JP2004263253A - Aluminum alloy hard sheet for can barrel, and production method therefor - Google Patents

Aluminum alloy hard sheet for can barrel, and production method therefor Download PDF

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JP2004263253A
JP2004263253A JP2003055368A JP2003055368A JP2004263253A JP 2004263253 A JP2004263253 A JP 2004263253A JP 2003055368 A JP2003055368 A JP 2003055368A JP 2003055368 A JP2003055368 A JP 2003055368A JP 2004263253 A JP2004263253 A JP 2004263253A
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plate
range
rolling
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hot rolling
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JP4257135B2 (en
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Akira Hibino
旭 日比野
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Furukawa Sky KK
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Furukawa Sky KK
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Abstract

<P>PROBLEM TO BE SOLVED: To provide the material for a DI (draw and ironing) can barrel excellent in the balance of strength, low earing ratio, ironing properties and flange formability at a low cost. <P>SOLUTION: The Al alloy hard sheet consists of an Al-Mg-Mn based alloy. Provided that the total of each orientation density of Cu, S and Bs belonging to βfiber in the sheet surface layer is defined as d<SB>0</SB>, the total of each orientation density of Cu, S and Bs belonging to βfiber at the position of 1/4 of the sheet thickness as d<SB>1/4</SB>, the Cube orientation density in the sheet surface layer as C<SB>o</SB>and the Cube orientation density at the position of 1/4 of the sheet thickness as C<SB>1/4</SB>, (d<SB>0</SB>+d<SB>1/4</SB>)>(C<SB>o</SB>+C<SB>1/4</SB>) is satisfied. The solid solution content of Mn is controlled to 0.05 to 0.35% and its electric conductivity to 34 to 45 IACS%. In the production method, an ingot is subjected to homogenizing treatment, then, on hot rolling, the starting temperature is controlled to 350 to 590°C, from a sheet thickness of 50 mm to a finish sheet thickness, the material temperature is controlled to 280 to 450°C, the strain rate in each pass to 2.0 to 350/s, the residence time between the passes to ≤10 min, the average surface temperature of a rolling roll to ≤350°C, the finish material temperature in the hot rolling to 280 to 350°C, the finish sheet thickness to 1.5 to 2.8 mm and the cooling rate to a room temperature to ≤100°C/hr. Thereafter, cold rolling of ≥65% is performed without carrying out process annealing. <P>COPYRIGHT: (C)2004,JPO&NCIPI

Description

【0001】
【発明が属する技術分野】
この発明はDI成形(絞り−しごき加工)による2ピースアルミニウム缶用の缶胴に使用されるAl−Mg−Mn系アルミニウム合金の硬質板、およびその製造方法に関し、特に深絞り耳が低くかつ塗装焼付後の強度が高く、しかもDI加工時における成形性、例えばしごき加工性などが優れると同時に塗装焼付後の成形性、例えばフランジ成形性などが優れたDI缶胴用アルミニウム合金硬質板およびその製造方法に関するものである。
【0002】
【従来の技術】
一般に2ピースアルミニウム缶(DI缶)の製造工程としては、缶胴用素材に対して、深絞り加工およびしごき加工によるDI成形を施して缶胴形状とした後、所定の寸法、形状にトリミングを施して脱脂・洗浄処理を行ない、さらに塗装・印刷を行って焼付け(ベーキング)を行ない、その後に缶胴縁部に対してネッキング加工、フランジ加工を行ない、別に成形した缶蓋と合せてシーミング加工を行なうのが通常である。
【0003】
このようにして製造されるDI缶胴用素材としては、従来からAl−Mg−Mn系合金からなるJIS3004合金の硬質板が広く使用されている。この3004合金は、しごき加工性に優れていて、強度を高めるために高圧延率で冷間圧延を施した場合でも比較的良好な成形性を示すところから、DI缶胴材として好適であるとされている。
【0004】
なおこのような3004合金からなるDI缶胴用硬質板の製造方法としては、一般にDC鋳造法などによって鋳造した後、鋳塊に均質化処理を施し、さらに熱間圧延および冷間圧延によって所定の板厚とし、かつその過程における熱間圧延後の冷間圧延前、もしくは冷間圧延の中途において、再結晶のために中間焼鈍を施す方法が一般的である。
【0005】
ところで2ピースアルミニウム缶胴(DI缶)については、主として材料コスト削減の観点から、薄肉化を図ることが強く望まれている。そしてこのように薄肉化を図る場合、薄肉化に伴なう缶の座屈強度低下の問題等を回避するため、材料の高強度化を図ることが不可欠である。
【0006】
さらにDI缶胴用材料としては、DI成形時における耳率が小さいことが望まれる。すなわち、DI成形時の耳率が低いことは、DI成形時の歩留り向上と、缶胴の耳切れに起因する缶胴破断防止の点から重要である。
【0007】
そしてまた、DI缶製造時におけるフランジ成形性(口拡げ性)が優れること、およびしごき性(耐缶切れ性)が優れることも必要である。
【0008】
ここで、これらの強度、耳率、フランジ成形性(口拡げ性)、しごき性(耐缶切れ性)は、いずれか一つが優れていれば良いというものではなく、これらのバランスが良好で総合的に優れていることが必要であり、また製造方法としては、上述のような材料特性からの諸要求のほか、製造コストが低廉であることも重要である。
【0009】
ところで従来の3004合金缶胴用硬質板の一般的な製造方法においては、前述のように熱間圧延後の冷間圧延前、あるいは冷間圧延の中途において、再結晶のために中間焼鈍を行なうのが通常である。このような中間焼鈍の観点から従来の主な製造プロセスを分類すれば、次の(a)〜(c)のプロセスに分けられる。
(a) 熱延−バッチ焼鈍プロセス
これは、通常の熱間圧延の後、加熱速度の遅い箱型焼鈍炉(バッチ式焼鈍炉;BAF)を用いて焼鈍する方法である。
(b) 熱延−連続焼鈍プロセス
これは、通常の熱間圧延の後、加熱速度の速い連続焼鈍炉(CAL)を用いて焼鈍する方法である。
(c) 冷延中間連続焼鈍プロセス
これは、通常の熱間圧延後の冷間圧延の中途において、加熱速度の速い連続焼鈍炉を用いて焼鈍する方法である。
【0010】
さらに、以上の(a)〜(c)のプロセスのほか、次の(d)のような方法もある。
(d) 自己再結晶プロセス
これは、熱間圧延の上がり温度を材料の再結晶温度以上に制御することによって、熱間圧延上がりの状態で材料を自己再結晶(自己焼鈍)させる方法である。
【0011】
以上のような(a)〜(d)のプロセスのうち、(a)、(b)、(d)のプロセスを適用した場合、いずれも最終的に得られた缶胴材のしごき性が劣るという共通の問題がある。また(d)のプロセスを適用した場合、得られた缶胴材の材料強度が不足するという問題がある。さらに(c)のプロセスを適用した場合、缶胴材としてしごき性は優れるものの、フランジ成形性が劣るという問題がある。そしてまた、熱間圧延後に再結晶のための焼鈍を必要とする(a)、(b)、(c)のプロセスでは、製造コストが割高であるという問題もある。
【0012】
ここで、Al−Mg−Mn系合金からなるDI缶胴材の製造方法として既に提案されている先行技術の方法としては、例えば特許文献1〜特許文献8に示すような方法があるが、これらのうち特許文献1〜特許文献6の方法は、いずれも熱間圧延の後、もしくは冷間圧延の中途で焼鈍を必須とするものであり、前述のようにコスト面等で問題があった。
【0013】
また特許文献7には、熱間圧延後に焼鈍なしで最終冷間圧延を施す方法も示されているが、この特許文献7に示されているのは熱間圧延機としてタンデム式圧延機を用いた場合の方法であり、リバース式圧延機(リバーシング・ミル、リバーシング・ウォームミル)を用いた場合については開示されていない。タンデム式圧延機とリバース式圧延機では、最適な熱間圧延プロセス条件が異なるのが通常であり、したがって特許文献7に示されている方法をリバース式圧延機を用いた場合に転用しても、直ちに前記諸特性の優れた缶胴材が得られるとは限らないのが実情である。
【0014】
さらに特許文献8の方法でも、熱間圧延後の焼鈍を省略しても良いとされているが、この特許文献8の方法も、熱間圧延機としてタンデム式圧延機を使用するものであり、またその熱間圧延条件も厳密に規定されてはおらず、そのため特許文献8の方法をリバース式圧延機を用いる場合に転用しても、前記諸特性のバランスに優れたDI缶胴材は得られなかったのである。
【0015】
【特許文献1】特開平11−256290号公報
【特許文献2】特開平11−256291号公報
【特許文献3】特開平11−256292号公報
【特許文献4】特開2000−234158号公報
【特許文献5】特開2001−40461号公報
