JPS61201749A - Rolled aluminum alloy sheet for forming and its manufacture - Google Patents

Rolled aluminum alloy sheet for forming and its manufacture

Info

Publication number
JPS61201749A
JPS61201749A JP4336885A JP4336885A JPS61201749A JP S61201749 A JPS61201749 A JP S61201749A JP 4336885 A JP4336885 A JP 4336885A JP 4336885 A JP4336885 A JP 4336885A JP S61201749 A JPS61201749 A JP S61201749A
Authority
JP
Japan
Prior art keywords
less
strength
aluminum alloy
rolled
alloy
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
JP4336885A
Other languages
Japanese (ja)
Inventor
Toshio Komatsubara
俊雄 小松原
Toshiki Muramatsu
俊樹 村松
Mamoru Matsuo
守 松尾
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.)
SUKAI ALUM KK
Original Assignee
SUKAI ALUM KK
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 SUKAI ALUM KK filed Critical SUKAI ALUM KK
Priority to JP4336885A priority Critical patent/JPS61201749A/en
Publication of JPS61201749A publication Critical patent/JPS61201749A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To manufacture a rolled Al alloy sheet excelling in strength and formability, causing no deterioration in strength after baking finish, and suitable for use in automobile body seats by subjecting an Al alloy ingot having a specific composition to homogenizing treatment, to rolling to prescribed thickness, and to heat treatment under specific conditions. CONSTITUTION:The Al alloy ingot containing, by weight, 1.2-1.5% Si, 0.25-0.85% Mg, 0.05-0.4% Fe, 0.3-1.5% Cu, and further 1 or >=2 kinds among 0.05-0.6% Mn, 0.05-0.3% Cr, and 0.05-0.15% Zr is cast. The ingot is heated at 450-580 deg.C for 1-48hr to be homogenized and is then subjected to hot rolling or further to cold rolling to be rolled into a sheet with prescribed thickness. The sheet is maintained in a temp. range of 500-580 deg.C for >=20sec, cooled rapidly at >=1,000 deg.C/min cooling rate and then subjected to ageing by an ordinary method.

Description

【発明の詳細な説明】 産業上の利用分野 この発明は成形加工用のアルミニウム合金圧延板および
その製造方法に関し、特に高強度が要求されしかも焼付
塗装を施して使用される用途、例えば自動車車体等に適
した成形加工用アルミニウム合金圧延板およびその製造
方法に関するものである。
DETAILED DESCRIPTION OF THE INVENTION Field of Industrial Application This invention relates to a rolled aluminum alloy plate for forming processing and a method for manufacturing the same, and particularly for applications that require high strength and are used with baking coating, such as automobile bodies. The present invention relates to an aluminum alloy rolled plate suitable for forming and a method for manufacturing the same.

従来の技術 自動車車体のボディシートには、従来は主として冷延鋼
板が用いられることが多かったが、最近では車体軽量化
の要求から、アルミニウム合金圧延板を使用する検討が
なされている。自動車車体のボディシートは、プレス成
形を施して使用されることから成形加工性が優れている
こと、特に伸び、張出し性が優れておりかつ成形加工時
におけるリューダースマークの発生がないことが要求さ
れ、しかも^強度を有することも必須であって、特に焼
付塗装を施すところから、焼付塗装後の強度が高いこと
が要求される。
BACKGROUND OF THE INVENTION Conventionally, cold-rolled steel sheets have been mainly used for body sheets of automobile bodies, but recently, due to the demand for lighter vehicle bodies, consideration has been given to using rolled aluminum alloy sheets. Since body sheets for automobile bodies are used after being press-formed, they are required to have excellent moldability, especially excellent elongation and extrusion properties, and no Lüders mark during molding. Moreover, it is also essential to have strength, and in particular, since baking coating is applied, high strength after baking coating is required.

ところで強度が要求される成形加工品の用途に使用され
るアルミニウム合金板としては従来から種々のものがあ
るが、その主要なものは合金に成分系によって次のよう
に分けられる。
By the way, there have been various types of aluminum alloy plates used for forming products that require strength, but the main ones can be divided into alloys as follows, depending on their composition.

(イ)非熱処理型へ〇 −MO系合金である5052合
金(Ml 2,2〜2.8%、Or 0.15〜0.3
5%、残部へgおよび不可避的不純物)の0材あるいは
同じ<5182合金(MnO620−0,50%、yg
i、o〜5.0%、残部^gおよび不可避的不純物)の
0材。
(a) To non-heat treatment type 〇 -5052 alloy which is MO type alloy (Ml 2.2~2.8%, Or 0.15~0.3
0 material or the same <5182 alloy (MnO620-0,50%, yg
i, o~5.0%, balance ^g and unavoidable impurities).

