JPH02149631A - Low thermal expansion aluminum alloy having excellent wear resistance and heat conductivity - Google Patents

Low thermal expansion aluminum alloy having excellent wear resistance and heat conductivity

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Publication number
JPH02149631A
JPH02149631A JP30451188A JP30451188A JPH02149631A JP H02149631 A JPH02149631 A JP H02149631A JP 30451188 A JP30451188 A JP 30451188A JP 30451188 A JP30451188 A JP 30451188A JP H02149631 A JPH02149631 A JP H02149631A
Authority
JP
Japan
Prior art keywords
wear resistance
thermal expansion
alloy
aluminum alloy
billet
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
JP30451188A
Other languages
Japanese (ja)
Inventor
Jiichi Nagai
滋一 永井
Ichizo Tsukuda
市三 佃
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.)
Altemira Co Ltd
Original Assignee
Showa Aluminum Corp
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 Showa Aluminum Corp filed Critical Showa Aluminum Corp
Priority to JP30451188A priority Critical patent/JPH02149631A/en
Publication of JPH02149631A publication Critical patent/JPH02149631A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To obtain the title Al alloy by adding specific amounts of Ni, Si, Cu, Mg and other metallic elements to Al. CONSTITUTION:An Al alloy having the compsn. of which, by weight, 8 to 10% Ni, 4 to 10% Si, 2 to 5% Cu and 0.3 to 2% Mg or furthermore one or more kinds among 0.01 to 1% Cr, 0.01 to 1% Mn, 0.01 to 0.5% Zr, 0.01 to 0.1% V, 0.01 to 1% Ti, 0.01 to 5% Zn and 0.01 to 5% Fe are added and incorporated is poured into a mold heated to its liquidus temp. +100 deg.C and is solidified under pressure into a billet. The billet is extruded into a round bar or the like, is subjected to solution heat treatment, is thereafter water-cooled and is successively subjected to aging treatment, by which the Al alloy material having excellent wear resistance and heat conductivity and having small thermal expansion coefficient can be obtd.

Description

【発明の詳細な説明】 産業上の利用分野 この発明は、例えばピストン、その地熱膨張係数が小さ
く耐摩耗性および熱伝導性の要求される自動車用部品や
各種機械部品等に使用される耐摩耗性及び熱伝導性に優
れた低熱膨張アルミニウム合金に関する。
DETAILED DESCRIPTION OF THE INVENTION Field of Industrial Application This invention is applicable to wear-resistant pistons used in, for example, automobile parts and various mechanical parts that have a small geothermal expansion coefficient and are required to have wear resistance and thermal conductivity. This invention relates to a low thermal expansion aluminum alloy with excellent properties and thermal conductivity.

従来の技術 従来、この種のアルミニウム合金としては、耐摩耗性を
向上させるための元素としてStを添加したAl−SL
系アルミニウム合金が良く知られているところであり、
一般に多く用いられている。
Conventional technology Conventionally, as this type of aluminum alloy, Al-SL has been added with St as an element to improve wear resistance.
aluminum alloys are well known,
Commonly used.

発明が解決しようとする課題 ところが、耐摩耗性の向上のために、Siの添加量を増
加すると、耐摩耗性が向上し、熱膨張係数が低下する反
面、鋳造性、切削性および鍛造性が低下するという問題
があり、自ずからその添加量に制約を受けるものであっ
た。
Problems to be Solved by the Invention However, when increasing the amount of Si added to improve wear resistance, the wear resistance improves and the coefficient of thermal expansion decreases, but the castability, machinability, and forgeability deteriorate. There is a problem that the amount of addition is naturally limited.

この発明はこのような事情に鑑み、耐摩耗性等の機械的
性質に優れ、かつ熱伝導性や熱膨張性等の物理的性質に
優れたアルミニウム合金を提供することを目的としてな
されたものである。
In view of these circumstances, this invention was made with the purpose of providing an aluminum alloy that has excellent mechanical properties such as wear resistance, and excellent physical properties such as thermal conductivity and thermal expansion. be.

