JPH08206706A - Hot rolling method of al-li alloy - Google Patents

Hot rolling method of al-li alloy

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Publication number
JPH08206706A
JPH08206706A JP4125995A JP4125995A JPH08206706A JP H08206706 A JPH08206706 A JP H08206706A JP 4125995 A JP4125995 A JP 4125995A JP 4125995 A JP4125995 A JP 4125995A JP H08206706 A JPH08206706 A JP H08206706A
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JP
Japan
Prior art keywords
rolling
alloy
hot rolling
temperature
ingot
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.)
Granted
Application number
JP4125995A
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Japanese (ja)
Other versions
JP3197774B2 (en
Inventor
Toshimasa Sakamoto
敏正 坂本
Takuzo Hagiwara
卓三 萩原
Kazunori Kobayashi
一徳 小林
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ALITHIUM KK
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ALITHIUM KK
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Priority to JP04125995A priority Critical patent/JP3197774B2/en
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Publication of JP3197774B2 publication Critical patent/JP3197774B2/en
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Abstract

PURPOSE: To provide a hot rolling method of an Al-Li alloy by which the generation of edge crack and surface defects is prevented. CONSTITUTION: In the method for hot-rolling the Al-Li alloy, a cast billet of the Al-Li alloy contg. 0.5-3.0% Li, further, one or >=2 kinds of 1.0-3.0% Cu, 0.5-2.0% Mg, 0.06-0.3% Zr, 0.06-0.3% V, 0.06-0.3% Mn, 0.06-0.3% Cr, 0.02-0.3% Ti as a selective component, the balance Al and inevitable impurities is homogenized in the temp. range of 520±50 deg.C for 1-24hours. After that, hot rolling is started in the temp. range of 520±30 deg.C and completed at >=250 deg.C, preferably, >=300 deg.C. As rolling reduction per pass, 3-30mm is preferable and it is preferable to execute rolling of 5-50mm in the width direction on one side by the number of >=20% of the total number of rolling.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、Al−Li合金の熱間
圧延方法、とくに、熱間圧延工程のおいて、耳割れなど
の割れの発生、縞模様などの表面欠陥の発生を防止でき
るAl−Li合金の熱間圧延方法に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention can prevent the occurrence of cracks such as edge cracks and the occurrence of surface defects such as striped patterns in the hot rolling method for Al-Li alloys, especially in the hot rolling process. The present invention relates to a hot rolling method for an Al-Li alloy.

【0002】[0002]

【従来の技術】Al−Li合金は、強度、剛性率が高く
密度が低いため、比強度、比剛性に優れ、航空・宇宙用
材料として期待されているが、その製造技術はまだ十分
に確立されていない。例えば、熱間圧延においても、従
来のアルミニウム合金以上に耳割れや表面欠陥が生じ易
く、圧延技術の確立が要望されている。
2. Description of the Related Art Al-Li alloys, which have high strength and rigidity and low density, are excellent in specific strength and specific rigidity and are expected as materials for aerospace, but their manufacturing technology is not yet fully established. It has not been. For example, even in hot rolling, edge cracks and surface defects are more likely to occur than in conventional aluminum alloys, and establishment of rolling technology is desired.

【0003】発明者らは、Al−Li合金の熱間圧延時
に発生する割れや表面結果を防止するために、合金成
分、鋳塊の面削方法、鋳塊の均質化処理、圧延条件とそ
れらの関連性について多角的に基礎的実験検討を行い、
種々の知見を得た。
In order to prevent cracks and surface results that occur during hot rolling of Al-Li alloys, the inventors have studied alloy components, ingot surface chamfering method, ingot homogenization treatment, rolling conditions and the like. We conducted basic experimental studies on the relevance of
We obtained various findings.

【0004】[0004]

【発明が解決しようとする課題】本発明は、上記の基礎
的実験検討から得られた知見に基づいてなされたもので
あり、その目的は、熱間圧延の工程で耳割れなどの割れ
や模様発生などの表面欠陥を生じることが防止されるA
l−Li合金の熱間圧延方法を提供することにある。
The present invention has been made on the basis of the knowledge obtained from the above-mentioned basic experimental examinations, and its purpose is to provide cracks and patterns such as ear cracks in the hot rolling process. A that prevents surface defects such as generation
An object of the present invention is to provide a hot rolling method for 1-Li alloy.

