JPH0252683B2 - - Google Patents
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- Publication number
- JPH0252683B2 JPH0252683B2 JP3023283A JP3023283A JPH0252683B2 JP H0252683 B2 JPH0252683 B2 JP H0252683B2 JP 3023283 A JP3023283 A JP 3023283A JP 3023283 A JP3023283 A JP 3023283A JP H0252683 B2 JPH0252683 B2 JP H0252683B2
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- JP
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- Prior art keywords
- aluminum alloy
- impurities
- alloy
- laser
- mirror
- 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
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- Mechanical Optical Scanning Systems (AREA)
- Heat Treatment Of Nonferrous Metals Or Alloys (AREA)
Description
本発明はレーザー反射鏡に用いられる精密鏡面
加工用アルミニウム合金素材の製造法に関するも
のである。
レーザースキヤナー用回転多面鏡等レーザー反
射鏡としてアルミニウム合金素材を用いる場合、
従来一般に耐食性、被削性、強度等のすぐれた
Al−Si−Mg系合金素材を精密研削盤若しくは精
密切削旋盤などによつて平面加工を行ない次いで
素材表面にニツケルメツキを施し、最後にポリシ
ングを施こすことによつてつくられていた。しか
し乍らこの方法ではメツキやポリシングに非常に
長時間を要し、また操作もはん雑であるために表
面キズの発生する機会が多く、これが製品歩留を
低下させ、コスト高の原因となつている。
このような鏡面加工法における欠点を改善する
ためにダイヤモンドバイトによる超精密切削加工
した後、表面保護被膜処理を行つて鏡面とする方
法が開発された。
この方法は素材表面にメツキやポリシング等の
はん雑な操作を行なう必要がなく、また加工時間
も短縮できるなどすぐれた鏡面仕上法であるが仕
上げられた素材面がそのまゝレーザー光の反射面
として機能しなければならないため、従来用いら
れたアルミニウム合金素材ではその要求特性を満
すことができない。
即ち、レーザー反射鏡の鏡面としては表面あら
さ(Rmax)0.03μm以下、平面精度(平面うね
りの高低)0.1μm以下で局部的なビツトやスクラ
ツチがない極めて高度の反射機能を有するものが
要求される。
またさらに、この材料をレーザースキヤナー用
の回転多面反射鏡に用いるなどの場合には、鏡体
を毎分数万回という高速回転を行なわせる関係
上、弾性変形もしくは塑性変形によつて反射機能
が低下しないような強度と剛性を有することが必
要である。
発明者らはダイヤモンドバイト等による超精密
旋削を施こして直ちにこれをレーザー反射鏡素材
として使用が可能なアルミニウム合金素材の製造
法について研究検討を重ねた結果本発明を完成し
たものであつて、本発明は重量でマグネシウム2
〜6%を含み、残部アルミニウムおよび不純物か
らなり、不純物の含有許容限界量が鉄0.15%、珪
素0.05%、銅0.25%、亜鉛0.50%、マンガン1.0
%、クロム0.05%、ジルコニウム0.10%、、チタ
ン0.02%およびその他の不純物の合計0.10%であ
るアルミニウム合金溶湯を孔径10μm以下の過
材を通過させた後、300℃/秒以上の冷却速度で
凝固が行われるように鋳造して鋳塊をつくり、こ
の鋳塊を常法に従つて溶体化処理、熱間、冷間圧
延または直ちに冷間圧延を行つて所定の厚みに加
工し、最終的に焼鈍することを特徴とするもので
ある。
即ち、発明者らの検討によるとレーザー反射鏡
として要求される諸特性のうち強度剛性や反射機
能を満足するアルミニウム合金系としてはマグネ
シウムを2〜6%含む固溶強化型のアルミニウム
−マグネシウム合金が適当であることが判つた。
しかし乍ら一般市販規格のアルミニウム−マグ
ネシウム合金によつてつくられた素材を用いてダ
イヤモンドバイト等による精密切削加工を施した
場合において、素材加工面に先に述べたような高
度の平滑度とそれに伴う反射機能を付与するため
には種々の問題点が存在した。
即ち、市販規格のアルミニウム合金素材中には
種々の不純物金属元素に基づく不溶性金属間化合
物粒子や、工程中で混入する非金属介在物粒子が
存在し、これらの介在物の多くは合金マトリツク
スより硬質であるために介在物粒子が仕上後の表
面に突起物として残留したり、あるいは切削など
