JPH07180009A - Production of high strength aluminum alloy sheet for forming - Google Patents
Production of high strength aluminum alloy sheet for formingInfo
- Publication number
- JPH07180009A JPH07180009A JP34579593A JP34579593A JPH07180009A JP H07180009 A JPH07180009 A JP H07180009A JP 34579593 A JP34579593 A JP 34579593A JP 34579593 A JP34579593 A JP 34579593A JP H07180009 A JPH07180009 A JP H07180009A
- Authority
- JP
- Japan
- Prior art keywords
- rolling
- alloy
- ingot
- strength
- thickness
- 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
Links
- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 19
- 238000004519 manufacturing process Methods 0.000 title claims description 9
- 238000005096 rolling process Methods 0.000 claims abstract description 19
- 229910052802 copper Inorganic materials 0.000 claims abstract description 6
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 5
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 4
- 229910052726 zirconium Inorganic materials 0.000 claims abstract description 4
- 238000000265 homogenisation Methods 0.000 claims description 10
- 238000000034 method Methods 0.000 claims description 9
- 238000005098 hot rolling Methods 0.000 abstract description 15
- 229910045601 alloy Inorganic materials 0.000 abstract description 12
- 239000000956 alloy Substances 0.000 abstract description 12
- 238000010438 heat treatment Methods 0.000 abstract description 4
- 238000007670 refining Methods 0.000 abstract description 2
- 230000001105 regulatory effect Effects 0.000 abstract description 2
- 229910018134 Al-Mg Inorganic materials 0.000 abstract 2
- 229910018467 Al—Mg Inorganic materials 0.000 abstract 2
- 208000009205 Tinnitus Diseases 0.000 abstract 1
- 230000007547 defect Effects 0.000 abstract 1
- 238000003801 milling Methods 0.000 abstract 1
- 229910052725 zinc Inorganic materials 0.000 abstract 1
- 230000000694 effects Effects 0.000 description 10
- 238000005336 cracking Methods 0.000 description 6
- 239000000463 material Substances 0.000 description 5
- 230000007423 decrease Effects 0.000 description 4
- 150000001875 compounds Chemical class 0.000 description 3
- 239000013078 crystal Substances 0.000 description 3
- 230000005496 eutectics Effects 0.000 description 3
- 238000002844 melting Methods 0.000 description 3
- 230000008018 melting Effects 0.000 description 3
- 241000270722 Crocodylidae Species 0.000 description 2
- 238000005266 casting Methods 0.000 description 2
- 238000005097 cold rolling Methods 0.000 description 2
- LNNWVNGFPYWNQE-GMIGKAJZSA-N desomorphine Chemical compound C1C2=CC=C(O)C3=C2[C@]24CCN(C)[C@H]1[C@@H]2CCC[C@@H]4O3 LNNWVNGFPYWNQE-GMIGKAJZSA-N 0.000 description 2
- 229910017818 Cu—Mg Inorganic materials 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 230000033228 biological regulation Effects 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 239000010960 cold rolled steel Substances 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 238000012733 comparative method Methods 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 229910000765 intermetallic Inorganic materials 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 241000894007 species Species 0.000 description 1
- 230000001988 toxicity Effects 0.000 description 1
- 231100000419 toxicity Toxicity 0.000 description 1
Landscapes
- Metal Rolling (AREA)
Abstract
Description
【0001】[0001]
【産業上の利用分野】この発明は、高強度でプレス成形
性に優れ、自動車ボディパネル材などに好適な、成形加
工用高強度アルミニウム合金板の製造方法、特に熱間圧
延の方法に関するものである。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a method for producing a high-strength aluminum alloy sheet for forming, particularly a hot rolling method, which has high strength and excellent press formability and is suitable for automobile body panel materials and the like. is there.
【0002】[0002]
【従来の技術】従来、自動車ボディパネル用板材として
は、冷延鋼板が用いられてきたが、燃費向上などのため
に車体を軽量化する必要に応じて、軽量のAl合金板が
使用されつつある。この自動車ボディパネル用板材は、
一般に鋳塊を熱間圧延、冷間圧延することにより得ら
れ、さらに所望の形状にプレス成形されるため高強度で
成形性に優れていることが必要である。したがって、上
記板材に使用されるAl合金としても、これら特性を満
たすAl−高Mg系合金(例えばMg:4.0〜5.0
wt%を含有した5182合金や、同じくMg:5.8
〜6.8wt%含有のAA−X5085合金など)が実
用化されている。2. Description of the Related Art Conventionally, cold-rolled steel sheets have been used as sheet materials for automobile body panels, but lightweight Al alloy sheets have been used as needed to reduce the weight of vehicle bodies to improve fuel efficiency. is there. This car body panel plate is
Generally, it is required to have high strength and excellent formability because it is obtained by hot rolling or cold rolling an ingot and press-molded into a desired shape. Therefore, even as an Al alloy used for the above plate material, an Al-high Mg-based alloy (for example, Mg: 4.0 to 5.0) that satisfies these characteristics.