【0005】[0005]

【課題を解決するための手段】上記の目的を達成するた
めの本発明によるAl−Li合金の熱間圧延方法は、L
i0.5 〜3.0 %を含有し、さらにCu1.0 〜3.0 %( 但
し、Mgを含有しない場合は1.5 〜5.5 %)、Mg0.5
〜2.0 %、Zr0.06〜0.3 %、V0.06〜0.3 %、Mn0.
06〜0.3 %、Cr0.06〜0.3 %、Ti0.02〜0.3 %のう
ちの1種または2種以上を含有し、残部がAlおよび不
可避的不純物からなるAl−Li合金の鋳塊を、520 ℃
±50℃の温度範囲に加熱して、1 〜24時間保持したの
ち、該温度範囲で熱間圧延を開始し、250 ℃以上の温度
で熱間圧延を終了することを第1の特徴とする。
A method of hot rolling an Al--Li alloy according to the present invention for achieving the above-mentioned object is L
i0.5-3.0%, further Cu1.0-3.0% (however, if Mg is not contained 1.5-5.5%), Mg0.5
.About.2.0%, Zr0.06 to 0.3%, V0.06 to 0.3%, Mn0.
An ingot of an Al-Li alloy containing one or more of 06 to 0.3%, Cr 0.06 to 0.3%, and Ti 0.02 to 0.3%, and the balance being Al and unavoidable impurities, ℃
The first feature is that after heating to a temperature range of ± 50 ° C and holding for 1 to 24 hours, hot rolling is started in the temperature range and hot rolling is finished at a temperature of 250 ° C or higher. .

【0006】また、Li0.5 〜3.0 %を含有し、さらに
Zr0.06〜0.3 %、V0.06〜0.3 %、Mn0.06〜0.3
%、Cr0.06〜0.3 %のうちの1種または2種以上を含
有し、残部がAlおよび不可避的不純物からなるAl−
Li合金の鋳塊を、450 ℃±30℃の温度範囲に1 〜30時
間加熱したのち、520 ℃±50℃の温度範囲に加熱して1
〜24時間保持し、ついで該温度範囲で熱間圧延を開始
し、250 ℃以上の温度で熱間圧延を終了することを本発
明の第2の特徴とする。
Further, it contains Li 0.5 to 3.0%, Zr 0.06 to 0.3%, V 0.06 to 0.3%, Mn 0.06 to 0.3%.
%, Cr 0.06 to 0.3%, and one or more of them, the balance being Al and unavoidable impurities.
The ingot of Li alloy is heated to a temperature range of 450 ° C ± 30 ° C for 1 to 30 hours, and then heated to a temperature range of 520 ° C ± 50 ° C for 1 hour.
The second feature of the present invention is to hold for up to 24 hours, then start hot rolling within the temperature range, and finish hot rolling at a temperature of 250 ° C. or higher.

【0007】さらに、熱間圧延の1回当たりの圧下量
を、最終圧延を除いて3 〜30mmとすると、総圧延回数の
うちの20%以上の回数の圧延段階で、それぞれ圧延板側
面部に片側5 〜50mmの幅方向圧延を行うこと、およびA
l−Li合金の鋳塊の圧延面および側面が5mm 以上面削
され、面粗度Raが2 μm 以下、うねりが200 μm 以下
に仕上げられていることをそれぞれ第3、第3および第
4の特徴とする。
Further, if the amount of reduction per hot rolling is 3 to 30 mm excluding the final rolling, the side surface of the rolled plate is rolled at 20% or more of the total rolling times. Performing widthwise rolling of 5 to 50 mm on one side, and A
The rolled surface and the side surface of the ingot of the l-Li alloy are chamfered by 5 mm or more, and the surface roughness Ra is 2 μm or less and the waviness is 200 μm or less. Characterize.

【0008】本発明の目的を達成するためには、まず本
発明のAl−Li合金の組成を特定の範囲に限定しなけ
ればならない。本発明において使用するAl−Li合金
における合金元素の意義および限定理由について説明す
ると、Liは、合金材料を軽量化し強度を向上させる元
素であり、好ましい含有範囲は0.5 〜3.0 %であり、1.
0 %未満では軽量化および比強度、比剛性向上の効果が
得られず、3.0 %を越えて含有すると、鋳造割れ感受性
を増加させると同時に、粗大なδ´相を生成し合金の延
性および靭性を低下させる。
In order to achieve the object of the present invention, the composition of the Al--Li alloy of the present invention must first be limited to a specific range. Explaining the meaning and limitation reason of the alloying element in the Al-Li alloy used in the present invention, Li is an element that reduces the weight of the alloy material and improves the strength, and the preferable content range is 0.5 to 3.0%, and 1.
If it is less than 0%, the effects of weight reduction and improvement of specific strength and specific rigidity cannot be obtained, and if it exceeds 3.0%, the susceptibility to casting cracking is increased, and at the same time, a coarse δ'phase is formed and the ductility and toughness of the alloy are increased. Lower.

