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CN113215451B - High-strength Al-Mg-Si-Cu aluminum alloy and preparation method thereof - Google Patents

High-strength Al-Mg-Si-Cu aluminum alloy and preparation method thereof Download PDF

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CN113215451B
CN113215451B CN202110523814.3A CN202110523814A CN113215451B CN 113215451 B CN113215451 B CN 113215451B CN 202110523814 A CN202110523814 A CN 202110523814A CN 113215451 B CN113215451 B CN 113215451B
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CN113215451A (en
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郭晓斌
邓运来
王宇
何锡宇
姜伟
谭桂薇
王冯权
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Central South University
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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
    • 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
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/02Making non-ferrous alloys by melting
    • C22C1/026Alloys based on aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/06Alloys based on aluminium with magnesium as the next major constituent
    • C22C21/08Alloys based on aluminium with magnesium as the next major constituent with silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/12Alloys based on aluminium with copper as the next major constituent
    • C22C21/14Alloys based on aluminium with copper as the next major constituent with silicon
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/12Alloys based on aluminium with copper as the next major constituent
    • C22C21/16Alloys based on aluminium with copper as the next major constituent with magnesium
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    • 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
    • C22F1/002Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working by rapid cooling or quenching; cooling agents used therefor
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    • 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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    • 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
    • C22F1/047Changing 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 magnesium 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
    • C22F1/057Changing 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 copper as the next major constituent

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Abstract

The invention discloses a high-strength Al-Mg-Si-Cu alloy and a preparation method thereof, and the high-strength Al-Mg-Si-Cu alloy comprises the following components in percentage by mass: 0.75-1.10 wt.%, Fe: 0.35 wt.%, Cu: 0.75-1.0 wt.%, Mn: 0.5-0.75 wt.%, Mg: 0.85-1.30 wt.%, Cr: less than or equal to 0.05 wt.%, Ti: not more than 0.10 wt.%, the balance being Al, the sum of the mass percentages of the components being 100%, and the mass ratio of (Mg + Si)/Cu being controlled to be 1.6-3.2, mixing the raw materials, and carrying out smelting, casting, homogenizing treatment, hot extrusion, quenching and aging treatment to obtain the high-strength Al-Mg-Si-Cu alloy. According to the Al-Mg-Si-Cu alloy, 0.85-1.30 wt.% of Mg element is added, and the mass ratio of (Mg + Si)/Cu is strictly controlled, so that the alloy material with the strength of more than 450MPa can be prepared.

Description

一种高强度Al-Mg-Si-Cu系铝合金及其制备方法A kind of high-strength Al-Mg-Si-Cu series aluminum alloy and preparation method thereof

技术领域technical field

本发明属于铝合金技术领域,具体涉及一种高强度Al-Mg-Si-Cu系铝合金及其制备方法。The invention belongs to the technical field of aluminum alloys, and in particular relates to a high-strength Al-Mg-Si-Cu series aluminum alloy and a preparation method thereof.

背景技术Background technique

随着新能源汽车的蓬勃发展,汽车轻量化的趋势越来越受到重视。Al-Mg-Si-(Cu)系合金由于具有优异的耐腐蚀、可焊及成形性能,而广泛应用于新能源汽车。然而,其强度普遍为300MPa级。为了实现高效、节能、环保的目的,发展更高强度的Al-Mg-Si-(Cu)系合金具有十分重要的意义。With the vigorous development of new energy vehicles, the trend of lightweight vehicles has attracted more and more attention. Al-Mg-Si-(Cu) alloys are widely used in new energy vehicles due to their excellent corrosion resistance, weldability and formability. However, its strength is generally in the 300MPa class. In order to achieve high efficiency, energy saving and environmental protection, it is of great significance to develop Al-Mg-Si-(Cu) alloys with higher strength.

