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
JPH0210215B2 - - Google Patents
[go: Go Back, main page]

JPH0210215B2 - - Google Patents

Info

Publication number
JPH0210215B2
JPH0210215B2 JP57079218A JP7921882A JPH0210215B2 JP H0210215 B2 JPH0210215 B2 JP H0210215B2 JP 57079218 A JP57079218 A JP 57079218A JP 7921882 A JP7921882 A JP 7921882A JP H0210215 B2 JPH0210215 B2 JP H0210215B2
Authority
JP
Japan
Prior art keywords
less
impurities
aluminum alloy
laser
weight
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
JP57079218A
Other languages
Japanese (ja)
Other versions
JPS58221255A (en
Inventor
Hiroshi Iinuma
Koichi Takada
Haruyumi Kosuge
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.)
Nippon Light Metal Co Ltd
Original Assignee
Nippon Light Metal 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 Nippon Light Metal Co Ltd filed Critical Nippon Light Metal Co Ltd
Priority to JP7921882A priority Critical patent/JPS58221255A/en
Publication of JPS58221255A publication Critical patent/JPS58221255A/en
Publication of JPH0210215B2 publication Critical patent/JPH0210215B2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Heat Treatment Of Nonferrous Metals Or Alloys (AREA)

Description

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

本発明はレーザー反射鏡用アルミニウム合金素
材およびその製造法に関する。レーザー反射鏡は
コンピユータ用データ入出力装置(レーザープリ
ンタ光デイスク装置など)、価格自動読取装置
(POS)、デジタル・オーデイオ・デイスク
(DAD)および表面検査装置などに重要な機能部
品として使用されており、その素材としてアルミ
ニウム合金、銅、黄銅、ガラスなどが用いられる
が、いずれも素材の表面を平滑に加工したのちに
レーザーに対して高反射率を有する表面処理を施
して使用される。レーザー鏡として用いるにはレ
ーザー光に対する最終的な反射率が90%以上必要
であり、このため素材にもできるだけ優れた平面
精度と表面粗さが要求され、またレーザー光を走
査手段に用いるための回転多面鏡においては高速
回転に耐える機械的強度が求められる。 このレーザー鏡素材としてアルミニウム合金が
用いられる場合、従来はまず素材を精密研削盤も
しくは精密切削旋盤などによつて平面加工を行な
い、次いで素材表面に無電解ニツケルメツキを施
し、最後にラツピング加工が行なわれて来た。し
かしながらこの方法では素材表面に光沢ニツケル
メツキ層を形成させるためのはん雑な工程やラツ
ピングの工程に非常な長時間を要するためにコス
ト高となり、また工程が多段階におよぶために表
面にキズが発生する機会が多くなり、これが製品
の歩留りを低下させる原因となつていた。これら
の問題を回避する方法としてアルミニウム合金素
材をダイヤモンド・バイトによつて超精密切削加
工したのち、表面保護処理を行なつて製品とする
方法があり、これによつて著しく加工費が低減さ
れる。しかしこの方法では機械加工されたアルミ
ニウム合金素材の表面がそのままレーザー光線の
反射面として使用されるために素材そのものに対
してレーザーの反射機能に関する高度の特性が要
求される結果となり、メツキとラツピング加工の
組み合わせによる従来の方法で用いられていたア
ルミニウム合金素材では到底それらの要求特性を
満足することは因難である。ダイヤモンド・バイ
トによる超精密切削加工と表面保護処理との組み
合わせによるレーザー鏡の製造法に用いられるア
ルミニウム合金素材には一般に次のような特性が
要求される。 (1) ダイヤモンド・バイトによる切削性能が優れ
ていること。すなわち刃先の圧縮応力に対して
弾性変形量が少なく、かつ加工変質層が生成し
にくいこと。また加工面に刃先の跡が筋状に残
らないこと。 (2) 加工面の表面粗さが小さく、Rmaxが
0.02μm以下であることが必要。このため結晶
粒界の段差や介在物が加工面上に残留したり、
あるいは刃先によつて切除された跡が凹部とな
つて残留してはならない。 (3) 加工面の平面度が良好であること。特に平板
状の側面を反射鏡面として利用する回転多面鏡
においては上下面の平行度が1μm以下であるこ
とが望ましく、加工歪が残路しにくい素材であ
ること。 (4) レーザー光に対する反射率ができだけ高いこ
と。素材の加工面においては少なくとも87%以
上、好ましくは90%以上の反射率が得られるこ
と。 (5) 回転多面鏡用素材としては毎分2万ないし8
万回転という高速回転において面振動、弾性変
形もしくは塑性変形などによつてレーザー光の
反射機能を低下させることのないように十分な
剛性と強度を有すること。 本発明者らはこのような要求特性を満足しうる
アルミニウム合金素材に関して種々検討をした結
果、ダイヤモンドバイトによる切削加工性に優
れ、介在物や晶出物を最小限に制御しかつ結晶粒
度を最適に調整したことによつて90%附近若しく
はそれ以上の反射率を保有するとともに高速回転
に対しても十分な機械的強度を有するレーザー鏡
用アルミニウム合金およびその製造方法を開発す
ることに成功した。以下にその発明の内容につい
て詳しく述べる。 前記所要特性(2)に示すような良好な表面特性を
得るには粗大な金属間化合物粒子や非金属介在物
粒子を素材中にできるだけ存在しないようにする
ことである。もしもこれらの粒子が存在すると切
削後の表面に突起物として残留したりあるいは切
削によつて脱落た跡が穴状の凹みとなつて表面に
残るためにこの部分でレーザー光の散乱が起る。 このような問題に対処するため(i)アルミニウム
合金の溶湯を孔径10μm以下のろ材を用いてろ過
することにより非金属介在物を除去することが必
要でありまた(ii)不溶性金属間化合物粒子の生成量
