JPH0588302B2 - - Google Patents
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- JPH0588302B2 JPH0588302B2 JP4572086A JP4572086A JPH0588302B2 JP H0588302 B2 JPH0588302 B2 JP H0588302B2 JP 4572086 A JP4572086 A JP 4572086A JP 4572086 A JP4572086 A JP 4572086A JP H0588302 B2 JPH0588302 B2 JP H0588302B2
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Description
産業上の利用分野
この発明はJIS 2000番系、6000番系あるいは
7000番系で代表される展伸用熱処理型アルミニウ
ム合金からなる微細結晶粒を有するアルミニウム
合金材料の製造方法に関し、特に超塑性加工用材
料に最適なアルミニウム合金材料の製造方法に関
するものである。
従来の技術
近年に至り微細結晶粒を有する金属材料の超塑
性現象を利用して超塑性加工を行なう技術が注目
を集めるようになつている。微細結晶粒による超
塑性現象は、展伸用熱処理型アルミニウム合金に
おいても認められるものであり、結晶粒を25μm
程度以下の微細なものとすれば所定の超塑性温度
域での加工により超塑性を呈することが知られて
いる。
従来、このような超塑性加工が可能となる程度
に結晶粒が微細な熱処理型アルミニウム合金圧延
板を製造する方法としては、
(イ) 金属間化合物の粗大粒子を過時効処理により
析出させて、温間加工で歪を与える方法(例え
ば特開昭53−132420号)、
(ロ) 溶体化処理後急冷して、冷間圧延にて歪を与
える方法(例えば特開昭60−86251号)、
(ハ) 溶体化処理温度から徐冷して冷間圧延する方
法(例えば特開昭60−12 5354号)、
が知られている。
発明が解決すべき問題点
前述のような微細結晶粒を有するアルミニウム
合金圧延板を製造するための各方法のうち、(イ)の
方法では、過時効処理や温間加工を行なうために
生産性が低くならざるを得ないという問題があ
る。また(ロ)の方法では、結晶粒は微細化すること
ができるが、溶体化処理・急冷後の圧延が困難と
なる問題がある。さらに(ハ)の方法では、圧延性は
良いものの、微細な結晶粒を得るためには90%以
上もの強冷間加工が必要となる問題がある。
この発明は以上の事情を背景としてなされたも
ので、生産性低下、冷間圧延性低下などの諸問題
を招くことなく、超塑性加工に適した微細な結晶
粒を有する材料を実際的に得ることができる方法
を提供することを目的とするものである。
問題点を解決するための手段
この発明の方法は、基本的には、溶体化処理温
度近傍の温度からの徐冷によつて析出粒子を粗大
に析出させて、これを再結晶核とし、しかもその
後の溶体化処理温度の40〜70%の温度域からの焼
入れによつて、冷間圧延性を溶体化処理温度から
焼入れした場合(完全焼入れの場合)よりも向上
させるとともに残留する合金元素の固溶もしくは
微細析出を図つてマトリツクス内の転位密度、変
形帯を多くし、もつて再結晶時における核発生頻
度を向上させ、結晶粒を微細化させるものであ
る。
具体的には、第1発明の方法は、展伸用熱処理
型アルミニウム合金であつて、しかもMn0.05〜
1.5%、Cr0.05〜0.4%、Zr0.05〜0.3%のうちの1
種または2種以上を含有するアルミニウム合金を
素材とし、その合金鋳塊に対して均質化処理とし
て、その合金の溶体化処理温度の90%以上の温度
で0.5〜24時間加熱し、その後0.001〜0.05℃/sec
の範囲内の冷却速度で溶体化処理温度の70〜90%
の温度まで冷却し、その温度から直ちにもしくは
その温度に24時間以内保持してから熱間圧延を開
始して、溶体化処理温度の40〜70%の温度で熱間
圧延を終了させ、引続いて0.1℃/sec以上の冷却
速度で180℃以下、好ましくは室温まで冷却し、
その後加工率60%以上の冷間加工を行なつた後、
その合金の再結晶温度以上の温度に1℃/sec以
上の昇温速度で昇温させて再結晶させることを特
徴とするものである。
また第2発明の方法は、展伸用熱処理型アルミ
ニウム合金であつて、しかもMn0.05〜1.5%、
Cr0.05〜0.4%、Zr0.05〜0.3%のうちの1種また
は2種以上を含有するアルミニウム合金を素材と
し、その合金鋳塊に対して均質化処理として、そ
の合金の溶体化処理温度の90%以上の温度で0.5
〜24時間加熱し、その後0.001〜0.05℃/secの範
囲内の冷却速度で室温まで冷却し、次いで溶体化
処理温度の70〜90%の温度に再加熱して、直ちに
もしくはその温度に24時間以内保持してから熱間
圧延を開始し、溶体化処理温度の40〜70%の温度
で熱間圧延を終了させ、引続いて0.1℃/sec以上
の冷却速度で180℃以下、好ましくは室温まで冷
却し、その後加工率60%以上の冷間加工を行なつ
た後、その合金の再結晶温度以上の温度に1℃/
sec以上の昇温速度で昇温させて再結晶させるこ
とを特徴とするものである。
作 用
先ずこの発明において対象とするアルミニウム
合金について説明する。
この発明の方法は、A−Cu系合金(JIS
2000番系)、A−Mg−Si系合金(JIS 6000番
系)、A−Zn−Mg系合金(JIS 7000番系)で
代表される所謂展伸用の熱処理型合金には全て適
用可能である。但し、これらの熱処理型合金にお
いて通常含有されているCu、あるいはMgおよび
Si、あるいはZnおよびMg等のほか、必須成分と
して特にMn0.05〜1.5%、Cr0.05〜0.4%、Zr0.05
〜0.3%のうちから選ばれた1種または2種以上
が含有されていることが必要である。すなわち、
Mn、Cr、Zrはいずも金属間化合物析出粒子の生
成を通じて結晶粒微細化に有効な元素であつて、
これらを含有させることによつてこの発明で目的
とする超塑性加工可能な微細結晶組織を得ること
が可能となる。ここでMn、Cr、またはZrの含有
量が0.05%未満では微細な結晶粒を得ることが困
難となり、一方Mn1.5%以上、もしくはCr0.4%
以上、またはZr0.3%以上を含有する場合には鋳
造時にこれらの元素が充分に固溶されずに巨大金
属間化合物が発生して充分な伸びが得られなくな
る。したがつてMnは0.05〜1.5%、Crは0.05〜0.4
%、Zrは0.05〜0.3%の範囲内とした。
なおここで展伸用熱処理型合金とは最も広い意
味で使用するものとし、前述のようにA−Cu
系合金である2000番系合金、例えばJIS規格や
AA規格の2014合金、2017合金、2024合金、2219
合金、あるいはA−Mg−Si系合金である6000
番系合金、例えば6061合金、さらにはA−Zn
−Mg系合金である7000番系合金、例えば7075合
金、7475合金、7N01合金、7003合金等がある。
そしてこの発明の場合、前述のようにMn、Cr、
Zr以外の成分組成は、熱処理型となるような成
分組成であれば特に限定されず、用途や要求され
る特性等に応じて定めれば良いが、例えばA−
