JPS6289838A - High strength aluminum alloy excellent in rolling workability - Google Patents

High strength aluminum alloy excellent in rolling workability

Info

Publication number
JPS6289838A
JPS6289838A JP18547285A JP18547285A JPS6289838A JP S6289838 A JPS6289838 A JP S6289838A JP 18547285 A JP18547285 A JP 18547285A JP 18547285 A JP18547285 A JP 18547285A JP S6289838 A JPS6289838 A JP S6289838A
Authority
JP
Japan
Prior art keywords
alloy
strength
high strength
rolling workability
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.)
Pending
Application number
JP18547285A
Other languages
Japanese (ja)
Inventor
Kenji Azuma
健司 東
Chuichi Onishi
大西 忠一
Ichizo Tsukuda
市三 佃
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.)
Altemira Co Ltd
Original Assignee
Showa Aluminum Corp
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 Showa Aluminum Corp filed Critical Showa Aluminum Corp
Priority to JP18547285A priority Critical patent/JPS6289838A/en
Priority to US06/854,777 priority patent/US4713216A/en
Priority to AU56593/86A priority patent/AU563780B1/en
Priority to DE8686303127T priority patent/DE3665327D1/en
Priority to EP86303127A priority patent/EP0202044B1/en
Publication of JPS6289838A publication Critical patent/JPS6289838A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To obtain a high strength Al alloy excellent in hot rolling workability in particular and used as rolled plate for various purposes such as structural use, machine parts, etc., by providing a composition containing Zn, Mg, one or more among rare earth elements and, if necessary, one or more elements among Mn, Cr and Zr each in a prescribed percentage. CONSTITUTION:The high strength Al alloy excellent in rolling workability has a composition consisting of, by weight, 4-12% Zn 0.3-2.5% Mg, 0.5-10% of one or more kinds among rare earth elements, and the balance Al with inevitable impurities and further containing, if necessary, the following optional additive components: one or more kinds among 0.1-0.8% Mn, 0.05-0.30% Cr and 0.05-0.25% Zr. This Al alloy combines high strength practically comparable to that of conventional rollable high-strength Al alloy with characteristics such as excellent rolling workability, etc.

Description

【発明の詳細な説明】 産業上の利用分野 この発明は圧延板として構造用、機械部品等の各種用途
に用いられる特に熱間圧延加工性に優れた高強度アルミ
ニウム合金に関する。
DETAILED DESCRIPTION OF THE INVENTION Field of Industrial Application This invention relates to a high-strength aluminum alloy particularly excellent in hot rolling workability, which is used as a rolled plate for various purposes such as structural and mechanical parts.

なお、この明細書において「%」はいずれも重最%を示
すものとして用いられる。
In this specification, "%" is used to indicate the maximum percentage.

従来の技術と問題点 従来、高強度を有しつつ圧延が可能なアルミニウム合金
の代表的なものとしてへΩ−Zn−MtJ系のA707
5合金が良く知られている。
Conventional Technology and Problems Conventionally, A707, a Ω-Zn-MtJ system, has been used as a typical aluminum alloy that has high strength and can be rolled.
5 alloy is well known.

しかしながら、上記7075合金はなおも圧延が容易な
ものではなく、しかもCUが1.2〜2.0%の範囲で
相当量含有されているために溶接が不可能なものであ′
った。
However, the 7075 alloy is still not easy to roll, and furthermore, it contains a considerable amount of CU in the range of 1.2 to 2.0%, making it impossible to weld.
It was.

また、最近圧延材においても高強度薄肉化の要請は益々
強いものがあり、このような要請下にあって圧延性を低
下させず一更なる強度の向上をはかる目的で、ln添加
量を増大させる傾向にある。しかしZnの添加量を増や
すと、これ(伴って合金の耐応力腐食割れ性が低下し、
実用に耐え得ないものとなってしまう。一方、耐応力腐
食割れ性を比較的良好に保ちつつ、強度向上をはかるべ
く、MO添加量を増大する傾向もみられるが、この場合
は圧延性の低下を招き圧延材の生産性が低下する問題点
が生じている。
In addition, recently there has been an increasingly strong demand for high-strength, thin-walled rolled materials, and in response to these demands, the amount of ln added has been increased in order to further improve strength without reducing rollability. There is a tendency to However, when the amount of Zn added increases, this (accompanyingly, the stress corrosion cracking resistance of the alloy decreases,
This results in something that cannot be put to practical use. On the other hand, there is a tendency to increase the amount of MO added in order to improve strength while maintaining relatively good stress corrosion cracking resistance, but in this case, there is a problem that the rollability decreases and the productivity of the rolled material decreases. points are occurring.

