JPH0565573B2 - - Google Patents
Info
- Publication number
- JPH0565573B2 JPH0565573B2 JP62314193A JP31419387A JPH0565573B2 JP H0565573 B2 JPH0565573 B2 JP H0565573B2 JP 62314193 A JP62314193 A JP 62314193A JP 31419387 A JP31419387 A JP 31419387A JP H0565573 B2 JPH0565573 B2 JP H0565573B2
- Authority
- JP
- Japan
- Prior art keywords
- alloy
- aluminum
- silicon
- casting
- magnesium
- 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
Links
Landscapes
- Mold Materials And Core Materials (AREA)
Description
(産業上の利用分野)
本発明は自動車、船舶、車両等のエンジン廻り
部品等の厳密に耐圧漏れ性を要求されるような機
械部品に使用するのに適した耐圧性の優れた鋳造
用アルミニウム−ケイ素−マグネシウム系合金、
またはアルミニウム−ケイ素−マグネシウム−銅
系合金に関するものである。
(従来の技術)
一般にJIS規格AC4A、AC4Cにて代表されるア
ルミニウム−ケイ素−マグネシウム系合金、
AC4D、AC8A、AC8B、AC8C等にて代表され
るアルミニウム−ケイ素−マグネシウム−銅系合
金は、鋳造性がよく、熱処理を施すことによつて
優れた機械的性質および耐圧性が得られるところ
から、自動車、船舶、車両等におけるピストン等
のエンジン廻り部品、油圧部品、保安部品その他
の機械部品鋳物用のアルミニウム合金として幅広
く用いられている。
(発明が解決しようとする問題点)
しかしながら、この種のアルミニウム合金にお
いては、合金中の鉄含有量が増加すると急激に鋳
物の耐圧性が低下し、鋳造された鋳物部品に往々
にして圧漏れ等の欠陥を生ずる危険性があつて問
題であつた。
発明者らの調査によると、この現象は合金中の
鉄含有量が0.2%以下であるときは殆ど見られな
いが、これを超えると次第に散見されるようにな
り、0.4%を超えるとその傾向が顕著になること
が判つた。
ところで、一般に鋳物工場においては、資源お
よび経費節約の見地から新塊と称する一次合金地
金にスクラツプ材を多量に添加配合した合金地金
や、スクラツプ材を主体として配合された二次合
金地金が大量に使用されているが、スクラツプ材
中には多量の鉄が不純物として混入しているのが
常であり、このため鋳物工場においてはこの系の
合金を前記の目的、殊に厳格に耐圧性を要求され
る自動車、船舶等のピストン等のエンジン廻り部
品に用いる場合には、不純物としての鉄含有量を
0.4%以下の可及的少ない量に調整する必要があ
り、このための合金配合操作は極めて煩わしく、
またコストアツプの原因になるので好ましくなか
つた。
また、複雑な形状を有する鋳物部品では、合金
中の鉄含有量の増加によつて、肉厚部の凝固の遅
い部分に耐圧性不良箇所を生じやすいので、これ
を防止するために厳密な指向性凝固を行なわねば
ならず、鋳型の設計や鋳造方案に殊更の工夫を要
する面倒があつた。
本発明者らは鋳物用アルミニウム−ケイ素−マ
グネシウム系またはアルミニウム−ケイ素−マグ
ネシウム−銅系合金における上記の問題点につい
て、鉄含有量増大に伴う鋳物の耐圧性低下原因を
究明した結果、これらの系の合金においては合金
中の鉄含有量が増大すると、合金溶湯から鋳物を
鋳込むに際して合金成分中の鉄がアルミニウム、
ケイ素と反応して針状のアルミニウム−ケイ素−
鉄系化合物を晶出し、この針状化合物が鋳物の肉
厚中心部等の溶湯最終凝固部付近において急激に
増加するとともに架橋状に発達粗大化し、この部
分の爾後の溶湯の充足を阻害して亀裂状の引き巣
や微細な連続した線状の引け巣の集合体を発生し
やすくして、これが鋳物の耐圧性を悪化させる原
因となることが判つた。
第1図a,b,c,dは、その代表例としてア
ルミニウム−ケイ素−マグネシウム−銅系合金鋳
物における合金中の鉄含有量と内部引け巣発生と
の関係を実験的に例示したものである。
実験に際しては、合金中の鉄含有量をそれぞれ
変化させたケイ素6.5%、マグネシウム0.3%、銅
3.0%を含むアルミニウム合金溶湯をテーターモ
ールドに鋳込み、鋳塊断面をカラーチエツクによ
り引け巣欠陥の有無を調べた。
第1図より判かるように、合金中の鉄含有量が
0.05%の合金aにあつては、鋳塊の最終凝固部で
ある凝固収縮底部が丸味を帯びた状態で凝固が終
了しており、引け巣欠陥が殆ど見られないもの
が、鉄含有量0.22%の合金bになると、凝固収縮
底部に細く小さな亀裂状の引け巣と多数の微細な
線状の引け巣が現われ、鉄含有量0.36%の合金
c、0.65%の合金dと鉄含有量がさらに増大する
につれて、凝固収縮底部におけるこれらの引き巣
欠陥の数や大きさが拡大し、部分的にこれらが互
いに連通するようになる。
発明者らの実験によれば、この関係は上記組成
の合金にとどまらず、あらゆる組成の実用鋳物用
アルミニウム−ケイ素−マグネシウム系合金およ
びアルミニウム−ケイ素−マグネシウム−銅系合
金に共通の傾向であつて、従つて、実際にこれら
の合金により作られた鋳物においては、鋳造後の
表面加工によつて、これらの鋳物内部において発
達した連通引き巣欠陥は容易にその表面に露出
し、液体や気体がこれらの欠陥を経由して外部に
流通してしまうので、このような合金で作られた
鋳物を耐圧部品等に用いた場合、その耐圧性が損
なわれるのである。
本発明者らは上述したような事実に鑑み、これ
らの問題点を克服すべく鋭意研究を重ねた結果、
鉄を多量に含むアルミニウム−ケイ素−マグネシ
ウム系またはアルミニウム−ケイ素−マグネシウ
ム−銅系合金において、合金中に適量のカルシウ
ムを添加含有させるときは、合金鋳造に際して鋳
物中に見られる互いに連通する亀裂状の引け巣お
よび微細な線状の引け巣の発生を大巾に減少させ
ることができ、従つて鋳物の耐圧性を一段と向上
させることができることを見出した。
(問題点を解決するための手段)
即ち、本発明は重量でケイ素4〜11%、マグネ
シウム0.1〜2%、カルシウム0.001〜0.01%を含
有し、さらに必要に応じて銅5%以下、マンガン
1%以下、ニツケル3%以下を含有し、残部アル
ミニウムおよび不純物とからなり、不純物中の鉄
の含有量が0.4%を超え0.8%未満である耐圧性の
優れた鋳物用アルミニウム合金である。
(作用)
本発明によるときは、合金中の鉄含有量が0.8
%程度迄であれば、カルシウム0.001〜0.01%を
添加含有させることによつて、従来の実用アルミ
ニウム−ケイ素−マグネシウム系合金鋳物または
アルミニウム−ケイ素−マグネシウム−銅系合金