Cu系合金の場合、Cuを1.5〜6.3%程度含有し、さ
らに必要に応じてMgを0.2〜1.8%程度、Siを0.2
〜1.3%程度含有するものとすれば良く、またA
−Mg−Si系合金の場合、Siを0.20〜1.2%程度、
Mgを0.35〜1.5%程度含有し、さらに必要に応じ
てCuを0.10〜0.40%程度含有するものとすれば良
く、またA−Zn−Mg系合金の場合Znを0.8〜
6.1%、Mgを0.5〜2.9%程度含有し、さらに必要
に応じてCuを1.2〜2.0%程度含有するものとすれ
ば良い。
次にこの発明の方法におけるプロセスについて
説明する。
先ず常法にしたがつて連続鋳造もしくは半連続
鋳造等によつて前述のようにMn、Cr、Zrの1種
以上を含有する熱処理型アルミニウム合金の鋳塊
を製造する。
次いでその鋳塊に対する均質化処理を施す。こ
の均質化処理は、対象となる合金の溶体化処理温
度近傍の温度、すなわち溶体化処理温度の90%以
上の温度(但し摂氏温度の90%以上;以下の温度
の%についても同様)で0.5〜24時間加熱するこ
とによつて行なう。ここで均質化処理の温度が溶
体化処理温度の90%未満では均質化が不充分であ
り、また合金成分元素の溶体化が不充分となる。
均質化処理時間が0.5時間未満でも均質化、溶体
化が不充分であり、一方24時間を越えればその効
果は飽和し、経済的に不利となるだけである。
なおここで溶体化処理温度は、対象とする合金
のα相領域における固相線温度と溶解度曲線との
間の温度であり、具体的な最適温度は合金組成に
よつて異なるが、典型的にはAA規格あるいは
JIS規格に代表的な溶体化処理温度が示されてお
り、これによれば2014合金の場合は495〜505℃、
2017合金では495〜510℃、2024合金(板材)では
490〜500℃、6061合金では515〜550℃、7075合金
(板材)では460〜500℃、7475合金では460〜499
℃、7N01合金では約450℃が最適とされている。
したがつてこの発明で溶体化処理温度のX%と
は、上述のような各合金の溶体化処理最適温度の
X%とすることが好ましい。
上述の均質化処理は、0.001〜0.05℃/secの範
囲内の冷却速度で溶体化処理温度の70〜90%の温
度まで冷却(第1発明の場合)し、必要に応じて
その温度に24時間以内保持し、その温度で熱間圧
延を開始する。あるいはまた均質化処理後、
0.001〜0.05℃/secの範囲内の冷却速度で室温ま
で冷却(第2発明の場合)し、その後、溶体化処
理温度の70〜90%の温度まで再加熱し、必要に応
じてその温度に24時間以内保持し、その温度で熱
間圧延を開始する。このような均質化処理後の
0.001〜0.05℃/secの冷却速度での徐冷によつて、
強化成分元素の粒子が粗大に析出される。ここ
で、冷却速度が0.05℃/sec以上では析出が不充
分となり、一方0.001℃/sec未満の冷却速度では
生産性が阻害されて経済的に不利となる。また熱
間圧延開始温度が溶体化処理温度の70%未満では
熱間圧延が困難となり、一方溶体化処理温度の90
%を越える場合は、粗大析出物の析出が少な過ぎ
て、最終板での結晶粒微細化が不充分となる。
上述のようにして溶体化処理温度の70〜90%の
温度域で開始した熱間圧延は、溶体化処理温度の
40〜70%の温度で終了させ、その温度から0.1
℃/sec以上の冷却速度で180℃以下、好ましくは
室温まで冷却することにより焼入れを行なう。こ
のように溶体化処理温度の40〜70%の温度から焼
入れることによつて、冷間圧延性が完全焼入れの
場合(溶体化処理温度から焼入れる場合)ほど低
下することなく、しかも析出せずに残留している
合金元素の固溶もしくは微細析出を図つて固溶や
微細析出によるマトリツクス内の転位密度、変形
帯の増大を図り、最終板において微細結晶粒組織
を得ることが可能となるのである。ここで、溶体
化処理温度の40%より低い温度から冷却(焼入
れ)した場合は、固溶・時効による転位の導入が
少なくなつて結晶粒微細化の効果が得られない。
一方溶体化処理温度の70%を越える高温から冷却
(焼入れ)した場合は、焼きが入り過ぎて硬質化
し、次の冷間圧延が困難となる。また焼入れのた
めの冷却速度が0.1℃/sec未満では焼きが充分に
入らず、その後の圧延による歪の導入が不充分と
なつて結晶粒微細化が達成されない。
また焼入終了時の温度は180℃以下とし、でき
れば室温まで焼入れることが望ましい。180℃よ
り高温で焼入れを終了すれば、その後の冷却で粗
大析出物が形成され、焼入れの効果が全く認めら
れない。焼入終了時の温度は低いほどマトリツク
ス中に固溶もしくは微細粒子として析出する溶質
量は多く、その後の冷間圧延でマトリツクス内の
転位密度や変形帯が増加し、最終的に微細結晶粒
組織を得やすい。
なお上述のように溶体化処理温度の40〜70%の
温度で熱間圧延を終了させてその温度から0.1
℃/sec以上の冷却速度で焼入れするためには、
熱間圧延を終了したコイルに、引続き圧延クーラ
ントを付加して冷却するか、あるいはスプレー水
冷または強制空冷装置を用いて冷却すれば良く、
いずれの手段も量産的規模で効率良く適用するこ
とができる。
溶体化処理温度の40〜70%の温度からの焼入れ
後には、60%以上の加工率で冷間圧延等の冷間加
工を行なう。この冷間加工は歪を導入してその後
の再結晶時における結晶粒微細化を図るためのも
のであり、加工率が60%未満では歪の導入が不充
分となり、結晶粒の微細化が充分に図れない。
上述の冷間加工後には、対象合金の再結晶温度
以上に1℃/sec以上の加熱速度で昇温させて、
再結晶させる。この再結晶にあたつて昇温速度が
速いほど再結晶粒微細化には有利となり、昇温速
度が1℃/sec未満では超塑性加工に適した微細
結晶粒が得られないから、昇温速度を1℃/sec
以上に限定した。このように1℃/sec以上で急
速加熱するためには、具体的にはソルトバスや、
連続空気加熱炉を用いれば良い。なお再結晶温度
は合金の種類によつて異なるが、その合金の溶体
化処理温度は必ず再結晶温度以上となつているか
ら、実際の操業にあたつては溶体化処理温度を目
途に加熱すれば充分である。なおまた再結晶のた
めの加熱後は常法にしたがつて水焼入れすれば良
い。
以上のように、熱間圧延前の均質化処理を溶体
化処理温度の90%以上の温度域で行なつた後、
0.001〜0.05℃/secの冷却速度で徐冷して粗大金
属間化合物粒子を粗大に析出させ、熱間圧延終了
に引続いてもしくは熱間圧延後、溶体化処理温度
の40〜70%の温度域から0.1℃/sec以上の冷却速
度で焼入れることにより、残留している合金元素
の固溶もしくは微細析出を図り、さらに60%以上
の冷間加工を行なつてから再結晶させることによ
つて、再結晶粒を著しく微細化することができ
る。ここで、再結晶前に歪を導入するための冷間
加工としてはさほど大きな加工率は必要なく、前
述のように加工率60%以上であれば最終的に微細
結晶粒を得ることができるから、生産性の低下や
冷間圧延の困難を招くことなく冷間加工を実施す
ることができる。
実施例
[実施例1]
第1表に示す成分組成の合金1〜5について、
400mm厚のスラブをDC鋳造法により鋳造した。得
られたスラブに対し第2表に示す加熱条件、冷却
条件A〜Hで均質化処理および熱間圧延を施し
