CN107267817A - A kind of high-strength antifatigue in-situ nano reinforced aluminium alloy and its pressure casting method - Google Patents
A kind of high-strength antifatigue in-situ nano reinforced aluminium alloy and its pressure casting method Download PDFInfo
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Abstract
本发明涉及铝基复合材料,特指一种高强抗疲劳原位纳米强化铝合金及其压铸方法。通过原位纳米强化和合金成分调控,并结合优化的非线性高压压铸工艺获得压铸件。借助原位纳米ZrB2增强体和纳米Al3Er析出相的尺度效应、界面效应、异质形核效应,显著提高合金的强度、抗疲劳性能和阻尼性能;与此同时,提高了Mg、Zn和Fe元素含量,并引入Mn和Ni元素,在提高强化相含量、获得高强度的同时,使Al‑Fe等有害的粗大析出相有效细化和圆顿化,并保障合金良好的压铸性能;从而,采用本发明合金及其压铸方法所生产的构件表现出高强塑性、高抗疲劳性、高阻尼性能以及良好的压铸性能的特点。
The invention relates to an aluminum-based composite material, in particular to a high-strength anti-fatigue in-situ nano-reinforced aluminum alloy and a die-casting method thereof. Die castings are obtained through in-situ nano-strengthening and alloy composition regulation, combined with an optimized nonlinear high-pressure die-casting process. With the help of the in-situ nano-ZrB 2 reinforcement and the scale effect, interface effect, and heterogeneous nucleation effect of the nano-Al 3 Er precipitated phase, the strength, fatigue resistance, and damping properties of the alloy are significantly improved; at the same time, the Mg, Zn and Fe element content, and the introduction of Mn and Ni elements, while increasing the strengthening phase content and obtaining high strength, the harmful coarse precipitates such as Al-Fe are effectively refined and rounded, and the good die-casting performance of the alloy is ensured; Therefore, the components produced by the alloy of the invention and its die-casting method exhibit the characteristics of high strength plasticity, high fatigue resistance, high damping performance and good die-casting performance.
Description
技术领域technical field
本发明涉及铝基复合材料,特指一种高强抗疲劳原位纳米强化铝合金及其压铸方法。The invention relates to an aluminum-based composite material, in particular to a high-strength anti-fatigue in-situ nano-reinforced aluminum alloy and a die-casting method thereof.
背景技术Background technique
随着经济和社会的发展,汽车已逐渐进入寻常百姓家,成为人们出行生活的必备工具。中国汽车工业协会统计显示,2016年中国品牌乘用车共销售1052.86万辆,同比增长20.50%。发动机作为汽车的心脏,其关键部件生产的高效率、低成本和高性能已成为各大汽车厂商提升产品竞争力的核心。With the development of economy and society, automobiles have gradually entered the homes of ordinary people and become an indispensable tool for people to travel and live. Statistics from the China Association of Automobile Manufacturers show that in 2016, a total of 10.5286 million Chinese brand passenger cars were sold, a year-on-year increase of 20.50%. The engine is the heart of the car, and the high efficiency, low cost and high performance of its key components have become the core of major car manufacturers to improve their product competitiveness.
高压铸造以其生产效率高、经济性好、铸件精度高、表面光洁度好的优点,逐渐替代高成本的低压、重力铸造,成为铝制发动机缸体、油泵壳体、减震构件等汽车发动机关键零部件的主要制造方式。然而,高压铸造由于液态金属充填型腔速度高,流态不稳,所生产的铸件易于产生气孔、不能热处理,导致铸件中析出相通常呈粗大的针状或片状结构、强化效果不明显、易于产生应力集中,使其强塑性、抗疲劳性能偏低。从而使高压压铸件难以完全替代低压铸造、重力铸造件,尤其是难以应用于对性能要求高的中高端汽车用发动机。With its advantages of high production efficiency, good economy, high casting precision and good surface finish, high-pressure casting gradually replaces high-cost low-pressure and gravity casting, and becomes the key to automobile engines such as aluminum engine cylinder blocks, oil pump housings, and shock absorbing components. The primary method of manufacturing the component. However, due to the high speed of liquid metal filling the cavity and the unstable flow state of high-pressure casting, the produced castings are prone to pores and cannot be heat-treated, resulting in the precipitated phases in the castings usually having a coarse needle-like or flaky structure, and the strengthening effect is not obvious. It is easy to produce stress concentration, making its strong plasticity and fatigue resistance low. As a result, it is difficult for high-pressure die castings to completely replace low-pressure castings and gravity castings, especially for mid-to-high-end automotive engines with high performance requirements.
发明内容Contents of the invention
本发明的目的就在于针对现有压铸用典型铝合金AlSi9Cu3强塑性、抗疲劳性能偏低,尤其是不能满足高性能发动机部件对其高强度、抗疲劳、高阻尼的技术要求的不足,通过合金成分调控和原位纳米强化,并结合优化的非线性高压压铸方法,在提高合金析出相含量、圆顿化和细化同时,实现晶内和晶界的原位纳米陶瓷增强体强化,显著提高压铸制品的强塑性、抗疲劳性和阻尼性能。The purpose of the present invention is to solve the problem that the existing typical aluminum alloy AlSi9Cu3 for die-casting has low strong plasticity and fatigue resistance, and especially cannot meet the technical requirements of high-performance engine parts for its high strength, fatigue resistance and high damping. Composition control and in-situ nano-strengthening, combined with the optimized nonlinear high-pressure die-casting method, can increase the content of alloy precipitates, rounding and refining, and at the same time realize the in-situ nano-ceramic reinforcement strengthening in the grain and grain boundary, significantly improving Strong plasticity, fatigue resistance and damping properties of die-casting products.