課題を解決するための手段 而して、この発明は鋭意研究の結果、Stによる硬質粒
子の他に、Al3Ni金属間化合物を分散させたものと
し、同時にCu及びMgを共存させることによって、耐
摩耗性及び熱膨張性の充分な改善をはかりつ−、同時に
熱伝導性、鋳造性、切削性および鍛造性の改善をはかり
うろことを見出し、か\る知見に基づいて完成し得たも
のである。
As a means to solve the problem, this invention has been developed as a result of intensive research.In addition to hard particles of St, Al3Ni intermetallic compound is dispersed, and at the same time, Cu and Mg are coexisting, thereby improving wear resistance. This work was completed based on the findings of the authors, who found it possible to sufficiently improve the properties of steel and thermal expansibility, while at the same time improving the thermal conductivity, castability, machinability, and forgeability. .

即ち、この発明の第1は、 Ni:8〜10% Si:4〜10% Cu:2〜5% Mg:0.3〜296 を含有し、残部Al及び不可避不純物からなる耐摩耗性
及び熱伝導性に優れた低熱膨張アルミニウム合金である
That is, the first aspect of the present invention has wear resistance and heat resistance, which contains Ni: 8 to 10%, Si: 4 to 10%, Cu: 2 to 5%, Mg: 0.3 to 296, and the balance is Al and inevitable impurities. A low thermal expansion aluminum alloy with excellent conductivity.

そして又、第2の発明は、上記第1発明の必須含有元素
S i、Ni、CuおよびMgのほかに、 Cr:0.01〜1% Mn:0、01〜1% Z r  :  0. 01〜0. 596V:0.0
1〜0.1% Ti:0.01〜1% Zn:0.01〜5% Fe:0.01〜5% のうちの1種または2種以上 を含有し、残部Al及び不可避不純物からなる耐摩耗性
及び熱伝導性に優れた低熱膨張アルミニウム合金である
Furthermore, the second invention provides, in addition to the essential elements Si, Ni, Cu, and Mg of the first invention, Cr: 0.01 to 1% Mn: 0, 01 to 1% Zr: 0. 01~0. 596V: 0.0
Contains one or more of the following: 1 to 0.1% Ti: 0.01 to 1% Zn: 0.01 to 5% Fe: 0.01 to 5%, and the remainder consists of Al and inevitable impurities A low thermal expansion aluminum alloy with excellent wear resistance and thermal conductivity.

なお、この明細書において、「%」はいずれも「重量%
」を示すものである。
In addition, in this specification, "%" refers to "% by weight".
”.

上記合金添加元素の意義とその含を量の限定理由は次の
とおりである。
The significance of the above-mentioned alloy additive elements and the reason for limiting their content are as follows.

即ち、Niは、A、Q3Ni金属間化合物を形成して合
金中に分散し、主として耐摩耗性の向上および熱膨張係
数の低下に寄与するものであり、その含有量が8%未満
では上記効果に乏しく、10%をこえて過多に含有する
と、熱伝導性を阻害する。特に好ましい含有量は、8.
5〜9.5%程度である。
That is, Ni forms the A,Q3Ni intermetallic compound and is dispersed in the alloy, which mainly contributes to improving wear resistance and lowering the coefficient of thermal expansion.If the content is less than 8%, the above effects are not achieved. If the content exceeds 10%, thermal conductivity will be inhibited. A particularly preferable content is 8.
It is about 5 to 9.5%.

Stは耐摩耗性および強度を向上させると共に、熱膨張
係数を低下させるものであり、4%未満では用途によっ
ては充分な効果が得られず、10%を超えると初晶St
により押出時に表面クラックが発生するおそれがある。
St improves wear resistance and strength as well as lowers the coefficient of thermal expansion. If it is less than 4%, sufficient effects may not be obtained depending on the application, and if it exceeds 10%, primary St
This may cause surface cracks during extrusion.

特に好ましい含有量は、7〜9%程度である。A particularly preferable content is about 7 to 9%.

