CN102747256A - Aluminum-silicon based aluminum section and preparation technology thereof - Google Patents
Aluminum-silicon based aluminum section and preparation technology thereof Download PDFInfo
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Abstract
本发明公开了一种铝硅基铝型材,按照重量百分数,该铝型材由以下组分组成:硅:5.0%—14.0%,镁:0.2%—0.7%,硼:<0.03%,锶:<0.06%,增强元素:0.1%-6.55%,杂质元素:<0.25%,铝:余量。该铝硅基铝型材具有强度高、硬度高、耐磨性能好的优点。本发明还公开了铝硅基铝型材的制备工艺:第一步:将铝硅合金置入石墨坩埚中,加热形成熔体;第二步:加入镁元素、硅元素和增强元素;第三步:加入六氯乙烷精炼;第四步:加入锶元素变质,浇铸到铸铁模具中,形成铸锭;第五步:将铸锭进行退火后,依次进行热挤压、热轧变形、固溶处理和时效处理,从而制得铝硅基铝型材。该制备工艺简单。
The invention discloses an aluminum-silicon-based aluminum profile. According to the weight percentage, the aluminum profile is composed of the following components: silicon: 5.0%-14.0%, magnesium: 0.2%-0.7%, boron: <0.03%, strontium: < 0.06%, reinforcing element: 0.1%-6.55%, impurity element: <0.25%, aluminum: balance. The aluminum-silicon-based aluminum profile has the advantages of high strength, high hardness and good wear resistance. The invention also discloses the preparation process of aluminum-silicon-based aluminum profiles: the first step: put the aluminum-silicon alloy into a graphite crucible, and heat it to form a melt; the second step: add magnesium, silicon and reinforcing elements; the third step : Refining by adding hexachloroethane; Step 4: Add strontium element to modify, cast into cast iron mold to form ingot; Step 5: After annealing the ingot, perform hot extrusion, hot rolling deformation, solid solution in sequence treatment and aging treatment to produce aluminum-silicon-based aluminum profiles. The preparation process is simple.
Description
技术领域 technical field
本发明涉及一种铝型材及其制备工艺,具体来说,涉及一种铝硅基铝型材及其制备工艺。The invention relates to an aluminum profile and a preparation process thereof, in particular to an aluminum-silicon-based aluminum profile and a preparation process thereof.
背景技术 Background technique
铝型材分为建筑铝型材(建筑门窗、幕墙、室内外装饰及建筑结构用铝型材,占铝型材消费量的75%)和工业用铝型材(建筑铝型材外所有铝型材)。我国是铝型材生产大国,建筑铝型材占整个铝型材市场的绝大部分,但提供的往往是低端产品,主要用作建筑门窗、室内外装饰及要求不高的幕墙结构。而对性能要求较高的幕墙结构,其铝型材不得不采用价格昂贵的进口产品。这主要是因为我国建筑铝型材采用6000系列Al-Si-Mg合金制造。该合金含有重量分数大约各为0.5%的Mg和Si,其余为Al,属于单相合金。由于所含强化元素的量少,强度低,特别是刚度小,耐磨性差,易变形,但具有非常优异的延展性,可方便地采用挤压成形(GB 5237.1-2004标准:6063合金T6状态下σb≥205MPa,σ0.2≥180MPa,δ≥8.0%)。Aluminum profiles are divided into architectural aluminum profiles (aluminum profiles for building doors and windows, curtain walls, interior and exterior decoration and building structures, accounting for 75% of aluminum profile consumption) and industrial aluminum profiles (all aluminum profiles except architectural aluminum profiles). my country is a big producer of aluminum profiles, and architectural aluminum profiles account for the vast majority of the entire aluminum profile market, but they often provide low-end products, mainly used for building doors and windows, indoor and outdoor decoration, and curtain wall structures with low requirements. For the curtain wall structure with high performance requirements, the aluminum profiles have to use expensive imported products. This is mainly because my country's architectural aluminum profiles are made of 6000 series Al-Si-Mg alloys. The alloy contains about 0.5% by weight of Mg and Si each, and the rest is Al, belonging to a single-phase alloy. Due to the small amount of strengthening elements contained, the strength is low, especially the stiffness is small, the wear resistance is poor, and it is easy to deform, but it has very excellent ductility and can be easily formed by extrusion (GB 5237.1-2004 standard: 6063 alloy T6 state Lower σ b ≥205MPa, σ 0.2 ≥180MPa, δ≥8.0%).