采用本发明技术生产的汽车发动机用减震支架和壳体的抗拉强度可达352MPa,屈服强度达到285MPa,延伸率可达10.6%。最终产品经专用台架进行耐久性试验,最少循环次数达到了100万次,远高于客户要求的50万次,达到了德国大众(减震支架)DIN EN1706-1998标准和日本马自达(减震壳体)MES MM 621-ADC12标准,同时也超过了采用低压铸造(固溶+时效热处理后)生产的减震支架性能(抗拉强度300MPa,屈服强度210MPa,延伸率7.5%)。The tensile strength of the vibration-absorbing support and the shell for the automobile engine produced by the technology of the invention can reach 352MPa, the yield strength can reach 285MPa, and the elongation can reach 10.6%. The final product has undergone a durability test on a special bench, and the minimum number of cycles has reached 1 million, which is much higher than the 500,000 times required by the customer. It has reached the DIN EN1706-1998 standard of German Volkswagen (shock absorbing bracket) and Japan Mazda (shock absorbing bracket) Shell) MES MM 621-ADC12 standard, and also exceeds the performance of the shock absorber bracket produced by low-pressure casting (after solid solution + aging heat treatment) (tensile strength 300MPa, yield strength 210MPa, elongation 7.5%).
本发明的一种高强抗疲劳且阻尼性能好的压铸用原位纳米强化铝合金及其压铸方法,通过合金成分调控和原位纳米强化,并结合优化的非线性高压压铸获得晶内和晶界包含大量且分散均匀的纳米ZrB2陶瓷增强体,晶内包含纳米Al3Er析出相,包括共晶Si相,Mg2Si相,Al2Cu相和含Fe相在内的合金析出相细小、圆顿的压铸件。借助纳米增强体和纳米析出相的弥散强化、界面阻尼效应以及低固溶度的Er元素在合金熔体产生的Al3Er相晶粒细化作用,显著提高合金构件的强塑性、抗疲劳和阻尼性能;与此同时,Mg、Zn和Fe元素含量的提高,以及Mn和Ni元素引入,在保障良好压铸性能、提高合金强化相含量的同时,使Al-Fe等合金强化相有效细化和圆顿化;从而,使本发明合金所生产的构件表现出高强塑性、高抗疲劳性和良好阻尼性能的特点。An in-situ nano-strengthened aluminum alloy for die-casting with high strength, anti-fatigue and good damping performance and its die-casting method, through alloy composition control and in-situ nano-strengthening, combined with optimized nonlinear high-pressure die-casting to obtain intra-granular and grain boundaries Contains a large number of uniformly dispersed nano-ZrB 2 ceramic reinforcements, contains nano-Al 3 Er precipitates in the grain, and alloy precipitates including eutectic Si phase, Mg2Si phase, Al2Cu phase and Fe-containing phase are fine and round Die-casting pieces. With the aid of the dispersion strengthening of nano-reinforcement and nano-precipitated phase, interface damping effect and the grain refinement of Al 3 Er phase produced by the low solid-solubility Er element in the alloy melt, the strong plasticity, fatigue resistance and Damping performance; at the same time, the increase of Mg, Zn and Fe element content, as well as the introduction of Mn and Ni elements, while ensuring good die-casting performance and increasing the content of alloy strengthening phase, can effectively refine and refine the alloy strengthening phase such as Al-Fe. Rounding; thus, the components produced by the alloy of the present invention exhibit the characteristics of high strength plasticity, high fatigue resistance and good damping performance.
本发明的制备方法包括以下步骤:The preparation method of the present invention comprises the following steps:
(1)合金熔炼:将AlSi9Cu3合金熔化至750-780℃并保温10min。所述的AlSi9Cu3合金为商用合金,其具体化学成分的元素质量百分比为:Si 8.0~11.0,Cu 2.0~3.5,Zn 1.0~1.5,Mg 0.3~0.5,Fe≤0.8,Mn 0.1~0.5,余量为Al。(1) Alloy smelting: Melt the AlSi9Cu3 alloy to 750-780°C and keep it warm for 10min. The AlSi9Cu3 alloy is a commercial alloy, and the mass percentages of its specific chemical composition are: Si 8.0-11.0, Cu 2.0-3.5, Zn 1.0-1.5, Mg 0.3-0.5, Fe≤0.8, Mn 0.1-0.5, the balance for Al.
(2)原位合成纳米ZrB2纳米陶瓷增强体:将Al-Zr和Al-B中间合金加入步骤(1)熔炼并保温的熔体中并迅速升温至840-860℃,同时采用石墨搅拌转子搅动熔体以促进合金的充分混合,保温时间为10-15min,使合金中的Zr和B元素在自由能降低的驱动力下原位反应合成纳米ZrB2陶瓷增强体,然后降温至730-750℃并保温。使得步骤(2)合金中锆硼元素的质量百分比达到Zr:3.0-5.0,B:0.5-1.0。(2) In situ synthesis of nano-ZrB 2 nano-ceramic reinforcement: Add Al-Zr and Al-B master alloys to the melt smelted and kept warm in step (1) and rapidly heat up to 840-860 ° C, while using graphite stirring rotor Stir the melt to promote the full mixing of the alloy. The holding time is 10-15min, so that the Zr and B elements in the alloy react in situ under the driving force of free energy reduction to synthesize nano - ZrB2 ceramic reinforcement, and then cool down to 730-750 ℃ and keep warm. Make the mass percent of zirconium and boron in the alloy in step (2) reach Zr: 3.0-5.0, B: 0.5-1.0.
(3)引入Er和Ni元素,调整合金中Fe和Mn元素的含量并精炼除气:将Al-Er、Al-Fe和Al-Mn中间合金以及纯Ni加入步骤(2)所获得的复合熔体中,并采用石墨搅拌转子搅动以促进合金的充分混合,保温搅拌时间为10-15min;然后将粒度小于500μm的粉末状复合精炼剂用惰性气体通过石墨转子的中空通道吹入熔体中,对熔体进行精炼除气,以去除合金高温熔炼和反应过程中产生的夹渣和熔体中溶入的氢,精炼温度为730-750℃,精炼保温时间为25-30min。最终使步骤(3)合金中铒镍铁元素含量达到Er:0.1-0.15,Fe:1.0~1.5,Mn:0.5~1.0,Ni 0.5~1.0。(3) Introducing Er and Ni elements, adjusting the content of Fe and Mn elements in the alloy and refining and degassing: adding Al-Er, Al-Fe and Al-Mn master alloys and pure Ni to the composite melt obtained in step (2) In the body, the graphite stirring rotor is used to stir to promote the full mixing of the alloy, and the heat preservation and stirring time is 10-15min; then the powdered composite refining agent with a particle size of less than 500 μm is blown into the melt through the hollow channel of the graphite rotor with inert gas, Refining and degassing the melt to remove slag inclusions and hydrogen dissolved in the melt during high-temperature smelting and reaction of the alloy. The refining temperature is 730-750°C, and the refining holding time is 25-30min. Finally, the content of erbium-nickel-iron element in the alloy in step (3) reaches Er: 0.1-0.15, Fe: 1.0-1.5, Mn: 0.5-1.0, Ni 0.5-1.0.
