JPH083701A - Production of wear resistant aluminum alloy extruded material excellent in strength and machinability - Google Patents

Production of wear resistant aluminum alloy extruded material excellent in strength and machinability

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Publication number
JPH083701A
JPH083701A JP15542394A JP15542394A JPH083701A JP H083701 A JPH083701 A JP H083701A JP 15542394 A JP15542394 A JP 15542394A JP 15542394 A JP15542394 A JP 15542394A JP H083701 A JPH083701 A JP H083701A
Authority
JP
Japan
Prior art keywords
aluminum alloy
strength
temperature
subjected
machinability
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.)
Pending
Application number
JP15542394A
Other languages
Japanese (ja)
Inventor
Koichi Ohori
紘一 大堀
Masahiko Miyazaki
雅彦 宮崎
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.)
MA Aluminum Corp
Original Assignee
Mitsubishi Aluminum 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 Mitsubishi Aluminum Co Ltd filed Critical Mitsubishi Aluminum Co Ltd
Priority to JP15542394A priority Critical patent/JPH083701A/en
Publication of JPH083701A publication Critical patent/JPH083701A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To produce an aluminum alloy material excellent in strength, wear resistance and chip treatability. CONSTITUTION:An aluminum alloy having a compsn. contg. 8 to 12% Si, 1.5 to 4% Cu, 0.2 to 1.0% Mg, 0.25 to 0.6% Mn and 0.01 to 0.1% Sr, furthermore contg. one or two kinds of 0.05 to 0.3% Cr and 0.05 to 0.25% Zr, and the balance Al with inevitable impurities is subjected to semicontinuous casting. This aluminum allay cast ingot is subjected to homogenizing treatment at 480 to 540 deg.C for <=1hr, thereafter subjected to extrusion at 400 to 500 deg.C, then subjected to solution treatment at 490 to 540 deg.C, thereafter subjected to cold drawing at 5 to 15% working ratio and subjected to artificial aging treatment at 160 to 200 deg.C for 2 to 16hr so as to regulate its elongation to <=10%. Thus, the aluminum alloy material having high strength and excellent wear resistance and furthermore excellent in chip treatability can be obtd.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】この発明は、強度、切削性および
耐摩耗性に優れ、したがって切削によって加工される空
調機器部品等の材料に好適なアルミニウム合金押出材の
製造方法に関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a method for producing an aluminum alloy extruded material which is excellent in strength, machinability and wear resistance and is therefore suitable as a material for air-conditioning equipment parts processed by cutting.

【0002】[0002]

【従来の技術】近年、空調機器や産業用機器等における
シリンダーやピストン等の摺動部品には軽量化のために
耐摩耗性を有するAl−Si系合金:代表的なものとし
てはSi:11〜13.5%wt%のAl−共晶Si系
合金JIS4032が用いられるようになった。しか
し、最近、小型軽量化及び高性能化ニーズが一段と厳し
くなるに伴い、従来Al合金材の特性向上が求められて
おり、製品形状を切削加工によって得るような上記部品
については、耐摩耗性、強度と共に良好な切削加工性、
例えば切削時の切粉処理性が重要視されるようになって
きている。
2. Description of the Related Art In recent years, sliding parts such as cylinders and pistons in air conditioners and industrial equipment have wear resistance to reduce weight. Al-Si alloy: Si: 11 .About.13.5% by weight of Al-eutectic Si-based alloy JIS4032 has come to be used. However, recently, as the needs for size reduction, weight reduction and high performance have become more severe, it has been required to improve the properties of conventional Al alloy materials. For the above-mentioned parts obtained by cutting the product shape, wear resistance, Good machinability with strength,
For example, the chip disposability at the time of cutting is becoming more important.

【0003】[0003]

【発明が解決しようとする問題点】しかしながら、従来
のAl−Si系合金は耐摩耗性には優れているものの切
削性、特に切粉処理性が劣っている。具体的には、切削
加工時に切粉がリボン状又はつる巻き状となり、これが
切削工具に巻きついて連続自動切削を困難にするばかり
か、被削材に傷をつけ仕上がり面の表面性状を劣化させ
るという問題点を有している。 これに対しては、合金
成分および製造工程を改良して切削性を向上させる方法
(例えば 特公昭64−10587号)も提案されてい
るが、切粉処理性の改善は十分といえるまでには至って
いない。本発明はこのような事情に鑑み、耐摩耗性、強
度を維持したままで、切削性(切粉処理性)の向上を計
ることを目的としてなされたものである。
However, although the conventional Al-Si alloys are excellent in wear resistance, they are inferior in machinability, especially in chip disposability. Specifically, the cutting chips become ribbon-shaped or spiral-shaped during cutting, which not only winds around the cutting tool and makes continuous automatic cutting difficult, but also scratches the work material and deteriorates the surface quality of the finished surface. There is a problem. On the other hand, a method of improving the machinability by improving the alloy composition and the manufacturing process (for example, Japanese Patent Publication No. 64-10587) has been proposed, but the improvement of the chip disposability is not sufficient. I haven't arrived. In view of such circumstances, the present invention has been made for the purpose of improving the machinability (cutting property) while maintaining the wear resistance and the strength.