を極力抑えるために不溶性金属間化合物を生成す
る元素の存在量を制限しなければならない。即ち
合金中に不純物として含まれる鉄を0.05%以下、
チタンを0.02%以下に、マンガンおよびクロムを
各々0.03%以下としなければならない。またケイ
素については合金の焼鈍時に配合元素であるマグ
ネシウムとの間に粗大な化合物Mg2Siを生じ、こ
れが原因で切削加工時の表面に凹凸部が生ずるの
で0.05%以下とすることが望ましい。 (4)に記した90%附近あるいはそれ以上の反射率
を得るためには前述したように非金属介在物や金
属間化合物の生成を極力抑制することはもとより
であるが、さらにダイヤモンド・バイトによる切
削加工によつて新生面の鏡面状態が化学的変化に
よつて劣化しないようにすることによつて一層そ
の効果が確実なものとなる。即ち鏡面状態の保存
は最終的には表面保護膜の形成によつて成される
が、一般には切削加工時に新生面が空気と接触を
開始した直後から表面の化学的変化が始まるため
の若干の反射率の低下がさけられない。本発明者
らはこのような変化を抑止する方法について種々
検討を重ねた結果、素材中への適量のベリリウム
を添加すると鏡面反射率は一層向上することを見
出した。この場合のベリリウムの添加量は0.001
%未満では効果が少なく、0.01%以上添加しても
効果の増大が期待できず、したがつて0.001%か
ら0.01%の範囲が適当である。 次に所要特性(1),(3)および(5)に記したようなダ
イヤモンド・バイトに対する被削性能や残留応力
特性および高速回転に対する剛性などの機械的強
度特性を得るための検討を行なつた。一般にアル
ミニウム合金の強化機構として広く(i)固溶体硬
化、(ii)時効(析出)効果が利用されている。しか
し(ii)の時効(析出)効果は高い強度が得られる反
面金属間化合物が形成されるために粗大粒子の危
険性が大きく、本目的には適切な強化方法とは言
い難い。そこで本発明においては(i)の固溶体効果
を利用することとした。即ちマグネシウムを2な
いし6%添加し、更に銅の0.02ないし0.25%およ
び悪鉛の0.02ないし0.5%のいずれか一方もしく
は両者を同時に添加することによつて必要とする
被削性能や剛性などの機械的特性を十分に満足で
きることを見出した。この場合に添加するマグネ
シウムは2%未満では十分な強度が得られた難
く、また6%を越えるとβ−Al2Mg3粒子が生成
しやすくなること、熱間加工性が著しく劣ること
などの不都合を生ずる。一方銅および亜鉛につい
ては各々0.02%の下限値未満では十分な機械的強
度が得られず、また各々0.25%および0.5%の上
限値を越えると素材の耐食性を低下させる結果を
招くので各々の上限値以下とすべきである。 強化元素として添加されるマグネシウム、銅、
および亜鉛は各々均一に固溶分布していることが
必要であり、このため合金の鋳塊を熱処理する条
件として400℃以上の温度で2時間以上24時間以
内の加熱処理を行なうのが有効である。加熱温度
が400℃未満であるか、あるいは400℃以上であつ
ても処理時間が2時間に満たない場合には元素の
均一な固溶分散状態が得られず、一方加熱温度が
550℃を越えるか、もしくは550℃以下であつても
熱処理時間が24時間を越えるとマグネシウムの酸
化が著くなり、切削加工面の反射率を低下させる
結果となるので不適当である。 次に前記の熱間加工条件ならびに以下の冷間加
工条件を限定する第2の理由はレーザー反射鏡用
アルミニウム合金素材中における結晶粒度を
100μm以下とすることにある。即ち素材の結晶粒
度が100μmを越えるとダイヤモンド・バイトで切
削した後の表面における粒界段差が著しくなり、
その結果良好な表面精度が得られ難くなる。この
ような粒界段差は結晶粒の大きさと深くかかわつ
ていると同時に同一の圧縮応力に対する素材の弾
性変形量や残留応力、あるいは加工変質層の生成
量などによつても強く影響されるが、本発明にお
けるアルミニウム合金の組成とその熱処理および
加工条件はこれらの諸問題に対しても顕著な効果
を発揮するものである。 次に本発明の効果を実施例によつて示す。 実施例 1 第1表に示す組成を有する合金1から合金14ま
でを各々溶解し、これを孔径10μm以下のフイル
ターを通過させた後、直接水冷半連続鋳造装置に
よつて断面が273mm径の円柱状鋳塊とした。なお
前記14種の合金のうち、合金1から合金6までは
本発明に該当する合金であり、合金7から合金14
までは比較合金である。
The present invention relates to an aluminum alloy material for a laser reflecting mirror and a method for manufacturing the same. Laser reflectors are used as important functional parts in computer data input/output devices (laser printer optical disk devices, etc.), automatic price reading devices (POS), digital audio disks (DAD), and surface inspection devices. The materials used include aluminum alloy, copper, brass, and glass, but all of them are used after processing the surface of the material to make it smooth and then subjecting it to a surface treatment that has a high reflectance to the laser. To be used as a laser mirror, the final reflectance of the laser beam must be 90% or more, and for this reason, the material must have the best possible flatness and surface roughness. A rotating polygon mirror is required to have mechanical strength that can withstand high-speed rotation. When aluminum alloy is used as the material for this laser mirror, conventionally the material is first plane-machined using a precision grinder or precision cutting lathe, then electroless nickel plating is applied to the surface of the material, and finally wrapping is performed. I came. However, this method requires a complicated process