JPH0368098B2 - - Google Patents
Info
- Publication number
- JPH0368098B2 JPH0368098B2 JP59195516A JP19551684A JPH0368098B2 JP H0368098 B2 JPH0368098 B2 JP H0368098B2 JP 59195516 A JP59195516 A JP 59195516A JP 19551684 A JP19551684 A JP 19551684A JP H0368098 B2 JPH0368098 B2 JP H0368098B2
- Authority
- JP
- Japan
- Prior art keywords
- alloy
- hot
- strength
- alloys
- hot rolling
- 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 - Lifetime
Links
Landscapes
- Powder Metallurgy (AREA)
- Metal Rolling (AREA)
Description
産業上の利用分野
この発明は熱間圧延のままで各種大型溶接構造
材などに使用されるAl−Mg合金熱延上り板、特
に高強度化のためにMg量を5.7%以上と高Mg化
したAl−Mg合金熱延上り板に関するものであ
る。
なお本明細書において熱延上り板とは、熱間圧
延機仕上げで冷間圧延機を通板しない板を意味す
る。
従来技術
従来の代表的Al−Mg合金である5083合金は、
非熱処理型高強度材であることから、近年の溶接
技術の進歩に伴なつてLNG(液化天然ガス)の陸
上貯蔵タンクや、タンカー用タンクなどの大型溶
接構造物、あるいはタンクローリーなどの大型成
形溶接構造物などに広く用いられるようになつて
いるが、材料使用量低減によるコストダウンを目
的として、この種の合金の強度をさらに向上させ
て薄肉化を図ることが強く望まれている。さらに
この種のAl−Mg合金には、実験用核融合炉の真
空チヤンバー材およびその他の付帯設備用として
導電率の低い高強度の構造用材への適用も期待さ
れており、そのためには一層の高強度化が望まれ
る。また一方、プラスチツク成形用の金型として
は従来は一般に熱処理合金が使用されていたが、
熱処理合金は一般に内部応力が高く、切削加工後
の寸法精度の面で問題となることが多かつた。そ
こで内部応力の低い非熱処理型合金であるAl−
Mg合金の高強度化を図ることにより、この種の
プラスチツク成形用金型の用途に対するAl−Mg
基合金の需要も期待される。
ところで5083合金は、JIS規格によればMg4.0
〜4.9%、Mn0.30〜1.0%、Cr0.05〜0.25%を含有
し、残部がAlおよび不可避的不純物よりなるも
のであつて、その他不純物成分としてCu0.10%以
下、Si0.40%以下、Fe0.40%以下、Zn0.25%以
下、Ti0.15%以下が許容されている。
このような5083合金を強度に寄与している合金
元素は主としてMg、Mn、Crであり、これらの
うちでも特にMgの含有量が多いことから、Mg
の強度に対する寄与が最も高い。そこでAl−Mg
合金の強度を従来の5083合金よりも高めるために
は、Mg添加量を5083合金の場合よりも増量して
5%以上とすることが考えられ、実際Mgの増量
により高強度化が図れることが確認されている
が、その反面Mgを増量すれば次に詳細に述べる
ように熱間圧延性が著しく損われる問題が生じ
る。したがつて従来はAl−Mg基合金における
Mg量は5083合金で規定されているように4.9%以
下が通常であつた。
発明が解決すべき問題点
前述にようにAl−Mg合金においてMgを増量
することは強度向上に有効であるが、その反面、
Mgを増量すればMgの固溶体硬化機構によつて
熱間変形抵抗が高くなり、熱間圧延性が著しく損
われる。またMgの含有量が6%前後を越えて高
くなれば、β相(Al3Mg)のような低融点共晶
が結晶粒界に介在して熱間変形での粒界割れを助
長し、熱延圧延に際してエツジ割れ(端部亀裂)
やアリゲーター割れ(ワニ口亀裂)が生じ易くな
る。特にこの系の合金では、NaやCaが微量でも
存在すれば、熱間圧延中の脆性割れ感受性が著し
く高められる。
このようにAl−Mg合金のMg量を、従来の代
表的な5083合金のMg量(4.0〜4.9%)よりも増
量することは、強度向上には有効であるが、熱間
圧延性を著しく劣化させることから、5%以上の
Mgを含有するAl−Mg基合金板を製造すること
は、実験室的規模ではともかく、工業的規模では
困難とされていたのが実情である。
Al−Mg合金の熱間圧延性を改善するための方
法としては、前述のCa、Naなどの微量有害不純
物を最低限に抑えること、および粒界への合金成
分の偏析や低融点共晶の介在を、充分な均熱処理
により除去することが必要と考えられるが、前者
の方法ではそれだけでは多量のMgを含有するAl
−Mg合金の熱間圧延性を著しく改善することは
困難であり、一方後者の方法においても実生産規
模で低融点共晶の介在を充分に除去するまで均熱
することは困難であつて特にMgを5〜6%以上
の高濃度に含有する系では均熱処理のみによつて
熱間圧延性を改善することは困難であつた。
この発明は以上の事情を背景としてなされたも
のであつて、強度を向上させるべく5.7%以上の
Mgを添加した高Mg系のAl−Mg合金において熱
間圧延性を充分に改善したAl−Mg基合金の熱延
上り板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
本発明者等は、高Mg系Al−Mg合金における