に際して脱落してピツトやスクラツチを生じたり
するために、この部分で投射光の散乱が起り、正
確で鮮明な反射像をうることが極めて困難であつ
た。
発明者らは合金素材中に含有されるこれら介在
物が素材鏡面仕上後のレーザー光に対する反射機
能におよぼす影響について詳細に検討を行つた結
果、不溶性金属間化合物粒子の大きさが2μm以下
であればレーザー反射鏡として良好な反射面を形
成しうること、即ち、合金溶湯を10μm以下の孔
径の過材で一回乃至数回過し非金属介在物を
除去するだけでなく、不溶性金属間化合物を生成
する元素の存在量を限度量まで制限した上で過
後の溶湯を300℃/秒以上の冷却速度で凝固する
ように鋳造することによつて素材中に含まれる不
溶性金属間化合物の量を僅少にとどめ、且つその
粒径をば2μm以下にすることに成功した。
本発明によつて得られた合金素材はダイヤモン
ドバイトによる被削性がすぐれているうえに被削
面の平滑度も良好で、反射率をほゞ90%以上にす
ることができ、また反射像の鮮明度も高いのでレ
ーザー反射鏡、特にレーザースキヤナー用回転多
面鏡としてすぐれた性能を有するものである。
本発明において合金元素としてのマグネシウム
を2〜6%と定めた理由はマグネシウム2%以下
では十分な強度とダイヤモンドバイトによる良好
な被削性がえられず、また6%を超えると合金組
織中にβAl−Mg金属間化合物を生じ、これが合
金の加工性を低下し、またこの化合物が2μm以上
の粗粒となつて鏡面の反射機能を低下させる。
本発明においては特に合金中に不溶性金属間化
合物を生ずるような金属不純物元素の含有量規制
が重要であることは前述した。即ち、これらの金
属元素としては鉄、珪素、クロム、マンガン、ジ
ルコニウム、チタンが挙げられるが、これらの元
素の最大含有許容量を鉄0.15%、珪素0.05%、ク
ロム0.05%、マンガン1.0%、ジルコニウム0.10
%、チタン0.02%に制限する理由は、各元素が上
記制限量以上あると300℃/秒以上の冷却速度で
溶湯を冷却凝固しても不溶性金属間化合物粒子の
大きさが2μm超えレーザー反射鏡としての機能を
達成できなくなるからである。
本発明は上記組成のアルミニウム−マグネシウ
ム合金溶湯を10μmの孔径を有するフイルターを
通過させて、非金属介在物を除去した後、300
℃/秒以上の冷却速度で凝固されるように鋳造し
て鋳塊とする。このような大きな冷却速度で合金
溶湯を凝固させるときは鋳塊は極めて急速に冷却
され不溶性金属間化合物の析出量も少く、またそ
の粒径も2μm以下にとどめることができる。
このようにして得られた鋳塊は直ちに所定の厚
さまで冷延するか、または400〜550℃で2〜24時
間焼鈍した後熱間圧延および冷間圧延を加えて所
望の厚さの冷延板とした後、最終的に300〜550℃
に0.5〜5時間焼鈍を施して歪取りを行つてレー
ザー反射鏡用素材に供する。
なお、最終焼鈍に際して焼鈍温度を500〜550℃
とし、且つ焼鈍後250℃までの冷却を100℃/分以
上の冷却速度とするときは素材反射率をさらに2
〜3%向上させることができるのでより好まし
い。
次に本発明の実施例を述べる。
実施例 1
第1表に示す合金組成を有する試料番号1〜14
までのアルミニウム−マグネシウム合金溶湯を孔
径10μmの多孔質黒鉛フイルターで過した後、
350℃/秒の冷却速度で凝固させて厚さ8μmの板
状鋳塊に鋳造した後、6mm厚さまで冷間圧延を施
し、次いでこの冷延板を420℃で4時間の焼鈍を
行つた。
このようにして得られた素材について機械的性
質、結晶粒径および不溶性金属間化合物の粒径測
定を行つた。
また更にこの素材をダイヤモンドバイトを用い
て精密切削加工を施して鏡面仕上を施こし、表面
粗さ、刃先跡、キズ等の条痕の有無およびレーザ
ー入射光に対する60゜反射率ならびに反射像の鮮
明度測定を行なつて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
す。
尚、適正評価に際し2μm以上の晶出物、介在物
の存在の有無、刃先跡目、表面キズの有無につい
ては顕微鏡(倍率400倍)により、また表面粗さ
については触針式表面あらさ計による測定を、反
射能の測定については2mW可視光領域のレーザ
ー光(He−Neレーザー:λ=632.8nm)の照射
による60゜反射率と反射像の形状の測定によつた。
The present invention relates to a method of manufacturing an aluminum alloy material for precision mirror finishing used in a laser reflecting mirror. When using aluminum alloy material as a laser reflecting mirror such as a rotating polygon mirror for a laser scanner,
In the past, materials with excellent corrosion resistance, machinability, strength, etc.