to form a glossy nickel plating layer on the surface of the material and the wrapping process takes a very long time, resulting in high costs.Also, since the process involves multiple steps, the surface may be scratched. The number of occurrences has increased, and this has been a cause of lower product yields. To avoid these problems, there is a method of cutting aluminum alloy material with ultra-precision cutting using a diamond cutting tool and then applying surface protection treatment to produce the product.This significantly reduces processing costs. . However, in this method, the surface of the machined aluminum alloy material is used as a reflection surface for the laser beam, so the material itself is required to have advanced characteristics regarding the laser reflection function, and the plating and wrapping processes are difficult. It is difficult to satisfy these required characteristics with the aluminum alloy materials used in the conventional combination method. The aluminum alloy material used in the manufacturing method of laser mirrors, which combines ultra-precision cutting with a diamond cutting tool and surface protection treatment, is generally required to have the following properties. (1) Excellent cutting performance with a diamond cutting tool. In other words, the amount of elastic deformation in response to compressive stress at the cutting edge is small, and a process-affected layer is difficult to form. Also, there should be no traces of the cutting edge left on the machined surface. (2) The surface roughness of the machined surface is small, and Rmax is
Must be 0.02μm or less. As a result, steps and inclusions at grain boundaries may remain on the machined surface,
Also, the cut by the cutting edge must not remain in the form of a recess. (3) The machined surface must have good flatness. In particular, for rotating polygon mirrors that use flat side surfaces as reflective mirror surfaces, it is desirable that the parallelism of the upper and lower surfaces be 1 μm or less, and the material must be difficult to retain machining distortion. (4) The reflectance for laser light should be as high as possible. The processed surface of the material must have a reflectance of at least 87% or more, preferably 90% or more. (5) 20,000 to 8 per minute as a material for rotating polygon mirrors
It must have sufficient rigidity and strength so that the laser light reflection function will not deteriorate due to surface vibration, elastic deformation, or plastic deformation during high-speed rotation of 10,000 rotations. The inventors of the present invention have conducted various studies on aluminum alloy materials that can satisfy these required properties, and have found that they have excellent machinability with a diamond cutting tool, minimize inclusions and crystallized substances, and optimize crystal grain size. We have successfully developed an aluminum alloy for laser mirrors that has a reflectance of around 90% or more and has sufficient mechanical strength even for high-speed rotation by adjusting the reflectance, and a method for manufacturing the same. The content of the invention will be described in detail