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JPH0621328B2 - Method for manufacturing extruded material with excellent hollow extrudability - Google Patents
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JPH0621328B2 - Method for manufacturing extruded material with excellent hollow extrudability - Google Patents

Method for manufacturing extruded material with excellent hollow extrudability

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Publication number
JPH0621328B2
JPH0621328B2 JP14788A JP14788A JPH0621328B2 JP H0621328 B2 JPH0621328 B2 JP H0621328B2 JP 14788 A JP14788 A JP 14788A JP 14788 A JP14788 A JP 14788A JP H0621328 B2 JPH0621328 B2 JP H0621328B2
Authority
JP
Japan
Prior art keywords
hollow
extruded material
alloy
extrudability
extrusion
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
Application number
JP14788A
Other languages
Japanese (ja)
Other versions
JPH01177341A (en
Inventor
照生 宇野
清一 平野
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.)
Sumitomo Light Metal Industries Ltd
Original Assignee
Sumitomo Light Metal Industries Ltd
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 Sumitomo Light Metal Industries Ltd filed Critical Sumitomo Light Metal Industries Ltd
Priority to JP14788A priority Critical patent/JPH0621328B2/en
Publication of JPH01177341A publication Critical patent/JPH01177341A/en
Publication of JPH0621328B2 publication Critical patent/JPH0621328B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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  • Extrusion Of Metal (AREA)

Description

【発明の詳細な説明】 [産業上の利用分野] 本発明は、ホロー押出性にすぐれた高比弾性係数を有す
る高力アルミニウム合金製の押出材の製造法に関する。
TECHNICAL FIELD The present invention relates to a method for producing an extruded material made of a high-strength aluminum alloy having a high specific elastic modulus which is excellent in hollow extrudability.

[従来の技術] 現在主に使われている高力アルミニウム合金としては、
2××× 系(Al−Cu系)合金及び 7××× 系(A
l−Zn−Mg系)合金の2種類がある。この中、C
u、Mg量の多い合金では熱間加工時の変形抵抗が高
く、かつホロー押出時の溶着性が悪い。したがって、ホ
ロー押出が実用化されているのは7NO1合金、7003合金等
の一部のAl−An−Mg系合金に限られている。
[Prior Art] As a high-strength aluminum alloy currently mainly used,
2xxxx system (Al-Cu system) alloy and 7xxx system (A
1-Zn-Mg-based alloy. Among these, C
Alloys containing a large amount of u and Mg have high deformation resistance during hot working and poor weldability during hollow extrusion. Therefore, the hollow extrusion is practically used only for some Al—An—Mg alloys such as 7NO1 alloy and 7003 alloy.

[発明が解決しようとする課題] 本発明は、前述のホロー押出に実用されている合金以外
の組成の合金で、ホロー押出性にすぐれた高比弾性係数
を有する高力アルミニウム合金をもってホロー押出材を
製造せんとするものである。
[Problems to be Solved by the Invention] The present invention relates to an alloy having a composition other than the alloy that is practically used for hollow extrusion described above, and a hollow extruded material having a high strength aluminum alloy having a high specific elastic modulus which is excellent in hollow extrusion. Is to be manufactured.

[課題を解決するための手段] 本発明は、Li: 0.5〜4.0 %、Cu: 0.2〜3.0 %、
Mg: 0.2〜2.0 %を必須成分として含み、あるいはさ
らにZr:0.05〜0.30%、Cr: 0.05〜0.30%、M
n: 0.05〜 1.0 %、V:0.05〜0.30%のうちの1種以
上を含み、残りアルミニウムと不純物よりなる合金を鋳
造した後、 480〜550 ℃で2〜48時間均質化処理し、
ついで 450〜550 ℃でホロー押出することを特徴とする
ホロー押出性にすぐれた押出材の製造法である。
[Means for Solving the Problems] The present invention provides Li: 0.5 to 4.0%, Cu: 0.2 to 3.0%,
Mg: 0.2 to 2.0% as an essential component, or Zr: 0.05 to 0.30%, Cr: 0.05 to 0.30%, M
n: 0.05 to 1.0%, V: 0.05 to 0.30%, and at least one of them are cast, and after casting an alloy consisting of the remaining aluminum and impurities, homogenized at 480 to 550 ° C for 2 to 48 hours,
Then, it is a method for producing an extruded material having excellent hollow extrudability, which is characterized by performing hollow extrusion at 450 to 550 ° C.