【0004】[0004]

【問題を解決するための手段】すなわち、本発明の耐摩
耗性アルミニウム合金押出材の製造方法は、重量%で、
Si:8〜12%、Cu:1.5〜4%、Mg:0.2
〜1.0%、Mn:0.25〜0.6%、Sr:0.0
1〜0.1%を含有し、さらにCr:0.05〜0.3
%、Zr:0.05〜0.25%の内の1種又は2種を
含有し、残部がAl及び不可避不純物からなるアルミニ
ウム合金を半連結鋳造し、該アルミニウム合金鋳塊を4
80〜540℃の温度で1時間以上の均質化処理を施し
た後、400〜500℃の温度で押出加工し、次いで4
90〜540℃の温度で溶体化処理を施し、その後、加
工率5〜15%の冷間引抜き加工を施してから、伸びが
10%以下になるように160〜200℃の温度で2〜
16時間の人工時効処理を施すことを特徴とする。
That is, the method for producing the wear resistant aluminum alloy extruded material of the present invention is
Si: 8-12%, Cu: 1.5-4%, Mg: 0.2
~ 1.0%, Mn: 0.25-0.6%, Sr: 0.0
1 to 0.1%, and further Cr: 0.05 to 0.3
%, Zr: 0.05 to 0.25% of one or two of them, and the balance of Al and inevitable impurities is semi-interlockingly cast into an aluminum alloy.
After performing homogenization treatment at a temperature of 80 to 540 ° C. for 1 hour or more, extrusion processing is performed at a temperature of 400 to 500 ° C., and then 4
Solution treatment is performed at a temperature of 90 to 540 ° C., and then cold drawing is performed at a processing rate of 5 to 15%, and then 2 to 3 at a temperature of 160 to 200 ° C. so that the elongation is 10% or less.
It is characterized by being subjected to artificial aging treatment for 16 hours.

【0005】[0005]

【作用】以下に本発明の限定理由をその作用とともに説
明する。 (アルミニウム合金成分) Si:8〜12% Siは耐摩耗性を向上させる目的で添加させる。但し、
Siが8wt%未満(以下wt%を単に%という)では
耐摩耗性が不十分であり、12%を越えると粗大な初晶
Siが多く発生し、熱間及び冷間(引抜き)加工性が低
下するので上記範囲に限定した。
The reason why the present invention is limited will be described below together with its function. (Aluminum alloy component) Si: 8 to 12% Si is added for the purpose of improving wear resistance. However,
If Si is less than 8 wt% (hereinafter wt% is simply referred to as%), wear resistance is insufficient, and if it exceeds 12%, a large amount of coarse primary crystal Si is generated, resulting in hot and cold (drawing) workability. Since it decreases, it is limited to the above range.

【0006】Cu:1.5〜4% Cuは強度を高め、同時に耐摩耗性を向上させるが、
1.5%未満ではその効果は小さく、一方、4%を越え
ると共晶Siが粗大化して伸びが低下し、更に耐食性も
低下するので上記範囲とする。 Mg:0.2〜1.0% Mgも強度を向上させるために含有させるが、0.2%
未満ではその効果は小さく、一方、1.0%を越えると
強度への寄与は少なくなるばかりでなく、熱間及び冷間
加工性を低下させるので上記範囲内とする。
Cu: 1.5-4% Cu enhances strength and at the same time improves wear resistance,
If it is less than 1.5%, the effect is small. On the other hand, if it exceeds 4%, the eutectic Si is coarsened, the elongation is lowered, and further the corrosion resistance is lowered. Mg: 0.2-1.0% Mg is also included to improve the strength, but 0.2%
If it is less than 1.0%, the effect is small. On the other hand, if it exceeds 1.0%, not only the contribution to the strength is reduced but also the hot and cold workability is deteriorated.