熱間圧延性の向上策として、次のような手段を検
討した。すなわち熱間変形における破壊は主とし
て粒界破壊であることから、粒界への変形ひずみ
の集中を緩和することを検討した。このように
Al−Mg合金の熱間変形において粒界への変形ひ
ずみの集中を緩和するための具体的方策を見出す
べく研究を重ねた結果、Feを積極的に添加する
ことにより第二相化合物としてのAl−Fe共晶化
合物を分散させ、さらにはその共晶化合物をMn
の共存下において高温で安定なAl−Fe−Mn系化
合物として、それらの分散化合物相に変形のひず
みを分担させ、同時にTiもしくはTiおよびBを
添加して結晶粒を微細化させることによつて、粒
界への変形ひずみの集中を実際に緩和させ、高
Mg系のAl−Mg合金でも熱間圧延性を著しく向
上させ得ることを見出し、この発明をなすに至つ
たのである。
具体的には、第1発明のAl−Mg合金熱延上り
板は、Mg5.7〜9%、Mn0.05〜1.0%、Cr0.05〜
0.3%、Ti0.005〜0.2%、Fe0.25〜1.00%を含有
し、残部がAlおよび不可避的不純物よりなるこ
とを特徴とするものである。
また第2発明のAl−Mg合金熱延上り板は、上
記各成分のほか、さらにCuを0.05〜0.3%含有す
るものである。
作 用
Mg量を5.7〜9%とした高Mg系のAl−Mg合
金において、Feを添加することにより第二相化
合物としてAl−Fe系共晶化合物が分散晶出され
る。この共晶化合物は、凝固過程で粒界近傍に分
散晶出されるため、熱間での変形のひずみが粒界
からこれらの分散晶出化合物にも分担されること
になる。そしてまた凝固過程で一旦晶出したAl
−Fe系共晶化合物は、Mnの共存によつて鋳造以
降の各種熱履歴過程で高温で安定なAl−Fe−Mn
系化合物となり、そのAl−Fe−Mn系化合物は熱
間圧延工程でさらに均一に破壊・分散化され、そ
の結果熱間での変形ひずみを均一に分散させて、
熱間圧延性を向上させる役割を果たす。
またTiを添加(必要に応じてTiおよびBの複
合添加)することによつて結晶粒が微細化され
る。このように結晶粒が微細化されることによつ
て、粒界へ偏析した合金元素が均熱処理により拡
散均一化され易くなるとともに前述のβ相の如き
低融点共晶の微細化、分散化が達成され、かつま
た個々の粒界へのひずみ変形の集中の度合も減じ
られ、これらが総合的に作用して熱間圧延性を向
上させることができる。
このようにして、Feの添加による第二相化合
物の晶出と、Tiの添加(必要に応じてTi+Bの
複合添加)による結晶粒微細化とが相俟つて、高
Mg系のAl−Mg合金でも熱間圧延性を充分に向
上させることが可能となる。
成分限定理由
次にこの発明における各成分の限定理由につい
て説明する。
Mg:
Mgは非熱処理型Al合金において高強度化のた
めに有効な元素であるが、5.7%未満の量ではこ
の発明で目的とする程度の高強度が達成されず、
また5.7%未満のMg量では熱間圧延性もさほど問
題とはならない。一方9%を越えてMgを増量し
ても強度向上への寄与は少なくなり、経済的でな
くならから、5.7〜9%の範囲に限定した。なお
この範囲内でも特に高強度を得るためには、Mg
を6%以上、さらには7%以上とすることが望ま
しい。
Mn,Cr:
これらの元素は強度、特に耐力の確保のおよび
耐応力腐食割れの低減に有効であるが、それぞれ
0.05%未満ではこれらの効果が得られない。一方
Mnが1.0%、Crが0.3%を越えれば金属間化合物
が多くなり、時には巨大金属間化合物が晶出して
健全な鋳塊が得られず、圧延材の品質の均一性を
損うおそれがあるから、Mnは0.05〜1.0%、Crは
0.05〜0.3%の範囲内に限定した。
Ti:
Tiは結晶粒の微細化に効果がある元素であり、
その結晶粒微細化を通じて熱間圧延性を向上させ
る役割を果すが、0.005%未満では結晶粒微細化
の効果が認められず、一方0.2%を越えれば靭性
を劣化させるから、Tiの添加量は0.005〜0.2%の
範囲内に限定した。なおTiはBと複合添加する
ことによりTi単独添加の場合よりも一層顕著な
結晶粒微細化効果を発揮するから、必要に応じて
Tiに併せてBを添加しても良い。但しBが0.001
%未満ではその効果が少なく、一方0.1%を越え
れば靭性が劣化するから、BをTiと複合添加す
る場合のB量は0.001〜0.1%の範囲内とすること
が好ましい。
Fe:
Feは前述のように鋳造段階でAl−Fe系共晶化
合物を晶出させる。このAl−Fe系共晶化合物は
さらにMnの共存により鋳造以降の各種熱履歴過
程において高温で安定なAl−Fe−Mn系化合物と
なり、熱間圧延工程で均一に破壊、分散化され、、
熱間変形での変形ひずみの分散化を促進して熱間
圧延性を向上させる役割を果たす。Feが0.25%未
満ではMgを5.7%以上の高濃度に含有するAl−
Mg合金の熱間圧延性を充分に向上させることは
困難であり、一方Feが1.00%を越えれば化合物の
分布数が多過ぎて合金素材の延性、靭性を劣化さ
せるおそれがある。したがつてFeは0.25〜1.00%
の範囲内とした。
以上の各成分元素のほか、本願の第2発明では
Cuを0.05〜0.30%を含有することとする。すなわ
ち、Cuは耐応力腐食割れ性の改善に効果がある
が、0.05%未満ではその効果が認められず、一方
0.30%を越えれば、Mgを高濃度に含有するAl−
Mg合金では熱間圧延性を損うおそれがあるか
ら、第2発明におけるCu含有量は0.05〜0.30%と
した。
さらにこの発明の合金においては、不可避的不
純物としてSiが、またその他の不純物としてZn
が含まれることがあり、これらは次のような範囲
内で許容される。