ここにおいて合金組成の限定理由は下記のとおりであ
る。
Here, the reason for limiting the alloy composition is as follows.

Li:Liは合金材の強度向上に効果がある。さらにL
iの添加で比重が減少し、弾性係数が増加することか
ら、合金材の低密度化、高弾性化にも効果的である。以
上の効果は、 1.5%未満ではなく、 4.0%より多いと鋳
造しにくく、また、均質化処理によっても鋳造時のミク
ロ偏析を取り除きにくいので、加工しにくく、ホロー押
出時の溶着性も劣る。さらに延性、靭性が低下する。
Li: Li is effective in improving the strength of the alloy material. Furthermore L
The addition of i decreases the specific gravity and increases the elastic coefficient, and is therefore effective in reducing the density and increasing the elasticity of the alloy material. The above effect is not less than 1.5%, but more than 4.0%, it is difficult to cast, and it is difficult to remove the microsegregation during casting even by homogenization treatment, so that it is difficult to process and the weldability during hollow extrusion is poor. Further, ductility and toughness are reduced.

Cu、Mg:Cu、Mgは共に合金材の強度向上に効果
がある。この効果は、下限未満では構造体としての強度
が得られず、また、上限を越えると変形抵抗が大きくな
り、ホロー押出がむずかしく、溶着性も劣る。
Cu, Mg: Cu and Mg are both effective in improving the strength of the alloy material. If the effect is less than the lower limit, the strength of the structure cannot be obtained, and if it exceeds the upper limit, the deformation resistance becomes large, hollow extrusion is difficult, and the weldability is poor.

Zr、Cr、Mn、V:これらは均質化処理時に微細な
金属間化合物として析出し、合金材の再結晶を抑制し、
微細な結晶粒を作るとともに、強度を向上させるため
に、単独もしくは複数で添加されることがある。ただ
し、これらの添加元素をその上限値より多く添加する
と、鋳造時に巨大な金属間化合物を晶出し、引き続いて
行われる塑性加工において欠陥となる。下限未満の場合
には、結晶粒微細化の効果が小さい。
Zr, Cr, Mn, V: These are precipitated as fine intermetallic compounds during homogenization treatment and suppress recrystallization of the alloy material,
In order to form fine crystal grains and improve the strength, they may be added alone or in plural. However, if these additive elements are added in excess of their upper limits, a huge intermetallic compound will crystallize during casting, resulting in defects in the subsequent plastic working. If it is less than the lower limit, the effect of refining the crystal grains is small.

上記必須成分の外に、本発明合金にはSi、Fe等の不
純物が含まれる。また、鋳造組織の微細化を行うため、
Ti、B等を添加することがある。この効果はTiでは
0.005%より少ない場合には小さく、一方0.10%より多
く添加すると巨大な金属間化合物を晶出する。Bでは0.
02%より多く添加すると、同様に巨大化合物を晶出す
る。
In addition to the above essential components, the alloy of the present invention contains impurities such as Si and Fe. Also, in order to refine the casting structure,
Ti, B, etc. may be added. This effect is
If it is less than 0.005%, it is small, while if it is added more than 0.10%, a huge intermetallic compound is crystallized. 0 for B.
Addition of more than 02% also crystallizes large compounds.

又、製造上の条件の限定理由は下記のとおりである。The reasons for limiting the manufacturing conditions are as follows.

均質化処理:鋳造時にデンドライト間に晶出した濃化相
を溶入化させるために、 480℃以上にする必要がある。
しかしながら、550℃を越えると共晶融解しやすくなる
とともに、酸化も激しくなる。この効果は2時間未満で
は不十分であり、また、48時間を越えても効果は向上
せず、工業的でない。
Homogenization treatment: It is necessary to raise the temperature to 480 ° C or higher in order to infiltrate the concentrated phase crystallized between dendrites during casting.
However, when the temperature exceeds 550 ° C, the eutectic melts easily and the oxidation becomes severe. This effect is insufficient if it is less than 2 hours, and the effect is not improved even if it exceeds 48 hours, which is not industrial.

押出温度: 450℃未満では押出時の変形抵抗が大きくホ
ロー押出がむずかしい。また、 550℃を越えると押出材
の表面が荒れ、割れが入りやすくなり、健全な押出材が
得にくい。
Extrusion temperature: If it is less than 450 ° C, the deformation resistance during extrusion is large and hollow extrusion is difficult. On the other hand, if the temperature exceeds 550 ° C, the surface of the extruded material becomes rough and cracks easily occur, making it difficult to obtain a sound extruded material.