て、6mm厚の熱延板とした。次いで冷間圧延率80
%で圧延し、再結晶のために各合金の溶体化処理
温度にソルトバスにより急速加熱し、10分間保持
した後、水焼入れした。また合金1について条件
記号Aにて均質化処理、熱間圧延を行なつたもの
の一部は、冷間圧延率80%で圧延した後、比較法
として0.01℃/secで昇温させて再結晶させた
(記号)。
以上のようにして得られた再結晶後の最終板の
板面の結晶粒度を調べた結果、第3表に示す結果
が得られた。
第3表から、所要量のMn、Cr、もしくはZrを
含有する発明合金1〜4についてこの発明で規定
する条件で処理した圧延板は、いずれも結晶粒径
が11μm以下と著しく小さいことが明らかであり、
これらの圧延板については充分に超塑性加工をな
し得ることが判明した。
一方Mn、Zr、Crを実質的に含まない比較合金
5についてこの発明の条件範囲内で処理した場合
(条件記号E)には結晶粒径が35μmと大きくなつ
た。また条件記号Fは溶体化処理温度の90%以上
の温度での均質化処理を行なわなかつたものであ
り、この場合も結晶粒径が33μmと大きくなつた。
さらに条件記号Gは熱間圧延開始温度が高過ぎた
例であり、この場合も結晶粒径が48μmと大きく
なつた。また条件記号Hは、熱間圧延終了後の溶
体化処理温度の40〜70%の温度からの焼入れ
(0.1℃/sec以上の冷却)を行なわなかつたもの
であり、この場合も結晶粒径が33μmと大きかつ
た。さらに条件記号は、再結晶焼入れのための
加熱を徐速昇温で行なつた例であり、この場合に
は結晶粒径が350μmと粗大化してしまつた。
Industrial Application Field This invention is applicable to JIS 2000 series, 6000 series or
The present invention relates to a method of manufacturing an aluminum alloy material having fine grains made of a heat-treatable aluminum alloy for drawing, typified by the No. 7000 series, and in particular to a method of manufacturing an aluminum alloy material optimal for superplastic working materials. BACKGROUND OF THE INVENTION In recent years, techniques for performing superplastic working using the superplastic phenomenon of metal materials having fine crystal grains have been attracting attention. The superplastic phenomenon caused by fine crystal grains is also observed in heat-treated aluminum alloys for drawing, and when the crystal grains are reduced to 25 μm
It is known that if it is made as fine as possible, it will exhibit superplasticity when processed in a predetermined superplastic temperature range. Conventionally, methods for manufacturing heat-treated rolled aluminum alloy sheets with grains fine enough to enable such superplastic working include (a) precipitating coarse particles of intermetallic compounds through overaging treatment; A method of applying strain through warm working (e.g., JP-A-53-132420); (b) A method of rapidly cooling after solution treatment and applying strain through cold rolling (e.g., JP-A-60-86251); (c) A method of slow cooling from the solution treatment temperature and cold rolling (for example, JP-A-60-12-5354) is known. Problems to be Solved by the Invention Among the methods for manufacturing aluminum alloy rolled sheets having fine grains as described above, method (a) requires overaging treatment and warm working, which reduces productivity. The problem is that it has no choice but to become low. Further, in the method (b), the crystal grains can be made finer, but there is a problem that rolling after solution treatment and rapid cooling becomes difficult. Furthermore, although the method (c) has good rolling properties, there is a problem in that intense cold working of 90% or more is required to obtain fine grains. This invention was made against the background of the above circumstances, and it is possible to practically obtain a material having fine crystal grains suitable for superplastic working without causing problems such as a decrease in productivity and a decrease in cold rollability. The purpose is to provide a method that can be used. Means for Solving the Problems The method of the