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JPH0474402B2 - - Google Patents
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JPH0474402B2 - - Google Patents

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Publication number
JPH0474402B2
JPH0474402B2 JP58240296A JP24029683A JPH0474402B2 JP H0474402 B2 JPH0474402 B2 JP H0474402B2 JP 58240296 A JP58240296 A JP 58240296A JP 24029683 A JP24029683 A JP 24029683A JP H0474402 B2 JPH0474402 B2 JP H0474402B2
Authority
JP
Japan
Prior art keywords
powder
resistant
aluminum alloy
wear
less
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
JP58240296A
Other languages
Japanese (ja)
Other versions
JPS60131944A (en
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 filed Critical
Priority to JP58240296A priority Critical patent/JPS60131944A/en
Priority to DE8484115701T priority patent/DE3483421D1/en
Priority to EP84115701A priority patent/EP0147769B1/en
Priority to BR8406548A priority patent/BR8406548A/en
Priority to US06/683,454 priority patent/US4722751A/en
Publication of JPS60131944A publication Critical patent/JPS60131944A/en
Publication of JPH0474402B2 publication Critical patent/JPH0474402B2/ja
Granted legal-status Critical Current

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Description

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

本発明は、超耐熱耐摩耗Al合金に係り、苛酷
な条件下での使用可能なアルミニウム合金および
その合金製造用複合粉末に関するものである。 近年、自動車用エンジンおよび航空機等の材料
は、省エネルギー・高性能化の必要から小型軽量
化、高出力化が図られ、それに伴つてピストン等
に使用される材料は、従来よりも高荷重・高温度
の厳しい条件下での使用に耐えることが要求され
ている。 自動車用ピストンを例にとれば、従来のピスト
ン用Al合金は、AC8BといつたAl−Si系の鋳造材
が用いられている。しかし鋳造法では、20%以上
の高Si量にすることは、偏析や初晶の粗大化の問
題もあつて、上記要求を満たすことは困難であ
る。従つて近年、急冷高Si含有アルミニウム合金
粉を出発原料として用い熱間押出法等によつて無
気孔の均一微細結晶粒の耐熱耐摩耗アルミニウム
合金材料の開発が開始されている。 しかしながら、急冷粉末を用いる場合には、緻
密化のための成形時の加熱による粒成長等の問題
もあり、おのずと製造方法に限界がある。又急冷
粉末中への分散粒子添加は技術的に困難である。
つまり急冷法だけにもとずく分散粒子添加による
強化によつてより一層耐熱耐摩耗性を向上させる
ことは、今まで実現していなかつた。 本発明は係る従来技術の問題点を解決するため
になされたものであり、メカニカルアロイングと
いう新手法によつて、過飽和固溶体・均一微細結
晶粒を有する急冷粉末の長所を保存し(ないし急
冷粉末と同様の効果を混合粉のメカニカルアロイ
ング処理それ自身によつて得)つつ、分散粒子添
加による分散強化効果の重複による二重の効果に
よつて、従来の鋳造材や溶製材ならびに最近開発
途上の急冷粉末による材料よりも優れた耐熱・耐
摩耗性を有するアルミニウム合金およびその合金
製造用複合粉末を提供することを目的とする。 係る目的は、本発明によれば、急冷Al合金粉
99.5〜90容積%と炭素粉(黒鉛粉)0.5〜10容積
%とをメカニカルアロイングして粉末を得、その
粉末を型押・焼結法、ホツトプレス、焼結鍛造、
粉末圧延、熱間静水圧、熱間押出の各種成形処理
を行うことによつて得られる。また急冷アルミニ
ウム合金粉と同様な性質を、それと同組成配合し
た混合粉と炭素粉(黒鉛粉)のメカニカルアロイ
ングによつて得られる。メカニカルアロイング処
理とその後の成形前の加熱中、成形体の熱処理中
に、当初の炭素(黒鉛)は炭化物Al4C3になり、
これが細かく均一に分散して合金の強化に寄与す
る。 以下、本発明のアルミニウム合金およびその合
金製造用複合粉末について説明する。 本発明は、急冷粉末の微細結晶粒等の効果によ
るマトリツクスの強化とメカニカルアロイングに
よる分散粒子(Al4C3)強化の相乗効果によつ
て、耐摩耗性を維持したまま著しく耐熱性を向上
させることができるとの知見に基づきなされたも
のである。 本発明において、メカニカルアロイング処理前
の素材粉として用いるAl−Si系急冷粉あるいは
混合粉においてSi量を重量比5〜30%と限定した
理由は、重量比5%Si以下では、鋳造法で容易に
製造できるししかも耐摩耗性が低いためであり、
重量比30%Siを越えると耐摩耗性は高くなるが粉
末の熱間成形およびその後の塑性加工が困難にな
るためである。 Cuは合金の熱処理による析出強化のために、
Mgは固溶強化のために、目的に応じて添加す
る。室温強度が重要でない場合には、無添加でさ
しつかえない。 後のメカニカルアロイング処理や熱間加工によ
つてAl4C4という炭化物粒子となる炭素粉(黒鉛
粉)の容積比を0.5〜10%と限定した理由は、容
積比0.5%以下では分散強化の効果がなく、容積
比10%以上ではかえつて脆くなり、メカニカルア
ロイング粉末の熱間成形加工および合金の塑性加
工が困難となるためである。 Al−Fe系急冷粉あるいは混合粉においてFe量
を重量比2〜12%と限定した理由は、重量比2%
Fe以下では耐熱耐摩耗の効果が少ないためであ
り、重量比12%Fe以上では、メカニカルアロイ
ング処理後の粉末の熱間加工性および合金の塑性
加工性が悪くなるためである。Co、Ni、Cr、
Mn、Ce、Ti、Zr、Mo等の遷移金属の添加は、
合金特性の一層の向上と粉末の成形加工性の向上
のために添加することが望ましいが、添加しなく
ても差しつかえはない。重量比7%以上添加し
Fe量よりも多量になるような場合でも全く問題
はないけれども、その場合には高価につくので、
重量比7%以下と限定した。 Al−Si−Fe系急冷粉あるいは混合粉と炭素粉
(黒鉛粉)をメカニカルアロイングすることは、
Al−Si系とAl−Fe系の両者の優れた性質を合せ
もたせる効果が得られるという知見にもとずいて
いる。特に組成が重量比10〜14%Si、重量比4〜
6%Feとなるメカニカルアロイング粉は、熱間
加工性に優れ、しかもAl合金の一般的弱点であ
る高熱膨張率を克服する効果があり、超耐熱耐摩
耗という特性に加えて低熱膨張という性質を加味
する。 アルミニウム粉のメカニカルアロイングは、ア
ルミニウム合金組成に依存して、十分に均一にメ
カニカルアロイングする以前に造粒して塊状にな
る場合が生じる。通常、高硬度の急冷粉末の場合
には上記現象は生じにくいが、純アルミニウム粉
や他の純金属粉との混合粉のメカニカルアロイン
グの場合に生じやすい。そのような場合には、
水、油、有機溶剤を適量(容積比0.05〜3%)添
加することによつて造粒を防止し、十分なメカニ
カルアロイングが確保されるようにしなけらばな
らない。添加した水、油、有機溶剤は、熱間加工
前のメカニカルアロイング粉末ないしその成形体
の加熱あるいは脱気処理によつて抜けるか、炭化
物Al4C3として分散する。 実施例 1 ガスアトマイズ法で製造された100メツシユ以
下の急冷アルミニウム合金粉末(組成Al−12Si
−5Fe−4.5Cu−1Mg)と炭化粉(カーボンブラ
ツク)とを、容積比で97:3に混合し、乾式アト
ライターにて5時間処理した。粉末は、メカニカ
ルアロイングによつて造粒粗大化し、平均粒径約
1mmとなり、組織はメカニカルアロイング特有の
波状になつている(第1図参照)。Siの初晶は全
く見られない。粉末のマイクロビツカース硬さ
は、250を越える。 上記粉末をAl製シースに入れ、450℃で2時間
加熱後、押出比10:1で熱間押出成形を行つた。