【0009】Cuは、Al−Cu系の板状析出物θ´
(Al2 Cu)やAl−Cu−Li系の板状析出物T1
相( Al2 CuLi)を生成し、強度および靭性の向上
に寄与する。好ましい含有範囲は1.0 〜3.0 %であり、
1.0 %未満ではその効果が不十分となり、3.0 %を越え
ると強度および靭性の向上効果が飽和するとともに軽量
化が損なわれる。なお、合金中にMgが含有されない場
合にはCuを1.5 〜5.5%の範囲で含有させるのが好ま
しい。また合金中にMgが含有される場合には、Mgに
よる強度向上効果が期待できるので、Cuの含有量を1.
0 〜2.5 %の範囲に減少することもできる。
Cu is a plate-like precipitate θ'of Al-Cu system.
(Al 2 Cu) or Al-Cu-Li-based plate-like precipitate T 1
It forms a phase (Al 2 CuLi) and contributes to the improvement of strength and toughness. The preferred content range is 1.0 to 3.0%,
If it is less than 1.0%, the effect becomes insufficient, and if it exceeds 3.0%, the effect of improving the strength and toughness is saturated and the weight reduction is impaired. When Mg is not contained in the alloy, Cu is preferably contained in the range of 1.5 to 5.5%. In addition, when Mg is contained in the alloy, the strength improving effect of Mg can be expected, so the content of Cu is set to 1.
It can also be reduced to the range of 0-2.5%.

【0010】Mgは、合金マトリックス中に固溶して合
金の延性および靭性を低下させることなく合金を強化す
ると同時に、Al−Cu−Mg系の準安定相の板状析出
物、S´(Al2 CuMg)を生成することにより、さ
らに強度を向上させる。好ましい含有範囲は0.5 〜2.0
%であり、0.5 %未満ではその効果が小さく、2.0 %を
越えて含有すると、強度は向上するが合金の延性および
靭性を劣化させる。
[0010] Mg solid-solves in the alloy matrix to strengthen the alloy without lowering the ductility and toughness of the alloy, and at the same time, the plate-like precipitate of the Al-Cu-Mg metastable phase, S '(Al. 2 CuMg) to further improve the strength. The preferred content range is 0.5 to 2.0
%, The effect is small if less than 0.5%, and if it exceeds 2.0%, the strength is improved but the ductility and toughness of the alloy are deteriorated.

【0011】Zr、V、Mn、CrおよびTiは、合金
組織を微細化するとともに再結晶を抑制する効果があ
り、合金組織を微細で未再結晶状態の結晶組織をするた
めに含有させるもので、好ましい含有範囲は、Zr、
V、MnおよびCrは0.1 〜0.3%、Tiは0.02〜0.3
%である。それぞれ下限未満では十分な効果が得られ
ず、それぞれ上限を越えると、粗大金属間化合物が生成
して強度および靭性を低下させ、またその効果も飽和す
る。
Zr, V, Mn, Cr and Ti have the effects of refining the alloy structure and suppressing recrystallization, and are included to form a fine and unrecrystallized crystal structure. , A preferable content range is Zr,
V, Mn and Cr are 0.1 to 0.3%, Ti is 0.02 to 0.3
%. If the amount is less than the lower limit, a sufficient effect cannot be obtained. If the amount exceeds the upper limit, a coarse intermetallic compound is formed to reduce strength and toughness, and the effect is saturated.

【0012】本発明のAl−Li合金において、0.30%
以下のFe、0.20%以下のSi、0.25%以下のZn、0.
10%以下のCr、0.10%以下のMn、0.15%以下のTi
は、本発明の効果を損なうことがなく、不純物として許
容されるが、これらの不純物は、化合物の生成、あるい
は亜粒界への偏析などにより靭性を低下させるおそれが
あるため、Fe0.10%以下、Si0.10%以下、Zn0.10
%以下、Cr0.05%以下、Mn0.05%以下、Ti0.05%
以下に制限するのがより好ましい。
In the Al--Li alloy of the present invention, 0.30%
Fe below, 0.20% or below Si, 0.25% or below Zn, 0.
10% or less Cr, 0.10% or less Mn, 0.15% or less Ti
Is acceptable as impurities without impairing the effect of the present invention, but since these impurities may reduce the toughness due to the formation of compounds, segregation to subgrain boundaries, etc., Fe0.10% Below, Si0.10% or less, Zn0.10
% Or less, Cr 0.05% or less, Mn 0.05% or less, Ti 0.05%
It is more preferable to limit to the following.

