JPH05202454A - Manufacture of baking hardenability aluminum alloy sheet for forming - Google Patents

Manufacture of baking hardenability aluminum alloy sheet for forming

Info

Publication number
JPH05202454A
JPH05202454A JP3555392A JP3555392A JPH05202454A JP H05202454 A JPH05202454 A JP H05202454A JP 3555392 A JP3555392 A JP 3555392A JP 3555392 A JP3555392 A JP 3555392A JP H05202454 A JPH05202454 A JP H05202454A
Authority
JP
Japan
Prior art keywords
aluminum alloy
cold
rolled
alloy sheet
subjected
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
JP3555392A
Other languages
Japanese (ja)
Inventor
Katsutoshi Sasaki
勝敏 佐々木
Kunihiko Kishino
邦彦 岸野
Hajime Watanabe
元 渡辺
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 JP3555392A priority Critical patent/JPH05202454A/en
Publication of JPH05202454A publication Critical patent/JPH05202454A/en
Pending legal-status Critical Current

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  • Heat Treatment Of Steel (AREA)

Abstract

PURPOSE:To provide an Al alloy sheet for forming which is used for an automobile exterior plate or the like, facilitates the solution heat treatment in a continuous annealing equipment and has high baking hardenability. CONSTITUTION:An Al alloy contg., by weight, 0.2 to 3.0wt.% Si and 0.2 to 3.0wt.% Mg, furthermore contg., as necessary 0.01 to 1.5wt.% Cu and 0.01 to 0.25wt.% Fe and, moreover, contg., if desired, total 0.01 to 1.0wt.% of one or >=two kinds among 0.01 to 0.3wt.% Mn, 0.01 to 0.5wt.% Cr, 0.01 to 0.5wt.% Zr, 0.01 to 0.5wt.% Ti and 0.01 to 0.3wt.% Ni, and the balance Al with inevitable impurities is subjected to hot rolling or cold rolling, is subsequently subjected to heat treatment at >=480 deg.C, is thereafter subjected to cold rolling, is subjected to solution heat treatment at >=400 deg.C and is cooled at >=3 deg.C/sec cooling rate to manufacture the objective Al alloy sheet.

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、優れた焼付け硬化性を
有し、自動車外板や包装用板材などの強度が要求され、
しかも焼付け塗装が施される様な部材に適した焼付け硬
化性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 The present invention has excellent bake hardenability, and is required to have strength for automobile outer plates and packaging plate materials.
In addition, the present invention relates to a method for producing a bake-hardenable aluminum alloy sheet for forming, which is suitable for a member to be baked and coated.

【0002】[0002]

【従来の技術】従来、自動車外板には冷延鋼板が主に用
いられていた。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、一部で実用化されている。自動車外板用材料とし
ては、プレス成形性が優れていること、強度が高いこ
と、耐食性に優れている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(Al− 2.5wt
%Mg−0.25wt%Cr)合金,5182(Al−0.35wt%M
n− 4.5wt%Mg)合金などのAl−Mg合金(5000系
合金)や6009(Al− 0.8wt%Si− 0.6wt%Mg−0.
33wt%Cu−0.5wt%Mn)合金,6061(Al− 0.6wt
%Si− 1.0wt%Mg−0.28wt%Cu− 0.2wt%Cr)
合金などのAl−Mg−Si合金(6000系合金)が用い
られていた。
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 studied due to the demand for weight reduction of an automobile body, and it has been partially put into practical use. Materials for automobile outer panels are required to have excellent press formability, high strength, and excellent corrosion resistance. As a material satisfying such requirements, 5052 (Al-2.5wt
% Mg-0.25wt% Cr) alloy, 5182 (Al-0.35wt% M)
Al-Mg alloy (5000 series alloy) such as n-4.5 wt% Mg) or 6009 (Al-0.8 wt% Si-0.6 wt% Mg-0.
33wt% Cu-0.5wt% Mn) alloy, 6061 (Al-0.6wt
% Si-1.0 wt% Mg-0.28 wt% Cu-0.2 wt% Cr)
Al-Mg-Si alloys (6000 series alloys) such as alloys have been used.