この発明は上記のような従来技術の問題点に鑑み、圧延
加工性に優れた合金として予見されるへΩ−高りn−低
MrJ合金をベースにしながら、その耐応力腐食割れ性
を改善することにより、圧延性、溶接性、耐応力腐食割
れ性に優れた圧延用高強度アルミニウム合金を提供する
ことを目的としてなされたものである。
In view of the problems of the prior art as described above, this invention improves the stress corrosion cracking resistance of the Ω-high n-low MrJ alloy, which is predicted to be an alloy with excellent rolling workability. The purpose of this invention is to provide a high-strength aluminum alloy for rolling that has excellent rolling properties, weldability, and stress corrosion cracking resistance.

問題点を解決する為の手段 この発明は、上記の目的において種々実験と研究の結果
、Mgl、Qu量を増やさずにZn量の増大によって所
要強度の向上をはかるものとしたAρ−高zn−低Mg
合金を基礎として、これにYlLa SCe 、Pr 
、Nd 、Sm 、等の希土類元素を添加することによ
り、耐応力腐食割れ性を顕著しうろことを見出し、結果
的に圧延性の良好な高強度アルミニウム合金の実用化を
可能とし得たものである。
Means for Solving the Problems The present invention, as a result of various experiments and research for the above-mentioned purpose, aims to improve the required strength by increasing the amount of Zn without increasing the amounts of Mgl and Qu. Low Mg
Based on the alloy, YlLa SCe, Pr
By adding rare earth elements such as , Nd, Sm, etc., we discovered that scales have remarkable stress corrosion cracking resistance, and as a result, we were able to commercialize a high-strength aluminum alloy with good rollability. be.

即ち、この発明は、Zn:4〜12%、Mg :0.3
〜2.5%、あるいは更にCu:0,05〜0.7%を
含有し、かつ希土類元素のうちの1種または2種以上を
合計で0.5〜10%含有し、更に必要に応じて下記の
任意的添加成分を含有して、残部アルミニウム及び不可
避不純物からなる圧延加工性に優れた圧延用高強度アル
ミニウム合金を要旨とするものである。
That is, in this invention, Zn: 4 to 12%, Mg: 0.3
~2.5%, or further contains Cu: 0.05~0.7%, and contains one or more rare earth elements in a total of 0.5~10%, and further as necessary. The gist of the present invention is to provide a high-strength aluminum alloy for rolling which has excellent rolling workability and contains the following optional additive components and the balance is aluminum and unavoidable impurities.

この発明の上記合金は、その具体的実施においては上記
必須含有成分のほかに、更に他の任意的添加成分として
Mn :0.1〜0.8%、Cr 、0.05〜0.3
0%、Zr :0.05〜0.25%のうちの1種また
は2種以上が必要に応じて含有され得るものである。従
って、これらの任意的成分を含む合金もこの発明の所期
目的に適合するものであり、その範囲に包含されるもの
である。
In the concrete implementation of the alloy of the present invention, in addition to the above-mentioned essential components, other optional additive components include Mn: 0.1-0.8%, Cr: 0.05-0.3%.
0% and Zr: 0.05 to 0.25%, one or more of them may be contained as necessary. Therefore, alloys containing these optional components are also compatible with the intended purpose of the present invention and are included within its scope.

上記各合金成分及びその成分割合の限定理由について説
明すれば次のとおりである。
The reasons for limiting each of the alloy components and their proportions are as follows.

ZnおよびMOは、既知のとおりいずれも主として合金
の強度向上に寄与するものであり、Znが4%未満、M
gが0.3%未満では、充分な強度を得ることができな
い。反面lnは12%をこえて含有しても比例的な強度
向上効果は望めず実質的に無意味である。Mgは2.5
%を超えて含有すると、強度は向上するが圧延性が低下
し、この発明の所期目的に適合し得ないものとなる。
As is known, both Zn and MO mainly contribute to improving the strength of the alloy, and when Zn is less than 4% and M
If g is less than 0.3%, sufficient strength cannot be obtained. On the other hand, even if ln is contained in an amount exceeding 12%, no proportional strength improvement effect can be expected and it is essentially meaningless. Mg is 2.5
If the content exceeds 5%, the strength will improve, but the rolling properties will decrease, making it impossible to meet the intended purpose of the present invention.

