JPS6369954A - Stretcher leveling method for high-tensile aluminum alloy plate - Google Patents

Stretcher leveling method for high-tensile aluminum alloy plate

Info

Publication number
JPS6369954A
JPS6369954A JP21568486A JP21568486A JPS6369954A JP S6369954 A JPS6369954 A JP S6369954A JP 21568486 A JP21568486 A JP 21568486A JP 21568486 A JP21568486 A JP 21568486A JP S6369954 A JPS6369954 A JP S6369954A
Authority
JP
Japan
Prior art keywords
stretcher
tensile
alloy plate
aluminum alloy
time
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP21568486A
Other languages
Japanese (ja)
Inventor
Masanori Ito
正徳 伊藤
Kazuhiro Nakada
和宏 中田
Yumi Hiraoka
平岡 優美
Tetsuro Ogawa
小河 哲朗
Hideyo Ono
大野 秀世
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Kobe Steel Ltd
Original Assignee
Kobe Steel Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Kobe Steel Ltd filed Critical Kobe Steel Ltd
Priority to JP21568486A priority Critical patent/JPS6369954A/en
Publication of JPS6369954A publication Critical patent/JPS6369954A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To prevent the occurrence of stretcher strain and also to shorten the length of aging time in the following stage, by heating an age-hardening high-tensile Al alloy plate at a temp. in a specific range for a period having specific relations with the above temp. at the time of subjecting the above Al alloy plate to stretcher leveling after solution heat treatment. CONSTITUTION:An age-hardening high-tensile Al alloy, e.g., metal plate of 2000 or 7000 type is first subjected to solution heat treatment in order to allow solute atoms such as Cu, Zn, Mg, etc., to enter into solid solution. Since thermal strain occurs at this time, stretcher leveling is carried out by means of a stretcher, etc., and, prior to the above leveling, the above Al alloy plate is subjected to heating treatment at a temp. T( deg.C) of 250-750 deg.C for a time (t)(hr) satisfying an inequality. By this heat treatment, the concentration of the solute atoms existing in solid solution in the plate matrix is lowered and, as a result, formation of GP zone is inhibited and repetition of multiple yield can also be inhibited during tensile deformation, so that prevention of stretcher strain can be attained.

Description

【発明の詳細な説明】 [産業上の利用分野1 本発明は高力アルミニウム合金板の引張矯正方法に関す
る。
DETAILED DESCRIPTION OF THE INVENTION [Industrial Field of Application 1] The present invention relates to a tensile straightening method for high-strength aluminum alloy plates.

[従来技術] 時効硬化型の高力アルミニウム合金、たとえば2000
系、7000系の材料(以後高力アルミ等の溶質原子を
固溶させるために溶体化処理を行なう。
[Prior art] Age-hardening high-strength aluminum alloy, such as 2000
7000 series materials (hereinafter, solution treatment is performed to dissolve solute atoms such as high-strength aluminum).

なお、上記の溶体化処理条件は、品種によって多少異な
るが、その温度は2000系では470〜530℃、7
000系では450〜500℃が一般的である。また、
処理時間は板厚によって異なるが通常0.1〜5時間で
行なわれる。
The above solution treatment conditions vary slightly depending on the product, but the temperature for the 2000 series is 470-530℃, 7
For the 000 series, the temperature is generally 450 to 500°C. Also,
The treatment time varies depending on the thickness of the plate, but is usually 0.1 to 5 hours.

しかるに、材料が板の場合にはこの溶体化処理時に熱歪
が発生するのでストレッチャー等により引張矯正を行な
い、板のそり、波等の歪を除去してフラットにする0通
常、引張は、板の永久伸びが0.5%程度になるような
引張力で行なわれる。
However, when the material is a plate, thermal distortion occurs during this solution treatment, so tensile straightening is performed using a stretcher or the like to remove distortions such as warps and waves on the plate and flatten it.Usually, the tension is The tensile force is such that the permanent elongation of the plate is about 0.5%.

以上のような引張矯正後、必要に応じて仕上加工、常温
時効処理あるいは焼戻処理が行なわれ、次工程の加工素
材として供給される。
After the tensile straightening as described above, finishing processing, room temperature aging treatment, or tempering treatment is performed as necessary, and the material is supplied as a processed material for the next process.