【0003】[0003]

【発明が解決しようとする課題】上記6000系合金はプレ
ス成形性が比較的良好であり、焼付け塗装後に高い強度
が得られるため、従来自動車外板材に適用されている。
このような目的で使用される熱処理型アルミニウム合金
板材は、通常連続焼鈍設備によって溶体化処理を行って
いる。しかしながら従来のこの方法では溶体化温度での
保持時間が短いため、充分な溶体化がなされない場合が
ある。従来の自動車の塗装焼付け温度は 180℃で1時間
程度であったが、塗装焼付け温度が低温・短時間化する
傾向があるなかで、高い焼付け塗装加熱後の強度が求め
られている。しかしながら連続焼鈍設備での溶体化が不
十分であるために低温・短時間での焼付け効果が小さ
い。
The above 6000 series alloys have relatively good press formability and can obtain high strength after baking coating, and thus have been conventionally applied to outer panel materials of automobiles.
The heat treatment type aluminum alloy sheet material used for such a purpose is usually subjected to solution treatment by continuous annealing equipment. However, in this conventional method, since the holding time at the solution temperature is short, the solution may not be sufficiently solutionized. The conventional paint baking temperature for automobiles was 180 ° C for about 1 hour, but there is a tendency for the paint baking temperature to be lower and shorter, so high strength after baking is required. However, since the solution treatment in the continuous annealing equipment is insufficient, the baking effect at low temperature and in a short time is small.

【0004】[0004]

【課題を解決するための手段】本発明はこれに鑑み種々
検討の結果、連続焼鈍設備での溶体化を容易にし、高い
焼付け硬化性を有する焼付け硬化性成形用アルミニウム
合金板の製造方法を開発したものである。
As a result of various studies in view of the above, the present invention has developed a method for producing a bake hardenable aluminum alloy sheet for bake hardenability, which facilitates solution treatment in continuous annealing equipment and has a high bake hardenability. It was done.

【0005】即ち本発明製造方法の一つは、Si 0.2〜
3.0wt%(以下wt%を%と略記),Mg 0.2〜 3.0%を
含み、残部Alと不可避的不純物からなるアルミニウム
合金を、熱間圧延又は冷間圧延後に 480℃以上の熱処理
を施し、更に冷間圧延を施してから 400℃以上の溶体化
処理を行い、3℃/sec以上の冷却速度で冷却することを
特徴とするものである。
That is, one of the manufacturing methods of the present invention is that Si 0.2-
An aluminum alloy containing 3.0 wt% (hereinafter wt% is abbreviated as%) and Mg 0.2 to 3.0% and the balance Al and unavoidable impurities is subjected to heat treatment at 480 ° C. or higher after hot rolling or cold rolling, and further, It is characterized in that after cold rolling, solution treatment is performed at 400 ° C or higher and cooling is performed at a cooling rate of 3 ° C / sec or higher.

【0006】また本発明製造方法の他の一つは、Si
0.2〜 3.0%,Mg 0.2〜 3.0%,Cu0.01〜 1.5%を
含み、残部Alと不可避的不純物からなるアルミニウム
合金を、熱間圧延又は冷間圧延後に 480℃以上の熱処理
を施し、更に冷間圧延を施してから 400℃以上の溶体化
処理を行い、3℃/sec以上の冷却速度で冷却することを
特徴とするものである。
Another one of the manufacturing methods of the present invention is Si
An aluminum alloy containing 0.2 to 3.0%, Mg 0.2 to 3.0%, Cu 0.01 to 1.5%, and the balance Al and unavoidable impurities is subjected to heat treatment at 480 ° C or higher after hot rolling or cold rolling, and further cooling. It is characterized by performing solution treatment at 400 ° C or higher after hot rolling and cooling at a cooling rate of 3 ° C / sec or higher.

