JPS62225B2 - - Google Patents
Info
- Publication number
- JPS62225B2 JPS62225B2 JP9417784A JP9417784A JPS62225B2 JP S62225 B2 JPS62225 B2 JP S62225B2 JP 9417784 A JP9417784 A JP 9417784A JP 9417784 A JP9417784 A JP 9417784A JP S62225 B2 JPS62225 B2 JP S62225B2
- Authority
- JP
- Japan
- Prior art keywords
- temperature
- heating
- cold working
- superplastic
- aluminum 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.)
- Expired
Links
- 238000010438 heat treatment Methods 0.000 claims description 48
- 229910000838 Al alloy Inorganic materials 0.000 claims description 28
- 238000004519 manufacturing process Methods 0.000 claims description 21
- 238000005482 strain hardening Methods 0.000 claims description 21
- 238000001816 cooling Methods 0.000 claims description 17
- 229910045601 alloy Inorganic materials 0.000 claims description 11
- 239000000956 alloy Substances 0.000 claims description 11
- 238000000137 annealing Methods 0.000 claims description 7
- 238000000265 homogenisation Methods 0.000 claims description 7
- 239000012535 impurity Substances 0.000 claims description 6
- 229910018134 Al-Mg Inorganic materials 0.000 claims description 5
- 229910018467 Al—Mg Inorganic materials 0.000 claims description 5
- 229910052782 aluminium Inorganic materials 0.000 claims description 4
- 239000000463 material Substances 0.000 description 17
- 238000000034 method Methods 0.000 description 13
- 238000005266 casting Methods 0.000 description 7
- 229910052804 chromium Inorganic materials 0.000 description 5
- 239000013078 crystal Substances 0.000 description 5
- 229910052748 manganese Inorganic materials 0.000 description 5
- 239000002244 precipitate Substances 0.000 description 4
- 229910052726 zirconium Inorganic materials 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 230000007704 transition Effects 0.000 description 3
- 229910016583 MnAl Inorganic materials 0.000 description 2
- 229910007880 ZrAl Inorganic materials 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000005097 cold rolling Methods 0.000 description 2
- 238000005098 hot rolling Methods 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- 230000009466 transformation Effects 0.000 description 2
- 229910052720 vanadium Inorganic materials 0.000 description 2
- 229910000861 Mg alloy Inorganic materials 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 229910000765 intermetallic Inorganic materials 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 238000001953 recrystallisation Methods 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Landscapes
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
- Heat Treatment Of Nonferrous Metals Or Alloys (AREA)
Description
〔産業上の利用分野〕
本発明は超塑性アルミニウム合金の製造方法に
