Deprecated: The each() function is deprecated. This message will be suppressed on further calls in /home/zhenxiangba/zhenxiangba.com/public_html/phproxy-improved-master/index.php on line 456
JP4124386B2 - Method for producing high-strength aluminum or aluminum alloy rod - Google Patents
[go: Go Back, main page]

JP4124386B2 - Method for producing high-strength aluminum or aluminum alloy rod - Google Patents

Method for producing high-strength aluminum or aluminum alloy rod Download PDF

Info

Publication number
JP4124386B2
JP4124386B2 JP27355998A JP27355998A JP4124386B2 JP 4124386 B2 JP4124386 B2 JP 4124386B2 JP 27355998 A JP27355998 A JP 27355998A JP 27355998 A JP27355998 A JP 27355998A JP 4124386 B2 JP4124386 B2 JP 4124386B2
Authority
JP
Japan
Prior art keywords
rod
aluminum
alloy
strength
twisted
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 - Fee Related
Application number
JP27355998A
Other languages
Japanese (ja)
Other versions
JP2000102818A (en
Inventor
博 穴田
重興 佐治
巌 田中
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.)
Furukawa Sky Aluminum Corp
Sumitomo Electric Toyama Co Ltd
Original Assignee
Furukawa Sky Aluminum Corp
Sumitomo Electric Toyama Co 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 Furukawa Sky Aluminum Corp, Sumitomo Electric Toyama Co Ltd filed Critical Furukawa Sky Aluminum Corp
Priority to JP27355998A priority Critical patent/JP4124386B2/en
Publication of JP2000102818A publication Critical patent/JP2000102818A/en
Application granted granted Critical
Publication of JP4124386B2 publication Critical patent/JP4124386B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Landscapes

  • Metal Extraction Processes (AREA)