(4)调整Mg,Zn元素的含量:将步骤(3)获得的熔体降温至660-700℃并保温,然后将纯Mg和纯Zn采用钟罩压入精炼除气后的熔体中,启动石墨搅拌转子,并慢速搅拌,保温搅拌时间>15min,以使Mg,Zn溶入合金并避免熔体吸气,且使步骤(4)合金中镁锌元素含量达到Mg:0.5~1.0,Zn:1.5~2.5。(4) Adjusting the content of Mg and Zn elements: cooling the melt obtained in step (3) to 660-700° C. and keeping it warm, then pressing pure Mg and pure Zn into the melt after refining and degassing with a bell jar, Start the graphite stirring rotor, and stir at a slow speed. The heat preservation and stirring time is >15min, so that Mg and Zn can be dissolved into the alloy and prevent the melt from absorbing gas, and the content of magnesium and zinc in the alloy in step (4) can reach Mg: 0.5~1.0, Zn: 1.5-2.5.
(5)非线性高压压铸:将步骤(4)获得的复合熔体置入压铸机的保温包中,采用优化的非线性压铸工艺进行压铸获得纳米复合强化压铸件,其中压射速度为从小到大的抛物线式压射、以实现前期缓慢充型2.5-3m/s,终了瞬间高速充型的非线性充型(最大压射速度达到40-50m/s,压铸压力达到100-150MPa)。(5) Non-linear high-pressure die-casting: Put the composite melt obtained in step (4) into the insulation bag of the die-casting machine, and use the optimized non-linear die-casting process for die-casting to obtain nano-composite reinforced die-castings, where the injection speed is from small to Large parabolic injection to realize the slow filling of 2.5-3m/s in the early stage, and the nonlinear filling of instantaneous high-speed filling at the end (the maximum injection speed reaches 40-50m/s, and the die-casting pressure reaches 100-150MPa).
(6)时效处理:将步骤(5)获得的压铸件进行时效处理(自然时效或人工时效),以获得高强抗疲劳且阻尼性能好的原位纳米强化铝合金压铸件。(6) Aging treatment: The die-casting obtained in step (5) is subjected to aging treatment (natural aging or artificial aging), so as to obtain an in-situ nano-strengthened aluminum alloy die-casting with high strength, fatigue resistance and good damping performance.
所述的Al-Zr、Al-B、Al-Er、Al-Fe和Al-Mn中间合金,优选合金化元素含量高的中间合金,如Al-10Zr、Al-10B、Al-20Er、Al-20Fe和Al-10Mn。The Al-Zr, Al-B, Al-Er, Al-Fe and Al-Mn master alloys are preferably master alloys with high content of alloying elements, such as Al-10Zr, Al-10B, Al-20Er, Al- 20Fe and Al-10Mn.
所述的原位合成纳米ZrB2纳米陶瓷增强体,是指利用该多元合金体系中ZrB2的吉布斯自由能低,且Zr在Al中具有低溶解度和低热扩散系数的热力学-动力学特性,在合金中引入Zr、B元素后,在熔体中原位合成纳米级的ZrB2陶瓷颗粒,其尺寸为20-80nm,含量为合金质量的2-6wt.%,合成温度为840-860℃。从而在合金熔体凝固过程中:一方面,原位纳米ZrB2陶瓷颗粒可作为异质形核核心提高合金的形核率,细化晶粒,并最终包含分散于合金晶粒内部,显著提高合金的强度、抗疲劳性能;另一方面,未成为形核核心的纳米ZrB2陶瓷颗粒会在晶粒长大的过程中分散于晶界,可有效钉扎晶界并阻碍晶界的迁移,提高合金强度的同时、最大化发挥界面阻尼作用,提高合金的阻尼性能。The in-situ synthesis of nano-ZrB2 nano - ceramic reinforcement refers to the use of the low Gibbs free energy of ZrB2 in the multi - element alloy system, and the thermodynamic-dynamic properties of Zr having low solubility and low thermal diffusivity in Al , after introducing Zr and B elements into the alloy, in - situ synthesis of nanoscale ZrB2 ceramic particles in the melt, the size of which is 20-80nm, the content is 2-6wt.% of the alloy mass, and the synthesis temperature is 840-860°C . Therefore, in the solidification process of the alloy melt: on the one hand, the in-situ nano - ZrB2 ceramic particles can be used as heterogeneous nucleation cores to improve the nucleation rate of the alloy, refine the grains, and finally include and disperse in the alloy grains, significantly improving The strength and fatigue resistance of the alloy; on the other hand, the nano - ZrB2 ceramic particles that have not become the nucleation core will disperse at the grain boundary during the grain growth process, which can effectively pin the grain boundary and hinder the migration of the grain boundary. While improving the strength of the alloy, it maximizes the interface damping effect and improves the damping performance of the alloy.
