JPS58100654A - Aluminum alloy for casting with superior heat resistance - Google Patents

Aluminum alloy for casting with superior heat resistance

Info

Publication number
JPS58100654A
JPS58100654A JP20072181A JP20072181A JPS58100654A JP S58100654 A JPS58100654 A JP S58100654A JP 20072181 A JP20072181 A JP 20072181A JP 20072181 A JP20072181 A JP 20072181A JP S58100654 A JPS58100654 A JP S58100654A
Authority
JP
Japan
Prior art keywords
heat resistance
alloy
aluminum alloy
casting
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.)
Granted
Application number
JP20072181A
Other languages
Japanese (ja)
Other versions
JPS6047898B2 (en
Inventor
Shunkai Magusa
麻草 春海
Isao Satake
佐竹 勇夫
Kimiyoshi Fujimoto
藤本 公義
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 Aluminum Smelting Co
Original Assignee
Sumitomo Aluminum Smelting Co
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 Aluminum Smelting Co filed Critical Sumitomo Aluminum Smelting Co
Priority to JP20072181A priority Critical patent/JPS6047898B2/en
Publication of JPS58100654A publication Critical patent/JPS58100654A/en
Publication of JPS6047898B2 publication Critical patent/JPS6047898B2/en
Expired legal-status Critical Current

Links

Landscapes

  • Mold Materials And Core Materials (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Abstract

PURPOSE:To obtain an Al alloy with superior heat resistance and castability by adding specified amounts of Si, Cu, Mg and V and/or Mo to Al. CONSTITUTION:The composition of an Al alloy is composed of, by weight, 8-13% Si, 2-5% Cu, 0.2-0.8% Mg, 0.05-0.5% V and/or 0.05-2% Mo and the balance A with inevitable impurities. Thus, by further adding V and/or Mo to an Al-Si-Cu-Mg alloy, the heat resistance of the alloy is remarkably enhanced. In case of <0.05% each of V and Mo, the effect of enhancing the heat resistance is not sufficiently produced, and in case of >0.5% V and >2% Mo, uniform solubilization is made difficult.

Description

【発明の詳細な説明】 本発!j!は、耐熱性のすぐれた鋳物用アルミニウム合
金に関するものである。
[Detailed description of the invention] This invention! j! relates to an aluminum alloy for casting with excellent heat resistance.

近年、自動車工業におかて、省エネルギ一対策の一環と
して、車体の軽量化が求められてお9、各種部品のアル
ミニウム化がはかられつつある。しかしながら、特に自
重が問題となる可動部品のうち、高温でのすぐれた機械
的性質が要求されるものには、依然として鋳鉄などの材
料が使用されている。
In recent years, in the automobile industry, there has been a demand for lighter vehicle bodies as part of energy-saving measures9, and efforts are being made to use aluminum for various parts. However, materials such as cast iron are still used for moving parts that require excellent mechanical properties at high temperatures, especially where weight is an issue.

従来の耐熱アルミニウム合金として蝶、比較的使用実績
の多い:fXB HjJOJの1種(AO#A 。
A type of conventional heat-resistant aluminum alloy that has been used relatively frequently: fXB HjJOJ (AO#A).

ムORB、ム020)がある0これら扛いずれもAJ−
81−Ou−Mg系合金であって、ムOtムおよびムO
IBについてはさらにニッケル含金んでおり、主にピス
トン用に用いられているものである・が、鉄系材料の耐
熱部品全代替しうる陛どの耐熱性はもっていない。耐熱
強度の高いアルミニウム合金があれば、従来鉄でつくら
れている部品をそのような耐熱強度の高いアルミニウム
合金鋳物に替えることができ、その結果、軽量化が可能
になる。
MUORB, MU020) are both AJ-
81-Ou-Mg based alloys, including MuOtmu and MuO
IB also contains nickel and is mainly used for pistons, but it does not have the heat resistance to fully replace heat-resistant parts made of iron-based materials. If there is an aluminum alloy with high heat resistance strength, parts conventionally made of iron can be replaced with aluminum alloy castings with high heat resistance strength, and as a result, weight can be reduced.