It was made by flattening an Al-Si-Mg alloy material using a precision grinder or precision cutting lathe, then applying nickel plating to the surface of the material, and finally polishing. However, with this method, plating and polishing take a very long time, and the operations are complicated, so there are many chances for surface scratches to occur, which reduces product yield and causes high costs. It's summery. In order to improve the drawbacks of such mirror finishing methods, a method has been developed in which ultra-precision cutting is performed using a diamond cutting tool and then a surface protective coating is applied to create a mirror finish. This method does not require complicated operations such as plating or polishing on the surface of the material, and it also shortens processing time, making it an excellent mirror finishing method.However, the finished material surface directly reflects the laser beam. Since it must function as a surface, conventionally used aluminum alloy materials cannot meet the required characteristics. In other words, the mirror surface of a laser reflecting mirror is required to have a surface roughness (Rmax) of 0.03 μm or less, a flatness accuracy (height of plane waviness) of 0.1 μm or less, and an extremely high level of reflection function with no local bits or scratches. . Furthermore, when this material is used in rotating polygonal reflectors for laser scanners, the mirror body is rotated at high speeds of tens of thousands of times per minute, so the reflective function is affected by elastic or plastic deformation. It is necessary to have such strength and rigidity that the material does not deteriorate. The inventors have completed the present invention as a result of repeated research and study on a method of manufacturing an aluminum alloy material that can be immediately used as a laser reflecting mirror material after ultra-precision turning with a diamond cutting tool or the like. The present invention uses magnesium 2 by weight.
~6%, the balance consists of aluminum and impurities, and the permissible impurity content limit is 0.15% iron, 0.05% silicon, 0.25% copper, 0.50% zinc, and 1.0 manganese.
%, 0.05% chromium, 0.10% zirconium, 0.02% titanium, and 0.10% in total of other impurities. After passing through a pore diameter of 10 μm or less, the molten aluminum alloy is solidified at a cooling rate of 300°C/sec or more. An ingot is produced by casting, and this ingot is solution-treated, hot-rolled, cold-rolled, or immediately cold-rolled to a specified thickness according to conventional methods, and finally It is characterized by being annealed. That is, according to the inventors' study, a solid solution strengthened aluminum-magnesium alloy containing 2 to 6% magnesium is an aluminum alloy system that satisfies the strength, rigidity, and reflective function among the various properties required for a laser reflecting mirror. It was found to be appropriate. However, when precision cutting is performed using a diamond cutting tool or the like using a material made from a general commercially available aluminum-magnesium alloy, the processed surface of the material has a high level of smoothness as described above. Various problems have arisen in order to impart the accompanying reflective function. In other words, in commercial standard aluminum alloy materials, there are insoluble intermetallic compound particles based on various impurity metal elements and nonmetallic inclusion particles that are mixed in during the process, and many of these inclusions are harder than the alloy matrix. Because of this, inclusion particles may remain as protrusions on the surface after finishing, or they may fall off during cutting, resulting in pits or scratches, resulting in scattering of the projected light in these areas, resulting in accurate and clear images. It was extremely difficult to obtain a clear reflection image. The inventors conducted a detailed study on the effect that these inclusions contained in the alloy material have on the laser beam reflection function after mirror finishing the material, and found that even if the size of the insoluble intermetallic compound particles is 2 μm or less, In other words, it is possible to form a good reflective surface as a laser reflecting mirror, that is, by passing the molten alloy through a pass material with a pore size of 10 μm or less once or several times, not only can nonmetallic inclusions be removed, but also insoluble intermetallic