JPS58224142A - Aluminum alloy plate with superior formability and its manufacture - Google Patents

Aluminum alloy plate with superior formability and its manufacture

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Publication number
JPS58224142A
JPS58224142A JP10738182A JP10738182A JPS58224142A JP S58224142 A JPS58224142 A JP S58224142A JP 10738182 A JP10738182 A JP 10738182A JP 10738182 A JP10738182 A JP 10738182A JP S58224142 A JPS58224142 A JP S58224142A
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JP
Japan
Prior art keywords
aluminum alloy
alloy
rolling
less
temperature
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP10738182A
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Japanese (ja)
Other versions
JPS6140299B2 (en
Inventor
Makoto Tsuchida
信 土田
Kazuhiro Hanaki
花木 和弘
Atsunori Fuse
布施 篤則
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.)
Nippon Steel Corp
Sumitomo Light Metal Industries Ltd
Original Assignee
Sumitomo Light Metal Industries Ltd
Sumitomo Metal Industries Ltd
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Publication date
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Priority to JP10738182A priority Critical patent/JPS58224142A/en
Publication of JPS58224142A publication Critical patent/JPS58224142A/en
Publication of JPS6140299B2 publication Critical patent/JPS6140299B2/ja
Granted legal-status Critical Current

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Abstract

PURPOSE:To obtain a fine-grained Al alloy plate with superior formability by single process annealing by subjecting an Al alloy having a specified composition after homogenizing to final cold rolling to a specified thickness at a specified draft. CONSTITUTION:An Al alloy contg. two or more among 0.1-0.7% Si, 0.3-1.0% Fe, 0.3-1.5% Mn and 0.01-2.0% Mg is homogenized. The alloy is cold rolled at about 480-580 deg.C starting temp. and >= about 290 deg.C finishing temp., optionally cold rolled, and annealed at about 400-570 deg.C for <=5min. It is then subjected to final cold rolling to <=0.3mm. thickness at >=20% draft. The grain size can be made as fine as <=25mum, so the workability can be improved. Since process annealing is required only once, energy necessary for the heat treatment and the cost are reduced.

Description

【発明の詳細な説明】 本発明は、例えばキャンプ用合金板の如く深絞り成形性
にすぐれ、低い耳率と適度な強度を有するアルミニウム
合金板およびその製造方法に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an aluminum alloy plate, such as an alloy plate for camping, which has excellent deep drawability, a low selvage ratio, and appropriate strength, and a method for manufacturing the same.

従来、上記深絞り成形用の如−きアルミニウム合金板に
おける諸物件を得るためには、造塊−十分な均質化処理
−熱間圧延−(冷間圧延)−中間焼鈍一冷間圧延一中間
焼鈍一冷間圧延の各工程を組み、均質化および2回以上
の中間焼鈍によって、十分長時間の加熱を加えている。
Conventionally, in order to obtain various objects in aluminum alloy sheets such as those for deep drawing, the following steps have been carried out: ingot formation, sufficient homogenization treatment, hot rolling, (cold rolling), intermediate annealing, cold rolling, and intermediate rolling. Each step of annealing and cold rolling is combined, and heating is applied for a sufficiently long time by homogenization and two or more intermediate annealing steps.

かかる従来法では、長時間の中間焼鈍を加えるために合
金板の結晶粒は50〜100μmの大きさになっている
。このように結晶粒が大きくなると成形性が低下し、特
に0.3 tm厚以下の薄板の成形性を向上させるため
には結晶粒をさらに小さくする必要がある。又、2回以
上の中間焼鈍は、できれば1回にした方が、工程の簡略
化並びに省エネルギの見地から望ましいことである。す
なわち、中間焼鈍は1回とし、しかもその1回の中間焼
鈍で結晶粒を細かくして、成形性並びに耳率が従来材と
同程度以上になるようにすることが有意義である。
In this conventional method, the crystal grains of the alloy plate have a size of 50 to 100 μm due to the addition of a long intermediate annealing. When the crystal grains become large as described above, the formability deteriorates, and in order to particularly improve the formability of thin plates with a thickness of 0.3 tm or less, it is necessary to further reduce the crystal grains. Further, it is preferable to carry out intermediate annealing once, rather than twice or more, from the viewpoint of process simplification and energy saving. That is, it is meaningful to carry out intermediate annealing once, and to refine the crystal grains in this single intermediate annealing so that the formability and selvage ratio are at least the same as those of conventional materials.