5182 alloy containing wt% and also Mg: 5.8
AA-X5085 alloy containing ˜6.8 wt% has been put to practical use.
【0003】[0003]
【発明が解決しようとする問題点】ところが、Al−M
g系合金は、Mg量が多くなると熱間加工性が悪化し、
特に4.5%を越えると、熱間圧延時に耳割れ、表面割
れやワニ口割れ、さらには二枚板が発生するようにな
り、歩留まりが悪いという問題がある。これに対して
は、熱間加工時の圧下率を小さくする方法も考えられ
る。例えば、通常1パス当り30mm程度の板厚減少で
行なっている圧下を、15mm程度の板厚減少で圧下す
ることにより割れの発生を防止しようとするものであ
る。しかし、通常30mmの板厚減少で20パスで行な
っていた圧延工程を上記板厚減少で行なうものとする
と、同程度の最終圧延厚さにするまでには40パス以上
を必要とするため作業能率が著しく低下するという問題
がある。本発明は上記の問題について検討の結果なされ
たもので、熱間加工時に致命的な割れが発生することが
なく、歩留まりよく、しかも作業能率の低下をできるだ
け少なくして成形用高強度Al合金板を得ることができ
る製造方法を提供するものである。[Problems to be Solved by the Invention] However, Al-M
When the amount of Mg in the g-based alloy increases, the hot workability deteriorates,
In particular, when it exceeds 4.5%, there is a problem that the yield becomes poor because the ear cracks, the surface cracks, the crocodile cracks, and the two plates are generated during the hot rolling. For this, a method of reducing the rolling reduction during hot working can be considered. For example, it is intended to prevent the occurrence of cracks by reducing the reduction which is usually performed by reducing the plate thickness by about 30 mm per pass by reducing the thickness by about 15 mm. However, if the rolling process, which was normally performed in 20 passes with a reduction in plate thickness of 30 mm, is performed with the above reduction in plate thickness, it takes 40 passes or more to reach the same final rolling thickness, and therefore work efficiency is improved. Is significantly reduced. The present invention has been made as a result of studying the above-mentioned problems. It does not cause fatal cracks during hot working, has a good yield, and minimizes the decrease in work efficiency as much as possible. The present invention provides a manufacturing method capable of obtaining
【0004】[0004]
【問題を解決するための手段】そこで、本発明者達は、
上述のような観点から、成形加工用高強度Al合金板の
製造方法、特に熱間圧延方法について研究を重ね、特定
の板厚範囲での圧延の1パス当りの板厚減少を規制する
ことにより、致命的な割れの発生を抑制できることを見
い出した。[Means for Solving the Problem] Therefore, the present inventors have
From the above viewpoints, by repeatedly studying a method for producing a high-strength Al alloy sheet for forming, particularly a hot rolling method, and by regulating the reduction in sheet thickness per pass of rolling in a specific sheet thickness range, , Found that the occurrence of fatal cracks can be suppressed.
【0005】本発明の成形加工用高強度アルミニウム合
金板の製造法は、かかる知見に基づいてなされたもので
あり、具体的には、重量%で、Mg:4.5〜8%、C
u:0.05〜0.4%、Ti:0.005%〜0.1
0%、Be:0.0001〜0.01%を含有するAl
合金鋳塊を、420〜510℃で2〜24時間の一段ま
たは二段均質化処理を行った後、450〜510℃の温
度で熱間加工を開始し、この圧延に際し、入口板厚が1
50mm以下で、かつ50mm以上の場合に1パス当り
の板厚減少を15mm以下とすることを特徴とする。The method for producing a high-strength aluminum alloy sheet for forming according to the present invention is based on this finding. Specifically, in terms of weight%, Mg: 4.5-8%, C
u: 0.05 to 0.4%, Ti: 0.005% to 0.1
Al containing 0% and Be: 0.0001 to 0.01%
The alloy ingot is subjected to a one-step or two-step homogenization treatment at 420 to 510 ° C. for 2 to 24 hours, and then hot working is started at a temperature of 450 to 510 ° C. In this rolling, the inlet plate thickness is 1
When the thickness is 50 mm or less and 50 mm or more, the reduction in plate thickness per pass is 15 mm or less.