【0007】また本発明製造方法の他の一つは、Si
0.2〜 3.0%,Mg 0.2〜 3.0%,Fe0.01〜0.25%を
含み,更にMn0.01〜 0.3%,Cr0.01〜 0.5%,Zr
0.01〜 0.5%,Ti0.01〜 0.5%,Ni0.01〜 0.3%の
うち1種又は2種以上を合計0.01〜 1.0%を含み、残部
Alと不可避的不純物からなるアルミニウム合金を、熱
間圧延又は冷間圧延後に 480℃以上の熱処理を施し、更
に冷間圧延を施してから 400℃以上の溶体化処理を行
い、3℃/sec以上の冷却速度で冷却することを特徴とす
るものである。
Another one of the manufacturing methods of the present invention is Si
0.2-3.0%, Mg 0.2-3.0%, Fe0.01-0.25%, Mn0.01-0.3%, Cr0.01-0.5%, Zr
An aluminum alloy containing 0.01 to 0.5%, 0.01 to 0.5%, and 0.01 to 0.3% of Ni, 0.01 to 0.3%, and 0.01 to 1.0% in total, and the balance Al and inevitable impurities are hot-rolled. Alternatively, it is characterized in that after cold rolling, heat treatment is performed at 480 ° C or higher, and further cold rolling is performed, then solution treatment is performed at 400 ° C or higher, and cooling is performed at a cooling rate of 3 ° C / sec or higher. ..

【0008】更に本発明製造方法の他の一つは、Si
0.2〜 3.0%,Mg 0.2〜 3.0%,Cu0.01〜 1.5%,
Fe0.01〜0.25%を含み,更にMn0.01〜 0.3%,Cr
0.01〜 0.5%,Zr0.01〜 0.5%,Ti0.01〜 0.5%,
Ni0.01〜 0.3%のうち1種又は2種以上を合計0.01〜
1.0%を含み、残部Alと不可避的不純物からなるアル
ミニウム合金を、熱間圧延又は冷間圧延後に 480℃以上
の熱処理を施し、更に冷間圧延を施してから 400℃以上
の溶体化処理を行い、3℃/sec以上の冷却速度で冷却す
ることを特徴とするものである。
Still another one of the manufacturing methods of the present invention is Si
0.2-3.0%, Mg 0.2-3.0%, Cu 0.01-1.5%,
Fe0.01-0.25%, Mn0.01-0.3%, Cr
0.01-0.5%, Zr0.01-0.5%, Ti0.01-0.5%,
Ni 0.01 to 0.3% of one or two or more total 0.01 to
Aluminum alloy containing 1.0% and balance Al and unavoidable impurities is hot-rolled or cold-rolled, then heat-treated at 480 ° C or higher, then cold-rolled, and then solution-treated at 400 ° C or higher. It is characterized by cooling at a cooling rate of 3 ° C./sec or more.

【0009】[0009]

【作用】本発明製造方法において、合金組成を上記の如
く限定したのは、次の理由によるものである。Siは焼
付け塗装時にMgと共にMg2 Siを析出させて強度を
向上させる。しかしてその添加量を 0.2〜 3.0%と限定
したのは、 0.2%未満ではその効果が小さく、 3.0%を
越えると溶体化処理後の成形性を低下するためである。
In the manufacturing method of the present invention, the alloy composition is limited as described above for the following reason. Si precipitates Mg 2 Si together with Mg during baking coating to improve the strength. However, the addition amount is limited to 0.2 to 3.0% because if it is less than 0.2%, its effect is small, and if it exceeds 3.0%, the formability after solution treatment deteriorates.

【0010】Mgは溶体化処理後にマトリックス中に固
溶しており、成形性の向上に寄与し、また焼付け塗装時
にSiと共にMg2 Siを析出させて強度を向上する。
しかしてその添加量を 0.2〜 3.0%と限定したのは、
0.2%未満ではその効果が小さく、 3.0%を越えると溶
体化処理後の成形性を低下するためである。
Since Mg is a solid solution in the matrix after the solution treatment, it contributes to the improvement of formability and also precipitates Mg 2 Si together with Si during baking coating to improve the strength.
The reason why the addition amount is limited to 0.2-3.0% is
If it is less than 0.2%, the effect is small, and if it exceeds 3.0%, the formability after solution treatment is deteriorated.