、Cu及びMgは、いずれも強度を高めるためのもので
あり、Cuが2%未満、およびMgが0.3%未満では
この効果が少なく、逆にCuが5%を超え、あるいはM
gが2%を超える場合には、粗大な晶出物が生成し、か
えって機械的性質が劣化する。特に好ましい含有量は、
CUにおいて2.5〜4.5%、Mgにおいて0゜5〜
1,5%程度である。
, Cu, and Mg are all used to increase strength, and if Cu is less than 2% and Mg is less than 0.3%, this effect will be small; on the other hand, if Cu is more than 5% or Mg
When g exceeds 2%, coarse crystallized substances are formed, and the mechanical properties are rather deteriorated. Particularly preferable content is
2.5-4.5% in CU, 0°5-4.5% in Mg
It is about 1.5%.

C「、Mn、Zr、V、Ti、Zn、Feは、いずれも
合金の機械的性質の改善に効果を有するものであり、こ
の発明においてはこの添加効果の点で相互に均等物とし
て評価しうるちのである。いずれもその個々の含有量が
0,01%より少ないときは、上記効果の実現に不十分
であり、逆に規定値をこえて過多に含有(Cr、Mn5
Ti11%超、Zr:0.5%超、■:0.1%超、Z
n、Fe:5%超)しても、上記効果が飽和し、他に格
別有益な効果を奏しない。
C, Mn, Zr, V, Ti, Zn, and Fe are all effective in improving the mechanical properties of the alloy, and in this invention, they are evaluated as equivalent to each other in terms of the effect of addition. When the individual content of any of them is less than 0.01%, it is insufficient to realize the above effect, and conversely, when the content exceeds the specified value and is excessively contained (Cr, Mn5
Ti over 11%, Zr: over 0.5%, ■: over 0.1%, Z
n, Fe: more than 5%), the above effects are saturated and no other particularly beneficial effects are produced.

ところで、本発明合金は常法に従う連続あるいは半連続
鋳造法によっても製造することができるが、加圧凝固法
により好適に製造されるものである。この加圧凝固法を
説明すると次のとおりである。即ち、本発明合金を溶解
し、その溶湯を加圧凝固用金型に注湯して加圧凝固せし
めることにより、欠陥のない結晶粒の均一かつ微細なビ
レットの作成を行うものである。加圧凝固用金型は、こ
れに押出機のコンテナを利用するものとしても良い。即
ち、アルミニウム合金溶湯を直接コンテナに注入し、ス
テムで加圧しつつ凝固させるものとしても良い。もちろ
ん、この場合、上記コンテナの前面は盲ダイスを付設し
て塞ぎ、加圧凝固中の溶湯の吹き出しを防ぐものとする
ことが必要である。また上記注湯に際しては前記金型を
予め300〜350℃程度に加熱しておくものとするこ
とが望ましい。
By the way, although the alloy of the present invention can also be manufactured by a conventional continuous or semi-continuous casting method, it is preferably manufactured by a pressure solidification method. This pressure coagulation method will be explained as follows. That is, by melting the alloy of the present invention and pouring the molten metal into a pressure solidification mold and solidifying it under pressure, a billet with uniform and fine crystal grains without defects is created. The pressurized solidification mold may utilize a container of an extruder. That is, the molten aluminum alloy may be directly poured into the container and solidified while being pressurized by the stem. Of course, in this case, it is necessary to close the front surface of the container with a blind die to prevent the molten metal from blowing out during pressurized solidification. Further, when pouring the molten metal, it is desirable that the mold be preheated to about 300 to 350°C.