below. In order to obtain good surface properties as shown in the above-mentioned required property (2), coarse intermetallic compound particles and nonmetallic inclusion particles should be prevented from existing in the material as much as possible. If these particles are present, they will remain as protrusions on the surface after cutting, or the marks left by the cutting will remain on the surface as hole-like depressions, causing laser light scattering in these areas. To deal with these problems, it is necessary (i) to remove nonmetallic inclusions by filtering the molten aluminum alloy using a filter medium with a pore size of 10 μm or less, and (ii) to remove insoluble intermetallic compound particles. In order to suppress the amount of formation as much as possible, the amount of elements that form insoluble intermetallic compounds must be limited. In other words, the iron contained as an impurity in the alloy is 0.05% or less,
Titanium must be kept below 0.02%, and manganese and chromium each below 0.03%. Regarding silicon, a coarse compound Mg 2 Si is formed with magnesium, which is a blended element, during annealing of the alloy, which causes unevenness on the surface during cutting, so it is desirable to limit the content to 0.05% or less. In order to obtain a reflectance of around 90% or higher as described in (4), it is necessary to suppress the formation of non-metallic inclusions and intermetallic compounds as much as possible as described above, but also to prevent the formation of non-metallic inclusions and intermetallic compounds. The effect can be further ensured by preventing the mirror-like state of the new surface from being deteriorated by chemical changes due to the cutting process. In other words, preservation of the mirror-like state is ultimately achieved by the formation of a surface protective film, but in general, chemical changes on the surface begin immediately after the new surface comes into contact with air during cutting, resulting in slight reflections. A decline in the rate cannot be avoided. The inventors of the present invention have conducted various studies on methods for suppressing such changes, and have found that adding an appropriate amount of beryllium to the material further improves the specular reflectance. In this case, the amount of beryllium added is 0.001
If it is less than 0.0%, the effect will be small, and if it is added at 0.01% or more, no increase in effect can be expected. Therefore, a range of 0.001% to 0.01% is appropriate. Next, we conducted a study to obtain the required characteristics (1), (3), and (5) for diamond cutting tools, such as machining performance, residual stress characteristics, and mechanical strength characteristics such as rigidity against high-speed rotation. Ta. In general, (i) solid solution hardening and (ii) aging (precipitation) effects are widely used as strengthening mechanisms for aluminum alloys. However, although the aging (precipitation) effect of (ii) provides high strength, it is difficult to say that it is an appropriate strengthening method for this purpose, because intermetallic compounds are formed and there is a great risk of coarse particles. Therefore, in