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JPS6237706B2 - - Google Patents
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JPS6237706B2 - - Google Patents

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Publication number
JPS6237706B2
JPS6237706B2 JP11982183A JP11982183A JPS6237706B2 JP S6237706 B2 JPS6237706 B2 JP S6237706B2 JP 11982183 A JP11982183 A JP 11982183A JP 11982183 A JP11982183 A JP 11982183A JP S6237706 B2 JPS6237706 B2 JP S6237706B2
Authority
JP
Japan
Prior art keywords
less
strength
alloys
cold workability
aluminum
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
Application number
JP11982183A
Other languages
Japanese (ja)
Other versions
JPS6013047A (en
Inventor
Shigeyuki Kikuchi
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 JP11982183A priority Critical patent/JPS6013047A/en
Publication of JPS6013047A publication Critical patent/JPS6013047A/en
Publication of JPS6237706B2 publication Critical patent/JPS6237706B2/ja
Granted legal-status Critical Current

Links

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  • Forging (AREA)
  • Conductive Materials (AREA)

Description

【発明の詳細な説明】[Detailed description of the invention]

産業上の利用分野 この発明は、冷間加工性に優れた高強度アルミ
ニウム合金、特に例えばオートバイのリム材のよ
うに、張出し加工等の冷間加工を必要とする高強
度材料に使用されるAl―Zn―Mg―Cu系合金に関
する。 従来の技術 オートバイ用等のリム材に使用されるようなア
ルミニウム合金は、強度、耐食性等にすぐれてい
ることのほか、スポーク取付用のくぼみ部等を張
出し加工によつて形成しなければならないため、
冷間加工性にも優れた性質を有するものであるこ
とが要請される。ところが、従来、高強度アルミ
ニウム合金として既知のAl―Zn―Mg―Cu系合金
では、溶体化状態ないし所謂O材状態等の加工の
容易な調質状態でも冷間加工性に劣り、上記張出
し加工等により割れを発生し易い難点がある。 発明が解決しようとする問題点 この原因につき種々研究したところ、Al―Zn
―Mg―Cu系合金においては、その結晶粒形状を
調整するために通常添加されるMnやCrが悪影響
を及ぼしているものであることが知見された。一
方、従来合金として、上記MnやCrの代りにZrを
添加したAl―Zn―Mg―Cu系合金、例えばA7050
合金のようなものが知られているが、これらの合
金においては、Cu量が多すぎるために、やはり
依然として張出し加工等の冷間加工性が劣るもの
となつていることが知見された。 この発明は上記のような知見に基づき、殊に
Mn及びCrの含有量を規制すると共に、Cuの含有
量をも特定範囲に制限することにより、高強度を
保有しつつ冷間加工性、特に張出し加工性に優れ
た、両特性を同時に満足するアルミニウム合金で
あつて、その他実用面から要求される耐食性、耐
応力腐食割れ性、押出性等の面でも所要性能を備
えたアルミニウム合金を提供しようとするもので
ある。 問題点を解決するための手段 上記の目的において、この発明に係る冷間加工
性に優れた高強度アルミニウム合金は、 Zn:5.5〜10.0% Mg:1.5〜2.2% Cu:0.65〜2.0% Zr:0.05〜0.25% を含み、かつ Ti:0.001〜0.1% V:0.05〜0.25% B:0.0001〜0.08% のうちの1種または2種以上が含有され、あるい
は更に、 Mn:0.08%以下 Cr:0.1%以下 のうちの1種または2種が含有され、残りアルミ
ニウム及び不可避不純物からなることを特徴とす
るものである。 なお、この明細書において「%」はいずれも重
量基準で示すものである。 この発明に係る上記アルミニウム合金の含有成
分とその成分割合の意義について説明すれば次の
とおりである。 Znは、硬化要素として合金の強度の増大のた
めに不可欠の元素であり、5.5%未満ではその効
果が少なく、また10.0%を超えて多く含有される
と耐腐食割れ性が劣化する。Znの最も好ましい
含有範囲は6.0〜8.0%程度である。 Mgは、これもZnと同様に強度を増大するのに
必須の成分であり、1.5%未満ではその効果が少
なく、2.2%を超えて含有しても強度の向上に寄
与することは少なく、逆に冷間加工性、熱間加工
性が低下する欠点が派生する。最も好ましい含有
範囲は1.6〜1.8%程度である。 Cuは、強度の向上と同時に耐応力割れ性を改
善するのに必須の重要な元素であるが、0.65%未
満ではその効果が少なく、2.0%を超えると冷間
加工性が低下し、強度向上への寄与も少ない。最
も好ましい範囲は、0.7〜1.5%程度である。 Zrは、合金中の粗大再結晶を抑止し、結晶粒形
状を繊維組織化して組織の安定化をはかると共
に、張出し加工性の改善のために有効なものであ
るが、0.05%未満ではそれらの効果が少なく、
0.25%を超えると粗大な晶出物が生成して靭性等
を劣化させる。最も好ましい範囲は0.1〜0.15%
程度である。 Mnは、元来結晶粒形状の調整に有効なもので
あるが、逆にその添加によつて冷間加工性を劣化
させる傾向がある。しかし0.08%以下であれば、
その有害な影響は少ない。 Crは、これもMnと同じく結晶粒形状の調整に
有効である反面冷間加工性を劣化させるものであ
るが、0.1%以下であれば、その影響は少ない。 Ti、V、Bは、いずれも組織の安定化をはか
る上から有効なものであるが、それらの少なくと
も1種以上を、Ti0.001%以上、V0.05%以上、
B0.0001%以上の少量含有させることによつてそ
の効果を得ることができる。ただし、それらの多
すぎる含有は押出性等を劣化させるため、Ti0.1
%以下、V0.25%以下、B0.08%以下の範囲にそ
れぞれ制限される。 発明の効果 この発明に係るアルミニウム合金は、下記の実
施例の参酌によつて明らかであるように、引張り
強さ、耐力、伸び等の機械的性質において従来既
知であるような各種比較合金に較べて何ら遜色の
ない、むしろそれより優れた性質を保有しつつ、
張出し加工等の冷間加工性に優れたものであり、
オートバイ用等のリム材としてはもとより、高強
度とともに曲げ加工、プレス加工、絞り加工、し
ごき加工等の冷間加工を施す必要のために延性の
要求される各種用途の材料として好適使用しうる
ものである。なお、この発明に係る合金は、上記
リム材のように押出材として使用される場合のほ
か、シート材としても使用し得るものである。 次にこの発明の実施例を示す。 実施例
Industrial Application Fields This invention relates to high-strength aluminum alloys with excellent cold workability, especially aluminum alloys used in high-strength materials that require cold working such as stretch processing, such as motorcycle rim materials. - Regarding Zn-Mg-Cu alloys. Prior Art Aluminum alloys, such as those used for rim materials for motorcycles, have excellent strength and corrosion resistance, and in addition, they must be formed with recesses for attaching spokes by extrusion processing. ,
It is also required to have excellent cold workability. However, Al-Zn-Mg-Cu alloys, which are conventionally known as high-strength aluminum alloys, have poor cold workability even in a tempered state that is easy to process, such as a solution treated state or a so-called O-material state, and the above-mentioned stretch processing is difficult. There is a drawback that cracks are likely to occur due to such factors. Problems to be solved by the invention After various studies on the cause of this problem, it was found that Al-Zn