present invention basically consists of coarsely precipitating precipitated particles by slow cooling from a temperature near the solution treatment temperature, and using these as recrystallization nuclei. Subsequent quenching from 40 to 70% of the solution treatment temperature improves cold rollability compared to when quenching from the solution treatment temperature (complete quenching) and removes residual alloying elements. It aims at solid solution or fine precipitation to increase the dislocation density and deformation bands in the matrix, thereby increasing the frequency of nucleation during recrystallization and making the crystal grains finer. Specifically, the method of the first invention is a heat-treated aluminum alloy for drawing, and Mn0.05~
1.5%, Cr0.05~0.4%, Zr0.05~0.3%
An aluminum alloy containing one or more species is used as a material, and the alloy ingot is homogenized by heating at a temperature of 90% or more of the solution treatment temperature of the alloy for 0.5 to 24 hours, and then 0.001 to 0.05℃/sec
70-90% of solution treatment temperature with cooling rate within the range of
After cooling to a temperature of to 180°C or less, preferably to room temperature, at a cooling rate of 0.1°C/sec or more,
After that, after performing cold working at a processing rate of 60% or more,
The alloy is characterized by being recrystallized by raising the temperature to a temperature higher than the recrystallization temperature of the alloy at a heating rate of 1° C./sec or higher. Further, the method of the second invention is a heat-treated aluminum alloy for drawing, and furthermore, 0.05 to 1.5% of Mn and
An aluminum alloy containing one or more of Cr0.05~0.4% and Zr0.05~0.3% is used as a material, and the alloy ingot is subjected to homogenization treatment at a solution treatment temperature of the alloy. 0.5 at temperatures above 90% of
Heating for ~24 hours, then cooling to room temperature at a cooling rate in the range of 0.001-0.05 °C/sec, then reheating to a temperature of 70-90% of the solution treatment temperature, either immediately or at that temperature for 24 hours. Hot rolling is started after the temperature is maintained within 180°C, preferably at room temperature, and the hot rolling is completed at a temperature of 40 to 70% of the solution treatment temperature. After cooling to a temperature of 60% or more, the alloy is heated to a temperature higher than the recrystallization temperature of the alloy by 1℃/
This method is characterized by recrystallization by increasing the temperature at a rate of sec or more. Function First, the aluminum alloy targeted by this invention will be explained. The method of this invention uses an A-Cu alloy (JIS
It can be applied to all heat-treated alloys for expansion, such as A-Mg-Si alloys (JIS 6000 series), A-Mg-Mg alloys (JIS 7000 series). be. However, Cu, Mg and
In addition to Si, Zn, Mg, etc., essential components include Mn0.05-1.5%, Cr0.05-0.4%, Zr0.05
It is necessary that one or more selected from ~0.3% be contained. That is,
Mn, Cr, and Zr are all effective elements for grain refinement through the formation of intermetallic compound precipitated particles.