[実施例] 実施例1〜4並びに比較例1〜4 第1表に示す合金をAr雰囲気下において溶解、鋳造し
た。鋳塊の均質化処理を同表に示す条件のもとで行った
後、φ6″のビレットに外削した。次に本鋳塊を同表に
示す温度に予熱し、外周部の一辺40mm、肉厚 3.5mmの角
パイプにホロー押出した。これをソルトバス中で 520
℃、40分間の溶体化処理の後、水冷し、ひずみ矯正の
後、 190℃、24時間の時効処理を行ってT 6材とし
た。
[Examples] Examples 1 to 4 and Comparative Examples 1 to 4 The alloys shown in Table 1 were melted and cast in an Ar atmosphere. After homogenizing the ingot under the conditions shown in the same table, it was externally cut into a φ6 ″ billet. Next, the ingot was preheated to the temperature shown in the same table, and one side of the outer periphery was 40 mm, Hollow extrusion was performed on a square pipe with a wall thickness of 3.5 mm.
After solution treatment at 40 ° C. for 40 minutes, water cooling, strain correction, and aging treatment at 190 ° C. for 24 hours were performed to obtain T 6 material.

第2表にホロー溶着性及び押出方向での引張試験結果を
示す。ホロー溶着性は溶着部断面のミクロ組織観察から
判定した。実施例No.1〜4ではホロー溶着性は良好
であり、またT 6材の引張強さσが45kgf/mm2 程度の
高強度材が得られている。これに対し比較例1ではホロ
ー溶着性は良好であるが、鋳塊均質化が不十分であるば
かりかCu、Mg量が請求範囲の下限値未満のため強度
が低い。比較例2ではMg量が請求範囲の上限を越えて
いるため、ホローの溶着が不十分であり、健全な押出材
でない。引張試験はしなかった。比較例3はLi量が多
いため表面酸化が激しく、また、 550℃を越える温度で
の均質化処理のため鋳塊の一部に共晶融解も認められ、
健全な押出材を得ることができなかった。比較例4は押
出温度が低いため、ホロー溶着性が悪い。
Table 2 shows the results of the hollow weldability and the tensile test in the extrusion direction. The hollow weldability was determined by observing the microstructure of the welded section. Example No. In Nos. 1 to 4, hollow weldability was good, and a high-strength material having a tensile strength σ B of T 6 material of about 45 kgf / mm 2 was obtained. On the other hand, in Comparative Example 1, the hollow weldability is good, but the homogenization of the ingot is insufficient and the strength is low because the amounts of Cu and Mg are less than the lower limit values of the claims. In Comparative Example 2, since the amount of Mg exceeds the upper limit of the claimed range, hollow welding is insufficient and the extruded material is not sound. No tensile test was performed. In Comparative Example 3, since the amount of Li was large, surface oxidation was severe, and eutectic melting was observed in a part of the ingot due to the homogenization treatment at a temperature over 550 ° C.
A sound extruded material could not be obtained. Since Comparative Example 4 has a low extrusion temperature, the hollow weldability is poor.

実施例5〜9並びに比較例5〜8 第3表に示す合金の押出材を実施例1と同様の工程で製
作し、評価した。
Examples 5 to 9 and Comparative Examples 5 to 8 Extruded alloys shown in Table 3 were manufactured in the same process as in Example 1 and evaluated.

第4表にホロー溶着性及び押出方向での引張試験結果を
示す。実施例5〜9ではホロー溶着性は良好であり、ま
たT 6材の引張強さσが50kgf/mm2 程度の高強度材が
得られている。しかし比較例5ではMg量が請求範囲の
下限値未満であるため、強度が低下している。
Table 4 shows hollow weldability and tensile test results in the extrusion direction. In Examples 5 to 9, the hollow weldability is good, and high strength materials having a tensile strength σ B of the T 6 material of about 50 kgf / mm 2 are obtained. However, in Comparative Example 5, since the amount of Mg is less than the lower limit value of the claimed range, the strength is lowered.

比較例6ではLi量、比較例7ではCr量及びZr量が
それぞれ請求範囲の上限を越えたため健全な押出材が得
られなかった、比較例8では押出温度が低すぎたため、
変形抵抗が大きく、溶着部の健全なホロー押出材を得る
ことができなかった。
In Comparative Example 6, the amount of Li, and in Comparative Example 7, the amount of Cr and the amount of Zr exceeded the upper limits of the claims, respectively, so that a sound extruded material could not be obtained. In Comparative Example 8, the extrusion temperature was too low.
It was not possible to obtain a hollow extruded material with a large weld resistance and a good weld resistance.

