JPH03173736A - High strength aluminum alloy capable of hollow extruding by combination die - Google Patents

High strength aluminum alloy capable of hollow extruding by combination die

Info

Publication number
JPH03173736A
JPH03173736A JP31235289A JP31235289A JPH03173736A JP H03173736 A JPH03173736 A JP H03173736A JP 31235289 A JP31235289 A JP 31235289A JP 31235289 A JP31235289 A JP 31235289A JP H03173736 A JPH03173736 A JP H03173736A
Authority
JP
Japan
Prior art keywords
hollow
combination die
die
high strength
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
JP31235289A
Other languages
Japanese (ja)
Inventor
Isao Murase
功 村瀬
Yukihiro Miyate
宮手 幸裕
Hisashi Maehara
前原 久
Noboru Oneda
大根田 昇
Shigeyuki Kikuchi
菊池 茂幸
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 JP31235289A priority Critical patent/JPH03173736A/en
Publication of JPH03173736A publication Critical patent/JPH03173736A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To manufacture the high strength Al alloy capable of extruding a thin hollow shape material by a combination die by incorporating specified ratios of Mg, Zn, Cu and Zr into Al. CONSTITUTION:An Al alloy contg., by weight, 1.3 to 2.0% Mg, 5.0 to 8.0% Zn, 0.4% to 1.0% Cu, 0.1 to 0.2% Zr and the balance Al with inevitable impurities is manufactured by the conventional method. In this way, the high strength Al alloy capable of subjecting a thin shape material to hollow extruding by an combination die such as a porthole die can be obtd., and the obtd. hollow extruded material is provided with about >=50kg.fmm<2> tensile strength.

Description

【発明の詳細な説明】 産業上の利用分野 この発明は、ボートホールダイス等の組合せダイスによ
る中空押出形材、例えばオートバイのフレーム、リャホ
ークその他構造用等の中空押出形材に用いられる組合せ
ダイスによる中空押出可能な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 hollow extruded sections by a combination die such as a boathole die, for example, a combination die used for hollow extrusion sections for motorcycle frames, rear hawks, and other structures. This invention relates to a high-strength aluminum alloy that can be hollow extruded.

従来の技術 雄型ダイスと雌型ダイスとの組合せからなるボートホー
ルダイス等の組合せダイスを用いて上記のような中空押
出形材を製作する場合、その材料としては従来、7N0
1.7003合金が用いられていた。
Conventional technology When producing a hollow extruded section as described above using a combination die such as a boathole die consisting of a combination of a male die and a female die, the material used is conventionally 7N0.
1.7003 alloy was used.

ところで、近時、車両等装置の軽量化の要求に伴い、部
品等として用いられる中空押出形材に対してもその薄肉
化による重量削減が要請されている。而して、形材を薄
肉化すると強度が低下することから、中空形材自体の強
度向上が不可欠であり、このために50 K9 f /
−程度以上の引張強度が要求されるようになってきてい
る。
Incidentally, in recent years, with the demand for weight reduction of devices such as vehicles, there has been a demand for reducing the weight of hollow extruded shapes used as parts and the like by making the walls thinner. Since the strength of the hollow shape material decreases when the shape is made thinner, it is essential to improve the strength of the hollow shape material itself.For this purpose, 50 K9 f/
- Tensile strength of at least a certain degree is now required.

発明が解決しようとする課題 しかるに、従来材である7N01.7003合金は材料
自体の強度に劣り、上記要請に満足を与えることはでき
なかった。
Problems to be Solved by the Invention However, the conventional material 7N01.7003 alloy has poor strength as a material itself, and cannot satisfy the above requirements.

一方、要求強度を満たす材料として7075合金が存在
するが、該合金はボートホール押出が不可能であった。
On the other hand, 7075 alloy exists as a material that satisfies the required strength, but boathole extrusion is not possible with this alloy.