【0013】本発明のAl−Li合金は、溶解後、連続
鋳造し、圧延用鋳塊を製造するが、鋳塊表面には合金成
分のLi、その他の含有成分が偏析し易く、このまま圧
延すると、圧延時に割れの起点となるおそれがあるた
め、熱間圧延に先立って、鋳塊の圧延面および側面を5m
m 以上面削し、表面を粗度Raが2 μm 以下、うねりが
200 μm 以下になるように仕上げるのが好ましい。
The Al-Li alloy of the present invention is melted and continuously cast to produce an ingot for rolling. Li, which is an alloy component, and other contained components are easily segregated on the surface of the ingot, and if it is rolled as it is. Since the starting point of cracking may occur during rolling, the rolling surface and side surface of the ingot should be 5 m before hot rolling.
After chamfering more than m, the surface has a roughness Ra of 2 μm or less and waviness
It is preferable to finish so that the thickness is 200 μm or less.

【0014】鋳塊には、鋳造時にAlLi、CuA
2 、Mg2 Si、FeAl3 などの粗大な金属間化合
物が生成し、これらの金属間化合物は圧延時に割れの原
因となり、合金強化の効果を阻害するので、粗大な金属
間化合物を分解、均質化するために、面削した鋳塊を高
温に加熱、保持することにより均質化処理を行う。好ま
しい均質化処理温度は520 ℃±50℃の範囲であり、保持
時間は1 〜24時間が好ましい。均質化処理温度は高い方
が効率的であるが、高過ぎると化合物やマトリックスが
部分溶解するおそれがあり、低過ぎると長時間の温度保
持を要するため生産効率を下げ、また活性なLiが周辺
の水分と反応して酸化し、製品の性状を劣化させること
からも好ましくない。
The ingot is made of AlLi, CuA during casting.
Coarse intermetallic compounds such as l 2 , Mg 2 Si, and FeAl 3 are generated, and these intermetallic compounds cause cracks during rolling and inhibit the alloy strengthening effect, so that the coarse intermetallic compounds are decomposed, In order to homogenize, the chamfered ingot is heated and held at a high temperature for homogenization. The preferred homogenization temperature is in the range of 520 ° C ± 50 ° C, and the holding time is preferably 1 to 24 hours. The higher the homogenization temperature is, the more efficient it is, but if it is too high, the compound or matrix may be partially dissolved. If it is too low, the temperature needs to be maintained for a long time, which lowers the production efficiency. It is also not preferable because it reacts with the water content of the product and oxidizes to deteriorate the properties of the product.

【0015】合金中に合金成分としてZr、V、Mn、
Crを含有している場合には、これらの元素とアルミニ
ウムの化合物をマトリックス中に微細分散析出させ、製
品板の品質、性状を高めるために、鋳塊を、まず450 ℃
±30℃の温度範囲で1 〜30時間保持し、その後520 ℃±
50℃の均質化処理温度に加熱するのが好ましい。
Zr, V, Mn as alloy components in the alloy,
When Cr is contained, a compound of these elements and aluminum is finely dispersed and precipitated in a matrix, and the ingot is first heated at 450 ° C in order to improve the quality and properties of the product plate.
Hold in the temperature range of ± 30 ° C for 1 to 30 hours, then 520 ° C ±
It is preferred to heat to a homogenization treatment temperature of 50 ° C.

【0016】発明者らは、Al−Li合金における加工
温度と限界加工率との関係を調査するために、Cu、Z
r、Mgを含むAl−Li合金について、直径20mm、高
さ20mmの試料を作製し、これらの試料について各温度で
すえこみ鍛造した場合の割れ発生から、各加工温度にお
ける限界加工率を求めた。その結果の一例を図1に示
す。図1にみられるように、Al−Li合金において
は、加工時の割れ発生を防ぐために、特定の温度域で熱
間加工を行う必要があることがわかる。
The inventors of the present invention investigated Cu, Z and Z in order to investigate the relationship between the processing temperature and the limit processing rate in Al-Li alloys.
For Al-Li alloys containing r and Mg, samples with a diameter of 20 mm and a height of 20 mm were prepared, and the limit processing rate at each processing temperature was determined from the cracking that occurred when the samples were indented and forged at each temperature. . An example of the result is shown in FIG. As can be seen from FIG. 1, in the Al—Li alloy, it is necessary to perform hot working in a specific temperature range in order to prevent cracking during working.