本発明は、以上の観点に基づいて発明されたもので、そ
の第1発明は、Sj O81〜0.7%、Fe 0.3
〜1.0%、Mn 0.3〜1.5 %、Mg 0.0
1〜2.0%のうちの2種以上を含むアルミニウム合金
よりなり、20q6以上の最終冷間圧延を行なって板厚
0.3配以下とした場合の結晶粒径が25μm以下であ
ることを特徴とする成形性のすぐれたアルミニウム合金
板である。
The present invention was invented based on the above viewpoints, and the first invention is Sj O81-0.7%, Fe 0.3
~1.0%, Mn 0.3-1.5%, Mg 0.0
Made of an aluminum alloy containing two or more of the following: This is an aluminum alloy plate with excellent formability.

Si、Mgは強度と成形性を付与し、Fe XMnは強
度を与えかつ深絞シ加工において発生する耳の大きさを
制御する効果を有する。各成分と′□     も上限
を越えると成形加工性を低下させるので好ましくない。
Si and Mg provide strength and formability, and FeXMn provides strength and has the effect of controlling the size of ears that occur during deep drawing. Exceeding the upper limits of each component and '□ is not preferable because it reduces moldability.

又、下限を有するものは下限より少ないと効果が小さい
Moreover, if the amount has a lower limit, the effect will be small if the amount is less than the lower limit.

かかる組成のものは所定の工程により20%以上の最終
冷間圧延を行なって板厚0.3111111以下とした
場合、結晶粒径が25μm以下となし得て、成形性にす
ぐれたものである。
When such a composition is subjected to a final cold rolling of 20% or more in a predetermined process to have a thickness of 0.3111111 or less, the crystal grain size can be reduced to 25 μm or less, and it has excellent formability.

かかる成形性のすぐれたアルミニウム合金板は、第2発
明によって得られる。す々ゎち、その第2発明は、Si
0.1−0.7%、F’e O,3〜1.0%、Mn 
0.3〜1.5 %、Mg0.01〜2.O%のうち2
種以上を含むアルミニウム合金を均質化処理したのち、
480〜580℃で熱間圧延を開始して290℃以上で
熱間圧延を終了し、必要に応じて冷間圧延したのち、4
oo〜570℃で5分以下の焼鈍処理を行ない、20%
以上の最終冷間圧延を行ない結晶粒径を25μm以下と
することを特徴とする成形性のすぐれたアルミニウム合
金板の製造方法である。
Such an aluminum alloy plate with excellent formability is obtained by the second invention. Susuwachi, the second invention is Si
0.1-0.7%, F'e O, 3-1.0%, Mn
0.3-1.5%, Mg0.01-2. 2 out of 0%
After homogenizing an aluminum alloy containing more than one species,
After starting hot rolling at 480 to 580°C, finishing hot rolling at 290°C or higher, and performing cold rolling as necessary, 4
Annealing treatment at oo~570℃ for 5 minutes or less, 20%
This is a method for producing an aluminum alloy sheet with excellent formability, which is characterized in that the final cold rolling described above is carried out to reduce the crystal grain size to 25 μm or less.