目前,在新能源汽车上应用较为广泛的Al-Mg-Si-(Cu)系合金主要包括低Cu含量6063、6005A、6082及中等Cu含量的6061等合金。然而,这些合金强度普遍在400MPa以下;此外,为进一步提升Al-Mg-Si-(Cu)系合金的强度,在上述合金的基础上,进一步提高Cu含量,发展了高Cu含量的6111、6013等合金。这些合金的Cu含量重量比达1%,尽管其强度可达400MPa级,然而,对于强度要求在450MPa级的合金,上述合金均不能满足要求;此外,由于合金时效强化能力等本质特性的限制,450MPa级Al-Mg-Si-(Cu)系合金的开发,仍然是目前的技术难点。At present, the Al-Mg-Si-(Cu) alloys widely used in new energy vehicles mainly include alloys with low Cu content 6063, 6005A, 6082 and 6061 with medium Cu content. However, the strength of these alloys is generally below 400MPa; in addition, in order to further improve the strength of Al-Mg-Si-(Cu) alloys, on the basis of the above alloys, the Cu content is further increased, and 6111 and 6013 with high Cu content have been developed. and other alloys. The Cu content of these alloys is up to 1% by weight, and although their strength can reach 400MPa, none of the above alloys can meet the requirements for alloys with a strength of 450MPa; The development of 450MPa grade Al-Mg-Si-(Cu) alloy is still a technical difficulty at present.

发明内容SUMMARY OF THE INVENTION

针对现有技术的不足,本发明的目的是提供一种高强Al-Mg-Si-(Cu)系合金及其制备方法,其强度能达450MPa级。In view of the deficiencies of the prior art, the purpose of the present invention is to provide a high-strength Al-Mg-Si-(Cu) alloy and a preparation method thereof, the strength of which can reach 450MPa.

为了达到上述目的,本发明提供以下技术方案:In order to achieve the above object, the present invention provides the following technical solutions:

一种高强度Al-Mg-Si-Cu系合金,其成分按质量百分比,包括,Si:0.75~1.10wt.%,Fe:≤0.35wt.%,Cu:0.75~1.0wt.%,Mn:0.5~0.75wt.%,Mg:0.85~1.30wt.%,Cr:≤0.05wt.%,Ti:≤0.10wt.%,余量为Al,各成分质量百分比之和为100%,控制(Mg+Si)/Cu的质量比为1.6~3.2。A high-strength Al-Mg-Si-Cu alloy, the composition of which, by mass percentage, comprises: Si: 0.75-1.10wt.%, Fe:≤0.35wt.%, Cu: 0.75-1.0wt.%, Mn: 0.5~0.75wt.%, Mg: 0.85~1.30wt.%, Cr: ≤0.05wt.%, Ti: ≤0.10wt.%, the balance is Al, the sum of the mass percentage of each component is 100%, control (Mg The mass ratio of +Si)/Cu is 1.6 to 3.2.

本发明通过添加0.85~1.30wt.%的Mg元素,用于尽可能多的补充Q相(Al5Cu2Mg8Si6)所需的Mg元素含量,且严格控制(Mg+Si)/Cu的质量比,一方面尽可能提高强化相Q相(Al5Cu2Mg8Si6)的含量,另一方面则避免形成过量的θ相(Al2Cu),从而显著提升合金材料的强度,获得450MPa级的Al-Mg-Si-Cu系合金。In the present invention, by adding 0.85-1.30 wt.% Mg element, the content of Mg element required for supplementing the Q phase (Al 5 Cu 2 Mg 8 Si 6 ) as much as possible is strictly controlled, and (Mg+Si)/Cu is strictly controlled. On the one hand, the content of the strengthening phase Q phase (Al 5 Cu 2 Mg 8 Si 6 ) can be increased as much as possible, and on the other hand, the formation of excessive θ phase (Al 2 Cu) can be avoided, thereby significantly improving the strength of the alloy material. An Al-Mg-Si-Cu alloy of 450MPa grade was obtained.

作为优选,所述(Mg+Si)/Cu的质量比为2.2。本发明优选(Mg+Si)/Cu的质量比为2.2,可以形成最多体积分数的Q相(Al5Cu2Mg8Si6),同时避免形成过量θ相(Al2Cu),进而最大程度的提升合金材料的强度。Preferably, the mass ratio of (Mg+Si)/Cu is 2.2. In the present invention, the mass ratio of (Mg+Si)/Cu is preferably 2.2, which can form the Q phase (Al 5 Cu 2 Mg 8 Si 6 ) with the largest volume fraction, while avoiding the formation of excessive theta phase (Al 2 Cu), so as to maximize the to enhance the strength of the alloy material.