第5表には既存の JIS H 4100 7NO1合金(Al-4.5%Zn-
1.5%Mg-0.5%Mn)と実施例5〜9の中で最高強度の得
られた実施例7の合金について、比重、弾性係数を比較
したものである。本発明合金では比弾性係数が2割近く
増加しており、例えば二輪車等のフレーム材の薄肉化に
有効と思われる。
Table 5 shows the existing JIS H 4100 7NO1 alloy (Al-4.5% Zn-
1.5% Mg-0.5% Mn) and the alloy of Example 7 having the highest strength among Examples 5 to 9 are compared in specific gravity and elastic modulus. The alloy of the present invention has a specific elastic modulus increased by nearly 20%, which is considered to be effective for thinning the frame material of a motorcycle, for example.

[発明の効果] 本発明によれば、ホロー押出性にすぐれた高強度の形材
の製造が可能であり、例えば2輪車のフレーム等の製造
に最適である。又、Liの添加により比重が低下し、弾
性係数が増加するため、高比弾性係数の材料を得ること
が可能となる。したがって製品を薄肉化できる。
[Effects of the Invention] According to the present invention, it is possible to manufacture a high-strength profile excellent in hollow extrudability, which is optimal for manufacturing a frame of a two-wheeled vehicle, for example. Further, the addition of Li lowers the specific gravity and increases the elastic modulus, so that it is possible to obtain a material having a high specific elastic modulus. Therefore, the product can be made thin.

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】Li: 1.5〜4.0 %、Cu: 0.2〜3.0
%、Mg: 0.2〜2.0 %を必須成分として含み、残りア
ルミニウムと不純物よりなる合金を鋳造した後、 480〜
550 ℃で2〜48時間均質化処理し、ついで 450〜550
℃でホロー押出することを特徴とするホロー押出性にす
ぐれた押出材の製造法。
1. Li: 1.5 to 4.0%, Cu: 0.2 to 3.0
%, Mg: 0.2-2.0% as an essential component, and after casting an alloy consisting of the remaining aluminum and impurities, 480-
Homogenize at 550 ℃ for 2-48 hours, then 450-550
A method for producing an extruded material having excellent hollow extrudability, which comprises performing hollow extrusion at ℃.
【請求項2】Li: 1.5〜4.0 %、Cu: 0.2〜3.0
%、Mg: 0.2〜2.0 %を必須成分として含み、さらに
Zr: 0.05〜0.30%、Cr: 0.05〜0.30%、Mn:
0.05〜1.0 %、V: 0.05〜0.30%のうちの1種以上を
含み、残りアルミニウムと不純物よりなる合金を鋳造し
た後、 480〜550 ℃で2〜48時間均質化処理し、つい
で 450〜550 ℃でホロー押出することを特徴とするホロ
ー押出性にすぐれた押出材の製造法。
2. Li: 1.5 to 4.0%, Cu: 0.2 to 3.0
%, Mg: 0.2 to 2.0% as an essential component, Zr: 0.05 to 0.30%, Cr: 0.05 to 0.30%, Mn:
After casting an alloy containing 0.05 to 1.0% and V: 0.05 to 0.30%, and consisting of the remaining aluminum and impurities, homogenize at 480 to 550 ° C for 2 to 48 hours, and then 450 to 550. A method for producing an extruded material having excellent hollow extrudability, which comprises performing hollow extrusion at ℃.
JP14788A 1988-01-05 1988-01-05 Method for manufacturing extruded material with excellent hollow extrudability Expired - Lifetime JPH0621328B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14788A JPH0621328B2 (en) 1988-01-05 1988-01-05 Method for manufacturing extruded material with excellent hollow extrudability

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP14788A JPH0621328B2 (en) 1988-01-05 1988-01-05 Method for manufacturing extruded material with excellent hollow extrudability

Publications (2)

Publication Number Publication Date
JPH01177341A JPH01177341A (en) 1989-07-13
JPH0621328B2 true JPH0621328B2 (en) 1994-03-23

Family

ID=11465920

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14788A Expired - Lifetime JPH0621328B2 (en) 1988-01-05 1988-01-05 Method for manufacturing extruded material with excellent hollow extrudability

Country Status (1)

Country Link
JP (1) JPH0621328B2 (en)

Also Published As

Publication number Publication date
JPH01177341A (en) 1989-07-13

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