関し、さらに詳しくは、Al―Mg系の超塑性アル
ミニウム合金の製造方法に関する。
本発明に係る超塑性アルミニウム合金の製造方
法において、超塑性とは、ある外的条件の下で材
料がくびれ(necking)なしに数百%〜千%とい
うような巨大な伸びを生じる現象をいうのであ
り、そして、恒温変態を利用した変態超塑性と微
細結晶粒材料で見られる微細粒超塑性(構造超塑
性)とに大別される。因に、本発明は微細結晶粒
超塑性アルミニウム合金の製造方法である。
〔従来技術〕
一般に、微細結晶粒超塑性を起させるために
は、その材料の結晶粒径を微細に制御することが
必須である。
また、一般にAl―Mg系アルミニウム合金は、
鋳造後鋳塊を400〜550℃の温度で均質化熱処理を
行ない、次いで、300〜550℃の温度で熱間加工お
よび冷間加工を行なつて、所望の材料を製造する
のであるが、このような通常の工程では結晶粒は
30〜100μmと大きくなつてしまい、高温におい
て変形してもアルミニウム合金には目的とする超
塑性(伸び)を付与することはできない。
〔発明が解決しようとする問題点〕
本発明は上記に説明したように、いままでは、
Al―Mg系のアルミニウム合金では困難であつた
微細結晶組織を得ることができる超塑性アルミニ
ウム合金の製造方法を提供するものである。
〔問題点を解決するための手段〕
本発明に係る超塑性アルミニウム合金の製造方
法は、
(1) Mg2〜7wt%
を含有し、さらに、
Mn0.05〜1.5wt%、Cr0.05〜0.5wt%、
Zr0.05〜0.5wt%、V0.05〜0.5wt%、
Ti0.15wt%以下
の中から選んだ1種または2種以上
を含有し、残部Alおよび不純物Al―Mg系合金
鋳塊を、400〜550℃の温度で均質化熱処理を行
ない、次いで、300〜550℃の温度で熱間加工を
行なつた後、第1回の加熱保持を450〜550℃の
温度で0.5〜10Hr行ない、次に、第2回の加熱
温度まで冷却し、350〜450℃の温度で0.5〜
50Hrの第2回の加熱保持を行ない、30℃/Hr
以上の冷却速度で冷却した後、少なくとも30%
以上の冷間加工を行なうことを特徴とする超塑
性アルミニウム合金の製造方法を第1の発明と
し、
(2) Mg2〜7wt%
を含有し、さらに、
Mn0.05〜1.5wt%、Cr0.05〜0.5wt%、
Zr0.05〜0.5wt%、V0.05〜0.5wt%、
Ti0.15wt%以下
の中から選んだ1種または2種以上
を含有し、残部Alおよび不純物からなるAl―
Mg系合金鋳塊を、400〜550の温度で均質化熱
処理を行ない、次いで、300〜550℃の温度で熱
間加工を行なつた後、第1回の加熱保持を450
〜550℃の温度で0.5〜10Hr行ない、次に第2
回の加熱温度まで冷却し、350〜450℃の温度で
0.5〜50Hrの第2回の加熱保持を行ない、30
℃/Hr以上の冷却速度で冷却した後、20〜60
%の冷間加工を行ない、続いて、300℃以下の
低温軟化焼鈍と冷間加工を1回以上行なうこと
を特徴とする超塑性アルミニウム合金の製造方
法を第2の発明とし、
(3) Mg2〜7wt%
を含有し、さらに、
Mn0.05〜1.5wt%、Cr0.05〜0.5wt%、
Zr0.05〜0.5wt%、V0.05〜0.5wt%、
Ti0.15wt%以下
の中から選んだ1種または2種以上
を含有し、残部Alおよび不純物からなるAl―
Mg系合金鋳塊を、400〜550℃の温度で均質化
熱処理を行ない、次いで、300〜550℃の温度で
熱間加工を行なつた後、第1回の加熱保持を
450〜550℃の温度で0.5〜10Hr行ない、次に、
第2回の加熱温度まで冷却し、350〜450℃の温
度で0.5〜50Hrの第2回の加熱保持を行ない、
30℃/Hr以上の冷却速度で冷却した後、少な
くとも30%以上の冷間加工を行なうか、或い
は、20〜60%の冷間加工を行ない、続いて、
300℃以下の低温軟化焼鈍と冷間加工を1回以
上行ない、さらに、100℃/Hr以上の加熱速度
で350〜550℃の温度に加熱軟化処理することを
特徴とする超塑性アルミニウム合金の製造方法
を第3の発明とする3つの発明よりなるもので
ある。
本発明に係る超塑性アルミニウム合金の製造方
法について以下詳細に説明する。
先ず、本発明に係る超塑性アルミニウム合金の
製造方法において使用するアルミニウム合金の含
有成分および成分割合について説明する。
Mgは2wt%未満では充分な強度が得られず、
また、7wt%を越えて含有される熱間加工性が著
しく低下する。よつて、Mg含有量は2〜7wt%
とする。
Mn、Cr、Zr、Vは含有量が0.05wt%未満では
後述するように微細な結晶粒が得られず、また、
Mn1.5wt%、Cr、Zr、V0.5wt%およびTi0.15wt
%を越えて含有されると鋳造時に充分な固溶が得
られず、巨大化合物の発生を招き充分な伸びが得
られない。よつて、Mn含有量は0.05〜1.5wt%、
Cr含有量は0.05〜0.5wt%、Zr0.05〜0.5wt%、
V0.05〜0.5wt%、Ti含有量は0.15wt%以下す
る。
なお、不純物として含有されるFeおよびSiは
その含有量が0.25wt%を越えると不溶出の晶出物
が生成し、伸びの低下が著しくなるので、Feお
よびSiの含有量は極力抑制する必要がある。
次に、本発明に係る超塑性アルミニウム合金の
製造方法における熱処理法について説明する。
上記に説明した含有成分および成分割合のアル
ミニウム合金を鋳造して得られた鋳塊を、内部に
不均質に分布している主要元素の均質化および熱
間加工性を向上させるため、400〜550℃の温度に
おいて充分な時間均質化熱処理を行ない、続い
て、300〜550℃の温度で熱間加工を行なつて所定
の板厚まで加工し、粗い鋳造組織は熱間フアイバ
ー組織となると同時に組織内にMg等の析出物お
よびMn、Cr、Zr、V、Ti等の遷移元素の一部が
部分析出する。さらに、熱間加工後、30%以上の
冷間加工を行なうとより微細な結晶粒が得られ超
塑性伸びも大きくなる。
この熱間加工された材料は450〜550℃の温度で
0.5〜10Hrの第1回の加熱保持を行ない、続いて
第2回の加熱保持温度まで冷却し、350〜450℃の
