JPH0588301B2 - - Google Patents
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- JPH0588301B2 JPH0588301B2 JP4571986A JP4571986A JPH0588301B2 JP H0588301 B2 JPH0588301 B2 JP H0588301B2 JP 4571986 A JP4571986 A JP 4571986A JP 4571986 A JP4571986 A JP 4571986A JP H0588301 B2 JPH0588301 B2 JP H0588301B2
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Description
産業上の利用分野
この発明はJIS2000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(冷えば特開昭60−125354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をうち、(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40〜80%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
焼入れした場合よりも向上させるとともに溶質の
一部を固溶もしくはGPゾーンなどの微細粒子と
して析出させ、その後の冷間圧延時にマトリツク
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、その素材を熱間圧延した後、その合金
の溶体化処理温度の80%以上の温度に加熱して
0.5〜24時間保持し、その温度から0.001〜0.05
℃/secの冷却速度で溶体化処理温度を40〜80%
の温度まで冷却し、引続いて直ちにもしくはその
温度に24時間以内保持してから、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以上の加熱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、その素
材を熱間圧延した後、その合金の溶体化処理温度
の80%以上の温度に加熱して0.5〜24時間保持し、
続いて0.001〜0.05℃/secの冷却速度で室温まで
冷却し、その後溶体化処理温度の40〜80%の温度
まで再加熱し、引続いて直ちにもしくはその温度
に24時間以内保持してから、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
上の加熱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、Al−Cu系合金(JIS2000番
系)Al−Mg−Si系合金(JIS6000番系)、Al−Zn
−Mg系合金(JIS7000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熱塑性加工
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Al−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Al−Mg−Si系合金である6000番系
合金、例えばJIS規格の6061合金、さらにはAl−
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Al−
Cu系合金の場合、Cuを1.5〜6.8%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Al
−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Al−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。次いで必要に応じて均質化処理を行
なつた後、常法に従つて熱間圧延を行なつて所要
の板厚とする。
その後、対象となる合金の溶体化処理温度の80
%以上の温度(但し摂氏温度の80%以上;以下温
度の%については全て同じ)に加熱してその温度
に0.5〜24時間保持し、その温度から0.001〜0.05
℃/secの冷却速度で溶体化処理温度の40〜80%
の温度まで徐冷(第1発明の場合)するかまたは
室温まで徐冷(第2発明の場合)する。このよう
に溶体化処理温度の80%以上の温度、すなわち溶
体化処理温度近傍の温度に加熱・保持することに
よつて、Mn、Cr、Zr等の元素を充分に固溶さ
せ、続く0.001〜0.05℃/secの冷却速度の徐冷に
よつて、MnAl6、Cr2Mg3Al18、ZrAl3等の金属間
化合物の粒子を粗大に析出させる。ここで、加熱
保持温度がその合金の溶体化処理温度の80%未満
では充分に固溶させることができない。またその
後の冷却速度が0.05℃/secを越えれば粗大粒子
の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。
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。
前述のように溶体化処理温度の80%以上の温度
から0.01〜0.05℃/secのの冷却速度で徐冷して、
溶体化処理温度の40〜80%の温度域に至つた時に
は、その温度から直ちに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て焼
入れを行なうか、または上述の溶体化処理温度に
24時間以内保持してから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して焼
入れを行なう。また第2発明の場合は前述のよう
に溶体化処理温度の80%以上の温度から0.001〜
0.05℃/secの冷却速度で速度で室温まで徐冷し
た後、改めて溶体化処理温度の40〜80%の温度に
再加熱し、その温度から直ちに、またはその温度
に24時間以内保持してから、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。このように対象合
金の溶体化処理温度の40〜80%の温度域から焼入
れを行なうことによつて、冷間圧延性は完全焼入
れの場合(溶体化処理温度から焼入れする場合)
ほど低下することなく、しかも溶質の一部を固溶
もしくはGPゾーンなどの微細粒子として析出さ
せ、その後の冷間圧延時にマトリツクス内の転位
密度、変形帯を多くして、後の再結晶時における
再結晶核発生頻度を高くし、最終的に微細結晶粒
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80%を越える高い温度から焼入れ
た場合には、焼きが入り過ぎて硬質化し、次の冷
間圧延が困難となり、一方溶体化処理温度の40%
より低い温度から焼入れた場合は、粗大析出粒子
の固溶もしくは微細化が充分に行なわれず転位密
度が低くなつて結晶粒微細化の効果が得られな
い。また焼入れの冷却速度が0.1℃/sec未満の場
合は焼きが充分に入らず、その後の圧延により歪
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。
溶体化処理温度の40〜80%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、熱間圧延後に溶体化処理温度の
80%以上の温度域に加熱・保持した後、0.001〜
0.05℃/secのの冷却速度で徐冷して粗大金属間
化合物粒子を一旦粗大に析出させ、溶体化処理温
度の40〜80%を温度域から0.1℃/sec以上の冷却
速度で焼入れることにより溶質の一部を固溶もし
くは微細粒子として析出させ、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
られたスラブをを第2表に示す条件で均質化処理
および熱間圧延を施して、6mm厚の熱延板とし
た。次いで各熱延板を第3表に示す条件記号A〜
Iの条件にて中間焼鈍を行なつて同じく第3表中