すなわち、Znは0.50%まで許容される。Znが
0.50%を越えれば特に溶接熱影響部の耐食性に問
題が生じる。さらにSiは0.40%まで許容される。
Siが0.40%を越えれば、Al−Mg−Si系の共晶化
合物が増加し、これらは大入熱の溶接において溶
融して熱影響部の粒界のミクロ割れを招き易い。
なおこの発明の合金は易酸化性のMgを高濃度
に含む合金であるから、合金の溶製・鋳造時にお
ける溶湯の酸化を防止するため、Beを0.0001〜
0.002%程度添加することが好ましい。
実施例
第1表のNo.1〜No.12に示される組成の合金を、
Be1〜2ppmを添加して溶製し、金型により厚さ
40mm、幅110mm、高さ150mmのインゴツトに鋳造し
た。次いでそのインゴツトに対し460℃、30時間
以上の均熱処理を施した後、厚さおよび幅方向の
両面を1mmずつ面削して厚さ38mm、幅108mm、高
さ150mmとした。その面削後のインゴツトを460℃
にて1時間加熱後、実験用圧延機にて1パスの圧
下量を2mmとして圧延460℃炉中再装填を繰返し
て38mm厚から5mm厚まで熱間圧延した。そして熱
間圧延中のワニ口割れの有無の観察および5mm厚
圧延上りの状態でのエツジ部の割れ発生状況のラ
ンク付けによつて熱間圧延性を評価した。また熱
間圧延機の各板に対し350℃×50時間の仕上焼鈍
を行つて0材とした後、引張試験を行つて機械的
特性を調べた。それらの結果を第2表に示す。な
お第2表において熱間圧延性の評価についてのエ
ツジ割れ発生状況のランクA、B、Cは次のよう
に区分した。すなわちAはエツジ割れの発生が従
来の5083合金なみの微小割れにとどまつた場合、
Bはエツジ割れが従来の5083合金なみの程度を越
えて10mm以下の場合、Cは10mm以上のエツジ割れ
が発生した場合を示す。
第2表から明らかなようにこの発明の組成範囲
内の合金(No.1〜No.5)いずれも従来の5083合金
と同等の良好な熱間圧延性を示し、また強度面も
特にMg含有量を7%以上としたNo.1、3〜5の
合金では引張強さが37Kg/mm3以上、耐力が17Kg/
mm3以上と高強度、高耐力を示すことが確認され
た。これに対しFe含有量が本願発明範囲よりも
少ない比較合金No.9、10、12とTi無添加の比較
合金No.11においてはいずれも熱間圧延性が劣つて
おり、またCrもしくはMnの含有量が本発明範囲
より少ない比較合金No.7、8においては耐力が劣
ることが判明した。
Industrial Application Field This invention is an Al-Mg alloy hot-rolled sheet that is used as hot-rolled for various large welded structural materials, etc., and in particular, the Mg content is increased to 5.7% or more to increase the strength. This relates to a hot-rolled Al-Mg alloy sheet. Note that in this specification, a hot-rolled plate means a plate that has been finished by a hot rolling mill and is not passed through a cold rolling mill. Prior art The 5083 alloy, which is a typical conventional Al-Mg alloy, is
As it is a non-heat-treated high-strength material, with recent advances in welding technology, it has become suitable for large welded structures such as onshore LNG (liquefied natural gas) storage tanks, tanker tanks, and large forming welds such as tank trucks. Although they are now widely used in structures, there is a strong desire to further improve the strength of this type of alloy and reduce its thickness in order to reduce costs by reducing the amount of material used. Furthermore, this type of Al-Mg alloy is expected to be applied to high-strength structural materials with low electrical conductivity, such as vacuum chamber materials for experimental fusion reactors and other auxiliary equipment, and for this purpose, further efforts are needed. High strength is desired. On the other hand, heat-treated alloys have traditionally been used as molds for plastic molding, but