【0011】このようにSiとMgは焼付け塗装時にM
2 Siとして析出し、強度を向上させる。しかしてこ
の両元素の存在比が異なるとその焼付け硬化性も異な
り、SiとMgの重量比がSi> 0.6Mg(%)と、M
2 Si量に対して過剰Siであれば、より優れた焼付
け硬化性が得られる。尚焼付け塗装時の時効挙動をコン
トロールするためにAg,Cdなどを添加しても本発明
の効果を損なうことはない。
As described above, Si and Mg are M during baking coating.
It precipitates as g 2 Si and improves the strength. However, if the abundance ratios of these two elements are different, the bake hardenability is also different.
If the amount of Si is excessive with respect to the amount of g 2 Si, more excellent bake hardenability can be obtained. It should be noted that addition of Ag, Cd, etc. to control the aging behavior during baking coating does not impair the effects of the present invention.

【0012】Cuは焼付け塗装時にGPゾーン,θ´,
S相などを析出して強度を向上させる。しかしてその添
加量を0.01〜 1.5%と限定したのは、0.01%未満では強
度向上が小さく、 1.5%を越えると耐食性が低下するば
かりか焼入れ感受性が高くなりすぎるためである。Fe
は通常Alの不純物として含まれているものである。し
かしFeはSiと化合物を作りやすく、0.25%を越えて
含まれると焼付け塗装時の強度向上を阻害する。一方0.
01%未満では、その効果が飽和し経済的にも不利であ
る。
Cu is used in the GP zone, θ ', and
Precipitation of S phase etc. improves the strength. The reason why the addition amount is limited to 0.01 to 1.5% is that if it is less than 0.01%, the strength is not improved so much, and if it exceeds 1.5%, not only the corrosion resistance decreases but also the quenching sensitivity becomes too high. Fe
Is usually contained as an impurity of Al. However, Fe easily forms a compound with Si, and if contained in excess of 0.25%, it hinders the improvement of strength during baking coating. Meanwhile 0.
If it is less than 01%, the effect is saturated and it is economically disadvantageous.

【0013】Mn,Cr,Zr,Ti,Niはそれぞれ
結晶粒の微細化、あるいはマトリックス強度を向上させ
るために添加される。しかしてそれぞれ下限未満では効
果が少なく、上限を越えると溶体化処理後の成形性を低
下する。またこれら元素の合計量が 1.0%を越えると溶
体化処理後の成形性を低下する。尚鋳造組織の微細化材
として通常添加されるBなどは 0.1%以下の添加であれ
ば本発明の効果を損なうことはない。
Mn, Cr, Zr, Ti and Ni are added to refine the crystal grains or improve the matrix strength. However, if it is less than the lower limit, the effect is small, and if it exceeds the upper limit, the formability after solution treatment is deteriorated. Further, if the total amount of these elements exceeds 1.0%, the formability after solution treatment deteriorates. If B or the like, which is usually added as a refinement material for the cast structure, is 0.1% or less, the effect of the present invention is not impaired.

【0014】次に本発明の製造工程について説明する。
本発明は上記組成のアルミニウム合金を常法により溶
解、DC鋳造により鋳塊とし、この鋳塊に均質化処理を
施した後、熱間圧延し、この熱間圧延後又は熱間圧延と
冷間圧延後に 480℃以上の熱処理を施し、さらに冷間圧
延を施してから400℃以上の溶体化処理を行い、3℃/se
c以上の冷却速度で冷却する。
Next, the manufacturing process of the present invention will be described.
The present invention melts an aluminum alloy having the above composition by a conventional method, forms an ingot by DC casting, homogenizes the ingot, and then hot-rolls the hot-rolled or hot-rolled and cold-rolled steel. After rolling, heat treatment at 480 ℃ or more, cold rolling, and solution heat treatment at 400 ℃ or more, 3 ℃ / se
Cool at a cooling rate of c or higher.