鋳物において、この種の合金鋳物特有の他の優れ
た特性を妨げること無く、合金中の鉄含有に基ず
く特殊な形状の内部引け巣の発生に起因する耐圧
性低下を防止することができ、強度、靭性等は寧
ろ向上するので、鋳物工場等において鉄分の多い
スクラツプ地金や二次合金地金を使用しても、何
等配合地金中の鉄含有量の調整に気を使うことな
しに自動車、船舶等のエンジン廻り部品等、厳密
な耐圧性を要求される鋳物製品の鋳造を行なうこ
とができるので極めて効果的である。
次に本発明の合金における各添加元素の作用お
よび限定理由について説明する。
ケイ素4〜11%の添加は合金基質を強化し、湯
流れ性、引け性、鋳造割れ防止等を改善する効果
を有し、4.0%以下ではその効果少なく、11%以
上では鋳物の靭性や耐熱衝撃性を著しく低下させ
る。
マグネシウム0.1〜2%の添加は鋳物に熱処理
を施すことによつて合金組織中にMg2Siを析出し
て合金基質を強化する効果を有し、0.1%以下で
はその効果少なく、2%以上では伸びが小さく、
また鋳造性も低下する。
銅の5%以下の添加は熱処理を施した場合に、
時効効果によつて合金鋳物に著しい強度を付与す
るものであるが、5%以上の添加は伸びを低下し
靭性を損なう。
マンガンの1%以下およびニツケルの3%以下
の添加は鋳物に耐熱性を付与するものであるが、
マンガン添加量が1%を超すと、添加したマンガ
ンが合金成分中のアルミニウム、ケイ素や不純物
として含まれる鉄と反応してアルミニウム−マン
ガン−ケイ素−鉄系の粗大な針状化合物を晶出し
て鋳物の靭性を低下させ、またニツケルの添加量
が3%を超すとアルミニウム−ニツケル系の粗大
化合物を生じて同様に靭性低下を来す。
本発明においては上記した組成範囲でケイ素、
マグネシウムを含み、さらに必要に応じて銅、マ
ンガン、ニツケルを含むアルミニウム−ケイ素−
マグネシウム系、またはアルミニウム−ケイ素−
マグネシウム−銅系合金において、カルシウムの
0.001〜0.01%を添加するものであるが、カルシ
ウムの上記範囲での含有は、先に述べた如くこの
二つの系の合金に於ける合金中の鉄含有に基ずく
合金鋳物製品の引け巣欠陥の増加に依る耐圧性低
下を防止する作用を有するものであつて、含有量
が0.001%以下ではその効果が少なく、またそれ
が0.01%を超えると、合金溶湯の流動性が低下し
て鋳物に湯境等を生じなくなり、健全な製品を描
たくなる。
而して、このようにカルシウム添加に依る耐圧
性改善効果が得られる合金中の鉄含有量の範囲は
0.4%を超え0.8%未満の範囲に限られるものであ
る。
何となれば鉄0.4%以下では合金鋳物の耐圧性
はもともと問題は無く、また鉄含有量が0.8%を
超えるとカルシウム添加によつても耐圧性改善効
果が十分に得られないからである。
本発明の合金の溶製はこの種の合金系において
通常行なわれる一般的な方法が採られ、カルシウ
ムの添加は金属カルシウムまたはアルミニウム−
カルシウム母合金またはカルシウム含有フラツク
ス等が用いられる。
また、本発明合金を鋳造して各種鋳物製品を得
るに際し、この種の合金系において婁々行なわれ
るナトリウムまたはストロンチウム等に依る鋳造
組織の改良処理、チタニウム、ボロン等に依る鋳
造組織の微細化処理等によつて合金中に添加され
るこれら金属の含有は、これらの処理が常法の添
加範囲にて行なわれている限り、本発明の効果を
妨げることが無いので何等支障は無い。
本発明の合金は砂型鋳造や金型鋳造に適用可能
なことは勿論であるが、近年大型化しつゝあるダ
イカスト、低圧鋳造に適用した場合にも鋳造製品
の耐圧性を向上することができる。
次に本発明の実施例を示す。
(実施例)
第1表に示す如き各種組成の合金を溶製し、鋳
込温度720℃、鋳型温度200℃にてJIS舟底金型お
よびテーターモールドに鋳込み、それらから強度
および伸び試験片、引き巣観察試験片を作成し
た。なお、合金組成中のカルシウムはアルミニウ
ム−5%カルシウム母合金を用いて添加した。強
度および伸びの測定は試験片を500℃に6時間保
持後、水焼き入れし、180℃で6時間焼き戻すT6
処理を施した後に行なつた。
引け巣の観察については、テーターモールドに
鋳込まれた合金鋳物の上下方向に2分割し、分割
面を面削して平滑化した後カラーチエツクして、
引き巣の存在状態を調べた。これらの結果を第1
表に示す。なお、引け巣の観察結果は第1図に示
す実験結果を参考にし、aの如く有害な引き巣の
観察されなかつたものをAランクとしb,c,d
と引け巣の存在が顕著になるに従つて、それぞれ
B、C、Dとランク付けした。
(Industrial Application Field) The present invention is an aluminum casting with excellent pressure resistance suitable for use in mechanical parts such as engine parts of automobiles, ships, vehicles, etc., which require strict pressure leak resistance. - silicon-magnesium alloy,
Or it relates to an aluminum-silicon-magnesium-copper alloy. (Prior art) Aluminum-silicon-magnesium alloys generally represented by JIS standards AC4A and AC4C,
Aluminum-silicon-magnesium-copper alloys, represented by AC4D, AC8A, AC8B, AC8C, etc., have good castability and can be heat-treated to provide excellent mechanical properties and pressure resistance. It is widely used as an aluminum alloy for casting engine parts such as pistons, hydraulic parts, safety parts, and other mechanical parts in automobiles, ships, vehicles, etc. (Problem to be solved by the invention) However, in this type of aluminum alloy, when the iron content in the alloy increases, the pressure resistance of the casting rapidly decreases, and pressure leakage often occurs in cast parts. This was a