(ロ)熱処理型へ〇 −Cu系合金である2036合金
(Cu 2.2〜3.0%、Mn0,1〜0.4%、M
l0.3〜0.6%、残部^Qおよび不可避的不純物)
のT4処理材。
(b) To heat treatment type - 2036 alloy which is a Cu-based alloy (Cu 2.2-3.0%, Mn 0.1-0.4%, M
l0.3-0.6%, balance ^Q and unavoidable impurities)
T4 treated material.

(ハ)熱処理型^fl −Ml −Zn −Cu系合金
のT4処理材。この系のアルミニウム合金としては、例
えば特開昭52−141409号の合金、特開昭53−
103914号の合金、あるいは特開昭57−9864
8号の合金などがある。
(c) T4-treated material of heat-treated ^fl-Ml-Zn-Cu-based alloy. Examples of this type of aluminum alloy include the alloy of JP-A-52-141409, the alloy of JP-A-53-141409,
Alloy No. 103914 or JP-A-57-9864
There are No. 8 alloys.

(ニ)熱処理型Al’ −1411−Si系合金である
6009合金(MOo、4〜0.8%、Si0.6〜1
.0%、CII 0.15〜0.6%、Mn0.2〜0
.8%、残部へQおよび不可避的不純物)のT4処理材
や同じ<6010合金(Mg0.6〜1.0%、Si0
.8〜1.2%、Cu0.15〜0.6%、Mn 0.
2〜0.8%、残部Mおよび不可避的不純物)のT4処
理材。
(d) 6009 alloy (MOo, 4-0.8%, Si0.6-1
.. 0%, CII 0.15-0.6%, Mn0.2-0
.. 8%, the remainder containing Q and unavoidable impurities) and the same <6010 alloy (Mg0.6-1.0%, Si0
.. 8-1.2%, Cu 0.15-0.6%, Mn 0.
2-0.8%, balance M and unavoidable impurities) T4 treated material.

しかしながらこれらの従来のアルミニウム合金では、自
動車車体のボディシートに要求される前述の特性を全て
充分に満足させることは困難であった。
However, with these conventional aluminum alloys, it has been difficult to fully satisfy all of the above-mentioned characteristics required for body sheets of automobile bodies.

すなわち(イ)の合金では、強度が不充分であり、しか
も成形加工時にリューダースマークが発生し易い問題が
あり、さらには塗装焼付工程によって強度が低下する問
題があった。また(口)の合金では、成形性が劣り、か
つまた塗装焼付工程によって強度が低下する問題もあっ
た。さらに(ハ)の合金では、成形性、特に曲げ性が充
分とは言えず、また塗装焼付工程で強度が低下する問題
もあった。また(二)の系の合金では、例えば6009
合金の場合強度が不充分であり、一方60106010
合金、曲げ性が不充分であった。
That is, the alloy (a) has insufficient strength, has the problem of easily generating Lüders marks during molding, and further has the problem of reduced strength due to the paint baking process. In addition, the alloy described above has poor formability and also has the problem of reduced strength due to the paint baking process. Furthermore, the alloy (c) has a problem in that the formability, especially the bendability, is not sufficient, and the strength decreases during the paint baking process. In addition, for the alloy of the (2) system, for example, 6009
In the case of alloys, the strength is insufficient, while 60106010
The alloy had insufficient bendability.

発明が解決すべき問題点 前述のように従来のアルミニウム合金では、自動車車体
のボディシートに要求される特性、すなわち優れた成形
加工性を有すること、特に伸び、張出し成形性が優れか
つリューダースマークの発生がないこと、また強度、特
に塗装焼付後の強度が高いこと等を充分に満足すること
は困難であった。
Problems to be Solved by the Invention As mentioned above, conventional aluminum alloys have the characteristics required for automobile body sheets, that is, excellent formability, especially excellent elongation and stretch formability, and the Lüders mark. It has been difficult to fully satisfy the following requirements: no occurrence of blemishes, and high strength, especially after paint baking.