【0015】溶体化処理は、SiやMg等の添加元素を
一旦マトリックス中に固溶させ、この後の焼付け塗装加
熱時に微細なMg2 Si等の化合物を析出させ、強度を
向上させる。このため熱間圧延後、または冷間圧延後に
480℃以上の熱処理を行い、溶体化処理前のSi,Mg
系の化合物を細かく、少なくすることにより、短時間の
溶体化処理での固溶を容易にする。ここで加熱温度を 4
80℃以上としたのは、480℃未満ではSi,Mgの析出
により化合物の粗大化が進行し、速やかな溶体化処理が
困難となり、焼付け塗装加熱後の強度向上が不十分とな
る。尚保持時間,冷却速度は特に規定されないが、保持
時間は1時間以上であり、冷却速度は3℃/sec以上であ
ることが好ましい。
In the solution treatment, additional elements such as Si and Mg are once solid-solved in the matrix, and fine compounds such as Mg 2 Si are precipitated during the subsequent baking and heating to improve the strength. Therefore, after hot rolling or cold rolling
Si, Mg before solution treatment after heat treatment at 480 ℃
By making the compound of the system fine and small, solid solution in a solution treatment for a short time is facilitated. Where the heating temperature is 4
The reason why the temperature is set to 80 ° C. or higher is that if the temperature is lower than 480 ° C., coarsening of the compound proceeds due to precipitation of Si and Mg, and rapid solution treatment becomes difficult, resulting in insufficient strength improvement after baking and heating. The holding time and the cooling rate are not particularly specified, but the holding time is preferably 1 hour or more and the cooling rate is preferably 3 ° C./sec or more.

【0016】溶体化処理温度を 400℃以上としたのは、
400℃未満では添加元素を充分に固溶させることができ
ず、焼付け塗装加熱時の強度向上が小さい。尚保持時間
は特に規定されないが、 400℃以上となる時間が5秒以
上であることが好ましい。溶体化処理後の冷却速度を3
℃/sec以上としたのは、3℃/sec未満の冷却速度では粗
大な化合物が析出してくるので、成形性の低下、及び焼
付け塗装加熱後の強度向上が小さくなるためである。
The solution treatment temperature is set to 400 ° C. or higher because
If the temperature is less than 400 ° C, the additional elements cannot be sufficiently solid-dissolved, and the improvement in strength during baking and baking is small. The holding time is not particularly specified, but the time at which the temperature is 400 ° C. or higher is preferably 5 seconds or longer. Cooling rate after solution treatment is 3
C./sec. Or more is because a coarse compound is precipitated at a cooling rate of less than 3.degree. C./sec, so that the formability is lowered and the improvement in strength after baking is reduced.

【0017】[0017]

【実施例】以下本発明を実施例について説明する。表1
に示す組成のアルミニウム合金を常法により溶解、DC
鋳造により鋳塊とし、この鋳塊に均質化処理を施した
後、熱間圧延により厚さ7mmの板材とした。この板材に
表2に示す圧延率で冷間圧延を施し、同じく表2に示す
条件の加熱処理と冷間圧延を施して厚さ1mmの板材とし
た。さらにこの板材を表2に示す条件で溶体化処理を施
して表2に示す速度で冷却した。
EXAMPLES The present invention will be described below with reference to examples. Table 1
The aluminum alloy of the composition shown in Figure 3
The ingot was cast to obtain an ingot, and the ingot was subjected to a homogenization treatment and then hot rolled into a plate material having a thickness of 7 mm. This plate material was cold-rolled at the rolling rate shown in Table 2, and also heat-treated and cold-rolled under the conditions shown in Table 2 to obtain a plate material having a thickness of 1 mm. Further, this plate material was subjected to solution treatment under the conditions shown in Table 2 and cooled at the rate shown in Table 2.

【0018】このようにして製造した板材について、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ミュレートした 1
50℃, 180℃, 200℃でそれぞれ 60minの加熱処理を施
した後に引張試験を行った。これらの結果を表3に示
す。引張試験はJIS5号試験片により、引張強さ,耐
力,伸びを測定した。エリクセン張出試験はJIS Z2247A
法により張出し高さを測定した。限界深絞り(LDR)
試験は直径33mm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。
A tensile test, an Erichsen bulge test, and a limit deep drawing (LDR) test were conducted on the plate material thus manufactured. Also simulated the baking coating process 1
Tensile tests were conducted after heat treatment at 50 ° C, 180 ° C, and 200 ° C for 60 minutes each. The results are shown in Table 3. In the tensile test, tensile strength, proof stress and elongation were measured using JIS No. 5 test pieces. Erichsen overhang test is JIS Z2247A
The overhang height was measured by the method. Limit deep drawing (LDR)
In the test, a blank coated with lubricating oil was deep-drawn with a punch having a diameter of 33 mm, and the maximum blank diameter without breaking was divided by the punch diameter to obtain a value.