まず均質化処理は、合金板の耳率を変化させる要因の一
つであり、一般には融解温度直下のできるだけ高温で行
なうが、必要十分な時間に止める。0.5%以上の地を
含む合金及び0.3俤以上のFeを含む合金は、560
℃以上で8時間以上均質化処理する必要があるが、陶と
Siを主に含む合金ではこれより低温短時間でよい。
First, homogenization treatment is one of the factors that changes the selvage ratio of the alloy plate, and is generally performed at as high a temperature as possible, just below the melting temperature, but for a sufficient period of time. Alloys containing 0.5% or more of Fe and alloys containing 0.3% or more of Fe are 560
Although it is necessary to homogenize at a temperature of 8° C. or higher for 8 hours or more, an alloy containing mainly ceramic and Si may require a lower temperature and a shorter time.

又、耳率を制御するため2段加熱を行なう場合もある。Further, two-stage heating may be performed to control the selvage ratio.

熱間圧延は均質化処理後冷却し、再加熱して行なっても
良い。その場合は、冷却再加熱中に起る鋳塊組織の変化
が耳率に影響を与えるので、均質化処理後引きつづいて
熱間圧延する場合と加熱温度が異なる場合がある。
Hot rolling may be performed by cooling after homogenization treatment and then reheating. In that case, changes in the structure of the ingot during cooling and reheating affect the selvage ratio, so the heating temperature may be different from that in the case of subsequent hot rolling after homogenization treatment.

熱間圧延終了時の材料温度は、材料が再結晶するのに十
分な高温でなければならない。通常の条件で500℃か
ら熱間圧延して3簡厚板にすると、温度は260〜28
0℃になる。そこで、圧延開始温度、圧下率、バス数、
圧延速度、潤滑油温度等に工夫を加えて、熱間圧延終了
温度を290℃以上、より好ましくは310℃以上に々
るようにする。
The material temperature at the end of hot rolling must be high enough to recrystallize the material. When hot-rolled from 500℃ under normal conditions into a 3-piece thick plate, the temperature is 260-28℃.
It becomes 0℃. Therefore, rolling start temperature, reduction rate, number of baths,
The rolling speed, lubricating oil temperature, etc. are adjusted so that the hot rolling end temperature is 290°C or higher, more preferably 310°C or higher.

このことは、耳率を制御すると同時に、圧延後進行する
合金成分の析出が最終板の加工性を向上させる効果をも
つため、最も重要な条件である。
This is the most important condition because it controls the selvedge ratio and at the same time, the precipitation of alloy components that progresses after rolling has the effect of improving the workability of the final plate.

本発明の合金板の目的とする用途に用いられる最終板の
多くは0.4 tarn を以下で最終冷間圧延量が2
0〜60チであるから、通常け1mt以下で中間焼鈍す
ることとなり、熱間圧延工程に次ぐ冷間圧延工程は必要
である。ただし、最終板厚が0.4 mm tよしも大
きい場合には、冷間圧延工程は必要がない。したがって
、冷間圧延工程は必要に応じて行なう。
Most of the final sheets used for the intended use of the alloy sheet of the present invention have a final cold rolling amount of 0.4 tar or less and a final cold rolling amount of 2.
Since the thickness is 0 to 60 inches, intermediate annealing is usually performed at a thickness of 1 mt or less, and a cold rolling process is required following the hot rolling process. However, if the final plate thickness is 0.4 mm, the cold rolling process is not necessary. Therefore, the cold rolling process is performed as necessary.

つづく焼鈍は、加工性向上のために高温で短時間性なう
。工業的にはコイル状に巻かれた板をほどきながら高温
の炉内を通過させて加熱焼鈍する。焼鈍温度が400℃
未満では再結晶が進みに<<、再結晶に長時間を要する
ことになり効果が薄れる。焼鈍温度の最高はその材料の
融点である。又、温度が高いときの結晶粒の成長を避け
るだめには処理時間を短かくしなければならず、5分以
下とする必要がある。
The subsequent annealing is performed at high temperature for a short time to improve workability. Industrially, a coiled plate is unwound and passed through a high-temperature furnace for heat annealing. Annealing temperature is 400℃
If it is less than <<, recrystallization progresses and recrystallization takes a long time, resulting in a weakened effect. The maximum annealing temperature is the melting point of the material. Furthermore, in order to avoid the growth of crystal grains when the temperature is high, the treatment time must be shortened, and must be 5 minutes or less.