【特許文献6】特開2002−212691号公報
【特許文献7】特開平10−310837号公報
【特許文献8】特開平11−140576号公報
【0016】
【発明が解決しようとする課題】
この発明は以上の事情を背景としてなされたもので、DI缶胴材として望まれる諸特性をバランスよく満足し得る材料、すなわち高強度を有すると同時に低耳率で、しかもフランジ成形性、しごき性に優れていて、これらの諸特性のバランスが総合的に良好なDI缶胴用のアルミニウム合金板を提供すると同時に、このような諸特性のバランスの優れた高品質のDI缶胴用硬質板を、低コストで得る方法を提供することを目的とするものであり、特に熱間圧延機としてタンデム圧延機ではなくリバース方式の圧延機を使用して上述のような高品質のDI缶胴材を低コストで得るに適した方法を提供することを目的とするものである。
【0017】
【課題を解決するための手段】
本発明者等が前述の課題を解決するべく種々実験・検討を重ねた結果、板の集合組織、特に板表面に近い部分の集合組織を適切に制御すると同時に、Mn固溶量、導電率を適切に調整することによって、高強度と低耳率を確保しながら、フランジ成形性としごき性のバランスを最適化し、高品質のDI缶胴材を得ることができることを見出した。そしてまた、製造方法として、熱間圧延条件、特に板厚50mmの段階から熱間圧延上がりの段階における条件を厳密に規制することによって、熱間圧延後の再結晶のための焼鈍を省略しつつ高品質のDI缶胴材を得ることができるプロセス、特にリバーシングミル方式の熱間圧延機を使用して高品質のDI缶胴材を得ることができるプロセスを実現できることを見出し、この発明をなすに至った。
【0018】
具体的には、請求項1の発明の缶胴用アルミニウム合金硬質板は、Mg0.5〜2.0%、Mn0.5〜2.0%、Fe0.1〜0.7%、Si0.05〜0.5%、Cu0.05〜0.5%を含有し、残部がAlおよび不可避的不純物よりなるアルミニウム合金からなり、かつ板表層のβファイバに属するCu方位、S方位、Bs方位の各方位密度の合計をdとするとともに、板表面から板厚方向に板厚の1/4の深さの位置におけるβファイバに属するCu方位、S方位、Bs方位の各方位密度の合計をd1/4とし、さらに板表層におけるCube方位の方位密度をCとし、かつ板表面から板厚方向に板厚の1/4の深さの位置におけるCube方位の方位密度をC1/4とした場合に、次式
(d+d1/4)>(C+C1/4
を満足し、さらにMn固溶量が0.05〜0.35%の範囲内でかつ導電率が34〜45IACS%の範囲内であることを特徴とするものである。
【0019】
また請求項2の発明の缶胴用アルミニウム合金硬質板は、請求項1の缶胴用アルミニウム合金硬質板において、前記アルミニウム合金の成分として、さらにCr0.05〜0.3%、Zn0.05〜0.5%、Ti0.005〜0.20%のうちの1種または2種以上を含有することを特徴とするものである。
【0020】
さらに請求項3の発明の缶胴用アルミニウム合金硬質板の製造方法は、請求項1もしくは請求項2において規定される成分組成のアルミニウム合金を鋳造した後、520〜630℃の範囲内の温度で1時間以上保持する均質化処理を行ない、次いで熱間圧延を行なって巻取り、100℃以下の温度まで冷却するにあたり、
(1)熱間圧延開始温度を350〜590℃の範囲内とし、
(2)板厚50mmから上がり板厚までの熱間圧延中において、材料温度を280〜450℃の範囲内に制御するとともに、各パスの歪み速度を2.0〜350/秒の範囲内に制御し、かつ各パス間での滞留時間を10分以内に制御し、
(3)板厚50mmから上がり板厚までの熱間圧延中において圧延ロールと板との接触部分の平均温度を350℃以下に保持し、
(4)熱間圧延上がりの材料温度を280〜350℃の範囲内とし、
(5)熱間圧延上がり板厚を1.5〜2.8mmの範囲とし、
(6)熱間圧延上がりの280〜350℃の範囲内の温度から100℃以下までの平均冷却速度を100℃/時間以下に制御し、
以上の(1)〜(6)によって、耐力が120MPa以下、板表面から板厚方向に板厚の1/4の深さの部位におけるCube方位の方位密度がランダム方位の5〜140倍の範囲内にあり、かつ圧延集合組織に属するCu方位、S方位、Bs方位の各方位密度がそれぞれランダム方位の10倍以下である熱間圧延板を得、さらに、中間焼鈍を施すことなく65%以上の圧延率で冷間圧延を施すことを特徴とするものである。
【0021】
さらにまた請求項4の発明の缶胴用アルミニウム合金硬質板の製造方法は、請求項3に記載の缶胴用アルミニウム合金硬質板の製造方法において、前記冷間圧延の後、さらに80〜200℃の範囲内の温度に加熱して0.1〜24時間保持する最終焼鈍を行なうことを特徴とするものである。
【0022】
【発明の実施の形態】
先ずこの発明の缶胴用アルミニウム合金硬質板に用いられるアルミニウム合金の成分組成の限定理由について説明する。
【0023】
Mg:
Mgの添加は、Mgそれ自体の固溶による強度向上に効果があり、またMgの固溶に伴なう加工硬化量の増大による強度向上が期待でき、さらにはSiとの共存によるMgSiの時効析出による強度向上も期待でき、したがってMgは缶胴材として必要な強度を得るためには不可欠の元素である。またMgは、加工時の転位の増殖作用があるため、再結晶粒を微細化させるためにも有効である。但しMg量が0.5%未満では上述の効果が少なく、一方2.0%を越えれば、高強度は容易に得られるものの、DI加工時の変形抵抗が大きくなって絞り性やしごき性を悪くする。したがってMg量は0.5〜2.0%の範囲内とした。
【0024】
Mn:
Mnは強度および成形性の向上に寄与する有効な元素である。特にこの発明で目的としている用途である缶胴材ではDI成形時にしごき加工が加えられるため、とりわけMnは重要となる。アルミニウム板のしごき加工においては通常エマルジョンタイプの潤滑剤が用いられているが、Mn系晶出物が少ない場合には同程度の強度を有していてもエマルジョンタイプ潤滑剤だけでは潤滑能が不足し、ゴーリングと称される擦り疵や焼付きなどの外観不良が発生するおそれがある。ゴーリングは晶出物の大きさ、量、種類に影響されることが知られており、その晶出物を形成するためにMnは不可欠な元素である。Mn量が0.5%未満ではMn系化合物による固体潤滑的な効果が得られず、一方Mn量が2.0%を越えればAlMnの初晶巨大金属間化合物が発生して、著しく成形性を損なってしまう。そこでMn量は0.5〜2.0%の範囲内とした。またここで製品板中における固溶Mnは、加工時の回復を抑制する効果および塗装焼付け時の軟化を低減する効果があり、そこでこの発明では後に改めて説明するように、材料中のトータルMn量のみならず、製品板中のMn固溶量をも規定している。
【0025】
Fe:
Feは、Mnの晶出や析出を促進して、アルミニウム基地中のMn固溶量やMn系金属間化合物の分散状態を制御するために必要な元素である。適切な化合物分散状態を得るためには、Mn添加量に応じてFeを添加することが必要である。Fe量が0.1%未満では適切な化合物分散状態を得ることが困難であり、一方Fe量が0.7%を越えれば、Mn添加に伴なって初晶巨大金属間化合物が発生しやすくなり、成形性を著しく損なう。そこでFe量の範囲は0.1〜0.7%とした。
【0026】
Si:
Siの添加は、MgSi系化合物の析出による時効硬化を通じて缶胴材の強度向上に寄与する。またSiは、Al−Mn−Fe−Si系金属間化合物を生成して、Mn系金属間化合物の分散状態を制御するために必要な元素である。Si量が0.05%未満では上記の効果が得られず、一方0.5%を越えれば時効硬化により材料が硬くなりすぎて成形性を阻害する。そこでSi量の範囲は0.05〜0.5%とした。
【0027】
Cu:
Cuは、アルミニウム基地中に溶体化させておき、塗装焼付処理時にAl−Cu−Mg系析出物として析出することによる析出硬化を利用した強度向上に寄与する。Cu量が0.05%未満ではその効果が得られず、一方Cuを0.5%を越えて添加した場合には、時効硬化は容易に得られるものの、硬くなりすぎて成形性を阻害し、また耐食性も劣化する。そこでCu量の範囲は0.05〜0.5%とした。
【0028】
以上の各元素のほかは、基本的にはAlおよび不可避的不純物とすれば良いが、必要に応じてTi、Cr、Znのうちの1種または2種以上を添加しても良い。これらのTi、Cr、Znについてさらに詳細に説明する。
【0029】
Ti:
通常のアルミニウム合金においては、鋳塊結晶粒微細化のためにTiを微量添加することが行なわれており、この発明においても、必要に応じて微量のTiを添加しても良い。但しTi量が0.005%未満ではその効果が得られず、一方0.20%を越えれば巨大なAl−Ti系金属間化合物が晶出して成形性を阻害するため、Tiを添加する場合のTi量は0.005〜0.20%の範囲内とした。またTiとともに微量のBを添加すれば鋳塊結晶粒微細化の効果が向上することが知られており、そこでこの発明の場合もTiとともに微量のBを添加することは許容される。このようにTiと併せてBを添加する場合、B量が0.0001%未満ではその効果がなく、0.05%を越えればTi−B系の粗大粒子が混入して成形性を害することから、TiとともにBを添加する場合のB量は0.0001〜0.05%の範囲内ととすることが望ましい。
【0030】
Cr:
Crは強度向上に効果的な元素であるが、0.05%未満ではその効果が少なく、0.3%を越えれば巨大晶出物生成によって成形性の低下を招くため、好ましくない。そこでCrを添加する場合のCr量の範囲は0.05〜0.3%とした。
【0031】
Zn:
Znの添加はAl−Mg−Zn系粒子の時効析出による強度向上に寄与するが、0.05%未満ではその効果が得られず、0.5%を越えれば、強度への寄与については問題がないが、耐食性を劣化させる。そこでZnを添加する場合のZr量の範囲は0.05〜0.5%とした。
【0032】
さらにこの発明の缶胴用アルミニウム合金硬質板においては、合金の成分組成を前述のように調整するばかりでなく、製品板中における固溶元素の固溶量を適切に調整する必要がある。そしてこの発明では、各固溶元素のうち、代表的なMnについてその固溶量を定めるとともに、その他の固溶元素を含めた総合的な固溶量の指標として導電率を定めた。
【0033】
すなわち、固溶元素は回復の抑制や塗装焼付け時における軟化の抑制などに効果があり、塗装焼付け後に適切な強度を得るためには、各元素の添加量だけではなく、固溶元素の固溶量を適切に制御する必要がある。そしてこの発明では、最も大きな影響を与えるMn固溶量を0.05〜0.35%の範囲内とするとともに、Mnのほかの固溶元素Mg、Cu、Si、Feの固溶量を、板の導電率を指標として34〜45IACS%の範囲内とすることによって、しごき性およびフランジ成形性を損なうことなく、塗装焼付け後に必要な高強度を得ることが可能となったのである。
【0034】
ここで、Mn固溶量が0.05%未満では、必要な強度を得ることが困難となり、一方0.35%を越えればしごき性およびフランジ成形性が悪くなる。したがってMn固溶量は0.05〜0.35%の範囲内とした。
【0035】
またMnのほかMg、Cu、Si、Fe等の総合的な固溶量の指標となる板の導電率が34IACS%未満では、全体の固溶量が多過ぎて、しごき性およびフランジ成形性が悪くなり、一方導電率が45IACS%を越えれば、全体の固溶量が少な過ぎて強度不足となるおそれがあり、そこで板の導電率を34〜45IACS%の範囲内に定めた。
【0036】
そしてまたこの発明の缶胴用アルミニウム合金硬質板では、板の表面やそれに近い部分(板表層の部位および板厚の1/4の部位)の集合組織を適切に制御することが、他の特性に悪影響を与えることなくしごき性を向上させるために重要である。
【0037】
すなわち、本願発明者等の詳細な実験によれば、d、d1/4、C、C1/4を、それぞれ
:板表層におけるβファイバに属するCu方位、S方位、Bs方位の各方位密度の合計
1/4:板表面から板厚方向に板厚の1/4の深さの部位におけるβファイバに属するCu方位、S方位、Bs方位の各方位密度の合計