【0019】[0019]

【表1】 [Table 1]

【0020】[0020]

【表2】 [Table 2]

【0021】[0021]

【表3】 [Table 3]

【0022】表3より明らかなように本発明製造法(N
o.1〜No.10)での板材は、従来製造法(No.21)に対
して溶体化処理後の成形性と、焼付け塗装処理後の強度
のいずれにおいても優れている。一方本発明の条件を外
れた比較製造法(No.11〜No.20)による板材は、上記
のいずれか1つ以上が劣っていることが判る。
As is clear from Table 3, the production method (N
The plate materials of No. 1 to No. 10) are superior to the conventional manufacturing method (No. 21) both in formability after solution treatment and strength after baking coating treatment. On the other hand, it can be seen that the plate materials according to the comparative manufacturing method (No. 11 to No. 20) that deviates from the conditions of the present invention are inferior in any one or more of the above.

【0023】[0023]

【発明の効果】このように本発明によれば、高い焼付け
硬化性を有する成形用アルミニウム合金板材を得ること
ができるもので工業上顕著な効果を奏する。
As described above, according to the present invention, an aluminum alloy sheet material for molding having a high bake hardenability can be obtained, and a remarkable effect is industrially exhibited.

───────────────────────────────────────────────────── フロントページの続き (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 (72)発明者 渡辺 元 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) Kunihiko Kishino 2-6-1, Marunouchi, Chiyoda-ku, Tokyo Furukawa Aluminum Co., Ltd. (72) Inventor Gen Watanabe 2-6-1, Marunouchi, Chiyoda-ku, Tokyo Furukawa Aluminum Co., Ltd.

Claims (4)