【0017】上記の実験に基づいて、本発明のAl−L
i合金における熱間圧延温度を検討した結果、均質化処
理後、鋳塊を熱間圧延するに際しては、圧延時における
側部割れ(耳割れ)、圧延面割れなどの割れ発生、縞状
模様などの表面欠陥の発生を防止するために、520 ℃±
50℃の温度域で熱間圧延を開始し、250 ℃以上の温度で
熱間圧延を終了するのが好ましいことが判明した。終了
温度は300 ℃以上とするのがより好ましい。
Based on the above experiment, the Al-L of the present invention is used.
As a result of studying the hot rolling temperature of the i alloy, when the ingot is hot rolled after the homogenization treatment, side cracks (ear cracks) during rolling, cracks such as rolling surface cracks, striped patterns, etc. 520 ℃ ± to prevent the occurrence of surface defects
It has been found to be preferable to start hot rolling in the temperature range of 50 ° C and finish hot rolling at a temperature of 250 ° C or higher. The end temperature is more preferably 300 ° C or higher.

【0018】また、Al−Li合金の熱間圧延において
は、圧延一回当たりの圧下量が割れの発生に大きな影響
があることが見出された。割れ発生の観点からは、一回
当たりの圧下量は出来るだけ小さいほうが好ましいが、
小さ過ぎると、所定厚の板に圧延するまでの圧延回数が
増加し、圧延時間が長くなるため、圧延板の温度が上記
の終了温度より低下し易く、また生産効率もわるくなる
という難点があり、一方、一回当たりの圧下量が大き過
ぎると圧延時に耳割れなどが生じる。実験、検討の結果
として見出された圧延一回当たりの最適圧下量は、板厚
を調整するための最終圧延を除き、3 〜30mmであり、可
逆式圧延機を使用して熱間圧延を実施するのが好まし
い。
In the hot rolling of Al-Li alloy, it was found that the amount of reduction per rolling has a great influence on the occurrence of cracks. From the viewpoint of cracking, it is preferable that the amount of reduction per operation is as small as possible.
If it is too small, the number of times of rolling until rolling to a plate of a predetermined thickness increases and the rolling time becomes long, so the temperature of the rolled plate tends to be lower than the above end temperature, and the production efficiency becomes poor. On the other hand, if the amount of reduction per one time is too large, cracks in the edges or the like occur during rolling. The optimum amount of reduction per rolling, which was found as a result of experiments and studies, is 3 to 30 mm, except for the final rolling for adjusting the strip thickness, and hot rolling is performed using a reversible rolling mill. It is preferably carried out.

【0019】さらに、Al−Li合金の熱間圧延時に生
じる欠陥、とくに耳割れの発生を防止するためには、圧
延機に設置されている幅圧延ロールの使用が有効であ
る。幅圧延ロールは、圧延用鋳塊または圧延板の側面部
を圧延するためのものであり、圧延一回毎に幅圧延を行
うのがより望ましいが、生産性を低下させ、側面部の温
度低下を生じて耳割れを引き起こす原因となるなどの難
点があるから、本発明においては、熱間圧延の総圧延回
数のうち少なくとも20%に当たる回数の圧延において、
片側5 〜50mmの幅方向圧延を行う。
Furthermore, in order to prevent the occurrence of defects, especially edge cracks, which occur during the hot rolling of the Al--Li alloy, it is effective to use the width rolling roll installed in the rolling mill. The width rolling roll is for rolling the side surface portion of the ingot for rolling or the rolled plate, and it is more preferable to perform the width rolling after each rolling, but it lowers the productivity and lowers the temperature of the side surface portion. Since there is a problem such as causing the ear cracks to occur, in the present invention, in the number of times of rolling at least 20% of the total number of hot rolling,
Roll widthwise from 5 to 50 mm on one side.

【0020】[0020]

【作用】本発明においては、Li:0.5〜3.0 %を含み、
さらに選択成分として特定量のCu、Mg、Zr、V、
Mn、Cr、Tiを含有させたAl−Li合金を用い、
鋳塊面削条件、鋳塊の均質化処理条件、熱間圧延条件を
特定し、これらの組み合わせにより、Al−Li合金の
熱間圧延時の割れおよび表面欠陥の発生を防止し、品
質、性状の優れたAl−Li合金の板材を得るものであ
る。
In the present invention, Li: 0.5 to 3.0% is contained,
Further, as a selective component, a specific amount of Cu, Mg, Zr, V,
Using an Al-Li alloy containing Mn, Cr and Ti,
Ingot ingot surface cutting conditions, ingot homogenization treatment conditions, and hot rolling conditions are specified, and by combining these, generation of cracks and surface defects during hot rolling of Al-Li alloy is prevented, quality and properties To obtain an excellent Al-Li alloy plate material.

