CN101805860B - Spherical silicon phase aluminum-silicon alloy and technological method thereof - Google Patents
Spherical silicon phase aluminum-silicon alloy and technological method thereof Download PDFInfo
- Publication number
- CN101805860B CN101805860B CN2010101541389A CN201010154138A CN101805860B CN 101805860 B CN101805860 B CN 101805860B CN 2010101541389 A CN2010101541389 A CN 2010101541389A CN 201010154138 A CN201010154138 A CN 201010154138A CN 101805860 B CN101805860 B CN 101805860B
- Authority
- CN
- China
- Prior art keywords
- silicon
- alloy
- aluminum
- melt
- phase
- 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 - Fee Related
Links
- 229910052710 silicon Inorganic materials 0.000 title claims abstract description 43
- 239000010703 silicon Substances 0.000 title claims abstract description 42
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 title claims abstract description 41
- 229910000676 Si alloy Inorganic materials 0.000 title claims abstract description 30
- CSDREXVUYHZDNP-UHFFFAOYSA-N alumanylidynesilicon Chemical compound [Al].[Si] CSDREXVUYHZDNP-UHFFFAOYSA-N 0.000 title claims abstract description 30
- 238000000034 method Methods 0.000 title abstract description 20
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims abstract description 34
- 239000011856 silicon-based particle Substances 0.000 claims abstract description 22
- 239000000155 melt Substances 0.000 claims abstract description 18
- 229910052786 argon Inorganic materials 0.000 claims abstract description 17
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 14
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 14
- 239000007789 gas Substances 0.000 claims abstract description 12
- 229910052751 metal Inorganic materials 0.000 claims abstract description 10
- 239000002184 metal Substances 0.000 claims abstract description 10
- 238000003756 stirring Methods 0.000 claims abstract description 9
- 229910052802 copper Inorganic materials 0.000 claims abstract description 7
- 239000011261 inert gas Substances 0.000 claims abstract description 6
- 239000000725 suspension Substances 0.000 claims abstract description 6
- 238000005266 casting Methods 0.000 claims description 16
- 239000011159 matrix material Substances 0.000 claims description 16
- 238000005728 strengthening Methods 0.000 claims description 8
- 238000002513 implantation Methods 0.000 claims description 7
- 239000002245 particle Substances 0.000 claims description 7
- 238000004140 cleaning Methods 0.000 claims description 4
- 238000002360 preparation method Methods 0.000 claims description 4
- 230000008018 melting Effects 0.000 claims description 2
- 238000002844 melting Methods 0.000 claims description 2
- 229910045601 alloy Inorganic materials 0.000 abstract description 33
- 239000000956 alloy Substances 0.000 abstract description 33
- 238000005516 engineering process Methods 0.000 abstract description 4
- 239000000758 substrate Substances 0.000 abstract 2
- 238000005275 alloying Methods 0.000 abstract 1
- 239000000203 mixture Substances 0.000 description 8
- 230000005496 eutectics Effects 0.000 description 3
- 239000007943 implant Substances 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 239000000843 powder Substances 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- 238000004458 analytical method Methods 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 238000007711 solidification Methods 0.000 description 2
- 230000008023 solidification Effects 0.000 description 2
- 238000009718 spray deposition Methods 0.000 description 2
- 238000009864 tensile test Methods 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- 238000003723 Smelting Methods 0.000 description 1
- KMWBBMXGHHLDKL-UHFFFAOYSA-N [AlH3].[Si] Chemical class [AlH3].[Si] KMWBBMXGHHLDKL-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000007385 chemical modification Methods 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 238000002425 crystallisation Methods 0.000 description 1
- 230000008025 crystallization Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000010907 mechanical stirring Methods 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 239000003607 modifier Substances 0.000 description 1
- 238000002161 passivation Methods 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 238000009827 uniform distribution Methods 0.000 description 1
Images
Landscapes
- Silicon Compounds (AREA)
Abstract
Description
技术领域 technical field
本发明涉及一种球形硅相铝硅合金及其工艺方法,属于金属材料制备技术领域,特别是铝硅合金铸造。The invention relates to a spherical silicon-phase aluminum-silicon alloy and a process method thereof, belonging to the technical field of metal material preparation, in particular to aluminum-silicon alloy casting.