Heat-treated alloys generally have high internal stress, which often causes problems in terms of dimensional accuracy after cutting. Therefore, Al-, which is a non-heat-treatable alloy with low internal stress,
By increasing the strength of the Mg alloy, Al-Mg is suitable for use in this type of plastic molding mold.
Demand for base alloys is also expected. By the way, 5083 alloy is Mg4.0 according to the JIS standard.
~4.9%, Mn0.30~1.0%, Cr0.05~0.25%, with the balance consisting of Al and inevitable impurities, and other impurity components include Cu0.10% or less and Si0.40% or less. , Fe 0.40% or less, Zn 0.25% or less, and Ti 0.15% or less are allowed. The alloying elements that contribute to the strength of 5083 alloy are mainly Mg, Mn, and Cr. Among these, Mg has a particularly high content, so Mg
has the highest contribution to the strength. Therefore, Al−Mg
In order to increase the strength of the alloy compared to the conventional 5083 alloy, it is possible to increase the amount of Mg added to 5% or more compared to the case of 5083 alloy, and it is actually possible to increase the strength by increasing the amount of Mg. However, on the other hand, if the amount of Mg is increased, a problem arises in that hot rollability is significantly impaired, as will be described in detail below. Therefore, in the past, Al-Mg based alloys
The amount of Mg was normally 4.9% or less as specified in the 5083 alloy. Problems to be solved by the invention As mentioned above, increasing the amount of Mg in Al-Mg alloys is effective in improving strength, but on the other hand,
If the amount of Mg is increased, hot deformation resistance will increase due to the solid solution hardening mechanism of Mg, and hot rollability will be significantly impaired. Furthermore, if the Mg content increases beyond around 6%, low melting point eutectics such as β phase (Al 3 Mg) will be present at grain boundaries, promoting intergranular cracking during hot deformation. Edge cracking (edge cracks) during hot rolling
Alligator cracks (crocodile cracks) are more likely to occur. In particular, in this type of alloy, the presence of even a trace amount of Na or Ca significantly increases the susceptibility to brittle cracking during hot rolling. Increasing the amount of Mg in the Al-Mg alloy compared to the amount of Mg in the conventional typical 5083 alloy (4.0 to 4.9%) is effective in improving strength, but it significantly impairs hot rollability. 5% or more due to deterioration.