发明内容 Contents of the invention
技术问题:本发明所要解决的技术问题是:提供一种铝硅基铝型材,该铝型材具有强度高、硬度高、耐磨性能好、成本低廉的优点,同时还提供了一种铝硅基铝型材的制备工艺,该制备工艺简单。Technical problem: The technical problem to be solved by the present invention is to provide an aluminum-silicon-based aluminum profile, which has the advantages of high strength, high hardness, good wear resistance and low cost, and also provides an aluminum-silicon-based The preparation process of the aluminum profile is simple.
技术方案:为解决上述技术问题,本发明采用的技术方案是:Technical scheme: in order to solve the above technical problems, the technical scheme adopted in the present invention is:
一种铝硅基铝型材,按照重量百分数,该铝型材由以下组分组成:An aluminum-silicon-based aluminum profile, which consists of the following components in terms of weight percentage:
硅:5.0%-14.0%,Silicon: 5.0%-14.0%,
镁:0.2%-0.7%,Magnesium: 0.2%-0.7%,
硼:<0.03%,Boron: <0.03%,
锶:<0.06%,Strontium: <0.06%,
增强元素:0.1%-6.55%,Enhancement elements: 0.1%-6.55%,
杂质元素:<0.25%,Impurity elements: <0.25%,
铝:余量;Aluminum: balance;
所述的杂质元素是指铁、锡、铅、钙中的任何一种或组合,所述的增强元素是指钛、锰、硼中的任何一种或组合。The impurity element refers to any one or combination of iron, tin, lead and calcium, and the reinforcing element refers to any one or combination of titanium, manganese and boron.
一种铝硅基铝型材的制备工艺,该制备工艺包括以下步骤:A preparation process for an aluminum-silicon-based aluminum profile, the preparation process comprising the following steps:
第一步:将铝硅合金置入石墨坩埚中,采用电阻丝加热至760℃熔清后,保温30分钟,形成熔体;Step 1: Put the aluminum-silicon alloy into a graphite crucible, heat it to 760°C with a resistance wire to melt it, and keep it warm for 30 minutes to form a melt;
第二步:向第一步制得的熔体中加入镁元素、硅元素和增强元素,使得硅元素的重量百分比在5.0%—14.0%之间,镁元素的重量百分比在0.2%—0.7%之间,增强元素的重量百分比在0.1%—6.55%之间,保温30分钟后,再降温到730℃,形成熔体;The second step: adding magnesium element, silicon element and reinforcing element to the melt prepared in the first step, so that the weight percentage of silicon element is between 5.0% and 14.0%, and the weight percentage of magnesium element is between 0.2% and 0.7%. Between, the weight percentage of reinforcing elements is between 0.1% and 6.55%, after 30 minutes of heat preservation, then cool down to 730°C to form a melt;
第三步:向第二步制得的熔体中加入六氯乙烷精炼,静置10分钟后,形成熔体;The third step: adding hexachloroethane to the melt obtained in the second step for refining, and leaving it to stand for 10 minutes to form a melt;
第四步:向第三步制得的熔体中加入锶元素变质,锶元素的重量百分数在0.03%—0.06%之间,保温30分钟后,形成熔体,保温5分钟后,将该熔体浇铸到预热到200摄氏度的铸铁模具中,自然冷却后形成铸锭;The fourth step: Add strontium element to the melt obtained in the third step to modify the quality. The weight percentage of strontium element is between 0.03% and 0.06%. After 30 minutes of heat preservation, a melt is formed. After 5 minutes of heat preservation, the melt Cast the body into a cast iron mold preheated to 200 degrees Celsius, and form an ingot after natural cooling;
第五步:将第四步制得的铸锭进行均匀化退火后,在400℃—550℃温度下进行热挤压和热轧变形,随后在500℃—550℃温度之间进行固溶处理,固溶处理时间为3—6小时,接着在150℃—250℃温度之间进行时效处理,时效处理时间为3—20小时,从而制得铝硅基铝型材。Step 5: After homogenizing and annealing the ingot obtained in Step 4, perform hot extrusion and hot rolling deformation at a temperature of 400°C-550°C, and then perform solution treatment at a temperature of 500°C-550°C , the solution treatment time is 3-6 hours, followed by aging treatment at a temperature of 150°C-250°C, and the aging treatment time is 3-20 hours, so as to obtain aluminum-silicon-based aluminum profiles.
