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JPS5950147A - High-strength and high-toughness aluminum alloy - Google Patents

High-strength and high-toughness aluminum alloy

Info

Publication number
JPS5950147A
JPS5950147A JP16052982A JP16052982A JPS5950147A JP S5950147 A JPS5950147 A JP S5950147A JP 16052982 A JP16052982 A JP 16052982A JP 16052982 A JP16052982 A JP 16052982A JP S5950147 A JPS5950147 A JP S5950147A
Authority
JP
Japan
Prior art keywords
strength
alloy
toughness
content
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.)
Granted
Application number
JP16052982A
Other languages
Japanese (ja)
Other versions
JPH0239574B2 (en
Inventor
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 JP16052982A priority Critical patent/JPS5950147A/en
Publication of JPS5950147A publication Critical patent/JPS5950147A/en
Publication of JPH0239574B2 publication Critical patent/JPH0239574B2/ja
Granted legal-status Critical Current

Links

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  • Conductive Materials (AREA)
  • Extrusion Of Metal (AREA)

Abstract

PURPOSE:To obtain an Al alloy with superior strength and toughness, by adding specified amounts of transition elements such as Mn, Cr and Zr to an Al-Mg-Si alloy. CONSTITUTION:0.05-0.8% Mn and 0.05-0.35% Cr and/or 0.05-0.20% Zr are added to an Al-Mg-Si alloy contg. 0.9-1.8% Si, 0.8-1.4% Mg and 0.4-1.8% Cu and having relation represented by Si content-Mg content/1.73>=0.3%. An Al alloy with superior strength and toughness suitable for use as a material for a baseball bat, a tent pole, a bobbin, bicycle parts, etc. is obtd.

Description

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

この発明は高強度、高靭性アルミニウム合金、特に例え
は野球用バット、テント用支柱、ホビン、自転車部品等
に使用される正j強度、高靭性のアルミニウム合金に関
する。 なお、この明細書において、「%」はいずれも「重量%
」を示すものとする。 従来、高強度Δl −M g −S i系合金として八
6066か良く知られている。このA6066合金は、
N4g、S i、Cuの硬化元素とともに、璧移元素と
してN41]を添加したものであるが、A6025、A
6061合金等に較へて、Mg、Siの高率含有により
高強度である反面、靭′旺を向」−させる遷移元素とし
てM nのみしか含刺しないために靭性に劣る欠点かあ
った。 この発明は高強度かつ高靭性のアルミニウム合金の開発
を急図してなされたものであり、Mg、Si、Cuの硬
化元素に加えてNin、、Sl、Cuの硬化元素に加え
てMn、Cr、Zrの遷移元素をそれぞれ特定の範囲で
含有することにより、へ6066合金に匹敵する高強度
を保有しつつ、靭性の著しく改善されたアルミニウム合
金か111られることを見出し、これを完成しく1また
ものである。 即ち、この発明に係るアルミニクくム合金は、Si:Q
、9〜18% Mg:0.8〜]、4% Cub  04〜18% を含有(但し、S1含有率−Mg含竹率/173≧0.
396 )すると共
The present invention relates to a high-strength, high-toughness aluminum alloy, and particularly to a high-strength, high-toughness aluminum alloy used in, for example, baseball bats, tent poles, hobbins, bicycle parts, and the like. In addition, in this specification, "%" refers to "% by weight".
” shall be indicated. Conventionally, 86066 is well known as a high strength Δl-Mg-Si alloy. This A6066 alloy is
In addition to the hardening elements of N4g, Si, and Cu, N41] is added as a transitional element, but A6025, A6025,
Compared to 6061 alloy, etc., it has high strength due to the high content of Mg and Si, but it has a disadvantage of inferior toughness because it contains only Mn as a transition element that promotes toughness. This invention was made with the urgent aim of developing a high-strength and high-toughness aluminum alloy. They discovered that by containing the transition elements Zr and Zr in specific ranges, it was possible to create an aluminum alloy with significantly improved toughness while possessing high strength comparable to H-6066 alloy. It is something. That is, the aluminum comb alloy according to the present invention has Si:Q
, 9-18% Mg: 0.8-], 4% Cub 04-18% (However, S1 content - Mg content / 173≧0.
396)