以上のような現状をふまえて、本発明者ら社既知の耐熱
アルミニウム合金よりも高い高温強度を有し、しかも鋳
造性の良好な材料の開発研究に取組み、研究をかさねた
結果、鋳造性をそこなわず、高温強度の高い材料の開発
に成功しI−6 すなわち本発明は、重量でケイ素I〜/3Ls。
Based on the above-mentioned current situation, the present inventors have undertaken research and development of a material that has higher high-temperature strength than known heat-resistant aluminum alloys and has good castability, and as a result of repeated research, has found that Without this, we succeeded in developing a material with high high temperature strength.In other words, the present invention has silicon I~/3Ls by weight.

鋼コ、o−jt14、マグネシウム0.J〜o、rチを
含み、場らにバナジウムO,Oj〜00j−およびモリ
ブデンO,Oj〜コ、o%から選ばれる元素の一方また
は双方を含み、残部アルミニウムおよび不純物よりなる
耐熱性のすぐれた鋳物用アルミニウム合金である。
Steel, o-jt14, magnesium 0. Excellent heat resistance, containing J~o,r, occasionally containing one or both of elements selected from vanadium O, Oj~00j- and molybdenum O, Oj~, o%, with the balance being aluminum and impurities. It is an aluminum alloy for casting.

本発明にお−て、各含有成分を前述のように限定しt理
由は、次のとおりである。
In the present invention, each of the contained components is limited as described above, and the reason is as follows.

ケイ素は、アルミニウム合金の鋳造性を改善するのに必
須の成分であり、また耐熱性の向上にも効果がある。し
かしtチ未満では、良好な鋳造性を維持するのが困難で
あるとともに、高温強度も十分でなくなる。また/3e
sを越えると、合金の靭性を低下させるので、好ましく
ない0 銅は、合金に熱処理性を与え、材料の強度を^めるのに
効果がある0銅の含有量が−0Oチ未満だと十分な強度
が得られず、5%を越えると鋳造性が悪くなる傾向があ
る。
Silicon is an essential component for improving the castability of aluminum alloys, and is also effective in improving heat resistance. However, if it is less than t, it will be difficult to maintain good castability and the high temperature strength will not be sufficient. Also/3e
If it exceeds s, it is undesirable because it reduces the toughness of the alloy.0 Copper is effective in imparting heat treatability to the alloy and increasing the strength of the material.If the content of copper is less than -00 Sufficient strength cannot be obtained, and if it exceeds 5%, castability tends to deteriorate.

マグネシウムは、銅と同じように、熱処理による時効硬
化管著しく高める。マグネシウムの含有量がO,コチ未
満になると、Mg81の析出硬鵞 化が十分でなく、シたがって高い強度が得られない。ま
た0、1慢を越えると、靭性を低下させ合金がもろくな
る。
Magnesium, like copper, significantly enhances age-hardening tubes through heat treatment. If the magnesium content is less than 0,000 yen, the precipitation of Mg81 will not harden sufficiently, and therefore high strength will not be obtained. Moreover, if it exceeds 0.1, the toughness decreases and the alloy becomes brittle.

本発明においては、以上のようなAノー81−0u−M
g系合金に、さらにバナジウムおよび/またはモリブデ
ンを含有させることにより1合金の耐熱強度を著しく向
上させる。バナジウムは、o、osqlr未満ではその
効果が十分でなく、またO、S%t−越えると、均一な
溶解が困難になるとともに、たとえ添加してもその耐熱
強度に著しい変化はみられない。モリブデンの場合もO
,OS−未満では耐熱強度向上の効果が十分でなく、ま
たコ、0St−越えると均一な溶解が困難になるととも
に、たとえ添加できてもその効果に著しい質化はみられ
ない。
In the present invention, the above A No. 81-0u-M
By further containing vanadium and/or molybdenum in the g-based alloy, the heat resistance strength of the alloy is significantly improved. The effect of vanadium is not sufficient if it is less than O, osqlr, and if it exceeds O, S%t-, it becomes difficult to dissolve uniformly, and even if it is added, there is no significant change in its heat resistance strength. O also in the case of molybdenum
If it is less than ,OS-, the effect of improving heat resistance strength will not be sufficient, and if it exceeds 0,0St-, uniform dissolution will be difficult, and even if it can be added, the effect will not be significantly improved.