押出した本合金の諸性質を第1表に示す。1000倍
程度の光学顕微鏡では確認できないほど微細な組
織を有し300℃で30Kg/mm2を超える引張強さを有
している。又低熱膨張係数である。
The present invention relates to a super heat-resistant and wear-resistant Al alloy, and relates to an aluminum alloy that can be used under severe conditions and a composite powder for producing the alloy. In recent years, materials for automobile engines and aircraft have become smaller, lighter, and have higher output due to the need to save energy and improve performance. It is required to withstand use under severe temperature conditions. Taking automobile pistons as an example, the conventional Al alloy for pistons is an Al-Si cast material such as AC8B. However, in the casting method, increasing the Si content to a high content of 20% or more causes problems of segregation and coarsening of primary crystals, making it difficult to meet the above requirements. Therefore, in recent years, development of heat-resistant and wear-resistant aluminum alloy materials with pore-free, uniform fine crystal grains has begun using quenched high-Si-containing aluminum alloy powder as a starting material and a hot extrusion method. However, when a rapidly cooled powder is used, there are problems such as grain growth due to heating during molding for densification, and there are limits to the manufacturing method. Furthermore, it is technically difficult to add dispersed particles to the rapidly cooled powder.
In other words, it has not been possible to further improve heat and wear resistance by strengthening by adding dispersed particles based only on the quenching method. The present invention has been made to solve the problems of the prior art, and uses a new method called mechanical alloying to preserve the advantages of quenched powders having supersaturated solid solutions and uniform fine crystal grains (or to improve quenched powders). While the same effect is obtained by the mechanical alloying process itself of the mixed powder, the dual effect of the duplication of the dispersion strengthening effect due to the addition of dispersed particles makes it possible to improve the performance of conventional cast materials, ingot materials, and recently developed materials. The purpose of the present invention is to provide an aluminum alloy that has better heat resistance and wear resistance than materials made from quenched powder, and a composite powder for producing the alloy. According to the present invention, such a purpose is to produce quenched Al alloy powder.
99.5 to 90% by volume and 0.5 to 10% by volume of carbon powder (graphite powder) are mechanically alloyed to obtain a powder, which is then processed by embossing and sintering, hot pressing, sintering, forging, etc.
It can be obtained by performing various forming treatments such as powder rolling, hot isostatic pressing, and hot extrusion. Properties similar to those of quenched aluminum alloy powder can be obtained by mechanical alloying of a mixed powder with the same composition and carbon powder (graphite powder). During the mechanical alloying process and subsequent heating before forming, during the heat treatment of the compact, the initial carbon (graphite) becomes a carbide Al 4 C 3 ,
This is finely and uniformly dispersed and contributes to strengthening the alloy. Hereinafter, the aluminum alloy of the present invention and the composite powder for producing the alloy will be explained. The present invention significantly improves heat resistance while maintaining wear resistance through the synergistic effect of strengthening the matrix due to the effects of fine crystal grains in the quenched powder and strengthening dispersed particles (Al 4 C 3 ) through mechanical alloying. This was done based on the knowledge that it is possible to In the present invention, the reason why the amount of Si is limited to 5 to 30% by weight in the Al-Si quenched powder or mixed powder used as the raw material powder before mechanical alloying treatment is that if the weight ratio is less than 5%Si, the casting method cannot be used. This is because it is easy to manufacture and has low wear resistance.
