JPH05306440A - Manufacture of aluminum alloy sheet for forming excellent baking hardenability - Google Patents

Manufacture of aluminum alloy sheet for forming excellent baking hardenability

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Publication number
JPH05306440A
JPH05306440A JP13810492A JP13810492A JPH05306440A JP H05306440 A JPH05306440 A JP H05306440A JP 13810492 A JP13810492 A JP 13810492A JP 13810492 A JP13810492 A JP 13810492A JP H05306440 A JPH05306440 A JP H05306440A
Authority
JP
Japan
Prior art keywords
treatment
aluminum alloy
cooling rate
sec
less
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.)
Pending
Application number
JP13810492A
Other languages
Japanese (ja)
Inventor
Hajime Watanabe
元 渡辺
Katsutoshi Sasaki
勝敏 佐々木
Kunihiko Kishino
邦彦 岸野
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.)
JFE Steel Corp
Furukawa Aluminum Co Ltd
Original Assignee
Furukawa Aluminum Co Ltd
Kawasaki Steel Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Furukawa Aluminum Co Ltd, Kawasaki Steel Corp filed Critical Furukawa Aluminum Co Ltd
Priority to JP13810492A priority Critical patent/JPH05306440A/en
Publication of JPH05306440A publication Critical patent/JPH05306440A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To improve the formability and strength after the baking finishing treatment of an aluminum alloy sheet for forming suitable for an automotive outer sheet, a sheet for packaging, etc. CONSTITUTION:An Al alloy contg., by weight, 0.02 to 2.0% Cu, 0.5 to 2.5% Mg and 0.5 to 3.0% Si, and the balance Al with inevitable impurities and an Al alloy, in addition, contg. one or two kinds among 0.001 to 0.1% Cr and 0.001 to 0.2% Zr are melted and cast, and the ingot is subjected to homogenizing treatment at 400 to 600 deg.C for >=1hr, is thereafter subjected to a hot rolling treatment, is rapidly cooled to <=120 deg.C at >=3 deg.C/sec cooling rate immediately after the completion of the hot rolling, is subsequently subjected to a solution heating treatment at >=400 deg.C and is immediately subjected to rapid cooling treatment at >=3 deg.C/sec cooling rate.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は優れた成形性ならびに焼
付け硬化性を有し、強度が要求され、しかも焼付け塗装
を施される様な部材、例えば自動車外板、包装用板材な
どに適した、成形用アルミニウム合金板の製造方法に関
するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention is suitable for members which have excellent moldability and bake hardenability, are required to have strength, and are subjected to bake coating, such as automobile outer plates and packaging plate materials. The present invention relates to a method for manufacturing an aluminum alloy plate for forming.

【0002】[0002]

【従来の技術】従来、自動車外板には冷延鋼板が主に用
いられてきた。しかしながら、最近になり自動車車体の
軽量化要求からアルミニウム合金板を使用することが検
討されている。自動車外板用材料としては、プレス成形
性に優れていること、強度が高いことなどが求められて
いる。このような要求を満足する材料として5052合金、
5182合金などのAl−Mg合金(5000系合金)や、6009
合金、6061合金などのAl−Mg−Si合金(6000系合
金)が用いられてきた。
2. Description of the Related Art Conventionally, cold-rolled steel sheets have been mainly used for automobile outer panels. However, recently, the use of an aluminum alloy plate has been considered in order to reduce the weight of an automobile body. Materials for automobile outer panels are required to have excellent press formability and high strength. 5052 alloy, which is a material that satisfies such requirements
Al-Mg alloy (5000 series alloy) such as 5182 alloy, 6009
Al-Mg-Si alloys (6000 series alloys) such as alloys and 6061 alloys have been used.

【0003】[0003]

【発明が解決しようとする課題】前記した6000系合金は
焼付け塗装後に高い強度が得られるため、自動車外板材
等に適用されている。従来の焼付け温度は180℃で1時
間程度であったが、焼付け温度が低温・短時間化する傾
向がある。このため、これらの合金では十分な焼付け塗
装後の強度が得られない。また、一般的に6000系合金は
5000系合金に比べプレス成形性が劣り、焼付け塗装後の
強度を高めようと添加合金量を増すことで、さらにプレ
ス成形性が劣化する傾向にある。本発明はこれに鑑み種
々検討の結果、プレス成形性に優れ、しかも低温での焼
付け硬化性に優れる成形用アルミニウム合金板の製造法
を開発したものである。
Since the above-mentioned 6000 series alloy can obtain high strength after baking and coating, it is applied to automobile outer plate materials and the like. The conventional baking temperature was 180 ° C for about 1 hour, but the baking temperature tends to be lower and shorter. Therefore, these alloys do not have sufficient strength after baking. Generally, 6000 series alloys
The press formability is inferior to that of the 5000 series alloy, and the press formability tends to be further deteriorated by increasing the amount of added alloy in order to increase the strength after baking coating. As a result of various studies in view of this, the present invention has developed a method for producing an aluminum alloy sheet for forming which is excellent in press formability and is excellent in bake hardenability at low temperatures.