所述的引入Er和Ni元素,调整合金中Fe和Mn元素的含量并精炼除气,是指在合金中引入的0.1-0.15wt.%的Er,一方面借助Er在铝溶体中低的溶解度(0.1wt.%),在合金熔体中析出Al3Er异质形核核心提高铝的形核率,细化合金,另一方面固溶于合金中Er元素,会在合金时效时在晶内析出细小且与铝基体晶格匹配良好的L12型纳米Al3Er析出相,显著提高合金压铸件的时效强度和抗疲劳性能;在合金中增加Fe元素的含量的目的是提高合金中Fe析出相含量,提高合金强度的同时,进一步提高合金的抗粘模性能,避免合金析出相含量增高、膨胀系降低所导致脱模难和粘模问题,引入Ni元素并提高Mn元素含量的目的是通过Ni、Mn与合金中针片状的β-Fe相转变成块状或汉字状的α-Al(Mn,Fe)Si和α-Al(Ni,Fe)Si相,避免Fe含量的提高产生大量的针状β-Fe相降低合金的塑韧性。The introduction of Er and Ni elements, adjusting the content of Fe and Mn elements in the alloy and refining and degassing refers to the introduction of 0.1-0.15wt.% Er in the alloy, on the one hand, by virtue of the low solubility of Er in the aluminum solution (0.1wt.%), the precipitation of Al 3 Er heterogeneous nucleation cores in the alloy melt improves the nucleation rate of aluminum and refines the alloy. The fine L1 2 nano-Al 3 Er precipitates that are finely matched with the aluminum matrix lattice are precipitated, which can significantly improve the aging strength and fatigue resistance of alloy die-casting parts; the purpose of increasing the content of Fe in the alloy is to increase the Fe content in the alloy. Precipitated phase content, while improving the strength of the alloy, further improve the anti-sticking performance of the alloy, avoiding the difficulty of demolding and sticking caused by the increase in the content of precipitated phases and the decrease in the expansion system of the alloy. The purpose of introducing Ni element and increasing the content of Mn element is Through the transformation of Ni, Mn and the needle-like β-Fe phase in the alloy into the bulk or Chinese character-like α-Al(Mn,Fe)Si and α-Al(Ni,Fe)Si phases, avoiding the increase of Fe content A large amount of acicular β-Fe phase reduces the ductility and toughness of the alloy.
所述的调整Mg,Zn元素的含量,是进一步提高合金中析出相的含量,以提高合金强度,抗疲劳性能,并借助增加的相界提高合金的阻尼性能。The adjustment of the content of Mg and Zn elements is to further increase the content of the precipitated phase in the alloy to improve the strength and fatigue resistance of the alloy, and to improve the damping performance of the alloy by means of the increased phase boundary.
所述的非线性高压压铸工艺,是指采用压铸缸体速度可编程控制的新型压铸机,并优化其获得的非线性高压压铸工艺,以从避免熔体充型过程中的紊流和卷气、利于型腔中气体的排出并在充满型腔的瞬时高速高压下促进纳米增强体的浸润和分散,以获得组织缺陷少、性能优良的压铸产品。其中压射速度为从小到大的抛物线式压射、以实现前期缓慢充型2.5-3m/s,终了瞬间高速充型的非线性充型(最大压射速度达到40-50m/s,压铸压力达到100-150MPa)。The non-linear high-pressure die-casting process refers to a new type of die-casting machine that adopts a programmable control of the speed of the die-casting cylinder, and optimizes the non-linear high-pressure die-casting process obtained to avoid turbulence and entrainment during the filling process of the melt , Facilitate the discharge of gas in the cavity and promote the infiltration and dispersion of nano-reinforcements under the instantaneous high-speed and high-pressure filling the cavity, so as to obtain die-casting products with less structural defects and excellent performance. Among them, the injection speed is parabolic injection from small to large, so as to realize the slow filling of 2.5-3m/s in the early stage, and the nonlinear filling of high-speed filling at the end (the maximum injection speed reaches 40-50m/s, and the die-casting pressure reach 100-150MPa).
附图说明Description of drawings
图1(a)为常规AlSi9Cu3压铸件金相组织图,(b)为本发明制备的高强抗疲劳且阻尼性能好的原位纳米强化铝合金减震支架压铸件金相组织图,从两金相组织图可以看出,采用本专利所制备的压铸件中针状析出相消失,转化为颗粒状或短片状的圆顿析出相,提高了析出相的弥散程度,利于工件强塑性和疲劳性能的提高。Fig. 1 (a) is the metallographic structure diagram of conventional AlSi9Cu3 die-casting parts, (b) is the metallographic structure diagram of the in-situ nano-strengthened aluminum alloy shock absorbing bracket die-casting parts with high strength anti-fatigue and good damping performance prepared by the present invention, from two gold It can be seen from the phase structure diagram that the needle-shaped precipitates in the die-casting parts prepared by this patent disappear and transform into granular or short-sheet-shaped rounded precipitates, which improves the dispersion of the precipitates and is beneficial to the strong plasticity and fatigue properties of the workpiece. improvement.
图2本发明制备的高强抗疲劳且阻尼性能好的原位纳米强化铝合金减震支架压铸件TEM组织图,从图中可以看出,采用本专利所制备的压铸件的晶内和晶界存在的原位纳米ZrB2陶瓷增强相和更加细小均匀纳米Al3Er纳米析出相,利于工件强塑性、抗疲劳性能和阻尼性能的综合提高。Fig. 2 The TEM structure diagram of the in-situ nano-reinforced aluminum alloy shock-absorbing bracket die-casting with high strength and fatigue resistance and good damping performance prepared by the present invention. It can be seen from the figure that the die-casting prepared by this patent has the intragranular and grain boundaries The existing in-situ nano-ZrB 2 ceramic reinforcement phase and finer and uniform nano-Al 3 Er nano-precipitated phase are beneficial to the comprehensive improvement of the workpiece's strong plasticity, fatigue resistance and damping performance.
具体实施方式detailed description
以下结合附图对本发明实施方案进一步描述:以下实施例在以本发明技术方案为前提下进行实施,给出了详细的实施方式和具体的操作过程,但本发明的保护范围不限于下述的实施例。The embodiments of the present invention are further described below in conjunction with the accompanying drawings: the following examples are implemented on the premise of the technical solutions of the present invention, and detailed implementation methods and specific operating procedures are provided, but the protection scope of the present invention is not limited to the following Example.
实施例1Example 1
以Al-10Zr、Al-10B、Al-20Er、Al-20Fe、Al-10Mn中间合金和纯Ni、纯Mg、纯Zn,以及AlSi9Cu3为原料,采用优化的非线性高压压铸技术制备汽车发动机用减震支架。Using Al-10Zr, Al-10B, Al-20Er, Al-20Fe, Al-10Mn master alloys and pure Ni, pure Mg, pure Zn, and AlSi9Cu3 as raw materials, the optimized non-linear high-pressure die-casting technology is used to prepare the automotive engine. Shock bracket.
