JPS62127447A - Aluminum alloy for casting - Google Patents
Aluminum alloy for castingInfo
- Publication number
- JPS62127447A JPS62127447A JP60265419A JP26541985A JPS62127447A JP S62127447 A JPS62127447 A JP S62127447A JP 60265419 A JP60265419 A JP 60265419A JP 26541985 A JP26541985 A JP 26541985A JP S62127447 A JPS62127447 A JP S62127447A
- Authority
- JP
- Japan
- Prior art keywords
- casting
- aluminum alloy
- alloy
- refined
- 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.)
- Pending
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/02—Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents
- F04C18/0207—Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents both members having co-operating elements in spiral form
- F04C18/0246—Details concerning the involute wraps or their base, e.g. geometry
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2201/00—Metals
- F05C2201/90—Alloys not otherwise provided for
- F05C2201/903—Aluminium alloy, e.g. AlCuMgPb F34,37
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Continuous Casting (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明はスクロール型流体機械のスクロール部材や各種
鋳造製品に適用される鋳造アルミニウム合金に関する。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a cast aluminum alloy that is applied to scroll members of scroll-type fluid machines and various cast products.
〔従来の技術と発明が解決しようとする問題点〕従来、
耐熱・耐摩耗アルミニウム合金としてエンジンピストン
等の鋳造製品に使用されるAC8Aは、第1表に示すよ
うにAl−5t系の共晶組成であることから、初晶シリ
コンは晶出しない筈であるが、実際の砂型鋳物では50
〜100μm長さの粗大な初晶が析出する。また、大部
分を占める共晶シリコンも50〜150μm長さの−粗
大なものとなる。このため、耐摩耗性は良好であるもの
の靭性が低く (引張り伸びで約1%程度)疲労強度と
くに応力集中部を有する切欠き疲労強度が弱いという欠
点がある。[Problems to be solved by conventional technology and invention] Conventionally,
AC8A, which is used as a heat-resistant and wear-resistant aluminum alloy for cast products such as engine pistons, has an Al-5t-based eutectic composition as shown in Table 1, so primary silicon should not crystallize. However, in actual sand casting, it is 50
Coarse primary crystals with a length of ~100 μm are precipitated. In addition, the eutectic silicon that occupies most of the material is coarse and has a length of 50 to 150 μm. Therefore, although the wear resistance is good, the toughness is low (approximately 1% in terms of tensile elongation), and the fatigue strength, especially notch fatigue strength having stress concentration areas, is weak.
本発明は上記の欠点を解決するためになされたもので、
その目的は、耐摩耗・耐疲労に優れた鋳造アルミニウム
合金を提供することにある。The present invention has been made to solve the above-mentioned drawbacks.
The purpose is to provide a cast aluminum alloy with excellent wear and fatigue resistance.
c問題点を解決するための手段と作用〕本発明に係る鋳
造アルミニウム合金は、従来のAC8Aと同等以上の耐
摩耗性を確保するためにSiを8〜10wt%(以下%
と略す)、引張強度を向ヒさせるためにCuを1.5〜
396およびMgを0.3〜0.5%、初晶シリコンを
微細化するためにTiを0.05〜0.15%、共晶シ
リコンを微細化するためにsbを0.1〜0.296含
有し、残りはAtと機態の不純物(F e。c.Means and effects for solving the problems] The cast aluminum alloy according to the present invention contains 8 to 10 wt% Si (hereinafter %
(abbreviated as ), Cu is added from 1.5 to 1.5 to improve the tensile strength.
396 and Mg by 0.3 to 0.5%, Ti by 0.05 to 0.15% to refine the primary silicon, and sb by 0.1 to 0.1 to refine the eutectic silicon. 296, and the rest are At and mechanical impurities (Fe.
Znなど)よりなるもので、初晶、共晶シリコンの微細
化およびデンドライト組織の微細化ならびに鋳込欠陥の
減少による強1文向1mを図るために高+l: 、u
+、’、l鋳逓法を採用した。Zn, etc.), and in order to achieve a strength of 1 m by 1 m by refining the primary crystal, eutectic silicon, refining the dendrite structure, and reducing casting defects.
+, ', l casting method was adopted.
以下、本発明の実施例について説明する。 Examples of the present invention will be described below.
本実施例では、第2表に示す成分の4種類のアルミニウ
ム合金を用いて試料を、溶湯温度750゛℃、金型温度
250°C1溶湯加圧力1000Kg/cIi2の高圧
凝固法で鋳造した後、510℃×4Hrの溶体化処理を
し、つづいて170℃×4Hrの人工時効処理を施した
。そして、上記の鋳造法で得られた各試料からT字型試
験片を切出し、シャンク式曲げ疲労試験を実施した結果
を第1図に示す。同図から明らかなようにアルミニウム
合金A、B、Cで作成した試料は、従来のAC8Aで作
成したものに比べて疲労強度が約1.5倍以上に向−卜
することがわかる。In this example, samples were cast using four types of aluminum alloys having the components shown in Table 2 using a high-pressure solidification method with a molten metal temperature of 750°C, a mold temperature of 250°C, and a molten metal pressing force of 1000 kg/cIi2. Solution treatment was performed at 510°C for 4 hours, followed by artificial aging treatment at 170°C for 4 hours. Then, T-shaped test pieces were cut out from each sample obtained by the above casting method and subjected to a shank bending fatigue test. The results are shown in FIG. As is clear from the figure, the fatigue strength of the samples made of aluminum alloys A, B, and C is approximately 1.5 times higher than that of the samples made of conventional AC8A.