【0004】[0004]

【課題を解決するための手段】本発明は、Cu0.02〜2.
0wt%、Mg0.5〜2.5wt%、Si0.5〜3.0wt%を含み残部A
lおよび不可避的不純物からなるアルミニウム合金を溶
解鋳造し、その鋳塊に400℃以上600℃以下の温度で1時
間以上の均質化処理を施した後、熱間圧延処理を行い、
熱間圧延終了後ただちに3℃/sec以上の冷却速度で120℃
以下に急冷し、その後冷間圧延処理を行い、冷間圧延処
理の後400℃以上の溶体化処理加熱を施し、ただちに3℃
/sec以上の冷却速度で急冷処理を行うことを特徴とする
焼付け硬化性に優れた成形用アルミニウム合金板の製造
方法を請求項1とし、また、Cu0.02〜2.0wt%、Mg0.
5〜2.5wt%、Si0.5〜3.0wt%を含み、さらにCr0.001
〜0.1wt%、Zr0.001〜0.2wt%のうち1種または2種を
含み残部Alおよび不可避的不純物からなるアルミニウ
ム合金を溶解鋳造し、その鋳塊に400℃以上600℃以下の
温度で1時間以上の均質化処理を施した後、熱間圧延処
理を行い、熱間圧延終了後ただちに3℃/sec以上の冷却
速度で120℃以下に急冷し、その後冷間圧延処理を行
い、冷間圧延処理の後400℃以上の溶体化処理加熱を施
し、ただちに3℃/sec以上の冷却速度で急冷処理を行う
ことを特徴とする焼付け硬化性に優れた成形用アルミニ
ウム合金板の製造方法を請求項2とするものである。
The present invention provides Cu 0.02 to 2.
0wt%, Mg 0.5-2.5wt%, Si 0.5-3.0wt%, balance A
1 and aluminum alloy consisting of unavoidable impurities are melt-cast, and the ingot is subjected to homogenizing treatment for 1 hour or more at a temperature of 400 ° C. or more and 600 ° C. or less, followed by hot rolling treatment,
Immediately after completion of hot rolling, 120 ℃ at a cooling rate of 3 ℃ / sec or more
It is rapidly cooled to the following, then cold-rolled, then solution-heated to 400 ° C or more and immediately cooled to 3 ° C.
The method for producing an aluminum alloy sheet for forming having excellent bake hardenability, which comprises performing rapid cooling treatment at a cooling rate of not less than / sec, is claim 1, and further comprises Cu0.02 to 2.0 wt% and Mg0.
5 to 2.5 wt%, Si 0.5 to 3.0 wt%, Cr 0.001
~ 0.1wt%, Zr0.001 ~ 0.2wt%, 1 or 2 kinds, aluminum alloy consisting of balance Al and unavoidable impurities is melt-cast, and the ingot is heated at a temperature of 400 ° C to 600 ° C After performing the homogenizing treatment for more than an hour, perform the hot rolling treatment, and immediately after finishing the hot rolling, rapidly cool to 120 ° C or less at a cooling rate of 3 ° C / sec or more, then perform the cold rolling treatment, and then perform the cold rolling treatment. Request a method for producing aluminum alloy sheet for forming with excellent bake hardenability, characterized by performing solution heat treatment at 400 ° C or higher after rolling treatment, and then performing rapid quenching at a cooling rate of 3 ° C / sec or higher. It is the item 2.

【0005】[0005]