しかも、焼入感受性が高いため、押出後容体化処理を行
わなければならず、その結果焼入れ歪が発生するためボ
ートホール押出によって得られるような複雑な中空形状
の製作は困難であった。
Moreover, since it is highly sensitive to quenching, it is necessary to carry out a compacting treatment after extrusion, and as a result, quenching distortion occurs, making it difficult to manufacture complex hollow shapes such as those obtained by boathole extrusion.

この発明はかかる技術的背景に鑑みてなされたものであ
って、ボートホールダイス等の組合せダイスによる中空
形材への製作が可能であって、かつ50Kyf/#II
j程度以上の引張強度を有するアルミニウム合金の提供
を目的とする。
The present invention was made in view of the above technical background, and it is possible to manufacture hollow shapes using a combination die such as a boat hole die, and a 50Kyf/#II
The purpose of the present invention is to provide an aluminum alloy having a tensile strength of approximately J or more.

課題を解決するための手段 上記目的は、Mg : 1. 3〜2. 0wt%、Z
n : 5.  O〜8. 0wt%、Cu:0.4〜
1゜0wt%、Zr:0.1〜0.2wt%を含有し、
残部アルミニウム及び不可避不純物からなることを特徴
とする組合せダイスによる中空押出可能な高強度アルミ
ニウム合金によって達成される。
Means for Solving the Problems The above objectives are as follows: Mg: 1. 3-2. 0wt%, Z
n: 5. O~8. 0wt%, Cu: 0.4~
Contains 1°0 wt%, Zr: 0.1 to 0.2 wt%,
This is achieved by a high-strength aluminum alloy that can be hollow extruded using a combination die, characterized in that the balance consists of aluminum and unavoidable impurities.

まず、本発明合金組成において、Mgは押出材の強度向
上に寄与するものである。しかし1゜3wt%未満では
その効果に乏しい。一方2.0wt%を超えると押出性
を阻害し、ボートホール押出等の組合せダイスによる中
空押出に支障を来たす。Mgの特に好ましい範囲は18
4〜1゜7vt%である。
First, in the alloy composition of the present invention, Mg contributes to improving the strength of the extruded material. However, if it is less than 1.3 wt%, the effect is poor. On the other hand, if it exceeds 2.0 wt%, extrudability will be inhibited, causing problems in hollow extrusion using a combination die such as boathole extrusion. A particularly preferable range of Mg is 18
It is 4-1°7vt%.

Znもまた押出材の強度向上に有効なものである。しか
し、5. 0wt5未満ではその効果に乏しい。一方8
.  0wt%を超えると耐応力腐食割れ性(耐SCC
性)が悪くなる。Znの特に好ましい範囲は5.5〜7
.5vt%である。
Zn is also effective in improving the strength of extruded materials. However, 5. If it is less than 0wt5, the effect is poor. On the other hand 8
.. If it exceeds 0wt%, stress corrosion cracking resistance (SCC resistance)
(sexuality) worsens. A particularly preferable range of Zn is 5.5 to 7
.. It is 5vt%.

Cuは押出材圧着部の耐応力腐食割れ性を向上する効果
がある。しかし、0.4vt%未満ではその効果が少な
く、1.0wt%を超えると焼入れ性、押出性が悪化し
、ボートホール押出が困難となる。Cuの特に好ましい
範囲は0.5〜0.7vt%である。
Cu has the effect of improving the stress corrosion cracking resistance of the crimped part of the extruded material. However, if it is less than 0.4 wt%, the effect is small, and if it exceeds 1.0 wt%, hardenability and extrudability deteriorate, making boathole extrusion difficult. A particularly preferred range of Cu is 0.5 to 0.7 vt%.

2「は組織の微細化に寄与するものである。2" contributes to the refinement of the structure.

