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JP2729479B2 - Manufacturing method of aluminum alloy excellent in high temperature strength - Google Patents
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JP2729479B2 - Manufacturing method of aluminum alloy excellent in high temperature strength - Google Patents

Manufacturing method of aluminum alloy excellent in high temperature strength

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Publication number
JP2729479B2
JP2729479B2 JP13865586A JP13865586A JP2729479B2 JP 2729479 B2 JP2729479 B2 JP 2729479B2 JP 13865586 A JP13865586 A JP 13865586A JP 13865586 A JP13865586 A JP 13865586A JP 2729479 B2 JP2729479 B2 JP 2729479B2
Authority
JP
Japan
Prior art keywords
weight
alloy
temperature strength
aluminum alloy
strength
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
JP13865586A
Other languages
Japanese (ja)
Other versions
JPS62294144A (en
Inventor
淳 守部
充 安達
大石  朗
敏郎 猿渡
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.)
Mitsui Aluminum Co Ltd
Original Assignee
Mitsui 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 Mitsui Aluminum Co Ltd filed Critical Mitsui Aluminum Co Ltd
Priority to JP13865586A priority Critical patent/JP2729479B2/en
Publication of JPS62294144A publication Critical patent/JPS62294144A/en
Application granted granted Critical
Publication of JP2729479B2 publication Critical patent/JP2729479B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Description