【こ、加えてM If : (l 
Q 5〜08% CI’:0.05〜035% ”’:0.05〜0.2096 のうぢ二種以−1l−を含有、し、残部アルミニウムお
よび不可避不純物からなることを特徴とするもSi、M
g、Cuは硬化元素として主に強度の増大に作用するも
のてあり、寸たM n、Cr、Zrは遷移元素として主
に靭性の向−1−に作用するものである。 而して、Siが09%未満、Mgか0896未1萬、C
uが04%未満の場合は所期する充分な高強度を実現す
ることかできない。反面SiおよびCuか18%を超え
、捷だM gか14%を超えるときは、押出性、延性、
靭性の低ドを来たすため、この発明の組成範囲から除外
される。 もっとも上記範囲内においても、Siは、M gとの相
対関係において常に0396す、上の過剰Si組成域に
おいて含イ1゛されることか必要である。 即ちS1含有率−M g含有率/173≧03%の範囲
においてSlの含1C4’ ;’(”+か規定され、こ
れを逸脱するときは強度面て充分な所期効果をr;する
ことかできない。 Mn、CrおよびZrは、それらの二種以上の任、C々
;の組合わせにおいて含有されれば良いが、特に好適に
は、Mnを必須成分とし、これとCrおよび7. rの
少なくとも一種以」二との組合わせにおいて含有せしめ
るのが靭性向上の点から望せしい。Mn、CrおよびZ
rの含有量は、それらかいずれも005%未満の場合に
は、所期する靭性の向上効果において充分でなく、また
逆に、M nか08%を超え、Crが0.35%を超え
、或いはZrが0.20%を超えるときは、粗大な金属
間化合物を生じて強度、靭性、延性を低1・″さぜる欠
点が派生する。 この発明に係る合金は、それ自体がAl−Mg−5i系
合金であるところから、押出性、耐食性、加工性が良好
であるのはもとより、高強度力つ高靭性の両特性を兼備
したものとなり、従来の比較的高価な2000番系ある
いは7000番系等の高強度アルミニウム合金に代替使
用可能な材料として低コストに提供できるものである。 次に、この発明の実施例を対照例と共に示す。 実施例 表  −1(W[%) 比較合金1・・・A606] 比較合金2・・・A6205 比較合金3・・A60G(う 表1に小ず各f中合金を、それぞれ金’f’s SJI
造により1白7子フインチのヒレソト(こして560°
Cて+ OII!1間均f5化処理した後、直径30訓
の棒にIt++ jl’+ +、た。次に550°Cて
] l14」Nil溶体化処理した抜水//l′i17
、史に180℃で7 [1」間のl:1」効処理を?i
−+たちのを試料とした。 ぞ(7て、この各試料につきJIS4す試験片(こ1戊
+ts力1目、1多、(ご:(、、:j、間1,1い幅
(50馴にて引張強さ、1[111力、伸び、1つ・よ
びシャルピー衝“”/+ 41’+をイ則定した。人、
’i 、!I:を1・記入2に小ず。 八  F  余  白 友  −2 土、記の結果から明らかなように、この発明(こ係るア
ルミニウム(r金は、幻照例3に、J<3\、11.る
従来のA 6066合金に相当づ−る俊れた杭、械的強
Jす(引張強さ、耐力)をイjするものでありなから、
靭性においてハしく数円1.\わ、ジ1照例1に示され
る従来のA6061合金に相当する高靭′1化をイ】す
るものである。 以  上
[In addition, M If: (l
Q 5-08% CI': 0.05-035% '': 0.05-0.2096 Contains at least 1 l- of 2 or more species, with the remainder consisting of aluminum and inevitable impurities. Also Si, M
G, Cu are hardening elements that mainly act to increase strength, and Mn, Cr, and Zr are transition elements that mainly act to increase toughness. Therefore, Si is less than 0.9%, Mg or 0896 is less than 10,000, and C
If u is less than 0.4%, the desired high strength cannot be achieved. On the other hand, when Si and Cu exceed 18% and Mg exceeds 14%, extrudability, ductility,
Since it causes low toughness, it is excluded from the composition range of this invention. However, even within the above range, Si must always be contained in the excess Si composition range above 0396 relative to Mg. That is, in the range of S1 content - Mg content / 173≧03%, the content of Sl is defined as 1C4';'('+), and when it deviates from this, a sufficient desired effect in terms of strength must be achieved. Mn, Cr and Zr may be contained in a combination of two or more of them, but it is particularly preferred that Mn is an essential component and Cr and 7. From the viewpoint of improving toughness, it is desirable to contain at least one of the following in combination with Mn, Cr and Z.
If the r content is less than 0.005%, it will not be sufficient to achieve the desired toughness improvement effect, and conversely, if Mn exceeds 0.08% and Cr exceeds 0.35%. , or when Zr exceeds 0.20%, coarse intermetallic compounds are formed, resulting in a decrease in strength, toughness, and ductility. -Since it is a Mg-5i alloy, it not only has good extrudability, corrosion resistance, and workability, but also has both high strength and toughness, which makes it difficult to replace the conventional 2000 series, which is relatively expensive. Alternatively, it can be provided at low cost as a material that can be used as an alternative to high-strength aluminum alloys such as No. 7000 series.Next, examples of the present invention are shown together with comparative examples.Example Table-1 (W [%) Comparative alloy 1...A606] Comparative alloy 2...A6205 Comparative alloy 3...A60G
Fillet fillet of 1 white 7 roe finch (strained 560°)
Cte + OII! After being equalized for 1 hour, it was made into a bar with a diameter of 30 mm. Next, at 550°C] l14'' Nil solution treated water removal//l'i17
, at 180°C between 7 [1] and 1:1" effect treatment? i
−+ and others were used as samples. (7) For each sample, JIS 4 test piece (this 1 + ts force 1 stitch, 1 more, (go: (,,: [111 force, elongation, 1, and Charpy opposition ""/+ 41'+ were defined as I.
'i,! I: 1・Enter 2 small pieces. As is clear from the results described above, this invention (aluminum (r gold) corresponds to the conventional A 6066 alloy in Gensho Example 3, J<3\, 11. - It is a good pile with good mechanical strength (tensile strength, yield strength),
A few yen higher in toughness 1. This alloy has high toughness equivalent to that of the conventional A6061 alloy shown in Example 1. that's all