【0021】[0021]

【実施例】以下、本発明の実施例を比較例と対比して説
明する。 実施例1 表1に示す組成を有するAl−Li合金の鋳塊を連続鋳
造により製造し、鋳塊の圧延面を10mm面削して、試験鋳
塊とした。まず、表1の試験鋳塊No.A〜Dを450 ℃
の温度で24時間加熱処理したのち、520 ℃の温度に昇温
し、6 時間保持した。ついで、500 ℃で熱間圧延を開始
した。試験鋳塊の厚さは260mm であり、一回当たり20mm
の圧下量で合計14回圧延し、20mm厚のAl−Li合金板
を得た。熱間圧延は400 ℃の温度で終了した。幅方向圧
延は行わなかったが、発生した耳割れは10mm程度でAl
−Li合金板材として十分に使用できるものであった。
Hereinafter, examples of the present invention will be described in comparison with comparative examples. Example 1 An ingot of an Al-Li alloy having the composition shown in Table 1 was produced by continuous casting, and the rolled surface of the ingot was chamfered by 10 mm to obtain a test ingot. First, the test ingot No. A to D 450 ℃
After heating at 24 ° C for 24 hours, the temperature was raised to 520 ° C and held for 6 hours. Then, hot rolling was started at 500 ° C. The thickness of the test ingot is 260 mm, 20 mm per time
It was rolled a total of 14 times with a rolling amount of 10 to obtain a 20 mm thick Al-Li alloy plate. The hot rolling was completed at a temperature of 400 ° C. Although width-direction rolling was not performed, the edge crack that occurred was about 10 mm and
It was a material that could be sufficiently used as a Li alloy plate material.

【0022】[0022]

【表1】 [Table 1]

【0023】実施例2 実施例1において、奇数回目の圧延終了毎に7 回( 総圧
延回数の50%に相当する回数)、片側10mmの幅方向圧延
を行った。その結果、耳割れの発生は完全に防止され
た。
Example 2 In Example 1, each time an odd number of rollings were completed, rolling was performed 7 times (the number of times corresponding to 50% of the total number of rollings) in the width direction of 10 mm on one side. As a result, the occurrence of ear cracks was completely prevented.

【0024】比較例1 表2の試験鋳塊No.E(260mm 厚) を、450 ℃の温度
に10時間加熱したのち、540 ℃の温度に昇温して6 時間
保持し、ついで、420 ℃の温度で熱間圧延を開始した。
一回当たり圧下量15mmで圧延を行い、圧延一回毎に片側
15mmの幅方向圧延を行ったところ、圧延回数16回で板厚
20mmまで圧延されたが、圧延板の温度が230 ℃となり大
きな耳割れが生じた。
Comparative Example 1 Test ingot No. E (260 mm thick) was heated to a temperature of 450 ° C. for 10 hours, then heated to a temperature of 540 ° C. and held for 6 hours, and then hot rolling was started at a temperature of 420 ° C.
Rolling is performed with a rolling reduction of 15 mm each time, and one side is used for each rolling.
When 15 mm width direction rolling is performed, the plate thickness is 16 times.
Although it was rolled to 20 mm, the temperature of the rolled plate reached 230 ° C and large edge cracks occurred.

【0025】実施例3 比較例1において、熱間圧延開始温度を500 ℃とし、圧
延を380 ℃で終了したところ、耳割れは完全に防止され
た。
Example 3 In Comparative Example 1, when the hot rolling start temperature was 500 ° C. and rolling was completed at 380 ° C., edge cracking was completely prevented.

【0026】実施例4 表3の試験鋳塊No.F(260mm 厚) を、450 ℃の温度
で24時間加熱したのち、550 ℃の温度に昇温して10時間
保持し、ついで、550 ℃の温度で熱間圧延を開始した。
一回当たり圧下量を25mmとし、最初の圧延で片側15mmの
幅方向圧延を行い、10回の圧延と圧下量12mmの最終圧延
により、圧延終了温度450 ℃となり、板厚8mm の板材を
得た。板材には、板として全く使用できないレベルでは
ないが、かなりの耳割れが発生し、歩留りのわるいもの
となった。
Example 4 Test ingot No. 3 in Table 3 F (260 mm thick) was heated at a temperature of 450 ° C. for 24 hours, then heated to a temperature of 550 ° C. and held for 10 hours, and then hot rolling was started at a temperature of 550 ° C.
A rolling amount of 25 mm was set for each rolling, widthwise rolling was performed on one side for 15 mm in the first rolling, and by 10 rolling and final rolling with a rolling reduction of 12 mm, the rolling end temperature was 450 ° C and a plate material with a thickness of 8 mm was obtained. . The plate material was not at a level that could not be used as a plate at all, but considerable ear cracking occurred, resulting in poor yield.