ところで、上記したように溶体化処理後に引張矯正を行
なうと、板表面にストレッチャー・ストシン(ストレッ
チャー矯正時に発生する板表面のしま状校様)が発生す
る。
By the way, as described above, when tensile straightening is performed after solution treatment, stretcher strutsine (stripes on the plate surface that occurs during stretcher straightening) occurs on the plate surface.

従来、ストレッチャーの防止技術としては次の技術が知
られている。
Conventionally, the following techniques are known as stretcher prevention techniques.

■軟鋼板についてものとしてローラレベル加工を行なう
技術。
■Technology for performing roller level processing on mild steel plates.

■軟鋼板についてのものとして引張予加工を行なう技術
■Technology for tensile pre-processing for mild steel plates.

■常温時効時間の増加や高速成形または低温成形する技
術。
■Technology for increasing room temperature aging time and high-speed molding or low-temperature molding.

以上は「塑性と加工J voJ115、No 162(
1974−7)P526〜P534に開示されている。
The above is from “Plasticity and Processing J voJ115, No. 162 (
1974-7) P526 to P534.

[発明が解決しようとする問題点] 上記した従来の方法による高力アルミニウム合金板のス
トレッチャー・ストレイン防止技術では次のような問題
点がある。
[Problems to be Solved by the Invention] The conventional technique for preventing stretcher strain of high-strength aluminum alloy plates as described above has the following problems.

■ローラレベル加工あるいは引張予加工を行なう技術で
はアルミニウム合金板についてはストレッチャー・スト
レインを防止することはできない。
■ Roller level processing or tension pre-processing techniques cannot prevent stretcher strain on aluminum alloy plates.

■常温時効時間を増加させる等の技術では、温度の制御
、加工速度の制御がむずかしく、同一の条件を毎回の処
理で維持することが困難である。
■With techniques such as increasing the aging time at room temperature, it is difficult to control the temperature and processing speed, and it is difficult to maintain the same conditions in each process.

その結果、製品間のバラツキが多くなり、すべてについ
てストレッチャー・ストレインのない均一な製品を製造
することができない、また生産性も悪い。
As a result, there are many variations between products, making it impossible to manufacture uniform products without stretcher strain, and productivity is also poor.

本発明以上のような事情に鑑み高力アルミニウム合金板
のストレッチャー・ストレインマークを制御するために
有効な引張矯正加工方法を見出し、それにもとづきなさ
れたものである。
In view of the above-mentioned circumstances, the present invention has discovered an effective tensile straightening method for controlling stretcher strain marks on high-strength aluminum alloy plates, and has developed the present invention based on this method.

[問題点を解決するための手段] 上記問題点は1時効硬化型の高力アルミニウム合金より
なる板を溶体化処理後引張矯正する方法において、該引
張矯正する前に該高力アルミニウム合金板を25℃以上
75℃以下の温度T (℃)で t≧−0.51T+42.75−6一式1を満足する時
間t(時間)加熱処理することを特徴とする高力アルミ
ニウム合金板の引張矯正方法によって解決される。
[Means for Solving the Problems] The above problem arises in the method of tensile straightening a plate made of an age-hardening high-strength aluminum alloy after solution treatment, in which the high-strength aluminum alloy plate is A method for tensile straightening a high-strength aluminum alloy plate, characterized by heat treatment for a time t (hours) satisfying t≧-0.51T+42.75-6 set 1 at a temperature T (℃) of 25℃ or higher and 75℃ or lower. solved by.

本発明では時効硬化型高力アルミニウム合金を対象とす
る。かかる合金としては、たとえば。
The present invention targets age-hardening high-strength aluminum alloys. Examples of such alloys include:

2000系、7000系の高力アルミニウム合金があげ
られる。
Examples include 2000 series and 7000 series high strength aluminum alloys.

本発明においては溶体化処理条件には限定されない、溶
体化処理条件は、品種によって多少異なるが、その温度
は、たとえば2000系では470〜530℃、700
0系では450〜500℃が一般的である。また、処理
時間は板厚によって異なるが通常0.1〜5時間で行な
われる。もちろん以上の条件は例示であり、かかる条件
により本発明範囲は限定されるものではない。
In the present invention, the solution treatment conditions are not limited to the solution treatment conditions.The solution treatment conditions differ somewhat depending on the product, but the temperature is, for example, 470-530℃ for the 2000 series, 700℃
For 0 series, the temperature is generally 450 to 500°C. Further, although the treatment time varies depending on the thickness of the plate, it is usually carried out for 0.1 to 5 hours. Of course, the above conditions are merely examples, and the scope of the present invention is not limited by these conditions.