本发明还提供了上述高强度Al-Mg-Si-Cu系合金的制备方法,将各原料混合配料,经熔炼、铸锭、均质处理、热挤压、淬火、时效处理,即得高强度Al-Mg-Si-Cu系合金。The present invention also provides a method for preparing the above-mentioned high-strength Al-Mg-Si-Cu series alloy. The raw materials are mixed and batched, and the high-strength alloy is obtained through smelting, ingot casting, homogenization treatment, hot extrusion, quenching and aging treatment. Al-Mg-Si-Cu alloy.

作为优选,所述熔炼的温度为720~760℃。Preferably, the temperature of the smelting is 720-760°C.

作为优选,所述铸锭采用半连续铸锭方式,铸造温度为690~710℃,铸造速度为45-140mm/min。Preferably, the ingot is in a semi-continuous ingot casting method, the casting temperature is 690-710° C., and the casting speed is 45-140 mm/min.

作为优选,所述均质处理过程为:将铸锭加热到530~560℃并保温1~10h,随后以不大于15℃/min的速率冷却到400~450℃,接着以不小于30℃/min的速率冷却到180℃以下冷却。Preferably, the homogenizing treatment process is as follows: heating the ingot to 530-560°C and keeping the temperature for 1-10 hours, then cooling to 400-450°C at a rate of not more than 15°C/min, and then cooling to 400-450°C at a rate of not less than 30°C/min. The rate of min cooling to below 180 ℃ cooling.

作为优选,所述热挤压的工艺参数为:均质处理后的铸锭加热到500~530℃,挤压筒温度为430~500℃,挤压材挤出速度为4-20m/min。Preferably, the process parameters of the hot extrusion are as follows: the homogenized ingot is heated to 500-530°C, the temperature of the extrusion cylinder is 430-500°C, and the extrusion speed of the extruded material is 4-20 m/min.

作为优选,所述淬火温度不低于535℃,淬火冷却介质为水。Preferably, the quenching temperature is not lower than 535°C, and the quenching cooling medium is water.

作为优选,所述时效处理的温度为100~200℃,时间为1~48h。Preferably, the temperature of the aging treatment is 100-200° C., and the time is 1-48 h.

本发明通过添加0.85~1.30wt.%的Mg元素,且严格控制(Mg+Si)/Cu的质量比,一方面尽可能提高强化相Q相(Al5Cu2Mg8Si6)的含量,另一方面则避免形成过量的θ相(Al2Cu),在合金材料制备过程中,Q相起到析出强化的作用,从而显著提升合金材料的强度,获得450MPa级的Al-Mg-Si-Cu系合金。In the present invention, by adding 0.85-1.30wt.% Mg element and strictly controlling the mass ratio of (Mg+Si)/Cu, on the one hand, the content of the strengthening phase Q phase (Al 5 Cu 2 Mg 8 Si 6 ) is increased as much as possible, On the other hand, the formation of excessive theta phase (Al 2 Cu) is avoided. During the preparation process of the alloy material, the Q phase plays the role of precipitation strengthening, thereby significantly improving the strength of the alloy material, and obtaining 450MPa grade Al-Mg-Si- Cu-based alloys.

与现有技术相比,本发明的优点在于:Compared with the prior art, the advantages of the present invention are:

本发明的Al-Mg-Si-Cu系合金,通过添加0.85~1.30wt.%的Mg元素,且严格控制(Mg+Si)/Cu的质量比,可以制得强度达到450MPa以上的合金材料。The Al-Mg-Si-Cu alloy of the present invention can be prepared by adding 0.85-1.30 wt.% Mg element and strictly controlling the mass ratio of (Mg+Si)/Cu to obtain an alloy material with a strength of more than 450 MPa.

具体实施方式Detailed ways

本发明中选用的所有材料、试剂和仪器都为本领域熟知的,但不限制本发明的实施,其他本领域熟知的一些试剂和设备都可适用于本发明以下实施方式的实施。All materials, reagents and instruments selected in the present invention are well known in the art, but do not limit the implementation of the present invention, and some other reagents and equipment well known in the art are applicable to the implementation of the following embodiments of the present invention.