【0027】実施例5 実施例4において、1回目、3回目および5回目の圧延
終了後に片側15mmの幅方向圧延を実施したところ、耳割
れは完全に防止された。
Example 5 In Example 4, when widthwise rolling of 15 mm on one side was carried out after completion of the first, third and fifth rolling, the edge crack was completely prevented.

【0028】比較例2 実施例4において、熱間圧延開始温度を420 ℃としたと
ころ、圧延終了温度は210 ℃となり、板表面全面に縞状
の模様が生じ、板製品として不合格であった。
Comparative Example 2 In Example 4, when the hot rolling start temperature was 420 ° C., the rolling finish temperature was 210 ° C., and striped patterns were formed on the entire surface of the plate, which was unacceptable as a plate product. .

【0029】実施例6 表1の試験鋳塊No.Fと同一組成の鋳塊を、圧延面お
よび側面をそれぞれ10mm面削し、実施例4と同一の工程
で処理したところ、圧延板には10mm程度の耳割れが発生
しただけであった。
Example 6 Test ingot No. 1 in Table 1 When the ingot having the same composition as F was ground by 10 mm on each of the rolled surface and the side surface and treated in the same process as in Example 4, only about 10 mm of ear cracks occurred on the rolled plate.

【0030】[0030]

【発明の効果】以上のとおり、本発明によれば、Al−
Li合金を熱間圧延する場合、耳割れ、圧延面割れなど
の割れ発生および縞模様などの表面欠陥の発生を防止す
ることができるAl−Li合金の熱間圧延方法が提供さ
れ、Al−Li合金の実用化に有用である。
As described above, according to the present invention, Al-
When hot-rolling a Li alloy, a hot-rolling method for an Al-Li alloy is provided, which can prevent the occurrence of cracks such as edge cracks and rolling surface cracks and the occurrence of surface defects such as striped patterns. It is useful for practical use of alloys.

【図面の簡単な説明】[Brief description of drawings]

【図1】Al−Li合金の加工温度と限界加工率の関係
を示すグラフである。
FIG. 1 is a graph showing the relationship between the processing temperature of an Al—Li alloy and the limit processing rate.

Claims (5)