Description

【0001】
【発明の属する技術分野】
本発明は、高強度のアルミニウム又はアルミニウム合金棒の製造方法に関するものである。
【0002】
【従来の技術】
アルミニウム又はアルミニウム合金の棒は、軽量、高比強度、高耐食性などの利点を活かして、電気部品、機械部品、二輪車の構造部品、自動車部品、船舶・車両・航空機の構造部材、土木・建築部材などに広く使用されている。また、その断面形状は、丸形をはじめとして、長方形、正方形、正六角形、正八角形などがJISに規定されている。
【0003】
アルミニウム合金の棒としては、非熱処理型合金の場合、▲1▼アルミニウム合金の鋳造ビレットを加熱後、熱間押出により所定の径に押出加工した押出棒と、▲2▼連続鋳造後、直ちにロール圧延により所定の径に熱間圧延加工した連続鋳造圧延棒と、▲3▼押出棒または連続鋳造圧延棒にさらに断面積を減ずるための冷間引抜き加工を施した引抜き棒の三種類がある。押出棒と連続鋳造圧延棒は熱間加工上がりのため強度・硬度が低いが、引抜き棒は冷間加工が施されているため強度・硬度が高いという特徴がある。アルミニウム棒の場合も同様である。
また熱処理型合金の場合は、上記のようにして製造した棒を溶体化処理した後、自然または人工時効処理により強度・硬度を向上させることが行われている。
【0004】
また上記のようにして製造した棒に、必要に応じ、矯正(引張またはロール矯正など)、最終焼鈍、安定化処理加熱が施される場合もある。
【0005】
棒用のアルミニウム又は非熱処理型アルミニウム合金としては、1070、1050、1100などの純アルミニウム、3003などのAl−Mn系合金、5052、5056、5083などのAl−Mg系合金がJISに規定されている。また熱処理型のアルミニウム合金としては、2011、2014、2024、2117などのAl−Cu−(Mg)系合金、6061、6063などのAl−Mg−Si系合金、7003、7N01、7075などのAl−Zn−Mg系合金がJISに規定されている。
【0006】
【発明が解決しようとする課題】
アルミニウム又は非熱処理型アルミニウム合金の高強度棒を得るためには前述のように、断面積を減ずる冷間引抜き加工を施す必要がある。ところが冷間引抜き加工の場合、得ようとする強度・硬度は引抜き加工の減面率の大小で調整することになるため、多水準の強度・硬度の棒を得るためには、穴径の異なる多数の引抜きダイスを用意するか、または穴径の異なる多数の押出ダイスを用意する必要があり、不経済である。特に引抜きダイスは超硬合金で作製されるのが一般的であり、高価であるため、多数のダイスを用意するのは経済的負担が大きい。
【0007】
さらに、Mg添加量の多いAl−Mg系合金の場合は加工硬化性が高いため、一定限度以上の減面率の引抜き加工を行うと、引抜き加工中に割れが発生したり、引抜きに要する力が過大となって加工できなくなるという問題が生じる。この点はJIS規格でも、Mg添加量が2.2 〜2.8 %と少ない5052合金についてはH14、H18の硬質棒が規定されているが、Mg添加量が4.5 〜5.6 %と多い5056合金についてはより加工度(減面率)の小さいH12のみしか規定されていない。これは、Mg添加量の増加にともない、硬質引抜き棒の製造が困難になることを反映したものである。
【0008】
本発明の目的は、かかる問題点に鑑み、引抜きダイスを使用することなく、所望の強度・硬度のアルミニウム又はアルミニウム合金棒を容易に製造できる方法を提供することにある。
【0009】
【課題を解決するための手段】
本発明者等は従来の引抜き加工法以外の棒の加工硬化方法について種々検討した結果、単なるねじり加工では表面荒れが大きく外観上の問題があるが、一方向にねじったものを逆方向にねじり戻すと、表面粗さと外観がねじり前の状態に復元し、しかも表面の硬度、棒の強度が向上することを新たに見いだし、本発明を完成するに至ったものである。
【0010】
すなわち本発明に係る高強度アルミニウム又はアルミニウム合金棒の製造方法は、アルミニウム又はアルミニウム合金の棒を一方向にねじり加工した後、逆方向にねじり戻すことを特徴とするものである(請求項1)。
本発明の製造方法において、一方向にねじる回数と逆方向にねじり戻す回数は実質的に同じにすることが好ましい。
また本発明の製造方法は、アルミニウム合金がAl−Mg系合金である場合に特に効果的である(請求項2)。
【0011】
【発明の実施の形態】
以下、本発明の実施形態を詳細に説明する。
まず素材としてアルミニウム又はアルミニウム合金の棒を用意する。この棒は、押出棒、連続鋳造圧延棒、引抜き棒、およびこれらの棒に焼鈍または安定化処理加熱を施したもののいずれでもよい。アルミニウムとしてはJISに規定されている工業用純アルミニウム、例えば1060(Al純度99.60 %以上)、1050(Al純度99.50 %以上)、1100(Al純度99.00 %以上)などを用いることができる。
【0012】
また、より高い強度が要求される場合は、アルミニウム合金のうちAl−Mg系合金を使用することが好ましい。これは、MgがAlの加工硬化性を向上させる添加元素であり、ねじり戻し後の強度・硬度がより向上するからである。Al−Mg系合金としては、例えばJISに規定されている5005合金(Al−0.50〜1.0 %Mg合金)、5052合金(Al−2.2 〜2.8 %Mg合金)、5454合金(Al−2.4 〜3.0 %Mg合金)、5154合金(Al−3.1 〜3.9 %Mg合金)、5182合金(Al−4.0 〜5.0 %Mg合金)、5083合金(Al−4.0 〜4.9 %Mg合金)、5056合金(Al−4.5 〜5.6 %Mg合金)などがあるが、いずれも本発明に好適な合金である。強度をなるべく向上させたい場合には、5056合金、5083合金、5182合金など、Mg添加量が4%以上と多い合金を使用することが本発明の実施形態としてさらに好ましい。
【0013】
このアルミニウム又はアルミニウム合金の棒に、まず一方向のねじり加工を施す。この一方向ねじり加工は棒の両端をチャックで把持し、一端のチャックを固定し他端のチャックを回転させるか、両端のチャックを互いに逆方向に回転させることにより、棒をねじる装置により実施すればよい。この一方向のねじりを加えただけでも強度向上効果はみられるが、表面粗さが大きくなり、また外観もねじりによるメタルフローが目立ち、実用上好ましくない。
【0014】
上記のようにして一方向にねじられたアルミニウム又はアルミニウム合金の棒を、次に前記一方向のねじり回転数と同じ回転数だけ逆方向にねじり戻すことにより、表面粗さとメタルフローはねじり前の状態にほぼ復元し、外観上はねじり加工を受けたことが全く判別できないほどの状態に戻すことができる。ねじり回転数が多いほどねじり戻した後の強度向上が大きいが、ある限度以上になると効果は飽和し、逆に表面の硬さは低下する。また、さらにねじり回転数を多くすると棒が破断してしまう。最適なねじり回転数は棒の材質、径、長さにより変わるので一概にはいえないが、例えば純アルミニウムの22mmφの丸棒で長さが200 mmの場合、7回程度のねじり・ねじり戻しで表面の硬さは最大となり、13回になると破断する。また破断に至らないまでも6回以上のねじりを加えると、ねじりを戻してもメタルフローが完全には復元しなくなる。したがって本発明の実施に際しては、硬さや表面状態を勘案し、使用目的に合った、ねじり・ねじり戻し回転数を設定すればよい。
【0015】
また上記のねじり・ねじり戻し加工を行った棒に、必要に応じ、矯正(引張またはロール矯正、あるいは軽度の引抜き加工など)、最終焼鈍、安定化処理加熱を常法により施してもよい。
【0016】
このように本発明の製造方法によれば、引抜きダイスを使用することなく所望の強度・硬度のアルミニウム又はアルミニウム合金棒を容易に製造することが可能である。
【0017】