最終冷間圧延は20%以上特に20%〜6゜チが最適で
ある。20%未満では強度が十分に発揮されず、又60
%以上では物によって加工性が低下することがある。
The optimum final cold rolling is 20% or more, especially 20% to 6°. If it is less than 20%, the strength will not be sufficiently exhibited, and if the
% or more, workability may deteriorate depending on the material.

さらに、嵐を含む合金板は室温放置により材料強度が低
下することがあるので、予め再結晶温度以下で安定化の
熱処理を加えることがある。
Furthermore, since the material strength of an alloy plate containing Arashi may decrease when left at room temperature, it may be subjected to stabilizing heat treatment at a temperature below the recrystallization temperature in advance.

以上の各工程を経ることによって第2発明では結晶粒径
を25μm以下と微細化することができ加工性を向上す
る。しかも中間焼鈍が1回ですむので熱処理に要するエ
ネルギコストを低減し、さらに製造工程の短縮による仕
掛コストの低減をはかることもできる。
By going through each of the above steps, in the second invention, the crystal grain size can be reduced to 25 μm or less, and workability is improved. Moreover, since intermediate annealing only needs to be performed once, the energy cost required for heat treatment can be reduced, and it is also possible to reduce in-process costs by shortening the manufacturing process.

つぎに実施例並びに比較例について説明する。Next, examples and comparative examples will be explained.

実施例1 Si0.65%、Fe0.82%、Cu O,04%、
Mn 0.01%、Mg 0.01%、Zn0.01%
、Ti、a   0.0”・At″”!J l a&!
a#jJl[FIJ L・580℃で10時間均質化し
て、540℃に冷却し、直ちに熱間圧延して2.8 w
m tとした。このときの圧延終了時の材料温度は32
0℃である。これを冷間加工して0.33IOItとし
、540℃で5秒間熱処理を加えて、30チの最終冷間
加工して0.23關t としだ。
Example 1 Si0.65%, Fe0.82%, CuO,04%,
Mn 0.01%, Mg 0.01%, Zn 0.01%
, Ti, a 0.0”・At””! J l a&!
a#jJl[FIJ L・Homogenized at 580°C for 10 hours, cooled to 540°C, and immediately hot rolled to 2.8 w
m t. At this time, the material temperature at the end of rolling was 32
It is 0°C. This was cold worked to 0.33 IOIt, heat treated at 540°C for 5 seconds, and finally cold worked to 30 inches to 0.23IOIt.

得られた0、23mmt板の特性は表に示す通りで、製
造過程で加える熱エネルギが少ないにもかかわらず、成
形性は向上している。
The properties of the obtained 0.23 mmt plate are as shown in the table, and the formability is improved despite the fact that less heat energy is applied during the manufacturing process.

比較例1 実施例1における合金鋳塊を580℃で10時間均質化
し、冷却、固剤を経て520℃に再加熱し、熱間圧延し
て5mtとし、400℃で1時間中間焼鈍したのち、冷
間圧延して0.33wqt とし、再び400℃で1時
間中間焼鈍を加えて、30%の最終冷間圧延をして0.
23mmtO板とした。この板の特性を表に示す。
Comparative Example 1 The alloy ingot in Example 1 was homogenized at 580°C for 10 hours, cooled, solidified, reheated to 520°C, hot rolled to 5 mt, and intermediately annealed at 400°C for 1 hour. Cold rolled to 0.33 wqt, intermediate annealed again at 400°C for 1 hour, and final cold rolled to 30% to 0.33 wqt.
A 23 mmtO plate was used. The characteristics of this board are shown in the table.