problem because there was a risk of causing defects such as. According to the inventors' research, this phenomenon is almost never observed when the iron content in the alloy is 0.2% or less, but when it exceeds this, it gradually becomes seen here and there, and when it exceeds 0.4%, it tends to become more common. was found to be significant. By the way, generally in foundries, from the viewpoint of saving resources and costs, alloy ingots are made by adding a large amount of scrap material to the primary alloy ingot called new ingot, and secondary alloy ingots are mixed mainly by scrap material. is used in large quantities, but a large amount of iron is usually mixed in as an impurity in the scrap material, so foundries use this type of alloy for the above purpose, especially for strict pressure resistance. When used in engine parts such as pistons for automobiles and ships that require high performance, the iron content as an impurity must be reduced.
It is necessary to adjust the amount to the lowest possible amount of 0.4% or less, and the alloy blending operation for this purpose is extremely troublesome.
Moreover, this is not preferable because it causes an increase in costs. In addition, in cast parts with complex shapes, the increase in iron content in the alloy tends to cause poor pressure resistance in thick-walled parts that solidify slowly. However, it was necessary to conduct solidification, which was troublesome and required special ingenuity in the design of the mold and the casting method. The present inventors investigated the cause of the decrease in pressure resistance of castings due to increased iron content regarding the above-mentioned problems in aluminum-silicon-magnesium alloys or aluminum-silicon-magnesium-copper alloys for castings, and found that these systems When the iron content in the alloy increases, when casting from the molten alloy, the iron in the alloy component becomes aluminum,
Reacts with silicon to form acicular aluminum-silicon
Iron-based compounds are crystallized, and these acicular compounds rapidly increase near the final solidification part of the molten metal, such as the thick center of the casting, and develop into a cross-linked shape and become coarse, inhibiting the subsequent sufficiency of the molten metal in this area. It was found that crack-like shrinkage cavities and aggregates of fine continuous linear shrinkage cavities are likely to occur, which causes deterioration of the pressure resistance of the casting. Figure 1 a, b, c, and d are representative examples of experimentally illustrating the relationship between the iron content in the alloy and the occurrence of internal shrinkage cavities in aluminum-silicon-magnesium-copper alloy castings. . During the experiment, silicon 6.5%, magnesium 0.3%, and copper were used, each with varying iron content in the alloy.
A molten aluminum alloy containing 3.0% was cast into a Tater mold, and the cross section of the ingot was color checked to check for shrinkage cavity defects. As can be seen from Figure 1, the iron content in the alloy is