【発明の詳細な説明】 <産業上の利用分野> 本発明は高温強度に優れたアルミニウム合金の製造方
法に関するものである。 <従来の技術及びその問題点> 内燃機関のピストン用材料をはじめ高温強度が要求さ
れるアルミニウム系材料としては、JIS規格AC8A,AC9Aや
AA規格A390等の合金があるが、これらの合金もその耐用
温度がさほど高くはないので近年急冷凝固法により更に
高温強度を向上せしめる研究が盛んに行われている。 ところが現在行なわれている急冷凝固法は、原料とし
て用いる急冷凝固材を出来る限り急速に冷却しようとい
う考え方から、粉末あるいはフレーク状の原料を用いて
いる。粉末やフレーク状材は確かに冷却速度を大きくな
す事は出来るが、表面積が大過ぎるが為に、表面に付着
している酸化物をはじめとする不純物が多くなる事、更
にその後の熱間成形段階で密着接合しなければならない
面積も大となるが為に成形体その物としてはそれ程大き
な強度の向上が望めないという事を確認した。 勿論粉末やフレーク状材を得る際に不活性ガス中で冷
却する等の対策を採れば表面の酸化物等は少なくはなる
が、それだけ高価となるし、その割には効果が少ないの
である。 <問題点を解決する為の手段> 本発明は上記問題点を解消し、高温強度が優れた成形
体を容易に造ることが出来る方法を提供せんとするもの
であり、その要旨は溶融紡糸法によって得られたFe3〜
9重量%、残部Alなる組成を有する合金繊維を出発原料
とし、該出発原料を冷間圧縮成形後乾燥を行ない、次い
で熱間押出し成形を行うことを特徴とする高温強度に優
れたアルミニウム合金の製造方法並びに溶融紡糸法によ
って得られたFe3〜9重量%と、10〜25重量%のSi,1〜
5重量%のNn,1〜5重量%のNi,1〜5重量%のCu,0.1〜
5重量%のMgの1種あるいは2種以上と、残部Alなる組
成を有する合金繊維を出発原料とし、該出発原料を冷間
圧縮成形後乾燥を行ない、次いで熱間押出し成形を行な
うことを特徴とする高温強度に優れたアルミニウム合金
の製造方法である。 <作用> 本発明の方法は、例えば本件出願人が先に出願した特
開昭59−82411号公報で示される様な溶融状の合金を大
気中に直接噴出させ急冷凝固させて得られる合金繊維を
出発原料とする所に大きな特長がある。この様にして得
られる合金繊維は、急冷凝固によってFeをはじめ、合金
成分たる各元素が微細な金属間化合物を形成し、高温域
での機械的強度を向上させるという所謂急冷凝固材特有
の効果を有する事は勿論、通常の粉末やフレーク状の急
冷凝固材と比べて、比表面積が小さいという点が異なっ
ている。その為に酸化物等の表面に付着する不純物量が
少なく、かつその後の熱間押出し成形時に互いに密着接
合しなければならない面積もそれだけ少なくなり、得ら
れる成形体の高温強度が大きく向上するのである。 本発明に於いて用いるアルミニウム合金の組成につい
て、その組成限定理由は以下の通りである。 まずFeは、急冷凝固により微細な金属間化合物を形成
し、マトリックス中に均一に分散し、高温域での機械的
強度を向上せしめるが、3重量%より少ないとその効果
が十分ではなく、9重量%を越えても高温強度の上昇は
少なく逆に伸び率が少なくなり加工性が悪くなるので3
〜9重量%とする。次にFe以外に添加するSi,Mn,Ni,Cu,
Mgについては、その用途に応じこれらの中の少なくとも
1種以上を添加するものであり、Siは高温強度の向上,
熱膨張係数の低下,耐磨耗性の向上の為に添加するが、
その様な効果は10重量%未満では殆ど発現されず、逆に
25重量%を越えてもあまり差がない、Mn及びNiは急冷凝
固によりFeと共存する微細な金属間化合物を形成し、高
温強度を高めるが1重量%未満ではその効果が十分では
なく、5重量%を越えても高温強度の向上はあまり期待
出来ない。次にCuは室温及び高温強度の向上の効果があ
るが、1重量%未満ではその効果が少なく、逆に5重量
%を越えると耐食性及び加工性が悪くなる、Mgは室温強
度の向上の効果があるが、0.1重量%未満ではその効果
が少なく、5重量%を越えてもその効果の増大は少なく
加工性が悪くなる。 <実施例> 以下本発明の実施例を、比較例と共に詳述する。 第1表No.1〜No.14に示す様な組成を有する合金を、
溶融状態から特開昭59−82411号公報に示される様な方
法により、大気中へ噴出し、急冷凝固させて、平均繊維
径100μmの合金繊維を得た。この合金繊維を冷間圧縮
により50mmφ×110mmLに予成形(充填率約70%)後、20
0℃で2時間乾燥を行ない、引き続きこの予成形材を400
℃で熱間押出しを行ない20mmφの丸棒を作製した(押出
し比6.2)。これらの押出し材を300℃で72時間加熱した
後室温に冷却し、高温引張試験片を作製し300℃で引張
試験を行ない機械的性質を求めた結果を第2表に示す。 又従来合金としてのNo.15〜No.17については、黒鉛る
つぼ中で溶融し、所定の溶湯処理を行った後、金型に鋳
込みインゴットを作り、T6処理をなした後、同様の高温
引張試験を行った結果を第2表に示す。 この第1表から今回の合金開発の基本となる本発明の
Al−Fe組成のNo.1,No.2と、その比較合金であるNo.12,N
o13を比較するために、第1図に示すように第2表から
引張強さと伸び率との関係を示すグラフ図を作成した。 このグラフ図から本発明請求範囲であるFeから5重量
%であるNo.1とFeが8重量%であるNo.2と比較例として
Feが2重量%であるNo.12とFeが10重量%であるNo.13と
を比較するとNo.12では引張強さが著しく低下し、又No.
13ではFeを8重量%から10重量%に増加しても引張強度
はさほど増加せずに逆に伸びの減少が著しくなるので、
Fe重量%を高くすることにより加工性の悪化を考慮した
場合、Fe3〜9重量%範囲とすることに合理性がある。 次にAl−Fe合金系にさらに他の合金成分を添加した本
発明のNo.3〜No.11と比較合金であるNo.13,No.14および
従来合金であるNo.15〜No.17を比較するために、第2図
に示すように第2表から引張強さと伸び率との関係を示
すグラフ図を作成した。 更にFe以外の成分Si17重量%、Cu4.5重量%、Mg0.6重
量%組成が同じものNo.6,No.7,No.8と比較例No.14とを
実線で結んだ。 この結果、Fe0.2重量%である比較合金No.14と本発明
合金No.6〜No.8とを比較した場合、引張強さが著しく低
下していることが判明した。 又従来合金であるNo.15〜No.17では本発明合金と比較
合金よりも引張強さおよび伸び率ともに低下しているこ
とが判明した。 なおAl−Fe系合金にさらに他の合金成分を添加した場
合では、Al−Fe系合金に比べ強度と伸びの機械的性質が
やや劣るが、Si添加による耐磨耗性や熱膨張率の低下の
改善などがなされている。 <発明の効果> 以上述べて来た如く、本発明方法によれば、出発原料
として溶融紡糸法による合金繊維を用いているので、急
冷凝固材としての特質は十分に維持し乍らも、成形体内
へ含有される不純物を極力少なくする事が出来、しかも
密着接合しなければならない面積が少ないという特長を
も活かし、結果として高温強度に優れた成形体を得る事
が出来るものである。 更に本発明方法は溶融紡糸の条件を変えることにより
任意の径及びアスペクト比を持つ合金繊維が得られる為
に最終製品の用途に応じ種々異なった性質の成形体とす
ることが出来るという特長をも有する。
The present invention relates to a method for producing an aluminum alloy having excellent high-temperature strength. <Conventional technology and its problems> Aluminum materials that require high-temperature strength, including materials for pistons of internal combustion engines, include JIS standard AC8A and AC9A.
