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JPS6310222B2 - - Google Patents
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JPS6310222B2 - - Google Patents

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Publication number
JPS6310222B2
JPS6310222B2 JP59172439A JP17243984A JPS6310222B2 JP S6310222 B2 JPS6310222 B2 JP S6310222B2 JP 59172439 A JP59172439 A JP 59172439A JP 17243984 A JP17243984 A JP 17243984A JP S6310222 B2 JPS6310222 B2 JP S6310222B2
Authority
JP
Japan
Prior art keywords
alloy
rapidly solidified
aluminum alloy
molded
present
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
Application number
JP59172439A
Other languages
Japanese (ja)
Other versions
JPS6152343A (en
Inventor
Shigenori Yamauchi
Susumu Inumaru
Kazuhisa Shibue
Hideo Sano
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.)
Sumitomo Light Metal Industries Ltd
Original Assignee
Sumitomo Light Metal Industries 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 Sumitomo Light Metal Industries Ltd filed Critical Sumitomo Light Metal Industries Ltd
Priority to JP17243984A priority Critical patent/JPS6152343A/en
Publication of JPS6152343A publication Critical patent/JPS6152343A/en
Publication of JPS6310222B2 publication Critical patent/JPS6310222B2/ja
Granted legal-status Critical Current

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  • Manufacture And Refinement Of Metals (AREA)
  • Powder Metallurgy (AREA)

