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CN1997763A - Thin strips or foils of alfesi alloy - Google Patents

Thin strips or foils of alfesi alloy Download PDF

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CN1997763A
CN1997763A CNA2004800210038A CN200480021003A CN1997763A CN 1997763 A CN1997763 A CN 1997763A CN A2004800210038 A CNA2004800210038 A CN A2004800210038A CN 200480021003 A CN200480021003 A CN 200480021003A CN 1997763 A CN1997763 A CN 1997763A
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CN100445405C (en
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阿梅勒·达尼埃卢
让马里·费蓬
布律诺·舍纳尔
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Novelis Inc Canada
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/02Alloys based on aluminium with silicon as the next major constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • C22F1/043Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with silicon as the next major constituent

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Abstract

The invention relates to a thin strip or foil, having a thickness of 6 to 200mum, preferably, of 6 to 50mum, and composed of an alloy containing (in weight %) Si: 1.0 to 1.5, Fe: 1.0 to 1.5, Cu < 0.2, Mn < 0.1, other elements < 0.05 each up to a total < 0.15, the remainder being Al. The annealed thin strip or foil has a tensile strength Rm > 110 MPa for a thickness > 9 mum and > 100 MPa for a thickness of 6 to 9 mum, and an elastic limit R0.2 > 70 MPa. Preferably, said alloy has a silicon content of 1.1 to 1.3 % and an iron content of 1.0 to 1.2 %. The aforementioned thin strips or foils may be used especially for the production of multilayer composites, overcaps for bottles or aluminium wrappings.

Description

铝铁硅合金薄带或箔Aluminum-iron-silicon alloy thin strip or foil

技术领域technical field

本发明涉及薄带或箔以及制造这种薄带或箔的方法,所述薄带或箔的厚度小于200μm、优选小于50μm,并由含有铁和硅的铝合金制成,而且具有相当低的锰含量。这些带可以通过传统板材(plate)的半连铸或连铸来获得,例如双带浇铸或双辊浇铸。The present invention relates to a thin strip or foil having a thickness of less than 200 μm, preferably less than 50 μm, made of an aluminum alloy containing iron and silicon and having a relatively low manganese content. These belts can be obtained by conventional semi-continuous or continuous casting of plates, for example twin-belt casting or twin-roll casting.

背景技术Background technique

铝合金薄箔市场的趋势正向着用于既定应用的厚度持续减小的方向发展,同时要求高机械性能和良好的成型性。The trend in the Aluminum Alloy Thin Foil market is towards a continuous reduction in thickness for given applications, while requiring high mechanical properties and good formability.

具有非常低的锰含量的合金通常用于薄箔,例如铝业协会(aluminumassociation)登记的具有以下组成(重量%)的8111合金:Alloys with very low manganese content are commonly used for thin foils, such as the Aluminum Association registered 8111 alloy with the following composition (wt %):

Si 0.30-1.1;Fe 0.40-1.0;Cu<0.10;Mn<0.10Si 0.30-1.1; Fe 0.40-1.0; Cu<0.10; Mn<0.10

缺少锰使得在最后的退火期间容易实现再结晶,但是极限拉伸强度Rm在厚度小于100μm时不足。The lack of manganese makes it easy to achieve recrystallization during the final annealing, but the ultimate tensile strength Rm is insufficient at a thickness of less than 100 μm.

因此,需要研制新型合金和/或最优化转变过程以满足市场需求。Therefore, there is a need to develop new alloys and/or optimize the transformation process to meet market demands.

一般加入锰以提高机械强度,例如铝业协会登记的具有以下组成(重量%)的8006合金:Manganese is generally added to improve mechanical strength, such as the 8006 alloy registered by the Aluminum Association with the following composition (weight %):

Si<0.40;Fe:1.2-2.0;Cu<0.30;Mn:0.30-1.0;Mg<0.10Si<0.40; Fe: 1.2-2.0; Cu<0.30; Mn: 0.30-1.0; Mg<0.10

加入锰的结果是使材料坚硬。对于具有下列组成的合金:Si=0.23%;Fe=1.26%;Cu=0.017%;Mn=0.37%;Mg=0.0032%;Ti=0.008%,采用属于本申请人的专利US 6 517 646结合有利的转变过程得到的机械性能为在厚度为6.6μm时Rm值等于103MPa。The result of adding manganese is to make the material hard. For alloys with the following composition: Si=0.23%; Fe=1.26%; Cu=0.017%; Mn=0.37%; Mg=0.0032%; The mechanical properties obtained during the transformation process are R m values equal to 103 MPa at a thickness of 6.6 μm.