【実施例】
以下、本発明の実施例を説明する。
〔実施例1〕
工業用純アルミニウムの棒(JIS−1060軟化焼鈍材、外径22mmφ、長さ300 mm)を片側回転式捻回試験機(富山住友電工株式会社製)により、チャック間距離200 mm、回転速度25 rpmで、所定の回転数だけ一方向にねじり加工した後、逆方向に同じ回転数だけねじり戻した。その後、表面硬さ、表面粗さの測定と、断面硬さ分布の測定を行った。またねじり戻し棒の強度を測定するため、長さ30mmの円柱を切り出し、圧縮試験を行った。
【0018】
図1は加工前の棒1を示す。棒1には長さ方向に標識線2を付してある。図2(a)は棒1を一方向(+方向)に3回転ねじり加工した状態、同図(b)はその後逆方向(−方向)に3回転ねじり戻した状態を示す。図3(a)は棒1を一方向に6回転ねじり加工した状態、同図(b)はその後逆方向に6回転ねじり戻した状態を示す。図4は棒1を一方向に12回転ねじり加工した後、逆方向に12回転ねじり戻した状態を示す。
【0019】
図2(a)、図3(a)によれば、一方向のねじりでは標識線2が一定ピッチのらせん状に見える。またこの状態ではメタルフローの筋3が見え、この筋3もらせん状になっているのが分かる。これをねじり戻すと、±3回転では図2(b)のように標識線2がほぼ直線に戻る。また±6回転では図3(b)のように標識線2が若干波打つようになるが、全体としては長さ方向に向いている。ところが±12回転になると、図4のように標識線Mが大きく不規則にねじれてしまい、元には戻らないことがわかる。
【0020】
図5は、ねじり加工前焼鈍材と、一方向ねじり加工材と、一方向ねじり後ねじり戻し加工材の表面粗さを示す。▲3▼の一方向ねじり加工材では表面粗さがかなり大きくなっているが、▲2▼、▲4▼のねじり戻し加工材では表面粗さが加工前の状態近くに復元している。ただし▲5▼のようにねじり回転数が±12回転と過大になると、表面粗さはねじり戻しをしても復元しなくなる。
【0021】
図6は一方向ねじり後ねじり戻しした棒の断面の硬さ分布を測定した結果を示す。棒の中心部の硬さは焼鈍材と大差ないが、表面に近づくに従い次第に硬さが増大し、またねじり回転数の増加とともに硬さが増大していることがわかる。
【0022】
図7は棒から30mmの長さに切り出した円柱試料の圧縮試験結果を示す。加工前焼鈍材(C)は0.2 %耐力が23.58 MPaであるのに対し、ねじり回転数が±6回転のねじり加工材は0.2 %耐力が125.9 MPaと顕著に増加していることがわかる。これは引抜き加工棒のH18の強度に相当する。
【0023】
〔実施例2〕
次にAl−Mg系合金についての実施例を説明する。JIS−5056合金の棒(焼鈍材、外径22mmφ、長さ300 mm)に対し、実施例1と同様に片側回転式捻回試験機により、チャック間距離200 mm、回転速度25 rpmで、±3回転のねじり・ねじり戻し加工を施した。その後、試料を切断して断面の硬さ分布の測定を行った。その結果、表面近傍のビッカース硬さは123 に達した。加工前焼鈍材のビッカース硬さは73であったので、大幅な強度の向上がみられた。Al−Mg系合金は引抜き加工法では高強度材を製造することが困難なため、棒材としてのJIS規格は存在しないが、この硬さを参考までに板材のJIS規格と比較すると、H18(またはH38)硬質材に相当するものである。また外観上のメタルフロー、表面粗さも加工前と同等であり、全く問題のないものであった。
【0024】
以上説明したように本発明の製造方法によれば、高価な引抜きダイスを使用することなく、高強度・高硬度のアルミニウム又はアルミニウム合金を容易に製造することができ、特に多品種少量生産において経済的効果が大きい。さらに従来の引抜き加工では製造そのものが困難であったMg添加量の多いAl−Mg系合金硬質棒を容易に製造することができる。
【図面の簡単な説明】
【図1】 標識線を付けたねじり加工前の棒を示す側面図。
【図2】 (a)は図1の棒を一方向に3回転ねじったときの標識線の状態、(b)はその後逆方向に3回転ねじり戻したときの標識線の状態を示す側面図。
【図3】 (a)は図1の棒を一方向に6回転ねじったときの標識線の状態、(b)はその後逆方向に6回転ねじり戻したときの標識線の状態を示す側面図。
【図4】 図1の棒を一方向に12回転ねじった後、逆方向に12回転ねじり戻したときの標識線の状態を示す側面図。
【図5】 ねじり加工前の棒と、本発明の方法によりねじり加工した棒の表面粗さを示すグラフ。
【図6】 ねじり加工前の棒と、本発明の方法によりねじり加工した棒の断面の硬さの分布を示すグラフ。
【図7】 ねじり加工前の棒と、本発明の方法によりねじり加工した棒の圧縮強度を示すグラフ。
【符号の説明】
1:アルミニウム棒
2:標識線
3:メタルフローの筋
[0001]
BACKGROUND OF THE INVENTION
The present invention relates to a method for producing high-strength aluminum or aluminum alloy rods.
[0002]
[Prior art]
Aluminum or aluminum alloy rods make use of advantages such as light weight, high specific strength, and high corrosion resistance. Electrical parts, mechanical parts, structural parts of motorcycles, automotive parts, structural parts of ships, vehicles, and aircraft, civil engineering and building parts Widely used in Moreover, the cross-sectional shape is prescribed | regulated by JIS, such as a round shape, a rectangle, a square, a regular hexagon, a regular octagon.
[0003]
As the aluminum alloy rod, in the case of a non-heat treatment type alloy, (1) an aluminum alloy cast billet is heated and then extruded to a predetermined diameter by hot extrusion, and (2) a roll immediately after continuous casting. There are three types: continuous cast and rolled rods that are hot rolled to a predetermined diameter by rolling, and (3) drawn rods that have been subjected to cold drawing to further reduce the cross-sectional area of the extruded rod or continuous cast and rolled rod. Extruded bars and continuous cast rolled bars have low strength and hardness due to hot working, but the drawn bars are characterized by high strength and hardness because they are cold worked. The same applies to the case of an aluminum rod.