CLIは、これも既知のとおり強度の向上に寄与するも
のであるが、含有量が0.05%未満では、その効果に
十分でなく、0.7%をこえると溶接性、耐食性、焼入
れ性が低下する。
As is known, CLI contributes to improving strength, but if the content is less than 0.05%, the effect is not sufficient, and if it exceeds 0.7%, it deteriorates weldability, corrosion resistance, and hardenability. decreases.

合金に添加される希土類元素は、特に限定されるもので
はないが、具体的には例えばY、 La 、Ce 1P
r 、Nd 、Sm等を好適物として挙示しうる。この
希土類に属する元素は、主に合金の耐応力腐食割れ性を
改善する効果を有する。この効果の点から、本発明にお
いては当該希土類元素のすべてを相互に実質的に均等物
として評価しうるちのである。従って、その1種または
2種以上を任意に組合わせて用いうるが、合金中におけ
るこれらの含有量が総量で0.5%未満では耐応力腐食
割れ性の改善効果に不充分である反面、10%を超えて
含有すると合金中に粗大な晶出物が多く発生し、強度の
低下を招く。最も好適な含有恐範囲I4コスト面も考慮
した場合概ね2.0〜7.0%程度である。
The rare earth element added to the alloy is not particularly limited, but specifically, for example, Y, La, Ce 1P
Preferred examples include r 2 , Nd 2 , Sm, and the like. This rare earth element mainly has the effect of improving the stress corrosion cracking resistance of the alloy. In view of this effect, all of the rare earth elements can be evaluated as substantially equivalent to each other in the present invention. Therefore, one or more of them can be used in any combination, but if the total content of these in the alloy is less than 0.5%, it is insufficient to improve the stress corrosion cracking resistance. If the content exceeds 10%, many coarse crystallized substances will be generated in the alloy, leading to a decrease in strength. The most suitable content range I4 is approximately 2.0 to 7.0% when cost is also taken into account.

任意含有成分で必るMn1Cr、Zrは、いずれも結晶
粒の微細化に役立つものでおり、Mn:0.1%未満、
Cr :0.05%未満、Zr:0.05%未満では上
記効果に乏しく、Mn:0.8%超過、Cr:0.3%
超過、Zr:0.25%超過の場合には、合金中に粗大
な晶出物を多く発生して合金の強度が低下する。
Mn, Cr, and Zr, which are optional components, are all useful for refining crystal grains, and Mn: less than 0.1%,
Cr: less than 0.05%, Zr: less than 0.05%, the above effects are poor, Mn: more than 0.8%, Cr: 0.3%
If Zr exceeds 0.25%, a large amount of coarse crystallized substances will be generated in the alloy, resulting in a decrease in the strength of the alloy.

発明の効果 この発明に係るアルミニウム合金は、上述したところか
ら既に理解しうるように、圧延材用として従来の圧延可
能な高強度アルミニウム合金にほぼ匹敵する高強度を有
しつつ、しかも圧延加工性に優れたものとなる。加えて
、Cuを多量に含有しないことにより、溶接性も良く、
溶接構造材として使用可能なものであると共に、希土類
元素の含有に基いて耐応力腐食割れ性にも優れたものと
なり、圧延材として生産性の良好な、しかも高強度のア
ルミニウム合金の実用化を可能とし、圧延材用途におけ
る薄肉軽但化、小型化の要請に好適に対応しうるちのと
なる。
Effects of the Invention As can be understood from the above, the aluminum alloy according to the present invention has high strength almost comparable to conventional rollable high-strength aluminum alloys for rolling materials, and has excellent rolling workability. Becomes excellent. In addition, since it does not contain a large amount of Cu, it has good weldability,
In addition to being usable as a welded structural material, it also has excellent stress corrosion cracking resistance due to the inclusion of rare earth elements, making it possible to commercialize a high-strength aluminum alloy with good productivity as a rolled material. This makes it possible to suitably meet the demands for thinner walls, lighter weight, and smaller size in rolled material applications.