- It has been found that Mn and Cr, which are usually added to adjust the crystal grain shape, have an adverse effect on Mg-Cu alloys. On the other hand, as conventional alloys, Al-Zn-Mg-Cu alloys containing Zr instead of Mn and Cr, such as A7050
Although such alloys are known, it has been found that these alloys still have poor cold workability such as stretch processing due to the excessive amount of Cu. This invention is based on the above findings, especially
By regulating the content of Mn and Cr and also limiting the content of Cu to a specific range, it simultaneously satisfies both properties: high strength and excellent cold workability, especially stretch workability. The present invention aims to provide an aluminum alloy that also has the required performance in terms of corrosion resistance, stress corrosion cracking resistance, extrudability, etc., which are required from a practical standpoint. Means for Solving the Problems For the above purpose, the high strength aluminum alloy with excellent cold workability according to the present invention has the following properties: Zn: 5.5 to 10.0% Mg: 1.5 to 2.2% Cu: 0.65 to 2.0% Zr: 0.05 to 0.25%, and one or more of Ti: 0.001 to 0.1%, V: 0.05 to 0.25%, B: 0.0001 to 0.08%, or further, Mn: 0.08% or less, Cr: 0.1 % or less, and the remainder consists of aluminum and unavoidable impurities. In this specification, all "%" are expressed on a weight basis. The significance of the components contained in the aluminum alloy and the proportions thereof according to the present invention will be explained as follows. Zn is an essential element for increasing the strength of alloys as a hardening element, and if it is less than 5.5%, its effect is small, and if it is contained in a large amount exceeding 10.0%, corrosion cracking resistance deteriorates. The most preferable Zn content range is about 6.0 to 8.0%. Mg, like Zn, is an essential component for increasing strength; if it is less than 1.5%, its effect is small, and if it is contained in more than 2.2%, it does not contribute much to improving strength, and vice versa. This results in the disadvantage of reduced cold workability and hot workability. The most preferable content range is about 1.6 to 1.8%. Cu is an important element that is essential for improving stress cracking resistance at the same time as improving strength, but if it is less than 0.65%, its effect is small, and if it exceeds 2.0%, cold workability decreases and strength is improved. The contribution to this is also small. The most preferable range is about 0.7 to 1.5%. Zr is effective in suppressing coarse recrystallization in the alloy, stabilizing the structure by forming a fibrous structure in the crystal grain shape, and improving stretchability, but if it is less than 0.05%, the less effective,
If it exceeds 0.25%, coarse crystallized substances will be formed and the toughness will deteriorate. The most preferred range is 0.1-0.15%
That's about it. Although Mn is originally effective in adjusting grain shape, its addition tends to deteriorate cold workability. However, if it is less than 0.08%,
Its harmful effects are low. Cr, like Mn, is effective in adjusting grain shape, but on the other hand it degrades cold workability, but if it is 0.1% or less, the effect is small. Ti, V, and B are all effective for stabilizing the structure, and at least one of them should be added to Ti0.001% or more, V0.05% or more,
This effect can be obtained by containing a small amount of B0.0001% or more. However, if too many of them are contained, the extrudability etc. will be deteriorated, so Ti0.1
% or less, V0.25% or less, and B0.08% or less. Effects of the Invention As is clear from the following examples, the aluminum alloy according to the present invention is superior to various conventionally known comparative alloys in terms of mechanical properties such as tensile strength, yield strength, and elongation. While possessing properties that are not inferior to, in fact, superior to,
It has excellent cold workability such as overhang processing,
It can be suitably used not only as a rim material for motorcycles, etc., but also as a material for various applications that require high strength and ductility due to the need for cold working such as bending, pressing, drawing, and ironing. It is. The alloy according to the present invention can be used not only as an extruded material like the rim material described above, but also as a sheet material. Next, examples of this invention will be shown. Example