the present invention, it was decided to utilize the solid solution effect (i). In other words, by adding 2 to 6% magnesium and further adding 0.02 to 0.25% copper and 0.02 to 0.5% bad lead, or both at the same time, the machine can achieve the required machining performance and rigidity. It was found that the characteristics can be fully satisfied. In this case, if the amount of magnesium added is less than 2%, it is difficult to obtain sufficient strength, and if it exceeds 6%, β-Al 2 Mg 3 particles are likely to be generated, and hot workability is significantly deteriorated. causing inconvenience. On the other hand, for copper and zinc, if each is less than the lower limit of 0.02%, sufficient mechanical strength cannot be obtained, and if the upper limits of 0.25% and 0.5% are exceeded, the corrosion resistance of the material will be reduced, so the upper limit of each Should be less than or equal to the value. Magnesium, copper, added as strengthening elements
It is necessary for each of zinc and zinc to be uniformly distributed in solid solution. Therefore, it is effective to heat treat the alloy ingot at a temperature of 400℃ or higher for 2 hours or more and less than 24 hours. be. If the heating temperature is less than 400℃, or if the treatment time is less than 2 hours even if the heating temperature is 400℃ or higher, a uniform solid solution dispersion state of the elements cannot be obtained;
If the temperature exceeds 550°C, or if the heat treatment time exceeds 24 hours even if it is below 550°C, the oxidation of magnesium will become significant, resulting in a decrease in the reflectance of the cut surface, which is inappropriate. Next, the second reason for limiting the above hot working conditions and the following cold working conditions is to limit the crystal grain size in the aluminum alloy material for laser reflecting mirrors.
It is to be 100μm or less. In other words, if the grain size of the material exceeds 100 μm, the grain boundary step on the surface after cutting with a diamond tool becomes significant.
As a result, it becomes difficult to obtain good surface accuracy. These grain boundary steps are closely related to the size of the crystal grains, and at the same time are also strongly influenced by the amount of elastic deformation and residual stress of the material in response to the same compressive stress, and the amount of formed damaged layers. The composition of the aluminum alloy and its heat treatment and processing conditions in the present invention exhibit remarkable effects on these problems. Next, the effects of the present invention will be illustrated by examples. Example 1 Alloys 1 to 14 having the compositions shown in Table 1 were each melted, passed through a filter with a pore size of 10 μm or less, and then cast into a circle with a cross section of 273 mm in diameter using a direct water-cooled semi-continuous casting machine. It was made into a columnar ingot. Of the 14 types of alloys mentioned above, Alloy 1 to Alloy 6 are alloys that fall under the present invention, and Alloy 7 to Alloy 14 are alloys that correspond to the present invention.
The above are comparison alloys.