【特許請求の範囲】[Claims] 【請求項1】 Al−Li合金を熱間圧延する方法にお
いて、Li0.5 〜3.0 %(wt%、以下同じ)を含有し、
さらにCu1.0 〜3.0 %(但し、Mgが含有されない場
合はCu1.5 〜5.5 %)、Mg0.5 〜2.0 %、Zr0.06
〜0.3 %、V0.06〜0.3 %、Mn0.06〜0.3 %、Cr0.
06〜0.3 %、Ti0.02〜0.3 %のうちの1種または2種
以上を含有し、残部がAlおよび不可避的不純物からな
るAl−Li合金の鋳塊を、520 ℃±50℃の温度範囲に
加熱して、1 〜24時間保持したのち、該温度範囲で熱間
圧延を開始し、250 ℃以上の温度で熱間圧延を終了する
ことを特徴とするAl−Li合金の熱間圧延方法。
1. A method of hot rolling an Al--Li alloy, which contains Li 0.5 to 3.0% (wt%, hereinafter the same),
Further, Cu1.0 to 3.0% (however, Cu1.5 to 5.5% when Mg is not contained), Mg0.5 to 2.0%, Zr0.06
~ 0.3%, V0.06-0.3%, Mn0.06-0.3%, Cr0.
An ingot of Al-Li alloy containing one or two or more of 06 to 0.3% and Ti 0.02 to 0.3%, and the balance of Al and unavoidable impurities in a temperature range of 520 ° C ± 50 ° C. After heating for 1 to 24 hours, hot rolling is started in the temperature range, and hot rolling is finished at a temperature of 250 ° C. or higher. .
【請求項2】 Al−Li合金を熱間圧延する方法にお
いて、Li0.5 〜3.0 %を含有し、さらにZr0.06〜0.
3 %、V0.06〜0.3 %、Mn0.06〜0.3 %、Cr0.06〜
0.3 %のうちの1種または2種以上を含有し、残部がA
lおよび不可避的不純物からなるAl−Li合金の鋳塊
を、450 ℃±30℃の温度範囲に1 〜30時間加熱したの
ち、520 ℃±50℃の温度範囲に加熱して、1 〜24時間保
持し、ついで該温度範囲で熱間圧延を開始し、250 ℃以
下の温度で熱間圧延を終了することを特徴とするAl−
Li合金の熱間圧延方法。
2. A method of hot rolling an Al--Li alloy, which contains Li 0.5 to 3.0% and further Zr 0.06 to 0.
3%, V0.06-0.3%, Mn0.06-0.3%, Cr0.06-
It contains one or more of 0.3% and the balance is A
The ingot of Al-Li alloy consisting of 1 and unavoidable impurities is heated to a temperature range of 450 ° C ± 30 ° C for 1 to 30 hours and then to a temperature range of 520 ° C ± 50 ° C for 1 to 24 hours. Al-characterized in that it is held, and then hot rolling is started in the temperature range, and hot rolling is finished at a temperature of 250 ° C or lower.
Method for hot rolling Li alloy.
【請求項3】 Al−Li合金を熱間圧延する方法にお
いて、熱間圧延における1回の圧下量を、最終圧延を除
いて3 〜30mmとすることを特徴とする請求項1〜2記載
のAl−Li合金の熱間圧延方法。
3. The method of hot rolling an Al--Li alloy according to claim 1, wherein the reduction amount per hot rolling is 3 to 30 mm except for the final rolling. Hot rolling method of Al-Li alloy.
【請求項4】 Al−Li合金を熱間圧延する方法にお
いて、総圧延回数のうちの20%以上の回数の圧延段階
で、圧延板側面部にそれぞれ片側5 〜50mmの幅方向圧延
を行うことを特徴とする請求項1〜3記載のAl−Li
合金の熱間圧延方法。
4. A method for hot rolling an Al-Li alloy, wherein widthwise rolling of 5 to 50 mm on each side is performed on each side surface of a rolled plate at a rolling stage of 20% or more of the total rolling times. The Al-Li according to claim 1, wherein
Hot rolling method for alloys.
【請求項5】 Al−Li合金を熱間圧延する方法にお
いて、Al−Li合金の鋳塊の圧延面および側面が5mm
以上切削され、粗度Ra が2 μm 以下、うねりが200 μ
m 以下に仕上げられていることを特徴とする請求項1〜
4記載のAl−Li合金の熱間圧延方法。
5. A method of hot rolling an Al—Li alloy, wherein the rolling surface and the side surface of the ingot of the Al—Li alloy are 5 mm.
After cutting, roughness Ra is less than 2 μm and waviness is 200 μ
It is finished to m or less.
4. The hot rolling method of the Al-Li alloy according to 4.
JP04125995A 1995-02-06 1995-02-06 Hot rolling method of Al-Li alloy Expired - Lifetime JP3197774B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP04125995A JP3197774B2 (en) 1995-02-06 1995-02-06 Hot rolling method of Al-Li alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP04125995A JP3197774B2 (en) 1995-02-06 1995-02-06 Hot rolling method of Al-Li alloy

Publications (2)

Publication Number Publication Date
JPH08206706A true JPH08206706A (en) 1996-08-13
JP3197774B2 JP3197774B2 (en) 2001-08-13

Family

ID=12603454

Family Applications (1)

Application Number Title Priority Date Filing Date
JP04125995A Expired - Lifetime JP3197774B2 (en) 1995-02-06 1995-02-06 Hot rolling method of Al-Li alloy

Country Status (1)

Country Link
JP (1) JP3197774B2 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2009007626A (en) * 2007-06-28 2009-01-15 Ulvac Material Kk Method for producing aluminum-lithium alloy target, and aluminum-lithium alloy target
CN115418534A (en) * 2022-09-19 2022-12-02 郑州轻研合金科技有限公司 8090 aluminum lithium alloy fine-grain plate and preparation method thereof

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2009007626A (en) * 2007-06-28 2009-01-15 Ulvac Material Kk Method for producing aluminum-lithium alloy target, and aluminum-lithium alloy target
CN115418534A (en) * 2022-09-19 2022-12-02 郑州轻研合金科技有限公司 8090 aluminum lithium alloy fine-grain plate and preparation method thereof

Also Published As

Publication number Publication date
JP3197774B2 (en) 2001-08-13

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