この発明は以上の事情を背景としてなされたもので、成
形加工性、特に伸び、張出し性が優れかつ成形加工時に
おけるリューダースマークの発生がなく、しかも高強度
を有し、特に成形加工後の塗装焼付工程での強度低下が
なく、むしろ成形加工後の塗装焼付工程によって強度が
上昇することにより高い強度を有する成形品が得られる
ようにしたアルミニウム合金圧延板、およびその製造方
法を提供することを目的とするものである。
This invention was made against the background of the above-mentioned circumstances, and has excellent moldability, especially elongation and stretchability, no Lüders marks during molding, and high strength, especially after molding. To provide an aluminum alloy rolled sheet and a method for producing the same, in which a molded product having high strength is obtained by not reducing strength in a paint baking process, but rather increasing the strength in a paint baking process after forming. The purpose is to

問題点を解決するための手段 第1発明の成形加工用アルミニウム合金圧延板は、Si
 1.2%(!量%、以下同じ)を越え1.5%以下、
Mll 0.25%以上0.85%以下、Fe o、o
s%以上0.4%以下、Cu 0.3%以上1.5%以
下を含有し、ざらにun o、os%以上0.6%以下
、Or 0.05%以上0.3%以下、z「0.05%
以上0.15%以下のうちから選ばれた1種または2種
以上を含有し、残部が八gおよび不可避的不純物よりな
ることを特徴とするものであり、このような特定の成分
系と−することによって、強度および成形加工性に優れ
、特に焼付塗装後の強度が大きい自動車車体ボディシー
ト等に好適な成形加工用アルミニウム合金圧延板を実現
できたのである。
Means for Solving the Problems The aluminum alloy rolled plate for forming processing of the first invention is made of Si
More than 1.2% (!Amount%, same below) and less than 1.5%,
Mll 0.25% or more and 0.85% or less, Fe o, o
Contains s% or more and 0.4% or less, Cu 0.3% or more and 1.5% or less, roughly un o, os% or more and 0.6% or less, Or 0.05% or more and 0.3% or less, z"0.05%
It is characterized by containing one or more selected from the above 0.15% or less, with the remainder consisting of 8g and unavoidable impurities, and such a specific component system and - By doing so, it was possible to realize an aluminum alloy rolled sheet for forming, which has excellent strength and formability, and is suitable for forming automobile body sheets, etc., which has particularly high strength after baking painting.

第2発明の方法は、上述のような優れた特性を有する成
形加工用アルミニウム合金圧延板を製造するための方法
であって、前記同様な成分を含有するアルミニウム台金
鋳塊に対し、450〜580℃の温度で1〜48時間均
質化処理し、次いで所要の板厚まで圧延した侵、500
〜580℃の範囲内の温度に20秒以上保持し、続いて
急速冷却して、室部で時効することを特徴とするもので
ある。
The method of the second invention is a method for manufacturing an aluminum alloy rolled plate for forming processing having the excellent properties as described above, and the method is a method for manufacturing an aluminum base ingot containing the same components as described above. Homogenized at a temperature of 580°C for 1 to 48 hours, then rolled to the required thickness, 500°C
It is characterized by being maintained at a temperature within the range of ~580°C for 20 seconds or more, followed by rapid cooling and aging in a room.

作   用 先ずこの発明のアルミニウム合金圧延板における成分限
定理由を説明する。
Function First, the reason for limiting the components in the aluminum alloy rolled plate of the present invention will be explained.

Si: SiはMllとの共存により一1129iを生成して析
出硬化により強度を付与するに有効であり、同時に成形
性特に伸びを向上させるに有効である。Slの下限は強
度の点から定められるが、この発明の場合強度向上に効
果のあるCuを0.3%以上添加しているから、Siが
1.2%を越えれば所要の強度を、得ることができ、一
方Siが1.5%を越えてもそれ以上強度向上は望めな
いから、Siは1.2%を越え 1□5%以下の範囲内
とした。
Si: Si is effective in coexisting with Mll to form -1129i and imparting strength through precipitation hardening, and at the same time is effective in improving formability, particularly elongation. The lower limit of Sl is determined from the viewpoint of strength, but in the case of this invention, 0.3% or more of Cu, which is effective in improving strength, is added, so if Si exceeds 1.2%, the required strength can be obtained. On the other hand, if the Si content exceeds 1.5%, no further improvement in strength can be expected, so the Si content is set to be in the range of more than 1.2% and less than 1□5%.

νg= 一〇は既に述べたようにSiとの共存によりkJI12
siを生成して強度を付与する。M9が0.25%未満
では強度が不充分であり、一方0.85%を越えれば伸
びが低下するから、0.25〜0.85%の範囲内とし
た。
As already mentioned, νg=10 is kJI12 due to coexistence with Si.
si is generated to impart strength. If M9 is less than 0.25%, the strength will be insufficient, while if it exceeds 0.85%, elongation will decrease, so it is set within the range of 0.25 to 0.85%.

Fe: 「eは結晶粒の微細化を通じて強度向上に寄与するが、
0.05%未満では結晶粒が粗大化し、一方0.4%を
越えれば成形性が低下するから、0.05〜0.4%の
範囲内とした。
Fe: "e contributes to improving strength through refinement of crystal grains, but
If it is less than 0.05%, the crystal grains will become coarse, while if it exceeds 0.4%, the formability will deteriorate, so it was set within the range of 0.05 to 0.4%.