The reality is that it has been difficult to produce Al-Mg-based alloy plates containing Mg on an industrial scale, even on a laboratory scale. Methods to improve the hot rolling properties of Al-Mg alloys include minimizing trace amounts of harmful impurities such as Ca and Na, as well as segregation of alloy components at grain boundaries and low melting point eutectic impurities. It is thought that it is necessary to remove the inclusions by sufficient soaking treatment, but with the former method alone, Al containing a large amount of Mg
- It is difficult to significantly improve the hot rolling properties of Mg alloys, and on the other hand, even in the latter method, it is difficult to soak to the point where low melting point eutectic inclusions are sufficiently removed on a commercial scale. In systems containing Mg at a high concentration of 5 to 6% or more, it is difficult to improve hot rolling properties by soaking alone. This invention was made against the background of the above-mentioned circumstances, and in order to improve the strength, 5.7% or more
The object of the present invention is to provide a hot-rolled sheet of an Al-Mg-based alloy that has sufficiently improved hot rolling properties in a high-Mg-based Al-Mg alloy to which Mg has been added. Means for Solving the Problems The present inventors have investigated the following means as a measure to improve the hot rolling properties of high Mg Al-Mg alloys. In other words, since fractures during hot deformation are mainly grain boundary fractures, we investigated ways to alleviate the concentration of deformation strain at grain boundaries. in this way
As a result of repeated research to find specific measures to alleviate the concentration of deformation strain at grain boundaries during hot deformation of Al-Mg alloys, we found that by actively adding Fe, Al as a second phase compound −Dispersing the Fe eutectic compound and further dispersing the eutectic compound with Mn
As an Al-Fe-Mn-based compound that is stable at high temperatures in the coexistence of , actually alleviates the concentration of deformation strain on the grain boundaries, resulting in high
It was discovered that even Mg-based Al-Mg alloys can significantly improve hot rolling properties, leading to the present invention. Specifically, the Al-Mg alloy hot-rolled sheet of the first invention contains 5.7 to 9% Mg, 0.05 to 1.0% Mn, and 0.05 to Cr.
0.3%, Ti 0.005-0.2%, Fe 0.25-1.00%, and the remainder consists of Al and inevitable impurities. Moreover, the Al-Mg alloy hot-rolled sheet of the second invention further contains 0.05 to 0.3% of Cu in addition to the above-mentioned components. Effect In a high Mg Al-Mg alloy with an Mg content of 5.7 to 9%, by adding Fe, an Al-Fe eutectic compound is dispersed and crystallized as a second phase compound. Since this eutectic compound is dispersed and crystallized near the grain boundaries during the solidification process, the strain of hot deformation is also shared from the grain boundaries to these dispersed and crystallized compounds. Also, Al crystallized during the solidification process.
- Fe-based eutectic compounds are Al-Fe-Mn that is stable at high temperatures during various thermal history processes after casting due to the coexistence of Mn.
The Al-Fe-Mn-based compound is further uniformly broken and dispersed during the hot rolling process, and as a result, the hot deformation strain is evenly distributed,
It plays a role in improving hot rolling properties. Further, by adding Ti (combined addition of Ti and B if necessary), crystal grains are made finer. By refining the crystal grains in this way, the alloying elements segregated to the grain boundaries can be easily diffused and homogenized by soaking treatment, and the low melting point eutectic such as the β phase described above can be refined and dispersed. This is achieved, and the degree of concentration of strain deformation on individual grain boundaries is also reduced, which together act to improve hot rollability. In this way, the crystallization of the second phase compound due to the addition of Fe and the grain refinement due to the addition of Ti (combined addition of Ti + B as necessary) combine to achieve high
Even Mg-based Al-Mg alloys can sufficiently improve hot rolling properties. Reasons for Limiting Components Next, the reasons for limiting each component in this invention will be explained. Mg: Mg is an effective element for increasing the strength of non-heat-treated Al alloys, but if the amount is less than 5.7%, the high strength targeted by this invention cannot be achieved.