温度で0.5〜50Hrの第2回の加熱保持を行ない、
30℃/Hr以上の冷却速度で冷却する。この加熱
保持の温度が高い程時間は短時間で良い。
2回の加熱保持において、第1回の加熱保持に
より析出している溶質元素はその大部分が固溶さ
れ、続く2回の加熱保持により遷移元素Mn、
Cr、Zr等とAlとの金属間化合物MnAl6、
Cr2Al3Al18、ZrAl3等が析出し、次の冷間加工後
の超塑性温度域での加熱によつて材料中に生成さ
れる微細粒組織が保持されて超塑性が得られる。
また、この2回の加熱保持は加熱保持を1回で
行なつた場合に比較して、遷移元素の析出形態が
微細なことおよび若干のMg等とAlとの高温時効
折出物が形成されるために、加熱保持後の冷却速
度も30℃/Hr以上と遅くなつても良く、製造が
より容易となり、かつ、冷間加工中に生成される
転位の密度がより高くなり、さらに微細な結晶粒
が生成され超塑性伸びの大きいものが得られる。
この加熱保持により熱間フアイバー組織を形成し
ていた転位の下部組織は回復、再結晶により歪エ
ネルギーが低減され、続く冷間加工で転位が導入
され易くなる。
この加熱保持後の冷却速度は30℃/Hr未満に
なると超塑性伸びが得られにくくなる。
冷却後、少なくとも30%以上の冷間加工を行な
うのであるが、30%未満の加工率では充分微細な
結晶粒が得られない。
また、20〜60%の冷間加工とこれに続く300℃
以下の低温軟化焼鈍とを1回以上行なうこともで
き、この低温焼純を導入することにより結晶粒は
さらに微細化される。
このように冷間加工された材料には、高い歪エ
ネルギーを持つ転位の下部組織が高密度に形成さ
れる。この材料を通常0.5Tm{Tmは材料の融点
(絶対温度)}以上の超塑性温度域(アルミニウム
合金では400℃以上)に加熱すると高密度の転位
組織を起点として新しい結晶粒が形成され、従つ
て、転位組織が高密度程、微細粒組織が得られ超
塑性伸びが大きくなる。そして、一度再結晶が完
了すると、結晶粒界のエネルギーを減少するため
に転位が移動して結晶粒は粗大化する傾向があ
り、この粗大化した結晶粒が超塑性変形を阻害す
ることになる。
よつて、本発明に係る超塑性アルミニウム合金
の製造方法においては、熱間圧延後の加熱保持中
に形成されたMnAl6、Cr2Mg3Al16、ZrAl3等の析
出物の寸法と分布とを制御することにより転位の
移動を阻止し、微細粒組織を保持するものであ
る。即ち、析出物の寸法が小さ過ぎたり、粒子間
隔が大き過ぎると転位移動阻止効果が得られな
い。
また、本発明に係る超塑性アルミニウム合金の
製造方法においては、冷間加工のままの材料を超
塑性加工してもよいが、100℃/Hr以上の加熱速
度で加熱し、350〜550℃の温度で加熱軟化処理を
行なつてから超塑性加工を行なうこともできる。
本発明に係る超塑性アルミニウム合金の製造方
法において製造された微細結晶粒超塑性材料は適
切な温度(通常400℃以上)において、くびれ
(局所伸び)が発生することなく500%以上の超塑
性伸びが得られる。
〔実施例〕
本発明に係る超塑性アルミニウム合金の製造方
法の実施例を説明する。
実施例 1
Mg2.5wt%、Cr0.15wt%、Zr0.15wt%、
Ti0.02wt%、残部Al(合金1)、Mg5.6wt%、
Cr0.1wt%、Mn0.1wt%、Ti0.02wt%、残部Al
(合金2)およびMg4.5wt%、Zr0.2wt%、
Mn0.1wt%、V0.05wt%、Ti0.02wt%、残部Al
(合金3)の厚さ400mm鋳塊を通常のDC鋳造法で
鋳造し後、510℃の温度で12Hrの均質化熱処理
後、450〜300℃の温度における熱間圧延により、
40mmの板に圧延し、540℃で3Hrおよび420℃で10
時間の加熱保持を行ない、約100℃/Hrの冷却速
度で冷却し、冷間圧延で厚さ1.5mmの板(冷間加
工率63%)を製造し、550℃で歪速度2×10-4/
secにて変形した。
第1表に示したように、超塑性伸びについて本
発明に係る超塑性アルミニウム合金の製造方法と
比較例の従来法とでは、本発明の方が2倍以上と
なつている。
[Industrial Application Field] The present invention relates to a method for producing a superplastic aluminum alloy, and more particularly, to a method for producing an Al--Mg-based superplastic aluminum alloy. In the method for producing a superplastic aluminum alloy according to the present invention, superplasticity refers to a phenomenon in which a material undergoes enormous elongation of several hundred to 1,000% without necking under certain external conditions. It is broadly divided into transformation superplasticity, which utilizes isothermal transformation, and fine-grained superplasticity (structural superplasticity), which is observed in fine-grained materials. In particular, the present invention is a method for producing a fine-grained superplastic aluminum alloy. [Prior Art] Generally, in order to cause fine grain superplasticity, it is essential to finely control the grain size of the material. In addition, generally Al-Mg aluminum alloys are