This is because if the weight ratio exceeds 30% Si, wear resistance increases, but hot forming of the powder and subsequent plastic working becomes difficult. Cu is used for precipitation strengthening due to heat treatment of the alloy.
Mg is added depending on the purpose for solid solution strengthening. If room temperature strength is not important, no additives can be used. The reason why we limited the volume ratio of carbon powder (graphite powder) that becomes carbide particles called Al 4 C 4 through mechanical alloying treatment and hot processing to 0.5 to 10% is that dispersion strengthening occurs when the volume ratio is 0.5% or less. This is because if the volume ratio exceeds 10%, it becomes brittle, making hot forming of the mechanical alloying powder and plastic working of the alloy difficult. The reason why we limited the amount of Fe to 2 to 12% by weight in the Al-Fe-based quenched powder or mixed powder is that it is 2% by weight.
This is because if the weight ratio is less than 12% Fe, the effect of heat and wear resistance is small, and if the weight ratio is 12% or more, the hot workability of the powder and the plastic workability of the alloy after mechanical alloying treatment deteriorate. Co, Ni, Cr,
Addition of transition metals such as Mn, Ce, Ti, Zr, Mo, etc.
Although it is desirable to add it to further improve the alloy properties and the moldability of the powder, there is no problem even if it is not added. Added at least 7% by weight
There is no problem at all if the amount is larger than the amount of Fe, but in that case it will be expensive, so
The weight ratio was limited to 7% or less. Mechanical alloying of Al-Si-Fe based quenched powder or mixed powder and carbon powder (graphite powder)
This is based on the knowledge that the effect of combining the excellent properties of both Al-Si and Al-Fe systems can be obtained. In particular, the composition is 10 to 14% Si by weight, 4 to 4% by weight
Mechanical alloying powder with 6% Fe has excellent hot workability and is effective in overcoming the high coefficient of thermal expansion, which is a general weakness of Al alloys, and has the property of low thermal expansion in addition to the characteristics of super heat and wear resistance. Take into consideration. When mechanically alloying aluminum powder, depending on the aluminum alloy composition, the aluminum powder may be granulated and become lumpy before being sufficiently uniformly mechanically alloyed. Normally, the above phenomenon does not easily occur in the case of rapidly solidified powder with high hardness, but it tends to occur in the case of mechanical alloying of pure aluminum powder or mixed powder with other pure metal powder. In such a case,
Pelletization must be prevented by adding appropriate amounts of water, oil, and organic solvents (0.05 to 3% by volume) to ensure sufficient mechanical alloying. The added water, oil, and organic solvent are either removed or dispersed as carbide Al 4 C 3 by heating or degassing the mechanical alloying powder or its compact before hot processing. Example 1 Rapidly solidified aluminum alloy powder (composition Al-12Si) of 100 mesh or less produced by gas atomization method
-5Fe-4.5Cu-1Mg) and carbonized powder (carbon black) were mixed at a volume ratio of 97:3 and treated with a dry attritor for 5 hours. The powder is granulated and coarsened by mechanical alloying, with an average particle size of about 1 mm, and the structure has a wavy structure characteristic of mechanical alloying (see Fig. 1). No primary Si crystals are observed. The microvits hardness of the powder exceeds 250. The above powder was placed in an Al sheath, heated at 450°C for 2 hours, and then hot extruded at an extrusion ratio of 10:1.
Table 1 shows the properties of the extruded alloy. It has a microstructure so fine that it cannot be seen with an optical microscope at 1000x magnification, and has a tensile strength of over 30 Kg/mm 2 at 300°C. It also has a low coefficient of thermal expansion.