In the case of 0.05% alloy a, solidification is completed with the bottom of the solidification shrinkage, which is the final solidified part of the ingot, being rounded and almost no shrinkage cavity defects are observed. % of alloy B, thin, small crack-like shrinkage cavities and many fine linear shrinkage cavities appear at the bottom of solidification shrinkage, and alloy C with iron content of 0.36%, alloy d with iron content of 0.65%, and alloy B with iron content of 0.65%. As the size increases further, the number and size of these nest defects at the bottom of the solidification shrinkage expand, and they become partially in communication with each other. According to the inventors' experiments, this relationship is common not only to alloys with the above compositions but also to aluminum-silicon-magnesium alloys and aluminum-silicon-magnesium-copper alloys for practical casting of all compositions. Therefore, in actual castings made from these alloys, the interconnected cavities developed inside these castings are easily exposed to the surface due to surface processing after casting, and liquids and gases are easily exposed to the surface. Since it is distributed to the outside via these defects, when castings made of such alloys are used for pressure-resistant parts, the pressure resistance is impaired. In view of the above-mentioned facts, the present inventors have conducted extensive research to overcome these problems, and as a result,
When adding an appropriate amount of calcium to an aluminum-silicon-magnesium or aluminum-silicon-magnesium-copper alloy that contains a large amount of iron, it is important to avoid the formation of interconnected cracks found in the casting during alloy casting. It has been found that the occurrence of shrinkage cavities and fine linear shrinkage cavities can be greatly reduced, and therefore the pressure resistance of castings can be further improved. (Means for Solving the Problems) That is, the present invention contains 4 to 11% silicon, 0.1 to 2% magnesium, and 0.001 to 0.01% calcium, and further contains up to 5% copper and 1 manganese as required. % or less, 3% or less of nickel, and the balance consists of aluminum and impurities, and the iron content of the impurities is more than 0.4% and less than 0.8%.It is an aluminum alloy for casting with excellent pressure resistance. (Function) According to the present invention, the iron content in the alloy is 0.8
%, by adding 0.001 to 0.01% calcium, this kind of alloy casting can be improved in conventional practical aluminum-silicon-magnesium alloy castings or aluminum-silicon-magnesium-copper alloy castings. Without interfering with other unique and excellent properties, it is possible to prevent a decrease in pressure resistance caused by the occurrence of internal shrinkage cavities of a special shape based on the iron content in the alloy, and the strength, toughness, etc. are improved. Therefore, even if scrap metal or secondary alloy metal with a high iron content is used in a foundry, etc., it can be