これによりビレットに一層微細な組織を得ることを可能
にする。即ち300℃程度未満であると、注湯後前記ア
ルミニウムの凝固が直ぐに開始してしまい、加圧凝固に
よる効果が十分に達成され難い。一方、350℃を越え
る高温に加熱しておくと、冷却速度が遅くなり、晶出物
が成長して上記微細化効果を十分に達成し難いものとな
る傾向がみられる。注湯後すぐさま前記金型内の溶湯を
加圧ピストンにより加圧し、凝固を進行せしめることに
よってビレットを作成する。即ち加圧凝固法によってビ
レットを作成する。この際の加圧力は50Kyflad
以上であれば良く、望ましくは500〜1000/(g
f/d程度とするのが良い。この加圧力の大小はビレッ
トの品質にさして大きな影響を与えるものではない。し
かしながら、50Kfff/cm未満では加圧凝固法に
よる鋳造割れ防止および結晶粒の微細化効果に不十分で
あり、反面例えば1500に9f/alを超えるような
高圧を付加しても、それに要するエネルギーの増大に見
合う効果の比例的向上を見ることができないためむしろ
無益である。このように、所定の加圧状態下においてア
ルミニウム合金を凝固させることにより、鋳造割れを生
じさせることなく、かつ晶出物の小さなビレットを作成
し得る。上記加圧凝固法により作成したビレットは、次
にこれを押出加工して所期するアルミニウム合金材とす
る。ここに、ビレットは一旦冷却された固相状態のもの
を用いても良いが、好ましくは前記加圧凝固の進行によ
り、ビレットの温度が押出し加工に適する温度、例えば
液相温度の約1/2程度にまで低下し半溶融状態となっ
た時点で加圧凝固工程を終了し、すぐさまそのまま押出
機のコンテナに装填して押出しを開始するものとなすこ
とが奨励される。このような手順を採用することにより
、押出し加工に際してのビレットの加熱工程を省くこと
が可能となり、その加熱に要するエネルギーおよび時間
を節約し、合金押出し材の製造能率の向上および製造コ
ストの低減の利益を享受しうる。
This makes it possible to obtain a finer texture in the billet. That is, if the temperature is less than about 300° C., solidification of the aluminum will start immediately after pouring, making it difficult to fully achieve the effect of pressure solidification. On the other hand, if it is heated to a high temperature exceeding 350° C., the cooling rate slows down, and crystallized substances tend to grow, making it difficult to sufficiently achieve the above-mentioned refinement effect. Immediately after pouring the molten metal, the molten metal in the mold is pressurized by a pressurizing piston to advance solidification, thereby creating a billet. That is, a billet is created by a pressure coagulation method. The pressing force at this time is 50Kyflad
or more, preferably 500 to 1000/(g
It is preferable to set it to about f/d. The magnitude of this pressing force does not significantly affect the quality of the billet. However, if the pressure is less than 50Kfff/cm, the effect of preventing casting cracks and refining grains by the pressure solidification method is insufficient.On the other hand, even if a high pressure of more than 9f/al is applied to 1500, the energy required for it is insufficient. It is rather useless as it is not possible to see a proportional improvement in the effect commensurate with the increase. In this manner, by solidifying the aluminum alloy under a predetermined pressurized state, a small billet of crystallized material can be created without causing casting cracks. The billet produced by the above pressure solidification method is then extruded to form the desired aluminum alloy material. Here, the billet may be used in a solid state that has been cooled once, but preferably, the temperature of the billet is adjusted to a temperature suitable for extrusion processing, for example, about 1/2 of the liquidus temperature, by the progress of the pressure solidification. It is recommended that the pressurized solidification process be completed when the temperature has decreased to a certain degree and the mixture has reached a semi-molten state, and that the extruder be immediately loaded into the container of the extruder and extrusion be started. By adopting such a procedure, it is possible to omit the billet heating step during extrusion processing, saving the energy and time required for heating, improving the manufacturing efficiency of alloy extrusions, and reducing manufacturing costs. can enjoy benefits.

発明の効果 この発明に係るアルミニウム合金は、下記の実施例の参
酌によって明らかなように、その合金組成の限定事項の
範囲からそのいずれか1以上が逸脱する比較合金に較べ
て、Si含有量が制限されているにもかかわらず耐摩耗
性、熱伝導性および低熱膨張性の点につき優れた効果を
実現し得るものである。
Effects of the Invention As is clear from the following Examples, the aluminum alloy according to the present invention has a lower Si content than a comparative alloy in which one or more of the alloy compositions deviates from the range of the limitations of the alloy composition. Despite the limitations, it is possible to achieve excellent effects in terms of wear resistance, thermal conductivity, and low thermal expansion.