Furthermore, when the Mg content is less than 5.7%, hot rolling properties do not pose much of a problem. On the other hand, even if Mg is increased beyond 9%, the contribution to strength improvement will be small and it will be uneconomical, so it is limited to a range of 5.7 to 9%. In order to obtain particularly high strength within this range, Mg
It is desirable that the amount is 6% or more, more preferably 7% or more. Mn, Cr: These elements are effective in ensuring strength, especially proof stress, and reducing stress corrosion cracking, but each
These effects cannot be obtained at less than 0.05%. on the other hand
If Mn exceeds 1.0% and Cr exceeds 0.3%, intermetallic compounds will increase, and sometimes large intermetallic compounds will crystallize, making it impossible to obtain a healthy ingot and potentially impairing the uniformity of the quality of the rolled material. From, Mn is 0.05-1.0%, Cr is
It was limited to within the range of 0.05-0.3%. Ti: Ti is an element that is effective in refining crystal grains.
Ti plays a role in improving hot rollability through grain refinement, but if it is less than 0.005%, the effect of grain refinement is not recognized, while if it exceeds 0.2%, the toughness will deteriorate, so the amount of Ti added is It was limited to within the range of 0.005-0.2%. Note that when Ti is added in combination with B, it exhibits a more pronounced crystal grain refining effect than when Ti is added alone, so it can be added as necessary.
B may be added together with Ti. However, B is 0.001
If it is less than 0.1%, the effect will be small, whereas if it exceeds 0.1%, the toughness will deteriorate. Therefore, when B is added in combination with Ti, it is preferable that the amount of B is within the range of 0.001 to 0.1%. Fe: As mentioned above, Fe crystallizes an Al-Fe-based eutectic compound during the casting stage. Due to the coexistence of Mn, this Al-Fe-based eutectic compound becomes an Al-Fe-Mn-based compound that is stable at high temperatures during various thermal history processes after casting, and is uniformly broken and dispersed during the hot rolling process.
It plays a role in promoting the dispersion of deformation strain during hot deformation and improving hot rollability. When Fe is less than 0.25%, Al− containing Mg at a high concentration of 5.7% or more
It is difficult to sufficiently improve the hot rolling properties of Mg alloys, and on the other hand, if Fe exceeds 1.00%, the number of compounds distributed is too large, which may deteriorate the ductility and toughness of the alloy material. Therefore, Fe is 0.25-1.00%
was within the range of In addition to the above-mentioned component elements, in the second invention of the present application,
It is assumed that Cu is contained in an amount of 0.05 to 0.30%. In other words, Cu is effective in improving stress corrosion cracking resistance, but this effect is not observed at less than 0.05%;
If it exceeds 0.30%, Al− containing a high concentration of Mg
Since there is a risk of impairing hot rolling properties in Mg alloys, the Cu content in the second invention was set to 0.05 to 0.30%. Furthermore, in the alloy of this invention, Si is an unavoidable impurity, and Zn is another impurity.
may be included, and these are permissible within the following ranges: That is, Zn is allowed up to 0.50%. Zn
If it exceeds 0.50%, problems will arise especially in the corrosion resistance of the weld heat affected zone. Furthermore, Si is allowed up to 0.40%.
If Si exceeds 0.40%, Al-Mg-Si-based eutectic compounds increase, and these tend to melt during welding with large heat input, leading to micro-cracks at grain boundaries in the heat-affected zone. The alloy of this invention is an alloy containing a high concentration of Mg, which is easily oxidized. Therefore, in order to prevent oxidation of the molten metal during melting and casting of the alloy, the Be content is set at 0.0001 to 0.0001.
It is preferable to add about 0.002%. Example Alloys with the compositions shown in No. 1 to No. 12 in Table 1 were
Add 1 to 2 ppm of Be and melt it, and the thickness is determined by the mold.