Cu: Cuは強度と成形性、特に曲げ性を向上させるが、0.
3%未満では強度向上効果が充分ではなく、一方1.5
%を越えれば強度は向上するものの成形性が低下するか
ら、0.3〜1.5%の範囲内とした。
Cu: Cu improves strength and formability, especially bendability, but 0.
If it is less than 3%, the strength improvement effect is not sufficient;
If it exceeds 0.3%, the strength will improve but the moldability will decrease, so it was set within the range of 0.3 to 1.5%.

Mn、 Or、 2r : コレラの元素はいずれも再結晶粒を微細化させ、組織ヲ
安定化させるとともに、成形性を向上させる。unが0
.05%未満、Orが0.05%未満、2「が0.OS
%未満では上記の効果が得られず、一方unが0.6%
をこえれば成形性が低下し、C「が003%、kが0.
15%を越えれば巨大金属間化合物が生成されて伸びが
低下するから、Mnは0.05〜0.6%、Orは0.
05〜0.3%、Zrは0.05〜0.15%の範囲内
とした。
Mn, Or, 2r: All elements of cholera make recrystallized grains finer, stabilize the structure, and improve formability. un is 0
.. 0.05%, Or is less than 0.05%, 2" is 0.OS
%, the above effect cannot be obtained, while un is 0.6%.
If the value exceeds 0.003%, the moldability decreases, and if the value of C exceeds 0.03%, k becomes 0.003%.
If it exceeds 15%, giant intermetallic compounds are formed and the elongation decreases, so Mn is 0.05-0.6% and Or is 0.05%.
05 to 0.3%, and Zr was within the range of 0.05 to 0.15%.

以上の各成分の残部は^Qおよび不可避的不純物とすれ
ば良い。なお通常のアルミニウム合金においては鋳塊結
晶粒微細化のためにTi、あるいは毛およびBを微量添
加することがあり、この発明のアルミニウム合金板圧延
板においても微】のTi、あるいTiおよびBを含有し
ていても良い。但しTiを添加する場合0.01%未満
ではその効果が得られず、0.15%以上では初晶Ti
 AN 3が晶出して成形性を害するから、Tiは0.
01〜0.15%の範囲内とすることが好ましい。また
Tiとともに8を添加する場合、11)l)1m未満で
はその効果がなく、5o o ppmを越えればTr 
82の粗大粒子が混入して成形性を害するから、Bは1
〜500 ppIlの範囲内とすることが好ましい。
The remainder of each of the above components may be ^Q and unavoidable impurities. Note that in ordinary aluminum alloys, small amounts of Ti, hair, and B are sometimes added to refine the ingot crystal grains, and the rolled aluminum alloy plate of the present invention also contains a small amount of Ti, or Ti and B. It may contain. However, when adding Ti, if it is less than 0.01%, the effect cannot be obtained, and if it is more than 0.15%, the primary crystal Ti
Since AN 3 crystallizes and impairs formability, Ti should be 0.
It is preferably within the range of 0.01 to 0.15%. Furthermore, when adding 8 along with Ti, 11) l) there is no effect if it is less than 1 m, and if it exceeds 5 o ppm, Tr
Since coarse particles of 82 are mixed in and impair the moldability, B is 1.
It is preferably within the range of ~500 ppIl.

以上のような成分組成のアルミニウム合金圧延板は、後
述する実施例でも示すように、伸び、張り出し性1曲げ
性等の成形加工性が優れかつ成形加工時のりューダース
マークの発生もなく、強度的にも充分である。特に成形
加工後の焼付工程において強度の低下がないばかりでな
く、むしろ塗装焼付工程で強度が上昇し、その結果強度
が高い焼付塗装成形品を得ることが可能となる。
The aluminum alloy rolled sheet having the above-mentioned composition has excellent formability such as elongation, stretchability, bendability, etc., and does not generate Luders marks during forming, and has excellent strength, as shown in the examples below. is also sufficient. In particular, not only is there no decrease in strength in the baking step after molding, but the strength is increased in the baking step, and as a result, it is possible to obtain baked-coated molded products with high strength.

次に本願の第2発明、ずなりもアルミニウム合金圧延板
の製造方法について、各プロセス条件の限定理由ととも
に説明する。
Next, the second invention of the present application, a method for manufacturing a rolled aluminum alloy plate, will be explained along with the reasons for limiting each process condition.

先ず前述のような成分組成を有するアルミニウム合金鋳
塊を常法にしたがって、連続i造法あるいは半連続鋳造
法または造塊法により作成する。
First, an aluminum alloy ingot having the above-mentioned composition is prepared by a continuous casting method, a semi-continuous casting method, or an ingot forming method according to a conventional method.