used to produce engine parts for automobiles, ships, etc. without having to take any care to adjust the iron content in the mixed metal. It is extremely effective because it allows casting of cast products that require strict pressure resistance. Next, the effects and reasons for limitations of each additive element in the alloy of the present invention will be explained. Addition of 4 to 11% silicon has the effect of strengthening the alloy matrix and improving flowability, shrinkage, prevention of casting cracks, etc. Below 4.0%, the effect is small, and above 11%, it improves the toughness and heat resistance of the casting. Significantly reduces impact resistance. Addition of 0.1 to 2% magnesium has the effect of precipitating Mg 2 Si in the alloy structure by heat-treating the casting and strengthening the alloy matrix; below 0.1%, the effect is small, and above 2%, the effect is weak. elongation is small,
Castability also deteriorates. Addition of less than 5% copper will result in heat treatment.
Although it imparts significant strength to alloy castings through the aging effect, addition of 5% or more reduces elongation and impairs toughness. Addition of 1% or less of manganese and 3% or less of nickel imparts heat resistance to the casting, but
If the amount of manganese added exceeds 1%, the added manganese reacts with aluminum and silicon in the alloy components and iron contained as an impurity, crystallizing coarse needle-shaped compounds of aluminum-manganese-silicon-iron system, resulting in castings. Moreover, if the amount of nickel added exceeds 3%, coarse aluminum-nickel compounds are formed, which also causes a decrease in toughness. In the present invention, silicon,
Aluminum-silicon containing magnesium and, if necessary, copper, manganese, and nickel
Magnesium-based or aluminum-silicon
In magnesium-copper alloys, calcium
0.001 to 0.01% of calcium is added, but as mentioned above, calcium content in the above range may cause shrinkage cavities in alloy casting products due to the iron content in these two types of alloys. It has the effect of preventing a decrease in pressure resistance due to an increase in molten alloy, and if the content is less than 0.001%, the effect will be small, and if it exceeds 0.01%, the fluidity of the molten alloy will decrease and it will not be able to form a casting. You will want to create healthy products that will not cause hot spots etc. Therefore, the range of iron content in the alloy where the pressure resistance improvement effect can be obtained by adding calcium is as follows.
It is limited to a range of more than 0.4% and less than 0.8%. This is because if the iron content is less than 0.4%, there is no problem with the pressure resistance of the alloy casting, and if the iron content exceeds 0.8%, even the addition of calcium will not have a sufficient effect of improving the pressure resistance. The alloy of the present invention is produced by the general method normally used for this type of alloy system, and calcium is added by metallic calcium or aluminum.