【作用】本発明に於いて、合金組成を限定したのは、以
下の理由による。Cuはマトリックス中に固溶し、焼付
け塗装時にG.P.B.ゾーン、S’−Al Cu Mg
などを析出、あるいはMg2 Siの析出を促進し、強
度、特に耐力を向上させる。その添加量を0.02〜2.0wt%
と限定したのは、0.02wt%未満ではその効果が小さく、
2.0wt%を越えると固溶硬化により成形時の延性が低下す
ると共に、耐食性が悪化するためである。Mgは焼付け
塗装時にSiと共にG.P.ゾーン、Mg2 Siを析出
させるため、焼付け塗装後の強度を向上させる。その添
加量を0.5〜2.5wt%と限定したのは、0.5wt%未満ではそ
の効果が小さく、2.5wt%を越えると成形時の伸びを低下
させるためである。Siは焼付け塗装時にMgと共に
G.P.ゾーン、Mg2 Siを析出させるため、焼付け
塗装後の強度を向上させる。その添加量を0.5〜3.0wt%
と限定したのは、0.5wt%未満ではその効果が小さく、3.
0wt%を越えると均質化処理中に単体Siとして析出する
ことでプレス成形性を下げ、耐食性を悪化させるためで
ある。Zr、Crの添加はそれぞれ結晶粒微細化の効果
があり、マトリックス強度を向上させる目的で添加され
る。各々の添加量を0.001〜0.1wt%、0.001〜0.2wt%と限
定したのは、下限未満ではその効果が小さく、上限を越
えると溶体化処理後の成形性が低下するためである。ま
た、通常Alの不純物として含まれるFeは、マトリッ
クス中に固溶しているSiとα−Al Fe Siを生成
しやすく、Si固溶量を減少させ、焼付け塗装時の硬化
性を低下させるため、0.5wt%未満であることが望まし
い。なお、一般に結晶粒微細化およびマトリックス強度
を向上のため添加されるNi、V、鋳造組織の微細化の
ため添加されるTi、Bなどは、これら元素の合計量が
1.0wt%未満であれば、特に本発明の効果を損うことはな
い。
In the present invention, the reason why the alloy composition is limited is as follows. Cu forms a solid solution in the matrix, and G. P. B. Zone, S'-Al Cu Mg
Etc. or promote precipitation of Mg 2 Si to improve strength, especially proof stress. 0.02 to 2.0 wt%
The reason is that if less than 0.02 wt%, the effect is small,
This is because if it exceeds 2.0 wt%, the ductility at the time of molding is lowered due to solid solution hardening, and the corrosion resistance is deteriorated. Mg and G. P. Since the zone and Mg 2 Si are deposited, the strength after baking coating is improved. The amount added is limited to 0.5 to 2.5 wt% because if it is less than 0.5 wt%, the effect is small, and if it exceeds 2.5 wt%, the elongation at the time of molding is lowered. Si is a G.I. P. Since the zone and Mg 2 Si are deposited, the strength after baking coating is improved. 0.5 ~ 3.0wt%
The reason is that the effect is small when less than 0.5 wt%, 3.
This is because if it exceeds 0 wt%, it is precipitated as simple substance Si during the homogenization treatment to lower the press formability and deteriorate the corrosion resistance. Additions of Zr and Cr each have the effect of refining crystal grains, and are added for the purpose of improving the matrix strength. The addition amount of each is limited to 0.001 to 0.1 wt% and 0.001 to 0.2 wt% because the effect is small below the lower limit and the formability after solution treatment decreases below the upper limit. Further, since Fe, which is usually contained as an impurity in Al, easily forms Si and α-Al Fe Si, which are solid-solved in the matrix, reduces the amount of Si solid-solution and reduces the curability during baking coating. , Less than 0.5 wt% is desirable. In addition, in general, Ni, V added for refining the crystal grains and improving the matrix strength, and Ti, B, etc. added for refining the cast structure have a total amount of these elements.
If it is less than 1.0 wt%, the effect of the present invention is not particularly impaired.