也可以通过在含铁的8000系列合金中加入少量的锰来改善机械性能。专利申请WO 02/64848(Alcan international)描述了通过连铸制造由含有1.2%-1.7%Fe和0.35%-0.8%Si的AlFeSi合金制成的薄带。通过向合金中加入0.07%-0.20%的锰来得到高机械强度。加入锰被认为是在最终退火之后得到小的晶粒尺寸所必需的。Mechanical properties can also be improved by adding small amounts of manganese to iron-containing 8000 series alloys. Patent application WO 02/64848 (Alcan international) describes the production by continuous casting of thin strips made of an AlFeSi alloy containing 1.2%-1.7% Fe and 0.35%-0.8% Si. High mechanical strength is obtained by adding 0.07%-0.20% manganese to the alloy. The addition of manganese is considered necessary to obtain a small grain size after the final anneal.

因此,锰似乎是能够改善8000合金机械性能的元素。但是,固溶液中或微细沉淀形式的锰可在最终退火期间阻碍或延迟再结晶。因此,需要在所述过程的每一步骤中精确控制含锰相的沉淀,但这通常是困难的。转变过程中的任何偏差对最终退火的效果都具有不可忽视的影响。因此,研制不含锰并且具有高机械性能的合金将非常有用。Therefore, manganese appears to be an element capable of improving the mechanical properties of 8000 alloy. However, manganese in solid solution or in finely precipitated form can hinder or delay recrystallization during final annealing. Therefore, the precipitation of the manganese-containing phase needs to be precisely controlled at each step of the process, but this is often difficult. Any deviation in the transformation process has a non-negligible effect on the final annealing effect. Therefore, it would be very useful to develop alloys that do not contain manganese and have high mechanical properties.

美国专利5 503 689(Reynolds Metals)描述了通过没有中间退火的连铸和冷轧制造薄带的方法,所述薄带由含有下列组成的合金制成:0.30%-1.1%Si和0.40%-1.0%Fe、少于0.25%的Cu和少于0.1%的Mn。铁和硅的优选含量是0.6%和0.75%。U.S. Patent 5 503 689 (Reynolds Metals) describes a method of manufacturing thin strip by continuous casting and cold rolling without intermediate annealing, said thin strip is made of an alloy containing the following composition: 0.30%-1.1% Si and 0.40%- 1.0% Fe, less than 0.25% Cu and less than 0.1% Mn. Preferred levels of iron and silicon are 0.6% and 0.75%.

美国专利5 725 695(Reynolds Metals)描述了在400℃-440℃(750_-825_)下中间退火并在288℃(550_)下最终再结晶退火处理相同组合物的过程。Si和Fe含量的比率大于或等于1。在实施例中,厚度为46μm(0.00185′)时,所得最大极限拉伸强度是90MPa(13.13ksi),最大屈服应力是39.1MPa(5.68ksi),伸长率是11.37%。这些机械性能对一些应用来说仍偏低。US Patent 5 725 695 (Reynolds Metals) describes the process of treating the same composition with intermediate annealing at 400°C-440°C (750mm-825mm) and final recrystallization annealing at 288°C (550mm). The ratio of Si and Fe content is greater than or equal to 1. In the embodiment, when the thickness is 46 μm (0.00185′), the obtained maximum ultimate tensile strength is 90 MPa (13.13 ksi), the maximum yield stress is 39.1 MPa (5.68 ksi), and the elongation is 11.37%. These mechanical properties are still low for some applications.