【表】 実施例 2 第2表記載の各種組成の急冷粉、混合粉と炭素
粉(カーボンブラツク)或は黒鉛粉を乾式のボー
ルミルにて10日間メカニカルアロイング処理し、
その粉末を冷間静水圧プレス4t/cm2で成形後、
450℃で2時間加熱し熱間押出成形加工を行つた。
得られた合金の密度、ロツクウエル硬さ(Bスケ
ール)、室温及び300℃での引張強さを第3表に示
す。いずれも高温での強さに優れており、単なる
急冷粉のみからなる合金よりも、炭素粉(或は黒
鉛粉)とのメカニカルアロイング処理によつて
300℃で10Kg/mm2以上も高い引張強さを有してい
ることが確認できる。
[Table] Example 2 Rapidly cooled powders and mixed powders with various compositions listed in Table 2 and carbon powder (carbon black) or graphite powder were mechanically alloyed for 10 days in a dry ball mill.
After molding the powder with a cold isostatic press of 4t/ cm2 ,
Hot extrusion processing was performed by heating at 450°C for 2 hours.
Table 3 shows the density, Rockwell hardness (B scale), and tensile strength at room temperature and 300°C of the obtained alloy. All of them have excellent strength at high temperatures, and are made by mechanical alloying with carbon powder (or graphite powder) rather than alloys made only of quenched powder.
It can be confirmed that it has a tensile strength as high as 10Kg/mm 2 or more at 300℃.