实施例1Example 1

一种高强度Al-Mg-Si-Cu合金,其化学成分按质量百分比为:Si:0.75%、Fe:0.18%、Cu、1.00%、Mn:0.60%、Mg:0.85%、Cr:0.05%、Ti:0.068%,余量为Al,各成分质量百分比之和为100%;(Mg+Si)/Cu的质量比为1.6。采用该成分的合金制备6mm厚挤压材,其挤压比为20。A high-strength Al-Mg-Si-Cu alloy, its chemical composition is: Si: 0.75%, Fe: 0.18%, Cu, 1.00%, Mn: 0.60%, Mg: 0.85%, Cr: 0.05% by mass percentage , Ti: 0.068%, the remainder is Al, the sum of the mass percentages of each component is 100%; the mass ratio of (Mg+Si)/Cu is 1.6. The alloy of this composition was used to prepare a 6 mm thick extrusion with an extrusion ratio of 20.

所述的合金挤压材制备方法,包括以下步骤:The described alloy extrusion material preparation method comprises the following steps:

S1熔炼:按设定比例配料,在740℃下熔炼熔化原料,充分搅拌、除气除渣;S1 smelting: ingredients according to the set proportion, smelting and melting raw materials at 740 ℃, fully stirring, degassing and slag removal;

S2铸锭:通过熔炼得到符合要求的熔体,采用半连续铸造方法于700℃浇铸出用于挤压的铸锭;S2 ingot: obtain the melt that meets the requirements by smelting, and cast the ingot for extrusion at 700°C by the semi-continuous casting method;

S3均质处理:将铸锭加热到560℃并保温1h,随后以10℃/min的速率冷却到450℃,接着以45℃/min的速率冷却到180℃以下出炉自然冷却,得到均质处理后的铸锭;S3 Homogenization treatment: The ingot is heated to 560°C and kept for 1 h, then cooled to 450°C at a rate of 10°C/min, and then cooled to below 180°C at a rate of 45°C/min. the ingot after

S4热挤压:将步骤(3)所得均质处理后的铸锭加热到530℃,挤压筒温度为500℃,随后以20m/min的挤压速度挤出;S4 hot extrusion: heating the homogenized ingot obtained in step (3) to 530°C, the extrusion cylinder temperature is 500°C, and then extruding at an extrusion speed of 20 m/min;

S5淬火:淬火温度为535℃,挤压材流出模孔后进入在线淬火装置进行穿水淬火处理;S5 quenching: the quenching temperature is 535℃, the extruded material flows out of the die hole and enters the online quenching device for water quenching treatment;

S6时效:淬火后的挤压材加热到100℃,并保温48h进行时效处理,出炉后得到所述高强Al-Mg-Si-Cu系合金挤压材,所得的挤压材力学性能见表1。S6 Aging: The quenched extruded material is heated to 100°C and kept for 48 hours for aging treatment. After being released from the furnace, the high-strength Al-Mg-Si-Cu alloy extruded material is obtained. The mechanical properties of the obtained extruded material are shown in Table 1. .

实施例2Example 2

一种高强度Al-Mg-Si-Cu合金,其化学成分按质量百分比为:Si:1.10%、Fe:0.18%、Cu、0.75%、Mn:0.50%、Mg:1.30%、Cr:0.05%、Ti:0.06%,余量为Al,各成分质量百分比之和为100%;(Mg+Si)/Cu的质量比为3.2。采用该成分的合金制备6mm厚挤压材,其挤压比为20。A high-strength Al-Mg-Si-Cu alloy, its chemical composition is: Si: 1.10%, Fe: 0.18%, Cu, 0.75%, Mn: 0.50%, Mg: 1.30%, Cr: 0.05% by mass percentage , Ti: 0.06%, the balance is Al, the sum of the mass percentages of each component is 100%; the mass ratio of (Mg+Si)/Cu is 3.2. The alloy of this composition was used to prepare a 6 mm thick extrusion with an extrusion ratio of 20.