有益效果:与现有技术相比,本发明具有以下有益效果:Beneficial effects: compared with the prior art, the present invention has the following beneficial effects:
1.本发明的铝硅基铝型材具有强度高、硬度高、耐磨性能好的技术优点。本发明的合金通过在熔炼时添加Sr或Sr+B细化组织中的共晶Si和枝晶团,改善了硅颗粒的形貌。在热变形过程中改善硅颗粒分布,使组织均匀。Mg的加入使得合金可是通过固溶时效进行强化。制备的型材在T6热处理态下强度、硬度和耐磨性远高于6000系型材,延伸率略低,但均高于国家标准。1. The aluminum-silicon-based aluminum profile of the invention has the technical advantages of high strength, high hardness and good wear resistance. The alloy of the invention improves the morphology of silicon particles by adding Sr or Sr+B to refine the eutectic Si and dendrites in the structure during smelting. Improve the distribution of silicon particles during thermal deformation to make the structure uniform. The addition of Mg allows the alloy to be strengthened by solution aging. The strength, hardness and wear resistance of the prepared profiles in the T6 heat treatment state are much higher than those of the 6000 series profiles, and the elongation is slightly lower, but they are all higher than the national standard.
2.低成本。本发明的合金系列用硅代替铝,可以降低电解铝的消耗量。如含硅量12.3%左右的近共晶铝硅镁合金,可以降低12%左右的电解铝用量,降低电能消耗,节能环保。2. low cost. The alloy series of the invention uses silicon instead of aluminum, which can reduce the consumption of electrolytic aluminum. For example, the near-eutectic aluminum-silicon-magnesium alloy with a silicon content of about 12.3% can reduce the amount of electrolytic aluminum by about 12%, reduce power consumption, and save energy and protect the environment.
3.热变形的流变应力低。本发明的合金系列热变形过程中流变抗力与通常铝型材的相当,可方便地进行热变形制备铝型材。3. Low flow stress for thermal deformation. The rheological resistance of the alloy series in the invention is equivalent to that of common aluminum profiles during thermal deformation, and the aluminum profiles can be prepared through thermal deformation conveniently.
附图说明 Description of drawings
图1本发明中实施例1的Al-12.3Si-0.4Mg合金在铸态下的组织结构图。Fig. 1 is the structural diagram of the Al-12.3Si-0.4Mg alloy of Example 1 in the cast state in the present invention.
图2本发明中实施例1的Al-12.3Si-0.4Mg合金在热挤压后的组织结构图。Fig. 2 is the microstructure diagram of the Al-12.3Si-0.4Mg alloy of Example 1 in the present invention after hot extrusion.
具体实施方式 Detailed ways
本发明的一种铝硅基铝型材,按照重量百分数,该铝型材由以下组分组成:An aluminum-silicon-based aluminum profile according to the present invention is composed of the following components according to the weight percentage:
硅:5.0%—14.0%,Silicon: 5.0%—14.0%,
镁:0.2%—0.7%,Magnesium: 0.2%—0.7%,
硼:<0.03%,Boron: <0.03%,
锶:<0.06%,Strontium: <0.06%,
增强元素:0.1%-6.55%,Enhancement elements: 0.1%-6.55%,
杂质元素:<0.25%,Impurity elements: <0.25%,
铝:余量。Aluminum: Balance.
