し、その後珍問圧延を行ないまたは行なわず
、400〜600°Cのン品度に+00°C/m i 
n以上の加熱速度で加熱し、加熱直後または10分以内
保持した後、100°C/l+r以−1−の冷却速度で
200℃以下に冷却して平均結晶粒径を25μ以下にし
、がっ、軟化防止に寄−リする含有成分を固溶状態とし
、次いで、10%以」二の冷間圧延を施すことを特徴と
するキャンエンド用アルミニウl、合金硬質板の製造法
(3) M62.0-5. Ou+1%, Cu 0.05~
0.50+n1%, and optionally Mn 0.
05~0.5(l41%, 0'0.10~0.4(1w
An aluminum alloy ingot containing t% and the remainder substantially consisting of A1 is subjected to soaking and hot rolling at a temperature of 450 to 550°C, and then heated to 400 to 600°C with or without rolling. +00°C/m i
Heating at a heating rate of n or more, immediately after heating or holding within 10 minutes, and then cooling to 200°C or less at a cooling rate of 100°C/l+r or more -1- to reduce the average crystal grain size to 25μ or less. 1. A method for manufacturing aluminum and alloy hard plates for can ends, which comprises bringing the contained components contributing to prevention of softening into a solid solution state, and then subjecting them to cold rolling of 10% or more.
JP15675883A 1983-08-27 1983-08-27 Hard aluminum alloy sheet for can end and its production Granted JPS6050141A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP15675883A JPS6050141A (en) 1983-08-27 1983-08-27 Hard aluminum alloy sheet for can end and its production

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15675883A JPS6050141A (en) 1983-08-27 1983-08-27 Hard aluminum alloy sheet for can end and its production

Publications (2)

Publication Number Publication Date
JPS6050141A true JPS6050141A (en) 1985-03-19
JPH0331779B2 JPH0331779B2 (en) 1991-05-08

Family

ID=15634674

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15675883A Granted JPS6050141A (en) 1983-08-27 1983-08-27 Hard aluminum alloy sheet for can end and its production

Country Status (1)

Country Link
JP (1) JPS6050141A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63286589A (en) * 1987-05-19 1988-11-24 Kobe Steel Ltd Hard al alloy sheet for packing having superior curlability and production thereof
JPH01119637A (en) * 1987-10-30 1989-05-11 Furukawa Alum Co Ltd Aluminum alloy material for can end
JPH01162753A (en) * 1987-12-18 1989-06-27 Kobe Steel Ltd Manufacture of hard aluminum-alloy sheet for package
JPH01201449A (en) * 1988-02-06 1989-08-14 Kobe Steel Ltd Manufacture of hard aluminum alloy sheet for package
JPH01301831A (en) * 1988-05-31 1989-12-06 Kobe Steel Ltd Al alloy plate for stay-on tab and its manufacture
CN105803275A (en) * 2016-03-17 2016-07-27 中铝科学技术研究院有限公司 Aluminum alloy sheet material for thin ring-pull can cover and preparation method
WO2019021899A1 (en) * 2017-07-26 2019-01-31 株式会社Uacj Aluminum alloy plate and method for producing same

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS56102565A (en) * 1980-01-16 1981-08-17 Kobe Steel Ltd Manufacture of al alloy plate for packing

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS56102565A (en) * 1980-01-16 1981-08-17 Kobe Steel Ltd Manufacture of al alloy plate for packing

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63286589A (en) * 1987-05-19 1988-11-24 Kobe Steel Ltd Hard al alloy sheet for packing having superior curlability and production thereof
JPH01119637A (en) * 1987-10-30 1989-05-11 Furukawa Alum Co Ltd Aluminum alloy material for can end
JPH01162753A (en) * 1987-12-18 1989-06-27 Kobe Steel Ltd Manufacture of hard aluminum-alloy sheet for package
JPH01201449A (en) * 1988-02-06 1989-08-14 Kobe Steel Ltd Manufacture of hard aluminum alloy sheet for package
JPH01301831A (en) * 1988-05-31 1989-12-06 Kobe Steel Ltd Al alloy plate for stay-on tab and its manufacture
CN105803275A (en) * 2016-03-17 2016-07-27 中铝科学技术研究院有限公司 Aluminum alloy sheet material for thin ring-pull can cover and preparation method
WO2019021899A1 (en) * 2017-07-26 2019-01-31 株式会社Uacj Aluminum alloy plate and method for producing same

Also Published As

Publication number Publication date
JPH0331779B2 (en) 1991-05-08

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