【0006】次に、上記の合金組成によって得られた合
金鋳塊の熱処理ならびに圧延処理について説明する。ま
ず、均質化処理は、合金鋳塊製造時の冷却凝固過程で生
じた晶出物を加熱によって強制的に固溶させ、鋳塊マト
リックスの固溶度を上げると共に添加元素の偏析を拡散
により緩和する。さらに、冷却凝固過程で生じた残留応
力を解消し、熱間圧延処理時の割れを防止する。その温
度を400℃以上600℃以下でおこなうこととしたのは、40
0℃未満では添加元素の拡散、とくに鋳塊の冷却凝固過
程で生じた晶出Siが十分に固溶拡散しないためであ
り、600℃を越えると添加元素の濃度偏析による部分溶
融がおこる為である。さらに、熱処理時間を1時間以上
としたのは、熱処理時間1時間未満では添加元素の固溶
拡散が十分におこなわれず、本発明の効果を著しく損う
ためである。均質化処理を終えた鋳塊は、圧延ロールと
の焼付き等の防止のために、若干の冷却の後に熱間圧延
処理を施される。この熱間圧延温度は通常行われる温度
で特に限定しないが、熱間圧延開始温度が380℃未満で
は熱間圧延時の加工性が劣化すると共に、熱間圧延終了
時に温度が下がりすぎることで添加元素の析出がおこ
り、後に溶体化処理を行っても十分に添加元素を固溶さ
せることが出来ない。従って、熱間圧延開始温度は380
℃以上で行う必要があり、添加元素の固溶を維持するた
め出来るだけ高温で行うことが望ましい。
Next, the heat treatment and rolling treatment of the alloy ingot obtained by the above alloy composition will be described. First, in the homogenization treatment, the crystallized substances generated during the cooling and solidification process during the production of alloy ingots are forcibly solid-solved by heating, the solid solubility of the ingot matrix is increased, and the segregation of additional elements is relaxed by diffusion. To do. Furthermore, residual stress generated in the cooling and solidifying process is eliminated, and cracking during hot rolling is prevented. The temperature was 400 ℃ or more and 600 ℃ or less.
This is because if the temperature is lower than 0 ° C, the diffusion of the additional element, especially the crystallized Si generated during the cooling and solidification process of the ingot is not sufficiently solid-solution diffused, and if it exceeds 600 ° C, partial melting due to the concentration segregation of the additional element occurs. is there. Further, the heat treatment time is set to 1 hour or more because if the heat treatment time is less than 1 hour, solid solution diffusion of the additional element is not sufficiently performed and the effect of the present invention is significantly impaired. The ingot that has been subjected to the homogenization treatment is subjected to a hot rolling treatment after being slightly cooled in order to prevent seizure with a rolling roll. This hot rolling temperature is not particularly limited to a temperature usually performed, but if the hot rolling start temperature is lower than 380 ° C, the workability during hot rolling is deteriorated, and the temperature is too low at the end of hot rolling. Precipitation of the element occurs, and even if a solution treatment is performed later, the additional element cannot be sufficiently solid-dissolved. Therefore, the hot rolling start temperature is 380
It is necessary to carry out at a temperature of not less than 0 ° C, and it is desirable to carry out at a temperature as high as possible in order to maintain the solid solution of the additional element.

【0007】熱間圧延終了の後に徐冷された圧延板は析
出物が粗大化しやすく、粗大化した析出物はその後の加
熱処理によっても十分に固溶させることが出来ない。従
って、鋳塊の均質化処理によって得た高い添加元素の固
溶状態を熱間圧延終了時まで維持し、添加元素の析出な
らびに粗大化を防ぐために、熱間圧延処理の終了した圧
延板はただちに3℃/sec以上の冷却速度で120℃以下に急
冷する。その冷却速度を3℃/sec以上と限定したのは、3
℃/sec未満の冷却速度では冷却時に添加元素の析出がお
こり、プレス成形性ならびに焼付け塗装時の硬化性を低
下させるためである。また、冷却後の温度を120℃以下
と限定したのは、120℃を越える温度で冷却を終了させ
た場合には、冷却終了時点でG.P.ゾーン、Mg2
iまたはMg2 Si等の析出初期のクラスタが生じ、後
の製造工程中に析出相の成長が起ることで、圧延板のマ
トリックスの固溶度が下がるためである。また、この熱
間圧延板の急冷の時に、10mmを越える熱間圧延上がり板
厚では、熱間圧延後の急冷時に3 ℃/sec以上の冷却速度
を得ることが難しく、3℃/sec未満の冷却速度では冷却
時に添加元素の析出が起こり、プレス成形性ならびに焼
付け塗装時の硬化性を低下させるため、熱間圧延上がり
板厚を10mm未満とすることが望ましい。熱間圧延後の急
冷を終了した圧延板は、続いて行う冷間圧延処理の後
に、溶体化処理加熱を施し、ただちに急冷を行うことで
析出物をマトリックス中に固溶し、過飽和固溶状態とす
る。溶体化処理加熱温度を400℃と限定したのは、加熱
温度4 00℃未満では析出物が十分に固溶しないため、焼
付け塗装時の強度向上が小さいためである。なお溶体化
処理加熱の保持時間は特に規定しないが、400℃以上の
温度に5秒以上となることが望ましい。また、溶体化処
理加熱後の冷却温度を3℃/sec以上としたのは、3℃/sec
未満の冷却速度では冷却途中において、溶体化処理加熱
によっていったん固溶した添加元素の析出が起こり、プ
レス成形性ならびに焼付け塗装時の硬化性を著しく低下
させるためである。
Precipitates tend to coarsen in the rolled plate that has been gradually cooled after the completion of hot rolling, and the coarsened precipitates cannot be sufficiently solid-solved by the subsequent heat treatment. Therefore, in order to maintain the solid solution state of the high additive element obtained by the homogenization treatment of the ingot until the end of hot rolling, and to prevent precipitation and coarsening of the additional element, the rolled plate immediately after the hot rolling treatment is immediately finished. Rapidly cool to 120 ° C or less at a cooling rate of 3 ° C / sec or more. Limiting the cooling rate to 3 ° C / sec or more is 3
This is because, at a cooling rate of less than ° C / sec, additional elements are precipitated during cooling, which deteriorates press formability and curability during baking coating. Further, the temperature after cooling is limited to 120 ° C. or less, because when the cooling is finished at a temperature higher than 120 ° C., G.I. P. Zone, Mg 2 S
This is because clusters such as i or Mg 2 Si in the initial stage of precipitation occur, and the growth of the precipitation phase occurs in the subsequent manufacturing process, which lowers the solid solubility of the matrix of the rolled plate. Further, when the hot-rolled sheet is rapidly cooled, if the hot-rolled sheet thickness exceeds 10 mm, it is difficult to obtain a cooling rate of 3 ° C / sec or more during the rapid cooling after hot-rolling, and if the hot-rolled sheet has a thickness of less than 3 ° C / sec. At the cooling rate, precipitation of the additional element occurs during cooling, which deteriorates press formability and hardenability during baking coating. Therefore, it is desirable that the hot-rolled sheet thickness be less than 10 mm. The rolled sheet that has undergone quenching after hot rolling is subjected to solution treatment heating after the subsequent cold rolling treatment, and the precipitate is solid-solved in the matrix by immediate quenching, resulting in a supersaturated solid solution state. And The reason for limiting the solution treatment heating temperature to 400 ° C. is that if the heating temperature is less than 400 ° C., the precipitates do not form a solid solution sufficiently, and the strength improvement during baking coating is small. The holding time of the solution heat treatment is not particularly limited, but it is desirable that the temperature is 400 ° C. or higher and 5 seconds or longer. The cooling temperature after solution heat treatment was set to 3 ° C / sec or more because it was 3 ° C / sec.
This is because at a cooling rate of less than, during the cooling, precipitation of the additional element once solid-solubilized by the solution heat treatment occurs, and press formability and curability during baking coating are significantly reduced.