compounds can be removed. The amount of insoluble intermetallic compounds contained in the material can be reduced by limiting the abundance of elements that produce We succeeded in reducing the particle size to 2 μm or less. The alloy material obtained by the present invention has excellent machinability with a diamond cutting tool, the smoothness of the cut surface is also good, the reflectance can be increased to approximately 90% or more, and the reflected image is Because of its high clarity, it has excellent performance as a laser reflecting mirror, especially as a rotating polygon mirror for laser scanners. The reason for setting magnesium as an alloying element in the present invention at 2 to 6% is that if magnesium is less than 2%, sufficient strength and good machinability with a diamond bite cannot be obtained, and if it exceeds 6%, the alloy structure A βAl-Mg intermetallic compound is produced, which reduces the workability of the alloy, and this compound becomes coarse grains of 2 μm or more, reducing the reflective function of the mirror surface. As mentioned above, in the present invention, it is particularly important to control the content of metal impurity elements that cause insoluble intermetallic compounds in the alloy. In other words, these metal elements include iron, silicon, chromium, manganese, zirconium, and titanium, but the maximum allowable content of these elements is 0.15% iron, 0.05% silicon, 0.05% chromium, 1.0% manganese, and zirconium. 0.10
%, and titanium to 0.02%.The reason for limiting the amount of each element to above limits is that even if the molten metal is cooled and solidified at a cooling rate of 300℃/second or more, the size of the insoluble intermetallic compound particles will exceed 2μm in the laser reflector. This is because it will no longer be possible to fulfill its functions. In the present invention, a molten aluminum-magnesium alloy having the above composition is passed through a filter having a pore size of 10 μm to remove nonmetallic inclusions, and then
It is cast into an ingot so that it is solidified at a cooling rate of ℃/second or higher. When the molten alloy is solidified at such a high cooling rate, the ingot is cooled extremely rapidly, the amount of insoluble intermetallic compounds precipitated is small, and the particle size can be kept to 2 μm or less. The ingot thus obtained can be immediately cold-rolled to a desired thickness, or it can be annealed at 400-550°C for 2-24 hours and then hot-rolled and cold-rolled to a desired thickness. After making the plate, the final temperature is 300~550℃.
The material is annealed for 0.5 to 5 hours to remove distortion, and then used as a material for a laser reflecting mirror. In addition, during final annealing, the annealing temperature is 500 to 550℃.
When cooling to 250℃ after annealing is performed at a cooling rate of 100℃/min or more, the material reflectance is further increased by 2.
This is more preferable since it can be improved by ~3%. Next, examples of the present invention will be described. Example 1 Sample numbers 1 to 14 having the alloy composition shown in Table 1
After passing the molten aluminum-magnesium alloy through a porous graphite filter with a pore size of 10 μm,
After solidifying at a cooling rate of 350°C/sec and casting into a plate-like ingot with a thickness of 8 μm, it was cold-rolled to a thickness of 6mm, and then this cold-rolled plate was annealed at 420°C for 4 hours. Mechanical properties, crystal grain size, and particle size of insoluble intermetallic compounds were measured for the material thus obtained. Furthermore, this material is precision cut using a diamond cutting tool to give it a mirror finish, and the surface roughness, the presence of marks such as cutting edge marks, scratches, etc., the 60° reflectance for laser incident light, and the clarity of the reflected image. The suitability of the mirror as a laser reflector was evaluated by measuring its strength. These results are summarized in Table 2. In addition, during proper evaluation, the presence or absence of crystallized substances and inclusions of 2 μm or more, cutting edge marks, and surface scratches are measured using a microscope (400x magnification), and the surface roughness is measured using a stylus type surface roughness meter. The reflectance was measured by measuring the 60° reflectance and the shape of the reflected image by irradiating with 2 mW visible light range laser light (He-Ne laser: λ = 632.8 nm).