【表】【table】

【表】 これらの鋳塊に対して各々480℃で12時間加熱
処理を行ない、次いで380℃で直径120mmの丸棒に
熱間押出加工し、さらに断面減少比43%の冷間引
抜きを行なつて直径90mmの丸棒を得た。このよう
にして得られた素材についてまず硬さ、引張り強
度、耐力および伸びなどの機械的性質を測定し、
次に結晶の粒径(最大値)を測定した。またダイ
ヤモンド・バイトを用いて精密切削加工を施した
面について表面粗さ、介在物もしくは晶出物の存
在量、刃先の跡やキズ等の条痕の有無、平行入射
可視光に対する60°反射率を測定し、レーザー反
射鏡としての適性を評価した。 これらの結果を一括して第2表に示したが、本
発明に係る合金はいずれも比較合金に比べてダイ
ヤモンド・バイトによる切削性に優れ、
Rmax0.02μm以下の表面粗さが得られるほか、
切削面上に介在物や晶出物が非常に少なく、88%
以上の反射率が得られるなどレーザー反射鏡とし
ての優れた適性が確認された。
[Table] Each of these ingots was heat treated at 480℃ for 12 hours, then hot extruded at 380℃ into a round bar with a diameter of 120mm, and then cold drawn with a cross-section reduction ratio of 43%. A round bar with a diameter of 90 mm was obtained. First, the mechanical properties of the material obtained in this way, such as hardness, tensile strength, yield strength, and elongation, were measured.
Next, the grain size (maximum value) of the crystals was measured. In addition, the surface roughness, the amount of inclusions or crystallized substances, the presence or absence of marks such as cutting edge marks and scratches, and the 60° reflectance of parallel incident visible light on surfaces that have been precision cut using a diamond cutting tool. were measured to evaluate its suitability as a laser reflector. These results are summarized in Table 2, and the alloys according to the present invention all have superior machinability with a diamond bite compared to comparative alloys.
In addition to achieving surface roughness of Rmax0.02μm or less,
Very few inclusions or crystallized substances on the cutting surface, 88%
The excellent suitability of the mirror as a laser reflector was confirmed as the above reflectance was obtained.

【表】【table】

【表】 実施例 2 実施例1で用いた本発明による合金2および合
金5を溶解し、孔径10μm以下のフイルターによ
るろ過の有無、熱間圧延加工温度および冷間圧延
率などの諸要因が合金板の結晶粒径やダイヤモン
ドバイトによる切削面の表面性状に及ぼす影響を
検討した。この場合の鋳塊の加熱処理は480℃で
16時間行ない、また冷間圧延板の焼鈍は380℃で
1時間行なつた。結果は第3表に示すように本発
明合金を使用し本発明条件で製造した素材(素材
番号2−2および5−2)即ちフイルター処理を
行ない、熱間圧延終了温度が400℃以下、冷間圧
延率が30%以上の条件で製造した素材においては
レーザー反射鏡素材として優れた特性が得られる
ことが判る。
[Table] Example 2 Alloys 2 and 5 according to the present invention used in Example 1 were melted, and various factors such as the presence or absence of filtration with a filter with a pore size of 10 μm or less, hot rolling processing temperature, and cold rolling rate were investigated. The influence of the grain size of the plate and the surface texture of the cut surface by a diamond tool was investigated. In this case, the ingot was heated at 480℃.
The annealing of the cold rolled plate was carried out at 380°C for 1 hour. The results are as shown in Table 3. Materials (material numbers 2-2 and 5-2) manufactured using the invention alloy under the conditions of the invention, i.e. filter treatment, had a hot rolling finish temperature of 400°C or less, and It can be seen that the material manufactured under the conditions of an inter-rolling ratio of 30% or more has excellent properties as a laser reflecting mirror material.