【0007】Mn:0.25〜0.6% Mnは強度及び耐摩耗性を高め、さらにFe不純物によ
る伸びの劣化を軽減し冷間引抜き時に形成されるボイド
の拡大、連結を防止して、微細なボイドを分散させ、切
削時の切粉を微細化する。Mnが0.25%未満ではそ
の効果は小さく、一方、0.6%を越えると、Mnを含
む粗大な金属間化合物が晶出し、熱間及び冷間加工性を
低下させる。また、上記効果を十分に得るためには、M
nの下限はさらに0.4%以上にするのが望ましい。
Mn: 0.25 to 0.6% Mn enhances strength and wear resistance, reduces deterioration of elongation due to Fe impurities, and prevents expansion and connection of voids formed during cold drawing, Disperses fine voids to make fine chips during cutting. If Mn is less than 0.25%, the effect is small. On the other hand, if it exceeds 0.6%, a coarse intermetallic compound containing Mn is crystallized to deteriorate hot workability and cold workability. In order to obtain the above effect sufficiently, M
The lower limit of n is preferably 0.4% or more.

【0008】Cr:0.05〜0.3% Crは強度及び耐摩耗性を改善する効果があるが、さら
にMnの効果を助長する効果がある。ただし、0.05
%未満ではその効果は不十分で、一方、0.3%を越え
ると粗大な晶出物が発生し、熱間及び冷間加工性を低下
させる。 Zr:0.05〜0.25% Zrは、Crと同様に強度及び耐摩耗性を改善する効果
があり、さらに耐応力腐食割れ性を改善する。ただし、
0.05%未満ではその効果は不十分であり、一方、
0.25%を越えると粗大な晶出物が生じて、熱間及び
冷間加工性を著しく低下させるので上記範囲とする。
Cr: 0.05 to 0.3% Cr has the effect of improving the strength and wear resistance, but further has the effect of promoting the effect of Mn. However, 0.05
If it is less than 0.1%, the effect is insufficient, while if it exceeds 0.3%, coarse crystallized substances are generated, and hot and cold workability are deteriorated. Zr: 0.05 to 0.25% Zr has an effect of improving strength and wear resistance similarly to Cr, and further improves stress corrosion cracking resistance. However,
If it is less than 0.05%, its effect is insufficient, while
If it exceeds 0.25%, coarse crystallized substances are generated, and the hot and cold workability are significantly deteriorated, so the above range is made.

【0009】Sr:0.01〜0.1% Srは共晶Siを微細化して強度及び伸び等の機械的性
質向上させる目的で添加する。Srが0.01%未満で
はその効果は不充分であり、一方、0.1%を越えると
Srを含む粗大な金属間化合物を晶出し、熱間及び冷間
加工性を低下させるので上記範囲とする。
Sr: 0.01 to 0.1% Sr is added for the purpose of refining eutectic Si to improve mechanical properties such as strength and elongation. If the Sr content is less than 0.01%, the effect is insufficient. On the other hand, if the Sr content exceeds 0.1%, a coarse intermetallic compound containing Sr is crystallized and the hot and cold workability are deteriorated. And

【0010】(製造工程の条件) 均質化処理:480〜540℃で1時間以上 次に上記アルミニウム合金鋳塊を均質化処理するのはミ
クロ偏析を均一化し、機械的性質、加工性を改善する通
常の目的の他に、共晶Siを球状化し、切削加工性を向
上させるためである。均質化温度が480℃未満ではそ
の効果は不充分であり、一方、540℃を越えると共晶
融解の恐れがあるので、均質化処理は、上記範囲内の温
度で1時間以上行うものとした。
(Conditions of the manufacturing process) Homogenization treatment: 480 to 540 ° C. for 1 hour or more Next, the aluminum alloy ingot is homogenized to homogenize microsegregation and improve mechanical properties and workability. This is for making the eutectic Si spherical and improving the machinability in addition to the usual purpose. If the homogenizing temperature is lower than 480 ° C, the effect is insufficient, while if it exceeds 540 ° C, eutectic melting may occur. Therefore, the homogenizing treatment is performed at a temperature within the above range for 1 hour or more. .