Description

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

産業上の利用分野 本発明は、アルミニウム合金をアトマイズ法、
ロール法などの急冷凝固法によつて急冷し、凝固
させることによつて得るアルミニウム合金の急冷
凝固材(粉末、フレーク、リボン状の形態)か
ら、押出、圧延、鍛造、焼結、高温静水圧プレス
など常法の高温圧縮加工により、所要の形状に成
形してなる成形材に関するものである。 従来の技術 自動車エンジンのコネクテイングロツド、ガス
タービンのインペラー又はフアンブレード、ある
いは超音速航空機体などの材料においては、100
〜400℃での高温強度が必要とされる。 これらの材料をアルミニウム合金にすれば、軽
量化に伴なう多大な利点が得られる。しかし、従
来のアルミニウム合金は150℃を越えると、強度
が大幅に減少するので、上記の用途に用いること
ができなかつた。 しかるところ、近年に至つて上記用途に適する
耐熱アルミニウム合金成形材として、急冷凝固法
によつて得た合金粉末から高温圧縮加工して成形
された、Al−Fe系合金すなわちAl−8Fe−4Ce、
Al−8Fe−2Co、Al−8Fe−2Moなどの成形材が
提供されている。 発明が解決しようとする問題点 前記Al−8Fe−4Ce合金の急冷凝固材から得た
成形材にあつては、Ceが高価であるため、Ce添
加が製品コストの上昇につながること、また前記
のAl−8Fe−2Co及びAl−8Fe−2Mo合金の同様
な成形材にあつては、それらの高温強度が必ずし
も十分でないことなどの欠点をそれぞれ有してい
る。 本発明の目的とするところは、前記のAl−8Fe
−4Ce、Al−8Fe−2Co又はAl−8Fe−2Moなど
のアルミニウム合金の急冷凝固材から常法の高温
圧縮加工によつて得る成形材が有している前記の
欠点を解消した、すなわち高価なCeを添加する
ことなしに、優れた高温強度が得られる新規組成
のアルミニウム合金の急冷凝固材からなる成形材
を提供することにある。 問題点を解決するための手段 本発明は、下記のとおりの特定組成をもつアル
ミニウム合金の急冷凝固材の成形体であつて、金
属間化合物の平均粒径が0.1〜1μmである高温強
度に優れたアルミニウム合金成形材である。 Fe:4〜15% Mo:0.5〜8% Zr:0.3〜8% Ti:0.5〜8% Cr:0.5〜8% Mn:0.5〜8% いずれか1種又は2種以上 Al:実質的に残部 作 用 本発明において急冷凝固材として用いる前記合
金各成分の合金内における作用をそれら含有量と
関連させて述べる。 Fe:急冷凝固時に微細な金属間化合物となつて、
マトリツクス中に分散して、その分散強化作用
により成形材の室温及び高温における強度を高
める。この作用は含有量が4%より少ない場合
には十分でなく、他方含有量が15%を越えると
作用の度合は飽和状態にあるばかりでなく、成
形材の延性が低下する。 Mo:Feを含む金属間化合物をより微細に分散さ
せ、また高温においても該化合物を安定化させ
ることにより成形材においてその高温強度を高
める。この作用は含有量が0.5%より少ない場
合には十分でなく、他方含有量を8%より多く
しても作用の度合は飽和しており、コストの上
昇になる。 Zr:Feを含む金属間化合物の分散を助けて分散
強化作用を向上させる。この作用は比較的低温
側(室温〜150℃)において著しい。この作用
は含有量が0.3%より少ない場合十分でなく、
他方含有量を8%より多くしても作用の度合は
飽和しており、コストの上昇になる。 Ti、Cr、Mn:以上のように、Fe、Mo及びZrを
含むアルミニウム合金に対して、Ti、Cr、Mn
を単独又は2種以上複合して添加する。これら
成分はFeを含む金属間化合物の分散を助け、
分散強化作用を一層向上させ、成形材の強度を
より大にする。これは高温(200℃以上)にお
いて著しい。この作用は含有量が共に0.5%よ
り少ないと十分でなく、一方、共に含有量を8
%より多くしても作用の度合は飽和しており、
コスト上昇をもたらす。 本発明で用いている急冷凝固材はガスアトマイ
ズでつくられるものであるから、冷却速度は103
〜104℃/secと小さい、得られる粉末、フレー
ク、リボン状形態のものの組織はデンドライトセ
ル組織のもので、これを予備圧縮、高温真空脱ガ
ス、成形の常法により、得たものは、金属間化合
物の平均粒径が0.1〜1μmのものとなる。 第1図は後述の実施例No.4の急冷凝固材の組
織を示す顕微鏡写真、第2図は同成形材の組織を
示す顕微鏡写真である。 次に、本発明の実施例について比較例と対比し
て述べる。 実施例 表1に掲げるNo.1〜No.13の合金を溶解し、こ
れら溶湯をArガス・アトマイズ法によつて急冷
し、凝固させて急冷凝固粉末を得た。この粉末を
冷間等方圧プレス(CIP)によつて64φ×100mm
の圧縮物(密度は真空度の70〜80%)とし、これ
をアルミニウム缶に封入して高温真空脱ガスを施
した。次いでこれをビレツトして400℃で、これ
を20mmφの棒に押出した。 別に、No.14の合金については、溶解後連続鋳
造により直径152.4mm(6インチ)のインゴツト
となし、これから44mmφの棒を押出した。次いで
この合金のみについては、T6処理(530℃×
24Hr→湯冷→200℃×20Hr)を施した。 以上のようにして得た各合金棒に対して室温及
び250℃(保持時間100Hr)において引張試験を
行なつた。その結果を表2に示す。 なお、表2の合金棒No.は表1の合金No.に対
応するものである。
Industrial Application Field The present invention is directed to an aluminum alloy atomizing method,
Extrusion, rolling, forging, sintering, and high-temperature isostatic pressing are performed from rapidly solidified aluminum alloy material (powder, flake, ribbon-like form) obtained by rapidly cooling and solidifying by a rapid solidifying method such as a roll method. It relates to a molded material formed into a desired shape by a conventional high-temperature compression process such as pressing. Prior Art In materials such as automobile engine connecting rods, gas turbine impellers or fan blades, or supersonic aircraft bodies, 100
High temperature strength at ~400°C is required. Using aluminum alloys as these materials provides significant advantages in terms of weight reduction. However, the strength of conventional aluminum alloys significantly decreases when the temperature exceeds 150°C, so they could not be used for the above applications. However, in recent years, Al-Fe alloys, namely Al-8Fe-4Ce, which are formed by high-temperature compression processing from alloy powder obtained by rapid solidification, have been developed as heat-resistant aluminum alloy forming materials suitable for the above-mentioned uses.
Molding materials such as Al-8Fe-2Co and Al-8Fe-2Mo are provided. Problems to be Solved by the Invention In the case of a molded material obtained from the rapidly solidified material of the Al-8Fe-4Ce alloy, the addition of Ce leads to an increase in product cost because Ce is expensive, and the above-mentioned problem also arises. Similar forming materials of Al-8Fe-2Co and Al-8Fe-2Mo alloys each have drawbacks such as not necessarily having sufficient high temperature strength. The object of the present invention is the above-mentioned Al-8Fe