After casting, the ingot is subjected to homogenization heat treatment at a temperature of 400 to 550°C, and then hot worked and cold worked at a temperature of 300 to 550°C to produce the desired material. In normal processes such as
The aluminum alloy becomes as large as 30 to 100 μm, and even if it is deformed at high temperatures, the desired superplasticity (elongation) cannot be imparted to the aluminum alloy. [Problems to be solved by the invention] As explained above, the present invention solves the problems hitherto;
The present invention provides a method for producing a superplastic aluminum alloy that can obtain a fine crystal structure, which is difficult to achieve with Al--Mg-based aluminum alloys. [Means for Solving the Problems] The method for producing a superplastic aluminum alloy according to the present invention includes: (1) containing 2 to 7 wt% Mg, and further containing 0.05 to 1.5 wt% Mn, and 0.05 to 0.5 wt% Cr; %, Zr0.05~0.5wt%, V0.05~0.5wt%, Ti0.15wt% or less, and the balance is Al and impurities Al-Mg alloy ingot. , homogenization heat treatment at a temperature of 400 to 550°C, then hot working at a temperature of 300 to 550°C, and then a first heating holding at a temperature of 450 to 550°C for 0.5 to 10 hours. , then cooled to the second heating temperature, and heated from 0.5 to 350 to 450℃.
Perform the second heating hold for 50 hours, and then heat to 30℃/hour.
After cooling at a cooling rate of at least 30%
The first invention is a method for manufacturing a superplastic aluminum alloy characterized by performing the above cold working, and (2) containing Mg2 to 7wt%, further comprising Mn0.05 to 1.5wt%, Cr0.05 Al containing one or more selected from ~0.5wt%, Zr0.05~0.5wt%, V0.05~0.5wt%, Ti0.15wt% or less, with the balance consisting of Al and impurities.
The Mg-based alloy ingot is homogenized at a temperature of 400 to 550°C, then hot worked at a temperature of 300 to 550°C, and then heated and held for the first time at a temperature of 450°C.
0.5-10Hr at a temperature of ~550℃, then the second
Cool to the heating temperature of 350-450℃
Perform the second heating and holding for 0.5 to 50Hr, and
After cooling at a cooling rate of ℃/Hr or higher, 20 to 60
% cold working, followed by low temperature softening annealing at 300°C or less and cold working one or more times, (3) Mg2 ~7wt% and further selected from Mn0.05~1.5wt%, Cr0.05~0.5wt%, Zr0.05~0.5wt%, V0.05~0.5wt%, Ti0.15wt% or less. Al-
The Mg alloy ingot is subjected to homogenization heat treatment at a temperature of 400 to 550°C, then hot worked at a temperature of 300 to 550°C, and then subjected to the first heating and holding process.