に示す条件で冷却した。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にて中間焼鈍−冷却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昇温させて再結晶させた(記号I)。
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4表に示す結果
が得られた。
第4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10μm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は中間焼鈍温度が溶体化処理
温度の80%よりも低く、かつ溶体化処理温度の40
%〜80%の温度域からの冷却を0.1℃/sec以上と
しなかつたものであり、この場合も結晶粒径が
25μmと大きくなつた。さらに条件記号Gは中間
焼鈍後の冷却を480℃の高温からの完全焼入れと
してしまつた例であり、この場合は80%の圧延率
の冷間圧延が不可能となつてしまつた。また条件
記号Hは、溶体化処理温度の40〜80%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、条件記号Iは熱間圧延と冷間圧延との
間で中間焼鈍を行なわなかつたものであり、これ
らの場合も結晶粒径が30〜32μmと大きかつた。
さらに条件記号J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320μmと粗大化してしまつた。
Industrial Application Field This invention is applicable to JIS2000 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 gradually cooling from the solution treatment temperature and cold rolling (Japanese Patent Application Laid-open No. 125354/1983) is known. Problems to be Solved by the Invention Among the methods for producing aluminum alloy rolled sheets having fine grains as described above, method (a) has low productivity due to overaging treatment and warm working. 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. By quenching at a temperature range of 40 to 80% of the solution treatment temperature, cold rollability is improved compared to when quenching is performed from the solution treatment temperature, and part of the solute is dissolved in solid solution or in the GP zone. This method increases the dislocation density and deformation bands in the matrix during subsequent cold rolling, 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%
The material is made of an aluminum alloy containing one or more of the following: hot-rolled, and then heated to a temperature of 80% or more of the solution treatment temperature of the alloy.
Hold for 0.5-24 hours and 0.001-0.05 from that temperature
Solution treatment temperature 40-80% with cooling rate of °C/sec
temperature, then immediately or held at that temperature for 24 hours, then cooled at a cooling rate of 0.1°C/sec or more to 180°C or less, preferably room temperature, and then cooled at a processing rate of 60% or more. After the preliminary working, the alloy is heated to a temperature higher than the recrystallization temperature by 1℃/
This method is characterized by recrystallization by raising the temperature at a heating rate of sec or more. Further, the method of the second invention is a wrought aluminum alloy, in which Mn0.05 to 1.5% and Cr0.05 to 0.4% are used.
%, Zr0.05 to 0.3%, the material is made of an aluminum alloy containing one or more types of Zr, and after hot rolling the material, it is heated to a temperature of 80% or more of the solution treatment temperature of the alloy. and hold for 0.5-24 hours,
followed by cooling to room temperature at a cooling rate of 0.001 to 0.05 °C/sec, then reheating to a temperature of 40 to 80% of the solution treatment temperature, followed by immediate or holding at that temperature for no more than 24 hours; Cooling to 180°C or less, preferably 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. Function First, the aluminum alloy targeted by this invention will be explained. The method of this invention applies Al-Cu alloy (JIS2000 series), Al-Mg-Si alloy (JIS6000 series), Al-Zn
- It is applicable to all heat-treatable alloys for expansion, such as Mg-based alloys (JIS7000 series).
However, Cu, Mg and Si, or Zn, which are normally contained in these heat-treatable alloys,
In addition to Mg, etc., especially Mn0.05 as an essential component.