:板表層におけるCube方位の方位密度
1/4:板表面から板厚方向に板厚の1/4の深さの部位におけるCube方位の方位密度
と規定した場合、次の(1)式
(d+d1/4)>(C+C1/4) ・・・(1)
を満たすように板の集合組織を調整することによって、しごき性を従来と比較して格段に向上させ得ることを見出し、この発明において(1)式を規定した。(1)式が満たさなければ充分なしごき性向上効果が得られない。
【0038】
なお各方位密度は、X線回折装置を用い、Schulz反射法により、{200}、{220}、{111}の不完全極点図を測定し、これらをもとに三次元結晶方位解析(ODF)を行なって得たものとする。またここで、Cu方位は{111}<112>方位、S方位は{123}<634>方位、Bs方位は{110}<112>方位、Cube方位は{001}<100>方位がそれぞれ理想方位であるが、これら理想方位を中心に方位差15°の範囲内のものも含むものとする。
【0039】
なおまた、d、Cの各方位密度については板の表層と規定しているが、これは板の表面で測定した方位密度を意味する。
【0040】
次にこの発明の缶胴用アルミニウム合金硬質板の製造プロセスについて説明する。
【0041】
先ず前述のような合金組成を有するアルミニウム合金鋳塊を、常法にしたがってDC鋳造法(半連続鋳造法)により鋳造する。次いでその鋳塊に対して均質化処理を行ない、鋳塊の偏析を均質化するとともにMn、Fe、Si系の第2相粒子サイズと分布を最適化する。またこのような第2相粒子のサイズと分布は最終板の集合組織に影響を及ぼすこともある。均質化処理温度が520℃未満では、均質化効果が不充分であるばかりでなく、最適な集合組織が得られなくなるおそれがあり、一方630℃を越えれば、共晶融解のおそれがある。また均質化処理の時間は、1時間未満では均質化効果が不充分となるばかりでなく、最適な集合組織が得られないおそれがある。したがって均質化処理条件は、520〜630℃の範囲内の温度で1時間以上と規定した。なお均質化処理時間の上限は特に規定しないが、経済性を考慮して48時間以下とすることが好ましい。
【0042】
均質化処理を施した鋳塊に対しては、熱間圧延を行なう。この発明の方法の場合、熱間圧延後に焼鈍を施さない方式を適用しているため、後述するように熱間圧延上がり板の状態で90%以上の再結晶率で再結晶している必要があり、また熱間圧延中の再結晶挙動は集合組織の制御を通じて耳率の低減およびしごき性の向上に大きな影響を与える。そこでこの発明では、熱間圧延開始温度や熱間圧延終了温度(熱延上がり温度)のみならず、熱間圧延中における板厚50mmの段階から熱延上がりまでの諸条件や、熱延上がり後、室温近くの温度(100℃以下の温度)に冷却されるまでの間の条件などを厳密に規定する。具体的には、次の(1)〜(6)の条件が必要である。
【0043】
(1)熱間圧延開始温度を350〜590℃の範囲内とする
(2)板厚50mmから上がり板厚までの熱間圧延中において、材料温度を280〜450℃の範囲内に制御するとともに、各パスの歪み速度を2.0〜350/秒に制御し、かつ各パス間での滞留時間を10分以内に制御する
(3)板厚50mmから上がり板厚までの熱間圧延中において圧延ロールと板との接触部分の平均温度を350℃以下に保持する
(4)熱間圧延上がりの材料温度を280〜350℃の範囲内とする
(5)熱間圧延上がり板厚を1.5〜2.8mmの範囲とする
(6)熱間圧延上がりの280〜350℃の範囲内の温度から100℃以下の温度までの平均冷却速度を100℃/時間以下に制御する
【0044】
なおこの発明の方法は、熱間圧延の仕上げ圧延機としてリバーシング・ミルおよびリバーシング・ウォームミルを用いる場合、あるいは熱間圧延の粗圧延および仕上げ圧延兼用の圧延機としてリバーシング・ミルを用いる場合を想定しており、上記の(1)〜(6)の条件も、少なくとも仕上げ圧延にリバース方式の圧延機を用いた場合に有効な条件として規定している。そしてまた上記の各条件中、「板厚50mmから上がり板厚までの熱間圧延中」とは、リバース方式による仕上げ圧延中に含まれる。
【0045】
上記(1)〜(6)の熱間圧延条件について次に詳細に説明する。
【0046】
(1)熱間圧延開始温度を350〜590℃の範囲内とする:
熱間圧延開始温度は、熱間圧延中の材料の回復、再結晶挙動に強い影響を及ぼす。熱間圧延開始温度が350℃未満では、圧延中に再結晶が起こりにくく、材料の延性が低下し、圧延中に板のエッジ割れ現象が生じやすい。一方590℃を越えた温度で熱間圧延を開始すれば、粗大な結晶粒が形成されやすく、板の表面品質が低下する。そこで熱間圧延開始温度は350〜590℃の範囲内とした。
【0047】
(2)板厚50mmから上がり板厚までの熱間圧延中において、材料温度を280〜450℃の範囲内に制御するとともに、各パスの歪み速度を2.0〜350/秒に制御し、かつ各パス間での滞留時間を10分以内に制御する:
熱間圧延中における板厚50mmの段階から仕上げ板厚までの熱間圧延諸条件は、再結晶挙動、適切な集合組織の形成に大きな影響を与える。この段階での材料温度、各パス歪み速度、各パス間滞留時間を上述のように定めて組合せることにより、熱間圧延板の再結晶挙動を調整し、板の集合組織を熱間圧延の段階から制御することによって、最終板での集合組織が前記(1)式を満足させることが可能となる。この段階で材料温度が280℃未満となれば、表面品質の低下と熱間圧延中の深刻なエッジ割れを招くおそれがあり、一方この段階の材料温度が450℃を越えれば、再結晶の進行が早まって、所要の集合組織が得られなくなる。またこの段階での各パスの歪み速度が2.0/秒未満では、生産性の低下を招き、一方350/秒を越えれば、エッジ割れや板表面品質の低下を招き、圧延負荷の過大化を招くおそれがある。さらに材料のパス間滞留時間が10分以上では、滞留中に回復と再結晶が進行し、所要の集合組織が得られなくなるおそれがあり、また生産性の低下をも招く。したがってこれらの条件を前述のように定めた。
【0048】
(3)板厚50mmから上がり板厚までの熱間圧延中において圧延ロールと板との接触部分の平均温度(ロール表面平均温度)を350℃以下に保持する:
板の集合組織、特に表層の集合組織の形成には、圧延ロール表面の状態、特にその温度が大きな影響を与える。50mmを越える厚板の段階ではその影響は小さいが、板厚50mmから上がり板厚までの間では、圧延ロール表面温度が板表層の集合組織形成に大きな影響を与える。ここで、熱間圧延においては、圧延板と圧延ロールの接触により圧延ロールの表面温度が室温より高くなるが、その圧延ロールと圧延板との接触部分の温度が350℃を越えれば、板の表層に適切な集合組織が得られなくなり、また板の表面品質の低下を招くおそれがある。そこでこの発明では、板厚50mmから仕上げ板厚までの間における圧延ロールと板との接触部分の平均温度を350℃以下に保持することとした。
【0049】
(4)熱間圧延上がりの材料温度を280〜350℃の範囲内とする:
熱間圧延の終了温度が280℃未満では、充分な再結晶が得られ難く、これをそのまま焼鈍せずに最終板厚まで冷間圧延した場合はDI缶の耳が高くなり、成形性の劣化を招く。一方熱間圧延終了温度が350℃を越える場合、材料は完全に再結晶するが、表面品質が低下してしまうおそれがある。そこで熱間圧延の終了温度は280〜350℃の範囲内とした。なおこの範囲内でも特に290〜340℃が好ましい。
【0050】
(5)熱間圧延上がり板厚を1.5〜2.8mmの範囲とする:
熱間圧延上がり板厚が1.5mm未満では、熱間圧延機での板厚精度の制御が困難となる。一方熱間圧延上がり板厚が2.8mmを越えれば、その後の冷間圧延率が高くなり過ぎて、高強度は容易に得られるが、耳率が大きくなってしまう。そこで熱間圧延上がり板厚は1.5〜2.8mmの範囲内とした。
【0051】
(6)熱間圧延上がりの280〜350℃の範囲内の温度から100℃以下の温度までの平均冷却速度を100℃/時間以下に制御する:
熱間圧延上がり材(コイル)の290〜350℃の範囲内の温度から100℃以下の温度までの冷却過程は、再結晶の進行過程であり、またCube方位結晶粒が成長する過程でもある。この過程での冷却速度が100℃/時間を越えれば、再結晶が充分に進行できず、Cube方位結晶粒の生成が不充分となる。その結果最終板の耳率を充分に低くすることができず、また成形性も低下するおそれがある。そこで熱間圧延上がりの280〜350℃の範囲内の温度から100℃以下の温度までの冷却過程の平均冷却速度を100℃/時間以下とした。
【0052】
以上のような(1)〜(6)の条件に従って、熱間圧延してコイルに巻上げ、さらに100℃以下の温度まで冷却した熱延板は、自己焼鈍により90%以上の再結晶率を達成することができ、このようなほぼ完全再結晶状態の組織の熱間圧延板に対しては、その後に改めて再結晶のための中間焼鈍を施すことなく、低コストで高品質の最終板に仕上げることができる。
【0053】
さらに、熱間圧延板の特性としては、耐力が120MPa以上で、しかも集合組織条件として、板表面から板厚方向に板厚の1/4の深さの部位におけるCube方位の方位密度がランダム方位の5〜140倍の範囲内で、かつ圧延集合組織に属するCu方位、S方位、Bs方位の各方位密度がそれぞれランダム方位の10倍以下となるように制御されているものとする。ここで、熱間圧延板における耐力が120MPaを越えている場合は、最終板において強度が高くなり過ぎ、しごき性の低下を招くおそれがある。また熱間圧延板における板厚1/4に相当する部位のCube方位の密度がランダム方位密度の5倍未満では、最終板に45°耳が高くなりやすく、一方140倍を越えれば、最終板に0−90°耳が高くなりやすい。さらに熱間圧延板における圧延集合組織に属するCu、S、Bs成分の方位密度がそれぞれランダム方位の10倍を越える場合は、最終板において45°耳が高くなりやすく、またしごき性の低下を招くおそれがある。
【0054】
熱間圧延板に対しては、その後に改めて再結晶のための中間焼鈍を施すことなく、最終板厚まで冷間圧延を行なう。ここで、冷間圧延率は65%以上とする必要がある。すなわち、中間焼鈍を施さずに最終冷間圧延率を65%未満にするためには、最終製品の板厚(通常0.35〜0.25mm)を考慮すれば、熱延上がり板を1mm未満にする必要があるが、そのようなことは実操業上極めて困難であるばかりでなく、材料の冷間加工硬化による強化が少なくなり、充分な材料強度が得られなくなるおそれがあり、さらには耳率の制御にも不利となる。したがって冷間圧延率は65%以上とした。
【0055】
以上のようにして得られた最終板(冷間圧延板)は、これをそのままDI缶胴に用いても良いが、最終板の延性の回復による成形性の向上を図るため、必要に応じて冷間圧延後の板に対し、80〜200℃の温度範囲で0.1〜24時間保持の条件で最終焼鈍(仕上げ焼鈍)を行なっても良い。この最終焼鈍の温度が80℃未満では、成形性の向上効果が不十分であり、一方200℃を越えれば、軟化による強度低下が大きくなる。また最終焼鈍の保持時間が0.1時間未満では成形性の向上効果が不十分となり、一方24時間を越えれば、成形性向上の効果が飽和し、コスト面で問題が生じる。なお、冷間圧延を高速で行なった場合に生じる加工熱を利用しても、上記の最終焼鈍と同様な焼鈍効果を得ることが可能である。
【0056】
【実施例】
表1に示す合金記号A〜Gの各合金について、常法に従ってDC鋳造法により鋳造した。得られた鋳塊に対し、均質化処理を施し、熱間圧延を行なってコイルに巻取り、100℃以下に冷却し、さらに冷間圧延を行なって最終板厚とし、一部のものについて最終焼鈍を行ない、最終板(製品板)とした。これらのプロセスの具体的な条件について、表2、表3の製造番号1〜12に示す。なお熱間圧延においては、仕上圧延機としてリバーシング・ミルを用いて、板厚50mm以下の段階での圧延はすべてリバーシング・ミルによるものとした。
【0057】