Carry out for 0.5-10Hr at a temperature of 450-550℃, then
Cool to the second heating temperature, perform a second heating hold at a temperature of 350 to 450 ° C for 0.5 to 50 Hr,
After cooling at a cooling rate of 30°C/Hr or more, cold working is performed by at least 30%, or cold working is performed by 20 to 60%, and then,
Production of a superplastic aluminum alloy characterized by performing low-temperature softening annealing at 300°C or less and cold working one or more times, and further heat-softening treatment at a temperature of 350 to 550°C at a heating rate of 100°C/Hr or more. This invention consists of three inventions, with the third invention being a method. The method for producing a superplastic aluminum alloy according to the present invention will be described in detail below. First, the components and component ratios of the aluminum alloy used in the method for producing a superplastic aluminum alloy according to the present invention will be explained. If Mg is less than 2wt%, sufficient strength cannot be obtained.
Moreover, if the content exceeds 7wt%, hot workability will be significantly reduced. Therefore, the Mg content is 2 to 7 wt%.
shall be. If the content of Mn, Cr, Zr, and V is less than 0.05wt%, fine crystal grains cannot be obtained as described later, and
Mn1.5wt%, Cr, Zr, V0.5wt% and Ti0.15wt
If the content exceeds %, sufficient solid solution cannot be obtained during casting, resulting in the formation of giant compounds, and sufficient elongation cannot be obtained. Therefore, the Mn content is 0.05-1.5wt%,
Cr content is 0.05~0.5wt%, Zr0.05~0.5wt%,
V0.05~0.5wt%, Ti content is 0.15wt% or less. In addition, if the content of Fe and Si contained as impurities exceeds 0.25wt%, undissolved crystallized substances will be formed and the elongation will decrease significantly, so it is necessary to suppress the content of Fe and Si as much as possible. There is. Next, a heat treatment method in the method for producing a superplastic aluminum alloy according to the present invention will be explained. In order to homogenize the main elements that are heterogeneously distributed inside the ingot and improve hot workability, we cast an ingot obtained by casting an aluminum alloy with the above-mentioned components and ratios. Homogenization heat treatment is carried out at a temperature of 300 to 550 degrees Celsius for a sufficient period of time, followed by hot working at a temperature of 300 to 550 degrees Celsius to reach a predetermined thickness. Precipitates such as Mg and some transition elements such as Mn, Cr, Zr, V, and Ti are partially separated. Furthermore, if cold working is performed by 30% or more after hot working, finer grains will be obtained and superplastic elongation will also increase. This hot-processed material is produced at temperatures of 450-550℃
Perform the first heating and holding for 0.5 to 10 Hr, then cool to the second heating and holding temperature, and perform the second heating and holding for 0.5 to 50 Hr at a temperature of 350 to 450°C,
Cool at a cooling rate of 30℃/Hr or higher. The higher the temperature for this heating and holding, the shorter the time. During the two heating and holding cycles, most of the solute elements precipitated during the first heating and holding process are solid-solubilized, and the subsequent two heating and holding processes convert the transition elements Mn, Mn,
Intermetallic compound of Cr, Zr, etc. and Al MnAl 6 ,
Cr 2 Al 3 Al 18 , ZrAl 3 , etc. are precipitated, and the fine grain structure generated in the material is maintained by heating in the superplastic temperature range after the next cold working, resulting in superplasticity. In addition, compared to the case where heating and holding is carried out only once, these two heating and holding processes result in finer precipitation of transition elements and the formation of some high-temperature aging precipitates of Mg, etc. and Al. In order to achieve this, the cooling rate after heating and holding may be as slow as 30°C/Hr or more, making manufacturing easier, and increasing the density of dislocations generated during cold working, resulting in finer Crystal grains are formed and a product with large superplastic elongation is obtained.