実施例 第1表に示す本発明合金及び比較合金のそれぞれについ
て、その溶湯を液相温度+100℃に加熱した加圧凝固
用金型に注湯し、1000Kyf/Ciの加圧下で凝固
させてビレットを作成し、このビレットを押出温度49
0℃にて直径12IIIIIの丸棒に押出加工し、49
0℃X6時間の溶体化処理後水冷し、180℃×7時間
の時効処理を施したものを供試材とした。
Examples For each of the present invention alloy and comparative alloy shown in Table 1, the molten metal is poured into a pressure solidification mold heated to the liquidus temperature +100°C, and solidified under a pressure of 1000 Kyf/Ci to form a billet. and extrude this billet at a temperature of 49
Extruded into a round bar with a diameter of 12III at 0°C,
A sample material was obtained by solution treatment at 0°C for 6 hours, water cooling, and aging treatment at 180°C for 7 hours.

そして、この各供試材につき、耐摩耗性、熱伝導率及び
熱膨張係数を調べた。その結果を第2表に示す。
The abrasion resistance, thermal conductivity, and coefficient of thermal expansion of each sample material were then examined. The results are shown in Table 2.

なお、耐摩耗性の試験は、回転円板による大越式摩耗試
験機を用いて、負荷荷重:2.IKy、摩擦距離:60
0m、、摩擦速度:3.67m/S1相手材: FC−
30(J Is) 、試験面:エメリペーパー1200
番仕上げ、の試験条件で摩擦した場合の供試材の比摩耗
量を、’1111定することによって評価した。
The abrasion resistance test was conducted using an Okoshi type abrasion tester using a rotating disk, and the applied load was 2. IKy, friction distance: 60
0m, Friction speed: 3.67m/S1 mating material: FC-
30 (J Is), test surface: Emery Paper 1200
The specific wear amount of the sample material when rubbed under the test conditions of 1111 was evaluated.

〔以下余白〕[Margin below]

上記第2表の結果に示されるように、本発明合金は、比
較合金に較べ、耐摩耗性が一段と向上され、熱伝導率お
よび低熱膨張性のいずれにも優れたものであることを確
認し得た。
As shown in the results in Table 2 above, the alloy of the present invention was confirmed to have much improved wear resistance and superior thermal conductivity and low thermal expansion compared to the comparative alloy. Obtained.

以上that's all

Claims (2)

【特許請求の範囲】[Claims] (1)Ni:8〜10% Si:4〜10% Cu:2〜5% Mg:0.3〜2% を含有し、残部Al及び不可避不純物からなる耐摩耗性
及び熱伝導性に優れた低熱膨張アルミニウム合金。
(1) Contains Ni: 8-10% Si: 4-10% Cu: 2-5% Mg: 0.3-2%, with the balance being Al and unavoidable impurities. Excellent wear resistance and thermal conductivity. Low thermal expansion aluminum alloy.
(2)Ni:8〜10% Si:4〜10% Cu:2〜5% Mg:0.3〜2% を含有し、かつ、 Cr:0.01〜1% Mn:0.01〜1% Zr:0.01〜0.5% V:0.01〜0.1% Ti:0.01〜1% Zn:0.01〜5% Fe:0.01〜5% のうちの1種または2種以上 を含有し、残部Al及び不可避不純物からなる耐摩耗性
及び熱伝導性に優れた低熱膨張アルミニウム合金。
(2) Contains Ni: 8-10% Si: 4-10% Cu: 2-5% Mg: 0.3-2%, and Cr: 0.01-1% Mn: 0.01-1 % Zr: 0.01-0.5% V: 0.01-0.1% Ti: 0.01-1% Zn: 0.01-5% Fe: 0.01-5% One type Or a low thermal expansion aluminum alloy containing two or more of them, the balance being Al and inevitable impurities, and having excellent wear resistance and thermal conductivity.
JP30451188A 1988-11-30 1988-11-30 Low thermal expansion aluminum alloy having excellent wear resistance and heat conductivity Pending JPH02149631A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
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Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP30451188A JPH02149631A (en) 1988-11-30 1988-11-30 Low thermal expansion aluminum alloy having excellent wear resistance and heat conductivity