【0008】[0008]

【実施例】以下に本発明の実施例について説明する。 実施例1 表1に示す組成のAl合金を常法により溶解、DC鋳造に
より鋳塊を得た。この鋳塊に520℃×1時間の均質化処
理を行い、熱間圧延上がり板厚を7mmとし、熱間圧延終
了後ただちに15℃/secの冷却速度で120℃に強制急冷
し、その後冷間圧延により厚さ1mmの板材とした。この
板材に550℃×10秒の加熱後15℃/secの冷却速度による
溶体化処理を施した。このように製造された板材につい
て、引張試験、エリクセン張出試験、限界深絞り(LDR)
試験を行った。また、焼付け塗装処理をシュミレートし
た150℃×20、30、60min、170℃×20、30、60min、200
×20、30、60minの加熱を施した後にも引張試験を行っ
た。引張試験は、JIS5号引張試験片により、引張強さ、
耐力、伸びを測定した。エリクセン張出試験は、JIS Z
2247 A法により張出し高さを測定した。限界深絞り(LD
R)試験は、φ33mmのポンチで潤滑油を塗布したブランク
の深絞りを行い、破断しない最大ブランク径をポンチ径
で除した値を求めた。この結果を表2および表3に示
す。
EXAMPLES Examples of the present invention will be described below. Example 1 An Al alloy having the composition shown in Table 1 was melted by a conventional method, and an ingot was obtained by DC casting. This ingot is homogenized at 520 ° C for 1 hour, the thickness of the hot rolled sheet is increased to 7 mm, and immediately after the hot rolling, it is forcibly and rapidly cooled to 120 ° C at a cooling rate of 15 ° C / sec, and then cold-rolled. It was rolled into a plate with a thickness of 1 mm. This plate material was heated at 550 ° C. for 10 seconds and then subjected to solution treatment at a cooling rate of 15 ° C./sec. Tensile test, Erichsen bulge test, limit deep drawing (LDR)
The test was conducted. In addition, 150 ℃ × 20, 30, 60min, 170 ℃ × 20, 30, 60min, 200 which simulated baking coating processing
Tensile tests were also conducted after heating for × 20, 30, 60 minutes. Tensile test, JIS No. 5 tensile test piece, tensile strength,
The yield strength and elongation were measured. Erichsen overhang test is JIS Z
The overhang height was measured by the 2247 A method. Limit deep drawing (LD
In the R) test, a blank coated with lubricating oil was deep-drawn with a punch of φ33 mm, and the maximum blank diameter that did not break was divided by the punch diameter to obtain a value. The results are shown in Tables 2 and 3.