次いでその鋳塊に対し、均質化処理を施して成形性を向
上させるとともに結晶粒を微細に均一化する。この均質
化処理の加熱温度が450℃未満ではその効果が充分に
得られず、一方580℃を越えれば共晶溶融のおそれが
ある。また均質化処理の加熱時間が1詩間未満でもその
効果がなく、一方48時間を越える良時間加熱してもそ
れ以上均質化処理の効果は増大せず、いたずらにコスト
上昇を招くだけである。したがって均質化処理は450
〜580℃の湿度域で1〜48時間行なうこととした。
Next, the ingot is subjected to a homogenization treatment to improve formability and to make the crystal grains fine and uniform. If the heating temperature for this homogenization treatment is less than 450°C, the effect will not be sufficiently obtained, while if it exceeds 580°C, there is a risk of eutectic melting. Furthermore, if the heating time for homogenization treatment is less than one hour, there is no effect, and on the other hand, heating for more than 48 hours will not further increase the effect of homogenization treatment and will only lead to an unnecessary increase in costs. . Therefore, the homogenization process is 450
The test was carried out in a humidity range of ~580°C for 1 to 48 hours.

均質化処理後の鋳塊は常法にしたがって圧延し、所要の
板厚とする。この圧延は、熱間圧延のみによって行なっ
ても良く、また熱間圧延と冷間圧延とを組合せても良い
The ingot after the homogenization treatment is rolled according to a conventional method to obtain the required thickness. This rolling may be performed only by hot rolling, or may be a combination of hot rolling and cold rolling.

圧延後の板に対しては溶体化処理を施して急速冷却(焼
入れ)する。ここで溶体化処理温度が500℃未満では
溶体化が不充分で充分な強度が得られず、一方580℃
を越えれば共晶溶融のおそれがあるから、溶体化処理温
度は500〜580℃とした。またその溶体化処理温度
における保持時間は、20秒未満では溶体化が完了しな
いことがあり、したがって20秒以上保持する必要があ
るが、好ましくは1分以上保持することが望ましい。溶
体化処理温度保持後の急速冷却(焼入れ)は、強制空冷
以上の冷却速度であれば充分であり、具体的には100
0℃/lllll1g、上の冷却速度が適当である。冷
却速度の点のみからは水焼入れが適当であるが、強制空
冷によれば歪のない焼入れが可能となる。なお溶体化処
理温度までの加熱昇温速度は特に限定しないが、結晶粒
をより微細とするためには、急速加熱が好ましく、した
がって急速連続熱処理炉を用いることができる。
After rolling, the plate is subjected to solution treatment and rapidly cooled (quenched). If the solution treatment temperature is less than 500℃, the solution treatment will be insufficient and sufficient strength will not be obtained;
If the temperature exceeds this temperature, there is a risk of eutectic melting, so the solution treatment temperature was set at 500 to 580°C. Further, if the holding time at the solution treatment temperature is less than 20 seconds, the solution treatment may not be completed, so it is necessary to hold the temperature for 20 seconds or more, but preferably for 1 minute or more. Rapid cooling (quenching) after solution treatment temperature maintenance is sufficient if the cooling rate is higher than forced air cooling, specifically 100
A cooling rate of 0°C/lllllg is suitable. Although water quenching is appropriate from the standpoint of cooling rate alone, forced air cooling allows quenching without distortion. Note that the rate of heating to the solution treatment temperature is not particularly limited, but in order to make the crystal grains finer, rapid heating is preferable, and therefore a rapid continuous heat treatment furnace can be used.

上述のように溶体化処理−焼入れを行なった後は、常法
にしたがって常法時効すれば良い。
After performing the solution treatment and quenching as described above, conventional aging may be performed according to a conventional method.

このようにして得られたアルミニウム合金圧延板を実際
に使用するにあたっては、プレス加工等の成形加工を施
すのが通常であるが、既に述べたように成形加工性が良
好でリューダースマークの発生もないため、成形加工時
に不良品が発生するおそれが極めて少なく、したがって
歩留りが高くなるとともに生産性も良好となる。また成
形加工後に焼付塗装を行なう場合、塗料によっても異な
るが通常は150〜250℃程度で加熱して塗料を焼付
けるが、この塗装焼付工程では既に述べたように強度が
一層上昇し、最終的に高強度の焼付塗装成形品を得るこ
とができる。
When actually using the aluminum alloy rolled sheet obtained in this way, it is usual to perform forming processes such as press working, but as already mentioned, the formability is good and the Lüders mark does not occur. Therefore, there is extremely little risk of producing defective products during molding, resulting in high yield and good productivity. In addition, when baking paint is applied after molding, the paint is usually baked at a temperature of 150 to 250°C, although this varies depending on the paint.As mentioned above, this paint baking process further increases the strength of the final product. It is possible to obtain high-strength baking-painted molded products.