- Eliminates the above-mentioned drawbacks of molded materials obtained from rapidly solidified materials of aluminum alloys such as 4Ce, Al-8Fe-2Co or Al-8Fe-2Mo by conventional high-temperature compression processing. The object of the present invention is to provide a molded material made of a rapidly solidified aluminum alloy material with a new composition that provides excellent high-temperature strength without adding Ce. Means for Solving the Problems The present invention is a molded product of a rapidly solidified aluminum alloy material having a specific composition as shown below, which has excellent high-temperature strength and has an intermetallic compound having an average grain size of 0.1 to 1 μm. This is an aluminum alloy molded material. Fe: 4-15% Mo: 0.5-8% Zr: 0.3-8% Ti: 0.5-8% Cr: 0.5-8% Mn: 0.5-8% Any one or more Al: Substantially the remainder Effects The effects of each component of the alloy used as the rapidly solidified material in the present invention in the alloy will be described in relation to their contents. Fe: becomes a fine intermetallic compound during rapid solidification,
It is dispersed in the matrix and its dispersion-strengthening effect increases the strength of the molded material at room and high temperatures. This effect is not sufficient when the content is less than 4%, and on the other hand, when the content exceeds 15%, not only is the degree of effect saturated, but the ductility of the molded material is reduced. By dispersing the intermetallic compound containing Mo:Fe more finely and stabilizing the compound even at high temperatures, the high-temperature strength of the molded material is increased. This effect is not sufficient when the content is less than 0.5%, and on the other hand, even if the content is greater than 8%, the degree of effect is saturated and costs increase. Zr: Helps disperse intermetallic compounds containing Fe and improves dispersion strengthening effect. This effect is remarkable at relatively low temperatures (room temperature to 150°C). This effect is not sufficient when the content is less than 0.3%;
On the other hand, even if the content is higher than 8%, the degree of action is saturated and the cost increases. Ti, Cr, Mn: As mentioned above, for aluminum alloys containing Fe, Mo and Zr, Ti, Cr, Mn
are added singly or in combination of two or more. These components help disperse intermetallic compounds containing Fe,
Further improves the dispersion strengthening effect and increases the strength of the molded material. This is remarkable at high temperatures (200°C or higher). This effect is not sufficient when the content of both is less than 0.5%; on the other hand, when the content of both is less than 8%,
%, the degree of effect is saturated,
resulting in increased costs. Since the rapidly solidified material used in the present invention is made by gas atomization, the cooling rate is 10 3
The structure of the resulting powder, flakes, and ribbons, which is as small as ~10 4 °C/sec, is that of a dendrite cell structure, and the structure obtained by pre-compression, high-temperature vacuum degassing, and molding is as follows: The intermetallic compound has an average particle size of 0.1 to 1 μm. FIG. 1 is a microscopic photograph showing the structure of a rapidly solidified material of Example No. 4, which will be described later, and FIG. 2 is a microscopic photograph showing the structure of the same molded material. Next, examples of the present invention will be described in comparison with comparative examples. Example Alloys No. 1 to No. 13 listed in Table 1 were melted, and the molten metals were rapidly cooled and solidified by Ar gas atomization to obtain rapidly solidified powder. This powder is 64φ×100mm by cold isostatic pressing (CIP).
A compressed product (density: 70-80% of the degree of vacuum) was sealed in an aluminum can and subjected to high-temperature vacuum degassing. Next, this was billeted and extruded at 400°C into a rod of 20 mmφ. Separately, alloy No. 14 was melted and then continuously cast to form an ingot with a diameter of 152.4 mm (6 inches), from which a rod with a diameter of 44 mm was extruded. Then, for this alloy only, T6 treatment (530℃×
24 hours → hot water cooling → 200℃ x 20 hours). A tensile test was conducted on each alloy rod obtained as described above at room temperature and 250°C (holding time 100 hours). The results are shown in Table 2. Note that the alloy rod numbers in Table 2 correspond to the alloy numbers in Table 1.