しかしO,1wt%未満ではその効果に乏しく、逆に0
.2wt%を超えても該効果の格別な増大がなく、却っ
て経済的な無駄を招く。特に好ましいZrの範囲は0.
12〜0.17vt%である。
However, if O is less than 1 wt%, the effect is poor;
.. Even if it exceeds 2 wt%, the effect will not be increased significantly, and on the contrary, it will cause economic waste. A particularly preferable range of Zr is 0.
It is 12-0.17vt%.

本発明に係るアルミニウム合金を用いたボートホール押
出等の組合せダイスによる中空押出は常法に従って行え
ば良い。その−例を示すと、鋳造ビレットに均熱処理を
施したのち熱間にて押出す。モして押出直後にファンや
水スプレーによって冷却して焼入を行い、あるいは別途
容体化処理と焼入処理を行い、時効処理を行って所期す
る中空押出材を得る。
Hollow extrusion using a combination die such as boathole extrusion using the aluminum alloy according to the present invention may be carried out according to a conventional method. For example, a cast billet is soaked and then hot extruded. Immediately after extrusion, the product is cooled and quenched using a fan or water spray, or separately subjected to compaction treatment and quenching treatment, followed by aging treatment to obtain the desired hollow extruded material.

発明の効果 この発明に係るアルミニウム合金は、各元素と組成範囲
の組合せにより、ボートホールダイス等の組合せダイス
を用いた中空押出が可能であるとともに、得られた中空
押出材に50 K’J f/−程度以上の引張強度を付
与することができる。従って複雑形状の中空形材の製作
が可能であるのはもとより、その高強度により該形材の
薄肉化が可能となり、車両等装置の小型軽量化に寄与し
うるちのとなる。しかも焼入感受性が7075合金はど
高くないことから容易に焼きを入れることができるとと
もにその後の時効処理を十分に行うことができる。
Effects of the Invention The aluminum alloy according to the present invention can be hollow extruded using a combination die such as a boathole die due to the combination of each element and composition range, and the obtained hollow extrusion material has a heat resistance of 50 K'J f. A tensile strength of /- or more can be imparted. Therefore, not only is it possible to manufacture a hollow section with a complicated shape, but its high strength also makes it possible to make the section thinner, which contributes to the reduction in size and weight of devices such as vehicles. Moreover, since the 7075 alloy is not very sensitive to hardening, it can be hardened easily and the subsequent aging treatment can be carried out satisfactorily.

実施例 次にこの発明の実施例を示す。Example Next, examples of this invention will be shown.

下記第1表に示す各種組成のアルミニウム合金鋳塊をD
C鋳造により直径178IIMのビレットに鋳造したの
ち、470℃で8時間均熱した。
D
After casting into a billet with a diameter of 178 IIM by C casting, it was soaked at 470° C. for 8 hours.

次に、組合せダイスであるブリッジダイスを用いて、上
記ビレットをビレット温度480℃、ラム速度0.1m
/■1nの速度で、縦40履、横100mgg、肉厚3
M中空角材に押出して、まず押出の可否を調査した。そ
の結果、試料N。
Next, using a bridge die which is a combination die, the above billet was diced at a billet temperature of 480°C and a ram speed of 0.1 m.
/ ■ At a speed of 1n, length 40 shoes, width 100 mgg, wall thickness 3
First, the feasibility of extrusion was investigated by extruding it into M hollow square material. As a result, sample N.

6の7075合金を除き支障なく押出を行うことができ
た。これに対し、7075合金では押出が困難であった
Extrusion could be carried out without any problems except for the 7075 alloy in No. 6. In contrast, 7075 alloy was difficult to extrude.

次に、上記各中空押出材を押出直後にファンと水スプレ
ーによって冷却することにより焼入れを行った。モして
押出後24時間放置したのち70℃×5時間+140℃
×10時間の時効処理を行った。
Next, each of the hollow extruded materials described above was quenched by cooling with a fan and water spray immediately after extrusion. After extruding and leaving for 24 hours, 70℃ x 5 hours + 140℃
Aging treatment was performed for 10 hours.