【表】 第1表に示す各種化学組成(残部はいずれもア
ルミニウム)のアルミニウム合金の常法によつて
製造した押出材を、470℃で1時間溶体化処理
し、水冷後、120℃で24時間の時効処理を施した
ものを試料とした。そして、この各試料につき、
その機械的性質と張出し加工性を調べたところ、
結果は下記第2表に示すとおりであつた。
[Table] Extruded materials of aluminum alloys with the various chemical compositions shown in Table 1 (the remainder is aluminum) were solution-treated at 470°C for 1 hour, cooled with water, and then heated at 120°C for 24 hours. The sample was subjected to time aging treatment. And for each sample,
When we investigated its mechanical properties and stretchability, we found that
The results were as shown in Table 2 below.

【表】【table】

【表】 なお、上記第2表において、張出し加工性は、
肉厚6mmの押出材を試料とし、直径17mmのポンチ
を有するエリクセン機により球面状に張出し加工
した場合の、試料に割れを生じるまでの張り出し
高さを測定したものである。また、評価はいずれ
もリム材としての用途を基準として、 〇:良好 △:やや良好 ×:不可 で示した。
[Table] In Table 2 above, the overhang workability is as follows:
The height of the overhang until the sample cracks was measured when an extruded material with a wall thickness of 6 mm was used as a sample and overhanged into a spherical shape using an Erichsen machine with a punch of 17 mm in diameter. In addition, all evaluations were made based on the use as a rim material, and were shown as 〇: Good, △: Fairly good, ×: Not good.