In the case of a heat-treatable alloy, the strength and hardness are improved by natural or artificial aging treatment after solution treatment of the rod produced as described above.
[0004]
Further, the rod manufactured as described above may be subjected to correction (such as tension or roll correction), final annealing, and stabilization treatment heating as necessary.
[0005]
As aluminum for rods or non-heat-treatable aluminum alloys, pure aluminum such as 1070, 1050 and 1100, Al—Mn alloys such as 3003, and Al—Mg alloys such as 5052, 5056 and 5083 are prescribed in JIS. Yes. Examples of heat-treatable aluminum alloys include Al-Cu- (Mg) alloys such as 2011, 2014, 2024, and 2117, Al-Mg-Si alloys such as 6061 and 6063, and Al-- such as 7003, 7N01, and 7075. A Zn—Mg alloy is defined in JIS.
[0006]
[Problems to be solved by the invention]
In order to obtain a high-strength rod of aluminum or non-heat-treatable aluminum alloy, it is necessary to perform cold drawing to reduce the cross-sectional area as described above. However, in the case of cold drawing, the strength and hardness to be obtained are adjusted according to the reduction in area of the drawing, so in order to obtain a bar with multiple levels of strength and hardness, the hole diameter is different. It is uneconomical to prepare a large number of drawing dies or a large number of extrusion dies having different hole diameters. In particular, the drawing dies are generally made of cemented carbide and are expensive, and it is expensive to prepare a large number of dies.
[0007]
Furthermore, in the case of an Al-Mg alloy with a large amount of Mg added, work hardenability is high, so if drawing with a surface area reduction rate above a certain limit, cracking occurs during drawing or the force required for drawing. There is a problem that machining becomes impossible due to excessively large thickness. In this regard, even in the JIS standard, hard rods of H14 and H18 are defined for the 5052 alloy with a small Mg addition of 2.2 to 2.8%, but the 5056 alloy with a large Mg addition of 4.5 to 5.6% is more processed. Only H12 having a small degree (area reduction rate) is defined. This reflects that it becomes difficult to manufacture a hard drawn rod as the amount of Mg added increases.
[0008]
In view of such problems, an object of the present invention is to provide a method capable of easily producing aluminum or an aluminum alloy rod having desired strength and hardness without using a drawing die.
[0009]
[Means for Solving the Problems]
As a result of various studies on work hardening methods for rods other than the conventional drawing method, the present inventors have found that surface roughness is large in mere twisting and there is a problem in appearance, but twisting in one direction is twisted in the opposite direction. When restored, the present invention has been completed by newly finding that the surface roughness and appearance are restored to the state before twisting, and the surface hardness and strength of the rod are improved.
[0010]
That is, the method for producing a high-strength aluminum or aluminum alloy rod according to the present invention is characterized by twisting an aluminum or aluminum alloy rod in one direction and then twisting it back in the opposite direction (Claim 1). .