実施例2 SiO,15%、Fe O,54%、Cu O,12%
、Mn 0.4891=、Mg 0.80%、Cr 0
.01%、Ti0102%、At残 よりなる合金の鋳
塊を固剤し、590℃で5時間加熱後、温度を下げて5
40℃で5時間均質化し、直ちに熱間圧延して2.4M
tとした。このときの圧延終了時の材料温度は310℃
であった。これを冷間加工して0.29mt とし、4
50℃で20秒間熱処理を加えて、30チの最終冷間加
工をして0.20wnt板としだ。
Example 2 SiO, 15%, FeO, 54%, CuO, 12%
, Mn 0.4891=, Mg 0.80%, Cr 0
.. An ingot of an alloy consisting of 01% Ti, 102% Ti, and the remainder At was solidified and heated at 590°C for 5 hours, then lowered to 500°C.
Homogenized at 40℃ for 5 hours and immediately hot rolled to 2.4M
It was set as t. The material temperature at the end of rolling at this time is 310℃
Met. This was cold worked to 0.29mt, and 4
Heat treatment was applied at 50°C for 20 seconds, and final cold working of 30 inches was performed to form a 0.20wnt plate.

得られた0、20+emt根の特性は表に示すとおりで
、結晶粒が細かく々ることにより成形性が向上するが、
強度、耳率ば後記する比較例2のものと変りがない。
The properties of the obtained 0, 20 + emt roots are as shown in the table, and the formability is improved due to finer grains, but
The strength and selvage ratio are the same as those of Comparative Example 2, which will be described later.

比較例2 実施例2における合金鋳塊を580℃で10時間均質化
し、冷却、固剤して、480℃に再加熱し、熱間圧延し
て6mmt とし、さらに冷間加工して2.5 tta
n t としてから、360℃で1時間中間焼鈍し、冷
間加工して0.29mmtとし、ここで再び360℃で
1時間中間焼鈍を加え、又、30チの最終冷間加工をし
て0.20mmt板とした。この板の特性を表に示す。
Comparative Example 2 The alloy ingot in Example 2 was homogenized at 580°C for 10 hours, cooled, solidified, reheated to 480°C, hot rolled to 6mmt, and further cold worked to 2.5mm. tta
nt, intermediate annealing at 360°C for 1 hour, cold working to 0.29mmt, intermediate annealing again at 360°C for 1 hour, and final cold working of 30 inches. .20mmt plate. The characteristics of this board are shown in the table.

実施例3 SiO,30%、F”e O,61%、Cu O,16
%、Mn 1.2%、Mg O,o 1 %、At残 
よりなる鋳塊を595℃で10時間均質化後、560℃
に冷却して熱間圧延して2.2 wry+ t とした
。このときの圧延終了時の拐料温度は332℃であった
Example 3 SiO, 30%, F”e O, 61%, Cu O, 16
%, Mn 1.2%, Mg O,o 1%, At remainder
After homogenizing the ingot at 595°C for 10 hours, the ingot was heated to 560°C.
It was cooled to 2.2 wry+t and hot rolled. At this time, the grain temperature at the end of rolling was 332°C.

これを冷間加工して0.31mmt とし、500℃で
10秒間の高速短時間焼鈍を加えてから、25チの最終
冷間加工をして0.23w+を板とした。
This was cold-worked to 0.31 mmt, subjected to high-speed short-time annealing at 500°C for 10 seconds, and then final cold-worked to 25 inches to form a 0.23W+ plate.

得られた0、23mt板の特性は表に示すとおりで、結
晶粒が細かくなり、絞り加工性が向上している。
The properties of the obtained 0.23 mt plate are as shown in the table, and the crystal grains are fine and the drawing workability is improved.

比較例3 実施例3における合金鋳塊を580℃で10時間均質化
し、冷却、固剤して、540℃に再加熱し、熱間圧延し
て3. Otan tとし、さらに冷間加工して1.5
mtとしてから、360〜380℃で1時間中間焼鈍し
、冷間加工して0.31TfnRtとし、再び360〜
380℃で1時間中間焼鈍を加え、25%の最終冷間加
工をして0.23w1t板とした。この板の特性を表に
示す。
Comparative Example 3 The alloy ingot in Example 3 was homogenized at 580°C for 10 hours, cooled, solidified, reheated to 540°C, and hot rolled. Otan t and further cold worked to 1.5
mt, intermediate annealing at 360-380°C for 1 hour, cold working to 0.31TfnRt, and then 360-380°C again.
An intermediate annealing was performed at 380° C. for 1 hour, and a final cold working of 25% was performed to obtain a 0.23w1t plate. The characteristics of this board are shown in the table.