【0011】押出加工:400〜500℃ その後押出加工するのは、鋳造組織を加工組織に変える
ためであるが、押出温度が400℃未満では押出の時の
変形応力が大きく、押出が困難であり、一方、500℃
を越えると加工熱が発生し、共晶融解のおそれがあるの
で押出温度を上記範囲に限定した。 溶体化処理:490〜540℃ 次いで、溶体化処理を施すが、処理温度が490℃未満
では溶体化が不十分で所望の高強度が得られず、一方、
540℃を越えると共晶融解恐れがあるので処理温度を
上記範囲に限定した。
Extrusion processing: 400 to 500 ° C. The subsequent extrusion processing is to change the casting structure into a processed structure. However, if the extrusion temperature is less than 400 ° C., the deformation stress at the time of extrusion is large and extrusion is difficult. Meanwhile, 500 ° C
If the temperature exceeds this, processing heat is generated, and there is a risk of eutectic melting, so the extrusion temperature was limited to the above range. Solution treatment: 490 to 540 ° C. Next, solution treatment is performed, but if the treatment temperature is lower than 490 ° C., solution treatment is insufficient and desired high strength cannot be obtained.
If the temperature exceeds 540 ° C, eutectic melting may occur, so the processing temperature was limited to the above range.

【0012】冷間引抜加工:加工率5〜15% 溶体化処理後の冷間引抜加工は素材内部に加工ひずみを
導入し、共晶Si粒子の周囲に微小なボイドを形成させ
るためであり、これにより切削加工時に切粉が該ボイド
で分解され、細かくなり、切粉処理性が向上する。冷間
引抜加工の加工率が5%未満では微小ボイドの形成が不
十分で切粉が細かくならず、15%を越えると冷間引抜
加工時に材料が破断してしまう。この冷間加工時に材料
が良好な伸び、加工性を有することにより多数の微小ボ
イドが形成されることになる。
Cold drawing: processing rate 5 to 15% The cold drawing after the solution treatment is to introduce a processing strain into the material to form minute voids around the eutectic Si particles. As a result, chips are decomposed by the voids during cutting and become finer, improving the chip disposability. If the working ratio of cold drawing is less than 5%, the formation of fine voids is insufficient and the chips are not fine, and if it exceeds 15%, the material breaks during cold drawing. Since the material has good elongation and workability during this cold working, a large number of minute voids are formed.

【0013】人工時効処理:160〜200℃、2〜1
6時間 冷間引抜加工後の人工時効処理は所望の材料強度を得る
ために行われる。処理温度が160℃未満では時効硬化
の進行が遅く、所望の強度を得るのに長時間を要するた
め経済的でなく、一方200℃を越える温度で時効して
も所望の強度が得られないので上記温度範囲とする。ま
た時効時間については実用的な2〜16時間の範囲で行
う。この時効処理では、押出材の伸びが10%以下とな
るように時効温度、時効時間を適宜選択する。伸びを1
0%以下に限定したのは10%を越えると材料の延性が
高くなって切粉が分断され難くなるためである。なお、
同様の理由で、伸びをさらに9%以下に限定するのが望
ましい。すなわち、本発明では、時効処理前には成分の
適正化によって十分な伸びを確保して、冷間引抜時のボ
イドの拡大、連結を防止して切粉処理性を向上させ、さ
らに時効処理後には伸びを抑制して、さらに切粉処理性
を向上させている。
Artificial aging treatment: 160 to 200 ° C., 2-1
The artificial aging treatment after the cold drawing for 6 hours is performed to obtain a desired material strength. When the treatment temperature is lower than 160 ° C, the progress of age hardening is slow, and it takes a long time to obtain the desired strength, which is not economical. On the other hand, even if the aging is performed at a temperature higher than 200 ° C, the desired strength cannot be obtained. Within the above temperature range. The aging time is within a practical range of 2 to 16 hours. In this aging treatment, the aging temperature and the aging time are appropriately selected so that the elongation of the extruded material is 10% or less. Growth 1
The reason for limiting the content to 0% or less is that if the content exceeds 10%, the ductility of the material becomes high and the chips are difficult to be divided. In addition,
For the same reason, it is desirable to limit the elongation to 9% or less. That is, in the present invention, before the aging treatment, sufficient elongation is ensured by optimizing the components, expansion of voids during cold drawing, prevention of connection and improvement of chip disposability, and further aging treatment. Suppresses elongation and further improves chip disposability.