A calcium mother alloy or a calcium-containing flux is used. In addition, when producing various cast products by casting the alloy of the present invention, treatment for improving the casting structure using sodium or strontium, etc., and refinement treatment for the casting structure using titanium, boron, etc., are carried out extensively in this type of alloy system. The inclusion of these metals added to the alloy by the above methods does not impede the effects of the present invention, so long as these treatments are carried out within the range of conventional methods. The alloy of the present invention can of course be applied to sand mold casting and die casting, but it can also improve the pressure resistance of cast products when applied to die casting and low pressure casting, which are becoming larger in size in recent years. Next, examples of the present invention will be shown. (Example) Alloys with various compositions as shown in Table 1 were melted and cast into JIS boat bottom molds and tater molds at a casting temperature of 720°C and a mold temperature of 200°C. A test piece for observation of nesting was created. Note that calcium in the alloy composition was added using an aluminum-5% calcium mother alloy. To measure strength and elongation, test specimens are held at 500°C for 6 hours, water quenched, and then tempered at 180°C for 6 hours.
This was done after the treatment. To observe shrinkage cavities, the alloy casting cast in the Tater mold is divided into two in the vertical direction, the divided surfaces are faceted and smoothed, and then a color check is performed.
We investigated the presence of nests. These results are the first
Shown in the table. For the observation results of shrinkage cavities, refer to the experimental results shown in Figure 1, and those with no harmful shrinkage cavities observed in a are ranked A and b, c, and d.
They were ranked as B, C, and D according to the degree of conspicuousness of the shrinkage cavity.
【表】
*:ppm表示
第1表の結果からカルシウム添加のない従来の
アルミニウム−ケイ素−マグネシウム系合金(試
料番号1〜4)およびアルミニウム−ケイ素−マ
グネシウム−銅係合金(試料番号9〜11)におい
ては、合金中の鉄含有量が低い間は引け巣ランク
はAと全く問題が無い(試料番号1)が、鉄含有
量が0.2%を超えると(試料番号2〜4および9
〜11)有害な引け巣が観測され、含有量が多くな
るに従つてB、C、Dとこれら有害な引け巣量が
多くなり、これらの合金によつて作られた鋳物の
耐圧性に問題を生ずる恐れがあるのに対し、これ
らの合金系に本発明の範囲でカルシウムを添加し
た本発明第1乃至第4の合金(試料番号5〜8お
よび12〜15)においては合金中の鉄含有量が0.2
%を超えて相当量高くなつても、いずれもランク
Aで有害な引け巣が存在せず、本発明合金は耐圧
性が優れていることが判かる。
また、強度、伸びの測定結果から本発明のアル
ミニウム−ケイ素−マグネシウム系合金およびア
ルミニウム−ケイ素−マグネシウム−銅系合金は
同一組成のケイ素、マグネシウム、銅を含む従来
合金に較べて概ね強度、伸びともに改善されてお
り、機械的性質、殊に靭性においても優れている
ことが判かる。
(効果)
以上述べたように、従来のアルミニウム−ケイ
素−マグネシウム系合金、またはアルミニウム−
ケイ素−マグネシウム−銅系合金に適量のカルシ
ウムを添加含有せしめた本発明の鋳物用アルミニ
ウム合金は、合金中の鉄含有量の増加にもかゝわ
らず、これを鋳造して得られた鋳物製品に鉄化合
物の生成に起因する特殊な形状の内部引け巣に依
る欠陥を生ずることが無いので、耐圧性に優れ、
また強度、靭性も改善されるので自動車、船舶の
ピストン等のエンジン廻り部品、油圧容器、その
他の耐圧性を必要とする機械部品鋳物の鋳造に最
適である。
また、鋳物工場等においてスクラツプ材、二次
合金地金の配合使用に際しても、配合地金中の鉄
不純物の調整に煩わされること無く、合金の溶製
ができるので極めて効率的かつ経済的である。[Table] *: ppm display From the results in Table 1, conventional aluminum-silicon-magnesium alloys without calcium addition (sample numbers 1 to 4) and aluminum-silicon-magnesium-copper alloys (sample numbers 9 to 11) As long as the iron content in the alloy is low, the shrinkage cavity rank is A and there is no problem (sample number 1), but when the iron content exceeds 0.2% (sample numbers 2 to 4 and 9).