In the production method of the present invention, it is preferable that the number of times of twisting in one direction and the number of times of twisting back in the opposite direction are substantially the same.
The production method of the present invention is particularly effective when the aluminum alloy is an Al—Mg alloy (claim 2).
[0011]
DETAILED DESCRIPTION OF THE INVENTION
Hereinafter, embodiments of the present invention will be described in detail.
First, an aluminum or aluminum alloy rod is prepared as a material. This rod may be any of an extruded rod, a continuous cast rolled rod, a drawn rod, and those obtained by annealing or stabilizing treatment heating. As aluminum, industrially pure aluminum prescribed in JIS, for example, 1060 (Al purity 99.60% or more), 1050 (Al purity 99.50% or more), 1100 (Al purity 99.00% or more), or the like can be used.
[0012]
Moreover, when higher strength is required, it is preferable to use an Al—Mg alloy among aluminum alloys. This is because Mg is an additive element that improves the work hardenability of Al, and the strength and hardness after untwisting are further improved. Examples of the Al-Mg alloy include 5005 alloy (Al-0.50 to 1.0% Mg alloy), 5052 alloy (Al-2.2 to 2.8% Mg alloy), and 5454 alloy (Al-2.4 to 3.0%) defined in JIS. Mg alloy), 5154 alloy (Al-3.1 to 3.9% Mg alloy), 5182 alloy (Al-4.0 to 5.0% Mg alloy), 5083 alloy (Al-4.0 to 4.9% Mg alloy), 5056 alloy (Al-4.5 to 5.6% Mg alloy) and the like are all suitable for the present invention. In order to improve the strength as much as possible, it is more preferable as an embodiment of the present invention to use an alloy having a large amount of Mg addition of 4% or more, such as 5056 alloy, 5083 alloy, and 5182 alloy.
[0013]
The aluminum or aluminum alloy bar is first twisted in one direction. This one-way twisting process is performed by a device that twists the rod by holding both ends of the rod with a chuck and fixing the chuck at one end and rotating the chuck at the other end, or rotating the chucks at both ends in opposite directions. That's fine. Even if this unidirectional twist is applied, the effect of improving the strength can be seen, but the surface roughness becomes large, and the metal flow due to the twist is conspicuous, which is not preferable in practice.
[0014]
The aluminum or aluminum alloy rod twisted in one direction as described above is then twisted back in the opposite direction by the same number of rotations as the one-way torsional rotation, so that the surface roughness and metal flow are It is almost restored to the state, and it can be returned to a state where it cannot be determined at all that it has undergone twisting. The greater the torsional rotational speed, the greater the improvement in strength after untwisting, but the effect is saturated when the value exceeds a certain limit, and the surface hardness decreases. Further, if the number of torsional rotations is further increased, the rod will break. The optimum number of torsional rotations varies depending on the material, diameter, and length of the rod. However, for example, when a 22 mmφ round rod of pure aluminum is 200 mm long, it can be twisted and untwisted about 7 times. The surface has the maximum hardness and breaks after 13 times. If the twist is applied six times or more before the breakage occurs, the metal flow is not completely restored even if the twist is restored. Therefore, in implementing the present invention, it is only necessary to set the number of rotations for twisting and untwisting according to the purpose of use in consideration of the hardness and the surface condition.