将熔融的500Kg商用AlSi9Cu3合金(760℃)转入中间保温炉中,然后将Al-10Zr和Al-10B中间合金加入保温炉中并升温至850℃,同时采用石墨搅拌转子搅动熔体以促进合金的充分混合,保温时间为15min,然后将合金降温至750℃并保温;将Al-20Er、Al-20Fe和Al-10Mn以及纯Ni加入熔体中,搅拌保温15min后将粒径小于500μm的粉末状复合精炼剂用惰性气体通过石墨转子的中空通道吹入熔体中,对熔体进行精炼除气,以去除合金高温熔炼和反应过程中产生的夹渣和熔体中溶入的氢,精炼时间为30min,温度保持在750℃,精炼除气结束后降温至680℃并将纯Mg和纯Zn用钟罩压入精炼除气后的熔体中,启动石墨搅拌转子,并慢速搅拌,保温搅拌时间18min,使合金最终成分达到Si 9.5,Cu 3,Zr 3.5,B0.75,Zn 1.5,Mg 0.8,Fe 1.3,Mn 1.0,Ni 0.7,Er 0.12,余量为Al,最后将获得的复合熔体以优化的非线性高压压铸工艺制备减震支架,其中前期为3m/s缓慢充型,以实现平流充型并利于模具型腔中气体的顺利排出,待型腔充满(冒口未充满)的瞬间,提高压射速度至40m/s,并在保持压力至100MPa,保压时间为15s,获得压铸减震支架。The molten 500Kg commercial AlSi9Cu3 alloy (760°C) was transferred to the intermediate holding furnace, then the Al-10Zr and Al-10B intermediate alloys were added to the holding furnace and the temperature was raised to 850°C, while the graphite stirring rotor was used to stir the melt to promote the alloying process. Mix well, keep warm for 15min, then cool the alloy down to 750°C and keep warm; add Al-20Er, Al-20Fe, Al-10Mn and pure Ni into the melt, stir and keep warm for 15min, then put the powder with particle size less than 500μm Shaped composite refining agent blows inert gas into the melt through the hollow channel of the graphite rotor, and refines and degasses the melt to remove the slag inclusions generated during the high-temperature melting and reaction of the alloy and the hydrogen dissolved in the melt. Refining The time is 30 minutes, the temperature is kept at 750°C, after the refining and degassing is completed, the temperature is lowered to 680°C and pure Mg and pure Zn are pressed into the refined and degassed melt with a bell jar, and the graphite stirring rotor is started and stirred at a slow speed. The heat preservation and stirring time is 18min, so that the final composition of the alloy reaches Si 9.5, Cu 3, Zr 3.5, B0.75, Zn 1.5, Mg 0.8, Fe 1.3, Mn 1.0, Ni 0.7, Er 0.12, and the balance is Al. Finally, the obtained Composite melt is used to prepare shock-absorbing bracket by optimized nonlinear high-pressure die-casting process. In the early stage, the mold is slowly filled at 3m/s to achieve advection filling and facilitate the smooth discharge of gas in the mold cavity. At the moment of full filling), increase the injection speed to 40m/s, and keep the pressure at 100MPa for 15s to obtain a die-casting shock absorber.
将切除浇冒口和飞边的压铸毛坯,放入热处理炉中进行人工时效,时效温度的300℃,时效时间为8小时。Put the die-casting blank with the sprue and flash removed into a heat treatment furnace for artificial aging. The aging temperature is 300°C and the aging time is 8 hours.
取样分析表明,减震支架的硬度大于97HBS,抗拉强度达到了352MPa,屈服强度达到了285MPa,延伸率为10.6%,在7.6kN载荷下拉压疲劳试验寿命大于2×106次,最终产品经专用台架进行耐久性试验,最少循环次数达到了100万次,远高于客户要求50万次。产品达到德国大众(减震支架)DIN EN1706-1998标准和日本马自达(减震壳体)MES MM 621-ADC12标准。如图1b所示为采用本实施例工艺所制备的减震支架的金相组织图,从图中可以看出相比常规AlSi9Cu3压铸件,本专利所制备的压铸件中的针状析出相消失,转化为颗粒状或短片状的圆顿析出相,提高了析出相的弥散程度,利于工件强塑性和疲劳性能的提高。图2为本实施例工艺所制备减震支架压铸件TEM组织图,从图中可以看出,采用本专利所制备的压铸件的晶内和晶界存在大量的原位纳米ZrB2陶瓷增强相和更加细小均匀纳米Al3Er纳米析出相,利于工件强塑性、抗疲劳性能和阻尼性能的综合提高。Sampling analysis shows that the shock absorber has a hardness greater than 97HBS, a tensile strength of 352MPa, a yield strength of 285MPa, and an elongation of 10.6%. The life of the compression fatigue test under a load of 7.6kN is greater than 2× 10 The durability test is carried out on a special bench, and the minimum number of cycles has reached 1 million, which is much higher than the customer's requirement of 500,000 times. The product meets the DIN EN1706-1998 standard of German Volkswagen (shock absorbing bracket) and the Japanese Mazda (shock absorbing shell) MES MM 621-ADC12 standard. As shown in Figure 1b, the metallographic structure diagram of the shock absorbing bracket prepared by the process of this example, it can be seen from the figure that compared with the conventional AlSi9Cu3 die casting, the needle-shaped precipitates in the die casting prepared by this patent disappear , into granular or short flake-like rounded precipitates, which improves the dispersion of the precipitates, which is beneficial to the improvement of the strong plasticity and fatigue properties of the workpiece. Fig. 2 is the TEM structure diagram of the shock-absorbing bracket die-casting prepared by the process of this embodiment, as can be seen from the figure, there are a large amount of in-situ nano ZrB ceramic reinforcement phases in the grain and grain boundary of the die-casting prepared by this patent And the finer and uniform nano-Al 3 Er nano-precipitated phase is beneficial to the comprehensive improvement of the workpiece's strong plasticity, fatigue resistance and damping performance.