実施例 [実ゐ例1] 第1表に示すような成分組成を有する合金番号1〜5の
本発明合金および合金番号6〜10の比較合金を常法に
したがって澄製して連続鋳造し、得られた鋳塊に対し第
2表中に示す均質化処理を施した。次いで4■厚まで熱
間圧延した後、1.0mi厚まで冷間圧延し、第2表中
の最終熱処理の欄に示すような溶体化処理もしくは最終
焼鈍を施し、その後2週間室温に放置して常温時効した
。常温時効後の機械的特性および成形加工性を調べた結
果を第3表に示す。
Examples [Example 1] The alloys of the present invention with alloy numbers 1 to 5 and comparative alloys with alloy numbers 6 to 10 having the compositions shown in Table 1 were clarified and continuously cast according to a conventional method. The obtained ingots were subjected to the homogenization treatment shown in Table 2. Then, it was hot rolled to a thickness of 4mm, then cold rolled to a thickness of 1.0mm, subjected to solution treatment or final annealing as shown in the column of final heat treatment in Table 2, and then left at room temperature for two weeks. It was aged at room temperature. Table 3 shows the results of examining the mechanical properties and moldability after aging at room temperature.

またその常温時効後の板に対し、成形加工後のtl焼付
工程による強度の変化を調べるため、成形加工に対応す
る5%冷間加工もしくは10%冷間加工を施し、ざらに
塗装焼付に相当する175’Cx1時間の加熱処理を、
冷間加工を行なわなかったもの(0%冷間加工材)、お
よび5%冷間加工材、10%冷間加工材について行ない
、各段階での強度を調べた。その結果を第4表に示す。
In addition, in order to investigate the change in strength due to the TL baking process after the room temperature aging, we applied 5% cold working or 10% cold working corresponding to the forming process, which roughly corresponds to paint baking. 175'C x 1 hour heat treatment,
The strength was examined at each stage for those that had not been cold worked (0% cold worked material), 5% cold worked material, and 10% cold worked material. The results are shown in Table 4.

第3表から明らかなように、本発明合金1〜7はいずれ
も張り出し性、曲げ性が優れ、かつリューダースマーク
の発生もなく、成形加工性が優れていることが判る。ま
た第4表から、本発明合金では成形加工後の塗装焼付工
程で強度が向上し、最終的に35 kQ/−以上の高い
引張強度を有する焼付塗装成形品が得られることが明ら
かである。
As is clear from Table 3, all of the alloys 1 to 7 of the present invention have excellent stretchability and bendability, and also have no Lüders marks, indicating that they have excellent moldability. Furthermore, from Table 4, it is clear that the strength of the alloy of the present invention is improved in the paint baking step after forming, and finally baked painted molded products having a high tensile strength of 35 kQ/- or more can be obtained.

[実施例2] 第1表の本発明合金1〜5について、実施例1ど同様に
連続鋳造、均質化処理、熱間圧延および冷間圧延を施し
て 1.0mm厚の冷延板を得た。その冷延板に対し、
溶体化処理−焼入れとして、急速加熱して540℃で6
0秒保持した後1200℃/鵬の冷却速度で強制空冷す
る処理を施した。その後2週間室温に保持して常温時効
した後の機械的特性、成形加工性を調べた結果を第5表
に示す。
[Example 2] Inventive alloys 1 to 5 in Table 1 were subjected to continuous casting, homogenization treatment, hot rolling, and cold rolling in the same manner as in Example 1 to obtain cold rolled sheets with a thickness of 1.0 mm. Ta. For the cold-rolled plate,
Solution treatment - as quenching, rapidly heated to 540 °C for 6
After holding for 0 seconds, forced air cooling was performed at a cooling rate of 1200° C./h. Table 5 shows the results of examining the mechanical properties and moldability after being kept at room temperature for two weeks and aging at room temperature.

第5表から、本発明合金の場合には溶体化処理を強制空
冷で行なった場合も優れた灘械的特性、成形加工性が得
られることが明らかである。
From Table 5, it is clear that in the case of the alloy of the present invention, excellent mechanical properties and formability can be obtained even when the solution treatment is performed by forced air cooling.