杂质元素是指铁、锡、铅、钙中的任何一种或组合。例如,杂质元素可以是铁和锡两种元素组成;杂质元素可以是铁、铅和钙三种元素的组合。作为一种优选方案,杂质元素由铁、锡、铅和钙四种元素组成,且杂质元素在铝硅基铝型材中的重量百分数优选:铁<0.2%、锡<0.01%、铅<0.01%、钙<0.03%。增强元素是指钛、锰、硼中的任何一种或组合。例如,增强元素可以是钛和锰两种元素的组合;增强元素可以是硼元素。作为一种优选方案,增强元素由钛、锰和硼三种元素组成,且增强元素在铝硅基铝型材中的重量百分数优选:铜:2.5%-5.0%,钛:Ti0.1%-0.35%,锰:0.3%-1.2%。Impurity elements refer to any one or combination of iron, tin, lead, and calcium. For example, the impurity element may be composed of two elements of iron and tin; the impurity element may be a combination of three elements of iron, lead and calcium. As a preferred solution, the impurity elements are composed of four elements: iron, tin, lead and calcium, and the weight percentage of the impurity elements in the aluminum-silicon-based aluminum profile is preferably: iron<0.2%, tin<0.01%, lead<0.01% , Calcium <0.03%. The reinforcing element refers to any one or combination of titanium, manganese and boron. For example, the reinforcing element may be a combination of titanium and manganese; the reinforcing element may be boron. As a preferred solution, the reinforcing element is composed of titanium, manganese and boron, and the weight percentage of the reinforcing element in the aluminum-silicon-based aluminum profile is preferably: copper: 2.5%-5.0%, titanium: Ti0.1%-0.35 %, Manganese: 0.3%-1.2%.
含硅量在重量百分比为5.0%到14.0%的铝硅基铝合金由于优异的铸造性能多用于铸造成型,在该铸造铝硅基合金的中加入少量Mg可大大提高其强度性能。该成分范围铸造铝硅基合金采用热变形,包括但不限于挤压、轧制、锻造和拉拔,其强度、硬度与耐磨性远高于6000系列的Al-SiMg合金型材,弹性模量略有提高,伸长率则相当。但该合金系列用硅代替铝,可以降低电解铝的消耗量,如含硅量12.3%左右的近共晶铝硅镁合金,可以降低12%左右的电解铝用量,降低电能的消耗,节能环保。The aluminum-silicon-based aluminum alloy with a silicon content of 5.0% to 14.0% by weight is mostly used for casting molding due to its excellent casting properties. Adding a small amount of Mg to the cast aluminum-silicon-based alloy can greatly improve its strength performance. Cast aluminum-silicon-based alloys in this composition range adopt hot deformation, including but not limited to extrusion, rolling, forging and drawing, and their strength, hardness and wear resistance are much higher than those of 6000 series Al-SiMg alloy profiles, and their elastic modulus Slightly improved, the elongation is the same. However, this alloy series uses silicon instead of aluminum, which can reduce the consumption of electrolytic aluminum. For example, the near-eutectic aluminum-silicon-magnesium alloy with a silicon content of about 12.3% can reduce the consumption of electrolytic aluminum by about 12%, reduce power consumption, and save energy and protect the environment. .
上述铝硅基铝型材的制备工艺,包括以下步骤:The preparation process of the above-mentioned aluminum-silicon-based aluminum profile comprises the following steps:
第一步:将铝硅合金置入石墨坩埚中,采用电阻丝加热至760℃熔清后,保温30分钟,形成熔体。Step 1: Put the aluminum-silicon alloy into a graphite crucible, heat it to 760°C with a resistance wire to melt it, and keep it warm for 30 minutes to form a melt.
第二步:向第一步制得的熔体中加入镁元素、硅元素和增强元素,使得硅元素的重量百分比在5.0%—14.0%之间,镁元素的重量百分比在0.2%—0.7%之间,增强元素的重量百分比在0.1%—6.55%之间,保温30分钟后,再降温到730℃,形成熔体。The second step: adding magnesium element, silicon element and reinforcing element to the melt prepared in the first step, so that the weight percentage of silicon element is between 5.0% and 14.0%, and the weight percentage of magnesium element is between 0.2% and 0.7%. Among them, the weight percentage of reinforcing elements is between 0.1% and 6.55%. After 30 minutes of heat preservation, the temperature is lowered to 730°C to form a melt.
第三步:向第二步制得的熔体中加入六氯乙烷精炼,静置10分钟后,形成熔体。The third step: adding hexachloroethane to the melt obtained in the second step for refining, and standing for 10 minutes to form a melt.