By this heating and holding, the dislocation underlying structure that had formed the hot fiber structure recovers and recrystallizes, reducing the strain energy, making it easier for dislocations to be introduced in the subsequent cold working. If the cooling rate after this heating and holding is less than 30°C/Hr, it becomes difficult to obtain superplastic elongation. After cooling, cold working is performed to a rate of at least 30%, but if the working rate is less than 30%, sufficiently fine grains cannot be obtained. Also, 20-60% cold working followed by 300℃
The following low-temperature softening annealing can be performed one or more times, and by introducing this low-temperature annealing, the crystal grains are further refined. In the material that has been cold-worked in this manner, a dense dislocation substructure with high strain energy is formed. When this material is heated to the superplastic temperature range (usually 400°C or higher for aluminum alloys) above 0.5Tm {Tm is the melting point (absolute temperature) of the material}, new crystal grains are formed starting from the high-density dislocation structure, and Therefore, the higher the density of the dislocation structure, the finer the grain structure and the greater the superplastic elongation. Once recrystallization is completed, dislocations move to reduce the energy at grain boundaries, and the grains tend to become coarser, and these coarsened grains inhibit superplastic deformation. . Therefore, in the method for producing a superplastic aluminum alloy according to the present invention, the size and distribution of precipitates such as MnAl 6 , Cr 2 Mg 3 Al 16 , and ZrAl 3 formed during heating and holding after hot rolling are By controlling this, the movement of dislocations is prevented and the fine grain structure is maintained. That is, if the size of the precipitates is too small or the particle spacing is too large, the effect of inhibiting dislocation movement cannot be obtained. In addition, in the method for producing a superplastic aluminum alloy according to the present invention, the material as it is cold-worked may be subjected to superplastic working, but the material is heated at a heating rate of 100°C/Hr or more, and the material is heated at a temperature of 350 to 550°C. Superplastic working can also be performed after heat softening treatment at a high temperature. The fine-grained superplastic material produced by the method for producing a superplastic aluminum alloy according to the present invention exhibits superplastic elongation of 500% or more without necking (local elongation) at an appropriate temperature (usually 400°C or higher). is obtained. [Example] An example of the method for producing a superplastic aluminum alloy according to the present invention will be described. Example 1 Mg2.5wt%, Cr0.15wt%, Zr0.15wt%,
Ti0.02wt%, balance Al (alloy 1), Mg5.6wt%,
Cr0.1wt%, Mn0.1wt%, Ti0.02wt%, balance Al
(Alloy 2) and Mg4.5wt%, Zr0.2wt%,
Mn0.1wt%, V0.05wt%, Ti0.02wt%, balance Al
After casting a 400 mm thick ingot of (alloy 3) using the normal DC casting method, after homogenizing heat treatment at a temperature of 510 °C for 12 hours, hot rolling at a temperature of 450 to 300 °C.
Rolled into 40mm plate, 3Hr at 540℃ and 10Hr at 420℃
After heating and holding for several hours, cooling at a cooling rate of approximately 100°C/Hr, a plate with a thickness of 1.5 mm was produced by cold rolling (cold working rate: 63%), and the strain rate was 2 × 10 - at 550°C. Four /
Transformed in sec. As shown in Table 1, the superplastic elongation of the method of the present invention for producing a superplastic aluminum alloy is more than twice that of the conventional method of the comparative example.
【表】
実施例 2
通常のDC鋳造法で鋳造した実施例1の合金3
(厚さ400mm)を、510℃の温度で12Hrの均質化熱
処理後、450〜300℃の熱間圧延により厚さ7.5mm
の板に加工し、540℃の温度で3Hrおよび420℃の
温度で10Hrの加熱保持を行ない、約100℃/Hrの
冷却速度で冷却し、第2表に示す冷間圧延および
低温軟化焼鈍により厚さ1.5mmの材料を作製し、
550℃に加熱後、歪速度2×10-4/secで変形し
た。本発明に係る超塑性アルミニウム合金の製造
方法により製造された材料は超塑性伸びが、低温
軟化焼鈍を行なわないものに比して格段に優れて
いることがわかる。[Table] Example 2 Alloy 3 of Example 1 cast by normal DC casting method
(thickness 400mm) was homogenized at a temperature of 510℃ for 12 hours, then hot rolled at 450~300℃ to a thickness of 7.5mm.
It was processed into a plate of Fabricate a material with a thickness of 1.5 mm,
After heating to 550°C, it was deformed at a strain rate of 2×10 -4 /sec. It can be seen that the superplastic elongation of the material manufactured by the method for manufacturing a superplastic aluminum alloy according to the present invention is significantly superior to that of a material that is not subjected to low-temperature softening annealing.