实施例2Example 2
以Al-10Zr、Al-5B、Al-10Er、Al-10Fe、Al-10Mn中间合金和纯Ni、纯Mg、纯Zn,以及AlSi9Cu3为原料,采用优化的非线性高压压铸技术制备汽车发动机用减震壳体(壳体结构复杂充型和排出气体难度高,通常降低Mg含量,提高压铸压力,提高压铸件性能和成品率)。Using Al-10Zr, Al-5B, Al-10Er, Al-10Fe, Al-10Mn master alloys and pure Ni, pure Mg, pure Zn, and AlSi9Cu3 as raw materials, the optimized non-linear high-pressure die-casting technology is used to prepare the automotive engine. Shock shell (the shell structure is complex and difficult to fill and exhaust gas, usually reduce the Mg content, increase the die-casting pressure, improve the performance and yield of die-casting parts).
将熔融的500Kg商用AlSi9Cu3合金(750℃)转入中间保温炉中,然后将Al-10Zr和Al-5B中间合金加入保温炉中并升温至840℃,同时采用石墨搅拌转子搅动熔体以促进合金的充分混合,保温时间为10min,然后将合金降温至740℃并保温;将Al-10Er、Al-10Fe和Al-10Mn以及纯Ni加入熔体中,搅拌保温10min后将粒径小于500μm的粉末状复合精炼剂用惰性气体通过石墨转子的中空通道吹入熔体中,对熔体进行精炼除气,以去除合金高温熔炼和反应过程中产生的夹渣和熔体中溶入的氢,精炼时间为25min,温度保持在740℃,精炼除气结束后降温至660℃并将纯Mg和纯Zn用钟罩压入精炼除气后的熔体中,启动石墨搅拌转子,并慢速搅拌,保温搅拌时间20min,使合金最终成分达到Si 11,Cu 3.5,Zr 5.0,B 1.0,Zn2.0,Mg 0.5,Fe 1.5,Mn 1.0,Ni 0.5,Er 0.15,余量为Al,最后将获得的复合熔体以优化的非线性高压压铸工艺制备减震壳体,其中前期为5m/s缓慢充型,以实现平流充型并利于模具型腔中气体的顺利排出,待型腔充满(冒口未充满)的瞬间,提高压射速度至50m/s,并在保持压力至150MPa,时间为15s,获得压铸减震壳体。Transfer the molten 500Kg commercial AlSi9Cu3 alloy (750°C) into the intermediate holding furnace, then add the Al-10Zr and Al-5B intermediate alloys into the holding furnace and raise the temperature to 840°C, and at the same time use graphite stirring rotor to stir the melt to promote alloying Mix well, keep warm for 10min, then cool the alloy down to 740°C and keep warm; add Al-10Er, Al-10Fe, Al-10Mn and pure Ni into the melt, stir and keep warm for 10min, then put the powder with particle size less than 500μm Shaped composite refining agent blows inert gas into the melt through the hollow channel of the graphite rotor, and refines and degasses the melt to remove the slag inclusions generated during the high-temperature melting and reaction of the alloy and the hydrogen dissolved in the melt. Refining The time is 25 minutes, the temperature is kept at 740°C, after the refining and degassing is completed, the temperature is lowered to 660°C and pure Mg and pure Zn are pressed into the melt after refining and degassing with a bell jar, and the graphite stirring rotor is started and stirred at a slow speed. Heat preservation and stirring for 20 minutes, so that the final composition of the alloy reaches Si 11, Cu 3.5, Zr 5.0, B 1.0, Zn2.0, Mg 0.5, Fe 1.5, Mn 1.0, Ni 0.5, Er 0.15, and the balance is Al. Finally, the obtained Composite melt is prepared by optimized nonlinear high-pressure die-casting process for damping shells, in which the mold is slowly filled at 5m/s in the early stage to achieve advection filling and facilitate the smooth discharge of gas in the mold cavity. After the cavity is full (riser At the moment when it is not filled), increase the injection speed to 50m/s, and keep the pressure at 150MPa for 15s to obtain a die-cast shock absorbing shell.
将切除浇冒口和飞边的压铸毛坯,放入热处理炉中进行人工时效,时效温度的250℃,时效时间为10小时。Put the die-casting blank with the sprue and flash removed into a heat treatment furnace for artificial aging. The aging temperature is 250°C and the aging time is 10 hours.
取样分析表明,减震支架的硬度大于92HBS,抗拉强度达到了315MPa,屈服强度达到了243MPa,延伸率为8.9%,在7.6kN载荷下拉压疲劳试验寿命大于1.5×106次,最终产品经专用台架进行耐久性试验,最少循环次数达到了100万次,远高于客户要求50万次。Sampling analysis shows that the hardness of the shock-absorbing bracket is greater than 92HBS , the tensile strength has reached 315MPa, the yield strength has reached 243MPa, and the elongation rate is 8.9%. The durability test is carried out on a special bench, and the minimum number of cycles has reached 1 million, which is much higher than the customer's requirement of 500,000 times.
实施例3Example 3
以Al-10Zr、Al-5B、Al-20Er、Al-20Fe、Al-5Mn中间合金和纯NIi、纯Mg、纯Zn,以及AlSi9Cu3为原料,采用优化的非线性高压压铸技术制备汽车发动机用油泵壳体。Using Al-10Zr, Al-5B, Al-20Er, Al-20Fe, Al-5Mn master alloys and pure NIi, pure Mg, pure Zn, and AlSi9Cu3 as raw materials, using optimized nonlinear high-pressure die-casting technology to prepare oil pumps for automotive engines case.