-1.5%, 0.05-0.4% of Cr, and 0.05-0.3% of Zr must be contained. In other words, Mn, Cr, and Zr are all elements that are effective in refining crystal grains through the formation of intermetallic compound precipitated particles, and by including them, fine crystals that can be thermoplastically processed as the object of this invention can be produced. It becomes possible to obtain tissue. Here, if the content of Mn, Cr, or Zr is less than 0.05%, it will be difficult to obtain fine crystal grains;
Mn1.5% or more, or Cr0.4% or more, or Zr0.3
% or more, these elements will not be sufficiently dissolved in solid solution during casting, resulting in the generation of giant intermetallic compounds, making it impossible to obtain sufficient elongation. Therefore Mn
is 0.05-1.5%, Cr is 0.05-0.4%, Zr is 0.05-0.3
It was set within the range of %. Note that heat-treatable alloys for drawing are used in the broadest sense here, and as mentioned above, 2000 series alloys, which are Al-Cu alloys, such as JIS standard and AA
Standard 2014 alloy, 2017 alloy, 2024 alloy, 2219 alloy, or 6000 series alloy which is Al-Mg-Si alloy, such as JIS standard 6061 alloy, and even Al-
7000 series alloy, which is a Zn-Mg alloy, e.g. 7075
alloy, 7475 alloy, 7N01 alloy, 7003 alloy, etc.
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 properties. For example, Al-
In the case of Cu-based alloys, it contains about 1.5 to 6.8% Cu, and if necessary, about 0.2 to 1.8% Mg and 0.2% Si.
It is sufficient that the content is approximately 1.3%, and Al
-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 Al-Zn-Mg alloys, Zn is about 0.8 to 6.1%.
%, Mg in an amount of about 0.5 to 2.9%, and further Cu in an amount of about 1.2 to 2.0% as 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, after homogenization treatment is performed as necessary, hot rolling is performed according to a conventional method to obtain a required thickness. Then, the target alloy is solution-treated at a temperature of 80°C.
% or more (however, 80% or more of the temperature in degrees Celsius; all percentages below are the same), hold at that temperature for 0.5 to 24 hours, and from that temperature 0.001 to 0.05
40-80% of solution treatment temperature with cooling rate of °C/sec
(in the case of the first invention) or gradually cooled to room temperature (in the case of the second invention). By heating and maintaining the temperature at 80% or more of the solution treatment temperature, that is, at a temperature close to the solution treatment temperature, elements such as Mn, Cr, and Zr are sufficiently dissolved, and the following 0.001~ By slow cooling at a cooling rate of 0.05° C./sec, coarse particles of intermetallic compounds such as MnAl 6 , Cr 2 Mg 3 Al 18 , and ZrAl 3 are precipitated. Here, if the heating and holding temperature is less than 80% of the solution treatment temperature of the alloy, sufficient solid solution cannot be achieved. Further, if the subsequent cooling rate exceeds 0.05°C/sec, precipitation of coarse particles 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. 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. As mentioned above, slowly cool from a temperature of 80% or more of the solution treatment temperature at a cooling rate of 0.01 to 0.05 °C/sec,
When the temperature range reaches 40 to 80% of the solution treatment temperature, immediately cool from that temperature to 180 °C or less, preferably room temperature, at a cooling rate of 0.1 °C/sec or more for quenching, or to the treatment temperature
After holding for within 24 hours, quenching is performed by cooling to 180°C or less, preferably room temperature, at a cooling rate of 0.1°C/sec or more. In addition, in the case of the second invention, as mentioned above, from a temperature of 80% or more of the solution treatment temperature to 0.001~
After slowly cooling to room temperature at a cooling rate of 0.05℃/sec, reheat to a temperature of 40 to 80% of the solution treatment temperature and either immediately from that temperature or after holding it at that temperature for less than 24 hours. Quenching is performed by cooling to 180°C or less, preferably room temperature, at a cooling rate of 0.1°C/sec or more. In this way, by quenching from a temperature range of 40 to 80% of the solution treatment temperature of the target alloy, cold rollability can be improved in the case of complete quenching (when quenching is performed from the solution treatment temperature).