【0006】また、第2の発明は、上記Al合金鋳塊の
成分に加え、さらにZn:0.1〜0.6%、Mn:
0.05〜0.20%、Cr:0.05〜0.15%、
Zr:0.05〜0.15%の1種以上を含有すること
を特徴とする。In addition, in the second invention, in addition to the components of the Al alloy ingot, Zn: 0.1 to 0.6%, Mn:
0.05 to 0.20%, Cr: 0.05 to 0.15%,
Zr: 0.05 to 0.15% at least one kind is contained.
【0007】本願発明の熱間圧延に際しては、入口板厚
が150mmを越える段階、または50mm未満の段階
では、上記規制の必要がなく、大きな圧下率で効率よく
圧延を行なうことができる。例えば、入口板厚が150
mmを越える段階では、初期圧延を除いて20mm以上
の板厚減少で行うのが望ましい。そして、50mm未満
では30%以上の圧下率で圧延を行なうのが望ましい。
これらの圧延によって、最終的には3〜10mm程度の
熱間圧延板を得る。その後は、常法により冷間圧延、成
形加工を行なう。In the hot rolling of the present invention, when the inlet plate thickness exceeds 150 mm or less than 50 mm, the above regulation is not necessary and the rolling can be efficiently performed with a large reduction rate. For example, the entrance plate thickness is 150
At the stage of exceeding mm, it is desirable to reduce the plate thickness by 20 mm or more excluding the initial rolling. If it is less than 50 mm, it is desirable to carry out rolling at a rolling reduction of 30% or more.
By these rolling, a hot rolled plate of about 3 to 10 mm is finally obtained. After that, cold rolling and forming are performed by a conventional method.
【0008】[0008]
【作用】すなわち、本発明によれば、高強度で成形性に
優れたAl合金板材を割れの発生を招くことなく良好に
熱間圧延を行なうことができ、また、その際の作業能率
の低下も最小限に止めることができる。次に、本願発明
における各条件の限定理由を説明するが、先ず本願発明
に用いるAl合金鋳塊の合金成分の限定理由について述
べる。In other words, according to the present invention, an Al alloy sheet material having high strength and excellent formability can be satisfactorily hot-rolled without causing cracking, and the work efficiency at that time is reduced. Can be kept to a minimum. Next, the reasons for limiting each condition in the present invention will be described. First, the reasons for limiting the alloy components of the Al alloy ingot used in the present invention will be described.
【0009】Mg:4.5〜8% Mgは本合金の基本成分であって、その添加量が高くな
る程、強度及び延性が向上する。その作用を十分に得る
ためには4.5%以上の添加が必要である。しかし、8
%を越えると熱間加工性が著しく低下し、本発明の方法
をもってしてもその圧延加工が不可能となる。そこでM
g含有量は4.5〜8%に定めた。 Cu:0.05〜0.4% Cuは強度を向上させる元素であり、とくに成形加工
後、塗装焼付けしたときの強度低下を抑制する。しか
し、0.05%未満ではその効果が少なく、一方0.4
0%を越えると冷間加工性が低下し、かつ耐食性も劣化
する。そこでCu含有量は0.05〜0.4%に定め
た。Mg: 4.5-8% Mg is a basic component of the present alloy, and the higher the amount added, the higher the strength and ductility. In order to obtain the effect sufficiently, it is necessary to add 4.5% or more. But 8
If it exceeds%, the hot workability is remarkably deteriorated, and the rolling process becomes impossible even by the method of the present invention. So M
The g content was set to 4.5-8%. Cu: 0.05 to 0.4% Cu is an element that improves the strength, and particularly suppresses the decrease in strength when coating baking is performed after the molding process. However, if less than 0.05%, the effect is small, while 0.4
If it exceeds 0%, the cold workability is deteriorated and the corrosion resistance is also deteriorated. Therefore, the Cu content is set to 0.05 to 0.4%.