本発明では溶体化処理後引張矯正する前に該高力アルミ
ニウム合金板を25℃以上75℃以下の温度T (’O
)で t≧−0.51T+42.75・・・式1を満足する時
間t(時間)加熱処理する。
In the present invention, the high-strength aluminum alloy plate is heated at a temperature T ('O
), t≧-0.51T+42.75...The heat treatment is performed for a time t (hours) that satisfies formula 1.

加熱温度25℃未満では引張矯正時にストレッチャー・
ストレインが発生する。
If the heating temperature is less than 25℃, a stretcher or a
Strain occurs.

すた、力nハ氾唯を椿厚温麻領成まで高くし、加熱時間
を長くすると金属間化合物の析出により高力アルミニウ
ム合金板に中間相が形成されて時効硬化が著しく進行し
、矯正加工が困難になるので、加熱温度は75℃以下、
従って式1から加熱時間は30時間以内にする。
When the strength and force are increased to the Tsubaki region and the heating time is prolonged, an intermediate phase is formed in the high-strength aluminum alloy plate due to the precipitation of intermetallic compounds, and age hardening progresses significantly, resulting in straightening. The heating temperature should not be more than 75℃, as it will be difficult to process.
Therefore, according to formula 1, the heating time should be within 30 hours.

なお、加熱温度30℃以上、加熱時間1時間以上がより
好ましい。
In addition, the heating temperature is more preferably 30° C. or more and the heating time is more preferably 1 hour or more.

ストレッチャー・ストレインの防止はこの予備加熱処理
によって板付材中に固溶していた溶質原子の濃度が低下
し、そのため引張変形中、GPゾーンの形成が抑制され
る。つまり、多重降伏の繰り返しが抑えられるためにス
トレッチャm−ストレインの防止が達成される。
Stretcher strain can be prevented by reducing the concentration of solute atoms dissolved in the plate material by this preheating treatment, thereby suppressing the formation of GP zones during tensile deformation. In other words, since the repetition of multiple yielding is suppressed, stretcher m-strain can be prevented.

以上の予備熱処理後に引張矯正を行なう、引張矯正の条
件については特に限定されない、たとえば、引張応力は
板の永久伸びが0.5%程度となるような応力でよい。
The conditions for tensile straightening after the above preliminary heat treatment are not particularly limited. For example, the tensile stress may be such that the permanent elongation of the plate is about 0.5%.

なお、引張矯正後は必要に応じて仕上加工、常温時効処
理あるいは焼戻処理が行なわれる0通常焼戻処理は品種
により処理温度が多少異なるが2000系で150〜2
00℃、7000系で110〜130℃、処理時間は2
000系で6〜24時間、7000系で20〜30時間
程度である。かかる処理により時効硬化が十分に達成さ
れる。もちろん、時効処理条件、焼戻処理条件により本
発明範囲は限定されるものではない。
After tensile straightening, finishing processing, room-temperature aging treatment, or tempering treatment is performed as necessary. Normally, the treatment temperature for tempering treatment varies depending on the product, but for the 2000 series it is 150~2
00℃, 110-130℃ for 7000 series, processing time is 2
For the 000 series, it takes about 6 to 24 hours, and for the 7000 series, it takes about 20 to 30 hours. Such treatment achieves sufficient age hardening. Of course, the scope of the present invention is not limited by the aging treatment conditions and tempering treatment conditions.

[発明の実施例] (第1実施例) 7000系の高力アルミニウム合金板の代表例として7
075合金板を用い4X1000X2000mmの平板
の試験片を作成した。
[Embodiments of the invention] (First embodiment) 7 as a representative example of a 7000 series high strength aluminum alloy plate
A flat test piece of 4 x 1000 x 2000 mm was prepared using a 075 alloy plate.

上記試験片を約470℃の塩浴中に0.7時間浸漬し、
その後水冷して溶体化処理を行なった。
The above test piece was immersed in a salt bath at about 470°C for 0.7 hours,
Thereafter, it was cooled with water and subjected to solution treatment.

試験片には溶体化処理終了後に空気温度を約50℃に保
持した炉に搬入し、10時間の保持を行なった・ 炉より取り出した試験片をストレッチャーを用いて板の
長手方向に伸びが約1%になるまで引張荷重を加え、試
験片の矯正を行なった。
After the solution treatment was completed, the test piece was transported into a furnace where the air temperature was maintained at approximately 50°C and held for 10 hours.The test piece was taken out of the furnace and stretched in the longitudinal direction of the plate using a stretcher. A tensile load was applied to the specimen until it reached approximately 1%, and the test piece was straightened.