Moreover, part of the solute is precipitated as a solid solution or fine particles such as GP zones, and the dislocation density and deformation bands in the matrix are increased during subsequent cold rolling, resulting in a reduction in the density during subsequent recrystallization. This increases the frequency of recrystallization nuclei and ultimately makes it possible to obtain a fine grain structure. If quenching is performed at a temperature higher than 80% of the solution treatment temperature, the quenching will be too high and hard, making the next cold rolling difficult;
When quenching is performed from a lower temperature, the coarse precipitated particles are not sufficiently dissolved or refined, resulting in a low dislocation density and no effect of grain refinement. Furthermore, if the cooling rate for quenching is less than 0.1° C./sec, quenching will not occur sufficiently, strain will not be introduced sufficiently during 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. After quenching at a temperature of 40 to 80% 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 processing 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, the solution treatment temperature after hot rolling is
After heating and holding at a temperature range of 80% or more, 0.001~
The coarse intermetallic compound particles are once precipitated into coarse particles by slow cooling at a cooling rate of 0.05℃/sec, and then quenched at a cooling rate of 0.1℃/sec or more from the temperature range of 40 to 80% of the solution treatment temperature. By precipitating a part of the solute as a solid solution or fine particles, and then recrystallizing after performing cold working of 60% or more, it is possible to significantly refine the recrystallized grains.
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 component compositions shown in Table 1,
A 400mm thick slab was cast using the DC casting method. The obtained slab was subjected to homogenization treatment and hot rolling under the conditions shown in Table 2 to obtain a 6 mm thick hot rolled plate. Next, each hot-rolled sheet was subjected to condition symbols A~ shown in Table 3.
Intermediate annealing was performed under the conditions of I, and cooling was performed under the same conditions shown in Table 3. The alloys were then rolled at a cold rolling rate of 80%, 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 was subjected to intermediate annealing and cooling under condition code A.
After rolling with a cold rolling rate of 80%, 0.01 as a comparative method
It was recrystallized by raising the temperature at ℃/sec (symbol I). 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 4 were obtained. From Table 4, 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 10 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. Condition code F means that the intermediate annealing temperature is lower than 80% of the solution treatment temperature and 40% of the solution treatment temperature.
% to 80% temperature range is not more than 0.1℃/sec, and in this case, the crystal grain size is
It grew to 25μm. Furthermore, condition code G is an example in which the cooling after intermediate annealing is complete quenching from a high temperature of 480°C, and in this case, cold rolling with a rolling reduction of 80% is impossible. Condition code H indicates that quenching from 40 to 80% of the solution treatment temperature (cooling of 0.1°C/sec or more) is not performed, and condition code I indicates that the temperature is between hot rolling and cold rolling. Intermediate annealing was not performed, and the crystal grain size was as large as 30 to 32 μm in these cases as well.
Further, condition code J is an example in which heating for recrystallization quenching was performed by slow temperature increase, and in this case, the crystal grain size became coarse to 320 μm.
【表】【table】
【表】【table】
【表】【table】
【表】【table】
【表】
[実施例 2]
実施例1の第1表の合金1および合金2につい
て、実施例1と同様にスラブを鋳造した後、第2
表に従つて均質化処理および熱間圧延を行なつ
た。その熱間圧延コイルを合金1については480
℃×2時間焼鈍して0.01℃/secで室温まで冷却
し、次いでそのコイルを300℃に連続的に昇温し、
3分間保持して炉の出側で水冷した。また合金2
については熱間圧延コイルを450℃×2時間焼鈍
して0.04℃/secで室温まで冷却し、次いでその
コイルを300℃に保持された炉内に連続的に通し
て出側で水冷した。これらの合金1、合金2のコ
イルを、1.2mm厚まで冷間圧延した後、連続炉を
用いて20℃/secの昇温速度で合金1は480℃、合
金2は490℃に昇温し、7分間で通板させて出側
で水冷することにより連続再結晶焼入れを行なつ
た。
得られた最終板の表面の結晶粒径を調べたとこ
ろ、合金1では12μm、合金2では13μm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 3]
実施例1の第1表の合金3について、実施例1
の第2表中の条件と同じ条件で均質化処理、熱間
圧延を行ない、さらに実施例1の第3表中の条件
記号Cにて中間焼鈍−冷却を行なつた。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5表に示す。[Table] [Example 2] For Alloy 1 and Alloy 2 in Table 1 of Example 1, slabs were cast in the same manner as in Example 1, and then the second
Homogenization treatment and hot rolling were performed according to the table. 480 for alloy 1 that hot rolled coil
℃ x 2 hours and cooled to room temperature at 0.01℃/sec, then the coil was continuously heated to 300℃,
It was held for 3 minutes and water cooled on the exit side of the furnace. Also alloy 2
For this, a hot rolled coil was annealed at 450°C for 2 hours and cooled to room temperature at a rate of 0.04°C/sec, and then the coil was continuously passed through a furnace maintained at 300°C and cooled with water on the exit side. These alloy 1 and alloy 2 coils were cold rolled to a thickness of 1.2 mm, and then heated to 480°C for alloy 1 and 490°C for alloy 2 at a heating rate of 20°C/sec using a continuous furnace. Continuous recrystallization quenching was performed by passing the plate through the plate for 7 minutes and cooling it with water on the exit side. When the crystal grain size on the surface of the final plate obtained was examined, it was found to be 12 μm for Alloy 1 and 13 μm for Alloy 2.