【0010】Ti:0.005%〜0.10% Tiは鋳造割れの防止と鋳塊の結晶粒の微細化に効果が
あるが、0.005%未満ではその効果が不十分であ
り、また、0.10%を越えると巨大な金属間化合物を
生じ、延性が低下する。そこでTi含有量は0.005
%〜0.10%にと定めた。 Be:0.0001〜0.01% BeはMg含有量の高い合金において、その鋳造性を向
上させる効果を有するが、0.0001%未満ではその
効果が不十分で、0.01%を越えるとその毒性が問題
となるので、その含有量を0.0001〜0.01%に
定めた。Ti: 0.005% to 0.10% Ti is effective in preventing casting cracks and refining the crystal grains of the ingot, but if it is less than 0.005%, the effect is insufficient. , 0.10%, a huge intermetallic compound is formed, and the ductility decreases. Therefore, the Ti content is 0.005
% To 0.10%. Be: 0.0001 to 0.01% Be has an effect of improving castability in an alloy having a high Mg content, but if it is less than 0.0001%, the effect is insufficient and exceeds 0.01%. Since its toxicity becomes a problem, its content was set to 0.0001 to 0.01%.
【0011】Zn:0.1〜0.6% Mn;0.05〜0.20% Cr:0.05〜0.15% Zr:0.05〜0.15% これらの元素は必要により1種以上含有させるもので、
再結晶粒の微細化と強度向上に効果があるが、いずれも
下限値未満では効果が少なく、一方、上限値を越えると
延性が低下するのでそれぞれ上記範囲に定めた。Zn: 0.1 to 0.6% Mn; 0.05 to 0.20% Cr: 0.05 to 0.15% Zr: 0.05 to 0.15% These elements are 1 if necessary. Including more than one species,
Although it is effective in making the recrystallized grains finer and improving the strength, if both are less than the lower limit, the effect is small, while if it exceeds the upper limit, the ductility decreases, so the respective ranges were set to the above.
【0012】次に製造条件の限定理由について述べる。 均質化処理:420〜510℃で2〜24時間 この処理は、鋳造時に偏析したMg,Cuを均質にする
効果がある。このためには420〜510℃で2〜24
時間、好ましくは2〜16時間加熱保持する。加熱温度
が420℃未満では均質化の効果が少なく、また510
℃を越えると結晶粒の粗大化又は偏析相の共晶融解の可
能性がある。また、加熱時間が2時間未満では均質化の
効果が少なく、24時間を越えるとその効果が飽和す
る。したがって、加熱温度および時間を上記に限定し
た。なお、特にMg量が高い場合、β相(Mg5Al
8)を含む共晶化合物の融点が約450℃となることか
ら、好ましくは420〜450℃未満で一段目の均質化
処理を行い、引き続いて450℃以上に昇温して二段目
の均質化処理を行う。Next, the reasons for limiting the manufacturing conditions will be described. Homogenization treatment: 420 to 510 ° C. for 2 to 24 hours This treatment has an effect of homogenizing Mg and Cu segregated during casting. For this purpose, 2 ~ 24 at 420 ~ 510 ℃
Heat and hold for a time, preferably 2 to 16 hours. If the heating temperature is less than 420 ° C, the effect of homogenization is small, and 510
If the temperature exceeds ℃, there is a possibility of coarsening of crystal grains or eutectic melting of the segregated phase. If the heating time is less than 2 hours, the homogenizing effect is small, and if it exceeds 24 hours, the effect is saturated. Therefore, the heating temperature and time were limited to the above. When the amount of Mg is high, the β phase (Mg5Al
Since the eutectic compound containing 8) has a melting point of about 450 ° C., the first-stage homogenization treatment is preferably performed at 420 to less than 450 ° C., and subsequently the temperature is raised to 450 ° C. or higher to obtain a second-stage homogenization treatment. Process.
【0013】熱間圧延開始温度:450〜510℃ 通常、鋳塊は上述の均質化処理後、一旦室温まで冷却さ
れ、その後熱間圧延前に再加熱される。この均質化処理
後の冷却時にAl−Cu−Mg系化合物が粒界に析出
し、熱間圧延割れの原因となる。この化合物を再固溶さ
せるには、450℃以上まで再加熱し、熱間圧延を開始
する。また、圧延温度が510℃を越えると共晶融解を
生じ、割れが起こるので上記範囲に限定する。Hot rolling start temperature: 450 to 510 ° C. Normally, the ingot is once cooled to room temperature after the above homogenization treatment, and then reheated before hot rolling. At the time of cooling after this homogenization treatment, the Al-Cu-Mg-based compound precipitates at the grain boundaries, which causes hot rolling cracks. In order to re-dissolve this compound, it is reheated to 450 ° C. or higher and hot rolling is started. Further, if the rolling temperature exceeds 510 ° C., eutectic melting occurs and cracking occurs, so the range is limited to the above range.