引張矯正加工した板は表面はフラットになり歪もなく、
ストレッチャー・ストレインも認められなかった。
The surface of the tensile straightened plate is flat and there is no distortion.
Stretcher strain was also not allowed.

さらに、約120℃の油中に浸漬して焼戻処をしたとこ
ろ、24時間で時効硬化せしめることができた。板の歪
もほとんど認められなかった。
Furthermore, when it was tempered by immersing it in oil at about 120°C, it was able to age harden in 24 hours. Almost no distortion of the board was observed.

(実施例2) 2000系の高力アルミニウム合金板の代表例として2
024合金板を用い、4X1000X2000mmの平
板の試験片を作成した。
(Example 2) As a representative example of 2000 series high strength aluminum alloy plate, 2
A flat test piece measuring 4 x 1000 x 2000 mm was prepared using a 024 alloy plate.

上記試験片を約490℃の塩浴中に浸清し、その後水冷
して溶体化処理を行なった。試験片には溶体化処理終了
後に空気温度を約60℃に保持した恒温槽に浸漬し4時
間内の保持を行なった。
The above test piece was immersed in a salt bath at about 490°C, and then cooled with water to perform solution treatment. After the solution treatment, the test piece was immersed in a constant temperature bath in which the air temperature was maintained at approximately 60°C for 4 hours.

その後、上記試験片をストレッチャーで板厚方向に伸び
が約0.5%になるまで引張荷重を加え、試験片の矯正
加工を行なった。
Thereafter, a tensile load was applied to the test piece using a stretcher until the elongation reached approximately 0.5% in the thickness direction, and the test piece was corrected.

引張矯正加工した板はフラットになり、歪もなく、スト
レッチャー・ストレインも認められなかったψ さらにこの板を常温時効(T4)、冷間圧延(T3)、
焼戻処理(T6)、あるいは冷間圧延後焼戻処理(T8
)をした。
The tensile straightened plate became flat, with no distortion, and no stretcher strain was observed.
Tempering treatment (T6) or tempering treatment after cold rolling (T8)
)Did.

いずれも歪のない板が得られた。なお、T4処理の時効
時間は500hrであった。
In both cases, plates without distortion were obtained. Note that the aging time of the T4 treatment was 500 hr.

以上実施例を示したが、ここで注意を要することは本発
明の予備加熱処理の温度、時間は30℃以上になるので
、大気中放置処理が可能にみえるが、大気温度が変化す
るため母材中の溶質原子の拡散速度も変化するのでスト
レッチャーψストレインの発生度合が異なるので加熱処
理時間が調整できない。
Although the examples have been shown above, it should be noted here that the temperature and time of the preheating treatment of the present invention are 30°C or higher, so it seems possible to leave the treatment in the atmosphere, but since the atmospheric temperature changes, Since the diffusion rate of solute atoms in the material also changes, the degree of occurrence of stretcher ψ strain differs, so the heat treatment time cannot be adjusted.

本発明の熱処理によりストレッチャーφストレインの発
生を防止するには加熱温度が30℃近傍の低い温度では
30時間近くの長い時間に一定に保持、あるいは75℃
近くの高い温度では30分程度の短い時間に一定に保持
してGPゾーンの形成を終了せしめることにある。
To prevent the occurrence of stretcher φ strain by the heat treatment of the present invention, the heating temperature must be kept constant for a long time of nearly 30 hours at a low temperature around 30°C, or 75°C.
At nearby high temperatures, the temperature is kept constant for a short period of about 30 minutes to complete the formation of the GP zone.

[発明の効果] 以上説明したように、本発明の引張矯正方法を埋用する
ことによ41 、時効硬イに型の高力アルミニウム合金
板、たとえば、2000系、7000系高力アルミニウ
ム合金板のストレッチャー・ストレインの発生を防止す
ることができるばかりでなく、後工程の時効処理(常温
時効、焼戻時効)の時間を大幅に短縮できる効果もある
[Effects of the Invention] As explained above, by applying the tensile straightening method of the present invention, high-strength aluminum alloy plates with aging hardness, such as 2000 series and 7000 series high-strength aluminum alloy plates, can be produced. Not only can stretcher strain be prevented from occurring, but the time for post-process aging treatment (room temperature aging, tempering aging) can also be significantly shortened.