~11) Harmful shrinkage cavities have been observed, and as the content increases, the amount of these harmful shrinkage cavities increases in B, C, and D, causing problems with the pressure resistance of castings made with these alloys. However, in the first to fourth alloys of the present invention (sample numbers 5 to 8 and 12 to 15) in which calcium is added to these alloy systems within the scope of the present invention, the iron content in the alloys is amount is 0.2
%, no harmful shrinkage cavities are present at rank A, indicating that the alloys of the present invention have excellent pressure resistance. In addition, the strength and elongation measurement results show that the aluminum-silicon-magnesium alloy and the aluminum-silicon-magnesium-copper alloy of the present invention have generally higher strength and elongation than conventional alloys containing silicon, magnesium, and copper with the same composition. It can be seen that the mechanical properties, especially the toughness, are improved. (Effects) As mentioned above, conventional aluminum-silicon-magnesium alloys or aluminum-
The aluminum alloy for casting of the present invention, which is a silicon-magnesium-copper alloy containing an appropriate amount of calcium, has a high iron content in the alloy. Since there are no defects caused by internal shrinkage cavities of a special shape caused by the formation of iron compounds, it has excellent pressure resistance.
It also has improved strength and toughness, making it ideal for casting engine parts such as pistons for automobiles and ships, hydraulic containers, and other machine parts that require pressure resistance. In addition, when mixing scrap materials and secondary alloy ingots in foundries, etc., it is extremely efficient and economical because the alloy can be melted without having to worry about adjusting iron impurities in the mixed ingots. .
第1図a,b,cおよびdは従来のアルミニウ
ム−ケイ素−マグネシウム−銅系合金における合
金中の鉄含有量と引け巣発生状態の関係を示すた
めのカラーチエツによる引け巣観察試料である。
本試料は同時に引け巣発生手段程度を示すランク
付け試料の兼ねており、A、B、C、Dの順で引
け巣量が増大することを示す。
Figures 1a, b, c, and d are specimens for observation of shrinkage cavities using a color check to show the relationship between the iron content in the alloy and the state of occurrence of shrinkage cavities in conventional aluminum-silicon-magnesium-copper alloys.
This sample also serves as a ranking sample that indicates the degree of shrinkage cavity generation means, and indicates that the amount of shrinkage cavities increases in the order of A, B, C, and D.
Claims (1)
〜2%、カルシウム0.001〜0.01%を含有し、残
部アルミニウムおよび不純物からなり、不純物中
の鉄の含有量が0.4%を超え0.8%未満である耐圧
性の優れた鋳物用アルミニウム合金。 2 重量で、ケイ素4〜11%、マグネシウム0.1
〜2%、銅5%以下、カルシウム0.001〜0.01%
を含有し、残部アルミニウムおよび不純物からな
り、不純物中の鉄の含有量が0.4%を超え0.8%未
満である耐圧性の優れた鋳物用アルミニウム合
金。 3 重量で、ケイ素4〜11%、マグネシウム0.1
〜2%、カルシウム0.001〜0.01%を含有し、さ
らに、マンガン1%以下およびニツケル3%以下
のうちの1種以上を含有し、残部アルミニウムお
よび不純物からなり、不純物中の鉄の含有量が
0.4%を超え0.8%未満である耐圧性の優れた鋳物
用アルミニウム合金。 4 重量で、ケイ素4〜11%、マグネシウム0.1
〜2%、銅5%以下、カルシウム0.001〜0.01%
を含有し、さらに、マンガン1%以下およびニツ
ケル3%以下のうちの1種以上を含有し、残部ア
ルミニウムおよび不純物からなり、不純物中の鉄
の含有量が0.4%を超え0.8%未満である耐圧性の
優れた鋳物用アルミニウム合金。[Claims] 1. Silicon 4-11%, magnesium 0.1% by weight
-2%, calcium 0.001-0.01%, the balance consists of aluminum and impurities, and the content of iron in the impurities is more than 0.4% and less than 0.8%, and has excellent pressure resistance for casting. 2 By weight, silicon 4-11%, magnesium 0.1
~2%, copper less than 5%, calcium 0.001~0.01%
An aluminum alloy for casting with excellent pressure resistance, the balance being aluminum and impurities, with an iron content of more than 0.4% and less than 0.8%. 3 By weight, silicon 4-11%, magnesium 0.1
~2%, calcium 0.001~0.01%, and one or more of 1% or less manganese and 3% or less nickel, with the balance consisting of aluminum and impurities, and the iron content in the impurities is
An aluminum alloy for castings with excellent pressure resistance of more than 0.4% and less than 0.8%. 4 By weight, silicon 4-11%, magnesium 0.1
~2%, copper less than 5%, calcium 0.001~0.01%