Publications (1)

Publication Number Publication Date
JPH02149631A true JPH02149631A (en) 1990-06-08

Family

ID=17933917

Family Applications (1)

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Country Status (1)

Country Link
JP (1) JPH02149631A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04323343A (en) * 1991-04-24 1992-11-12 Showa Alum Corp Aluminum alloy excellent in wear resistance
JPH055147A (en) * 1991-06-26 1993-01-14 Showa Alum Corp Low thermal expansion aluminum alloy with excellent wear resistance
JPH055146A (en) * 1991-06-26 1993-01-14 Showa Alum Corp Aluminum alloy excellent in wear resistance and thermal conductivity
US5374295A (en) * 1992-03-04 1994-12-20 Toyota Jidosha Kabushiki Kaisha Heat resistant aluminum alloy powder, heat resistant aluminum alloy and heat and wear resistant aluminum alloy-based composite material
US5409661A (en) * 1991-10-22 1995-04-25 Toyota Jidosha Kabushiki Kaisha Aluminum alloy
US5464463A (en) * 1992-04-16 1995-11-07 Toyota Jidosha Kabushiki Kaisha Heat resistant aluminum alloy powder heat resistant aluminum alloy and heat and wear resistant aluminum alloy-based composite material
US5614036A (en) * 1992-12-03 1997-03-25 Toyota Jidosha Kabushiki Kaisha High heat resisting and high abrasion resisting aluminum alloy
CN106702226A (en) * 2016-12-20 2017-05-24 重庆顺博铝合金股份有限公司 Aluminum alloy used for preparing engine cylinder cover and preparation method for aluminum alloy

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61259830A (en) * 1985-05-10 1986-11-18 Showa Alum Corp Production of wear resistant aluminum alloy extrudate having excellent machineability
JPS61259829A (en) * 1985-05-10 1986-11-18 Showa Alum Corp Production of wear resistant aluminum alloy extrudate

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61259830A (en) * 1985-05-10 1986-11-18 Showa Alum Corp Production of wear resistant aluminum alloy extrudate having excellent machineability
JPS61259829A (en) * 1985-05-10 1986-11-18 Showa Alum Corp Production of wear resistant aluminum alloy extrudate

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04323343A (en) * 1991-04-24 1992-11-12 Showa Alum Corp Aluminum alloy excellent in wear resistance
JPH055147A (en) * 1991-06-26 1993-01-14 Showa Alum Corp Low thermal expansion aluminum alloy with excellent wear resistance
JPH055146A (en) * 1991-06-26 1993-01-14 Showa Alum Corp Aluminum alloy excellent in wear resistance and thermal conductivity
US5409661A (en) * 1991-10-22 1995-04-25 Toyota Jidosha Kabushiki Kaisha Aluminum alloy
US5374295A (en) * 1992-03-04 1994-12-20 Toyota Jidosha Kabushiki Kaisha Heat resistant aluminum alloy powder, heat resistant aluminum alloy and heat and wear resistant aluminum alloy-based composite material
US5464463A (en) * 1992-04-16 1995-11-07 Toyota Jidosha Kabushiki Kaisha Heat resistant aluminum alloy powder heat resistant aluminum alloy and heat and wear resistant aluminum alloy-based composite material
US5614036A (en) * 1992-12-03 1997-03-25 Toyota Jidosha Kabushiki Kaisha High heat resisting and high abrasion resisting aluminum alloy
CN106702226A (en) * 2016-12-20 2017-05-24 重庆顺博铝合金股份有限公司 Aluminum alloy used for preparing engine cylinder cover and preparation method for aluminum alloy

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