[0015]
Further, the rod subjected to the twisting / twisting processing may be subjected to straightening (tensile or roll straightening, mild drawing processing, etc.), final annealing, and stabilization treatment heating according to a conventional method.
[0016]
As described above, according to the manufacturing method of the present invention, it is possible to easily manufacture aluminum or an aluminum alloy rod having a desired strength and hardness without using a drawing die.
[0017]
【Example】
Examples of the present invention will be described below.
[Example 1]
A pure aluminum rod for industrial use (JIS-1060 soft annealed material, outer diameter 22mmφ, length 300mm) with a single-side rotary twist tester (manufactured by Toyama Sumitomo Electric Co., Ltd.) with a chuck distance of 200mm and a rotational speed of 25 After twisting in one direction at a predetermined number of revolutions at rpm, it was twisted back in the opposite direction by the same number of revolutions. Then, the measurement of surface hardness and surface roughness and the measurement of cross-sectional hardness distribution were performed. Further, in order to measure the strength of the untwisting rod, a 30 mm long cylinder was cut out and subjected to a compression test.
[0018]
FIG. 1 shows the rod 1 before processing. The bar 1 is provided with a marker line 2 in the length direction. 2A shows a state in which the rod 1 is twisted three times in one direction (+ direction), and FIG. 2B shows a state in which the rod 1 is twisted back three times in the opposite direction (− direction). FIG. 3A shows a state in which the rod 1 has been twisted six times in one direction, and FIG. 3B shows a state in which the rod 1 has been twisted six times in the opposite direction. FIG. 4 shows a state in which the rod 1 is twisted 12 turns in one direction and then twisted back 12 turns in the opposite direction.
[0019]
According to FIGS. 2 (a) and 3 (a), the marker line 2 looks like a spiral with a constant pitch when twisted in one direction. Further, in this state, the metal flow streak 3 is seen, and it can be seen that the streak 3 is also spiral. When this is twisted back, the marker line 2 returns to a substantially straight line as shown in FIG. In addition, at ± 6 rotations, the marker line 2 is slightly waved as shown in FIG. 3B, but as a whole, it is directed in the length direction. However, when the rotation is ± 12, the marker line M is greatly irregularly twisted as shown in FIG. 4 and cannot be restored.
[0020]
FIG. 5 shows the surface roughness of the pre-twisted annealed material, the unidirectional twisted material, and the unidirectional twisted untwisted material. (3) The surface roughness of the one-way twisted material is considerably large, but the surface roughness of the twisted-back processed materials (2) and (4) is restored to the state before the processing. However, if the torsional rotational speed is excessively ± 12 as in (5), the surface roughness will not be restored even after twisting back.
[0021]