発明の効果 以上の実滴例からも明らかなようにこの発明の成形加工
用アルミニウム合金圧延板は、張り出し性や曲げ性が優
れかつリューダースマークの発生がない等、成形加工性
が優れており、しかも強度も充分であって、特に成形加
工後に焼付塗装を行なう場合に塗装焼付工程で強度が上
昇して最終的に著しく高強度の焼付塗装成形品を得るこ
とができ、したがって特に自動車車体ボディシートの如
く、焼付塗装が施されて使用される高強度成形品の用途
に最適なものである。まこの発明のアルミニウム合金圧
延板は、主要元素としては通常の圧延板、押出材、鋳物
等に最も広く用いられているSi、MQおよび微量のC
uを含んでいるだけであるため、他の合金のスクラップ
の使用が容易であり、また逆にこの発明の圧延板のスク
ラップを他の合金、他の用途に使用することも容易であ
って、スクラップ処理性が良好であり、経済的にも有利
である。
Effects of the Invention As is clear from the actual droplet examples, the rolled aluminum alloy plate for forming of the present invention has excellent formability, such as excellent stretchability and bendability, and no Lüders marks. Moreover, it has sufficient strength, and especially when baking paint is applied after molding, the strength increases in the paint baking process, and it is possible to finally obtain a baking-painted molded product with extremely high strength.Therefore, it is especially suitable for automobile bodies. It is ideal for use in high-strength molded products such as sheets that are baked and used. The aluminum alloy rolled plate of this invention contains Si, MQ, and a trace amount of C, which are most widely used in ordinary rolled plates, extruded materials, castings, etc., as main elements.
Since it only contains u, it is easy to use scraps of other alloys, and conversely, it is also easy to use scraps of the rolled plate of this invention for other alloys and other uses. It has good scrap disposal properties and is economically advantageous.

なおこの発明のアルミニウム合金圧延板は、前述のよう
に自動車車体のボディシートにJ1遍なものであるが、
強度が要求される成形加工品のその他の用途、例えばホ
イールやオイルタンク、エアクリーナー等の自動車部品
、あるいは各種キャップやブラインド、アルミ化、家随
用器物、計器カバー、電気機器のシャーシー等に用いて
も侭れた性能を発揮し得ることは勿論である。
The aluminum alloy rolled sheet of the present invention is used as a J1 body sheet for automobile bodies as described above.
Other uses of molded products that require strength, such as automobile parts such as wheels, oil tanks, and air cleaners, various caps and blinds, aluminization, household appliances, instrument covers, chassis of electrical equipment, etc. Of course, it is possible to exhibit inferior performance even if the

第2表:熱処理条件Table 2: Heat treatment conditions

Claims (2)

【特許請求の範囲】[Claims] (1)Si1.2%(重量%、以下同じ)を越え1.5
%以下、Mg0.25%以上0.85%以下、Fe0.
05%以上0.4%以下、Cu0.3%以上1.5%以
下を含有し、さらにMn0.05%以上0.6%以下、
Cr0.05%以上0.3%以下、Zr0.05%以上
0.15%以下のうちから選ばれた1種または2種以上
を含有し、残部がAlおよび不可避的不純物よりなるこ
とを特徴とする成形加工用アルミニウム合金圧延板。
(1) Si exceeding 1.2% (weight%, same hereinafter) and 1.5
% or less, Mg 0.25% or more and 0.85% or less, Fe0.
Contains 0.05% or more and 0.4% or less, Cu 0.3% or more and 1.5% or less, and Mn 0.05% or more and 0.6% or less,
It is characterized by containing one or more selected from 0.05% to 0.3% of Cr and 0.05% to 0.15% of Zr, with the remainder consisting of Al and inevitable impurities. Aluminum alloy rolled plate for forming processing.
(2)Si1.2%(重量%、以下同じ)を越え1.5
%以下、Mg0.25%以上0.85%以下、Fe0.
05%以上0.4%以下、Cu0.3%以上1.5%以
下を含有し、さらにMn0.05%以上0.6%以下、
Cr0.05%以上0.3%以下、Zr0.05%以上
0.15%以下のうちから選ばれた1種または2種以上
を含有し、残部がAlおよび不可避的不純物よりなるア
ルミニウム合金鋳塊に対し、450〜580℃の温度で
1〜48時間均質化処理を施し、次いで所要の板厚まで
圧延した後、500〜580℃の範囲内の温度に20秒
以上保持し、続いて急速冷却して、室温で時効すること
を特徴とするアルミニウム合金圧延板の製造方法。
(2) Si exceeding 1.2% (weight%, same hereinafter) and 1.5
% or less, Mg 0.25% or more and 0.85% or less, Fe0.
Contains 0.05% or more and 0.4% or less, Cu 0.3% or more and 1.5% or less, and Mn 0.05% or more and 0.6% or less,
Aluminum alloy ingot containing one or more selected from 0.05% to 0.3% of Cr, 0.05% to 0.15% of Zr, and the balance consisting of Al and inevitable impurities. The material is subjected to homogenization treatment at a temperature of 450 to 580°C for 1 to 48 hours, then rolled to the required thickness, held at a temperature in the range of 500 to 580°C for 20 seconds or more, and then rapidly cooled. A method for producing an aluminum alloy rolled sheet, which comprises aging at room temperature.
JP4336885A 1985-03-05 1985-03-05 Rolled aluminum alloy sheet for forming and its manufacture Pending JPS61201749A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4336885A JPS61201749A (en) 1985-03-05 1985-03-05 Rolled aluminum alloy sheet for forming and its manufacture