Although there are alloys such as AA standard A390, these alloys do not have very high service temperatures, and in recent years, studies to further improve the high-temperature strength by rapid solidification have been actively conducted. However, the rapid solidification method currently used uses a powdery or flake-like raw material from the viewpoint of cooling a rapidly solidified material used as a raw material as quickly as possible. Although the cooling rate of powder and flakes can be increased, the surface area is too large, so that impurities such as oxides adhering to the surface increase, and the subsequent hot forming step However, it was confirmed that the molded article itself could not be expected to have such a large improvement in strength because the area required to be closely bonded to the molded article became large. Of course, when taking measures such as cooling in an inert gas when obtaining powders or flakes, oxides on the surface are reduced, but they are more expensive and less effective. <Means for Solving the Problems> The present invention has been made to solve the above problems and to provide a method capable of easily producing a molded article having excellent high-temperature strength. Fe3 obtained by
An aluminum alloy having excellent high-temperature strength, wherein alloy fibers having a composition of 9% by weight and the balance of Al are used as a starting material, and the starting material is subjected to cold compression molding, drying, and then hot extrusion molding. Production method and Fe3 to 9% by weight obtained by melt spinning method and 10 to 25% by weight of Si, 1 to
5% by weight of Nn, 1 to 5% by weight of Ni, 1 to 5% by weight of Cu, 0.1 to
One or more kinds of Mg of 5% by weight and a balance of Al are used as a starting material, and the starting material is cold-compressed, dried, and then hot-extruded. This is a method for producing an aluminum alloy having excellent high-temperature strength. <Function> The method of the present invention is to provide an alloy fiber obtained by directly injecting a molten alloy into the atmosphere and rapidly cooling and solidifying the alloy as disclosed in Japanese Patent Application Laid-Open No. 59-82411 filed by the present applicant. There is a great feature in using as a starting material. The alloy fiber obtained in this way has a unique effect of the so-called rapidly solidified material in that each element, including Fe, forms a fine intermetallic compound by rapid solidification and improves the mechanical strength in a high temperature range. Of course, the difference is that the specific surface area is smaller than that of an ordinary powder or flake-like rapidly solidified material. Therefore, the amount of impurities adhering to the surface of oxides and the like is small, and the area that must be closely bonded to each other during the subsequent hot extrusion molding is also reduced accordingly, and the high-temperature strength of the obtained molded body is greatly improved. . The reasons for limiting the composition of the aluminum alloy used in the present invention are as follows. First, Fe forms a fine intermetallic compound by rapid solidification, is uniformly dispersed in a matrix, and improves mechanical strength in a high temperature range. However, if less than 3% by weight, its effect is not sufficient, and 9 Even if the content exceeds 10% by weight, the increase in high-temperature strength is small, and conversely, the elongation is reduced and workability deteriorates.
To 9% by weight. Next, Si, Mn, Ni, Cu,
For Mg, at least one of them is added depending on the application, and Si improves high temperature strength,
It is added to lower the coefficient of thermal expansion and improve wear resistance.
Such effects are hardly exhibited at less than 10% by weight,
Even if it exceeds 25% by weight, Mn and Ni form fine intermetallic compounds coexisting with Fe by rapid solidification, and increase the high-temperature strength. Even if it exceeds 10% by weight, improvement in high-temperature strength cannot be expected very much. Next, Cu has the effect of improving the room temperature and high temperature strength, but less than 1% by weight has little effect, and if it exceeds 5% by weight, the corrosion resistance and workability deteriorate. On the other hand, Mg has the effect of improving the room temperature strength. However, if the content is less than 0.1% by weight, the effect is small, and if it exceeds 5% by weight, the effect is not increased much and the processability is deteriorated. <Examples> Hereinafter, examples of the present invention will be described in detail along with comparative examples. An alloy having a composition as shown in Table 1 No. 1 to No. 14