背景技术 Background technique
铝硅系铸造合金具有密度小、比强度高、热膨胀系数小、耐磨耐蚀及高温性能优良等特点,同时有良好的铸造性能,广泛用于汽车、机械等行业中,是发动机及压缩机活塞、汽缸体、斜盘等零部件的理想材料。随着硅含量的升高,高温强度等性能更加优异,铝硅合金已成为制造行业中最受重视的结构材料之一。Aluminum-silicon series casting alloy has the characteristics of low density, high specific strength, small thermal expansion coefficient, excellent wear resistance and corrosion resistance, and high temperature performance, and has good casting performance. It is widely used in automobiles, machinery and other industries. Ideal material for components such as pistons, cylinder blocks, and swash plates. With the increase of silicon content, the properties such as high-temperature strength are more excellent, and aluminum-silicon alloy has become one of the most valued structural materials in the manufacturing industry.
但是,由于铝硅合金在铸造过程中的冷速受到限制,微观组织主要由初生相α-Al和共晶组织(α-Al+Si)或初晶硅和共晶组织构成。其中硅对合金一系列性能有显著影响,而合金中的硅相一般成粗大的板片状(初晶硅)或针状(共晶硅)。因此,国内外对改变硅的形貌以改善合金的微观组织形态进行了各种各样的细化或球化的方法研究。化学变质剂处理虽然能改变铝硅合金中的硅相形貌,但很难使其球形化,硅相尺寸也较大,很难小于10μm。半固态技术、喷射沉积、固液混合铸造技术等是目前很有应用价值的主要方法。固液混合铸造技术结合了半固态铸造和喷射沉积特点,是在过热的铝硅合金熔体中加入同成分或近成分的铝硅合金粉末,经电磁强力搅拌或其他机械搅拌后使熔体与粉末混合均匀,并实现快速凝固,硅相的平均粒径可控制在5μm以下(陈振华,严红革,康智涛等,CN1262334A,2000年8月9日)。但是由于加入是同成分或近成分的合金粉末,熔点较低,易熔解,并且需要复杂的电磁或机械搅拌系统进行强力搅拌才能解决分布均匀化等问题,控制难度及成本仍然较高。However, since the cooling rate of aluminum-silicon alloy is limited during the casting process, the microstructure is mainly composed of primary phase α-Al and eutectic structure (α-Al+Si) or primary silicon and eutectic structure. Among them, silicon has a significant impact on a series of properties of the alloy, and the silicon phase in the alloy is generally in the shape of a thick plate (primary silicon) or needle (eutectic silicon). Therefore, at home and abroad, various methods of refining or spheroidizing have been researched on changing the morphology of silicon to improve the microstructure of the alloy. Although the chemical modification agent treatment can change the morphology of the silicon phase in the aluminum-silicon alloy, it is difficult to make it spherical, and the size of the silicon phase is also relatively large, which is difficult to be smaller than 10 μm. Semi-solid technology, spray deposition, and solid-liquid mixed casting technology are currently the main methods with great application value. The solid-liquid mixed casting technology combines the characteristics of semi-solid casting and spray deposition. It is to add aluminum-silicon alloy powder with the same composition or close composition to the overheated aluminum-silicon alloy melt, and make the melt and The powder is mixed uniformly and solidified rapidly, and the average particle size of the silicon phase can be controlled below 5 μm (Chen Zhenhua, Yan Hongge, Kang Zhitao, etc., CN1262334A, August 9, 2000). However, due to the addition of alloy powders with the same composition or similar composition, the melting point is low and it is easy to melt, and complex electromagnetic or mechanical stirring systems are required for strong stirring to solve problems such as uniform distribution, and the control difficulty and cost are still high.
发明内容 Contents of the invention
本发明的目的在于提供一种球形硅相铝硅合金及其工艺方法,即:首先熔制含Si量为4%左右的铝硅合金熔体,并可添加Cu、Mg、Mn等强化元素对铝基体进行强化。在可控温度的悬浮浇口杯中通过氩气或其他惰性气体向熔体中植入硅颗粒,再浇注到具有负压的金属型模具中,凝固后获得球形硅相铝硅合金铸件或铸锭,球形硅相均匀分布在铝基体中,其大小和数量随植入的硅颗粒粒度和数量而变化,尺寸在2-10μm之间。合金具有高强度、高韧性。工艺简单,易于控制,从而克服现有技术的不足。The purpose of the present invention is to provide a spherical silicon-phase aluminum-silicon alloy and its process method, that is: first melt the aluminum-silicon alloy melt with a Si content of about 4%, and add Cu, Mg, Mn and other strengthening elements to Aluminum matrix for reinforcement. Implant silicon particles into the melt through argon or other inert gases in a suspended sprue cup with controllable temperature, and then pour into a metal mold with negative pressure. After solidification, spherical silicon-phase aluminum-silicon alloy castings or castings are obtained. Ingot, the spherical silicon phase is uniformly distributed in the aluminum matrix, and its size and quantity vary with the size and quantity of implanted silicon particles, and the size is between 2-10 μm. The alloy has high strength and high toughness. The process is simple and easy to control, thereby overcoming the deficiencies of the prior art.