なお、この発明の合金は、熱間鍛造にも好適に使用しう
る。
Note that the alloy of the present invention can also be suitably used for hot forging.

実施例 第1表に示す各種化学組成の合金を、厚さ55#×巾1
50mに水冷金型鋳造し、次いで、460’Cで12時
間の均質化処理を行った。その後厚さ50mに開削し、
これを450’Cにて3Mの厚さになるまで熱間圧延す
ることにより、そのときのパス回数で圧延性を評価する
と共に、耐応力割れ性、及び引張り強さについて性能測
定を行った。その結果を第2表に示す。
Example Alloys with various chemical compositions shown in Table 1 were made into a sheet with a thickness of 55# and a width of 1
It was cast in a water-cooled mold at 50 m and then homogenized at 460'C for 12 hours. After that, excavation was made to a thickness of 50m,
This was hot-rolled at 450'C to a thickness of 3M, and the rollability was evaluated by the number of passes at that time, and the performance was measured for stress cracking resistance and tensile strength. The results are shown in Table 2.

U以下余白] 第2表 ※1・・・・・・・・・ 厚さ5071111から厚さ
3#1l11までの熱間圧延バス回数。
Margin below U] Table 2 *1... Number of hot rolling baths from thickness 5071111 to thickness 3#1l11.

※2・・・・・・・・・ 3.5%Na Cfl水溶液
中にて、試験片に20KjJf/(Bdの応力を圧延方
向に負荷し、割れ発生までの 日数を測定鴫た。
*2... In a 3.5% Na Cfl aqueous solution, a stress of 20 KjJf/(Bd) was applied to the test piece in the rolling direction, and the number of days until cracking occurred was measured.

※3・・・・・・・・・T6材 溶体化処理条件 460℃・×2時間 →水冷 人工時効処理条件 120℃X24時間 上記第2表の結果に見られるように、本発明に係る合金
は、Znを高率に含有し、Mgの含有量を比較的低く抑
えたアルミニウム合金の範囲にあって、その固有の性質
としての高強度を保有したものでありながら、比較例合
金に較べて圧延性、耐応力腐食割れ性において優れた性
質を有するものであることがわかる。しかも本発明によ
る合金は、結晶粒も比較合金に較べて微細化されたもの
であり、焼入れ性、溶接性にも優れたものであった。
*3...T6 material solution treatment condition: 460°C x 2 hours → water cooling artificial aging treatment condition: 120°C x 24 hours As seen in the results in Table 2 above, the alloy according to the present invention is in the range of aluminum alloys that contain a high percentage of Zn and a relatively low content of Mg, and although it has high strength as its inherent property, it has a high strength compared to the comparative example alloy. It can be seen that it has excellent properties in terms of rolling properties and stress corrosion cracking resistance. Moreover, the alloy according to the present invention had finer grains than the comparative alloy, and had excellent hardenability and weldability.

以上 −と1 昭和60年10月18日 昭和60年 特許願第185472号 2、発明の名称 圧延加工性に優れた高強度アルミニウム合金3、補正を
する者 事件との関係  特許出願人 住所   堺市海山町6丁224番地 名称     昭和アルミニウム株式会社イ堕者石井 
親 4、代理人 住所   大阪市南区鰻谷中之町72−4心斎橋岩崎ビ
ル    、5.1.・ 氏名  (7118)弁理士清水大義、 。
Above - and 1 October 18, 1985 Patent Application No. 185472 2 Name of the invention High-strength aluminum alloy with excellent rolling workability 3 Relationship with the amended person's case Patent applicant address Sakai City 6-224 Kaizancho Name Showa Aluminum Co., Ltd. Fallen Ishii
Parent 4, agent address: Shinsaibashi Iwasaki Building, 72-4 Unagidani Nakanocho, Minami-ku, Osaka, 5.1.・Name (7118) Patent Attorney Daiyoshi Shimizu.

置 (06)245−2718 −一″5、補正命令の
日付  (自発補正) 6、補正により増加する発明の数 7、補正の対象 明細書の第10頁に記載の第2表を別紙のi′iす、訂
、正する。
(06) 245-2718 -1''5, Date of amendment order (voluntary amendment) 6, Number of inventions increased by amendment 7, Table 2 stated on page 10 of the specification subject to amendment in attached sheet i 'Isu, revise, correct.