By containing these, it becomes possible to obtain a microcrystalline structure capable of superplastic processing, which is the objective of the present invention. Here, if the content of Mn, Cr, or Zr is less than 0.05%, it will be difficult to obtain fine crystal grains, whereas if the content of Mn, Cr, or Zr is less than 0.05%, it will be difficult to obtain fine crystal grains.
If the Zr content exceeds 0.3%, or if the Zr content exceeds 0.3%, these elements will not be sufficiently solid-dissolved during casting, resulting in the formation of giant intermetallic compounds, making it impossible to obtain sufficient elongation. Therefore, Mn is 0.05-1.5% and Cr is 0.05-0.4.
%, Zr was within the range of 0.05 to 0.3%. Note that the term heat-treatable alloy for drawing is used here in the broadest sense, and as mentioned above, A-Cu
2000 series alloys, such as JIS standards and
AA standard 2014 alloy, 2017 alloy, 2024 alloy, 2219
6000, which is an alloy or A-Mg-Si alloy
series alloys, such as 6061 alloy, and even A-Zn
- There are 7000 series alloys, which are Mg-based alloys, such as 7075 alloy, 7475 alloy, 7N01 alloy, and 7003 alloy.
In the case of this invention, as mentioned above, Mn, Cr,
The composition of components other than Zr is not particularly limited as long as it can be heat treated, and may be determined depending on the application and required characteristics. For example, A-
In the case of Cu-based alloys, it contains about 1.5 to 6.3% Cu, and if necessary, about 0.2 to 1.8% Mg and 0.2% Si.
It is sufficient that the content is about 1.3%, and A
-In the case of Mg-Si alloy, Si is about 0.20 to 1.2%,
It is sufficient to contain about 0.35 to 1.5% Mg, and if necessary, about 0.10 to 0.40% Cu, and in the case of an A-Zn-Mg alloy, Zn is about 0.8 to 1.5%.
6.1%, Mg about 0.5 to 2.9%, and Cu about 1.2 to 2.0% if necessary. Next, the process in the method of this invention will be explained. First, an ingot of a heat-treated aluminum alloy containing one or more of Mn, Cr, and Zr as described above is produced by continuous casting or semi-continuous casting according to a conventional method. Next, the ingot is subjected to homogenization treatment. This homogenization treatment is performed at a temperature close to the solution treatment temperature of the target alloy, that is, at a temperature of 90% or more of the solution treatment temperature (however, 90% or more of Celsius temperature; the same applies to the percentage of temperatures below). This is done by heating for ~24 hours. If the temperature of the homogenization treatment is less than 90% of the solution treatment temperature, homogenization will be insufficient and the alloying elements will not be sufficiently solutionized.
If the homogenization treatment time is less than 0.5 hours, homogenization and solutionization will be insufficient, while if it exceeds 24 hours, the effect will be saturated and it will only be economically disadvantageous. Note that the solution treatment temperature here is the temperature between the solidus temperature and the solubility curve in the α phase region of the target alloy, and the specific optimum temperature varies depending on the alloy composition, but typically is AA standard or
Typical solution treatment temperatures are shown in the JIS standard, and according to this, for 2014 alloy, it is 495-505℃,
495-510℃ for 2017 alloy, 2024 alloy (plate material)
490~500℃, 515~550℃ for 6061 alloy, 460~500℃ for 7075 alloy (plate material), 460~499 for 7475 alloy
℃, approximately 450℃ for 7N01 alloy is said to be optimal.
Therefore, in the present invention, X% of the solution treatment temperature is preferably X% of the optimal solution treatment temperature of each alloy as described above. The above-mentioned homogenization treatment is performed by cooling to a temperature of 70 to 90% of the solution treatment temperature at a cooling rate within the range of 0.001 to 0.05 °C/sec (in the case of the first invention), and heating to that temperature for 24 hours as necessary. The temperature is maintained within an hour and hot rolling is started at that temperature. Alternatively, after homogenization treatment,
Cool to room temperature at a cooling rate within the range of 0.001 to 0.05°C/sec (in the case of the second invention), then reheat to a temperature of 70 to 90% of the solution treatment temperature, and if necessary, heat to that temperature. Hold for less than 24 hours and start hot rolling at that temperature. After such homogenization process
By slow cooling at a cooling rate of 0.001-0.05℃/sec,
Coarse particles of the reinforcing element are precipitated. Here, if the cooling rate is 0.05° C./sec or more, precipitation will be insufficient, while if the cooling rate is less than 0.001° C./sec, productivity will be inhibited and this will be economically disadvantageous. In addition, if the hot rolling start temperature is less than 70% of the solution treatment temperature, hot rolling becomes difficult;
%, the precipitation of coarse precipitates will be too small and grain refinement in the final plate will be insufficient. Hot rolling started in the temperature range of 70 to 90% of the solution treatment temperature as described above is
Terminate at a temperature of 40-70%, from that temperature 0.1
Quenching is carried out by cooling to 180°C or less, preferably room temperature, at a cooling rate of 0°C/sec or more. By quenching at a temperature of 40 to 70% of the solution treatment temperature, the cold rollability does not decrease as much as with complete quenching (quenching from the solution treatment temperature), and furthermore, precipitation does not occur. It is possible to obtain a fine grain structure in the final plate by increasing the dislocation density and deformation band in the matrix by solid solution or fine precipitation of the remaining alloying elements. It is. Here, if cooling (quenching) is performed from a temperature lower than 40% of the solution treatment temperature, the introduction of dislocations due to solid solution/aging will be reduced and the effect of grain refinement will not be obtained.