本发明的技术方案是球形硅相铝硅合金及其工艺方法,合金中的Si含量为11-30wt%,硅成细小球形硅相均匀分布于铝基体中,球形硅相尺寸在2-10μm之间,并可添加Cu、Mg、Mn等强化元素对铝基体进行强化。通过以下工艺方法来实现。The technical solution of the present invention is a spherical silicon-phase aluminum-silicon alloy and its process method. The Si content in the alloy is 11-30 wt%, and the silicon is uniformly distributed in the aluminum matrix in the form of a fine spherical silicon phase, and the size of the spherical silicon phase is between 2-10 μm. Between, and Cu, Mg, Mn and other strengthening elements can be added to strengthen the aluminum matrix. This is achieved through the following process methods.
(1)首先熔制含Si量为4wt%左右的铝硅合金熔体,并可添加对铝基体进行强化的Cu、Mg、Mn等强化元素。(1) First, an aluminum-silicon alloy melt with a Si content of about 4wt% is melted, and strengthening elements such as Cu, Mg, and Mn, which strengthen the aluminum matrix, may be added.
(2)将其浇注于可控温度的定量悬浮浇口杯中,熔体温度控制在液相线以上100-150℃。再用纯净氩气或其他惰性气体植入洁净硅颗粒,氩气或其他惰性气体的压力为10-20MPa,硅颗粒的植入量为7-26wt%,粒度为2-10μm。植入前在300-400℃和真空度不低于4.0×10-3Pa的条件下进行洁净处理。(2) It is poured into a temperature-controllable quantitative suspension sprue cup, and the melt temperature is controlled at 100-150° C. above the liquidus line. Then clean silicon particles are implanted with pure argon or other inert gas, the pressure of argon or other inert gas is 10-20MPa, the implanted amount of silicon particles is 7-26wt%, and the particle size is 2-10μm. Before implantation, carry out cleaning treatment under the conditions of 300-400°C and vacuum degree not lower than 4.0×10 -3 Pa.
(3)硅植入后继续通入氩气搅拌熔体10-30秒,立即将熔体从悬浮浇口杯底部的浇注口浇注于具有负压的金属型中获得铸件或铸锭,负压金属型的负压力不低于8.5×10-2Pa。(3) After silicon implantation, continue to pass through the argon gas to stir the melt for 10-30 seconds, and immediately pour the melt from the sprue at the bottom of the suspended sprue cup into a metal mold with negative pressure to obtain castings or ingots. The negative pressure of the metal type is not lower than 8.5×10 -2 Pa.
本发明的优点是:The advantages of the present invention are:
(1)本发明的球形硅相铝硅合金有很好的综合力学性能。球形硅相铝硅合金组织由铝基体和均匀分布的细小球形硅相组成,合金中的球形硅相是通过植入预制的硅颗粒形成,并且硅颗粒在合金熔体中,尖角的熔解而钝化进一步促进了球形硅相的形成,控制结晶凝固过程而得到2-10μm的球形硅相,其大小和数量可随植入的硅颗粒粒度和数量而变化,使合金在具有高强度的同时,又具有高韧性。(1) The spherical silicon-phase aluminum-silicon alloy of the present invention has good comprehensive mechanical properties. The spherical silicon phase aluminum-silicon alloy structure is composed of an aluminum matrix and a uniformly distributed fine spherical silicon phase. The spherical silicon phase in the alloy is formed by implanting prefabricated silicon particles, and the silicon particles are melted in the alloy melt with sharp corners. Passivation further promotes the formation of spherical silicon phase, controlling the crystallization and solidification process to obtain a spherical silicon phase of 2-10 μm, its size and quantity can vary with the size and quantity of implanted silicon particles, so that the alloy has high strength while , and has high toughness.