From the molten state, it was injected into the atmosphere by rapid cooling and solidification by the method described in JP-A-59-82411 to obtain an alloy fiber having an average fiber diameter of 100 μm. After pre-forming this alloy fiber to 50mmφ × 110mmL by cold compression (filling rate about 70%),
Dry at 0 ° C for 2 hours.
A 20 mmφ round bar was produced by hot extrusion at a temperature of ° C. (extrusion ratio 6.2). These extruded materials were heated at 300 ° C. for 72 hours and then cooled to room temperature to prepare high-temperature tensile test pieces, which were subjected to a tensile test at 300 ° C. to determine the mechanical properties. Table 2 shows the results. For No. 15 to No. 17 as conventional alloys, they were melted in a graphite crucible, subjected to a prescribed molten metal treatment, made into an ingot in a mold, subjected to T6 treatment, and then subjected to the same high-temperature tensile Table 2 shows the results of the test. Table 1 shows that the alloy of the present invention
No.1 and No.2 of Al-Fe composition and No.12 and N
In order to compare o13, a graph showing the relationship between tensile strength and elongation was prepared from Table 2 as shown in FIG. From this graph, No. 1 which is 5% by weight of Fe and No. 2 which is 8% by weight of Fe, which are claims of the present invention, and Comparative Example
When No. 12 having 2% by weight of Fe is compared with No. 13 having 10% by weight of Fe, the tensile strength of No. 12 is significantly reduced,
In the case of 13, even if Fe is increased from 8% by weight to 10% by weight, the tensile strength does not increase so much and conversely the elongation decreases significantly.
When considering the deterioration of workability by increasing the Fe weight%, it is reasonable to set the range of Fe 3 to 9 wt%. Next, No. 3 to No. 11 of the present invention in which another alloy component was further added to the Al-Fe alloy system, No. 13 and No. 14 as comparative alloys, and No. 15 to No. 17 as conventional alloys. In order to compare the above, a graph showing the relationship between tensile strength and elongation was created from Table 2 as shown in FIG. Further, No. 6, No. 7, No. 8 having the same composition of 17% by weight of Si, 4.5% by weight of Cu, and 0.6% by weight of Mg other than Fe and Comparative Example No. 14 were connected by a solid line. As a result, when the comparative alloy No. 14 having 0.2% by weight of Fe was compared with the alloys Nos. 6 to 8 of the present invention, it was found that the tensile strength was significantly reduced. In addition, it was found that in the conventional alloys No. 15 to No. 17, both the tensile strength and the elongation were lower than those of the alloy of the present invention and the comparative alloy. When other alloy components are further added to the Al-Fe alloy, the mechanical properties of strength and elongation are slightly inferior to those of the Al-Fe alloy, but the wear resistance and the coefficient of thermal expansion are reduced by the addition of Si. Improvements have been made. <Effects of the Invention> As described above, according to the method of the present invention, since the alloy fiber obtained by the melt spinning method is used as a starting material, the characteristics as a rapidly solidified material can be maintained while the molding is sufficiently maintained. Impurities contained in the body can be reduced as much as possible, and the advantage that the area which must be in close contact bonding is small is utilized, and as a result, a molded article excellent in high-temperature strength can be obtained. Further, the method of the present invention also has the advantage that by changing the conditions of melt spinning, an alloy fiber having an arbitrary diameter and an aspect ratio can be obtained, so that a molded article having various properties can be obtained according to the use of the final product. Have.