对于通过连铸得到的合金,通常需要进行高温热处理,从而通过再吸收沉淀块和使整个厚度上的结构均质化来降低偏析的有害性。通过双辊浇铸得到的8011合金(组成0.71%Fe;0.77%Si;0.038%Cu;0.006%Mn;98.45%Al)在600℃均质化的效果在Y.Birol的文章“Centerline Segregation in a Twin-Roll Cast AA8011 Alloy”Aluminium,74,1998,pp 318-321中有描述。沉淀相得以改进并且降低了不均匀性。因此中心偏析的减少限制了超薄箔的孔隙率并改善了它们的成型性。For alloys obtained by continuous casting, high temperature heat treatment is usually required to reduce the deleteriousness of segregation by reabsorbing precipitates and homogenizing the structure through the thickness. 8011 alloy (composition 0.71% Fe; 0.77% Si; 0.038% Cu; 0.006% Mn; 98.45% Al) obtained by twin-roll casting at 600 ° C in the article "Centerline Segregation in a Twin -Roll Cast AA8011 Alloy" Aluminum, 74, 1998, pp 318-321 described. The precipitated phase is improved and inhomogeneity is reduced. The reduction of central segregation thus limits the porosity of ultrathin foils and improves their formability.

限制热处理温度从经济角度讲是吸引人的。对于组成为0.7%Fe;0.7%Si;Mn<0.02,Zn<0.02;Cu<0.02的8111合金,虽然为了得到更彻底的转变必须在550℃-580℃退火(参见M.Slamova等人的“Response of AA8006 and AA8111 Strip-CastRolled Alloys to High Temperature Annealing”,ICAA-6,1998),但是在460℃观察到得到完全再结晶的相转变开始。因此,可以考虑对不含锰的合金进行低温均质化。Limiting the heat treatment temperature is economically attractive. For the 8111 alloy whose composition is 0.7% Fe; 0.7% Si; Mn<0.02, Zn<0.02; Cu<0.02, although it must be annealed at 550°C-580°C in order to obtain a more complete transformation (see "M.Slamova et al. Response of AA8006 and AA8111 Strip-CastRolled Alloys to High Temperature Annealing", ICAA-6, 1998), but at 460°C the onset of phase transition leading to complete recrystallization was observed. Therefore, low-temperature homogenization of alloys that do not contain manganese can be considered.

而且,在均质化之后向低厚度的转变中,标准作法是加入中间退火步骤以软化金属。对于锰合金,中间退火控制通常需要高温处理(在400℃以上)以实现再结晶。Also, in the transition to low thickness after homogenization, it is standard practice to add an intermediate annealing step to soften the metal. For manganese alloys, intermediate annealing control usually requires high temperature treatment (above 400°C) to achieve recrystallization.

对于无锰8000型合金,可以设想在低于8006型合金的热处理温度下进行热处理。For manganese-free Type 8000 alloys, it is conceivable to heat treat at temperatures lower than those for Type 8006 alloys.

专利申请WO 99/23269(Nippon Light Metal and Alcan International)描述了一种可应用于AlFeSi合金的方法,该合金含有0.2%-1%的Si和0.3%-1.2%的Fe,并且Si/Fe比率为0.4-1.2,在该方法中中间退火分两步进行,第一步在350℃-450℃下进行,第二步在200℃-330℃下进行。该方法目的是减少箔中的表面缺陷。没有提及机械性能。Patent application WO 99/23269 (Nippon Light Metal and Alcan International) describes a method applicable to AlFeSi alloys containing 0.2%-1% Si and 0.3%-1.2% Fe, and the Si/Fe ratio In this method, the intermediate annealing is carried out in two steps, the first step is carried out at 350°C-450°C, and the second step is carried out at 200°C-330°C. The purpose of this method is to reduce surface defects in the foil. No mention is made of mechanical properties.

本发明的目的是利用尽可能最经济的工业制造方法,得到由不加入锰的AlFeSi合金制成的并且具有高机械强度同时保持良好成型性的薄带或箔。The object of the present invention is to obtain, using the most economical industrial manufacturing method possible, a thin strip or foil made of an AlFeSi alloy without addition of manganese and having high mechanical strength while maintaining good formability.