(2)工艺简单,易于控制。采用氩气植入硅颗粒,硅颗粒被植入的同时,氩气还可对熔体起到精炼、搅拌和保护作用,混合均匀。预制的硅颗粒的粒度和植入量容易控制,植入熔体后获得相应尺寸的球形硅相,从而易于控制合金中球形硅相的大小和数量。(2) The process is simple and easy to control. The silicon particles are implanted with argon gas. While the silicon particles are implanted, the argon gas can also refine, stir and protect the melt, and mix evenly. The particle size and implantation amount of prefabricated silicon particles are easy to control, and spherical silicon phases of corresponding sizes are obtained after implanting into the melt, so that it is easy to control the size and quantity of spherical silicon phases in the alloy.
(3)对合金无污染,节能节材。本发明在合金熔炼和硅颗粒植入过程中不采用机械或电磁搅拌,无复杂的机械或电磁搅拌系统,也不需要添加各种变质剂。(3) No pollution to the alloy, energy saving and material saving. The invention does not use mechanical or electromagnetic stirring in the process of alloy smelting and silicon particle implantation, has no complicated mechanical or electromagnetic stirring system, and does not need to add various modifiers.
附图说明 Description of drawings
图1是球形硅相铝硅合金的铸态组织(200×)。化学成分为(wt%):Si11.6,加入对合金铝基体的强化元素Cu 1.61,Mg 0.52,Mn 0.83。合金铸态组织致密,球形硅相均匀分布于合金基体中,尺寸约为5-8μm。植入的颗粒硅粒度范围为5-10μm,植入量约为合金熔体量的8%。Figure 1 is the as-cast structure (200×) of a spherical silicon-phase aluminum-silicon alloy. The chemical composition is (wt%): Si11.6, adding Cu 1.61, Mg 0.52, Mn 0.83 to strengthen the alloy aluminum matrix. The as-cast structure of the alloy is dense, and the spherical silicon phase is evenly distributed in the alloy matrix, with a size of about 5-8 μm. The particle size of the implanted silicon particles ranges from 5-10 μm, and the implanted amount is about 8% of the amount of the alloy melt.
图2是球形硅相铝硅合金的铸态组织(200×)。化学成分为(wt%):Si 26.3,未加入对合金铝基体的强化元素Cu、Mg、Mn等。合金铸态组织与图1相似,硅相的数量比图1中的多,仍均匀分布于合金基体中,尺寸在5μm以下。植入的硅颗粒硅粒度范围为2-5μm,植入量约为合金熔体量的24%。Fig. 2 is the as-cast structure (200×) of spherical silicon-phase aluminum-silicon alloy. The chemical composition is (wt%): Si 26.3, without adding Cu, Mg, Mn, etc., which are strengthening elements for the alloy aluminum matrix. The as-cast structure of the alloy is similar to that in Figure 1, and the number of silicon phases is more than that in Figure 1, which is still uniformly distributed in the alloy matrix, and the size is below 5 μm. The silicon particle size of the implanted silicon particles ranges from 2-5 μm, and the implanted amount is about 24% of the amount of the alloy melt.
具体实施方式 Detailed ways
下面通过具体实施例子进一步阐述本发明的实质性特点和显著的进步。但本发明并非尽限于此实施案例。The substantive features and remarkable progress of the present invention will be further elaborated below through specific implementation examples. But the present invention is not limited to this implementation case.
实施例1:制备含硅量为12wt%的球形硅相铝硅合金Example 1: Preparation of a spherical silicon-phase aluminum-silicon alloy with a silicon content of 12 wt%
首先熔制含Si量为4wt%左右的铝硅合金熔体,并添加对铝基体进行强化的Cu 1.61,Mg 0.52,Mn 0.83强化元素。将其浇注于可控温度的定量悬浮浇口杯中,熔体温度控制在液相线以上100-150℃。再用纯净氩气植入洁净硅颗粒,氩气的压力为10MPa,硅颗粒的植入量约为合金熔体量的8wt%,粒度范围为5-10μm,植入前在300-400℃和真空度不低于4.0×10-3Pa的条件下进行洁净处理。硅植入后继续通入氩气搅拌熔体10-30秒,立即将熔体从悬浮浇口杯底部的浇注口浇注于具有负压的金属型中获得铸件或铸锭,负压金属型的负压力为7.4×10-2Pa。所得球形相铝硅合金铸件或铸锭的化学成分为(wt%):Si11.6,Cu 1.61,Mg 0.52,Mn 0.83。First, an aluminum-silicon alloy melt with a Si content of about 4wt% is melted, and Cu 1.61, Mg 0.52, and Mn 0.83 strengthening elements for strengthening the aluminum matrix are added. It is poured into a temperature-controllable quantitative suspension sprue cup, and the melt temperature is controlled at 100-150°C above the liquidus line. Then use pure argon gas to implant clean silicon particles, the pressure of argon gas is 10MPa, the implanted amount of silicon particles is about 8wt% of the alloy melt, and the particle size range is 5-10μm. Carry out cleaning treatment under the condition that the vacuum degree is not lower than 4.0×10 -3 Pa. After the silicon is implanted, continue to pass through the argon gas to stir the melt for 10-30 seconds, and immediately pour the melt from the sprue at the bottom of the suspended sprue cup into the metal mold with negative pressure to obtain castings or ingots, the negative pressure metal mold The negative pressure is 7.4×10 -2 Pa. The chemical composition of the obtained spherical phase aluminum-silicon alloy casting or ingot is (wt%): Si11.6, Cu1.61, Mg0.52, Mn0.83.