【表】【table】

【表】【table】

【表】 表2から明らかなように、本発明成形材に係る
合金棒No.1〜No.10の室温強度及び高温強度は、
比較例の合金棒のすべてより高く、特に、急冷凝
固法による合金の高温圧縮成形材用として従来よ
り知られている合金のNo.11〜No.13によるもの
の強度より高くなつている。 本発明において急冷凝固材として用いるアルミ
ニウム合金の真価は、急冷凝固法を適用するとき
に発揮される。急冷凝固法としては、ガス・アト
マイズ法、ロール法、スプラツトクウエンチ法な
どのいずれの方法によつても差し支えないが、通
常、100℃/s以上の冷却速度が得られる方法を
用いるのが適当である。 発明の効果 (1) 従来の、Ce添加アルミニウム合金の急冷凝
固材を用いた高温用成形材に対して、本発明よ
り、急冷凝固材にCe無添加のアルミニウム合
金を用いることによつて、さらに室温強度及び
高温強度が高い当該成形材が低コストで製造で
きる。 (2) 本発明の、急冷凝固材からなる成形材は、従
来の、Al−8Fe−2Co又はAl−8Fe−2Moのア
ルミニウム合金の急冷凝固材からなる成形材よ
りも一層大きい室温強度および高温強度を有す
る。 (3) 本発明の、急冷凝固材からなる成形材は、従
来のインゴツト法による耐熱アルミニウム合金
材が使用できなかつた高温環境、特に150℃以
上にある環境での使用が可能であり、したがつ
てこの環境に使用される機材にアルミニウム合
金材を提供することによつて、機材の軽量化が
得られるので、本発明成形材は、技術的及び経
済的価値が大きい。
[Table] As is clear from Table 2, the room temperature strength and high temperature strength of alloy rods No. 1 to No. 10 related to the molded material of the present invention are as follows:
The strength is higher than all of the alloy rods of the comparative examples, and especially higher than those of alloys No. 11 to No. 13, which are conventionally known for use in high-temperature compression molded materials of alloys produced by rapid solidification. The true value of the aluminum alloy used as the rapid solidification material in the present invention is demonstrated when a rapid solidification method is applied. As the rapid solidification method, any method such as the gas atomization method, roll method, or splat quench method may be used, but it is usually preferable to use a method that can obtain a cooling rate of 100°C/s or more. Appropriate. Effects of the Invention (1) In contrast to the conventional high-temperature forming material using a rapidly solidified Ce-added aluminum alloy material, the present invention uses an aluminum alloy without Ce addition as the rapidly solidified material. The molded material having high room temperature strength and high temperature strength can be manufactured at low cost. (2) The molded material made of the rapidly solidified material of the present invention has higher room temperature strength and high temperature strength than the conventional molded material made of the rapidly solidified material of Al-8Fe-2Co or Al-8Fe-2Mo aluminum alloy. has. (3) The molded material made of the rapidly solidified material of the present invention can be used in high-temperature environments where heat-resistant aluminum alloy materials produced by the conventional ingot method cannot be used, particularly in environments at temperatures above 150°C. By providing aluminum alloy material to equipment used in this environment, the weight of the equipment can be reduced, so the molded material of the present invention has great technical and economic value.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本発明の実施例における急冷凝固材の
金属組織を示す顕微鏡写真、第2図は同じく成形
体の金属組織を示す顕微鏡を示す顕微鏡写真であ
る。
FIG. 1 is a photomicrograph showing the metallographic structure of a rapidly solidified material in an example of the present invention, and FIG. 2 is a photomicrograph showing the metallographic structure of a molded article.

Claims (1)

【特許請求の範囲】[Claims] 1 Fe:4〜15%、Mo:0.5〜8%及びZr:0.3
〜8%と、更にTi:0.5〜8%、Cr:0.5〜8%及
びMn:0.5〜8%の1種又は2種以上を含み、残
部は実質的にAlであるアルミニウム合金の急冷
凝固材の成形体であつて、金属間化合物の平均粒
径が0.1〜1μmであることを特徴とする高温強度
に優れたアルミニウム合金成形材。
1 Fe: 4-15%, Mo: 0.5-8% and Zr: 0.3
-8% and further contains one or more of Ti: 0.5-8%, Cr: 0.5-8% and Mn: 0.5-8%, and the remainder is substantially Al. An aluminum alloy molded material having excellent high-temperature strength, which is a molded product having an intermetallic compound having an average grain size of 0.1 to 1 μm.
JP17243984A 1984-08-21 1984-08-21 Formed material having superior strength at high temperature, made of aluminum alloy material solidified by rapid cooling Granted JPS6152343A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP17243984A JPS6152343A (en) 1984-08-21 1984-08-21 Formed material having superior strength at high temperature, made of aluminum alloy material solidified by rapid cooling

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP17243984A JPS6152343A (en) 1984-08-21 1984-08-21 Formed material having superior strength at high temperature, made of aluminum alloy material solidified by rapid cooling

Publications (2)

Publication Number Publication Date
JPS6152343A JPS6152343A (en) 1986-03-15
JPS6310222B2 true JPS6310222B2 (en) 1988-03-04

Family

ID=15942000

Family Applications (1)

Application Number Title Priority Date Filing Date
JP17243984A Granted JPS6152343A (en) 1984-08-21 1984-08-21 Formed material having superior strength at high temperature, made of aluminum alloy material solidified by rapid cooling

Country Status (1)

Country Link
JP (1) JPS6152343A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6247448A (en) * 1985-08-26 1987-03-02 Toyo Alum Kk Heat resistant aluminum alloy for powder metallurgy adn its manufacture
CA1330400C (en) 1987-12-01 1994-06-28 Seiichi Koike Heat-resistant aluminum alloy sinter and process for production of the same

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60248860A (en) * 1983-10-03 1985-12-09 アライド・コ−ポレ−シヨン Aluminum-transition metal alloy with high strength at high temperatures

Also Published As

Publication number Publication date
JPS6152343A (en) 1986-03-15

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