Claims (1)

【特許請求の範囲】 +ns1:o9〜18% Mg:Q8〜1.4% Cu;Q4−18% を含有(但し、Si含有率−Mg含有率/173≧03
%)すると共に、 M n : 0.05〜0.8% Cr:QQ5−035% 7、r:0.05〜020% のうち二種以上を金相し、残部アルミニウムおよび不可
避不純物からなることを特徴とする高強度、高靭性アル
ミニウム合金。 f21  M nを必須成分として金相′シ、更に0丁
およびZrの一種以」二を含1自することを特徴とする
特許請求の・n間第1項記載の高強度、高靭性アルミニ
ウム合金。
[Claims] Contains +ns1: o9 to 18% Mg: Q8 to 1.4% Cu; Q4 to 18% (However, Si content - Mg content / 173≧03
%), and Mn: 0.05-0.8% Cr: QQ5-035% 7, r: 0.05-020% Two or more of these should be made into a gold phase, and the remainder should consist of aluminum and inevitable impurities. High strength, high toughness aluminum alloy. A high-strength, high-toughness aluminum alloy according to claim 1, characterized in that it contains f21Mn as an essential component, a metal phase, and one or more of Zr and Zr. .
JP16052982A 1982-09-14 1982-09-14 High-strength and high-toughness aluminum alloy Granted JPS5950147A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP16052982A JPS5950147A (en) 1982-09-14 1982-09-14 High-strength and high-toughness aluminum alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP16052982A JPS5950147A (en) 1982-09-14 1982-09-14 High-strength and high-toughness aluminum alloy

Publications (2)

Publication Number Publication Date
JPS5950147A true JPS5950147A (en) 1984-03-23
JPH0239574B2 JPH0239574B2 (en) 1990-09-06