【表】【table】
【表】
第2表の結果より試料番号1〜7で示される本
発明による合金素材は金属間化合物粒子の最大粒
径が2μm以下であり、またダイヤモンドバイトに
よる切削性も良好で刃先跡目や表面キズも残ら
ず、しかもレーザー光による60゜反射率も88〜91
で反射像の鮮明度も著しく良好であるのに対し、
試料番号8〜14で示される比較素材は金属間化合
物粒子の最大粒径が2μm以上であり、またダイヤ
モンドバイトによる切削加工による刃先跡目や表
面キズが存在するなど、切削性が劣り、且つレー
ザー光による反射率や反射像の鮮明度も低いなど
すべての点において劣ることが判る。
実施例 2
実施例1に用いた本発明による合金(第1表試
料番号2)溶湯について実施例1と同様の過処
理を施した後、凝固時の冷却速度が15℃/秒(試
料番号2−1)、200℃/秒(試料番号2−2)、
および400℃/秒(試料番号2−3および2−
4)、になるようにして厚さ8mmの板状鋳塊に鋳
造した。
次いで、鋳塊を480℃に8時間均質化処理を施
した後6mmまで熱間圧延し、さらに4mmまで冷間
圧延して、340℃に1時間の最終焼鈍を施し室温
まで自然冷却した。。なお試料番号2−4につい
ては試料番号2−3の試料について最終焼鈍を
520℃で1時間行ない、250℃までを150℃/分の
冷却速度で冷却した。
第3表に評価試験結果を示す。[Table] From the results in Table 2, the alloy materials according to the present invention shown in sample numbers 1 to 7 have a maximum grain size of intermetallic compound particles of 2 μm or less, and also have good machinability with a diamond cutting tool, such as cutting edge marks and surface No scratches left, and the 60° reflectance from laser light is 88-91.
While the clarity of the reflected image is also extremely good,
The comparative materials shown in sample numbers 8 to 14 have poor machinability, such as the maximum particle size of intermetallic compound particles of 2 μm or more, and the presence of cutting edge marks and surface scratches from cutting with a diamond cutting tool. It can be seen that it is inferior in all respects, such as low reflectance and low clarity of reflected images. Example 2 The molten alloy of the alloy according to the present invention (Sample No. 2 in Table 1) used in Example 1 was overtreated in the same manner as in Example 1, and the cooling rate during solidification was 15° C./sec (Sample No. 2). -1), 200℃/sec (sample number 2-2),
and 400℃/sec (sample numbers 2-3 and 2-
4) It was cast into a plate-shaped ingot with a thickness of 8 mm. Next, the ingot was homogenized at 480°C for 8 hours, hot rolled to 6 mm, further cold rolled to 4 mm, final annealed at 340°C for 1 hour, and naturally cooled to room temperature. . For sample number 2-4, final annealing was performed for sample number 2-3.
It was heated at 520°C for 1 hour and cooled to 250°C at a cooling rate of 150°C/min. Table 3 shows the evaluation test results.
【表】
第3表の結果より同一組成の合金であつても本
発明の条件で製造されない試料番号2−1および
2−2の合金素材には2μm以上の金属間化合物粒
子が発生し、またダイヤモンドバイトによる切削
性も不良で且つレーザー光による60゜反射率、反
射像鮮明度も良好でないのに対し本発明による素
材(試料番号2−3および2−4)は反射性能評
価のすべての点ですぐれていることが判る。[Table] From the results in Table 3, even though the alloys have the same composition, intermetallic compound particles of 2 μm or more are generated in the alloy materials of sample numbers 2-1 and 2-2, which are not manufactured under the conditions of the present invention. The machinability with a diamond bite was poor, and the 60° reflectance and reflection image clarity with laser light were also poor, whereas the materials according to the present invention (sample numbers 2-3 and 2-4) were good in all points of reflection performance evaluation. It turns out that it is excellent.