ここで、熱間圧延終了後100℃以下の温度まで冷却した段階で、その熱間圧延板について、強度(圧延方向の引張強さおよび耐力)を調べるとともに、その集合組織として、板表面から板厚方向に板厚の1/4の深さの位置のCube方位密度、Cu方位密度、S方位密度、Bs方位密度を測定したので、その結果を表3中に示す。
【0058】
また最終板について、板表層および板表面から板厚の1/4の部位のCube方位密度C、C1/4と、同じく板表層および板表面から板厚の1/4の部位におけるβファイバに属するCu方位密度、S方位密度、Bs方位密度を調べ、板表層のCube方位密度Cと、板表面から板厚の1/4の部位のCube方位密度C1/4との和の値(C+C1/4)を求め、同時に板表層のCu方位、S方位、Bs方位の各方位密度の合計dと、板表面から板厚の1/4の部位のCu方位、S方位、Bs方位の各方位密度の合計d1/4との和の値(d+d1/4)を求めたので、その結果を表4中に示す。
【0059】
なおここで上述のような各方位密度の測定、すなわち集合組織の測定は、次のようにして行なった。
【0060】
すなわち、板厚表層の集合組織を求めるにあたっては、圧延板そのままで、エッチングなしで測定サンプルとした。一方板厚の1/4に相当する部位の集合組織を求めるにあたっては、NaOH水溶液で表面から板厚の1/4に相当する部位までエッチングして測定サンプルとした。そしてX線回折装置を用い、Schulz反射法により、{200}、{220}、{111}の不完全極点図を測定し、これらをもとに三次元結晶方位解析(ODF)を行なった。なおCu方位は{112}<111>方位、S方位は{123}<634>方位、Bs方位は{110}<112>方位、Cube方位は{001}<100>方位がそれぞれ理想方位であるが、これら理想方位を中心に方位差15°のものもそれぞれの方位の結晶として算定した。
【0061】
さらに、前述のようにして得られた各最終板については、導電率(%IACS)と、Mn固溶量も調べたので、その結果を表4中に併せて示す。ここで導電率は、渦電流式導電率測定装置を用いて、銅、黄銅を基準試料として測定を行なった。
【0062】
前述のようにして得られた最終板(缶胴用の薄板)について、圧延方向と平行に採取した引張試験片を用いて元板の引張強度(TS)、耐力(YS)、伸び(EL)を測定し、また塗装焼付(ベーク)を想定した200℃×20分の熱処理を行なった後の引張強度(TS)、耐力(YS)、伸び(EL)を測定した。さらに元板の耳率を調べるとともに、しごき性の指標として「DI缶苛酷しごきの成功率」を調べるとともに、フランジ成形性(口拡げ性)の指標として口拡げ率を調べた。これらの結果を表4、表5に示す。
【0063】
ここで、耳率は、ポンチ径32mm、ブランク径56mmの条件でカップ深絞り試験を行なって調べた。またしごき性の指標としての「DI苛酷しごきの成功率」は、DI缶成形において第2のダイスを抜き、第1と第3のダイスのしごき率を55%としたときに、連続100缶の製缶で缶切れが発生しない缶の比率を調べた。さらにフランジ成形性(口拡げ性)の指標としての口拡げ率は、4段ネッキング後のDI缶について、トリミング、洗浄、ベークを行ない、そのDI缶の上部開口部分に、15°の勾配を有するポンチを、材料に割れが生じるまで押し込む試験を行ない、割れが生じるまでの口拡げ率を以下の式で求めた。
口拡げ率=[R1−R0]×100%
但し、R0:4段ネッキング後のDI缶開口部の半径(29mm)
R1:割れが生じる限界まで口拡げしたときの開口部の半径
【0064】
【表1】

Figure 2004263253
【0065】
【表2】
Figure 2004263253
【0066】
【表3】
Figure 2004263253
【0067】
【表4】
Figure 2004263253
【0068】
【表5】
Figure 2004263253
【0069】
表2〜表5において、製造番号1〜5は、いずれもこの発明で規定する成分組成範囲内の合金を用いて、この発明で規定する製造方法に従って製造した例である。これらの例では、表4、表5に示す通り、耳率が低く、ベーク後の強度も充分に高く、しかもしごき性とフランジ成形性にも優れた材料を得ることができた。
【0070】
これに対し製造番号6は、合金成分はこの発明で規定する範囲内であるが、製造方法がこの発明で規定する範囲から外れたものである。すなわち熱間圧延における板厚50mm以降における最高温度が472℃と高く、この発明で規定する280〜450℃の範囲を外れ、また熱間圧延の上がり温度が256℃と低く、この発明で規定する280〜350℃の範囲を外れ、さらに熱間圧延上がり板の耐力が144MPaと高く、この発明で規定する120MPa以下の範囲を外れ、そしてまた熱間圧延板の集合組織と最終板の集合組織も、この発明で規定する範囲を外れたものであって、DI缶胴用の板として45°耳率が高く、苛酷しごきの成功率が低く、口拡げ率も劣った。
【0071】
また製造番号7は合金成分がこの発明で規定する範囲から外れたものであり、ベーク後の強度が不足し(注:DI缶の耐圧性などの点から、材料の耐力は240MPa以上が必要)、またしごき性とフランジ成形性も劣っていた。
【0072】
さらに製造番号8から製造番号10までの場合は、均質化処理あるいは熱間圧延の条件がこの発明で規定する範囲を外れたため、熱間圧延中途からエッジ割れにより熱間圧延の続行が困難となってしまった。
【0073】
また製造番号11の場合は、熱間圧延ロールの表面温度がこの発明で規定する範囲の上限を越えてしまったため、45°耳率が高く、またDI缶のしごき性も劣ってしまった。
【0074】
そしてまた製造番号12の場合は、均質化処理条件がこの発明で規定する範囲を外れたため、0°、90°耳率が高く、またDI缶のしごき性も劣ってしまった。
【0075】
【発明の効果】
前述の実施例からも明らかなように、この発明によれば、DI缶胴用硬質板としてバランスの優れた板、すなわち塗装焼付後の強度として高強度を有すると同時に低耳率で、しかもしごき性およびフランジ成形性のいずれもが優れた板を得ることができる。そしてまた、製造方法として、熱間圧延後や冷間圧延中途における中間焼鈍を省略したプロセスで上述のような優れた材料を得ることができるところから、低コストで高品質の材料を得ることができる。[0001]
TECHNICAL FIELD OF THE INVENTION
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a hard plate made of an Al-Mg-Mn-based aluminum alloy used for a can body for a two-piece aluminum can by DI molding (drawing and ironing), and a method for producing the same, in particular, having a low deep drawing ear and coating. Aluminum alloy hard plate for DI can body with high strength after baking and excellent formability during DI processing, such as ironing workability, as well as formability after paint baking, such as flange formability, and its production It is about the method.
[0002]
[Prior art]
Generally, as a manufacturing process of a two-piece aluminum can (DI can), the material for the can body is subjected to DI forming by deep drawing and ironing to form a can body, and then trimmed to a predetermined size and shape. Degrease and wash, paint and print, bake (baking), then neck and flange the can body edge, and seam together with the separately formed can lid Is usually performed.
[0003]
As a material for the DI can body thus manufactured, a hard plate of JIS3004 alloy made of an Al-Mg-Mn alloy has been widely used. This 3004 alloy is excellent in ironing workability and shows relatively good formability even when cold-rolled at a high rolling ratio in order to increase strength, so that it is suitable as a DI can body material. Have been.
[0004]
In addition, as a method for manufacturing such a hard plate for a DI can body made of 3004 alloy, generally, after casting by a DC casting method or the like, a homogenization treatment is applied to the ingot, and a predetermined ingot is further subjected to hot rolling and cold rolling. In general, a method of reducing the sheet thickness and performing intermediate annealing for recrystallization during cold rolling after hot rolling before cold rolling or in the middle of cold rolling.
[0005]
By the way, it is strongly desired to reduce the thickness of a two-piece aluminum can body (DI can), mainly from the viewpoint of material cost reduction. When the thickness is reduced in this way, it is indispensable to increase the strength of the material in order to avoid a problem such as a decrease in the buckling strength of the can caused by the reduction in the thickness.
[0006]
Further, it is desired that the material for the DI can have a small ear ratio at the time of DI molding. That is, a low ear ratio during the DI molding is important from the viewpoint of improving the yield during the DI molding and preventing the can body from being broken due to the cut end of the can body.