Family

ID=15716932

Family Applications (1)

Application Number Title Priority Date Filing Date
JP16052982A Granted JPS5950147A (en) 1982-09-14 1982-09-14 High-strength and high-toughness aluminum alloy

Country Status (1)

Country Link
JP (1) JPS5950147A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5240519A (en) * 1991-08-28 1993-08-31 Nippon Light Metal Company, Ltd. Aluminum based Mg-Si-Cu-Mn alloy having high strength and superior elongation
US5571347A (en) * 1994-04-07 1996-11-05 Northwest Aluminum Company High strength MG-SI type aluminum alloy
US5571346A (en) * 1995-04-14 1996-11-05 Northwest Aluminum Company Casting, thermal transforming and semi-solid forming aluminum alloys
US5911843A (en) * 1995-04-14 1999-06-15 Northwest Aluminum Company Casting, thermal transforming and semi-solid forming aluminum alloys
US5968292A (en) * 1995-04-14 1999-10-19 Northwest Aluminum Casting thermal transforming and semi-solid forming aluminum alloys
WO2013065583A1 (en) * 2011-11-02 2013-05-10 住友電気工業株式会社 Aluminum alloy sheet for terminal, terminal fitting, and electric wire terminal connection structure
CN105838944A (en) * 2015-01-16 2016-08-10 昆山捷安特轻合金科技有限公司 High-strength weldable aluminum alloy for vehicle bodies and preparation method thereof
CN104745902B (en) * 2013-12-30 2017-02-08 鼎镁(昆山)新材料科技有限公司 High strength Al-Mg-Si-Cu alloy for bicycles and processing technology thereof

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS505212A (en) * 1973-05-18 1975-01-20
JPS5292812A (en) * 1976-02-02 1977-08-04 Mitsubishi Metal Corp Production of corrosion-resisting al alloy sheet having high strength and tough ductility
JPS5319117A (en) * 1976-08-05 1978-02-22 Aluminum Co Of America Modified aluminium structure

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS505212A (en) * 1973-05-18 1975-01-20
JPS5292812A (en) * 1976-02-02 1977-08-04 Mitsubishi Metal Corp Production of corrosion-resisting al alloy sheet having high strength and tough ductility
JPS5319117A (en) * 1976-08-05 1978-02-22 Aluminum Co Of America Modified aluminium structure

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5240519A (en) * 1991-08-28 1993-08-31 Nippon Light Metal Company, Ltd. Aluminum based Mg-Si-Cu-Mn alloy having high strength and superior elongation
US5571347A (en) * 1994-04-07 1996-11-05 Northwest Aluminum Company High strength MG-SI type aluminum alloy
US5571346A (en) * 1995-04-14 1996-11-05 Northwest Aluminum Company Casting, thermal transforming and semi-solid forming aluminum alloys
US5846350A (en) * 1995-04-14 1998-12-08 Northwest Aluminum Company Casting thermal transforming and semi-solid forming aluminum alloys
US5911843A (en) * 1995-04-14 1999-06-15 Northwest Aluminum Company Casting, thermal transforming and semi-solid forming aluminum alloys
US5968292A (en) * 1995-04-14 1999-10-19 Northwest Aluminum Casting thermal transforming and semi-solid forming aluminum alloys
WO2013065583A1 (en) * 2011-11-02 2013-05-10 住友電気工業株式会社 Aluminum alloy sheet for terminal, terminal fitting, and electric wire terminal connection structure
JPWO2013065583A1 (en) * 2011-11-02 2015-04-02 住友電気工業株式会社 Aluminum alloy plate for terminals, terminal fittings, and terminal connection structure for electric wires
CN104745902B (en) * 2013-12-30 2017-02-08 鼎镁(昆山)新材料科技有限公司 High strength Al-Mg-Si-Cu alloy for bicycles and processing technology thereof
CN105838944A (en) * 2015-01-16 2016-08-10 昆山捷安特轻合金科技有限公司 High-strength weldable aluminum alloy for vehicle bodies and preparation method thereof

Also Published As

Publication number Publication date
JPH0239574B2 (en) 1990-09-06

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