【0014】[0014]

【実施例】次に本発明の実施例を説明する。表1に示す
合金組成のAl合金を半連結鋳造法により2.28mm
径のビレットに鋳造し、表2に示す処理を施した後、こ
れを供試材として強度、伸び、耐摩耗性および切削加工
性について評価し、表3の結果を得た。なお、切削加工
性は超硬バイトにより主軸回転数を1600rpm、切
込み深さ/mm、及び送り速度0.117mm/rev
の切削条件にて、切削油を用いず切削した場合の切粉の
長さ及び状態を目視により評価し、3段階にランク分け
した。耐摩耗性は大越式摩耗試験機で比摩耗量を求め評
価した。摩耗子にはFC25を用い、荷重2.1kg、
摩擦速度2.0m/sで行った。
EXAMPLES Examples of the present invention will be described below. 2.28 mm of Al alloy having the alloy composition shown in Table 1 by the semi-connecting casting method
After being cast into a billet having a diameter and subjected to the treatment shown in Table 2, this was used as a test material to evaluate strength, elongation, wear resistance and machinability, and the results in Table 3 were obtained. The machinability is 1600 rpm for spindle speed, depth of cut / mm, and feed rate of 0.117 mm / rev with a carbide tool.
Under the cutting conditions of No. 3, the length and state of the cutting chips when cut without using the cutting oil were visually evaluated, and ranked into three ranks. The wear resistance was evaluated by determining the specific wear amount with an Ogoshi-type wear tester. FC25 is used for the wearer and the load is 2.1 kg.
The friction speed was 2.0 m / s.

【0015】[0015]

【表1】 [Table 1]

【0016】[0016]

【表2】 [Table 2]

【0017】[0017]

【表3】 [Table 3]

【0018】上記評価試験結果から明らかなように、本
発明法によって得られた供試材は、強度、耐摩耗性、切
粉処理性のいずれの点でも優れているの対し、比較法に
よる供試材では、いずれかの点で劣っており、特に強度
が高いものは切粉処理性に劣っており、切粉処理性が良
好なものは強度が不十分であった。
As is clear from the above evaluation test results, the test material obtained by the method of the present invention is excellent in all of the strength, wear resistance and chip disposability, whereas the test material obtained by the comparison method is excellent. The test materials were inferior in some respects, particularly those having high strength were inferior in chip disposability, and those having good chip disposability were insufficient in strength.

【0019】[0019]

【発明の効果】以上説明したように、本発明の耐摩耗性
アルミニウム合金押出材の製造方法によれば、重量%
で、Si:8〜12%、Cu:1.5〜4%、Mg:
0.2〜1.0%、Mn:0.25〜0.6%、Sr:
0.01〜0.1%を含有し、さらにCr:0.05〜
0.3%、Zr:0.05〜0.25%の内の1種又は
2種を含有し、残部がAl及び不可避不純物からなるア
ルミニウム合金を半連結鋳造し、該アルミニウム合金鋳
塊を480〜540℃の温度で1時間以上の均質化処理
を施した後、400〜500℃の温度で押出加工し、次
いで490〜540℃の温度で溶体化処理を施し、その
後、加工率5〜15%の冷間引抜き加工を施してから、
伸びが10%以下になるように160〜200℃の温度
で2〜16時間の人工時効処理を施したので、高い強度
と耐摩耗性が得られるとともに、切削加工時には切粉が
多数の微細なボイドで分断され、優れた切粉処理性が得
られる効果がある。
As described above, according to the method for producing the wear resistant aluminum alloy extruded material of the present invention, the weight% is
Then, Si: 8-12%, Cu: 1.5-4%, Mg:
0.2-1.0%, Mn: 0.25-0.6%, Sr:
0.01-0.1%, and Cr: 0.05-
Aluminum alloy containing 0.3% and Zr: 0.05 to 0.25%, one or two of which is Al and inevitable impurities, and the balance is semi-continuously cast, and the aluminum alloy ingot is 480 After subjecting to homogenizing treatment at a temperature of ˜540 ° C. for 1 hour or more, extrusion processing is performed at a temperature of 400 to 500 ° C., then solution treatment is performed at a temperature of 490 to 540 ° C., and then a processing rate of 5 to 15 % After cold drawing,
Since the artificial aging treatment was performed at a temperature of 160 to 200 ° C. for 2 to 16 hours so that the elongation was 10% or less, high strength and wear resistance were obtained, and a large number of fine chips were generated during cutting. It is divided by voids, and has the effect of providing excellent chip disposability.