It was found that all of them had a fine grain structure. [Example 3] Regarding alloy 3 in Table 1 of Example 1, Example 1
Homogenization treatment and hot rolling were performed under the same conditions as in Table 2 of Example 1, and intermediate annealing and cooling were performed under condition symbol C in Table 3 of Example 1. after that,
Cold rolling was performed at three different cold rolling ratios: 55%, 75%, and 90%, and then, as in Example 1, the material was heated in a salt bath for recrystallization. Table 5 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.
Fine grains can be obtained without significantly increasing the cold working rate and without overaging or warm working, which reduces productivity and makes cold working difficult. It has now become possible to produce rolled aluminum alloy sheets that are practically suitable for superplastic working on a mass-production scale without any problems.
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、その素材を熱間圧延した後、その合金の溶体
化処理温度の80%以上の温度に加熱して0.5〜24
時間保持し、その温度から0.001〜0.05℃/secの
冷却速度で溶体化処理温度の40〜80%の温度まで
冷却し、引続いて直ちにもしくはその温度に24時
間以内保持してから、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
加熱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、その素材を熱間圧延した後、
その合金の溶体化処理温度の80%以上の温度に加
熱して0.5〜24時間保持し、続いて0.001〜0.05
℃/secの冷却速度で室温まで冷却し、その後溶
体化処理温度の40〜80%の温度まで再加熱し、引
続いて直ちにもしくはその温度に24時間以内に保
持してから、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以上の加熱速度
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 0.05 to 0.4% of Cr and 0.05 to 0.3% of Zr is used as a material, and after hot rolling the material, 80% of the solution treatment temperature of the alloy is applied. Heat to a temperature of 0.5 to 24
from that temperature at a cooling rate of 0.001 to 0.05 °C/sec to a temperature of 40 to 80% of the solution treatment temperature, and then immediately or after holding at that temperature for no more than 24 hours, cool to 0.1 °C. After cooling to 180°C or less, preferably room temperature, at a cooling rate of 1°C/sec or more, and then cold working at a processing rate of 60% or more, the alloy is cooled to a temperature of 1°C/sec or more at a cooling rate of 1°C/sec or more. A method for producing an aluminum alloy material having fine crystal grains, which comprises recrystallizing the material by increasing the temperature at a heating rate. 2. It is an aluminum alloy for drawing, and
After hot-rolling an aluminum alloy containing one or more of Mn0.05-1.5%, Cr0.05-0.4%, and Zr0.05-0.3%,
Heating to a temperature above 80% of the alloy's solution treatment temperature and holding for 0.5 to 24 hours, followed by 0.001 to 0.05
Cool to room temperature at a cooling rate of °C/sec, then reheat to a temperature between 40 and 80% of the solution treatment temperature, followed by immediate or no more than 24 hours at that temperature, then 0.1 °C/sec. 180℃ at a cooling rate of over 180℃
Below, preferably cool down to room temperature, then process rate
Aluminum having fine crystal grains, which is characterized by being cold-worked by 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. Method of manufacturing alloy materials.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4571986A JPS62202060A (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 |
|---|---|---|---|
| JP4571986A JPS62202060A (en) | 1986-03-03 | 1986-03-03 | Manufacture of aluminum alloy material having fine grain |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS62202060A JPS62202060A (en) | 1987-09-05 |
| JPH0588301B2 true JPH0588301B2 (en) | 1993-12-21 |
Family
ID=12727156
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP4571986A Granted JPS62202060A (en) | 1986-03-03 | 1986-03-03 | Manufacture of aluminum alloy material having fine grain |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS62202060A (en) |
-
1986
- 1986-03-03 JP JP4571986A patent/JPS62202060A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS62202060A (en) | 1987-09-05 |
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