FIG. 6 shows the result of measuring the hardness distribution of the cross-section of the bar that was twisted back after unidirectional twisting. Although the hardness of the center part of the rod is not much different from that of the annealed material, it can be seen that the hardness gradually increases as it approaches the surface, and that the hardness increases as the torsional rotational speed increases.
[0022]
FIG. 7 shows the compression test results of a cylindrical sample cut out to a length of 30 mm from the rod. It can be seen that the annealed material (C) before processing has a 0.2% yield strength of 23.58 MPa, whereas the torsion processed material with a torsional rotational speed of ± 6 turns has a markedly increased 0.2% yield strength of 125.9 MPa. This corresponds to the strength of H18 of the drawn rod.
[0023]
[Example 2]
Next, examples of the Al—Mg alloy will be described. For a JIS-5056 alloy rod (annealed material, outer diameter 22 mmφ, length 300 mm), a single-side rotary twist tester was used in the same manner as in Example 1 with a chuck distance of 200 mm and a rotational speed of 25 rpm. Three rotations were twisted and untwisted. Thereafter, the sample was cut and the hardness distribution of the cross section was measured. As a result, the Vickers hardness near the surface reached 123. Since the Vickers hardness of the annealed material before processing was 73, a significant improvement in strength was observed. Since it is difficult to produce a high-strength material with an aluminum-Mg based alloy, there is no JIS standard as a bar material. Compared to the JIS standard for a plate material for reference, this hardness is H18 ( Or H38) It corresponds to a hard material. Also, the metal flow and surface roughness on the appearance were the same as before processing, and there were no problems at all.
[0024]
As described above, according to the manufacturing method of the present invention, it is possible to easily manufacture high-strength and high-hardness aluminum or an aluminum alloy without using an expensive drawing die, and it is economical especially in a variety of small-quantity production. Great effect. Furthermore, it is possible to easily produce an Al—Mg alloy hard bar with a large amount of Mg added, which was difficult to produce by conventional drawing.
[Brief description of the drawings]
FIG. 1 is a side view showing a rod before twisting with a marker line.
2A is a side view showing a state of a marker line when the rod of FIG. 1 is twisted three times in one direction, and FIG. 2B is a side view showing a state of the marker line when the rod is twisted back three times in the opposite direction thereafter. .
3A is a side view showing the state of the marker line when the rod of FIG. 1 is twisted six turns in one direction, and FIG. 3B is a side view showing the state of the marker line when the rod is twisted back six times in the opposite direction. .
4 is a side view showing a state of a marker line when the rod of FIG. 1 is twisted 12 times in one direction and then twisted back 12 times in the opposite direction.
FIG. 5 is a graph showing the surface roughness of a bar before twisting and a bar twisted by the method of the present invention.
FIG. 6 is a graph showing the hardness distribution of the cross section of the rod before twisting and the rod twisted by the method of the present invention.
FIG. 7 is a graph showing the compressive strength of a bar before twisting and a bar twisted by the method of the present invention.
[Explanation of symbols]
1: Aluminum rod 2: Marking line 3: Metal flow streaks