拉伸实验在SHT4305万能试验机上进行,合金T6处理后抗拉强度σb=377MPa,延伸率δ=4.3%,远高于普通铸造法得到的相当牌号ZL108合金(σb=261MPa,延伸率δ=0.4%,T6处理)的力学性能,有高的强韧性能。金相分析,合金组织致密,球形硅相均匀分布于合金基体中,尺寸约为5-8μm。The tensile test was carried out on the SHT4305 universal testing machine. The tensile strength σ b = 377MPa and the elongation δ = 4.3% of the alloy T6 after treatment were much higher than the equivalent brand ZL108 alloy obtained by the ordinary casting method (σ b = 261MPa, elongation δ =0.4%, T6 treatment) mechanical properties, high toughness. According to the metallographic analysis, the alloy structure is dense, and the spherical silicon phase is evenly distributed in the alloy matrix, with a size of about 5-8 μm.
实施例2:制备含硅量为27wt%的高硅球形硅相铝硅合金Example 2: Preparation of a high-silicon spherical silicon-phase aluminum-silicon alloy with a silicon content of 27wt%
首先熔制含Si量为4wt%左右的铝硅合金熔体,将其浇注于可控温度的定量悬浮浇口杯中,熔体温度控制在液相线以上100-150℃。再用纯净氩气植入洁净硅颗粒,氩气压力为10MPa,硅颗粒的植入量约为合金熔体量的24wt%,植入的颗粒硅粒度范围为2-5μm,植入前在300-400℃和真空度不低于4.0×10-3Pa的条件下进行洁净处理。硅植入后继续通入氩气搅拌熔体10-30秒,立即将熔体从悬浮浇口杯底部的浇注口浇注于具有负压的金属型中获得铸件或铸锭,负压金属型的负压力不低于7.4×10-2Pa。First, an aluminum-silicon alloy melt with a Si content of about 4wt% is melted, and poured into a temperature-controllable quantitative suspension sprue cup, and the melt temperature is controlled at 100-150° C. above the liquidus line. Then use pure argon gas to implant clean silicon particles, the pressure of argon gas is 10MPa, the implanted amount of silicon particles is about 24wt% of the alloy melt, and the particle size range of implanted silicon particles is 2-5μm. Carry out cleaning treatment under the condition of -400℃ and vacuum not lower than 4.0×10 -3 Pa. After the silicon is implanted, continue to pass through the argon gas to stir the melt for 10-30 seconds, and immediately pour the melt from the sprue at the bottom of the suspended sprue cup into the metal mold with negative pressure to obtain castings or ingots, the negative pressure metal mold The negative pressure is not lower than 7.4×10 -2 Pa.