(別紙) 第2表(Attachment) Table 2

Claims (2)

【特許請求の範囲】[Claims] (1)、Zn:4〜12% Mg:0.3〜2.5% 希土類元素のうちの1種または2種以上 :0.5〜10% を含有し、かつ必要に応じて、 Mn:0.1〜0.8% Cr:0.05〜0.30% Zr:0.05〜0.25% のうちの1種または2種以上を含有し、残 部アルミニウム及び不可避不純物からなる 圧延加工性に優れた高強度アルミニウム合 金。(1), Zn: 4-12% Mg: 0.3-2.5% One or more rare earth elements :0.5~10% and, if necessary, Mn: 0.1-0.8% Cr: 0.05-0.30% Zr: 0.05-0.25% Contains one or more of the following, with no residual Part consists of aluminum and unavoidable impurities High-strength aluminum alloy with excellent rolling workability Money. (2)、Zn:4〜12% Mg:0.3〜2.5% Cu:0.05〜0.7% 希土類元素のうちの1種または2種以上 :0.5〜10% を含有し、かつ必要に応じて、 Mn:0.1〜0.8% Cr:0.05〜0.30% Zr:0.05〜0.25% のうちの1種または2種以上を含有し、残 部アルミニウム及び不可避不純物からなる 圧延加工性に優れた高強度アルミニウム合 金。(2), Zn: 4-12% Mg: 0.3-2.5% Cu: 0.05-0.7% One or more rare earth elements :0.5~10% and, if necessary, Mn: 0.1-0.8% Cr: 0.05-0.30% Zr: 0.05-0.25% Contains one or more of the following, with no residual Part consists of aluminum and unavoidable impurities High-strength aluminum alloy with excellent rolling workability Money.
JP18547285A 1985-04-27 1985-08-22 High strength aluminum alloy excellent in rolling workability Pending JPS6289838A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
JP18547285A JPS6289838A (en) 1985-08-22 1985-08-22 High strength aluminum alloy excellent in rolling workability
US06/854,777 US4713216A (en) 1985-04-27 1986-04-22 Aluminum alloys having high strength and resistance to stress and corrosion
AU56593/86A AU563780B1 (en) 1985-04-27 1986-04-24 Al-mg-zn-rare earth alloy
DE8686303127T DE3665327D1 (en) 1985-04-27 1986-04-25 Aluminium alloy
EP86303127A EP0202044B1 (en) 1985-04-27 1986-04-25 Aluminium alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP18547285A JPS6289838A (en) 1985-08-22 1985-08-22 High strength aluminum alloy excellent in rolling workability

Publications (1)

Publication Number Publication Date
JPS6289838A true JPS6289838A (en) 1987-04-24

Family

ID=16171365

Family Applications (1)

Application Number Title Priority Date Filing Date
JP18547285A Pending JPS6289838A (en) 1985-04-27 1985-08-22 High strength aluminum alloy excellent in rolling workability

Country Status (1)

Country Link
JP (1) JPS6289838A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6396241A (en) * 1986-10-09 1988-04-27 Showa Alum Corp High strength aluminum alloy having superior resistance to stress corrosion cracking

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61238937A (en) * 1985-04-12 1986-10-24 Showa Alum Corp High-strength aluminum alloy for welding construction material excelling in extrudability and stress corrosion cracking resistance
JPS6244550A (en) * 1985-08-22 1987-02-26 Showa Alum Corp Aluminum alloy having superior cold workability
JPS6331537A (en) * 1986-07-21 1988-02-10 マサチユ−セツツ インスチチユ−ト オブ テクノロジイ Method for feeding out composition if necessary

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61238937A (en) * 1985-04-12 1986-10-24 Showa Alum Corp High-strength aluminum alloy for welding construction material excelling in extrudability and stress corrosion cracking resistance
JPS6244550A (en) * 1985-08-22 1987-02-26 Showa Alum Corp Aluminum alloy having superior cold workability
JPS6331537A (en) * 1986-07-21 1988-02-10 マサチユ−セツツ インスチチユ−ト オブ テクノロジイ Method for feeding out composition if necessary

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6396241A (en) * 1986-10-09 1988-04-27 Showa Alum Corp High strength aluminum alloy having superior resistance to stress corrosion cracking

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