JPH05117797A - Heat and creep resistant aluminum alloy excellent in toughness - Google Patents

Heat and creep resistant aluminum alloy excellent in toughness

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Publication number
JPH05117797A
JPH05117797A JP2414154A JP41415490A JPH05117797A JP H05117797 A JPH05117797 A JP H05117797A JP 2414154 A JP2414154 A JP 2414154A JP 41415490 A JP41415490 A JP 41415490A JP H05117797 A JPH05117797 A JP H05117797A
Authority
JP
Japan
Prior art keywords
alloy
toughness
less
heat
aluminum alloy
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
JP2414154A
Other languages
Japanese (ja)
Inventor
Jun Kusui
潤 楠井
Masahiko Kawai
正彦 川井
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.)
Toyo Aluminum KK
Original Assignee
Toyo Aluminum KK
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 Toyo Aluminum KK filed Critical Toyo Aluminum KK
Priority to JP2414154A priority Critical patent/JPH05117797A/en
Publication of JPH05117797A publication Critical patent/JPH05117797A/en
Pending legal-status Critical Current

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  • Powder Metallurgy (AREA)

Abstract

PURPOSE:To provide an Al alloy having excellent strength and creep resistance at high temp. and also having excellent toughness at ordinary temp., by powder metallurgical processing. CONSTITUTION:This Al alloy consists of 5-<10% Si, 2-7% Fe, 1-5% Ni, 0.5-<2% Mo, 0.3-<2% Zr (Mo+Zr<2%) and the balance essentially Al.

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、靭性ならびに耐熱強度
および耐クリープ特性に優れたアルミニウム合金に関す
る。なお、本明細書においては、“%”とあるのは、
“重量%”を意味する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an aluminum alloy excellent in toughness, heat resistance and creep resistance. In this specification, "%" means
Means "wt%".

【0002】[0002]

【従来技術とその問題点】粉末冶金法(以下PM法とい
う)により製造されたアルミニウム合金(以下Al合金
という)は、インゴット冶金法(以下IM法という)に
より製造されたAl合金に比して、より多くの添加元素
をより均一にAlマトリクス中に分散させることが出来
るので、IM法では得られなかった優れた耐熱性、耐摩
耗性などを具備している。
2. Description of the Related Art Aluminum alloys (hereinafter referred to as Al alloys) manufactured by powder metallurgy (hereinafter referred to as PM method) are compared with Al alloys manufactured by ingot metallurgy (hereinafter referred to as IM method). Since more additive elements can be more uniformly dispersed in the Al matrix, it has excellent heat resistance and wear resistance which cannot be obtained by the IM method.

【0003】PM法によるAl製品の製造に際しては、
通常、急冷凝固させて製造した粉末、フレークまたはリ
ボン状の材料を使用して、先ず熱間押出し成形を行い、
次いで得られた成形ビレットを使用して、各種成形製品
を得ている。この方法によれば、熱間押出し時の剪断力
によって、個々の粉末、フレークまたはリボンの表面の
酸化皮膜が破られ、露出したAl面同志での結合が得ら
れる。粉末圧延法および粉末鍛造法によっても、酸化皮
膜の破壊は生じるが、個々の粉末にかかる剪断力および
変形量が、押出し時における程大きくないため、結合
は、押出しによる場合ほどには、強固とはならない。
When manufacturing an Al product by the PM method,
Usually, using powder, flakes or ribbon-shaped material produced by rapid solidification, first hot extrusion molding,
Next, various molded products are obtained by using the obtained molded billet. According to this method, the oxide film on the surface of each powder, flake or ribbon is broken by the shearing force at the time of hot extrusion, and a bond between the exposed Al surfaces is obtained. The powder rolling method and the powder forging method also cause the destruction of the oxide film, but the shearing force and the amount of deformation applied to the individual powders are not so large as during extrusion, so the bond is as strong as when extruding. Don't

【0004】本発明者は、先にAl−Si系にFe、C
rなどの遷移金属元素を添加した合金を使用する場合に
は、10以下という比較的低い押出し比においても、さ
らには2〜5という極めて低い押出し比においても、十
分に強固な成形体が得られることを見出した(特願昭6
3−115625号)。しかしながら、その後の研究に
より、特願昭63−115625号に開示されたAl合
金組成範囲の一部のものは、特に厳しい耐熱強度および
耐クリープ性が要求される部材としての性能を十分に満
足しないことが判明した。また、高温での強度および耐
クリープ性に優れている組成範囲の合金には、常温での
靭性が不充分であるものが存在することも判明した。
The inventor of the present invention first found that Fe and C were added to the Al--Si system.
When an alloy to which a transition metal element such as r is added is used, a sufficiently strong molded body can be obtained even at a relatively low extrusion ratio of 10 or less, and even at an extremely low extrusion ratio of 2 to 5. I found out that
3-115625). However, as a result of subsequent research, some of the Al alloy composition ranges disclosed in Japanese Patent Application No. 63-115625 do not sufficiently satisfy the performance as members requiring particularly severe heat resistance and creep resistance. It has been found. It was also found that there are alloys having a composition range that is excellent in strength and creep resistance at high temperatures and has insufficient toughness at room temperature.