【表】
実施例 3
通常のDC鋳造法により鋳造した実施例1の合
金3(厚さ400mm)を510℃の温度で12Hrの均質
化処理後、450〜300℃の温度で加熱圧延を行なつ
て厚さ4.0mmの板に加工し、540℃で3Hrおよび
450℃の温度で10Hrの加熱保持を行なつた後、約
100℃/Hrの冷却速度で冷却後、冷間圧延で1.5
mm厚(冷間加工率63%)の板に加工し、第3表に
示す加熱速度で530℃の温度で加熱軟化処理を行
ない、550℃の温度で歪速度2×10-4/secで変形
をした。[Table] Example 3 Alloy 3 of Example 1 (thickness: 400 mm), which was cast by a normal DC casting method, was homogenized at a temperature of 510°C for 12 hours, and then heated and rolled at a temperature of 450 to 300°C. Processed into a 4.0mm thick plate and heated at 540℃ for 3 hours and
After heating and holding for 10 hours at a temperature of 450℃, approx.
1.5 by cold rolling after cooling at a cooling rate of 100℃/Hr
mm thick (cold working ratio 63%), heat softened at a temperature of 530°C at the heating rate shown in Table 3, and heated at a temperature of 550°C with a strain rate of 2×10 -4 /sec. Deformed.
以上説明したように、本発明に係る超塑性アル
ミニウム合金の製造方法は上記の構成を有してい
るものであるから、適切な温度においてくびれ
(necking)の局所伸び等がない。優れた超塑性
伸びを有する材料が得られるという効果がある。
As explained above, since the method for producing a superplastic aluminum alloy according to the present invention has the above configuration, there is no local elongation of necking at an appropriate temperature. This has the effect of providing a material with excellent superplastic elongation.
Claims (1)
系合金鋳塊を、400〜550℃の温度で均質化熱処理
を行ない、次いで、300〜550℃の温度で熱間加工
を行なつた後、第1回の加熱保持を450〜550℃の
温度で0.5〜10Hr行ない、次に、第2回の加熱温
度まで冷却し、350〜450℃の温度で0.5〜50Hrの
第2回の加熱保持を行ない、30℃/Hr以上の冷
却速度で冷却した後、少なくとも30%以上の冷間
加工を行なうことを特徴とする超塑性アルミニウ
ム合金の製造方法。 2 Mg2〜7wt% を含有し、さらに、 Mn0.05〜1.5wt%、Cr0.05〜0.5wt%、 Zr0.05〜0.5wt%、V0.05〜0.5wt%、 Ti0.15wt%以下 の中から選んだ1種または2種以上 を含有し、残部Alおよび不純物からなるAl―Mg
系合金鋳塊を、400〜550℃の温度で均質化熱処理
を行ない、次いで、300〜550℃の温度で熱間加工
を行なつた後、第1回の加熱保持を450〜550℃の
温度で0.5〜10Hr行ない、次に、第2回の加熱温
度まで冷却し、350〜450℃の温度で0.5〜50Hrの
第2回の加熱保持を行ない、30℃/Hr以上の冷
却速度で冷却した後、20〜60%の冷間加工を行な
い、続いて、300℃以下の低温軟化焼鈍と冷間加
工を1回以上行なうことを特徴とする超塑性アル
ミニウム合金の製造方法。 3 Mg2〜7wt% を含有し、さらに、 Mn0.05〜1.5wt%、Cr0.05〜0.5wt%、 Zr0.05〜0.5wt%、V0.05〜0.5wt%、 Ti0.15wt%以下 の中から選んだ1種または2種以上 を含有し、残部Alおよび不純物からなるAl―Mg
系合金鋳塊を、400〜550℃の温度で均質化熱処理
を行ない、次いで、300〜550℃の温度で熱間加工
を行なつた後、第1回の加熱保持を450〜550℃の
温度で0.5〜10Hr行ない、次に、第2回の加熱温
度まで冷却し、350〜450℃の温度で0.5〜50Hrの
第2回の加熱保持を行ない、30℃/Hr以上の冷
却速度で冷却した後、少なくとも30%以上の冷間
加工を行なうか、或いは、20〜60%の冷間加工を
行ない、続いて、300℃以下の低温軟化焼鈍と冷
間加工を1回以上行ない、さらに、100℃/Hr以
上の加熱速度で350〜550℃の温度に加熱軟化処理
することを特徴とする超塑性アルミニウム合金の
製造方法。[Claims] 1 Contains Mg2-7wt%, and further includes Mn0.05-1.5wt%, Cr0.05-0.5wt%, Zr0.05-0.5wt%, V0.05-0.5wt%, Ti0 Al-Mg containing one or more selected from .15wt% or less, with the balance consisting of Al and impurities.