On the other hand, if the material is cooled (quenched) from a high temperature that exceeds 70% of the solution treatment temperature, it becomes too hard and hard, making subsequent cold rolling difficult. Further, if the cooling rate for hardening is less than 0.1° C./sec, hardening will not occur sufficiently, strain will not be introduced sufficiently by subsequent rolling, and grain refinement will not be achieved. In addition, the temperature at the end of quenching should be 180°C or less, and if possible, it is desirable to quench to room temperature. If quenching is completed at a temperature higher than 180°C, coarse precipitates will be formed during subsequent cooling, and no quenching effect will be observed. The lower the temperature at the end of quenching, the greater the amount of solute that dissolves in the matrix or precipitates as fine particles, and the subsequent cold rolling increases the dislocation density and deformation bands in the matrix, ultimately resulting in a fine grain structure. Easy to get. As mentioned above, hot rolling is finished at a temperature of 40 to 70% of the solution treatment temperature, and the temperature is reduced by 0.1% from that temperature.
In order to harden at a cooling rate of ℃/sec or higher,
After hot rolling, the coil may be cooled by adding rolling coolant, or by using spray water cooling or forced air cooling equipment.
Either means can be efficiently applied on a mass production scale. After quenching at a temperature of 40 to 70% of the solution treatment temperature, cold working such as cold rolling is performed at a processing rate of 60% or more. This cold working is intended to introduce strain and refine the crystal grains during subsequent recrystallization. If the working rate is less than 60%, the introduction of strain will be insufficient and the grains will not be refined enough. I can't plan on it. After the above-mentioned cold working, the temperature is raised above the recrystallization temperature of the target alloy at a heating rate of 1°C/sec or more,
recrystallize. During this recrystallization, the faster the heating rate is, the more advantageous it is to refine the recrystallized grains, and if the heating rate is less than 1°C/sec, fine grains suitable for superplastic processing cannot be obtained. Speed 1℃/sec
limited to the above. In order to rapidly heat at 1°C/sec or more in this way, it is necessary to use a salt bath,
A continuous air heating furnace may be used. Although the recrystallization temperature differs depending on the type of alloy, the solution treatment temperature of the alloy is always higher than the recrystallization temperature, so in actual operation, heat should be aimed at the solution treatment temperature. It is sufficient. Furthermore, after heating for recrystallization, water quenching may be performed in accordance with a conventional method. As mentioned above, after performing homogenization treatment before hot rolling at a temperature range of 90% or more of the solution treatment temperature,
Gradual intermetallic compound particles are coarsely precipitated by slow cooling at a cooling rate of 0.001 to 0.05°C/sec, and subsequent to the completion of hot rolling or after hot rolling, a temperature of 40 to 70% of the solution treatment temperature is applied. By quenching at a cooling rate of 0.1°C/sec or more from a temperature range, the remaining alloying elements are dissolved or finely precipitated, and then cold worked by 60% or more and then recrystallized. As a result, recrystallized grains can be significantly refined. Here, a very large processing rate is not required for cold working to introduce strain before recrystallization, and as mentioned above, if the processing rate is 60% or more, fine crystal grains can be obtained in the end. , cold working can be carried out without reducing productivity or causing difficulties in cold rolling. Examples [Example 1] Regarding alloys 1 to 5 having the composition shown in Table 1,
A 400mm thick slab was cast using the DC casting method. The obtained slabs were subjected to homogenization treatment and hot rolling under the heating conditions and cooling conditions A to H shown in Table 2 to obtain hot rolled sheets with a thickness of 6 mm. Then cold rolling rate 80
%, and rapidly heated in a salt bath to the solution treatment temperature of each alloy for recrystallization, held for 10 minutes, and then water quenched. In addition, some of Alloy 1 that was homogenized and hot rolled under condition code A was rolled at a cold rolling rate of 80% and then recrystallized by raising the temperature at 0.01°C/sec as a comparative method. Let (symbol). As a result of examining the crystal grain size of the plate surface of the final plate after recrystallization obtained as described above, the results shown in Table 3 were obtained. From Table 3, it is clear that the rolled sheets of invention alloys 1 to 4 containing the required amount of Mn, Cr, or Zr treated under the conditions specified in this invention all have extremely small crystal grain sizes of 11 μm or less. and
It has been found that these rolled plates can be sufficiently subjected to superplastic working. On the other hand, when Comparative Alloy 5, which does not substantially contain Mn, Zr, and Cr, was treated within the condition range of the present invention (condition symbol E), the crystal grain size became as large as 35 μm. Furthermore, condition code F was a condition in which the homogenization treatment was not performed at a temperature of 90% or more of the solution treatment temperature, and in this case as well, the crystal grain size was as large as 33 μm.