実施例4 Si0.14%、Fe 0.35 %、CuO,06%
、Mn 0.35%、Mg1.55%、Cr O,02
%、Zn001%、Ti O,04%、At残よりなる
鋳塊を550℃で10時間均質化後、500℃で熱間圧
延して2. Orran tとしだ。このときの圧延終
了時の材料温度は298℃であった。これを冷間加工し
て0.6 mm tとし、500℃で60秒間の高速短
時間焼鈍を加えてから、58%の最終冷間加工をして0
.25mmt板としだ。
Example 4 Si0.14%, Fe 0.35%, CuO, 06%
, Mn 0.35%, Mg 1.55%, CrO,02
%, Zn001%, TiO,04%, At balance was homogenized at 550°C for 10 hours, and then hot rolled at 500°C. Orrant and Toshida. At this time, the material temperature at the end of rolling was 298°C. This was cold-worked to 0.6 mm t, high-speed short-time annealing at 500°C for 60 seconds, and then final cold-worked to 58% to 0.
.. Toshida 25mmt plate.

得られた0、25mmt板の特性は表に示すとおりで、
後記の比較例4では最終冷間圧延量に伴なって発達する
45−4方向耳率を小さくすることができなかったが、
本実施例では耳率を小さくすると同時に成形性が向上し
ている。
The properties of the obtained 0.25mmt plate are as shown in the table.
In Comparative Example 4 described later, it was not possible to reduce the 45-4 direction ear ratio that develops with the final cold rolling amount, but
In this example, the selvage ratio is reduced and at the same time the moldability is improved.

比較例4 実施例4における合金鋳塊を、固剤後550」 ℃で10時間均質化後、500℃に冷却して熱間圧延し
て3.0mmtとし、さらに冷間加工して0.6mmt
 としてから、360℃で1時間中間焼鈍を加えて、5
8係の最終冷間加工して0.25mmt板とした。この
板の特性を表に示す。
Comparative Example 4 The alloy ingot in Example 4 was solidified, homogenized at 550°C for 10 hours, cooled to 500°C, hot rolled to 3.0mmt, and further cold worked to 0.6mmt.
After that, intermediate annealing was performed at 360°C for 1 hour, and 5
The final cold working of Section 8 was made into a 0.25 mmt plate. The characteristics of this board are shown in the table.

Claims (1)

【特許請求の範囲】[Claims] (1)  Si 0.1〜0.7%、Fe O,3〜1
.0 %、Mn0.3〜1.5係、Mg0.01〜2.
0%のうちの2種以上を含むアルミニウム合金よりなり
、20チ以上の最終冷間圧延を行なって板厚0.3 w
+以下とした場合の結晶粒径が25μm以下であること
を特徴とする成形性のすぐれたアルミニウム合金板。 (21SiO,1〜0.7%、Fe O,3〜1.0%
、崗0、3〜1,5%、Mg 0.01〜2.0%のう
ち2種以上を含むアルミニウム合金を均質化処理したの
ち、480〜580℃で熱間圧延を開始して290℃以
上で熱間圧延を終了し、必要に応じて冷間圧延したのち
、400〜570℃で5分以下の焼鈍処理を行ない、2
0チ以上の最終冷間圧延を行ない結晶粒径を25μm以
下とすることを特徴とする成形性のすぐれたアルミニウ
ム合金板の製造方法。
(1) Si 0.1-0.7%, FeO, 3-1
.. 0%, Mn0.3-1.5, Mg0.01-2.
Made of an aluminum alloy containing two or more of the following:
An aluminum alloy plate with excellent formability, characterized in that the crystal grain size is 25 μm or less when the value is 25 μm or less. (21SiO, 1-0.7%, FeO, 3-1.0%
After homogenizing an aluminum alloy containing two or more of the following: 0.3% to 1.5% Mg and 0.01% to 2.0% Mg, hot rolling was started at 480°C to 580°C and then rolled to 290°C. After completing hot rolling and performing cold rolling as necessary, annealing treatment is performed at 400 to 570°C for 5 minutes or less, and
A method for producing an aluminum alloy sheet with excellent formability, which comprises performing a final cold rolling of 0 mm or more to have a crystal grain size of 25 μm or less.
JP10738182A 1982-06-22 1982-06-22 Aluminum alloy plate with superior formability and its manufacture Granted JPS58224142A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10738182A JPS58224142A (en) 1982-06-22 1982-06-22 Aluminum alloy plate with superior formability and its manufacture