[0007]
Further, it is necessary that the moldability of the DI can be excellent at the time of manufacturing the DI can (opening property) and that the ironing property (can-cut resistance) is excellent.
[0008]
Here, any one of these strength, ear ratio, flange formability (mouth expansion property), and ironing property (can-break resistance) is not a matter that any one of them is excellent. It is important that the production method be low, in addition to the above-mentioned requirements from the material characteristics, as well as the production method.
[0009]
By the way, in the conventional method for manufacturing a hard plate for a 3004 alloy can body, intermediate annealing is performed for recrystallization before cold rolling after hot rolling or in the middle of cold rolling as described above. Is usually the case. If the conventional main manufacturing processes are classified from the viewpoint of such intermediate annealing, they can be classified into the following processes (a) to (c).
(A) Hot rolling-batch annealing process
In this method, after normal hot rolling, annealing is performed using a box-type annealing furnace (batch annealing furnace; BAF) having a low heating rate.
(B) Hot rolling-continuous annealing process
In this method, after normal hot rolling, annealing is performed using a continuous annealing furnace (CAL) having a high heating rate.
(C) Cold rolling intermediate continuous annealing process
This is a method of annealing using a continuous annealing furnace with a high heating rate in the middle of cold rolling after ordinary hot rolling.
[0010]
Further, in addition to the above processes (a) to (c), there is also a method as shown in the following (d).
(D) Self-recrystallization process
This is a method in which a material is self-recrystallized (self-annealed) in a hot-rolled state by controlling the rising temperature of hot rolling to be equal to or higher than the recrystallization temperature of the material.
[0011]
When the processes (a), (b) and (d) are applied among the processes (a) to (d) as described above, the ironability of the finally obtained can body is inferior. There is a common problem. Further, when the process (d) is applied, there is a problem that the material strength of the obtained can body is insufficient. Furthermore, when the process (c) is applied, there is a problem that although the ironability is excellent as a can body material, the flange formability is inferior. Further, in the processes (a), (b), and (c) that require annealing for recrystallization after hot rolling, there is a problem that manufacturing costs are relatively high.
[0012]
Here, as a prior art method already proposed as a method for manufacturing a DI can body made of an Al-Mg-Mn-based alloy, for example, there are methods as shown in Patent Documents 1 to 8; Among them, the methods of Patent Documents 1 to 6 require annealing after hot rolling or in the middle of cold rolling, and have a problem in terms of cost as described above.
[0013]
Patent Literature 7 also discloses a method of performing final cold rolling without annealing after hot rolling. However, Patent Literature 7 uses a tandem rolling mill as a hot rolling mill. And a method using a reverse rolling mill (reversing mill, reversing worm mill) is not disclosed. Usually, the optimal hot rolling process conditions are different between the tandem rolling mill and the reverse rolling mill. Therefore, even if the method disclosed in Patent Document 7 is diverted to the case where the reverse rolling mill is used, In fact, it is not always the case that a can body material excellent in the above-mentioned various properties can be obtained immediately.
[0014]
Further, in the method of Patent Document 8, annealing after hot rolling may be omitted, but the method of Patent Document 8 also uses a tandem-type rolling mill as a hot rolling mill. Also, the hot rolling conditions are not strictly defined, and therefore, even if the method of Patent Document 8 is diverted to use a reverse type rolling mill, a DI can body material excellent in the balance of the above-mentioned properties can be obtained. There was no.
[0015]
[Patent Document 1] JP-A-11-256290
[Patent Document 2] JP-A-11-256291
[Patent Document 3] JP-A-11-256292
[Patent Document 4] JP-A-2000-234158
[Patent Document 5] JP-A-2001-40461
[Patent Document 6] JP-A-2002-212691
[Patent Document 7] JP-A-10-310837
[Patent Document 8] JP-A-11-140576
[0016]
[Problems to be solved by the invention]
The present invention has been made in view of the above circumstances, and is a material capable of satisfying various characteristics desired as a DI can body material in a well-balanced manner, that is, having high strength, low ear rate, and flange formability, ironing property. In addition to providing an aluminum alloy plate for a DI can body that is excellent in the balance of these various properties and has a good balance of these properties, a hard plate for a high quality DI can body with an excellent balance of such properties is provided. It is an object of the present invention to provide a method of obtaining a high-quality DI can body as described above using a reverse type rolling mill instead of a tandem rolling mill as a hot rolling mill. The purpose is to provide a method suitable for obtaining at low cost.
[0017]
[Means for Solving the Problems]
As a result of various experiments and studies conducted by the present inventors to solve the above-described problems, the texture of the plate, particularly the texture of the portion close to the plate surface, is appropriately controlled, and at the same time, the Mn solid solution amount and the conductivity are adjusted. It has been found that by properly adjusting the balance between the flange formability and the ironability while securing high strength and a low ear ratio, a high-quality DI can body can be obtained. In addition, as a manufacturing method, by strictly controlling the hot rolling conditions, particularly the conditions in the stage after hot rolling from the stage of the plate thickness of 50 mm, annealing for recrystallization after hot rolling is omitted. The present inventors have found that a process capable of obtaining a high-quality DI can body, particularly a process capable of obtaining a high-quality DI can body using a reversing mill type hot rolling mill, can be realized. I've reached the point.
[0018]
More specifically, the aluminum alloy hard plate for a can body according to the first aspect of the present invention includes: Mg 0.5 to 2.0%, Mn 0.5 to 2.0%, Fe 0.1 to 0.7%, Si 0.05 0.50.5%, Cu 0.05〜0.5%, the balance being an aluminum alloy consisting of Al and unavoidable impurities, and each of Cu, S, and Bs directions belonging to β fiber of the plate surface layer. D is the sum of the azimuth densities 0 And the sum of the azimuth densities of the Cu, S, and Bs directions belonging to the β fiber at a position at a depth of 1/4 of the plate thickness in the plate thickness direction from the plate surface is d 1/4 And the cubic density of the Cube azimuth in the plate surface layer is C 0 And the azimuth density of the Cube azimuth at a position at a depth of 1/4 of the plate thickness in the plate thickness direction from the plate surface is C 1/4 And the following equation
(D 0 + D 1/4 )> (C 0 + C 1/4 )
And the Mn solid solution amount is in the range of 0.05 to 0.35% and the conductivity is in the range of 34 to 45 IACS%.
[0019]
The aluminum alloy hard plate for a can body according to the second aspect of the present invention is the aluminum alloy hard plate for a can body according to the first aspect, further comprising, as a component of the aluminum alloy, 0.05 to 0.3% of Cr and 0.05 to 0.3% of Zn. It is characterized by containing one or more of 0.5% and 0.005 to 0.20% of Ti.
[0020]
Further, the method for producing an aluminum alloy hard plate for a can body of the invention according to claim 3 is characterized in that after casting an aluminum alloy having a component composition defined in claim 1 or 2, the aluminum alloy is hardened at a temperature in the range of 520 to 630 ° C. Performing a homogenization treatment for 1 hour or more, then performing hot rolling and winding, and cooling to a temperature of 100 ° C. or less,
(1) The hot rolling start temperature is in the range of 350 to 590 ° C,
(2) During hot rolling from a plate thickness of 50 mm to a rising plate thickness, the material temperature is controlled within a range of 280 to 450 ° C., and the strain rate of each pass is set within a range of 2.0 to 350 / sec. Control and control the residence time between each pass within 10 minutes,
(3) During hot rolling from a plate thickness of 50 mm to a rising plate thickness, the average temperature of the contact portion between the rolling roll and the plate is maintained at 350 ° C. or less,
(4) The material temperature after hot rolling is set to a range of 280 to 350 ° C,
(5) The hot-rolled sheet thickness is in the range of 1.5 to 2.8 mm,
(6) controlling the average cooling rate from a temperature in the range of 280 to 350 ° C. after hot rolling to 100 ° C. or less to 100 ° C./hour or less,
According to the above (1) to (6), the proof strength is 120 MPa or less, and the azimuth density of the Cube orientation in a portion having a depth of 1/4 of the thickness in the thickness direction from the surface of the plate is 5 to 140 times the random orientation. And a hot-rolled sheet in which each of the Cu, S, and Bs orientations belonging to the rolling texture is 10 times or less the random orientation, and 65% or more without intermediate annealing Cold rolling at a rolling rate of
[0021]
Furthermore, the method for producing an aluminum alloy hard plate for a can body according to the invention of claim 4 is the method for producing an aluminum alloy hard plate for a can body according to claim 3, further comprising: The final annealing is carried out by heating to a temperature within the range described above and holding for 0.1 to 24 hours.
[0022]
BEST MODE FOR CARRYING OUT THE INVENTION
First, the reasons for limiting the component composition of the aluminum alloy used for the aluminum alloy hard plate for a can body of the present invention will be described.
[0023]
Mg:
The addition of Mg is effective in improving the strength due to solid solution of Mg itself, and can be expected to improve the strength by increasing the amount of work hardening accompanying the solid solution of Mg. 2 It can be expected that the strength will be improved by aging precipitation of Si. Therefore, Mg is an indispensable element for obtaining the strength required for the body of the can. Also, Mg has an effect of increasing dislocations during processing, and is therefore effective for making recrystallized grains finer. However, when the Mg content is less than 0.5%, the above-mentioned effect is small. On the other hand, when the Mg content is more than 2.0%, although high strength is easily obtained, deformation resistance at the time of DI processing is increased and drawability and ironability are reduced. Make it worse. Therefore, the amount of Mg was set in the range of 0.5 to 2.0%.
[0024]
Mn:
Mn is an effective element that contributes to improvement in strength and formability. In particular, in the can body material, which is the intended use of the present invention, ironing is added during DI molding, and therefore Mn is particularly important. Emulsion type lubricants are usually used for ironing aluminum plates, but when the amount of Mn-based crystals is small, lubricating ability is insufficient with only emulsion type lubricants even if they have the same strength. However, there is a possibility that poor appearance such as abrasion and seizure called "goling" may occur. It is known that galling is affected by the size, amount, and type of a crystallized substance, and Mn is an essential element for forming the crystallized substance. If the Mn content is less than 0.5%, the solid lubricating effect of the Mn-based compound cannot be obtained, while if the Mn content exceeds 2.0%, Al 6 A primary crystal giant intermetallic compound of Mn is generated, which significantly impairs formability. Therefore, the Mn content is set in the range of 0.5 to 2.0%. Further, here, the solute Mn in the product plate has an effect of suppressing recovery during processing and an effect of reducing softening during baking, so that in the present invention, as will be described later, the total Mn amount in the material In addition, it defines the amount of Mn solid solution in the product plate.