【0014】熱間圧延軽圧下 通常、板厚数百mm程度である本合金鋳塊を、通常圧下
で板厚150mmまで圧延すると、板表面部では内部に
比べて結晶粒の変形の程度が大きく、β相の析出量も多
く、かつ硬度も高くなるなど著しい不均一性が現われて
くる。すなわち、圧延に伴って表面部に比較して内部が
相対的に強度が弱くなっており、この状態で強圧下を加
えると、圧延出口側で働く板厚方向の引張応力により、
弱い内部で割れ(ワニ口割れ)が発生し、さらにはその
割れの伝播により二枚板となる場合もある。一方、板厚
50mm未満では板内部にも圧下が効いて上述の組織、
強度等の不均一性が解消されるため、高い圧下率で強圧
下を加えても割れは発生しない。 以上より、本発明で
は、板厚150mm以下、50mm以上での圧延を軽圧
下(1パス当りの板厚減少を15mm以下)で行う。Hot rolling light reduction When the ingot of the present alloy, which has a plate thickness of about several hundred mm, is rolled under a normal pressure to a plate thickness of 150 mm, the degree of deformation of crystal grains is larger at the plate surface portion than in the inside. A large amount of β-phase is precipitated, and the hardness is increased, resulting in remarkable non-uniformity. That is, the strength of the inside is relatively weakened as compared with the surface portion due to rolling, and when a strong reduction is applied in this state, due to the tensile stress in the plate thickness direction that acts on the rolling exit side,
Cracks (crocodile cracks) may occur inside the weak interior, and the cracks may propagate to form a double plate. On the other hand, when the plate thickness is less than 50 mm, the reduction is effective even inside the plate and the above-mentioned structure,
Since the non-uniformity of strength and the like is eliminated, cracking does not occur even if strong reduction is applied at a high reduction rate. From the above, in the present invention, rolling with a plate thickness of 150 mm or less and 50 mm or more is performed under a light pressure (a reduction in plate thickness per pass of 15 mm or less).
【0015】[0015]
【実施例】以下、実施例によって本発明を説明する。表
1に示すNo.1〜3(本発明例)およびNo.4、5
(比較例)の組成の合金鋳塊(厚さ508mm、幅15
75mm)を常法により作製し、その鋳塊に表2に示す
条件で均質化処理および熱間圧延を行い、最終的に5m
m厚の熱延板を得た。その結果を表2に併せて示す。表
2から明らかなように、本発明方法による板材は、熱間
圧延時に割れの発生がなく良好に圧延を行なうことがで
きた。一方、比較法によれば、熱間圧延の際に割れが発
生し、使用に耐え得ないものであった。EXAMPLES The present invention will be described below with reference to examples. No. shown in Table 1 1 to 3 (invention example) and No. 4,5
Alloy ingot having the composition of (Comparative Example) (thickness 508 mm, width 15
75 mm) by an ordinary method, the ingot is subjected to homogenization treatment and hot rolling under the conditions shown in Table 2, and finally 5 m
A hot rolled sheet having a thickness of m was obtained. The results are also shown in Table 2. As is clear from Table 2, the plate material according to the method of the present invention could be satisfactorily rolled without cracking during hot rolling. On the other hand, according to the comparative method, cracking occurred during hot rolling and it could not be used.