Claims (1)
ルミニウムおよび不純物からなり、不純物の含有
許容限界量が鉄0.15%、珪素0.05%、銅0.25%、
亜鉛0.50%、マンガン1.0%、クロム0.05%、ジル
コニウム0.10%、チタン0.02%およびその他の不
純物の合計0.10%であるアルミニウム合金溶湯を
孔径10μm以下の過材を通過させた後、300℃/
秒以上の冷却速度で凝固するよう鋳造して鋳塊を
つくり、必要あれば均質化処理を施した後、常法
により熱間圧延および冷間圧延、または冷間圧延
のみを行ない、最終焼鈍を施こすことを特徴とす
るレーザー反射鏡用アルミニウム合金素材の製造
法。 2 最終焼鈍は500〜550℃で30分乃至5時間の加
熱保持を行なつた後100℃/分以上の温度で冷却
する特許請求の範囲第1項記載のレーザー反射鏡
用アルミニウム合金素材の製造法。[Claims] 1 Contains 2 to 6% magnesium by weight, the balance consists of aluminum and impurities, and the permissible content limit amount of impurities is 0.15% iron, 0.05% silicon, 0.25% copper,
After passing molten aluminum alloy containing 0.50% zinc, 1.0% manganese, 0.05% chromium, 0.10% zirconium, 0.02% titanium and a total of 0.10% other impurities through an overmetal with a pore size of 10 μm or less, it was heated at 300℃/
An ingot is made by casting to solidify at a cooling rate of seconds or more, and after homogenization treatment if necessary, hot rolling and cold rolling, or only cold rolling are carried out by conventional methods, and final annealing is carried out. A method for manufacturing an aluminum alloy material for laser reflecting mirrors, which is characterized by applying 2. Production of an aluminum alloy material for a laser reflecting mirror according to claim 1, wherein the final annealing is performed by heating and holding at 500 to 550°C for 30 minutes to 5 hours, and then cooling at a temperature of 100°C/min or more. Law.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3023283A JPS59157235A (en) | 1983-02-26 | 1983-02-26 | Manufacturing method of aluminum alloy material for laser reflector |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3023283A JPS59157235A (en) | 1983-02-26 | 1983-02-26 | Manufacturing method of aluminum alloy material for laser reflector |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS59157235A JPS59157235A (en) | 1984-09-06 |
| JPH0252683B2 true JPH0252683B2 (en) | 1990-11-14 |
Family
ID=12297961
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP3023283A Granted JPS59157235A (en) | 1983-02-26 | 1983-02-26 | Manufacturing method of aluminum alloy material for laser reflector |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS59157235A (en) |
Cited By (2)
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|---|---|---|---|---|
| CN107008902A (en) * | 2016-01-27 | 2017-08-04 | 通用汽车环球科技运作有限责任公司 | Rapid curing high temperature aluminum ferro-silicium |
| US10260131B2 (en) | 2016-08-09 | 2019-04-16 | GM Global Technology Operations LLC | Forming high-strength, lightweight alloys |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH063499B2 (en) * | 1984-12-04 | 1994-01-12 | 株式会社リコー | Rotary polygon mirror and manufacturing method thereof |
| JPS61159545A (en) * | 1984-12-29 | 1986-07-19 | Canon Inc | Aluminum alloy for precision processing, tube materials and photoconductive materials using this |
| JP3720456B2 (en) * | 1996-05-17 | 2005-11-30 | キヤノン株式会社 | Photovoltaic element |
| DE10231437B4 (en) | 2001-08-10 | 2019-08-22 | Corus Aluminium N.V. | Process for producing an aluminum wrought alloy product |
| BR112019020061A2 (en) | 2017-04-05 | 2020-04-28 | Novelis Inc | aluminum alloy, product, and method for producing an aluminum product. |
| CN110527878B (en) * | 2019-09-23 | 2021-06-18 | 东莞市灿煜金属制品有限公司 | Manufacturing method of aluminum alloy special for notebook computer |
-
1983
- 1983-02-26 JP JP3023283A patent/JPS59157235A/en active Granted
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107008902A (en) * | 2016-01-27 | 2017-08-04 | 通用汽车环球科技运作有限责任公司 | Rapid curing high temperature aluminum ferro-silicium |
| US10294552B2 (en) | 2016-01-27 | 2019-05-21 | GM Global Technology Operations LLC | Rapidly solidified high-temperature aluminum iron silicon alloys |
| CN107008902B (en) * | 2016-01-27 | 2019-07-09 | 通用汽车环球科技运作有限责任公司 | Rapid curing high temperature aluminum ferro-silicium |
| US10435773B2 (en) | 2016-01-27 | 2019-10-08 | GM Global Technology Operations LLC | Rapidly solidified high-temperature aluminum iron silicon alloys |
| US10260131B2 (en) | 2016-08-09 | 2019-04-16 | GM Global Technology Operations LLC | Forming high-strength, lightweight alloys |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS59157235A (en) | 1984-09-06 |
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