[0025]
Fe:
Fe is an element that promotes crystallization and precipitation of Mn, and controls the amount of Mn solid solution in the aluminum matrix and the dispersion state of the Mn-based intermetallic compound. In order to obtain an appropriate compound dispersion state, it is necessary to add Fe according to the amount of Mn added. If the Fe content is less than 0.1%, it is difficult to obtain an appropriate compound dispersion state, while if the Fe content exceeds 0.7%, a primary intermetallic compound is likely to be generated with the addition of Mn. And the moldability is significantly impaired. Therefore, the range of the Fe amount is set to 0.1 to 0.7%.
[0026]
Si:
The addition of Si 2 It contributes to the improvement of the strength of the can body through age hardening due to the precipitation of the Si-based compound. Si is an element necessary for generating an Al-Mn-Fe-Si-based intermetallic compound and controlling the dispersion state of the Mn-based intermetallic compound. If the Si content is less than 0.05%, the above effects cannot be obtained, while if it exceeds 0.5%, the material becomes too hard due to age hardening, and the formability is impaired. Therefore, the range of the amount of Si is set to 0.05 to 0.5%.
[0027]
Cu:
Cu is dissolved in an aluminum matrix, and contributes to an improvement in strength utilizing precipitation hardening due to precipitation as an Al-Cu-Mg-based precipitate during coating baking. When the Cu content is less than 0.05%, the effect cannot be obtained. On the other hand, when Cu is added in excess of 0.5%, although age hardening is easily obtained, it becomes too hard and impairs formability. Also, the corrosion resistance deteriorates. Therefore, the range of the amount of Cu is set to 0.05 to 0.5%.
[0028]
In addition to the above elements, Al and unavoidable impurities may be basically used, but one or more of Ti, Cr, and Zn may be added as necessary. These Ti, Cr and Zn will be described in more detail.
[0029]
Ti:
In ordinary aluminum alloys, a small amount of Ti is added to refine the ingot crystal grains. In the present invention, a small amount of Ti may be added as needed. However, if the Ti content is less than 0.005%, the effect cannot be obtained. On the other hand, if the Ti content exceeds 0.20%, a giant Al-Ti-based intermetallic compound is crystallized to inhibit formability. Was made in the range of 0.005 to 0.20%. It is known that the effect of refinement of ingot crystal grains can be improved by adding a small amount of B together with Ti. Therefore, in the case of the present invention, addition of a small amount of B together with Ti is permitted. When B is added together with Ti, the effect is not obtained if the B content is less than 0.0001%, and if the B content exceeds 0.05%, Ti-B-based coarse particles are mixed to impair the formability. Therefore, when B is added together with Ti, the amount of B is desirably in the range of 0.0001 to 0.05%.
[0030]
Cr:
Cr is an element effective for improving the strength. However, if it is less than 0.05%, its effect is small, and if it exceeds 0.3%, the formability is reduced due to the formation of giant crystals, which is not preferable. Therefore, the range of the Cr content when Cr is added is set to 0.05 to 0.3%.
[0031]
Zn:
Addition of Zn contributes to the improvement in strength due to aging precipitation of Al-Mg-Zn-based particles. However, if the content is less than 0.05%, the effect cannot be obtained. If it exceeds 0.5%, the contribution to the strength is problematic. No, but deteriorates corrosion resistance. Therefore, the range of the amount of Zr when adding Zn is set to 0.05 to 0.5%.
[0032]
Further, in the aluminum alloy hard plate for a can body of the present invention, it is necessary to not only adjust the component composition of the alloy as described above, but also to appropriately adjust the amount of solid solution elements in the product plate. In the present invention, the amount of solid solution of typical Mn among the solid solution elements is determined, and the conductivity is determined as an index of the total amount of solid solution including other solid solution elements.
[0033]
In other words, solid-solution elements are effective in suppressing recovery and suppressing softening during paint baking.In order to obtain appropriate strength after paint baking, not only the amount of each element added but also the solid solution It is necessary to control the amount appropriately. In the present invention, the Mn solid solution having the greatest effect is set in the range of 0.05 to 0.35%, and the solid solution of Mg, Cu, Si, and Fe other than Mn, By setting the conductivity of the plate as an index within the range of 34 to 45 IACS%, it was possible to obtain the necessary high strength after baking without painting, without impairing the ironing property and the flange formability.
[0034]
Here, if the Mn solid solution amount is less than 0.05%, it becomes difficult to obtain the required strength, while if it exceeds 0.35%, the ironing property and the flange formability deteriorate. Therefore, the Mn solid solution amount is set in the range of 0.05 to 0.35%.
[0035]
If the conductivity of the plate, which is an index of the total solid solution amount of Mg, Cu, Si, Fe, etc. in addition to Mn, is less than 34 IACS%, the total solid solution amount is too large and ironing property and flange formability are poor. On the other hand, if the electrical conductivity exceeds 45 IACS%, the total amount of solid solution may be too small and the strength may be insufficient. Therefore, the electrical conductivity of the plate is set in the range of 34 to 45 IACS%.
[0036]
In addition, in the aluminum alloy hard plate for a can body according to the present invention, it is necessary to appropriately control the texture of the surface of the plate or a portion close to the surface (a portion of the plate surface layer and a portion 板 of the plate thickness). It is important to improve the ironability without adversely affecting the iron.
[0037]
That is, according to the detailed experiments by the inventors of the present application, d 0 , D 1/4 , C 0 , C 1/4 , Respectively
d 0 : Total of each orientation density of Cu orientation, S orientation, and Bs orientation belonging to β fiber in plate surface layer
d 1/4 : The sum of the azimuth densities of the Cu, S, and Bs orientations belonging to the β fiber at a depth of 1/4 of the plate thickness in the plate thickness direction from the plate surface
C 0 : Orientation density of Cube orientation in plate surface layer
C 1/4 : Azimuth density of Cube orientation at a depth of 1/4 of the plate thickness in the plate thickness direction from the plate surface
If it is specified, the following equation (1)
(D 0 + D 1/4 )> (C 0 + C 1/4 …… (1)
By adjusting the texture of the plate so as to satisfy the above, it has been found that the ironing property can be remarkably improved as compared with the related art, and the formula (1) is defined in the present invention. If the formula (1) is not satisfied, the effect of improving the ironing property cannot be obtained sufficiently.
[0038]
For each azimuth density, an incomplete pole figure of {200}, {220}, and {111} was measured by the Schulz reflection method using an X-ray diffractometer, and a three-dimensional crystal orientation analysis (ODF) was performed based on these. ). Here, the Cu orientation is ideally the {111} <112> orientation, the S orientation is the {123} <634> orientation, the Bs orientation is the {110} <112> orientation, and the Cube orientation is the {001} <100> orientation. It is assumed that the azimuth includes those having an azimuth difference of 15 ° around the ideal azimuth.
[0039]
In addition, d 0 , C 0 Is defined as the surface layer of the plate, which means the azimuth density measured on the surface of the plate.
[0040]
Next, the manufacturing process of the aluminum alloy hard plate for a can body of the present invention will be described.
[0041]
First, an aluminum alloy ingot having the above-described alloy composition is cast by a DC casting method (semi-continuous casting method) according to a conventional method. Next, the ingot is subjected to a homogenization treatment to homogenize segregation of the ingot and optimize the size and distribution of the Mn, Fe, and Si-based second phase particles. Also, the size and distribution of such second phase particles may affect the texture of the final sheet. If the homogenization treatment temperature is lower than 520 ° C., not only the homogenization effect is insufficient, but also an optimum texture may not be obtained, while if it exceeds 630 ° C., eutectic melting may occur. If the time for the homogenization treatment is less than 1 hour, not only the effect of homogenization will be insufficient, but also an optimum texture may not be obtained. Therefore, the homogenization treatment condition was defined as a temperature within the range of 520 to 630 ° C. for 1 hour or more. The upper limit of the homogenization treatment time is not particularly limited, but is preferably 48 hours or less in view of economy.
[0042]
Hot rolling is performed on the ingot subjected to the homogenization treatment. In the case of the method of the present invention, since a method in which annealing is not performed after hot rolling is applied, it is necessary to recrystallize at a recrystallization rate of 90% or more in a hot-rolled finished plate as described later. In addition, the recrystallization behavior during hot rolling has a great influence on reduction of ear rate and improvement of ironability through texture control. Therefore, in the present invention, not only the hot rolling start temperature and the hot rolling end temperature (hot rolling temperature), but also various conditions from the stage of the thickness of 50 mm to the hot rolling during the hot rolling, and the conditions after the hot rolling. Strictly stipulate the conditions until cooling to a temperature close to room temperature (a temperature of 100 ° C. or less). Specifically, the following conditions (1) to (6) are required.
[0043]
(1) The hot rolling start temperature is in the range of 350 to 590 ° C.
(2) During hot rolling from a plate thickness of 50 mm to a rising plate thickness, the material temperature is controlled within a range of 280 to 450 ° C., and the strain rate of each pass is controlled at 2.0 to 350 / sec. And control the residence time between passes within 10 minutes
(3) During hot rolling from a plate thickness of 50 mm to a rising plate thickness, the average temperature of the contact portion between the rolling roll and the plate is maintained at 350 ° C. or less.
(4) The material temperature after hot rolling is in the range of 280 to 350 ° C.
(5) The hot-rolled finished sheet thickness is in the range of 1.5 to 2.8 mm.
(6) The average cooling rate from the temperature in the range of 280 to 350 ° C after hot rolling to a temperature of 100 ° C or less is controlled to 100 ° C / hour or less.
[0044]
The method of the present invention uses a reversing mill and a reversing worm mill as a finishing mill for hot rolling, or uses a reversing mill as a rolling mill for both rough rolling and finishing rolling of hot rolling. A case is assumed, and the above-mentioned conditions (1) to (6) are also defined as effective conditions at least when a reverse type rolling mill is used for finish rolling. In the above conditions, "during hot rolling from a plate thickness of 50 mm to an increased plate thickness" is included in the finish rolling by the reverse method.
[0045]
Next, the hot rolling conditions (1) to (6) will be described in detail.
[0046]
(1) The hot rolling start temperature is in the range of 350 to 590 ° C:
The hot rolling start temperature has a strong influence on the recovery and recrystallization behavior of the material during hot rolling. If the hot rolling start temperature is lower than 350 ° C., recrystallization is unlikely to occur during rolling, the ductility of the material is reduced, and the edge cracking of the sheet is likely to occur during rolling. On the other hand, if hot rolling is started at a temperature exceeding 590 ° C., coarse crystal grains are likely to be formed, and the surface quality of the sheet is reduced. Therefore, the hot rolling start temperature was set in the range of 350 to 590 ° C.