Claims (1)

【特許請求の範囲】 時効硬化型の高力アルミニウム合金よりなる板を溶体化
処理後引張矯正する方法において、該引張矯正する前に
該高力アルミニウム合金板を25℃以上75℃以下の温
度T(℃)で t≧−0.51T+42.75・・・式1 を満足する時間t(時間)加熱処理することを特徴とす
る高力アルミニウム合金板の引張矯正方法。
[Scope of Claims] In a method of tensile straightening a plate made of an age-hardening high-strength aluminum alloy after solution treatment, the high-strength aluminum alloy plate is heated at a temperature T of 25°C or more and 75°C or less before the tensile straightening. A method for tensile straightening a high-strength aluminum alloy plate, which comprises heat-treating a high-strength aluminum alloy plate for a time t (hours) satisfying the following formula: t≧-0.51T+42.75 (°C).
JP21568486A 1986-09-11 1986-09-11 Stretcher leveling method for high-tensile aluminum alloy plate Pending JPS6369954A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP21568486A JPS6369954A (en) 1986-09-11 1986-09-11 Stretcher leveling method for high-tensile aluminum alloy plate

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP21568486A JPS6369954A (en) 1986-09-11 1986-09-11 Stretcher leveling method for high-tensile aluminum alloy plate

Publications (1)

Publication Number Publication Date
JPS6369954A true JPS6369954A (en) 1988-03-30

Family

ID=16676445

Family Applications (1)

Application Number Title Priority Date Filing Date
JP21568486A Pending JPS6369954A (en) 1986-09-11 1986-09-11 Stretcher leveling method for high-tensile aluminum alloy plate

Country Status (1)

Country Link
JP (1) JPS6369954A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100857497B1 (en) 2007-03-28 2008-09-08 한병수 Method for producing aluminium alloy plate comprising leveling process and the leveling apparatus
CN105385969A (en) * 2015-12-23 2016-03-09 常熟市淼泉压缩机配件有限公司 Thermal treatment process for thin-wall aluminum alloy component

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100857497B1 (en) 2007-03-28 2008-09-08 한병수 Method for producing aluminium alloy plate comprising leveling process and the leveling apparatus
CN105385969A (en) * 2015-12-23 2016-03-09 常熟市淼泉压缩机配件有限公司 Thermal treatment process for thin-wall aluminum alloy component

Similar Documents

Publication Publication Date Title
KR100374104B1 (en) Heat treatment process for aluminum alloy sheet
US20150240339A1 (en) Tailored rolling of high strength aluminum
US3232796A (en) Treatment of aluminum-magnesium alloy
US4799974A (en) Method of forming a fine grain structure on the surface of an aluminum alloy
US4374682A (en) Process for producing deep-drawing cold rolled steel strips by short-time continuous annealing
JPS60211057A (en) Production of al-base alloy product
US4295901A (en) Method of imparting a fine grain structure to aluminum alloys having precipitating constituents
KR20180070935A (en) Roll-forming method of high strength aluminum alloy and roll-forming molding using the same
US4528042A (en) Method for producing superplastic aluminum alloys
JPS6369954A (en) Stretcher leveling method for high-tensile aluminum alloy plate
US4486242A (en) Method for producing superplastic aluminum alloys
US4358324A (en) Method of imparting a fine grain structure to aluminum alloys having precipitating constituents
JPH0967659A (en) Method for heat treating aluminum-magnesium-silicon base aluminum alloy
JPH0517857A (en) Method for treating metal matrix composite material
RU2335571C2 (en) Method of fabricating plates out of titanium alloy
US2836527A (en) Method for producing flat solution heat treated titanium and zirconium alloy sheets
SU933789A1 (en) Process for treating aluminium-based alloys
JPH0421747A (en) Heat treatment for hot formed parts of al-li alloy
JPS63162818A (en) Manufacture of ferritic stainless steel sheet extremely excellent in press formability
RU2052533C1 (en) Method for thermomechanical treatment of sheets from aluminum alloys containing lithium
JPS634907B2 (en)
JP2578174B2 (en) Processing method of β-type titanium alloy
JPH0130893B2 (en)
JPH0261042A (en) Production of beta titanium alloy wire having high fatigue strength
JPS62127455A (en) Manufacture of heat treatment-type aluminum-alloy rolled sheet