上記により得られた各中空押出形材の引張強度を測定し
た。なお7075合金については、φ25の押出棒を4
70℃X2Hr保持後水冷し、120℃×12時間の時
効処理したものの引張強度を測定した。その結果を第1
表に併せて示す。
The tensile strength of each hollow extruded shape obtained above was measured. For 7075 alloy, 4 extruded rods of φ25
After being held at 70°C for 2 hours, it was water-cooled and aged at 120°C for 12 hours, and its tensile strength was measured. The result is the first
It is also shown in the table.

〔以下余白〕[Margin below]

第1表の結果から、本発明合金は組合せダイスによる中
空押出が可能であり、かつ得られた押出材は50 Kg
 f /−を超える引張強度を有していることを確認し
えた。これに対し、7N01.7003合金は強度に劣
り、7075合金は上記押出が不可能であった。
From the results in Table 1, the alloy of the present invention can be hollow extruded using a combination die, and the obtained extruded material weighs 50 kg.
It was confirmed that it had a tensile strength exceeding f/-. On the other hand, the 7N01.7003 alloy had poor strength, and the 7075 alloy could not be extruded as described above.

以上 205that's all 205

Claims (1)

【特許請求の範囲】[Claims] Mg:1.3〜2.0wt%、Zn:5.0〜8.0w
t%、Cu:0.4〜1.0wt%、Zr:0.1〜0
.2wt%を含有し、残部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組合せダイスによる中空押
出可能な高強度アルミニウム合金。
Mg: 1.3-2.0wt%, Zn: 5.0-8.0w
t%, Cu: 0.4-1.0wt%, Zr: 0.1-0
.. A high-strength aluminum alloy that can be hollow extruded using a combination die, characterized in that the aluminum alloy contains 2 wt% and the balance consists of aluminum and unavoidable impurities.
JP31235289A 1989-11-30 1989-11-30 High strength aluminum alloy capable of hollow extruding by combination die Pending JPH03173736A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP31235289A JPH03173736A (en) 1989-11-30 1989-11-30 High strength aluminum alloy capable of hollow extruding by combination die

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP31235289A JPH03173736A (en) 1989-11-30 1989-11-30 High strength aluminum alloy capable of hollow extruding by combination die

Publications (1)

Publication Number Publication Date
JPH03173736A true JPH03173736A (en) 1991-07-29

Family

ID=18028215

Family Applications (1)

Application Number Title Priority Date Filing Date
JP31235289A Pending JPH03173736A (en) 1989-11-30 1989-11-30 High strength aluminum alloy capable of hollow extruding by combination die

Country Status (1)

Country Link
JP (1) JPH03173736A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010196089A (en) * 2009-02-24 2010-09-09 Kobe Steel Ltd Extruded pipe of aluminum alloy having high strength and superior stress corrosion cracking resistance for hydroforming process

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5336812A (en) * 1977-08-27 1978-04-05 Hitachi Ltd Current collector
JPS5779142A (en) * 1980-10-31 1982-05-18 Kobe Steel Ltd Extruded aluminum alloy with superior flash butt weldability
JPS63297543A (en) * 1987-05-28 1988-12-05 Kobe Steel Ltd Production of al-zn-mg alloy extruded material having light alumite tone

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5336812A (en) * 1977-08-27 1978-04-05 Hitachi Ltd Current collector
JPS5779142A (en) * 1980-10-31 1982-05-18 Kobe Steel Ltd Extruded aluminum alloy with superior flash butt weldability
JPS63297543A (en) * 1987-05-28 1988-12-05 Kobe Steel Ltd Production of al-zn-mg alloy extruded material having light alumite tone

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010196089A (en) * 2009-02-24 2010-09-09 Kobe Steel Ltd Extruded pipe of aluminum alloy having high strength and superior stress corrosion cracking resistance for hydroforming process

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