【0009】[0009]

【表1】 [Table 1]

【0010】[0010]

【表2】 [Table 2]

【0011】[0011]

【表3】 [Table 3]

【0012】表2および表3より明らかなように本発明
に係るNo.1〜7は、いずれも機械的性質および成形性に
優れ、かつ焼付け塗装処理後の強度が優れていることが
判る。一方、本発明の対象とする合金組成を外れるNo.8
は、Mgが多くSiが少ないため、No.9はMgが少な
くSiが多いため、No.10はCr、Zrが多いため、No.
11はCrが多いため、溶体化処理後の成形性、焼付け塗
装処理後の強度のいずれか一つ以上が劣っている。
As is clear from Tables 2 and 3, it can be seen that Nos. 1 to 7 according to the present invention are all excellent in mechanical properties and moldability, and are excellent in strength after baking treatment. On the other hand, No. 8 out of the alloy composition targeted by the present invention
No. 9 has a large amount of Mg and a small amount of Si, and No. 9 has a large amount of Mg and a small amount of Si.
Since No. 11 has a large amount of Cr, one or more of the formability after the solution treatment and the strength after the baking coating treatment are inferior.

【0013】実施例2 実施例1における表1の合金のうち、No.2、7の二合金
について、表4に示す条件A〜Dの熱処理条件で熱間圧
延処理まで行い、熱間圧延上がり板厚を7mmとし、続い
て冷間圧延処理により、厚さ1mmの板材とした。この板
材に550℃×10secの加熱後15℃/secの冷却速度による溶
体化処理を施した。このように製造された板材につい
て、引張試験、エリクセン張出試験、限界深絞り(LDR)
試験を行った。また、焼付け塗装処理シュミレートした
150℃×20、30、60min、170℃×20、30、60min、200℃
×20、30、60minの加熱を施した後にも引張試験を行っ
た。結果を表5および表6に示す。
Example 2 Of the alloys of Table 1 in Example 1, two alloys Nos. 2 and 7 were subjected to hot rolling under the heat treatment conditions A to D shown in Table 4 and then hot rolled. The plate thickness was set to 7 mm, and then cold rolled to obtain a plate material having a thickness of 1 mm. This plate material was heated at 550 ° C. for 10 seconds and then solution-treated at a cooling rate of 15 ° C./sec. Tensile test, Erichsen bulge test, limit deep drawing (LDR)
The test was conducted. Also, simulated baking treatment
150 ° C x 20, 30, 60min, 170 ° C x 20, 30, 60min, 200 ° C
Tensile tests were also conducted after heating for × 20, 30, 60 minutes. The results are shown in Tables 5 and 6.

【0014】[0014]

【表4】 [Table 4]

【0015】[0015]

【表5】 [Table 5]

【0016】[0016]

【表6】 [Table 6]

【0017】表4〜表6より明らかなように、本発明方
法の条件AおよびBによるものは、ずれも機械的性質お
よび成形性に優れ、かつ焼付け塗装処理後の強度が優れ
ている。一方、本発明方法を外れる条件Cは熱間圧延後
の冷却速度が遅いため、条件Dは均質化処理温度が低い
ため、溶体化処理後の成形性、焼付け塗装処理後の強度
のいずれか一つ以上が劣っている。
As can be seen from Tables 4 to 6, the conditions A and B of the method of the present invention are excellent in mechanical properties and moldability even in deviation, and are excellent in strength after baking coating. On the other hand, condition C, which deviates from the method of the present invention, has a slow cooling rate after hot rolling, and condition D has a low homogenization treatment temperature. Therefore, one of moldability after solution treatment and strength after baking coating treatment is required. One or more are inferior.

【0018】実施例3 実施例1における表1の合金のうちNo.6を、実施例1と
同様に厚さ1mmの板材とした。この板材を表7に示す条
件による溶体化処理(保持時間10sec)を施した。以上の
工程により製造された板材について、引張試験、エリク
セン張出試験、限界深絞り(LDR)試験を行った。また、
焼付け塗装処理シュミレートした150℃×20、30min、17
0℃×20、30min、200℃×20、30minの加熱を施した後に
も引張試験を行った。結果を表7に併せて示す。
Example 3 No. 6 of the alloys shown in Table 1 in Example 1 was used as a plate material having a thickness of 1 mm as in Example 1. This plate material was subjected to solution treatment (holding time 10 sec) under the conditions shown in Table 7. A tensile test, an Erichsen bulge test, and a limit deep drawing (LDR) test were performed on the plate material manufactured through the above steps. Also,
Baking coating treatment simulated 150 ℃ × 20, 30min, 17
Tensile tests were also conducted after heating at 0 ° C. × 20, 30 min and 200 ° C. × 20, 30 min. The results are also shown in Table 7.