第四步:向第三步制得的熔体中加入锶元素变质,锶元素的重量百分数在0.03%—0.06%之间,保温30分钟后,形成熔体;保温5分钟后,将该熔体浇铸到预热到200摄氏度的铸铁模具中,自然冷却后形成铸锭;The fourth step: add strontium element to the melt obtained in the third step to modify the quality, the weight percentage of the strontium element is between 0.03% and 0.06%, after 30 minutes of heat preservation, a melt is formed; after 5 minutes of heat preservation, the melt Cast the body into a cast iron mold preheated to 200 degrees Celsius, and form an ingot after natural cooling;
在第四步中,向熔体中加入Al 3B,其中,硼元素的占整个熔体的重量百分比小于0.03%,保温5分钟,然后再制备铸锭。In the fourth step, Al 3 B is added to the melt, wherein the boron element accounts for less than 0.03% by weight of the entire melt, and the temperature is kept for 5 minutes, and then an ingot is prepared.
第五步:将第四步制得的铸锭进行均匀化退火后,在400℃—550℃温度下进行热挤压和热轧变形,随后在500℃—550℃温度之间进行固溶处理,固溶处理时间为3—6小时,接着在150℃—250℃温度之间进行时效处理,时效处理时间为3—20小时,从而制得铝硅基铝型材。Step 5: After homogenizing and annealing the ingot obtained in Step 4, perform hot extrusion and hot rolling deformation at a temperature of 400°C-550°C, and then perform solution treatment at a temperature of 500°C-550°C , the solution treatment time is 3-6 hours, followed by aging treatment at a temperature of 150°C-250°C, and the aging treatment time is 3-20 hours, so as to obtain aluminum-silicon-based aluminum profiles.
在第五步中,铸锭进行均匀化退火后,在400℃—550℃温度下进行热挤压和热轧变形后,获得的型材进行淬火后为挤压态型材。固溶处理和时效处理为金属材料领域的T6处理。经过固溶处理和时效处理的型材为T6处理态型材。In the fifth step, after the ingot is homogenized and annealed, hot extrusion and hot rolling are carried out at a temperature of 400° C. to 550° C., and the obtained profile is quenched into an extruded profile. Solution treatment and aging treatment are T6 treatments in the field of metal materials. The profiles after solution treatment and aging treatment are T6 treated profiles.
下面给出利用本发明的制备工艺制备铝硅基铝型材的两个实施例。Two examples of preparing aluminum-silicon-based aluminum profiles using the preparation process of the present invention are given below.
实施例1Example 1
原料为ZL102(ZL102表示铸铝102,含硅量为10.0%-13.0%,余量为铝)。将ZL102加入石墨坩埚中,采用电阻丝加热至760℃熔清后,保温30分钟;然后向ZL102中加入0.4wt%的纯镁,保温30分钟后再降温到730℃,加六氯乙烷精炼,静置10分钟后加锶Sr元素,保温30分钟后,形成熔体;保温5分钟后,将得到的熔体浇铸到预热到200摄氏度的铸铁模具中,自然冷却形成铸锭,铸锭进行均匀化退火后,在400℃—550℃温度下进行热挤压和热轧变形,随后在500℃—550℃温度之间进行固溶处理,固溶处理时间为3—6小时,接着在150℃—250℃温度之间进行时效处理,时效处理时间为3—20小时,从而制得铝硅基铝型材。The raw material is ZL102 (ZL102 means cast aluminum 102, the silicon content is 10.0%-13.0%, and the balance is aluminum). Add ZL102 into the graphite crucible, heat it to 760°C with resistance wire, keep it warm for 30 minutes; then add 0.4wt% pure magnesium to ZL102, keep it warm for 30 minutes, then cool down to 730°C, add hexachloroethane to refine , after standing for 10 minutes, add strontium Sr element, after 30 minutes of heat preservation, a melt is formed; after 5 minutes of heat preservation, the obtained melt is cast into a cast iron mold preheated to 200 degrees Celsius, and naturally cooled to form an ingot. After homogenization annealing, hot extrusion and hot rolling deformation are carried out at a temperature of 400°C-550°C, and then solution treatment is carried out at a temperature of 500°C-550°C, and the solution treatment time is 3-6 hours. Aging treatment is carried out at a temperature between 150°C and 250°C, and the aging treatment time is 3-20 hours, so as to obtain aluminum-silicon-based aluminum profiles.