本発明合金の鋳造において、一般に行なわれている0、
3嗟以下のチタンおよび/または00OS−以下のホウ
素を添加して、合金の微細化t−hかることは、なんら
さしつかえない。
In the casting of the alloy of the present invention, 0,
There is nothing wrong with adding less than 3 moss of titanium and/or less than 000s of boron to refine the alloy th.

また、鋳造した鋳物は熱処理して用いるのが好tしく、
一般的なτ5処理またはTt処理が採用できる。
In addition, it is preferable to use the cast metal after heat treatment,
General τ5 processing or Tt processing can be adopted.

次に本発明を実施例によってさらに騨細に説明する。Next, the present invention will be explained in more detail with reference to examples.

実施例 第1!1社%本発明合金ならびに比較のための既知の耐
熱アルミニウム合金の化学成分を示したものである。な
お第1表の成分中、鉄(F@)d不純物として混入して
いるものであるO 第1表に示し念各々の合金管、JT8 HjコOコの付
図1に示される金mに鋳造し、得られた鋳塊は熱処理を
施し九後、:fN841号引張試験片および高温引張試
験片に加工し、室温での引張試験および硬さ測定ならび
に高温(JOOC)での引張試験および硬さ測定に供し
た〇熱処理はすべてT6処31會行ない、その条件は、
jOOCx♂時間の溶体化処理後、水焼入れを行ない、
直ちに一コ0Cx41時間の焼戻し処理を行なったもの
である。
Example 1! 1% This shows the chemical composition of the present invention alloy and a known heat-resistant aluminum alloy for comparison. In addition, among the components in Table 1, iron (F@) d is mixed as an impurity. After heat treatment, the obtained ingot was processed into No.fN841 tensile test piece and high temperature tensile test piece, which were subjected to tensile test and hardness measurement at room temperature and tensile test and hardness at high temperature (JOOC). All heat treatments used in the measurements were performed at T6 for 31 sessions, and the conditions were as follows:
After solution treatment for jOOCx♂ hours, water quenching is performed,
Immediately, each piece was tempered for 41 hours at 0C.

高温引張試験の条件は、所定のT1処理後コooCで2
00時間連続加熱し、一度室温まで自然冷却した試験片
を高温引張試験装置にセットし、5oOcで30分間保
持した状態で引張試験を行なったものである。te高温
硬さに9いては、高温引張試験後の試験片?チャック部
を面側し、ブリネル硬さ計で測定したものであり、測定
温度自体は室温である。
The conditions of the high temperature tensile test are 2 at 00C after the specified T1 treatment.
A test piece that was continuously heated for 00 hours and once naturally cooled to room temperature was set in a high-temperature tensile test device, and a tensile test was conducted while holding it at 50°C for 30 minutes. If the high temperature hardness is 9, is the test piece after high temperature tensile test? The chuck portion was placed face side and measured using a Brinell hardness meter, and the measurement temperature itself was room temperature.

第−表に、室温および高温での引張試験および硬さ測定
の結果を示す。
Table 1 shows the results of tensile tests and hardness measurements at room and elevated temperatures.

第   コ   表 第2表かられかるように、本発明合金は、公知合金に比
べて高温強度が著しく改善されている0ムOlム(&l
)に代表される従来の耐熱合金に比べ、高温での引張強
さ、O,コー耐力および硬さともに、約30−前後高く
なっている。
As can be seen from Table 2, the alloy of the present invention has significantly improved high temperature strength compared to known alloys.
Compared to conventional heat-resistant alloys represented by ), the tensile strength at high temperatures, O, Co yield strength, and hardness are approximately 30 times higher.

以上のように本発明合金は、従来にない高温強Wiをも
ち、しかも鋳造性のすぐれ友まったく新しい材料である
。したがって、自動車?はじめ、その他の産業機械のエ
ンジンまわりなど、耐熱性の要求される部品の材料とし
て幅広い用途が期待できる。
As described above, the alloy of the present invention has unprecedented high-temperature strength Wi and is a completely new material with excellent castability. Therefore, a car? It is expected to have a wide range of uses as a material for parts that require heat resistance, such as those around the engines of other industrial machinery.