【表】【table】

【表】【table】 【図面の簡単な説明】[Brief explanation of drawings]

第1図は本発明実施例1のメカニカルアロイン
グして得られた粉末の400倍拡大の顕微鏡写真を
示す。
FIG. 1 shows a 400 times enlarged micrograph of the powder obtained by mechanical alloying of Example 1 of the present invention.

Claims (1)

【特許請求の範囲】 1 急冷アルミニウム合金粉または混合粉(純金
属粉ないし母合金粉末かならる)99.5〜90容積
%、炭素粉(又は黒鉛粉)0.5〜10容積%および
以上の合計量に対しさらに潤滑剤として水、油、
有機溶剤等を0.05〜3容積%添加して混合し、更
にメカニカルアロイングして上記成分を均一微細
に分散させたことを特徴とする超耐熱耐摩耗アル
ミニウム合金製造用複合粉末。 2 急冷アルミニウム合金粉または混合粉が重量
比でSi5〜30%、Cu5%以下、Mg2%以下、Al残
部の組成あるいは重量比でFe2〜12%、Co・
Ni・Cr・Mn・Ce・Ti・Zr・Moよりなる群より
選ばれた1種又は2種以上を7%以下、Al残部
の組成よりなることを特徴とする特許請求の範囲
第1項記載の超耐熱耐摩耗アルミニウム合金製造
用複合粉末。 3 急冷アルミニウム合金粉または混合粉が重量
比でSi5〜15%、Fe2〜12%、Cu5%以下、Mg2%
以下、Co・Ni・Cr・Mn・Ce・Ti・Zr・Moよ
りなる群より選ばれた1種又は2種以上を7%以
下、Al残部よりなることを特徴とする特許請求
の範囲第1項記載の超耐熱耐熱摩耗アルミニウム
合金製造用複合粉末。 4 特許請求の範囲第1項〜第3項記載の粉末を
用いて、熱間加工によつて固化され、炭素(又は
黒鉛)の全量とAlで形成されたAl4C3及びSi、Fe
等アルミニウム以外の成分がアルミニウムマトリ
ツクス中に均一微細に分散されており、ロツクウ
エルBスケール硬度75以上、300℃での引張強さ
26Kg/mm2以上の超耐熱耐摩耗アルミニウム合金。
[Claims] 1. Quenched aluminum alloy powder or mixed powder (consisting of pure metal powder or master alloy powder) 99.5 to 90% by volume, carbon powder (or graphite powder) 0.5 to 10% by volume, and the total amount of the above In addition, water, oil,
A composite powder for producing a super heat-resistant and wear-resistant aluminum alloy, characterized in that 0.05 to 3% by volume of an organic solvent is added and mixed, and then mechanically alloyed to uniformly and finely disperse the above components. 2 Quenched aluminum alloy powder or mixed powder has a weight ratio of Si5 to 30%, Cu5% or less, Mg2% or less, and the remaining Al composition or weight ratio Fe2 to 12%, Co.
Claim 1, characterized in that the composition consists of 7% or less of one or more selected from the group consisting of Ni, Cr, Mn, Ce, Ti, Zr, and Mo, and the remainder Al. Composite powder for manufacturing super heat-resistant and wear-resistant aluminum alloys. 3 Quenched aluminum alloy powder or mixed powder has a weight ratio of Si5 to 15%, Fe2 to 12%, Cu not more than 5%, Mg2%
Claim 1 below, characterized in that the content is 7% or less of one or more selected from the group consisting of Co, Ni, Cr, Mn, Ce, Ti, Zr, and Mo, and the remainder is Al. Composite powder for producing ultra-heat-resistant, heat-resistant, wear-resistant aluminum alloy as described in . 4 Al 4 C 3 and Si, Fe which are solidified by hot working using the powder described in claims 1 to 3 and formed of the entire amount of carbon (or graphite) and Al.
Components other than aluminum are uniformly and finely dispersed in the aluminum matrix, and have a Rockwell B scale hardness of 75 or more and a tensile strength at 300℃.
Super heat-resistant and wear-resistant aluminum alloy of 26Kg/mm 2 or more.
JP58240296A 1983-12-19 1983-12-19 Superheat-and wear-resistant aluminum alloy and its manufacture Granted JPS60131944A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
JP58240296A JPS60131944A (en) 1983-12-19 1983-12-19 Superheat-and wear-resistant aluminum alloy and its manufacture
DE8484115701T DE3483421D1 (en) 1983-12-19 1984-12-18 DISPERSION-REINFORCED ALUMINUM ALLOY WITH GOOD WEAR AND RESISTANCE AND METHOD FOR THEIR PRODUCTION.
EP84115701A EP0147769B1 (en) 1983-12-19 1984-12-18 Dispersion-strengthened heat- and wear-resistant aluminum alloy and process for producing same
BR8406548A BR8406548A (en) 1983-12-19 1984-12-18 ALUMINUM ALLOY REINFORCED BY DISPERSION AND RESISTANT TO HEAT AND WEAR AND PROCESS FOR ITS PRODUCTION
US06/683,454 US4722751A (en) 1983-12-19 1984-12-19 Dispersion-strengthened heat- and wear-resistant aluminum alloy and process for producing same

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58240296A JPS60131944A (en) 1983-12-19 1983-12-19 Superheat-and wear-resistant aluminum alloy and its manufacture

Publications (2)

Publication Number Publication Date
JPS60131944A JPS60131944A (en) 1985-07-13
JPH0474402B2 true JPH0474402B2 (en) 1992-11-26

Family

ID=17057359

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58240296A Granted JPS60131944A (en) 1983-12-19 1983-12-19 Superheat-and wear-resistant aluminum alloy and its manufacture

Country Status (1)

Country Link
JP (1) JPS60131944A (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63312901A (en) * 1987-06-16 1988-12-21 Kobe Steel Ltd Heat resistant high tensile al alloy powder and composite ceramics reinforced heat resistant al alloy material using said powder
US4832734A (en) * 1988-05-06 1989-05-23 Inco Alloys International, Inc. Hot working aluminum-base alloys
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