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 重量%で、Si:8〜12%、Cu:
1.5〜4%、Mg:0.2〜1.0%、Mn:0.2
5〜0.6%、Sr:0.01〜0.1%を含有し、さ
らにCr:0.05〜0.3%、Zr:0.05〜0.
25%の内の1種又は2種を含有し、残部がAl及び不
可避不純物からなるアルミニウム合金を半連結鋳造し、
該アルミニウム合金鋳塊を480〜540℃の温度で1
時間以上の均質化処理を施した後、400〜500℃の
温度で押出加工し、次いで490〜540℃の温度で溶
体化処理を施し、その後、加工率5〜15%の冷間引抜
き加工を施してから、伸びが10%以下になるように1
60〜200℃の温度で2〜16時間の人工時効処理を
施すことを特徴とする強度と切削性の優れた耐摩耗性ア
ルミニウム合金押出材の製造方法
1. By weight%, Si: 8-12%, Cu:
1.5-4%, Mg: 0.2-1.0%, Mn: 0.2
5 to 0.6%, Sr: 0.01 to 0.1%, Cr: 0.05 to 0.3%, Zr: 0.05 to 0.
An aluminum alloy containing one or two of 25% and the balance consisting of Al and unavoidable impurities is semi-continuously cast,
The aluminum alloy ingot at a temperature of 480 to 540 ° C. for 1
After the homogenization treatment for more than an hour, extrusion processing is performed at a temperature of 400 to 500 ° C., then solution treatment is performed at a temperature of 490 to 540 ° C., and then cold drawing processing at a processing rate of 5 to 15% is performed. After applying, 1 so that the elongation is less than 10%
A method for producing an abrasion-resistant aluminum alloy extruded material having excellent strength and machinability, characterized by performing artificial aging treatment for 2 to 16 hours at a temperature of 60 to 200 ° C.
JP15542394A 1994-06-15 1994-06-15 Production of wear resistant aluminum alloy extruded material excellent in strength and machinability Pending JPH083701A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP15542394A JPH083701A (en) 1994-06-15 1994-06-15 Production of wear resistant aluminum alloy extruded material excellent in strength and machinability

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15542394A JPH083701A (en) 1994-06-15 1994-06-15 Production of wear resistant aluminum alloy extruded material excellent in strength and machinability

Publications (1)

Publication Number Publication Date
JPH083701A true JPH083701A (en) 1996-01-09

Family

ID=15605686

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15542394A Pending JPH083701A (en) 1994-06-15 1994-06-15 Production of wear resistant aluminum alloy extruded material excellent in strength and machinability

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JP (1) JPH083701A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0937162A1 (en) * 1997-07-11 1999-08-25 Alcoa Inc. Extruding and forging an aluminum silicon alloy
WO2003010349A1 (en) * 2001-07-25 2003-02-06 Showa Denko K. K. Aluminum alloy excellent in machinability, and aluminum alloy material and method for production thereof
KR100425528B1 (en) * 2001-01-03 2004-03-30 조홍식 Method for manufacturing the rod type member using aluminium alloy
WO2009003365A1 (en) * 2007-06-29 2009-01-08 Northeastern University A structural material part of a high-si mg-containing al alloy and the manufacture method thereof
CN104328315A (en) * 2014-10-22 2015-02-04 江苏大学 Process method for improving friction and wear properties of multi-element aluminum-silicon alloy
RU2661525C1 (en) * 2017-04-18 2018-07-17 Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") Aluminium-based alloy
CN113667863A (en) * 2021-08-30 2021-11-19 安徽华深铝业有限公司 Aluminum bar homogenization heat treatment process before extrusion of industrial aluminum profile

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0937162A1 (en) * 1997-07-11 1999-08-25 Alcoa Inc. Extruding and forging an aluminum silicon alloy
EP0937162A4 (en) * 1997-07-11 2000-11-15 Alcoa Inc Extruding and forging an aluminum silicon alloy
KR100425528B1 (en) * 2001-01-03 2004-03-30 조홍식 Method for manufacturing the rod type member using aluminium alloy
WO2003010349A1 (en) * 2001-07-25 2003-02-06 Showa Denko K. K. Aluminum alloy excellent in machinability, and aluminum alloy material and method for production thereof
WO2009003365A1 (en) * 2007-06-29 2009-01-08 Northeastern University A structural material part of a high-si mg-containing al alloy and the manufacture method thereof
CN104328315A (en) * 2014-10-22 2015-02-04 江苏大学 Process method for improving friction and wear properties of multi-element aluminum-silicon alloy
RU2661525C1 (en) * 2017-04-18 2018-07-17 Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") Aluminium-based alloy
CN113667863A (en) * 2021-08-30 2021-11-19 安徽华深铝业有限公司 Aluminum bar homogenization heat treatment process before extrusion of industrial aluminum profile

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