and further contains one or more of manganese or less and nickel or less and 3% or less, with the balance consisting of aluminum and impurities, and the iron content of the impurities is more than 0.4% and less than 0.8%. Aluminum alloy for casting with excellent properties.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP31419387A JPH01156446A (en) | 1987-12-14 | 1987-12-14 | Aluminum alloy for casting with excellent pressure resistance |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP31419387A JPH01156446A (en) | 1987-12-14 | 1987-12-14 | Aluminum alloy for casting with excellent pressure resistance |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH01156446A JPH01156446A (en) | 1989-06-20 |
| JPH0565573B2 true JPH0565573B2 (en) | 1993-09-20 |
Family
ID=18050386
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP31419387A Granted JPH01156446A (en) | 1987-12-14 | 1987-12-14 | Aluminum alloy for casting with excellent pressure resistance |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH01156446A (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6412164B1 (en) * | 2000-10-10 | 2002-07-02 | Alcoa Inc. | Aluminum alloys having improved cast surface quality |
| JP4590784B2 (en) | 2001-06-18 | 2010-12-01 | アイシン精機株式会社 | Sliding member and valve opening / closing timing control device |
| JP4623372B2 (en) * | 2005-07-27 | 2011-02-02 | アイシン・エィ・ダブリュ株式会社 | Aluminum alloy for casting, method for producing the same, and method for producing aluminum alloy cast product |
| KR101273579B1 (en) * | 2010-10-19 | 2013-06-11 | 한국생산기술연구원 | Aluminum alloy extruded products and manufacturing method thereof |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5538965A (en) * | 1978-09-14 | 1980-03-18 | Sukai Alum Kk | Solder alloy for vacuum brazing aluminum |
| JPS6126744A (en) * | 1984-07-16 | 1986-02-06 | Honda Motor Co Ltd | Wear-resistant aluminum alloy |
-
1987
- 1987-12-14 JP JP31419387A patent/JPH01156446A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPH01156446A (en) | 1989-06-20 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CA2574962C (en) | An al-si-mg-zn-cu alloy for aerospace and automotive castings | |
| US20050199318A1 (en) | Castable aluminum alloy | |
| US20080060723A1 (en) | Aluminum alloy for engine components | |
| JP5758402B2 (en) | Cast parts made of copper aluminum alloy with high mechanical strength and high heat-resistant creep resistance | |
| US20180010214A1 (en) | High strength high creep-resistant cast aluminum alloys and hpdc engine blocks | |
| CN102676887A (en) | Aluminum alloy for pressure casting and casting of the aluminum alloy | |
| JP2005264301A (en) | Cast aluminum alloy, aluminum alloy casting and method for producing the same | |
| Kearney et al. | Aluminum foundry products | |
| JP4145242B2 (en) | Aluminum alloy for casting, casting made of aluminum alloy and method for producing casting made of aluminum alloy | |
| JP2006291327A (en) | Heat-resistant magnesium alloy casting | |
| JP2005187896A (en) | Heat resistant magnesium alloy casting | |
| JPH0565573B2 (en) | ||
| EP1190107B1 (en) | Aluminum-base alloy for cylinder heads | |
| JP2005240129A (en) | Heat resistant magnesium alloy casting | |
| JPH09296245A (en) | Aluminum alloy for casting | |
| CN108149083A (en) | A kind of semisolid pressure casting aluminium alloy and the method for preparing semisolid pressure casting aluminium alloy castings | |
| JPH07258784A (en) | Production of aluminum alloy material for forging excellent in castability and high strength aluminum alloy forging | |
| JPH0375329A (en) | Aluminum alloy and method for its casting | |
| JPS60152648A (en) | Aluminum alloy for molding foundry | |
| JP2005240130A (en) | Heat resistant magnesium alloy casting | |
| JP7749260B1 (en) | Aluminum alloy, aluminum alloy solidified part, and method of manufacturing the same | |
| JP3724362B2 (en) | Aluminum alloy for die casting | |
| Vojtěch et al. | High strength Al–Zn–Mg–Cu–Ni–Si alloy with improved casting properties | |
| RU2022045C1 (en) | Aluminium-base alloy | |
| JPH1017975A (en) | Aluminum alloy for casting |