将熔融的500Kg商用AlSi9Cu3合金(780℃)转入中间保温炉中,然后将Al-10Zr和Al-5B中间合金加入保温炉中并升温至860℃,同时采用石墨搅拌转子搅动熔体以促进合金的充分混合,保温时间为15min,然后将合金降温至750℃并保温;将Al-20Er、Al-20Fe和Al-50Mn以及纯Ni加入熔体中,搅拌保温10min后将超细的粉末状精炼剂用惰性气体通过石墨转子的中空通道吹入熔体中,对熔体进行精炼除气,以去除合金高温熔炼和反应过程中产生的夹渣和熔体中溶入的氢,精炼时间为30min,温度保持在750℃,精炼除气结束后降温至680℃并将纯Mg和纯Zn用钟罩压入精炼除气后的熔体中,启动石墨搅拌转子,并慢速搅拌,保温搅拌时间20min,使合金最终成分达到Si 11,Cu 2.5,Zr 5.0,B 1.0,Zn 2.5,Mg 1.0,Fe 1.5,Mn 1.0,Ni 1.0,Er 0.1,余量为Al,最后将获得的复合熔体以优化的非线性高压压铸工艺制备油泵壳体,其中前期为4m/s缓慢充型,以实现平流充型并利于模具型腔中气体的顺利排出,待型腔充满(冒口未充满)的瞬间,提高压射速度至50m/s,并在保持压力至130MPa,时间为15s,获得压铸油泵壳体。Transfer the molten 500Kg commercial AlSi9Cu3 alloy (780°C) into the intermediate holding furnace, then add the Al-10Zr and Al-5B intermediate alloys into the holding furnace and raise the temperature to 860°C, and at the same time use graphite stirring rotor to agitate the melt to promote alloying Fully mixed, the holding time is 15min, then the alloy is cooled to 750°C and kept warm; Al-20Er, Al-20Fe and Al-50Mn and pure Ni are added to the melt, stirred and kept warm for 10min, and the ultrafine powder is refined The inert gas used as agent is blown into the melt through the hollow channel of the graphite rotor, and the melt is refined and degassed to remove the slag inclusions generated during the high-temperature melting and reaction of the alloy and the hydrogen dissolved in the melt. The refining time is 30 minutes , the temperature is kept at 750°C, and after refining and degassing, the temperature is lowered to 680°C and pure Mg and pure Zn are pressed into the melt after refining and degassing with a bell jar, and the graphite stirring rotor is started and stirred at a slow speed. 20min, make the final composition of the alloy reach Si 11, Cu 2.5, Zr 5.0, B 1.0, Zn 2.5, Mg 1.0, Fe 1.5, Mn 1.0, Ni 1.0, Er 0.1, the balance is Al, and finally the composite melt obtained is The oil pump casing is prepared by the optimized nonlinear high-pressure die-casting process, in which the mold is slowly filled at 4m/s in the early stage to achieve advection filling and facilitate the smooth discharge of gas in the mold cavity. , increase the injection speed to 50m/s, and keep the pressure at 130MPa for 15s to obtain a die-cast oil pump casing.
将切除浇冒口和飞边的压铸毛坯,放入热处理炉中进行人工时效,时效温度的220℃,时效时间为15小时。Put the die-casting blank with the sprue and flash removed into a heat treatment furnace for artificial aging. The aging temperature is 220°C and the aging time is 15 hours.
取样分析表明,减震支架的硬度大于93HBS,抗拉强度达到了330MPa,屈服强度达到了250MPa,延伸率为7.8%,在7.6kN载荷下拉压疲劳试验寿命大于1.2×106次,最终产品经专用台架进行耐久性试验,最少循环次数达到了100万次,远高于客户要求50万次。Sampling analysis shows that the shock absorber has a hardness greater than 93HBS, a tensile strength of 330MPa, a yield strength of 250MPa, and an elongation of 7.8%. The compression fatigue test life under a load of 7.6kN is greater than 1.2×106 times. The durability test is carried out on a special bench, and the minimum number of cycles has reached 1 million, which is much higher than the customer's requirement of 500,000 times.
对比实施方式Comparative implementation
对比实施例1Comparative Example 1
以AlSi9Cu3合金为原料,采用优化的非线性高压压铸技术制备汽车发动机用减震支架。Using AlSi9Cu3 alloy as raw material, the shock absorber bracket for automobile engine was prepared by optimized nonlinear high-pressure die-casting technology.
将熔融的500Kg商用AlSi9Cu3合金(700℃)采用优化的非线性高压压铸技术制备汽车发动机用减震支架,并对切除浇冒口和飞边的压铸毛坯进行人工时效,时效温度的300℃,时效时间为8小时。The melted 500Kg commercial AlSi9Cu3 alloy (700°C) was prepared by optimized nonlinear high-pressure die-casting technology to prepare shock absorbers for automobile engines, and artificially aged the die-casting blanks with the sprue and flash removed. The aging temperature was 300°C. The time is 8 hours.
取样分析表明,减震支架的硬度大于82HBS,抗拉强度达到了285MPa,屈服强度达到了193MPa,延伸率为6.4%,在7.6kN载荷下拉压疲劳试验寿命大于1×106次。Sampling analysis shows that the shock absorber has a hardness greater than 82HBS, a tensile strength of 285MPa, a yield strength of 193MPa, an elongation of 6.4%, and a compression fatigue test life of more than 1×10 6 times under a load of 7.6kN.
对比实施例2Comparative Example 2
以Al-10Zr、Al-10B、Al-20Er、Al-20Fe、Al-10Mn中间合金和纯Ni、纯Mg、纯Zn,以及AlSi9Cu3为原料,采用常规压铸技术制备汽车发动机用减震支架。Using Al-10Zr, Al-10B, Al-20Er, Al-20Fe, Al-10Mn master alloys, pure Ni, pure Mg, pure Zn, and AlSi9Cu3 as raw materials, conventional die-casting technology is used to prepare shock absorbers for automobile engines.
原位合成纳米ZrB2增强体及合金成分调控与实施例1相同,将获得温度为680℃,成分为Si 9.5,Cu 3,Zr 3.5,B 0.75,Zn 1.5,Mg 0.8,Fe 1.3,Mn 1.0,Ni 0.7,Er 0.12,余量为Al的合金熔体,采用常规压铸工艺获得压铸减震支架。The in-situ synthesis of nano-ZrB 2 reinforcement and the control of alloy composition are the same as in Example 1. The obtained temperature is 680°C, and the composition is Si 9.5, Cu 3, Zr 3.5, B 0.75, Zn 1.5, Mg 0.8, Fe 1.3, Mn 1.0 , Ni 0.7, Er 0.12, and the alloy melt with the balance of Al, the die-casting shock absorber was obtained by conventional die-casting process.