发明内容Contents of the invention

本发明的主题是厚度为6-200μm、优选6-50μm的合金薄箔,具有以下组成(重量%):The subject of the invention is a thin alloy foil with a thickness of 6-200 μm, preferably 6-50 μm, having the following composition (% by weight):

Si:1.0-1.5;Fe:1.0-1.5;Cu<0.2;Mn<0.1;其它元素各自<0.05并且总计<0.15;剩余的为Al,优选条件Si/Fe≥0.95,并且厚度>9μm时退火回火下的极限拉伸强度Rm>110MPa、厚度为6-9μm时Rm>100MPa。优选薄箔的屈服应力R0.2>70MPa(对剪切试样进行测试)。作为箔厚度的函数的极限伸长率大于下列值:Si: 1.0-1.5; Fe: 1.0-1.5; Cu<0.2;Mn<0.1; other elements each <0.05 and the total <0.15; the rest is Al, the preferred condition is Si/Fe≥0.95, and the thickness is >9μm when annealed The ultimate tensile strength R m >110MPa under fire, and R m >100MPa when the thickness is 6-9μm. Preferably the yield stress R 0.2 of the thin foil is >70 MPa (tested on shear specimens). Ultimate elongation as a function of foil thickness greater than:

 厚度(μm) Thickness (μm)  A(%)大于 A(%) is greater than  优选大于 preferably greater than  6-9 6-9  3 3  4 4  9-15 9-15  5 5  7 7  15-25 15-25  10 10  15 15  25-50 25-50  18 18  25 25  50-200 50-200  20 20  25 25

所述合金的硅含量优选为1.1%-1.3%并且它的铁含量为1.0%-1.2%。The silicon content of the alloy is preferably between 1.1% and 1.3% and its iron content between 1.0% and 1.2%.

本发明的另一主题是厚度小于200μm的薄带的制造方法,所述薄带由具有下列组成(重量%)的合金制成:Si:1.0-1.5;Fe:1.0-1.5;Cu<0.2;Mn<0.1;其它元素各自<0.05并且总计<0.15;其余为Al,优选条件Si/Fe≥0.95,所述方法包括通过板材立式半连铸和热轧或通过可以随后热轧的连铸来制备初始带,将该初始带冷轧至最终厚度,同时可以在250℃-350℃、优选280℃-340℃的温度下进行中间退火2h-20h,以及在200℃-370℃的温度下进行最终退火。Another subject of the invention is a method for the manufacture of thin strips with a thickness of less than 200 μm, made of alloys with the following composition (% by weight): Si: 1.0-1.5; Fe: 1.0-1.5; Cu<0.2; Mn < 0.1; other elements < 0.05 each and in total < 0.15; the rest is Al, the preferred condition Si/Fe ≥ 0.95, the method includes by vertical semi-continuous casting and hot rolling of the plate or by continuous casting that can be followed by hot rolling Preparation of initial strip, which is cold rolled to final thickness, while intermediate annealing may be carried out at a temperature of 250°C-350°C, preferably 280°C-340°C for 2h-20h, and at a temperature of 200°C-370°C Final annealing.

具体实施方式Detailed ways

根据本发明的薄带或箔由几乎不含锰的8000 AlSiFe合金制成,其中锰的含量通常少于0.1%。铁和硅的含量明显高于最常用于薄箔的无锰AlSiFe合金8011和8111合金。一个优选的组成范围是含有1.1%-1.3%的硅和1.0%-1.2%的铁的合金。The thin strip or foil according to the invention is made of 8000 AlSiFe alloy which contains almost no manganese, where the manganese content is usually less than 0.1%. The iron and silicon contents are significantly higher than the manganese-free AlSiFe alloys 8011 and 8111 alloys most commonly used for thin foils. A preferred composition range is an alloy containing 1.1%-1.3% silicon and 1.0%-1.2% iron.

根据本发明的合金优选具有这样的组成,即硅和铁的含量之比Si/Fe≥0.95。对于具有这种组成的合金,退火回火(O回火)下它们的机械强度十分优异,即厚度>9μm时极限拉伸强度Rm>110Mpa或甚至是115Mpa、厚度为6-9μm时Rm>100Mpa,0.2%处的常规屈服应力R0.2>70MPa。由于伸长率至少与8011和8111合金一样高并且爆破压力(bursting pressure)更高,因此这种高机械强度不是以成型性为代价而得到的。The alloy according to the invention preferably has a composition such that the ratio of silicon and iron contents is Si/Fe≧0.95. For alloys with this composition, their mechanical strength under annealing and tempering (O tempering) is excellent, i.e. ultimate tensile strength Rm > 110Mpa or even 115Mpa for thickness > 9μm, Rm for thickness 6-9μm >100 MPa, normal yield stress R 0.2 >70 MPa at 0.2%. This high mechanical strength is not obtained at the expense of formability since the elongation is at least as high as the 8011 and 8111 alloys and the bursting pressure is higher.