Claims (1)

【特許請求の範囲】[Claims] 重量でケイ素l〜/3−1銅コ−Q−j%%  マグネ
シウムO,コ〜0.14 f含み、さらにバナジウムo
、oj〜o、s %およびモリブデンo、oj〜コ、O
−から選ばれる元素の一方または双方を含み、残部アル
ミニウムおよび不純物よりなる耐熱性のすぐれ九鋳物用
アルミニウム合金
Contains by weight silicon l~/3-1 copper co-Q-j%% magnesium O, co~0.14 f, and further vanadium o
, oj~o, s % and molybdenum o, oj~ko, O
An excellent heat-resistant aluminum alloy for casting containing one or both of the following elements, with the balance being aluminum and impurities.
JP20072181A 1981-12-11 1981-12-11 Aluminum alloy for casting with excellent heat resistance Expired JPS6047898B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP20072181A JPS6047898B2 (en) 1981-12-11 1981-12-11 Aluminum alloy for casting with excellent heat resistance

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP20072181A JPS6047898B2 (en) 1981-12-11 1981-12-11 Aluminum alloy for casting with excellent heat resistance

Publications (2)

Publication Number Publication Date
JPS58100654A true JPS58100654A (en) 1983-06-15
JPS6047898B2 JPS6047898B2 (en) 1985-10-24

Family

ID=16429092

Family Applications (1)

Application Number Title Priority Date Filing Date
JP20072181A Expired JPS6047898B2 (en) 1981-12-11 1981-12-11 Aluminum alloy for casting with excellent heat resistance

Country Status (1)

Country Link
JP (1) JPS6047898B2 (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60215732A (en) * 1984-04-11 1985-10-29 Furukawa Alum Co Ltd Al alloy for structure suitable for nuclear fusion device
JPS62185857A (en) * 1986-02-12 1987-08-14 Honda Motor Co Ltd Heat resistant and high strength aluminum alloy
JP2006016693A (en) * 2004-06-29 2006-01-19 Aluminium Rheinfelden Gmbh Aluminum alloy for die casting
WO2010012875A1 (en) * 2008-07-30 2010-02-04 Alcan International Limited Casting made from aluminium alloy, having high hot creep and fatigue resistance
EP2758557B1 (en) 2011-09-19 2015-11-04 Alcoa GmbH Improved aluminum casting alloys containing vanadium
US20160281195A1 (en) * 2011-10-28 2016-09-29 Alcoa Inc. HIGH PERFORMANCE AlSiMgCu CASTING ALLOY

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60215732A (en) * 1984-04-11 1985-10-29 Furukawa Alum Co Ltd Al alloy for structure suitable for nuclear fusion device
JPS62185857A (en) * 1986-02-12 1987-08-14 Honda Motor Co Ltd Heat resistant and high strength aluminum alloy
JP2006016693A (en) * 2004-06-29 2006-01-19 Aluminium Rheinfelden Gmbh Aluminum alloy for die casting
KR101295458B1 (en) * 2004-06-29 2013-08-09 알루미늄 라인펠덴 게엠베하 Aluminium alloy and use of an aluminium alloy
WO2010012875A1 (en) * 2008-07-30 2010-02-04 Alcan International Limited Casting made from aluminium alloy, having high hot creep and fatigue resistance
JP2011529529A (en) * 2008-07-30 2011-12-08 リオ ティント アルカン インターナショナル リミテッド Aluminum alloy castings with high resistance to fatigue and hot creep
US9982328B2 (en) 2008-07-30 2018-05-29 Rio Tinto Alcan International Limited Casting made from aluminium alloy, having high hot creep and fatigue resistance
EP2758557B1 (en) 2011-09-19 2015-11-04 Alcoa GmbH Improved aluminum casting alloys containing vanadium
US20160281195A1 (en) * 2011-10-28 2016-09-29 Alcoa Inc. HIGH PERFORMANCE AlSiMgCu CASTING ALLOY

Also Published As

Publication number Publication date
JPS6047898B2 (en) 1985-10-24

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