采用实施例1相同的时效工艺对压铸件进行时效处理。The die casting was subjected to aging treatment using the same aging process as in Example 1.
取样分析表明,减震支架的硬度大于93HBS,抗拉强度达到了335MPa,屈服强度达到了263MPa,延伸率为9.2%,在7.6kN载荷下拉压疲劳试验寿命大于1.8×106次。Sampling analysis shows that the shock absorber has a hardness greater than 93HBS, a tensile strength of 335MPa, a yield strength of 263MPa, an elongation of 9.2%, and a compressive fatigue life of more than 1.8×10 6 times under a load of 7.6kN.
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108342606A (en) * | 2018-01-19 | 2018-07-31 | 江苏大学 | A kind of method that mischmetal improves in-situ Al-base composition tissue and performance |
CN108672702A (en) * | 2018-05-21 | 2018-10-19 | 宁波市奇强精密冲件有限公司 | Damper knuckle support |
WO2018214631A1 (en) * | 2017-05-25 | 2018-11-29 | 江苏大学 | High-strength anti-fatigue in-situ nano strengthening aluminium alloy for vibration-damping part of automobile engine, and high-density die-casting method therefor |
CN111074113A (en) * | 2020-01-02 | 2020-04-28 | 苏州先准电子科技有限公司 | Production process for in-situ generation of zirconium boride particle reinforced aluminum-silicon-based composite material |
CN111647785A (en) * | 2020-06-17 | 2020-09-11 | 帅翼驰新材料集团有限公司 | High-strength die-casting aluminum alloy and preparation method thereof |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114438376A (en) * | 2022-02-17 | 2022-05-06 | 江西理工大学 | A kind of aluminum-cerium-erbium heat-resistant cast aluminum alloy and preparation method thereof |
CN114959372B (en) * | 2022-03-08 | 2023-06-27 | 山东金马汽车装备科技有限公司 | Aluminum-based composite hub and manufacturing method thereof |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104451236A (en) * | 2014-11-07 | 2015-03-25 | 江苏大学 | A kind of in-situ preparation method of nano ZrB2 particle reinforced aluminum matrix composite |
CN104874772A (en) * | 2015-05-20 | 2015-09-02 | 柳州市百田机械有限公司 | Preparation method of highly dense pressure casting aluminum alloy |
CN105256185A (en) * | 2015-11-11 | 2016-01-20 | 天津爱田汽车部件有限公司 | Cast aluminum alloy high in thermal conductivity |
CN105861887A (en) * | 2016-04-01 | 2016-08-17 | 江苏大学 | Anti-fatigue in-situ aluminum-based composite for heavy-load hubs and preparation method thereof |
CN106282685A (en) * | 2016-08-31 | 2017-01-04 | 中车戚墅堰机车车辆工艺研究所有限公司 | A kind of high strength cast aluminum alloys and preparation method thereof |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2001252754A (en) * | 2000-03-09 | 2001-09-18 | Hitachi Metals Ltd | Aluminum wheel and its manufacturing method |
CN107267817B (en) * | 2017-05-25 | 2019-04-19 | 江苏大学 | A kind of high-strength anti-fatigue in-situ nano-strengthened aluminum alloy and its die-casting method |
-
2017
- 2017-05-25 CN CN201710376448.7A patent/CN107267817B/en active Active
-
2018
- 2018-03-23 CH CH00580/19A patent/CH714442B1/en unknown
- 2018-03-23 WO PCT/CN2018/080114 patent/WO2018214631A1/en active Application Filing
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104451236A (en) * | 2014-11-07 | 2015-03-25 | 江苏大学 | A kind of in-situ preparation method of nano ZrB2 particle reinforced aluminum matrix composite |
CN104874772A (en) * | 2015-05-20 | 2015-09-02 | 柳州市百田机械有限公司 | Preparation method of highly dense pressure casting aluminum alloy |
CN105256185A (en) * | 2015-11-11 | 2016-01-20 | 天津爱田汽车部件有限公司 | Cast aluminum alloy high in thermal conductivity |
CN105861887A (en) * | 2016-04-01 | 2016-08-17 | 江苏大学 | Anti-fatigue in-situ aluminum-based composite for heavy-load hubs and preparation method thereof |
CN106282685A (en) * | 2016-08-31 | 2017-01-04 | 中车戚墅堰机车车辆工艺研究所有限公司 | A kind of high strength cast aluminum alloys and preparation method thereof |
Non-Patent Citations (3)
Title |
---|
侯雅尘 等: ""Er、Zr、B对耐热导电铝合金组织和性能的影响"", 《特种铸造及有色合金》 * |
王鹏驹,殷国富 主编: "《压铸模具设计师手册》", 31 January 2008, 机械工业出版社 * |
胡济川: ""离合器壳体压铸工艺优化——瑞士布勒H-1100B压铸机调试与应用"", 《特种铸造及有色合金》 * |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2018214631A1 (en) * | 2017-05-25 | 2018-11-29 | 江苏大学 | High-strength anti-fatigue in-situ nano strengthening aluminium alloy for vibration-damping part of automobile engine, and high-density die-casting method therefor |
CN108342606A (en) * | 2018-01-19 | 2018-07-31 | 江苏大学 | A kind of method that mischmetal improves in-situ Al-base composition tissue and performance |
CN108672702A (en) * | 2018-05-21 | 2018-10-19 | 宁波市奇强精密冲件有限公司 | Damper knuckle support |
CN111074113A (en) * | 2020-01-02 | 2020-04-28 | 苏州先准电子科技有限公司 | Production process for in-situ generation of zirconium boride particle reinforced aluminum-silicon-based composite material |
CN111074113B (en) * | 2020-01-02 | 2021-12-24 | 苏州先准电子科技有限公司 | Production process for in-situ generation of zirconium boride particle reinforced aluminum-silicon-based composite material |
CN111647785A (en) * | 2020-06-17 | 2020-09-11 | 帅翼驰新材料集团有限公司 | High-strength die-casting aluminum alloy and preparation method thereof |
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