拉伸实验在SHT4305万能试验机上进行,合金抗拉强度σb=184MPa,延伸率δ=6.6%,远高于普通铸造法得到的含硅量为27%的铝硅合金(σb=38MPa,延伸率δ=0%)的力学性能,有高的强韧性能。金相分析,合金组织致密,球形硅相均匀分布于合金基体中,尺寸约为2-4μm。The tensile test was carried out on the SHT4305 universal testing machine. The tensile strength of the alloy σ b = 184MPa, the elongation δ = 6.6%, much higher than the aluminum-silicon alloy with a silicon content of 27% obtained by the ordinary casting method (σ b = 38MPa, Elongation δ = 0%) mechanical properties, high strength and toughness. Metallographic analysis shows that the structure of the alloy is dense, and the spherical silicon phase is evenly distributed in the alloy matrix, with a size of about 2-4 μm.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2010101541389A CN101805860B (en) | 2010-04-21 | 2010-04-21 | Spherical silicon phase aluminum-silicon alloy and technological method thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2010101541389A CN101805860B (en) | 2010-04-21 | 2010-04-21 | Spherical silicon phase aluminum-silicon alloy and technological method thereof |
Publications (2)
Publication Number | Publication Date |
---|---|
CN101805860A CN101805860A (en) | 2010-08-18 |
CN101805860B true CN101805860B (en) | 2011-11-16 |
Family
ID=42607815
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2010101541389A Expired - Fee Related CN101805860B (en) | 2010-04-21 | 2010-04-21 | Spherical silicon phase aluminum-silicon alloy and technological method thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN101805860B (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103757499B (en) * | 2014-01-03 | 2016-02-24 | 西华大学 | Hot spray iron particle prepares the processing method of ferroaluminium |
CN111482613B (en) * | 2019-01-25 | 2021-11-09 | 北京理工大学 | High-physical-activity aluminum-silicon spherical alloy powder and preparation method and application thereof |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH01180938A (en) * | 1988-01-12 | 1989-07-18 | Ryobi Ltd | Wear-resistant aluminum alloy |
US7069897B2 (en) * | 2001-07-23 | 2006-07-04 | Showa Denko K.K. | Forged piston for internal combustion engine and manufacturing method thereof |
CN1298878C (en) * | 2003-12-03 | 2007-02-07 | 东华大学 | Aluminum silicon alloy series possessing granulated silicon phase and its process |
-
2010
- 2010-04-21 CN CN2010101541389A patent/CN101805860B/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
CN101805860A (en) | 2010-08-18 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN105525158B (en) | A kind of semisolid pressure casting aluminum alloy materials and the method using the material die cast | |
CN106609331B (en) | High-ductility diecast magnesium alloy and its manufacturing process | |
CN100588733C (en) | A kind of magnesium alloy for semi-solid forming and its semi-solid blank preparation method | |
CN102304642A (en) | Cast wear-resistant tin bronze alloy and preparation method thereof | |
CN108342606B (en) | A method for improving the microstructure and properties of in-situ aluminum matrix composites with mixed rare earths | |
CN103993200B (en) | A silicon-containing wear-resistant zinc-based alloy and its preparation method | |
CN109957686B (en) | A kind of aluminum-silicon alloy for cylinder liner and preparation process | |
CN110438371A (en) | A kind of low segregation control of the high cobalt as cast condition nickel alloy of high tungsten and plasticity method for improving | |
CN104894447A (en) | Layered/acicular two-phase composite enhanced rare earth magnesium alloy and preparation technology thereof | |
CN101857934A (en) | Heat-resistant magnesium alloy and preparation method thereof | |
CN103243236A (en) | High-toughness wear-resistant zinc alloy containing fine crystalline grains and preparation process for same | |
CN117026003A (en) | Aluminum-based composite material stirring casting preparation method based on composite modification refinement | |
CN101774013A (en) | Composite grain finer for Mg-Al alloy and preparation method thereof | |
CN102965556B (en) | Multi-element Mg-Zn-Al based magnesium alloy and preparation method thereof | |
CN101805860B (en) | Spherical silicon phase aluminum-silicon alloy and technological method thereof | |
CN102418009B (en) | Aluminum alloy capable of digesting high-hardness compounds and smelting method of aluminum alloy | |
CN102660693A (en) | Aluminum alloy treated by using TiN powder and BeH2 powder, and preparation method thereof | |
CN101705405B (en) | Magnesium base spherical quasicrystal master alloy and preparation method thereof | |
CN106756180B (en) | A kind of calcium/magnesia grain refiner and its preparation method and application | |
CN101880806A (en) | Heatproof magnesium alloy and preparation method thereof | |
CN101705407B (en) | Magnesium-based spherical quasicrystalline master alloy and its preparation method | |
CN101654745B (en) | Preparation method of Al-5 percent Cu base alloy with low heat cracking tendency | |
CN102433471A (en) | High-toughness aluminum alloy and preparation method thereof | |
CN107385259A (en) | A kind of method of hypoeutectic al-si alloy fine degenerate | |
CN106011563A (en) | Hypo eutectic aluminum-magnesium alloy reinforcing method through melt compounding treatment |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C17 | Cessation of patent right | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20111116 Termination date: 20130421 |