Furthermore, condition symbol G is an example in which the hot rolling start temperature was too high, and in this case too, the crystal grain size became large at 48 μm. Condition code H means that quenching from 40 to 70% of the solution treatment temperature after hot rolling (cooling at 0.1°C/sec or more) is not performed, and in this case as well, the grain size is It was large at 33μm. Furthermore, the condition symbol is an example in which heating for recrystallization quenching was performed at a slow temperature increase, and in this case, the crystal grain size became coarse to 350 μm.
【表】【table】
【表】【table】
【表】【table】
【表】
[実施例2]
実施例1の合金1について、第2表の条件記号
Aに従つて均質化処理および熱間圧延するにあた
り、均質化処理後3×10-3℃/secの冷却速度で
室温まで冷却した後、熱間圧延開始温度まで再加
熱を行なつた。また実施例1の合金3について
も、第2表の条件記号Cに従つて均質化処理およ
び熱間圧延するにあたり、均質化処理後3×10-3
℃/secの冷却速度で室温まで冷却した後、熱間
圧延開始温度まで再加熱した。その他の条件は実
施例1と同様にして処理した。
得られた再結晶後の圧延板の結晶粒径は、合金
1では9μm、合金3では10μmであり、実施例1
の場合と同様に充分に微細化されていることが判
明した。
[実施例3]
実施例1の合金1および合金3について、それ
ぞれ第2表の条件記号A、Cに従つて均質化処理
および熱間圧延した後、圧延率80%の冷間圧延を
行ない、次いで連続焼鈍炉を用いて20℃/secの
昇温速度で合金1は480℃に、合金3は490℃に昇
温し、7分間で通板させ、炉の出側で水冷するこ
とにより連続的な再結晶化処理を行なつた。
得られた再結晶板の結晶粒径を調べたところ、
合金1では10μm、合金3では11μmであり、いず
れも微細結晶粒組織となつていることが判明し
た。
[実施例4]
実施例1の第1表の合金3について、実施例1
の第2表中の条件Cと同じ条件で均質化処理、熱
間圧延を行なつた。その後、冷間圧延率を55%、
75%、90%と3種に変えて冷間圧延を行ない、次
いで実施例1と同様にソルトバスにて加熱して再
結晶させた。
この実施例3における最終板の結晶粒径を冷間
圧延率に対応して第4表に示す。[Table] [Example 2] Alloy 1 of Example 1 was subjected to homogenization treatment and hot rolling according to condition symbol A in Table 2, with cooling at 3 × 10 -3 °C/sec after homogenization treatment. After cooling to room temperature at a high speed, reheating was performed to the hot rolling start temperature. Also, for Alloy 3 of Example 1, when homogenizing and hot rolling according to condition symbol C in Table 2, 3 × 10 -3
After cooling to room temperature at a cooling rate of °C/sec, it was reheated to the hot rolling start temperature. The other conditions were the same as in Example 1. The crystal grain size of the obtained rolled plate after recrystallization was 9 μm for Alloy 1 and 10 μm for Alloy 3.
It was found that the particles were sufficiently refined as in the case of . [Example 3] Alloy 1 and Alloy 3 of Example 1 were homogenized and hot rolled according to condition symbols A and C in Table 2, respectively, and then cold rolled at a rolling reduction of 80%, Next, Alloy 1 was heated to 480℃ and Alloy 3 to 490℃ using a continuous annealing furnace at a heating rate of 20℃/sec. A typical recrystallization treatment was performed. When the crystal grain size of the obtained recrystallized plate was examined, it was found that
The diameter was 10 μm for Alloy 1 and 11 μm for Alloy 3, and it was found that both had a fine grain structure. [Example 4] Regarding alloy 3 in Table 1 of Example 1, Example 1
Homogenization treatment and hot rolling were performed under the same conditions as Condition C in Table 2. After that, the cold rolling rate was increased to 55%,
Cold rolling was carried out in three different proportions, 75% and 90%, and then recrystallized by heating in a salt bath in the same manner as in Example 1. Table 4 shows the grain size of the final plate in Example 3 in correspondence with the cold rolling rate.
【表】
発明の効果
この発明の方法によれば、超塑性加工に適した
微細な結晶粒を有するアルミニウム合金圧延板を
得ることができ、しかも単にそればかりでなく、
冷間圧延性を低下させことなく、しかも冷間加工
の加工率をさほど大きくせずにかつ過時効処理や
温間加工等を行なうことなく微細結晶粒を得るこ
とができるため、生産性が低下したり冷間加工が
困難となつたりすることなく、量産的規模で実際
的に超塑性加工に適したアルミニウム合金圧延板
を製造することが可能となつた。[Table] Effects of the Invention According to the method of the present invention, an aluminum alloy rolled sheet having fine grains suitable for superplastic working can be obtained.
It is possible to obtain fine grains without reducing cold rolling properties, without increasing the cold working rate, and without performing overaging or warm working, which reduces productivity. It has now become possible to produce rolled aluminum alloy sheets that are practically suitable for superplastic working on a mass production scale without causing any problems such as deformation or difficulty in cold working.