【0019】[0019]

【表7】 [Table 7]

【0020】表7より明らかなように、本発明方法によ
るものは、いずれも機械的性質および成形性に優れ、か
つ焼付け塗装処理後の強度が優れている。一方、本発明
方法を外れる比較方法においては、溶体化処理の冷却速
度が遅いため、または溶体化処理温度が低いため、溶体
化処理後の成形性、焼付け塗装処理後の強度のいずれか
一つ以上が劣っている。
As is clear from Table 7, all of the products produced by the method of the present invention are excellent in mechanical properties and moldability, and are excellent in strength after baking treatment. On the other hand, in the comparative method deviating from the method of the present invention, the cooling rate of the solution heat treatment is slow, or the solution heat treatment temperature is low, so that the moldability after the solution heat treatment or the strength after the baking coating treatment is one of The above is inferior.

【0021 】[002]

【発明の効果】このように本発明によれば、溶体化処理
後の成形性、焼付け後の強度に優れた成形用アルミニウ
ム合金板を得ることが出来るもので、特に自動車車体外
板の様に焼付け塗装工程を有し、高成形性、高強度、高
耐力を必要とする成形品に最適なものである。さらに、
焼付け塗装やそれに準じた製造工程を有する成形品に優
れた特性を発揮するため、建築用構造部材、包装用板
材、器物、電気機器のシャーシ等応用範囲が広く、工業
上顕著な効果を奏するものである。
As described above, according to the present invention, it is possible to obtain an aluminum alloy sheet for forming which is excellent in formability after solution treatment and strength after baking, and particularly in the case of outer panels of automobile bodies. It has a baking coating process and is most suitable for molded products that require high moldability, high strength and high yield strength. further,
Since it exhibits excellent characteristics for molded products that have baking coating and manufacturing processes similar to it, it has a wide range of applications such as structural members for construction, plate materials for packaging, appliances, chassis of electrical equipment, etc., and has remarkable industrial effects Is.

───────────────────────────────────────────────────── フロントページの続き (72)発明者 佐々木 勝敏 東京都千代田区丸の内2丁目6番1号 古 河アルミニウム工業株式会社内 (72)発明者 岸野 邦彦 東京都千代田区丸の内2丁目6番1号 古 河アルミニウム工業株式会社内 ─────────────────────────────────────────────────── ─── Continuation of the front page (72) Inventor Katsutoshi Sasaki 2-6-1, Marunouchi, Chiyoda-ku, Tokyo Furukawa Aluminum Co., Ltd. (72) Kunihiko Kishino 2-6-1, Marunouchi, Chiyoda-ku, Tokyo Furukawa Aluminum Co., Ltd.

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 Cu0.02〜2.0wt%、Mg0.5〜2.5wt%、
Si0.5〜3.0wt%を含み残部Alおよび不可避的不純物
からなるアルミニウム合金を溶解鋳造し、その鋳塊に40
0℃以上600℃以下の温度で1時間以上の均質化処理を施
した後、熱間圧延処理を行い、熱間圧延終了後ただちに
3℃/sec以上の冷却速度で120℃以下に急冷し、その後冷
間圧延処理を行い、冷間圧延処理の後400℃以上の溶体
化処理加熱を施し、ただちに3℃/sec以上の冷却速度で
急冷処理を行うことを特徴とする焼付け硬化性に優れた
成形用アルミニウム合金板の製造方法。
1. Cu0.02 to 2.0 wt%, Mg0.5 to 2.5 wt%,
An aluminum alloy containing 0.5 to 3.0 wt% of Si and the balance of Al and unavoidable impurities is melt-cast, and 40
After performing homogenizing treatment at a temperature of 0 ° C or more and 600 ° C or less for 1 hour or more, hot rolling treatment is performed, and immediately after hot rolling is finished.
Rapid cooling to 120 ° C or less at a cooling rate of 3 ° C / sec or more, then cold rolling treatment, solution heat treatment to 400 ° C or more after cold rolling treatment, and immediately cooling rate of 3 ° C / sec or more A method for producing an aluminum alloy sheet for forming, which is excellent in bake hardenability, characterized by performing a quenching treatment at.
【請求項2】 Cu0.02〜2.0wt%、Mg0.5〜2.5wt%、
Si0.5〜3.0wt%を含み、さらにCr0.001〜0.1wt%、Z
r0.001〜0.2wt%のうち1種または2種を含み残部Al
および不可避的不純物からなるアルミニウム合金を溶解
鋳造し、その鋳塊に400℃以上600℃以下の温度で1時間
以上の均質化処理を施した後、熱間圧延処理を行い、熱
間圧延終了後ただちに3℃/sec以上の冷却速度で120℃以
下に急冷し、その後冷間圧延処理を行い、冷間圧延処理
の後400℃以上の溶体化処理加熱を施し、ただちに3℃/s
ec以上の冷却速度で急冷処理を行うことを特徴とする焼
付け硬化性に優れた成形用アルミニウム合金板の製造方
法。
2. Cu0.02 to 2.0 wt%, Mg0.5 to 2.5 wt%,
Si 0.5-3.0 wt%, Cr 0.001-0.1 wt%, Z
r 0.001 to 0.2 wt% of 1 or 2 types and balance Al
And aluminum alloy consisting of unavoidable impurities are melt-cast, and the ingot is homogenized at a temperature of 400 ° C or more and 600 ° C or less for 1 hour or more, then hot-rolled, and after hot-rolling is completed. Immediately, it is rapidly cooled to 120 ° C or less at a cooling rate of 3 ° C / sec or more, then cold-rolled, then solution-heated to 400 ° C or more after cold-rolling, and immediately 3 ° C / s.
A method for producing an aluminum alloy sheet for forming, which is excellent in bake hardenability, characterized by performing a quenching treatment at a cooling rate of ec or more.
JP13810492A 1992-04-30 1992-04-30 Manufacture of aluminum alloy sheet for forming excellent baking hardenability Pending JPH05306440A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP13810492A JPH05306440A (en) 1992-04-30 1992-04-30 Manufacture of aluminum alloy sheet for forming excellent baking hardenability