铝硅基铝型材的化学成分用ICP直读光谱仪测定,结果如下:Si:12.3%、Mg:0.411%、Fe:0.151%、Sr:0.020%、Pb:<0.0005、Sn:<0.001、Ca:0.00080、余量为Al。利用金相显微镜对实施例1的Al-12.3Si-0.4Mg合金在铸态下和热挤压后的组织结构进行拍照,结果如图1和图2所示。从两幅图中可以看出:热挤压过程使得硅颗粒沿流线分布,分散更加均匀,挤压过程中硅颗粒发生了球化、长大,降低了其对机体的割裂作用,有利于提高材料的强度,改善材料的塑性。The chemical composition of the aluminum-silicon-based aluminum profile was measured with an ICP direct-reading spectrometer, and the results are as follows: Si: 12.3%, Mg: 0.411%, Fe: 0.151%, Sr: 0.020%, Pb: <0.0005, Sn: <0.001, Ca: 0.00080, the balance is Al. The microstructure of the Al-12.3Si-0.4Mg alloy in Example 1 in the as-cast state and after hot extrusion was photographed with a metallographic microscope, and the results are shown in Fig. 1 and Fig. 2 . It can be seen from the two figures that the hot extrusion process makes the silicon particles distribute along the streamline, and the dispersion is more uniform. Improve the strength of the material and improve the plasticity of the material.
将淬火后的挤压态样品和T6处理态样品用线切割加工成板状拉伸样,每个状态取三个平行样。按照国家标准《GBT228-2002金属材料室温拉伸试验方法》,在WJ-10型机械式万能实验机上,对挤压态样品和T6处理态样品进行屈服强度、抗拉强度和延伸率的测试。测试结果如表1所示。The extruded sample after quenching and the T6 treated sample were processed into a plate-shaped tensile sample by wire cutting, and three parallel samples were taken for each state. According to the national standard "GBT228-2002 Metal Materials Tensile Test Method at Room Temperature", on the WJ-10 mechanical universal testing machine, the yield strength, tensile strength and elongation of the extruded sample and the T6 treated sample were tested. The test results are shown in Table 1.
另外,对实施例1的Al-12.3Si-0.4Mg合金在Gleeble3500在热模拟机上,进行热压缩模拟实验,获得的不同温度、不同应变速率下的稳态流变应力(MPa)。热压缩模拟实验的过程是:将材料加工成热压缩模拟所需的的圆柱体,在535℃下进行均匀化退火6小时后水淬;在Gleeble3500热模拟机将试样以5℃/s的升温速度加热到相应温度,保温1分钟,以相应的真应变速率进行热压缩模拟,至真应变为1。记录下热压缩过程的真应力-真应变曲线,取各变现条件下的稳态流变应力得到表2。结果如表2所示。表2中的第一列表示温度,表2的第一行表示应变速率。从表2可以看出:该合金在400℃到500℃之间具有较小的流变抗力,具有很好的挤压性能。In addition, the Al-12.3Si-0.4Mg alloy of Example 1 was subjected to thermal compression simulation experiments on a Gleeble 3500 thermal simulator to obtain the steady-state flow stress (MPa) at different temperatures and different strain rates. The process of the thermal compression simulation experiment is: processing the material into the required thermal compression simulation The cylinder was subjected to homogenization annealing at 535°C for 6 hours and then water quenched; in the Gleeble3500 thermal simulator, the sample was heated to the corresponding temperature at a heating rate of 5°C/s, kept for 1 minute, and carried out at the corresponding true strain rate Thermal compression simulation, until the true strain is 1. Record the true stress-true strain curve of the thermal compression process, and take the steady-state flow stress under each realization condition to obtain Table 2. The results are shown in Table 2. The first column in Table 2 indicates temperature, and the first row of Table 2 indicates strain rate. It can be seen from Table 2 that the alloy has a small rheological resistance between 400°C and 500°C and has good extrusion performance.
表1Table 1
表2Table 2
实施例2Example 2
制备过程与实施例1相同,不同之处:一方面是实施例2采用的原料是ZL101(ZL101表示铸铝101,含硅量为6.5%-7.5%,含镁0.25%-0.45%,余量为铝),另一方面:向ZL101中加入0.2wt%的纯镁补镁的烧损,而不是实施例1中的0.4wt%的纯镁。The preparation process is the same as that of Example 1, the difference: on the one hand, the raw material used in Example 2 is ZL101 (ZL101 means cast aluminum 101, containing 6.5%-7.5% silicon, 0.25%-0.45% magnesium, and the balance Aluminum), on the other hand: add 0.2wt% pure magnesium to ZL101 to supplement the burning loss of magnesium, instead of 0.4wt% pure magnesium in Example 1.