得到的这些高机械性能与通过传统立式半连铸和热轧获得的板材生产的带和得自通过带浇铸或双辊浇铸的连铸的带一样好。连续带浇铸之后也进行热轧。These high mechanical properties obtained are as good as strips produced from plates obtained by conventional vertical semi-continuous casting and hot rolling, and strips obtained from continuous casting by strip casting or twin-roll casting. Continuous strip casting is also followed by hot rolling.

通过连续双辊浇铸获得的热轧带或铸造(as-cast)带可以在低温(450℃-500℃之间)下均质化以减少会降低成型性的中心偏析,从而达到最终厚度。这种低温热处理足以再吸收这些无锰合金中的任何中心偏析。然后将所述带冷轧至最终厚度或者至0.5mm-5mm的中间厚度,此时进行中间退火。与含锰合金不同,该中间退火可以在250℃-350℃、优选280℃-340℃的较低温度下持续进行超过2小时。虽然文献中尤其是上述专利申请WO 02/64848中描述了该温度范围,但是该温度范围低于保持在400℃以上的正常范围。Hot-rolled or as-cast strip obtained by continuous twin-roll casting can be homogenized at low temperature (between 450°C and 500°C) to reduce center segregation, which reduces formability, to achieve final thickness. This low temperature heat treatment is sufficient to resorb any center segregation in these manganese-free alloys. The strip is then cold rolled to a final gauge or to an intermediate gauge of 0.5mm-5mm, at which point an intermediate anneal is performed. Unlike alloys containing manganese, this intermediate annealing can be carried out for more than 2 hours at a lower temperature of 250°C-350°C, preferably 280°C-340°C. Although this temperature range is described in the literature, especially in the above-mentioned patent application WO 02/64848, it is lower than the normal range kept above 400°C.

本申请人已经发现,对AlFeSi合金更具体而言是具有Si/Fe>0.95的组成的AlFeSi合金实施低温热处理,在技术上可能的情况下可以取消中间退火,这样得到的机械强度明显高于正常中间退火可得到的机械强度,至少高15%。得到更高的机械强度的同时改善了根据ISO标准2758通过爆破压力或圆顶高度(dome height)测量的成型性。The applicant has found that the low-temperature heat treatment of AlFeSi alloys, more specifically AlFeSi alloys with a composition Si/Fe > 0.95, can eliminate, where technically possible, intermediate annealing, resulting in mechanical strengths significantly higher than normal The mechanical strength obtainable by intermediate annealing is at least 15% higher. Higher mechanical strength is obtained while improving formability as measured by burst pressure or dome height according to ISO standard 2758.

在220℃-370℃的温度下进行最终退火1h-72h。退火时间取决于箔的除油质量。退火之后得到精细晶粒结构,通过扫描电子显微镜的图像分析测得平均晶粒尺寸小于3μm。The final annealing is carried out at a temperature of 220°C-370°C for 1h-72h. The annealing time depends on the degreasing quality of the foil. After annealing a fine grain structure is obtained, with an average grain size of less than 3 μm as measured by image analysis with a scanning electron microscope.

低温均质化或完全不均质化与低温中间退火或完全不中间退火的组合在经济上是有利的,而且也有助于得到精细的晶粒尺寸。晶粒尺寸比高温热处理可得到的小约30%,因而提高了机械性能R0.2和Rm,对于小厚度而言,这些机械性能与晶粒接合点(grain joints)的数量相关。所述机械性能的提高不是以牺牲伸长率为代价来实现的,这是因为厚度方向上晶粒数量的增加还限制了所述箔厚度方向上一个或两个单晶粒局部破坏的风险。The combination of low-temperature homogenization or complete heterogeneity with low-temperature intermediate annealing or no intermediate annealing at all is economically advantageous and also contributes to a fine grain size. The grain size is about 30% smaller than achievable with high temperature heat treatment, thus improving the mechanical properties R 0.2 and R m , which are related to the number of grain joints for small thicknesses. The increase in mechanical properties is not achieved at the expense of elongation, since the increased number of grains through the thickness also limits the risk of local failure of one or two single grains through the thickness of the foil.