【0005】[0005]

【問題点を解決するための手段】本発明者は、上記の如
き技術の現状に鑑みてさらに研究を進めた結果、新たな
組成のAl合金が、例えば300℃程度の高温における
耐熱強度および耐クリープ性にも極めて優れているとと
もに、常温での靭性にも優れていることを見出した。
As a result of further research in view of the current state of the art as described above, the present inventor has found that an Al alloy having a new composition has a high heat resistance and a high resistance at a high temperature of about 300 ° C., for example. It was found that the creep property is also extremely excellent and the toughness at room temperature is also excellent.

【0006】すなわち、本発明は、下記のAl合金を提
供するものである: 1 (イ)Si5%以上且つ10%未満、(ロ)Fe2
〜7%、(ハ)Ni1〜5%、(ニ)Mo0.5%以上
且つ2%未満および(ホ)Zr0.3%以上〜2%未満
(但しMoとZrの合計量は2%未満である)を含有
し、残余が実質的にAlからなる靭性に優れた耐熱耐ク
リープ性アルミニウム合金、および 2 さらにCu0.3〜6%およびMg0.3〜5%の
少なくとも1種を含む上記第1項に記載の耐熱耐クリー
プ性アルミニウム合金。」
[0006] That is, the present invention provides the following Al alloys: 1 (a) Si 5% or more and less than 10%, (b) Fe2
~ 7%, (C) Ni 1-5%, (D) Mo 0.5% or more and less than 2% and (e) Zr 0.3% or more to less than 2% (however, the total amount of Mo and Zr is less than 2%. 1) and a heat-resistant and creep-resistant aluminum alloy having excellent toughness, the balance being substantially Al, and 2) the first alloy further containing at least one of Cu 0.3 to 6% and Mg 0.3 to 5%. The heat-resistant and creep-resistant aluminum alloy according to the item. "

【0007】本発明において使用するAl合金粉末は、
(イ)Si5%以上且つ10%未満、(ロ)Fe2〜7
%、(ハ)Ni1〜5%、(ニ)Mo0.5%以上且つ
2%未満および(ホ)Zr0.3%以上〜2%未満(但
しMoとZrの合計量は2%未満である)を含有するこ
とを必須とする。Siを5〜10%未満含有するこの組
成範囲内のAl合金は、低い押出し比であっても個々の
粉末同志が十分強固に結合することが可能で、実施例に
示す様に、押出し比にかかわらずほぼ一定の強度と伸び
を示す。Siの含有量を10〜30%とした場合にも、
同様の効果が得られるが、Alマトリックス中に占める
Si粒子の体積含有率が高くなるので、常温における靭
性が低下する。FeおよびNiは、Alの耐熱性および
強度を改善する成分である。Fe2〜7%およびNi1
〜5%を含む合金は、耐熱性、強度および靭性において
バランスのとれた特性を示す。これらの含有量が、上記
の下限値を上回る場合には、耐熱性及び強度の改善が十
分でなく、一方、上限値を上回る場合には、耐熱性およ
び強度は向上するものの、靭性が低下する。Moおよび
Zrは、Alの耐熱性、耐クリープ性および強度を改善
する成分である。これらの含有量が、上記の下限値を下
回る場合には、これらの特性の改善が十分に行われない
のに対し、上限値(合計量としても2%未満)を上回る
場合には、やはり靭性が低下する。
The Al alloy powder used in the present invention is
(A) Si 5% or more and less than 10%, (b) Fe2 to 7
%, (C) Ni 1 to 5%, (d) Mo 0.5% or more and less than 2% and (e) Zr 0.3% or more to less than 2% (however, the total amount of Mo and Zr is less than 2%). Is required to be included. An Al alloy containing Si in an amount of less than 5 to 10% in this composition range allows the individual powders to be firmly bonded to each other even at a low extrusion ratio. Regardless, it shows almost constant strength and elongation. Even when the content of Si is 10 to 30%,
Although the same effect can be obtained, since the volume content of Si particles in the Al matrix is high, the toughness at room temperature is lowered. Fe and Ni are components that improve the heat resistance and strength of Al. Fe2 to 7% and Ni1
Alloys containing ~ 5% exhibit well-balanced properties in heat resistance, strength and toughness. If the content is more than the above lower limit, the heat resistance and strength are not sufficiently improved, while if it exceeds the upper limit, the heat resistance and strength are improved, but the toughness is reduced. . Mo and Zr are components that improve the heat resistance, creep resistance and strength of Al. When these contents are below the above lower limits, these properties are not sufficiently improved, whereas when they are above the upper limits (total amount is less than 2%), the toughness is also high. Is reduced.