铝硅基铝型材的化学成分用ICP直读光谱仪测定,结果如下:Si:6.99%、Mg:0.560%、Fe:0.124%、Sr:0.011%、Ti:0.131%、Pb:<0.0005、Sn:<0.001、Ca:0.00070,余量为Al。将淬火后的挤压态样品和T6处理态样品用线切割加工成板状拉伸样,每个状态取三个平行样。按照国家标准《GBT228-2002金属材料室温拉伸试验方法》,在WJ-10型机械式万能实验机上,对挤压态样品和T6处理态样品进行屈服强度、抗拉强度和延伸率的测试。测试结果如表3所示。The chemical composition of the aluminum-silicon-based aluminum profile was measured with an ICP direct-reading spectrometer, and the results are as follows: Si: 6.99%, Mg: 0.560%, Fe: 0.124%, Sr: 0.011%, Ti: 0.131%, Pb: <0.0005, Sn: <0.001, Ca:0.00070, the balance is Al. The extruded sample after quenching and the T6 treated sample were processed into a plate-shaped tensile sample by wire cutting, and three parallel samples were taken for each state. According to the national standard "GBT228-2002 Metal Materials Tensile Test Method at Room Temperature", on the WJ-10 mechanical universal testing machine, the yield strength, tensile strength and elongation of the extruded sample and the T6 treated sample were tested. The test results are shown in Table 3.
表3table 3
从上述两个实施例的力学性能测试结果可以看出:该系列合金可以方便地采用挤压成型,合金在T6状态下的力学性能远超过了6063合金相同状态下力学性能标准的要求。From the mechanical performance test results of the above two examples, it can be seen that this series of alloys can be conveniently formed by extrusion, and the mechanical properties of the alloy in the T6 state far exceed the requirements of the mechanical performance standard of the 6063 alloy in the same state.
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Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1936051A (en) * | 2006-10-17 | 2007-03-28 | 山东大学 | Aluminium-silicon-copper-magnesium series deforming alloy and its preparing method |
| CN101144134A (en) * | 2007-10-15 | 2008-03-19 | 李贞宽 | Aluminum-silicon series deforming alloy and manufacturing method thereof |
| CN101158001A (en) * | 2007-11-23 | 2008-04-09 | 苏州有色金属研究院有限公司 | Vacuum Stirring Composite Particle Reinforced Aluminum Matrix Composite Material and Its Preparation Technology |
| CN101333614A (en) * | 2007-06-29 | 2008-12-31 | 东北大学 | Structural material piece of magnesium-containing high-silicon aluminum alloy and preparation method thereof |
| CN102397905A (en) * | 2011-11-25 | 2012-04-04 | 沈阳工业大学 | Hot extrusion forming method for hypereutectic Al-Si alloy |
| CN102418013A (en) * | 2011-12-08 | 2012-04-18 | 东北大学 | Magnesium-containing regenerated high-silicon wrought aluminum alloy and preparation method thereof |
-
2012
- 2012-06-19 CN CN2012102034018A patent/CN102747256A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1936051A (en) * | 2006-10-17 | 2007-03-28 | 山东大学 | Aluminium-silicon-copper-magnesium series deforming alloy and its preparing method |
| CN101333614A (en) * | 2007-06-29 | 2008-12-31 | 东北大学 | Structural material piece of magnesium-containing high-silicon aluminum alloy and preparation method thereof |
| CN101144134A (en) * | 2007-10-15 | 2008-03-19 | 李贞宽 | Aluminum-silicon series deforming alloy and manufacturing method thereof |
| CN101158001A (en) * | 2007-11-23 | 2008-04-09 | 苏州有色金属研究院有限公司 | Vacuum Stirring Composite Particle Reinforced Aluminum Matrix Composite Material and Its Preparation Technology |
| CN102397905A (en) * | 2011-11-25 | 2012-04-04 | 沈阳工业大学 | Hot extrusion forming method for hypereutectic Al-Si alloy |
| CN102418013A (en) * | 2011-12-08 | 2012-04-18 | 东北大学 | Magnesium-containing regenerated high-silicon wrought aluminum alloy and preparation method thereof |
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