根据本发明的薄箔特别适合于要求良好机械强度和高成型性的应用,例如制造多层复合材料,尤其是用于包装新鲜产品的盖、封盖或铝包装材料。The thin foils according to the invention are particularly suitable for applications requiring good mechanical strength and high formability, such as the production of multilayer composites, especially lids, closures or aluminum packaging materials for packaging fresh products.

实施例Example

实施例1Example 1

通过连续双辊浇铸制造由根据本发明的合金A和8111型合金B制成的两条6.1mm厚的带,以论证合金组成的影响,表1中示出合金A和合金B的组成(重量%):Two 6.1 mm thick strips made of alloy A according to the invention and alloy B of the 8111 type were produced by continuous twin roll casting to demonstrate the effect of alloy composition, the compositions of alloy A and alloy B are shown in Table 1 (wt. %):

                                 表1 Table 1

 合金 Alloy  Si Si  Fe Fe Fe  Cu Cu  Mn Mn  Mg Mg  Cr Cr  Ti Ti  B B  A A  1.17 1.17  1.11 1.11  0.001 0.001  0.003 0.003  0.0004 0.0004  0.0007 0.0007  0.006 0.006  0.0005 0.0005  B B  0.7 0.7  0.7 0.7  0.001 0.001  0.003 0.003  0.0005 0.0005  0.001 0.001  0.007 0.007  0.0005 0.0005

将所述带冷轧至2mm的厚度然后在320℃下对其进行中间退火5小时。然后冷轧这些带几遍直到38μm的最终厚度。然后在270℃下对它们实施最终退火40小时。The strip was cold rolled to a thickness of 2 mm and then intermediate annealed at 320° C. for 5 hours. These strips were then cold rolled several times to a final thickness of 38 μm. They were then subjected to a final anneal at 270°C for 40 hours.

测量每种情况下的机械性能。测量值是根据NF-EN标准546-2的极限拉伸强度Rm(以MPa计)、0.2%处的常规屈服应力R0.2和极限伸长率A(以%计)、根据ISO标准2758测量的爆破压力Pe(以kPa计)和圆顶高度Hd(以mm计)。结果在表2中给出:Mechanical properties were measured in each case. The measured values are the ultimate tensile strength R m (in MPa) according to NF-EN standard 546-2, the normal yield stress R 0.2 at 0.2% and the ultimate elongation A (in %), measured according to ISO standard 2758 The burst pressure Pe (in kPa) and the dome height Hd (in mm). The results are given in Table 2:

                       表2 Table 2

 合金 Alloy  Rm(MPa)R m (MPa)  R0.2(MPa)R 0.2 (MPa)  A(%) A(%)  Pe(kPA) Pe(kPA)  Hd Hd  A A  123 123  76 76  30 30  394 394  9.2 9.2  B B  104 104  54 54  15.8 15.8  284 284  6.6 6.6

发现,与8111型合金B不同,合金A带的极限强度远大于110MPa,并且屈服应力大于70MPa。爆破压力和伸长率也更高,因此该合金的强度和成型性更高。It was found that, unlike alloy B of the 8111 type, the ultimate strength of the alloy A ribbon was much greater than 110 MPa, and the yield stress was greater than 70 MPa. The burst pressure and elongation are also higher, so the alloy is stronger and more formable.

实施例2Example 2

通过连续双辊浇铸制造由实施例1中所述的合金A制成的6.1mm厚的带。随后将所述带冷轧至2mm的厚度,然后在500℃下对该带的一部分进行这类合金的正常中间退火5小时。根据本发明对该带的其余部分在320℃下进行中间退火5小时。再将该带的这两部分冷轧几遍直至10.5μm的最终厚度。然后在270℃下对它们进行最终退火40小时。A 6.1 mm thick strip made of alloy A as described in Example 1 was produced by continuous twin roll casting. The strip was then cold rolled to a thickness of 2 mm, and a portion of the strip was then subjected to the normal intermediate annealing for this type of alloy at 500° C. for 5 hours. The remainder of the tape was intermediate annealed at 320° C. for 5 hours according to the invention. These two parts of the strip were then cold rolled several times to a final thickness of 10.5 μm. They were then subjected to final annealing at 270°C for 40 hours.