It was cast into an ingot measuring 40 mm, width 110 mm, and height 150 mm. The ingot was then subjected to soaking treatment at 460° C. for 30 hours or more, and then faceted by 1 mm on both sides in the thickness and width directions to a thickness of 38 mm, width of 108 mm, and height of 150 mm. The ingot after face cutting is heated to 460℃.
After heating for 1 hour in an experimental rolling mill, the roll was rolled at 460° C. and reloaded in a furnace at a rolling reduction of 2 mm per pass, and hot rolled from 38 mm to 5 mm thick. Then, hot rolling properties were evaluated by observing the presence or absence of alligator cracks during hot rolling and ranking the occurrence of cracking at the edge after rolling to a thickness of 5 mm. Further, each plate of the hot rolling mill was subjected to finish annealing at 350°C for 50 hours to obtain a zero material, and then a tensile test was conducted to examine the mechanical properties. The results are shown in Table 2. In addition, in Table 2, ranks A, B, and C of the occurrence of edge cracking regarding the evaluation of hot rollability were classified as follows. In other words, A is when the occurrence of edge cracks remains as small as the conventional 5083 alloy.
B indicates a case where edge cracking exceeds that of conventional 5083 alloy and is 10 mm or less, and C indicates a case where edge cracking of 10 mm or more occurs. As is clear from Table 2, all of the alloys within the composition range of this invention (No. 1 to No. 5) exhibited good hot rollability equivalent to that of the conventional 5083 alloy, and their strength was also improved, especially since they contained Mg. Alloys No. 1, 3 to 5 with a content of 7% or more have a tensile strength of 37Kg/mm3 or more and a yield strength of 17Kg/mm3.
It was confirmed that it exhibits high strength and yield strength with a value of mm 3 or more. On the other hand, comparative alloys Nos. 9, 10, and 12 with Fe contents lower than the range of the present invention, and comparative alloy No. 11 without Ti addition, all have poor hot rollability, and also have Cr or Mn. It was found that Comparative Alloys No. 7 and 8, in which the content was lower than the range of the present invention, had poor yield strength.
【表】【table】
【表】
発明の効果
以上の説明で明らかなようにこの発明のAl−
Mg合金熱延上り板においては、強度を向上させ
るべく従来の5083合金よりもMg量を増量したも
のであるにもかかわらず、熱間圧延性は従来の
5083合金と同等以上に優れており、熱間圧延に支
障を来たすことなく安定して割れ等のない板材と
することができる。したがつて非熱処理型高強度
Al合金熱延上り板として、従来よりも一層強度
を高めたAl−Mg合金材を実生産的規模で製造す
ることが可能となり、Al−Mg合金を用いた大型
溶接構造物の薄肉化を通じてそれらの構造物のコ
スト低減を達成することができるとともに従来熱
処理型合金を用いていた分野への適用によつて熱
処理コストの低減を図り得る等各種の利益をもた
らすことができる。[Table] Effects of the invention As is clear from the above explanation, the Al-
Although the Mg alloy hot-rolled sheet has an increased amount of Mg compared to the conventional 5083 alloy to improve strength, its hot rolling properties are lower than that of the conventional 5083 alloy.
It is as good as or better than 5083 alloy, and can be stably made into crack-free plates without hindrance to hot rolling. Therefore, non-heat treated high strength
It has become possible to manufacture Al-Mg alloy materials with even higher strength than conventional sheets on a commercial scale as Al alloy hot-rolled sheets, and by thinning large welded structures using Al-Mg alloys, It is possible to reduce the cost of the structure, and by applying it to fields where heat treatable alloys have been used in the past, it is possible to bring about various benefits such as being able to reduce heat treatment costs.