【0008】CuおよびMgは、上記の元素に比して、
Alマトリックス中への固溶量が多いことと、準安定相
を析出させることにより、常温〜300℃、特に常温〜
200℃の温度域での本発明Al合金の強度を10〜2
0%程度改善する。CuおよびMgの含有量が0.3%
未満の場合には、添加の効果が少ない。一方、Cuの量
が6%を上回る場合には、合金強度のそれ以上の向上
は、認められない。これは、Al中のCuの最大固溶限
が5.65%であることから考えても、当然の結果であ
るといえる。また、Al合金中のMgの添加量が5%を
超える場合には、常温での靭性の低下をきたす。
Cu and Mg are, in comparison with the above elements,
Due to the large amount of solid solution in the Al matrix and the precipitation of the metastable phase, room temperature to 300 ° C, especially room temperature to
The strength of the Al alloy of the present invention in the temperature range of 200 ° C. is 10 to 2
Improve about 0%. Cu and Mg content is 0.3%
If it is less than the above, the effect of addition is small. On the other hand, when the amount of Cu exceeds 6%, the alloy strength is not further improved. It can be said that this is a natural result even considering that the maximum solid solubility limit of Cu in Al is 5.65%. Further, if the amount of addition of Mg in the Al alloy exceeds 5%, the toughness at room temperature will deteriorate.

【0009】なお、一般に、如何なる合金においても、
各合金成分は、相互に関連して合金の特性に影響するも
のである。従って、上記において、各合金成分含有量の
規定理由を個々に単純化して記載したが、この様な記載
は、必ずしも合金成分と本発明Al合金の特性との関係
を完全に説明し尽したものではないことは、いうまでも
ない。
[0009] Generally, in any alloy,
The alloy components are related to one another and affect the properties of the alloy. Therefore, in the above description, the reasons for defining the content of each alloy component have been individually simplified, but such description does not always completely explain the relationship between the alloy components and the characteristics of the Al alloy of the present invention. Not to mention that.

【0010】[0010]

【発明の効果】特定組成の本発明Al合金においては、
10以下という低い押出し比で、さらには2〜5という
極めて低い押出し比で、強固な結合を得ることが出来
る。また、本発明Al合金は、耐熱性および耐クリープ
性にも極めて優れており、しかもこれらの性質を損なう
ことなく、常温から300℃までの温度範囲での強度を
10〜20%程度改善した材料となる。さらに、本発明
Al合金は、靭性に優れているので、得られた押出し成
形体の熱間鍛造性などの後加工性が良好となり、機械部
品などの材料として実用性に極めて優れている。従っ
て、本発明によりAl合金は、コンプレッサー用部品、
タービンのインペラー、自動車のエンジン部品(例え
ば、バルブ系統、コンロッドなど)への適用が期待され
る。
In the Al alloy of the present invention having a specific composition,
With a low extrusion ratio of 10 or less, and an extremely low extrusion ratio of 2 to 5, a strong bond can be obtained. In addition, the Al alloy of the present invention is also extremely excellent in heat resistance and creep resistance, and moreover, the strength in the temperature range from room temperature to 300 ° C. is improved by about 10 to 20% without impairing these properties. Becomes Further, since the Al alloy of the present invention is excellent in toughness, the post-processability such as hot forgeability of the obtained extruded molded product is good, and it is extremely excellent in practicality as a material for machine parts and the like. Therefore, according to the present invention, an Al alloy is used for compressor parts,
It is expected to be applied to turbine impellers and automobile engine parts (for example, valve systems and connecting rods).

【0011】[0011]

【実施例】以下に実施例および比較例を示し、本発明の
特徴とするところをより一層明確にする。
EXAMPLES Examples and comparative examples will be shown below to further clarify the characteristics of the present invention.

【実施例1】第1表に示す組成のAl合金No.1〜1
4をエアアトマイズ法により粉末化し、−100メッシ
ュに分級した。なお、第1表において、各成分の量は、
“%”を示し、残余は実質的にAlである。また、Al
合金No.1〜6およびNo.12〜14が本発明品で
あり、No.7〜11が比較例品である。
Example 1 Al alloy No. 1 having the composition shown in Table 1 was used. 1-1
4 was pulverized by an air atomizing method and classified to -100 mesh. In Table 1, the amount of each component is
"%" Is shown and the balance is essentially Al. Also, Al
Alloy No. 1 to 6 and No. Nos. 12 to 14 are the products of the present invention, and No. 7 to 11 are comparative example products.