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10738182A JPS58224142A (en) 1982-06-22 1982-06-22 Aluminum alloy plate with superior formability and its manufacture

Publications (2)

Publication Number Publication Date
JPS58224142A true JPS58224142A (en) 1983-12-26
JPS6140299B2 JPS6140299B2 (en) 1986-09-08

Family

ID=14457671

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10738182A Granted JPS58224142A (en) 1982-06-22 1982-06-22 Aluminum alloy plate with superior formability and its manufacture

Country Status (1)

Country Link
JP (1) JPS58224142A (en)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59193251A (en) * 1983-03-10 1984-11-01 Kobe Steel Ltd Preparation of aluminum alloy plate having deep drawing property
JPS59193253A (en) * 1983-03-31 1984-11-01 Kobe Steel Ltd Preparation of deep drawing aluminum alloy plate
JPS6144150A (en) * 1984-08-08 1986-03-03 Kobe Steel Ltd Aluminum sheet material for photosensitive drum and its manufacture
JPS61264149A (en) * 1985-05-15 1986-11-22 Kobe Steel Ltd Aluminum alloy sheet for can superior in formability
JPS6280256A (en) * 1985-10-01 1987-04-13 Sky Alum Co Ltd Manufacture of material for redrawn vessel
JPS62250144A (en) * 1986-04-21 1987-10-31 Showa Alum Corp Aluminum-alloy foil for package
JPS6326340A (en) * 1986-07-18 1988-02-03 Kobe Steel Ltd Manufacture of aluminum alloy having superior directional property
JPS6369953A (en) * 1986-09-11 1988-03-30 Kobe Steel Ltd Manufacture of aluminum alloy excellent in directionality
JPS63145758A (en) * 1987-11-07 1988-06-17 Kobe Steel Ltd Production of al alloy sheet for packaging
JPH01123045A (en) * 1987-11-06 1989-05-16 Sumitomo Light Metal Ind Ltd Aluminum sheet having superior formability and manufacture thereof
JPH01129688A (en) * 1987-11-16 1989-05-22 Mitsubishi Electric Corp Picture signal receiver
JPH01176048A (en) * 1987-12-29 1989-07-12 Kobe Steel Ltd Aluminum alloy for deep drawing having excellent orientation characteristics and its manufacture
JPH02274833A (en) * 1989-04-14 1990-11-09 Kobe Steel Ltd Aluminum alloy-soft material for supporting substrate and its manufacture
JP2000319741A (en) * 1998-09-10 2000-11-21 Kobe Steel Ltd Al-Mg-Si BASED ALLOY SHEET

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JP6688828B2 (en) * 2018-03-30 2020-04-28 株式会社神戸製鋼所 Aluminum alloy plate for automobile structural member, automobile structural member and method for manufacturing aluminum alloy plate for automobile structural member