Claims (1)
%、Ti0.005〜0.2%、Fe0.25〜1.00%を含有し、
残部がAlおよび不可避的不純物よりなることを
特徴とする熱間圧延性の優れた高耐力アルミニウ
ム−マグネシウム合金熱延上り板。 2 Mg5.7〜9%、Mn0.05〜1.0%、Cr0.05〜0.3
%、Ti0.005〜0.2%、Fe0.25〜1.00%、Cu0.05〜
0.3%を含有し、残部がAlおよび不可避的不純物
よりなることを特徴とする熱間圧延性の優れた高
耐力アルミニウム−マグネシウム合金熱延上り
板。[Claims] 1 Mg5.7-9%, Mn0.05-1.0%, Cr0.05-0.3
%, Ti0.005~0.2%, Fe0.25~1.00%,
A hot-rolled aluminum-magnesium alloy hot-rolled sheet with excellent hot rollability, characterized in that the remainder consists of Al and unavoidable impurities. 2 Mg5.7~9%, Mn0.05~1.0%, Cr0.05~0.3
%, Ti0.005~0.2%, Fe0.25~1.00%, Cu0.05~
A hot-rolled aluminum-magnesium alloy hot-rolled sheet with excellent hot rollability, characterized in that the aluminum-magnesium alloy contains 0.3% and the remainder consists of Al and unavoidable impurities.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19551684A JPS6173856A (en) | 1984-09-18 | 1984-09-18 | Aluminum-magnesium alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19551684A JPS6173856A (en) | 1984-09-18 | 1984-09-18 | Aluminum-magnesium alloy |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6173856A JPS6173856A (en) | 1986-04-16 |
| JPH0368098B2 true JPH0368098B2 (en) | 1991-10-25 |
Family
ID=16342379
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP19551684A Granted JPS6173856A (en) | 1984-09-18 | 1984-09-18 | Aluminum-magnesium alloy |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6173856A (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2837499B1 (en) * | 2002-03-22 | 2004-05-21 | Pechiney Rhenalu | AL-Mg ALLOY PRODUCTS FOR WELDED CONSTRUCTION |
| JP2006316303A (en) * | 2005-05-11 | 2006-11-24 | Furukawa Sky Kk | Aluminum alloy extruded material for high temperature forming and high temperature formed product |
-
1984
- 1984-09-18 JP JP19551684A patent/JPS6173856A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6173856A (en) | 1986-04-16 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN100475999C (en) | Weldable high strength AI-Mg-Si alloy | |
| KR102841879B1 (en) | Method of manufacturing an al-mg-mn alloy plate product having an improved corrosion resistance | |
| JP6719219B2 (en) | High strength aluminum alloy sheet excellent in formability and method for producing the same | |
| CN106574328B (en) | Aluminum alloy plate | |
| JPH0380862B2 (en) | ||
| US4113472A (en) | High strength aluminum extrusion alloy | |
| CN117165821B (en) | Aluminum alloy plate for hydrogen storage bottle of hydrogen energy automobile and processing method thereof | |
| JP5379463B2 (en) | Method for producing high-strength aluminum alloy for LNG spherical tank | |
| EP4488393A1 (en) | High-ni alloy thick steel sheet having excellent weld high-temperature cracking resistance, and method for producing same | |
| JPS6150141B2 (en) | ||
| JP2001032031A (en) | Aluminum alloy sheet for structural material, excellent in stress corrosion cracking resistance | |
| JPH10121170A (en) | Ni-Cr based alloy excellent in corrosion resistance and method for producing the same | |
| JP2004027253A (en) | Aluminum alloy sheet for forming and method of manufacturing the same | |
| JP4452630B2 (en) | Manufacturing method of aluminum alloy hot-rolled sheet for welded structure | |
| JP2021095619A (en) | Aluminum alloy sheet for cap material and method for producing the same | |
| JPH0368098B2 (en) | ||
| JPS63270446A (en) | Production of al-mg base alloy thick plate for welded structure | |
| JPS6410584B2 (en) | ||
| JPS5919987B2 (en) | Manufacturing method of Al-Mg alloy | |
| JP2858069B2 (en) | Stress corrosion cracking resistant high strength aluminum alloy sheet and method for producing the same | |
| CN117535570B (en) | An aluminum-magnesium alloy sheet with both high formability and high weldability and its preparation method | |
| JPS6296643A (en) | superplastic aluminum alloy | |
| JPH0613748B2 (en) | Method for producing stress corrosion resistant aluminum-magnesium alloy soft material | |
| JP2698888B2 (en) | Manufacturing method of aluminum alloy sheet with excellent stress corrosion cracking resistance | |
| JPH08302440A (en) | Aluminum alloy sheet with high strength |