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13810492A JPH05306440A (en) 1992-04-30 1992-04-30 Manufacture of aluminum alloy sheet for forming excellent baking hardenability

Publications (1)

Publication Number Publication Date
JPH05306440A true JPH05306440A (en) 1993-11-19

Family

ID=15214044

Family Applications (1)

Application Number Title Priority Date Filing Date
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Country Status (1)

Country Link
JP (1) JPH05306440A (en)

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WO1995022634A1 (en) * 1994-02-16 1995-08-24 Sumitomo Light Metal Industries, Ltd. Method of manufacturing aluminum alloy plate for molding
WO1996003531A1 (en) * 1994-07-22 1996-02-08 Alcan International Limited Aluminum alloys and process for making aluminum alloy sheet
WO1997041272A1 (en) * 1996-04-29 1997-11-06 Pechiney Rhenalu Aluminium-silicon-magnesium alloy for motor vehicle body
WO2011000635A1 (en) 2009-06-30 2011-01-06 Hydro Aluminium Deutschland Gmbh Almgsi strip for applications having high plasticity requirements
WO2012160720A1 (en) * 2011-05-20 2012-11-29 住友軽金属工業株式会社 Aluminum alloy material with excellent bendability and process for producing same
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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5616189A (en) * 1993-07-28 1997-04-01 Alcan International Limited Aluminum alloys and process for making aluminum alloy sheet
WO1995022634A1 (en) * 1994-02-16 1995-08-24 Sumitomo Light Metal Industries, Ltd. Method of manufacturing aluminum alloy plate for molding
WO1996003531A1 (en) * 1994-07-22 1996-02-08 Alcan International Limited Aluminum alloys and process for making aluminum alloy sheet
EP0949344A1 (en) * 1994-07-22 1999-10-13 Alcan International Limited Aluminium alloys and process for making aluminium alloy sheet
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US10612115B2 (en) 2009-06-30 2020-04-07 Hydro Aluminium Deutschland Gmbh AlMgSi strip for applications having high formability requirements
WO2011000635A1 (en) 2009-06-30 2011-01-06 Hydro Aluminium Deutschland Gmbh Almgsi strip for applications having high plasticity requirements
JP2012531521A (en) * 2009-06-30 2012-12-10 ハイドロ アルミニウム ドイチュラント ゲー エム ベー ハー AlMgSi strip for applications with high formability requirements
KR101401060B1 (en) * 2009-06-30 2014-05-29 하이드로 알루미늄 도이칠란트 게엠베하 Almgsi strip for applications having high plasticity requirements
EP2270249B2 (en) 2009-06-30 2020-05-27 Hydro Aluminium Deutschland GmbH AlMgSi-sheet for applications with high shaping requirements
US10047422B2 (en) 2009-06-30 2018-08-14 Hydro Aluminium Deutschland Gmbh AlMgSi strip for applications having high formability requirements
WO2012160720A1 (en) * 2011-05-20 2012-11-29 住友軽金属工業株式会社 Aluminum alloy material with excellent bendability and process for producing same
US9834833B2 (en) 2011-05-20 2017-12-05 Uacj Corporation Aluminum alloy material exhibiting excellent bendability and method for producing the same
JP2020519772A (en) * 2017-05-26 2020-07-02 ノベリス・インコーポレイテッドNovelis Inc. High-strength corrosion resistance 6xxx series aluminum alloy and manufacturing method thereof
US11466351B2 (en) * 2018-05-15 2022-10-11 Novells Inc. F* and W temper aluminum alloy products and methods of making the same

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