【表】【table】

Claims (1)

【特許請求の範囲】 1 必須元素として重量%でMg2.0〜6.0%を含
み、さらにCu0.02〜0.25%、Zn0.02〜0.5%のうち
いずれか一者または両者を含み、残部Alおよび
不可避的不純物よりなり、不純物としてのMnお
よびCrがそれぞれ0.03%以下、FeおよびSiがそれ
ぞれ0.05%以下、Tiが0.02%以下であり、かつ前
記以外の不純物の合計が0.1%以下であることを
特徴とするレーザー鏡用アルミニウム合金素材。 2 必須元素として重量%でMg2.0〜6.0%を含
み、さらにCu0.02〜0.25%、Zn0.02〜0.5%のうち
いずれか一者または両者を含み、残部Alおよび
不可避的不純物よりなり、不純物としてのMnお
よびCrがそれぞれ0.03%以下、FeおよびSiがそれ
ぞれ0.05%以下、Tiが0.02%以下であり、かつ前
記以外の不純物の合計が0.1%以下であるような
アルミニウム合金溶湯を孔径10μm以下のろ過材
を通過させた後所定の鋳塊に鋳造し、ついでこの
鋳塊を400〜550℃の温度範囲で2〜24時間の加熱
処理を行なつた後、熱間加工終了時の温度が400
℃以下になるようにして熱間加工を行ない、つぎ
に30%以上の加工度となるように冷間加工を行な
い、しかる後焼鈍を行なつて平均結晶粒径が
100μm以下の素材とすることを特徴とするレーザ
ー鏡用アルミニウム合金素材の製造法。 3 必須元素として重量%でMg2.0〜6.0%、
Be0.001〜0.01%を含み、さらにCu0.02〜0.25%、
Zn0.02〜0.5%のうちいずれか一者または両者を
含み、残部Alおよび不可避的不純物よりなり、
不純物としてのMnおよびCrがそれぞれ0.03%以
下、FeおよびSiがそれぞれ0.05%以下、Tiが0.02
%以下であり、かつ前記以外の不純物の合計が
0.1%以下であることを特徴とするレーザー鏡用
アルミニウム合金素材。
[Claims] 1 Contains 2.0 to 6.0% by weight of Mg as an essential element, further contains one or both of Cu 0.02 to 0.25% and Zn 0.02 to 0.5%, and the balance is Al and Consisting of unavoidable impurities, the impurities Mn and Cr are each 0.03% or less, Fe and Si are each 0.05% or less, Ti is 0.02% or less, and the total of impurities other than the above is 0.1% or less. Features aluminum alloy material for laser mirrors. 2 Contains Mg2.0 to 6.0% by weight as an essential element, further contains one or both of Cu0.02 to 0.25% and Zn0.02 to 0.5%, and the remainder consists of Al and inevitable impurities, A molten aluminum alloy containing impurities of 0.03% or less each of Mn and Cr, 0.05% or less each of Fe and Si, and 0.02% or less of Ti, and a total of 0.1% or less of impurities other than the above, is heated to a pore size of 10 μm. After passing through the following filter media, it is cast into a specified ingot, and then this ingot is heat treated at a temperature range of 400 to 550℃ for 2 to 24 hours, and the temperature at the end of hot working is is 400
℃ or less, then cold working to a working degree of 30% or more, and then annealing to reduce the average grain size.
A method for producing an aluminum alloy material for laser mirrors, characterized by making the material 100μm or less. 3 Mg2.0-6.0% by weight as an essential element,
Contains Be0.001~0.01%, further Cu0.02~0.25%,
Contains one or both of Zn0.02 to 0.5%, and the remainder consists of Al and inevitable impurities,
As impurities, Mn and Cr are each 0.03% or less, Fe and Si are each 0.05% or less, and Ti is 0.02%.
% or less, and the total amount of impurities other than those listed above is
An aluminum alloy material for laser mirrors characterized by a content of 0.1% or less.
JP7921882A 1982-05-13 1982-05-13 Aluminum alloy material for laser mirror and its manufacture Granted JPS58221255A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7921882A JPS58221255A (en) 1982-05-13 1982-05-13 Aluminum alloy material for laser mirror and its manufacture

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7921882A JPS58221255A (en) 1982-05-13 1982-05-13 Aluminum alloy material for laser mirror and its manufacture