性能与实施例1中相同,数值示于表3:Performance is identical with embodiment 1, and numerical value is shown in table 3:

                               表3 table 3

 中间退火 Intermediate annealing  Rm(MPa)R m (MPa)  R0.2(MPa)R 0.2 (MPa)  A(%) A(%)  Pe(kPa) Pe(kPa)  Hd(mm) Hd(mm)  470℃ 470°C  99 99  63 63  7.3 7.3  71 71  5.1 5.1  320℃ 320℃  117 117  84 84  8.1 8.1  92 92  5.7 5.7

发现,较低的中间退火温度提高了机械强度、伸长率、爆破强度和成型性。通过SEM图像分析测得的平均晶粒尺寸在470℃退火时为3.6μm、在320℃退火时为2.3μm。因此,低温退火对机械性能的提高与最终退火后所得晶粒尺寸的减少有关。It was found that lower intermediate annealing temperatures improved mechanical strength, elongation, burst strength and formability. The average grain size measured by SEM image analysis was 3.6 μm at 470° C. annealing and 2.3 μm at 320° C. annealing. Therefore, the enhancement of mechanical properties by low-temperature annealing is related to the reduction in grain size obtained after final annealing.

Claims (10)

1. alloy thin band or paper tinsel, its thickness is 6-200 μ m, preferred 6-50 μ m, described alloy has following composition (weight %):
Si:1.0-1.5; Fe:1.0-1.5; Cu<0.2; Mn<0.1; Other element separately<0.05 and amount to<0.15, residue is Al, the ultimate tensile strength R during thickness>9 μ m under the annealing tempering mR when>110MPa, thickness are 6-9 μ m m>100MPa.
2. according to the strip or the paper tinsel of claim 1, it is characterized in that described strip or the paper tinsel ultimate tensile strength R under the annealing tempering when thickness>9 μ m m>115MPa.
3. according to the strip or the paper tinsel of claim 1 or 2, it is characterized in that the yielding stress R of described strip or paper tinsel 0.2>70MPa.
4. according to strip any among the claim 1-3 or paper tinsel, the elongation limit A that it is characterized in that described strip or paper tinsel is the function of thickness, and is as follows:
Thickness (μ m) A (%) greater than Be preferably greater than 6-9 3 4 9-15 5 7 15-25 10 15 25-50 18 25 50-200 20 25
5. according to strip any among the claim 1-4 or paper tinsel, what it is characterized in that described alloy consists of Si/Fe 〉=0.95.
6. according to strip any among the claim 1-5 or paper tinsel, the silicone content that it is characterized in that described alloy is that 1.1%-1.3% and its iron level are 1.0%-1.2%.
7. the manufacture method of strip, described strip thickness is made less than 200 μ m and by the Al-Fe-Si alloy with following composition (weight %):
Si:1.0-1.5; Fe:1.0-1.5; Cu<0.2; Mn<0.1; Other element separately<0.05 and amount to<0.15; Remaining is Al,
Described method comprises by the vertical D.C.casting of sheet material and hot rolling or by hot rolled continuous casting subsequently and prepares initial strip, this initial strip is cold-rolled to final thickness, simultaneously can under 250 ℃-350 ℃, preferred 280 ℃-340 ℃ temperature, carry out process annealing, and under 200 ℃-370 ℃ temperature, carry out final annealing.
8. according to the method for claim 7, what it is characterized in that described alloy consists of Si/Fe 〉=0.95.
9. according to the method for claim 7 or 8, it is characterized in that described initial strip being homogenized before cold rolling under 450 ℃ of-500 ℃ of temperature.
10. according to method any among the claim 7-9, it is characterized in that described band is by continuous double-roller casting preparation.
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FR0308864A FR2857981A1 (en) 2003-07-21 2003-07-21 Thin sheet or strip of aluminum alloy for bottle caps and wrapping foil has a thickness of less than 200 microns, is essentially free of manganese, and has increased mechanical strength
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US8381796B2 (en) 2007-04-11 2013-02-26 Alcoa Inc. Functionally graded metal matrix composite sheet
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CN101899596A (en) * 2008-10-07 2010-12-01 美铝公司 Raw material for metal foil product and method for producing same
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