Claims (2)

アルミニウム又はアルミニウム合金の棒を一方向にねじり加工した後、逆方向にねじり戻すことを特徴とする高強度アルミニウム又はアルミニウム合金棒の製造方法A method for producing a high-strength aluminum or aluminum alloy rod, characterized by twisting an aluminum or aluminum alloy rod in one direction and then twisting it back in the opposite direction アルミニウム合金がAl−Mg系合金であることを特徴とする請求項1記載の高強度アルミニウム合金棒の製造方法。The method for producing a high-strength aluminum alloy rod according to claim 1, wherein the aluminum alloy is an Al-Mg alloy.
JP27355998A 1998-09-28 1998-09-28 Method for producing high-strength aluminum or aluminum alloy rod Expired - Fee Related JP4124386B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP27355998A JP4124386B2 (en) 1998-09-28 1998-09-28 Method for producing high-strength aluminum or aluminum alloy rod

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP27355998A JP4124386B2 (en) 1998-09-28 1998-09-28 Method for producing high-strength aluminum or aluminum alloy rod

Publications (2)

Publication Number Publication Date
JP2000102818A JP2000102818A (en) 2000-04-11
JP4124386B2 true JP4124386B2 (en) 2008-07-23

Family

ID=17529503

Family Applications (1)

Application Number Title Priority Date Filing Date
JP27355998A Expired - Fee Related JP4124386B2 (en) 1998-09-28 1998-09-28 Method for producing high-strength aluminum or aluminum alloy rod

Country Status (1)

Country Link
JP (1) JP4124386B2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1310711C (en) * 2005-04-19 2007-04-18 哈尔滨工业大学 Reverse temperature field extrusion process for producing microcrystal magnesium alloy
JP2007084889A (en) * 2005-09-22 2007-04-05 Aisin Seiki Co Ltd Aluminum alloy and method for producing the same
CN119411038B (en) * 2025-01-07 2025-03-11 湖南乾龙新材料有限公司 A production process for 7xxx aluminum alloy coils with high cold upsetting formability

Also Published As

Publication number Publication date
JP2000102818A (en) 2000-04-11

Similar Documents

Publication Publication Date Title
US11517952B2 (en) Shear assisted extrusion process
JP3592310B2 (en) Magnesium-based alloy wire and method of manufacturing the same
AU655326B2 (en) Method and apparatus for wire drawing
JP3597186B2 (en) Magnesium-based alloy tube and method of manufacturing the same
Eftekhari et al. Hot tensile deformation behavior of Mg-Zn-Al magnesium alloy tubes processed by severe plastic deformation
EP3362581B1 (en) Aluminum-iron-zirconium alloys
JP7658921B2 (en) Aluminum alloys, aluminum alloy wires, aluminum alloy members, and bolts
US5123973A (en) Aluminum alloy extrusion and method of producing
JP2004353067A (en) Magnesium-based alloy formed body manufacturing method
JP4124386B2 (en) Method for producing high-strength aluminum or aluminum alloy rod
EP1063313B1 (en) Steel wire and method of manufacturing the same
JP6112438B1 (en) Aluminum alloy wire, aluminum alloy stranded wire, covered wire, and wire with terminal
Kulczyk et al. The effect of high-pressure plastic forming on the structure and strength of AA5083 and AA5754 alloys intended for fasteners
CA2050208C (en) Manufacturing process for products with very high fracture loads from unstable austenitic steel and use thereof
US5571349A (en) Method of producing twisted aluminum articles
Rassa et al. Effects of Equal Channel Angular Pressing (ECAP) Process with an Additional Expansion-Extrusion Stage on Microstructure and Mechanical Properties of Mg–, 9Al–, 1Zn
JPH09216004A (en) Pure titanium thin plate for press forming and method for producing the same
JP3273686B2 (en) Manufacturing method of steel cord for rubber reinforcement
KR20240019227A (en) Base material for screw, screw and manufacturing method thereof
JPH0716729A (en) High tensile composite wire
Loginov et al. Accumulation of deformation in the winding circuit
JP2593207B2 (en) High-strength steel wire and steel cord for reinforcing rubber products
JP2004052043A (en) METHOD OF PRODUCING Al-Si BASED ALLOY MATERIAL HAVING FINE STRUCTURE
JPH0313302B2 (en)
JP4987640B2 (en) Titanium alloy bar wire for machine parts or decorative parts suitable for manufacturing cold-worked parts and method for manufacturing the same

Legal Events

Date Code Title Description
A711 Notification of change in applicant

Free format text: JAPANESE INTERMEDIATE CODE: A712

Effective date: 20040202

RD02 Notification of acceptance of power of attorney

Free format text: JAPANESE INTERMEDIATE CODE: A7422

Effective date: 20040226

A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20050902

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20060404

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20080501

A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20080501

R150 Certificate of patent or registration of utility model

Free format text: JAPANESE INTERMEDIATE CODE: R150

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20110516

Year of fee payment: 3

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20120516

Year of fee payment: 4

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20130516

Year of fee payment: 5

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

LAPS Cancellation because of no payment of annual fees