[0047]
(2) During hot rolling from a plate thickness of 50 mm to a rising plate thickness, the material temperature is controlled within a range of 280 to 450 ° C., and the strain rate of each pass is controlled at 2.0 to 350 / sec. And control the residence time between each pass within 10 minutes:
The hot rolling conditions from the stage of the plate thickness of 50 mm to the finished plate thickness during the hot rolling greatly affect the recrystallization behavior and the formation of an appropriate texture. At this stage, the material temperature, the strain rate of each pass, and the residence time between the passes are determined and combined as described above, thereby adjusting the recrystallization behavior of the hot-rolled sheet and changing the texture of the sheet to hot rolling. By controlling from the stage, the texture in the final plate can satisfy the above expression (1). If the material temperature is lower than 280 ° C. at this stage, the surface quality may be degraded and serious edge cracking may occur during hot rolling. On the other hand, if the material temperature at this stage exceeds 450 ° C., recrystallization proceeds. Prematurely, the required texture cannot be obtained. If the strain rate of each pass at this stage is less than 2.0 / sec, the productivity is reduced. On the other hand, if the strain rate is more than 350 / sec, the edge cracks and the surface quality of the sheet are deteriorated, and the rolling load becomes excessive. May be caused. Further, when the residence time between the passes of the material is 10 minutes or more, the recovery and recrystallization progress during the residence, and a required texture may not be obtained, and the productivity may be reduced. Therefore, these conditions were determined as described above.
[0048]
(3) During hot rolling from a plate thickness of 50 mm to a rising plate thickness, the average temperature (roll surface average temperature) of the contact portion between the rolling roll and the plate is maintained at 350 ° C. or less:
The formation of the texture of the sheet, particularly the texture of the surface layer, is greatly affected by the state of the surface of the rolling roll, particularly its temperature. The effect is small at the stage of a thick plate exceeding 50 mm, but in the range from the plate thickness of 50 mm to the rising plate thickness, the surface temperature of the rolling roll has a great influence on the texture formation of the surface layer of the plate. Here, in the hot rolling, the surface temperature of the rolling roll becomes higher than room temperature due to the contact between the rolling plate and the rolling roll, but if the temperature of the contact portion between the rolling roll and the rolling plate exceeds 350 ° C., An appropriate texture cannot be obtained on the surface layer, and the surface quality of the plate may be degraded. Therefore, in the present invention, the average temperature of the contact portion between the rolling roll and the plate between the plate thickness of 50 mm and the finished plate thickness is kept at 350 ° C. or less.
[0049]
(4) The material temperature after hot rolling is in the range of 280 to 350 ° C:
If the end temperature of hot rolling is lower than 280 ° C., it is difficult to obtain sufficient recrystallization, and if this is cold-rolled to the final thickness without annealing, the ears of the DI can become high and the formability deteriorates. Invite. On the other hand, when the hot rolling end temperature exceeds 350 ° C., the material is completely recrystallized, but the surface quality may be deteriorated. Therefore, the end temperature of the hot rolling is set in the range of 280 to 350 ° C. In addition, even in this range, 290 to 340 ° C. is particularly preferable.
[0050]
(5) The hot-rolled sheet thickness is in the range of 1.5 to 2.8 mm:
When the thickness after hot rolling is less than 1.5 mm, it is difficult to control the thickness accuracy in a hot rolling mill. On the other hand, if the thickness of the hot-rolled sheet exceeds 2.8 mm, the subsequent cold-rolling rate becomes too high, and high strength can be easily obtained, but the ear rate increases. Therefore, the thickness of the hot-rolled sheet was set in the range of 1.5 to 2.8 mm.
[0051]
(6) Controlling the average cooling rate from a temperature in the range of 280 to 350 ° C. after hot rolling to a temperature of 100 ° C. or less to 100 ° C./hour or less:
The cooling process of the hot-rolled material (coil) from a temperature in the range of 290 to 350 ° C. to a temperature of 100 ° C. or less is a progress of recrystallization and a process of growing Cube-oriented crystal grains. If the cooling rate in this process exceeds 100 ° C./hour, recrystallization cannot proceed sufficiently, and the generation of Cube-oriented crystal grains becomes insufficient. As a result, the ear ratio of the final plate cannot be sufficiently reduced, and the moldability may be reduced. Therefore, the average cooling rate in the cooling process from a temperature in the range of 280 to 350 ° C. after the hot rolling to a temperature of 100 ° C. or less was set to 100 ° C./hour or less.
[0052]
According to the above conditions (1) to (6), the hot-rolled sheet is hot-rolled and wound into a coil, and further cooled to a temperature of 100 ° C. or less, and achieves a recrystallization rate of 90% or more by self-annealing. It is possible to finish a low-cost, high-quality final plate on a hot-rolled plate having such a structure of a substantially completely recrystallized state without performing intermediate annealing for recrystallization again thereafter. be able to.
[0053]
Further, as the characteristics of the hot-rolled sheet, the proof strength is 120 MPa or more, and the texture condition is that the azimuth density of the Cube orientation at a depth of 1/4 of the sheet thickness in the sheet thickness direction from the sheet surface is random orientation. And the orientation density of each of the Cu orientation, S orientation, and Bs orientation belonging to the rolling texture is controlled to be 10 times or less the random orientation. Here, when the proof stress of the hot-rolled sheet exceeds 120 MPa, the strength of the final sheet becomes too high, which may cause a reduction in ironing property. If the density of the Cube orientation at a portion corresponding to a thickness of 1/4 in the hot-rolled sheet is less than 5 times the random orientation density, the final sheet tends to have a 45 ° ear, while if it exceeds 140 times, the final sheet has 0-90 ° ears tend to be high. Further, when the orientation density of the Cu, S, and Bs components belonging to the rolling texture in the hot-rolled sheet each exceeds 10 times the random orientation, the 45 ° ear tends to be high in the final sheet, and the ironing property is reduced. There is a risk.
[0054]
The hot-rolled sheet is then cold-rolled to the final sheet thickness without intermediate annealing for recrystallization. Here, the cold rolling reduction needs to be 65% or more. That is, in order to make the final cold rolling reduction less than 65% without performing intermediate annealing, the thickness of the hot-rolled sheet is less than 1 mm in consideration of the thickness of the final product (usually 0.35 to 0.25 mm). This is not only extremely difficult in practical operation, but also the strength of the material due to cold work hardening is reduced, and sufficient material strength may not be obtained. It is also disadvantageous for rate control. Therefore, the cold rolling reduction was set to 65% or more.
[0055]
The final plate (cold rolled plate) obtained as described above may be used as it is in a DI can body, but if necessary, in order to improve the formability by recovering the ductility of the final plate, The cold-rolled sheet may be subjected to final annealing (finish annealing) at a temperature of 80 to 200 ° C. for 0.1 to 24 hours. If the temperature of the final annealing is less than 80 ° C., the effect of improving the formability is insufficient, while if it exceeds 200 ° C., the strength decrease due to softening increases. If the holding time of the final annealing is less than 0.1 hour, the effect of improving the formability will be insufficient, while if it exceeds 24 hours, the effect of improving the formability will be saturated and a problem will arise in terms of cost. It should be noted that the same annealing effect as the above-described final annealing can be obtained even by utilizing the processing heat generated when cold rolling is performed at a high speed.
[0056]
【Example】
Each of the alloy symbols A to G shown in Table 1 was cast by a DC casting method according to a conventional method. The obtained ingot is subjected to a homogenization treatment, subjected to hot rolling, wound into a coil, cooled to 100 ° C. or lower, further subjected to cold rolling to a final sheet thickness, and finalized for a part of the ingot. Annealing was performed to obtain a final plate (product plate). Specific conditions of these processes are shown in production numbers 1 to 12 in Tables 2 and 3. In the hot rolling, a reversing mill was used as a finishing mill, and all rolling at a stage of a plate thickness of 50 mm or less was performed by a reversing mill.
[0057]
Here, at the stage of cooling to a temperature of 100 ° C. or less after the completion of the hot rolling, the strength (tensile strength and proof stress in the rolling direction) of the hot-rolled sheet is examined. The Cube azimuth density, Cu azimuth density, S azimuth density, and Bs azimuth density were measured at a position at a depth of 1/4 of the plate thickness in the thickness direction, and the results are shown in Table 3.
[0058]
In addition, for the final plate, the Cube orientation density C at a portion 1 / of the plate thickness from the plate surface layer and the plate surface 0 , C 1/4 In the same manner, the Cu orientation density, S orientation density, and Bs orientation density belonging to the β fiber in the plate surface layer and at a portion 部位 of the plate thickness from the plate surface are examined, and the Cube orientation density C of the plate surface layer is determined. 0 And the Cube azimuth density C at a portion 板 of the plate thickness from the plate surface 1/4 And the value of the sum (C 0 + C 1/4 ), And at the same time, the sum d of the respective orientation densities of the Cu, S, and Bs orientations of the plate surface layer 0 And the total d of the azimuth densities of Cu orientation, S orientation, and Bs orientation at a quarter of the plate thickness from the plate surface 1/4 And the sum (d 0 + D 1/4 ) Was obtained, and the results are shown in Table 4.
[0059]
Here, the measurement of each orientation density as described above, that is, the measurement of the texture was performed as follows.
[0060]
That is, when obtaining the texture of the surface layer of the sheet thickness, the rolled sheet was used as it was, without etching, as a measurement sample. On the other hand, when obtaining the texture of a portion corresponding to 1 / of the plate thickness, a measurement sample was obtained by etching from the surface with a NaOH aqueous solution to a portion corresponding to 1 / of the plate thickness. Then, using an X-ray diffractometer, imperfect pole figures of {200}, {220}, and {111} were measured by the Schulz reflection method, and three-dimensional crystal orientation analysis (ODF) was performed based on these. Note that the Cu orientation is the ideal orientation, the {112} <111> orientation, the S orientation is the {123} <634> orientation, the Bs orientation is the {110} <112> orientation, and the Cube orientation is the {001} <100> orientation. However, those having a misorientation of 15 ° around these ideal orientations were also calculated as crystals of each orientation.
[0061]
Further, the electric conductivity (% IACS) and the Mn solid solution amount of each final plate obtained as described above were also examined, and the results are also shown in Table 4. Here, the conductivity was measured by using an eddy current conductivity measuring device with copper and brass as reference samples.