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4336885A JPS61201749A (en) 1985-03-05 1985-03-05 Rolled aluminum alloy sheet for forming and its manufacture

Publications (1)

Publication Number Publication Date
JPS61201749A true JPS61201749A (en) 1986-09-06

Family

ID=12661900

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4336885A Pending JPS61201749A (en) 1985-03-05 1985-03-05 Rolled aluminum alloy sheet for forming and its manufacture

Country Status (1)

Country Link
JP (1) JPS61201749A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62177143A (en) * 1986-01-30 1987-08-04 Kobe Steel Ltd Aluminum alloy sheet excellent in formability and baking hardening and its production
JPS62278245A (en) * 1986-02-21 1987-12-03 Sky Alum Co Ltd Aluminum-alloy rolled plate for forming and its production
JPS6411937A (en) * 1987-07-02 1989-01-17 Sky Aluminium Aluminum alloy rolled plate for forming and its production
US4808247A (en) * 1986-02-21 1989-02-28 Sky Aluminium Co., Ltd. Production process for aluminum-alloy rolled sheet
JPH0565587A (en) * 1991-09-05 1993-03-19 Sky Alum Co Ltd Aluminum alloy rolled sheet for forming and its production
WO1996003748A1 (en) * 1994-07-27 1996-02-08 Minnesota Mining And Manufacturing Company Tape cartridge base plate comprising a novel aluminum alloy
CN104093868A (en) * 2012-02-10 2014-10-08 株式会社神户制钢所 Aluminum alloy sheet for connecting components and manufacturing process therefor
CN104093868B (en) * 2012-02-10 2016-11-30 株式会社神户制钢所 Connection member aluminium alloy plate and manufacture method thereof

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3392062A (en) * 1964-08-27 1968-07-09 Alusuisse Process of producing heat-treatable strips and sheets from heat-treatable aluminum alloys with a copper content of less than 1%
JPS5319117A (en) * 1976-08-05 1978-02-22 Aluminum Co Of America Modified aluminium structure
JPS5794546A (en) * 1980-12-05 1982-06-12 Mitsubishi Alum Co Ltd Al alloy plate with high press formability and enameling hardenability

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3392062A (en) * 1964-08-27 1968-07-09 Alusuisse Process of producing heat-treatable strips and sheets from heat-treatable aluminum alloys with a copper content of less than 1%
JPS5319117A (en) * 1976-08-05 1978-02-22 Aluminum Co Of America Modified aluminium structure
JPS5794546A (en) * 1980-12-05 1982-06-12 Mitsubishi Alum Co Ltd Al alloy plate with high press formability and enameling hardenability

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62177143A (en) * 1986-01-30 1987-08-04 Kobe Steel Ltd Aluminum alloy sheet excellent in formability and baking hardening and its production
JPH0569898B2 (en) * 1986-01-30 1993-10-04 Kobe Steel Ltd
JPS62278245A (en) * 1986-02-21 1987-12-03 Sky Alum Co Ltd Aluminum-alloy rolled plate for forming and its production
US4808247A (en) * 1986-02-21 1989-02-28 Sky Aluminium Co., Ltd. Production process for aluminum-alloy rolled sheet
JPS6411937A (en) * 1987-07-02 1989-01-17 Sky Aluminium Aluminum alloy rolled plate for forming and its production
JPH0480109B2 (en) * 1987-07-02 1992-12-17 Sky Aluminium
JPH0565587A (en) * 1991-09-05 1993-03-19 Sky Alum Co Ltd Aluminum alloy rolled sheet for forming and its production
WO1996003748A1 (en) * 1994-07-27 1996-02-08 Minnesota Mining And Manufacturing Company Tape cartridge base plate comprising a novel aluminum alloy
CN104093868A (en) * 2012-02-10 2014-10-08 株式会社神户制钢所 Aluminum alloy sheet for connecting components and manufacturing process therefor
CN104093868B (en) * 2012-02-10 2016-11-30 株式会社神户制钢所 Connection member aluminium alloy plate and manufacture method thereof

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