Claims (1)
しかもMn0.05〜1.5%(重量%、以下同じ)、
Cr0.05〜0.4%、Zr0.05〜0.3%のうちの1種また
は2種以上を含有するアルミニウム合金を素材と
し、その合金鋳塊に対して均質化処理として、そ
の合金の溶体化処理温度の90%以上の温度で0.5
〜24時間加熱し、その後0.001〜0.05℃/secの範
囲内の冷却速度で溶体化処理温度の70〜90%の温
度まで冷却し、その温度から直ちにもしくはその
温度に24時間以内保持してから熱間圧延を開始し
て、溶体化処理温度の40〜70%の温度で熱間圧延
を終了させ、引続いて0.1℃/sec以上の冷却速度
で180℃以下、好ましくは室温まで冷却し、その
後加工率60%以上の冷間加工を行なつた後、その
合金の再結晶温度以上の温度に1℃/sec以上の
昇温速度で昇温させて再結晶させることを特徴と
する微細結晶粒を有するアルミニウム合金材料の
製造方法。 2 展伸用熱処理型アルミニウム合金であつて、
しかもMn0.05〜1.5%、Cr0.05〜0.4%、Zr0.05〜
0.3%のうちの1種または2種以上を含有するア
ルミニウム合金を素材とし、その合金鋳塊に対し
て均質化処理として、その合金の溶体化処理温度
の90%以上の温度で0.5〜24時間加熱し、その後
0.001〜0.05℃/secの範囲内の冷却速度で室温ま
で冷却し、次いで溶体化処理温度の70〜90%の温
度に再加熱して、直ちにもしくはその温度に24時
間以内保持してから熱間圧延を開始し、溶体化処
理温度の40〜70%の温度で熱間圧延を終了させ、
引続いて0.1℃/sec以上の冷却速度で180℃以下、
好ましくは室温まで冷却し、その後加工率60%以
上の冷間加工を行なつた後、その合金の再結晶温
度以上の温度に1℃/sec以上の昇温速度で昇温
させて再結晶させることを特徴とする微細結晶粒
を有するアルミニウム合金材料の製造方法。[Claims] 1. A heat-treated aluminum alloy for drawing, comprising:
Moreover, Mn0.05-1.5% (weight%, same below),
An aluminum alloy containing one or more of Cr0.05~0.4% and Zr0.05~0.3% is used as a material, and the alloy ingot is subjected to homogenization treatment at a solution treatment temperature of the alloy. 0.5 at temperatures above 90% of
Heating for ~24 hours, then cooling at a cooling rate within the range of 0.001~0.05°C/sec to a temperature of 70~90% of the solution treatment temperature, either immediately or after being held at that temperature for no more than 24 hours. Start hot rolling and finish hot rolling at a temperature of 40 to 70% of the solution treatment temperature, and then cool to 180 ° C or less, preferably room temperature, at a cooling rate of 0.1 ° C / sec or more, After that, cold working is performed at a processing rate of 60% or more, and then the temperature is raised to a temperature higher than the recrystallization temperature of the alloy at a heating rate of 1°C/sec or higher to recrystallize. A method for producing an aluminum alloy material having grains. 2. A heat-treated aluminum alloy for drawing,
Moreover, Mn0.05~1.5%, Cr0.05~0.4%, Zr0.05~
The material is an aluminum alloy containing one or more of 0.3%, and the alloy ingot is homogenized at a temperature of 90% or more of the solution treatment temperature of the alloy for 0.5 to 24 hours. heat and then
Cool to room temperature at a cooling rate within the range of 0.001 to 0.05°C/sec, then reheat to a temperature of 70 to 90% of the solution treatment temperature, either immediately or after holding at that temperature for no more than 24 hours before hot processing. Start rolling and finish hot rolling at a temperature of 40 to 70% of the solution treatment temperature,
180℃ or less at a cooling rate of 0.1℃/sec or more,
Preferably, the alloy is cooled to room temperature, then cold worked at a processing rate of 60% or more, and then recrystallized by raising the temperature to a temperature higher than the recrystallization temperature of the alloy at a heating rate of 1°C/sec or higher. A method for producing an aluminum alloy material having fine crystal grains.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4572086A JPS62202061A (en) | 1986-03-03 | 1986-03-03 | Manufacture of aluminum alloy material having fine grain |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4572086A JPS62202061A (en) | 1986-03-03 | 1986-03-03 | Manufacture of aluminum alloy material having fine grain |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS62202061A JPS62202061A (en) | 1987-09-05 |
| JPH0588302B2 true JPH0588302B2 (en) | 1993-12-21 |
Family
ID=12727181
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP4572086A Granted JPS62202061A (en) | 1986-03-03 | 1986-03-03 | Manufacture of aluminum alloy material having fine grain |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS62202061A (en) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6333538A (en) * | 1986-07-24 | 1988-02-13 | Kobe Steel Ltd | Al-mg-si alloy for extrusion forging |
| JPH03247738A (en) * | 1990-02-22 | 1991-11-05 | Kobe Steel Ltd | Aluminum alloy excellent in bendability |
| JP3705320B2 (en) * | 1997-04-18 | 2005-10-12 | 株式会社神戸製鋼所 | High strength heat treatment type 7000 series aluminum alloy with excellent corrosion resistance |
| JP3557953B2 (en) * | 1999-05-25 | 2004-08-25 | 日本軽金属株式会社 | Aluminum alloy sheet for precision machining and method of manufacturing the same |
| CA2887468C (en) * | 2012-06-27 | 2020-04-07 | Uacj Corporation | Aluminum alloy sheet for blow molding and production method therefor |
-
1986
- 1986-03-03 JP JP4572086A patent/JPS62202061A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS62202061A (en) | 1987-09-05 |
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