【特許請求の範囲】[Claims] 【請求項1】 Si 0.2〜 3.0wt%,Mg 0.2〜 3.0wt
%を含み、残部Alと不可避的不純物からなるアルミニ
ウム合金を、熱間圧延又は冷間圧延後に 480℃以上の熱
処理を施し、更に冷間圧延を施してから 400℃以上の溶
体化処理を行い、3℃/sec以上の冷却速度で冷却するこ
とを特徴とする焼付け硬化性成形用アルミニウム合金板
の製造方法。
1. Si 0.2-3.0 wt%, Mg 0.2-3.0 wt
%, Aluminum alloy consisting of balance Al and unavoidable impurities is subjected to heat treatment at 480 ° C. or higher after hot rolling or cold rolling, and further cold rolling is performed, and then solution treatment is performed at 400 ° C. or more, A method for producing a bake-hardenable aluminum alloy sheet for forming, which comprises cooling at a cooling rate of 3 ° C./sec or more.
【請求項2】 Si 0.2〜 3.0wt%,Mg 0.2〜 3.0wt
%,Cu0.01〜 1.5wt%を含み、残部Alと不可避的不
純物からなるアルミニウム合金を、熱間圧延又は冷間圧
延後に 480℃以上の熱処理を施し、更に冷間圧延を施し
てから 400℃以上の溶体化処理を行い、3℃/sec以上の
冷却速度で冷却することを特徴とする焼付け硬化性成形
用アルミニウム合金板の製造方法。
2. Si 0.2-3.0 wt%, Mg 0.2-3.0 wt
%, Cu 0.01 to 1.5 wt%, and aluminum alloy consisting of balance Al and unavoidable impurities, hot-rolled or cold-rolled, then heat-treated at 480 ° C. or higher, and then cold-rolled at 400 ° C. A method for producing a bake-hardenable aluminum alloy sheet for forming, which comprises performing the above solution treatment and cooling at a cooling rate of 3 ° C./sec or more.
【請求項3】 Si 0.2〜 3.0wt%,Mg 0.2〜 3.0wt
%,Fe0.01〜0.25wt%を含み、更にMn0.01〜 0.3wt
%,Cr0.01〜 0.5wt%,Zr0.01〜 0.5wt%,Ti0.
01〜 0.5wt%,Ni0.01〜 0.3wt%のうち1種又は2種
以上を合計0.01〜 1.0wt%を含み、残部Alと不可避的
不純物からなるアルミニウム合金を、熱間圧延又は冷間
圧延後に 480℃以上の熱処理を施し、更に冷間圧延を施
してから 400℃以上の溶体化処理を行い、3℃/sec以上
の冷却速度で冷却することを特徴とする焼付け硬化性成
形用アルミニウム合金板の製造方法。
3. Si 0.2-3.0 wt%, Mg 0.2-3.0 wt
%, Fe 0.01 to 0.25 wt%, Mn 0.01 to 0.3 wt%
%, Cr 0.01 to 0.5 wt%, Zr 0.01 to 0.5 wt%, Ti0.
An aluminum alloy containing 0.01 to 1.0 wt% of 01 to 0.5 wt% and 0.01 to 0.3 wt% of Ni and 0.01 to 1.0 wt% in total, and the balance Al and unavoidable impurities are hot-rolled or cold-rolled. A bake-hardening aluminum alloy characterized by being heat-treated at 480 ° C or higher, cold-rolled, then solution-treated at 400 ° C or higher, and cooled at a cooling rate of 3 ° C / sec or higher. Method of manufacturing a plate.
【請求項4】 Si 0.2〜 3.0wt%,Mg 0.2〜 3.0wt
%,Cu0.01〜 1.5wt%,Fe0.01〜0.25wt%を含み、
更にMn0.01〜 0.3wt%,Cr0.01〜 0.5wt%,Zr0.
01〜 0.5wt%,Ti0.01〜 0.5wt%,Ni0.01〜 0.3wt
%のうち1種又は2種以上を合計0.01〜 1.0wt%を含
み、残部Alと不可避的不純物からなるアルミニウム合
金を、熱間圧延又は冷間圧延後に 480℃以上の熱処理を
施し、更に冷間圧延を施してから 400℃以上の溶体化処
理を行い、3℃/sec以上の冷却速度で冷却することを特
徴とする焼付け硬化性成形用アルミニウム合金板の製造
方法。
4. Si 0.2-3.0 wt%, Mg 0.2-3.0 wt
%, Cu 0.01 to 1.5 wt%, Fe 0.01 to 0.25 wt%,
Furthermore, Mn0.01-0.3wt%, Cr0.01-0.5wt%, Zr0.
01-0.5wt%, Ti0.01-0.5wt%, Ni0.01-0.3wt
% Or more of 0.01% to 1.0% by weight in total, and aluminum alloy consisting of balance Al and unavoidable impurities is subjected to heat treatment at 480 ° C. or higher after hot rolling or cold rolling, and then cold A method for producing a bake-hardenable aluminum alloy sheet for forming, which comprises subjecting a solution treatment to 400 ° C or more after rolling, and cooling at a cooling rate of 3 ° C / sec or more.
JP3555392A 1992-01-27 1992-01-27 Manufacture of baking hardenability aluminum alloy sheet for forming Pending JPH05202454A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3555392A JPH05202454A (en) 1992-01-27 1992-01-27 Manufacture of baking hardenability aluminum alloy sheet for forming

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3555392A JPH05202454A (en) 1992-01-27 1992-01-27 Manufacture of baking hardenability aluminum alloy sheet for forming

Publications (1)

Publication Number Publication Date
JPH05202454A true JPH05202454A (en) 1993-08-10

Family

ID=12444922

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3555392A Pending JPH05202454A (en) 1992-01-27 1992-01-27 Manufacture of baking hardenability aluminum alloy sheet for forming

Country Status (1)

Country Link
JP (1) JPH05202454A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT407533B (en) * 1999-01-22 2001-04-25 Aluminium Lend Gmbh ALUMINUM ALLOY

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT407533B (en) * 1999-01-22 2001-04-25 Aluminium Lend Gmbh ALUMINUM ALLOY

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