Related Child Applications (1)

Application Number Title Priority Date Filing Date
JP21612889A Division JPH0639664B2 (en) 1989-08-24 1989-08-24 Manufacturing method of aluminum alloy material for laser mirror

Publications (2)

Publication Number Publication Date
JPS58221255A JPS58221255A (en) 1983-12-22
JPH0210215B2 true JPH0210215B2 (en) 1990-03-07

Family

ID=13683781

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7921882A Granted JPS58221255A (en) 1982-05-13 1982-05-13 Aluminum alloy material for laser mirror and its manufacture

Country Status (1)

Country Link
JP (1) JPS58221255A (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0615699B2 (en) * 1984-12-12 1994-03-02 キヤノン株式会社 Photoconductive member for electrophotography
JPS61179842A (en) * 1985-02-04 1986-08-12 Sumitomo Light Metal Ind Ltd Aluminum alloy for magnetic disc superior in plating property
JPS62133038A (en) * 1985-12-04 1987-06-16 Showa Alum Corp Aluminum alloy having superior machinability to mirror finished surface
JP2624648B2 (en) * 1986-04-01 1997-06-25 株式会社神戸製鋼所 Aluminum alloy for amorphous silicon photoreceptor drum with excellent mirror surface finish
JPS6372848A (en) * 1986-09-16 1988-04-02 Kobe Steel Ltd Aluminum-based alloy sheet for magnetic disk
JPS6376857A (en) * 1986-09-19 1988-04-07 Showa Alum Corp Manufacture of aluminum alloy for mirror finish working
CN112391563B (en) * 2019-08-19 2021-11-09 南京理工大学 Preparation method of layered nano heterogeneous aluminum magnesium alloy block material

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS54107816A (en) * 1978-02-13 1979-08-24 Mitsubishi Heavy Ind Ltd Aluminum alloy for marine propeller

Also Published As

Publication number Publication date
JPS58221255A (en) 1983-12-22

Similar Documents

Publication Publication Date Title
US4431461A (en) Method for producing Al-base alloy substrates for magnetic recording media
JPH0210215B2 (en)
JPS59157255A (en) Aluminum alloy material for ultra-precision mirror finishing
KR0129525B1 (en) Aluminum Alloy for Magnetic Disk Substrates with Excellent Plating
JPH0448859B2 (en)
JPH0252683B2 (en)
JPH02205651A (en) Aluminum alloy for magnetic disk base
JPH02194152A (en) Manufacture of aluminum alloy stock for laser mirror
JPH01225739A (en) Aluminum alloy for magnetic disk substrate
JPH04272150A (en) Aluminum alloy for magnetic disk excellent in grindability
JPS63319143A (en) Plymetal of aluminum alloy for base of magnetic disk
JPS6154854B2 (en)
JPH07195150A (en) Method for casting aluminum alloy for hdd
JPH04341535A (en) Aluminum alloy substrate for high density coating type magnetic disk
JPH0310168B2 (en)
JPH10310836A (en) Aluminum alloy clad plate for high capacity magnetic disk substrate with excellent recyclability and method of manufacturing the same
JPH07331397A (en) Production of aluminum alloy sheet for magnetic disk substrate
US5126179A (en) Disk substrate for magnetic disk
JPH01298134A (en) Aluminum alloy plate for disk having excellent grindability and plating characteristics and its manufacture
JPH02159340A (en) Aluminum alloy sheet for disk having excellent plating characteristics
CN121629231A (en) Aluminum alloy plate for magnetic disk, method for producing the same, aluminum alloy blank for magnetic disk, and aluminum alloy substrate for magnetic disk
JP2000054094A (en) Manufacture of aluminum foil
JPH01225740A (en) Aluminum alloy for magnetic disk substrate
JPH0390528A (en) Aluminum alloy excellent in mirror finishing characteristic
JPH01225741A (en) Aluminum alloy for magnetic disk substrate