また、各試料から平板状試験片を切出し、平板と回転リ
ング試片の組合わせで、面圧10に’j/mrn2.す
べり速度1m/see、油潤滑条件下で30mInのす
べり摩耗試験を実施した結果を第2図に、さらに静的強
度を比較した結果を第3図に示す。アルミニウム合金A
、B、Cで作成した試!−1と従来のAC8Aで作成し
たものとは、第2図に示すようにIIf:耗量かほぼ同
じてあり、両者の11−摩耗性が同等であることかわか
る。また、静的強度は第3図に示すように引張強度およ
び伸び率か従来のAC8Aに比べて高くなることがわか
る。In addition, a flat test piece was cut out from each sample, and a surface pressure of 10 and 'j/mrn2. Fig. 2 shows the results of a sliding wear test of 30 mIn at a sliding speed of 1 m/see under oil lubrication conditions, and Fig. 3 shows the results of a comparison of static strength. Aluminum alloy A
Trial created with , B, and C! As shown in FIG. 2, IIf: wear amount is almost the same between the 11-1 and the conventional AC8A, and it can be seen that the 11-abrasion properties of the two are the same. Furthermore, as shown in FIG. 3, it can be seen that the static strength is higher than that of the conventional AC8A in terms of tensile strength and elongation.
以」二のように本発明によれば、従来のAC8Aに比べ
て疲労強度を約1.5倍に向上させることができ、しか
も従来のAC8Aと同等以上の耐摩耗性を得ることがで
きるので、耐摩耗・耐疲労に優れた鋳造アルミニウム合
金を提供できる。As described above, according to the present invention, the fatigue strength can be improved by about 1.5 times compared to the conventional AC8A, and wear resistance equivalent to or higher than that of the conventional AC8A can be obtained. , we can provide cast aluminum alloys with excellent wear and fatigue resistance.
第1図は本発明に係るアルミニウム合金と従来例の疲労
強度を比較した図、第2図は同じく両者の耐摩耗性を比
較した図、第3図は両者の静的強度を比較した図である
。Figure 1 is a diagram comparing the fatigue strength of the aluminum alloy according to the present invention and a conventional example, Figure 2 is a diagram comparing the wear resistance of both, and Figure 3 is a diagram comparing the static strength of both. be.
Claims (1)
:0.3〜0.5%、Ti:0.05〜0.15%、S
b:0.1〜0.2%、残部Al及び不純物からなる耐
摩耗・耐疲労に優れた鋳造アルミニウム合金。Si: 8-10%, Cu: 1.5-3%, Mg in weight%
:0.3~0.5%, Ti:0.05~0.15%, S
b: Cast aluminum alloy with excellent wear and fatigue resistance, consisting of 0.1 to 0.2%, balance Al and impurities.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP60265419A JPS62127447A (en) | 1985-11-26 | 1985-11-26 | Aluminum alloy for casting |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP60265419A JPS62127447A (en) | 1985-11-26 | 1985-11-26 | Aluminum alloy for casting |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS62127447A true JPS62127447A (en) | 1987-06-09 |
Family
ID=17416895
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP60265419A Pending JPS62127447A (en) | 1985-11-26 | 1985-11-26 | Aluminum alloy for casting |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS62127447A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0561212A2 (en) * | 1992-03-16 | 1993-09-22 | AGINFOR AG für industrielle Forschung | Fluid displacement apparatus with a spiral element |
EP0724077A1 (en) * | 1995-01-24 | 1996-07-31 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Scroll type compressor and method for manufacturing the same |
EP0796926A1 (en) * | 1996-03-19 | 1997-09-24 | Denso Corporation | Production method for high strength die cast product |
JP2020125527A (en) * | 2019-02-06 | 2020-08-20 | 昭和電工株式会社 | Aluminum alloy casting material |
-
1985
- 1985-11-26 JP JP60265419A patent/JPS62127447A/en active Pending
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0561212A2 (en) * | 1992-03-16 | 1993-09-22 | AGINFOR AG für industrielle Forschung | Fluid displacement apparatus with a spiral element |
EP0561212A3 (en) * | 1992-03-16 | 1994-01-19 | Aginfor Ag | |
EP0724077A1 (en) * | 1995-01-24 | 1996-07-31 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Scroll type compressor and method for manufacturing the same |
US5755898A (en) * | 1995-01-24 | 1998-05-26 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Scroll type compressor and method for manufacturing the same |
EP0796926A1 (en) * | 1996-03-19 | 1997-09-24 | Denso Corporation | Production method for high strength die cast product |
JP2020125527A (en) * | 2019-02-06 | 2020-08-20 | 昭和電工株式会社 | Aluminum alloy casting material |
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