[0062]
With respect to the final sheet (thin sheet for can body) obtained as described above, the tensile strength (TS), proof stress (YS), and elongation (EL) of the original sheet were obtained using a tensile test piece taken in parallel with the rolling direction. And a tensile strength (TS), a proof stress (YS), and an elongation (EL) after a heat treatment at 200 ° C. for 20 minutes assuming baking of the coating (baking). Further, the ear ratio of the base plate was examined, and the "success rate of severe canning of DI cans" was examined as an index of the ironing property, and the mouth spread rate was examined as an index of the flange formability (mouth spreadability). Tables 4 and 5 show these results.
[0063]
Here, the ear ratio was determined by performing a cup deep drawing test under the conditions of a punch diameter of 32 mm and a blank diameter of 56 mm. The “success rate of DI severe ironing” as an index of ironing property is obtained by extracting the second die in the DI can molding and setting the ironing rates of the first and third dies to 55%, for 100 continuous cans. The ratio of cans that did not cause can breakage in can making was examined. Further, the opening ratio as an index of the flange formability (mouth opening property) is such that the DI can after 4-stage necking is trimmed, washed and baked, and has a gradient of 15 ° in the upper opening portion of the DI can. A test was performed in which the punch was pushed into the material until cracks were generated, and the mouth expansion rate until the cracks were generated was determined by the following equation.
Mouth expansion rate = [R1-R0] × 100%
R0: radius of DI can opening after four-stage necking (29 mm)
R1: radius of the opening when the mouth is expanded to the limit where cracks occur
[0064]
[Table 1]
Figure 2004263253
[0065]
[Table 2]
Figure 2004263253
[0066]
[Table 3]
Figure 2004263253
[0067]
[Table 4]
Figure 2004263253
[0068]
[Table 5]
Figure 2004263253
[0069]
In Tables 2 to 5, Production Nos. 1 to 5 are examples of production using alloys within the component composition range specified in the present invention and according to the manufacturing method specified in the present invention. In these examples, as shown in Tables 4 and 5, it was possible to obtain a material having a low ear ratio, a sufficiently high strength after baking, and excellent ironing properties and flange formability.
[0070]
On the other hand, in the production number 6, the alloy component is within the range specified in the present invention, but the manufacturing method is out of the range specified in the present invention. That is, the maximum temperature in the hot rolling after a thickness of 50 mm or more is as high as 472 ° C., which is outside the range of 280 to 450 ° C. specified in the present invention, and the rising temperature of hot rolling is as low as 256 ° C., which is specified in the present invention. Outside the range of 280 to 350 ° C., the proof strength of the hot-rolled finished sheet is as high as 144 MPa, out of the range of 120 MPa or less specified in the present invention, and the texture of the hot-rolled sheet and the texture of the final sheet are also This is outside the range specified by the present invention, and as a plate for a DI can body, the 45 ° ear ratio is high, the success rate of severe ironing is low, and the mouth opening rate is inferior.
[0071]
In the case of Production No. 7, the alloy component is out of the range specified in the present invention, and the strength after baking is insufficient. (Note: The strength of the material must be 240 MPa or more from the viewpoint of the pressure resistance of the DI can, etc.) Also, the ironing property and the flange formability were inferior.
[0072]
Further, in the case of serial numbers 8 to 10, since the conditions of the homogenization treatment or the hot rolling were out of the range specified in the present invention, it was difficult to continue the hot rolling due to edge cracks during the hot rolling. I have.
[0073]
In the case of the production number 11, the surface temperature of the hot rolling roll exceeded the upper limit of the range specified in the present invention, so that the 45 ° ear ratio was high and the ironing property of the DI can was poor.
[0074]
In the case of the production number 12, the homogenization treatment conditions were out of the range specified in the present invention, so that the 0 ° and 90 ° ear ratios were high, and the ironing property of the DI can was inferior.
[0075]
【The invention's effect】
As is apparent from the above-described embodiment, according to the present invention, a hard plate for a DI can body has an excellent balance, that is, it has a high strength after baking, has a low ear rate, and has a high strength. A plate excellent in both properties and flange formability can be obtained. Further, as a manufacturing method, the above-described excellent material can be obtained by a process in which intermediate annealing is omitted after hot rolling or in the middle of cold rolling. it can.

Claims (4)

Mg0.5〜2.0%(mass%、以下同じ)、Mn0.5〜2.0%、Fe0.1〜0.7%、Si0.05〜0.5%、Cu0.05〜0.5%を含有し、残部がAlおよび不可避的不純物よりなるアルミニウム合金からなり、かつ板表層のβファイバに属するCu方位、S方位、Bs方位の各方位密度の合計をdとするとともに、板表面から板厚方向に板厚の1/4の深さの位置におけるβファイバに属するCu方位、S方位、Bs方位の各方位密度の合計をd1/4とし、さらに板表層におけるCube方位の方位密度をCとし、かつ板表面から板厚方向に板厚の1/4の深さの位置におけるCube方位の方位密度をC1/4とした場合に、次式
(d+d1/4)>(C+C1/4
を満足し、さらにMn固溶量が0.05〜0.35%の範囲内でかつ導電率が34〜45IACS%の範囲内であることを特徴とする、缶胴用アルミニウム合金硬質板。
Mg 0.5 to 2.0% (mass%, the same applies hereinafter), Mn 0.5 to 2.0%, Fe 0.1 to 0.7%, Si 0.05 to 0.5%, Cu 0.05 to 0.5 %, And the balance is made of an aluminum alloy consisting of Al and unavoidable impurities, and the total of the orientation densities of the Cu, S, and Bs orientations belonging to the β fiber in the surface layer of the sheet is defined as d 0, and the surface of the sheet is determined. , The sum of the azimuth densities of the Cu, S, and Bs orientations belonging to the β fiber at a position at a depth of 板 of the thickness in the thickness direction is d 4, and the azimuth of the Cube orientation in the surface layer of the plate When the density is C 0 and the azimuth density of the Cube orientation at a position at a depth of 板 of the plate thickness from the plate surface in the plate thickness direction is C , the following formula (d 0 + d 4) is obtained. )> (C 0 + C 1/4 )
Characterized in that the solid solution amount of Mn is in the range of 0.05 to 0.35% and the electrical conductivity is in the range of 34 to 45 IACS%.
請求項1の缶胴用アルミニウム合金硬質板において、
前記アルミニウム合金の成分として、さらにCr0.05〜0.3%、Zn0.05〜0.5%、Ti0.005〜0.20%のうちの1種または2種以上を含有することを特徴とする、缶胴用アルミニウム合金硬質板。
The aluminum alloy hard plate for a can body according to claim 1,
The aluminum alloy further comprises one or more of 0.05 to 0.3% Cr, 0.05 to 0.5% Zn, and 0.005 to 0.20% Ti. Aluminum alloy hard plate for can body.
請求項1もしくは請求項2において規定される成分組成のアルミニウム合金を鋳造した後、520〜630℃の範囲内の温度で1時間以上保持する均質化処理を行ない、次いで熱間圧延を行なって巻取り、100℃以下の温度まで冷却するにあたり、
(1)熱間圧延開始温度を350〜590℃の範囲内とし、
(2)板厚50mmから上がり板厚までの熱間圧延中において、材料温度を280〜450℃の範囲内に制御するとともに、各パスの歪み速度を2.0〜350/秒の範囲内に制御し、かつ各パス間での滞留時間を10分以内に制御し、
(3)板厚50mmから上がり板厚までの熱間圧延中において圧延ロールと板との接触部分の平均温度を350℃以下に保持し、
(4)熱間圧延上がりの材料温度を280〜350℃の範囲内とし、
(5)熱間圧延上がり板厚を1.5〜2.8mmの範囲とし、
(6)熱間圧延上がりの280〜350℃の範囲内の温度から100℃以下までの平均冷却速度を100℃/時間以下に制御し、
以上の(1)〜(6)によって、耐力が120MPa以下、板表面から板厚方向に板厚の1/4の深さの部位におけるCube方位の方位密度がランダム方位の5〜140倍の範囲内にあり、かつ圧延集合組織に属するCu方位、S方位、Bs方位の各方位密度がそれぞれランダム方位の10倍以下である熱間圧延板を得、
さらに、中間焼鈍を施すことなく65%以上の圧延率で冷間圧延を施すことを特徴とする、缶胴用アルミニウム合金硬質板の製造方法。
After casting the aluminum alloy having the component composition defined in claim 1 or 2, a homogenization treatment is performed at a temperature in the range of 520 to 630 ° C. for 1 hour or more, and then hot rolling is performed. To cool to below 100 ° C
(1) The hot rolling start temperature is in the range of 350 to 590 ° C,
(2) During hot rolling from a plate thickness of 50 mm to a rising plate thickness, the material temperature is controlled within a range of 280 to 450 ° C., and the strain rate of each pass is set within a range of 2.0 to 350 / sec. Control and control the residence time between each pass within 10 minutes,
(3) During hot rolling from a plate thickness of 50 mm to a rising plate thickness, the average temperature of the contact portion between the rolling roll and the plate is maintained at 350 ° C. or less,
(4) The material temperature after hot rolling is set to a range of 280 to 350 ° C,
(5) The hot-rolled sheet thickness is in the range of 1.5 to 2.8 mm,
(6) controlling the average cooling rate from a temperature in the range of 280 to 350 ° C. after hot rolling to 100 ° C. or less to 100 ° C./hour or less,
According to the above (1) to (6), the proof strength is 120 MPa or less, and the azimuth density of the Cube orientation in a portion having a depth of 1/4 of the thickness in the thickness direction from the surface of the plate is 5 to 140 times the random orientation. And hot-rolled sheet having Cu orientation, S orientation, and Bs orientation belonging to the rolling texture, each having an orientation density of 10 times or less of the random orientation,
Further, a method for producing an aluminum alloy hard plate for a can body, wherein cold rolling is performed at a rolling rate of 65% or more without performing intermediate annealing.
請求項3に記載の缶胴用アルミニウム合金硬質板の製造方法において、
前記冷間圧延の後、さらに80〜200℃の範囲内の温度に加熱して0.1〜24時間保持する最終焼鈍を行なうことを特徴とする、缶胴用アルミニウム合金硬質板の製造方法。
The method for producing an aluminum alloy hard plate for a can body according to claim 3,
A method for producing an aluminum alloy hard plate for a can body, comprising: performing a final annealing in which the steel sheet is further heated to a temperature in the range of 80 to 200 ° C. and maintained for 0.1 to 24 hours after the cold rolling.
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