The alloy ingot is subjected to homogenization heat treatment at a temperature of 400 to 550°C, then hot worked at a temperature of 300 to 550°C, and then the first heating holding is carried out at a temperature of 450 to 550°C. Then, it was cooled to the second heating temperature, and the second heating was held at a temperature of 350 to 450°C for 0.5 to 50 hours, and then cooled at a cooling rate of 30°C/Hr or more. 1. A method for producing a superplastic aluminum alloy, which is then subjected to cold working of at least 30% or more. 2 Contains Mg2~7wt%, and further contains Mn0.05~1.5wt%, Cr0.05~0.5wt%, Zr0.05~0.5wt%, V0.05~0.5wt%, and Ti0.15wt% or less. Al-Mg containing one or more selected from the following, with the balance consisting of Al and impurities
The alloy ingot is subjected to homogenization heat treatment at a temperature of 400 to 550°C, then hot worked at a temperature of 300 to 550°C, and then the first heating holding is carried out at a temperature of 450 to 550°C. Then, it was cooled to the second heating temperature, and the second heating was held at a temperature of 350 to 450°C for 0.5 to 50 hours, and then cooled at a cooling rate of 30°C/Hr or more. A method for producing a superplastic aluminum alloy, which comprises performing cold working of 20 to 60%, followed by low-temperature softening annealing at 300°C or less and cold working one or more times. 3 Contains Mg2~7wt%, and further contains Mn0.05~1.5wt%, Cr0.05~0.5wt%, Zr0.05~0.5wt%, V0.05~0.5wt%, and Ti0.15wt% or less. Al-Mg containing one or more selected from the following, with the balance consisting of Al and impurities
The alloy ingot is subjected to homogenization heat treatment at a temperature of 400 to 550°C, then hot worked at a temperature of 300 to 550°C, and then the first heating holding is carried out at a temperature of 450 to 550°C. Then, it was cooled to the second heating temperature, and the second heating was held at a temperature of 350 to 450°C for 0.5 to 50 hours, and then cooled at a cooling rate of 30°C/Hr or more. After that, cold working is performed by at least 30%, or cold working is performed by 20 to 60%, followed by low temperature softening annealing and cold working at 300°C or less, and then 100% cold working is performed. A method for producing a superplastic aluminum alloy, comprising heating and softening the alloy to a temperature of 350 to 550°C at a heating rate of ℃/Hr or more.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9417784A JPS60238461A (en) | 1984-05-11 | 1984-05-11 | Manufacture of superplastic aluminum alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9417784A JPS60238461A (en) | 1984-05-11 | 1984-05-11 | Manufacture of superplastic aluminum alloy |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS60238461A JPS60238461A (en) | 1985-11-27 |
| JPS62225B2 true JPS62225B2 (en) | 1987-01-06 |
Family
ID=14103056
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP9417784A Granted JPS60238461A (en) | 1984-05-11 | 1984-05-11 | Manufacture of superplastic aluminum alloy |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS60238461A (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6376857A (en) * | 1986-09-19 | 1988-04-07 | Showa Alum Corp | Manufacture of aluminum alloy for mirror finish working |
| JP2640993B2 (en) * | 1990-06-11 | 1997-08-13 | スカイアルミニウム株式会社 | Aluminum alloy rolled plate for superplastic forming |
| WO2007080938A1 (en) | 2006-01-12 | 2007-07-19 | Furukawa-Sky Aluminum Corp. | Aluminum alloys for high-temperature and high-speed forming, processes for production thereof, and process for production of aluminum alloy forms |
| CN115896652B (en) * | 2022-12-01 | 2024-05-03 | 中南大学 | Preparation method of superplastic aluminum-lithium alloy fine-grain plate with high strain rate |
-
1984
- 1984-05-11 JP JP9417784A patent/JPS60238461A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS60238461A (en) | 1985-11-27 |
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