【図面の簡単な説明】 第1図は本願発明のAl−Fe系合金と、その比較例との引
張強さと伸び率の関係を示すグラフ図。 第2図は本願発明のAl−Fe系合金に更に他の合金成分を
添加した場合と、その比較例および従来合金との引張強
さと伸び率の関係を示すグラフ図。
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a graph showing the relationship between tensile strength and elongation of an Al—Fe alloy of the present invention and a comparative example. FIG. 2 is a graph showing the relationship between the tensile strength and the elongation of the Al-Fe alloy of the present invention in which other alloy components are further added, the comparative example, and the conventional alloy.

Claims (1)

(57)【特許請求の範囲】 1.溶融紡糸法によって得られたFe3〜9重量%、残部A
lなる組成を有する合金繊維を出発原料とし、該出発原
料を冷間圧縮成形後乾燥を行ない、次いで熱間押出し成
形を行うことを特徴とする高温強度に優れたアルミニウ
ム合金の製造方法。 2.溶融紡糸法によって得られたFe3〜9重量%と、10
〜25重量%のSi,1〜5重量%のMn,1〜5重量%のNi,1〜
5重量%のCu,0.1〜5重量%のMgの1種あるいは2種以
上と、残部Alなる組成を有する合金繊維を出発原料と
し、該出発原料を冷間圧縮成形後乾燥を行ない、次いで
熱間押出し成形を行なうことを特徴とする高温強度に優
れたアルミニウム合金の製造方法。
(57) [Claims] Fe3-9% by weight obtained by melt spinning method, balance A
(1) A method for producing an aluminum alloy having excellent high-temperature strength, comprising using an alloy fiber having a composition of 1 as a starting material, subjecting the starting material to cold compression molding, drying, and then performing hot extrusion. 2. Fe3 to 9% by weight obtained by the melt spinning method;
~ 25 wt% Si, 1-5 wt% Mn, 1-5 wt% Ni, 1 ~
An alloy fiber having a composition of 5% by weight of Cu, 0.1 to 5% by weight of Mg, and the balance of Al and a balance of Al is used as a starting material. A method for producing an aluminum alloy having excellent high-temperature strength, comprising performing cold extrusion.
JP13865586A 1986-06-13 1986-06-13 Manufacturing method of aluminum alloy excellent in high temperature strength Expired - Lifetime JP2729479B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP13865586A JP2729479B2 (en) 1986-06-13 1986-06-13 Manufacturing method of aluminum alloy excellent in high temperature strength

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13865586A JP2729479B2 (en) 1986-06-13 1986-06-13 Manufacturing method of aluminum alloy excellent in high temperature strength

Publications (2)

Publication Number Publication Date
JPS62294144A JPS62294144A (en) 1987-12-21
JP2729479B2 true JP2729479B2 (en) 1998-03-18

Family

ID=15227051

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13865586A Expired - Lifetime JP2729479B2 (en) 1986-06-13 1986-06-13 Manufacturing method of aluminum alloy excellent in high temperature strength

Country Status (1)

Country Link
JP (1) JP2729479B2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0699772B2 (en) * 1988-09-08 1994-12-07 本田技研工業株式会社 High strength aluminum alloy for machine structural members
DE102007056298A1 (en) * 2007-11-22 2009-05-28 Bayerische Motoren Werke Aktiengesellschaft Piston for internal combustion engine, suitable for use in motor sports, is hardened by very rapid cooling of specified composition
CN117888010B (en) * 2024-03-15 2024-06-04 中铝材料应用研究院有限公司 High-silicon aluminum alloy and preparation method and application thereof

Also Published As

Publication number Publication date
JPS62294144A (en) 1987-12-21

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