【0016】[0016]
【表1】 [Table 1]
【0017】[0017]
【表2】 [Table 2]
【0018】[0018]
【発明の効果】以上説明したように、本発明の成形加工
用高強度アルミニウム合金板の製造方法によれば、重量
%で、Mg:4.5〜8%、Cu:0.05〜0.4
%、Ti:0.005%〜0.10%、Be:0.00
01〜0.01%を含有し、さらに、所望により、Z
n:0.1〜0.6%、Mn:0.05〜0.20%、
Cr:0.05〜0.15%、Zr:0.05〜0.1
5%の1種以上を含有するAl合金鋳塊を、420〜5
10℃で2〜24時間の一段または二段均質化処理を行
った後、450〜510℃の温度で熱間加工を開始し、
この圧延に際し、入口板厚が150mm以下で、かつ5
0mm以上の場合に1パス当りの板厚減少を15mm以
下としたので、Al合金鋳塊を割れの発生を招くことな
く熱間圧延することができ、高強度で成形性の優れたア
ルミニウム合金板を歩留まりよく、また能率よく製造す
ることができる。As described above, according to the method for producing a high-strength aluminum alloy sheet for forming according to the present invention, Mg: 4.5-8%, Cu: 0.05-0. Four
%, Ti: 0.005% to 0.10%, Be: 0.00
01-0.01%, and optionally Z
n: 0.1 to 0.6%, Mn: 0.05 to 0.20%,
Cr: 0.05 to 0.15%, Zr: 0.05 to 0.1
The Al alloy ingot containing 5% of one or more of
After performing a one-step or two-step homogenization treatment at 10 ° C for 2 to 24 hours, start hot working at a temperature of 450 to 510 ° C,
In this rolling, the inlet plate thickness is 150 mm or less, and 5
When the thickness is 0 mm or more, the reduction in plate thickness per pass is set to 15 mm or less, so that the aluminum alloy ingot can be hot-rolled without causing cracking, and the aluminum alloy plate has high strength and excellent formability. Can be manufactured with good yield and efficiency.
───────────────────────────────────────────────────── フロントページの続き (72)発明者 川俣 淳 静岡県裾野市平松85番地 三菱アルミニウ ム株式会社内 ─────────────────────────────────────────────────── ─── Continuation of the front page (72) Inventor Atsushi Kawamata 85 Hiramatsu, Susono City, Shizuoka Prefecture Mitsubishi Aluminum Co., Ltd.
Claims (2)
0.05〜0.4%、Ti:0.005%〜0.10
%、Be:0.0001〜0.01%を含有するAl合
金鋳塊を、420〜510℃で2〜24時間の一段また
は二段均質化処理を行った後、450〜510℃の温度
で熱間加工を開始し、この圧延に際し、入口板厚が15
0mm以下で、かつ50mm以上の場合に1パス当りの
板厚減少を15mm以下とすることを特徴とする成形加
工用高強度アルミニウム合金板の製造法1. By weight percent, Mg: 4.5-8%, Cu:
0.05 to 0.4%, Ti: 0.005% to 0.10.
%, Be: 0.0001-0.01% containing Al alloy ingot, after performing a one-step or two-step homogenization treatment at 420-510C for 2-24 hours, at a temperature of 450-510C. Hot working was started, and at the time of this rolling, the inlet plate thickness was 15
A method for manufacturing a high-strength aluminum alloy sheet for forming, characterized in that the thickness reduction per pass is 0 mm or less when the thickness is 0 mm or less and 50 mm or more.
え、さらにZn:0.1〜0.6%、Mn:0.05〜
0.20%、Cr:0.05〜0.15%、Zr:0.
05〜0.15%の1種以上を含有することを特徴とす
る成形加工用高強度アルミニウム合金板の製造法2. In addition to the components of the Al alloy ingot according to claim 1, Zn: 0.1-0.6%, Mn: 0.05-
0.20%, Cr: 0.05 to 0.15%, Zr: 0.
A method for producing a high-strength aluminum alloy sheet for forming, characterized by containing at least one of 05 to 0.15%
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JP34579593A JP3539996B2 (en) | 1993-12-24 | 1993-12-24 | Manufacturing method of high strength aluminum alloy sheet for forming |
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JP34579593A JP3539996B2 (en) | 1993-12-24 | 1993-12-24 | Manufacturing method of high strength aluminum alloy sheet for forming |
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JP3539996B2 JP3539996B2 (en) | 2004-07-07 |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2007070672A (en) * | 2005-09-06 | 2007-03-22 | Furukawa Sky Kk | Method for producing aluminum alloy thick plate having excellent fatigue property |
JP2008280574A (en) * | 2007-05-10 | 2008-11-20 | Sumitomo Chemical Co Ltd | Method for producing aluminum alloy and use thereof |
-
1993
- 1993-12-24 JP JP34579593A patent/JP3539996B2/en not_active Expired - Fee Related
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2007070672A (en) * | 2005-09-06 | 2007-03-22 | Furukawa Sky Kk | Method for producing aluminum alloy thick plate having excellent fatigue property |
JP2008280574A (en) * | 2007-05-10 | 2008-11-20 | Sumitomo Chemical Co Ltd | Method for producing aluminum alloy and use thereof |
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