Claims (1)

【特許請求の範囲】 1 Zn:5.5〜10.0% Mg:1.5〜2.2% Cu:0.65〜2.0% Zr:0.05〜0.25% を含み、かつ Ti:0.001〜0.1% V:0.05〜0.25% B:0.0001〜0.08% のうちの1種または2種以上が含有され、残りア
ルミニウム及び不可避不純物からなることを特徴
とする、冷間加工性に優れた高強度アルミニウム
合金。 2 Zn:5.5〜10.0% Mg:1.5〜2.2% Cu:0.65〜2.0% Zr:0.05〜0.25% を含み、かつ Mn:0.08%以下 Cr:0.1%以下 のうちの1種または2種が含有され、更に Ti:0.001〜0.1% V:0.05〜0.25% B:0.0001〜0.08% のうちの1種または2種以上が含有され、残りア
ルミニウム及び不可避不純物からなることを特徴
とする、冷間加工性に優れた高強度アルミニウム
合金。
[Claims] 1 Contains Zn: 5.5-10.0% Mg: 1.5-2.2% Cu: 0.65-2.0% Zr: 0.05-0.25%, and Ti: 0.001-0.1% V: 0.05-0.25% B: 0.0001 A high-strength aluminum alloy with excellent cold workability, characterized in that it contains one or more of the following: ~0.08%, with the remainder consisting of aluminum and unavoidable impurities. 2 Contains Zn: 5.5 to 10.0% Mg: 1.5 to 2.2% Cu: 0.65 to 2.0% Zr: 0.05 to 0.25%, and contains one or two of the following: Mn: 0.08% or less Cr: 0.1% or less , and further contains one or more of Ti: 0.001-0.1%, V: 0.05-0.25%, and B: 0.0001-0.08%, with the remainder consisting of aluminum and inevitable impurities, and has cold workability. High strength aluminum alloy with excellent properties.
JP11982183A 1983-06-30 1983-06-30 High-strength aluminum alloy with superior cold workability Granted JPS6013047A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11982183A JPS6013047A (en) 1983-06-30 1983-06-30 High-strength aluminum alloy with superior cold workability

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11982183A JPS6013047A (en) 1983-06-30 1983-06-30 High-strength aluminum alloy with superior cold workability

Publications (2)

Publication Number Publication Date
JPS6013047A JPS6013047A (en) 1985-01-23
JPS6237706B2 true JPS6237706B2 (en) 1987-08-13

Family

ID=14771079

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11982183A Granted JPS6013047A (en) 1983-06-30 1983-06-30 High-strength aluminum alloy with superior cold workability

Country Status (1)

Country Link
JP (1) JPS6013047A (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4863528A (en) * 1973-10-26 1989-09-05 Aluminum Company Of America Aluminum alloy product having improved combinations of strength and corrosion resistance properties and method for producing the same
US5221377A (en) * 1987-09-21 1993-06-22 Aluminum Company Of America Aluminum alloy product having improved combinations of properties
US5496426A (en) * 1994-07-20 1996-03-05 Aluminum Company Of America Aluminum alloy product having good combinations of mechanical and corrosion resistance properties and formability and process for producing such product
RU2184166C2 (en) * 2000-08-01 2002-06-27 Государственное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" Aluminum-based high-strength alloy and product manufactured therefrom
JP4848099B2 (en) * 2001-07-18 2011-12-28 タカノ株式会社 Chair
US20040099352A1 (en) * 2002-09-21 2004-05-27 Iulian Gheorghe Aluminum-zinc-magnesium-copper alloy extrusion
JP5128124B2 (en) * 2003-04-10 2013-01-23 アレリス、アルミナム、コブレンツ、ゲゼルシャフト、ミット、ベシュレンクテル、ハフツング Al-Zn-Mg-Cu alloy
US20050034794A1 (en) * 2003-04-10 2005-02-17 Rinze Benedictus High strength Al-Zn alloy and method for producing such an alloy product
JP5083816B2 (en) * 2007-11-08 2012-11-28 住友軽金属工業株式会社 Al-Zn-Mg-Cu alloy extruded material excellent in warm workability, production method thereof, and warm worked material using the extruded material
CN102108463B (en) * 2010-01-29 2012-09-05 北京有色金属研究总院 Aluminium alloy product suitable for manufacturing structures and preparation method

Also Published As

Publication number Publication date
JPS6013047A (en) 1985-01-23

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