【0011】 [0011]

【0012】得られたAl合金粉末を直径30mm×高
さ80mmのビレットに冷間予備成形した後、450℃
において押出し比=3にて押出した。得られた押出し棒
から引張試験片およびクリープ試験片を作製し、常温で
の引張強度および伸び、300℃での引張強度ならびに
300℃でのクリープ試験(8kg/mmの応力をか
けた場合の破断までの時間を測定)を行なった。結果を
第2表に示す。
The obtained Al alloy powder was cold preformed into a billet having a diameter of 30 mm and a height of 80 mm, and then 450 ° C.
In, the extrusion ratio = 3 was extruded. Tensile test pieces and creep test pieces were produced from the obtained extruded rods, and the tensile strength and elongation at room temperature, the tensile strength at 300 ° C. and the creep test at 300 ° C. (when a stress of 8 kg / mm 2 was applied) The time to break was measured). The results are shown in Table 2.

【0013】 [0013]

【0014】第2表に示す結果から明らかな様に、本発
明のA1合金No.1〜6は、常温での高い強度および
2%以上の伸びを有し、且つ300℃においても高い引
張強度と優れた耐クリープ性を発揮する。また、本発明
のAl合金No.12〜14は、常温での強度が大きく
向上している。これに対し、本発明外の組成のAl合金
No.7〜11では、各種の特性のバランスが失われて
いる。即ち、合金No.8および9では、300℃での
クリープ破断時間が長いが、常温での伸びが低い。一
方、合金No.7,10および11では、常温での伸び
が高いものの、クリープ破断時間が極めて短くなってい
る。
As is clear from the results shown in Table 2, the A1 alloy No. 1 of the present invention was used. Nos. 1 to 6 have high strength at room temperature and elongation of 2% or more, and exhibit high tensile strength and excellent creep resistance even at 300 ° C. In addition, the Al alloy No. In Nos. 12 to 14, the strength at room temperature is greatly improved. On the other hand, the Al alloy No. having a composition outside the present invention. In Nos. 7 to 11, the balance of various characteristics is lost. That is, alloy No. In Nos. 8 and 9, the creep rupture time at 300 ° C. is long, but the elongation at room temperature is low. On the other hand, alloy No. In Nos. 7, 10 and 11, although the elongation at room temperature was high, the creep rupture time was extremely short.

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】(イ)Si5%以上且つ10%未満、
(ロ)Fe2〜7%、(ハ)Ni1〜5%、(ニ)Mo
0.5%以上且つ2%未満および(ホ)Zr0.3%以
上〜2%未満(但しMoとZrの合計量は2%未満であ
る)を含有し、残余が実質的にAlからなる靭性に優れ
た耐熱耐クリープ性アルミニウム合金。
(A) Si 5% or more and less than 10%,
(B) Fe 2 to 7%, (c) Ni 1 to 5%, (d) Mo
Toughness containing 0.5% or more and less than 2% and (e) Zr 0.3% or more to less than 2% (however, the total amount of Mo and Zr is less than 2%), and the balance substantially consisting of Al. Excellent heat and creep resistance aluminum alloy.
【請求項2】さらにCu0.3〜6%およびMg0.3
〜5%の少なくとも1種を含む請求項1に記載の耐熱耐
クリープ性アルミニウム合金。 【0001】
2. Further, Cu0.3-6% and Mg0.3
The heat-resistant and creep-resistant aluminum alloy according to claim 1, containing at least one of -5%. [0001]
JP2414154A 1990-04-18 1990-12-06 Heat and creep resistant aluminum alloy excellent in toughness Pending JPH05117797A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2414154A JPH05117797A (en) 1990-04-18 1990-12-06 Heat and creep resistant aluminum alloy excellent in toughness

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP2-103835 1990-04-18
JP10383590 1990-04-18
JP2414154A JPH05117797A (en) 1990-04-18 1990-12-06 Heat and creep resistant aluminum alloy excellent in toughness

Publications (1)

Publication Number Publication Date
JPH05117797A true JPH05117797A (en) 1993-05-14

Family

ID=26444424

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2414154A Pending JPH05117797A (en) 1990-04-18 1990-12-06 Heat and creep resistant aluminum alloy excellent in toughness

Country Status (1)

Country Link
JP (1) JPH05117797A (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63192838A (en) * 1987-02-04 1988-08-10 Showa Denko Kk Aluminum-alloy powder compact excellent in creep resisting characteristic
JPH0250902A (en) * 1988-05-12 1990-02-20 Sumitomo Electric Ind Ltd Method for forming aluminum alloy for product having large diameter

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63192838A (en) * 1987-02-04 1988-08-10 Showa Denko Kk Aluminum-alloy powder compact excellent in creep resisting characteristic
JPH0250902A (en) * 1988-05-12 1990-02-20 Sumitomo Electric Ind Ltd Method for forming aluminum alloy for product having large diameter

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