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5111011A (en) * 1974-07-18 1976-01-28 Mitsubishi Aluminium FUKAJIBORYOARUMINIUMUGOKINPANNO SEIZOHOHO
JPS5273112A (en) * 1975-12-16 1977-06-18 Sumitomo Light Metal Ind Hard aluminium alloy plate for deep drawing and method of making thereof
JPS52105509A (en) * 1976-03-03 1977-09-05 Mitsubishi Aluminium Production of aluminium alloy sheet for deep drawing
JPS5432113A (en) * 1977-08-18 1979-03-09 Nitsukei Atsuen Kk Method of producing allmnnmg alloy hard plate having deep drawability
JPS56102562A (en) * 1980-01-11 1981-08-17 Kobe Steel Ltd Manufacture of al alloy plate for packing

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5111011A (en) * 1974-07-18 1976-01-28 Mitsubishi Aluminium FUKAJIBORYOARUMINIUMUGOKINPANNO SEIZOHOHO
JPS5273112A (en) * 1975-12-16 1977-06-18 Sumitomo Light Metal Ind Hard aluminium alloy plate for deep drawing and method of making thereof
JPS52105509A (en) * 1976-03-03 1977-09-05 Mitsubishi Aluminium Production of aluminium alloy sheet for deep drawing
JPS5432113A (en) * 1977-08-18 1979-03-09 Nitsukei Atsuen Kk Method of producing allmnnmg alloy hard plate having deep drawability
JPS56102562A (en) * 1980-01-11 1981-08-17 Kobe Steel Ltd Manufacture of al alloy plate for packing

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59193251A (en) * 1983-03-10 1984-11-01 Kobe Steel Ltd Preparation of aluminum alloy plate having deep drawing property
JPS59193253A (en) * 1983-03-31 1984-11-01 Kobe Steel Ltd Preparation of deep drawing aluminum alloy plate
JPS6160143B2 (en) * 1983-03-31 1986-12-19 Kobe Steel Ltd
JPH0413418B2 (en) * 1984-08-08 1992-03-09 Kobe Steel Ltd
JPS6144150A (en) * 1984-08-08 1986-03-03 Kobe Steel Ltd Aluminum sheet material for photosensitive drum and its manufacture
JPS61264149A (en) * 1985-05-15 1986-11-22 Kobe Steel Ltd Aluminum alloy sheet for can superior in formability
JPS6280256A (en) * 1985-10-01 1987-04-13 Sky Alum Co Ltd Manufacture of material for redrawn vessel
JPS62250144A (en) * 1986-04-21 1987-10-31 Showa Alum Corp Aluminum-alloy foil for package
JPS6326340A (en) * 1986-07-18 1988-02-03 Kobe Steel Ltd Manufacture of aluminum alloy having superior directional property
JPS6369953A (en) * 1986-09-11 1988-03-30 Kobe Steel Ltd Manufacture of aluminum alloy excellent in directionality
JPH0122346B2 (en) * 1986-09-11 1989-04-26 Kobe Steel Ltd
JPH01123045A (en) * 1987-11-06 1989-05-16 Sumitomo Light Metal Ind Ltd Aluminum sheet having superior formability and manufacture thereof
JPS63145758A (en) * 1987-11-07 1988-06-17 Kobe Steel Ltd Production of al alloy sheet for packaging
JPH01129688A (en) * 1987-11-16 1989-05-22 Mitsubishi Electric Corp Picture signal receiver
JPH01176048A (en) * 1987-12-29 1989-07-12 Kobe Steel Ltd Aluminum alloy for deep drawing having excellent orientation characteristics and its manufacture
JPH0366382B2 (en) * 1987-12-29 1991-10-17 Kobe Steel Ltd
JPH02274833A (en) * 1989-04-14 1990-11-09 Kobe Steel Ltd Aluminum alloy-soft material for supporting substrate and its manufacture
JPH0570696B2 (en) * 1989-04-14 1993-10-05 Kobe Steel Ltd
JP2000319741A (en) * 1998-09-10 2000-11-21 Kobe Steel Ltd Al-Mg-Si BASED ALLOY SHEET

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