所述的合金挤压材制备方法,包括以下步骤:The described alloy extrusion material preparation method comprises the following steps:

S1熔炼:按设定比例配料,在740℃下熔炼熔化原料,充分搅拌、除气除渣;S1 smelting: ingredients according to the set proportion, smelting and melting raw materials at 740 ℃, fully stirring, degassing and slag removal;

S2铸锭:通过熔炼得到符合要求的熔体,采用半连续铸造方法于700℃浇铸出用于挤压的铸锭;S2 ingot: obtain the melt that meets the requirements by smelting, and cast the ingot for extrusion at 700°C by the semi-continuous casting method;

S3均质处理:将铸锭加热到530℃并保温10h,随后以5℃/min的速率冷却到400℃,接着以不小于50℃/min的速率冷却到180℃以下出炉自然冷却,得到均质处理后的铸锭;S3 Homogenization treatment: the ingot is heated to 530°C and kept for 10h, then cooled to 400°C at a rate of 5°C/min, and then cooled to below 180°C at a rate of not less than 50°C/min. Ingot after quality treatment;

S4热挤压:将步骤(3)所得均质处理后的铸锭加热到500℃,挤压筒温度为430℃,随后以4m/min的挤压速度挤出;S4 hot extrusion: heating the ingot after the homogenization treatment obtained in step (3) to 500 ° C, the extrusion barrel temperature is 430 ° C, and then extruding at an extrusion speed of 4 m/min;

S5淬火:淬火温度为535℃,挤压材流出模孔后进入在线淬火装置进行穿水淬火处理;S5 quenching: the quenching temperature is 535℃, the extruded material flows out of the die hole and enters the online quenching device for water quenching treatment;

S6时效:淬火后的挤压材加热到200℃,并保温1h进行时效处理,出炉后得到所述高强Al-Mg-Si-Cu系合金挤压材,所得的挤压材力学性能见表1。S6 aging: the quenched extruded material is heated to 200°C, and kept for 1 h for aging treatment. After being released from the furnace, the high-strength Al-Mg-Si-Cu alloy extruded material is obtained. The mechanical properties of the obtained extruded material are shown in Table 1. .

实施例3Example 3

一种高强度Al-Mg-Si-Cu合金,其化学成分按质量百分比为:Si:0.9%、Fe:0.18%、Cu、0.95%、Mn:0.60%、Mg:1.2%、Cr:0.05%、Ti:0.068%,余量为Al,各成分质量百分比之和为100%;(Mg+Si)/Cu的质量比为2.2。采用该成分的合金制备6mm厚挤压材,其挤压比为20。A high-strength Al-Mg-Si-Cu alloy, its chemical composition is: Si: 0.9%, Fe: 0.18%, Cu, 0.95%, Mn: 0.60%, Mg: 1.2%, Cr: 0.05% by mass percentage , Ti: 0.068%, the remainder is Al, the sum of the mass percentages of each component is 100%; the mass ratio of (Mg+Si)/Cu is 2.2. The alloy of this composition was used to prepare a 6 mm thick extrusion with an extrusion ratio of 20.

所述的合金挤压材制备方法,包括以下步骤:The described alloy extrusion material preparation method comprises the following steps:

S1熔炼:按设定比例配料,在740℃下熔炼熔化原料,充分搅拌、除气除渣;S1 smelting: ingredients according to the set proportion, smelting and melting raw materials at 740 ℃, fully stirring, degassing and slag removal;

S2铸锭:通过熔炼得到符合要求的熔体,采用半连续铸锭方法于700℃浇铸出用于挤压的铸锭;S2 ingot: obtain the melt that meets the requirements by smelting, and cast the ingot for extrusion at 700 ℃ by the semi-continuous ingot casting method;

S3均质处理:将铸锭加热到540℃并保温8h,随后以10℃/min的速率冷却到400℃,接着以30℃/min的速率冷却到180℃以下出炉自然冷却,得到均质处理后的铸锭;S3 Homogenization treatment: The ingot is heated to 540°C and kept for 8 hours, then cooled to 400°C at a rate of 10°C/min, and then cooled to below 180°C at a rate of 30°C/min. the ingot after

S4热挤压:将步骤(3)所得均质处理后的铸锭加热到500℃,挤压筒温度为430℃,随后以12m/min的挤压速度挤出;S4 hot extrusion: heating the ingot after the homogenization treatment obtained in step (3) to 500°C, the temperature of the extrusion cylinder is 430°C, and then extruding at an extrusion speed of 12 m/min;

S5淬火:淬火温度为535℃,挤压材流出模孔后进入在线淬火装置进行穿水淬火处理;S5 quenching: the quenching temperature is 535℃, the extruded material flows out of the die hole and enters the online quenching device for water quenching treatment;

S6时效:淬火后的挤压材加热到160℃,并保温24h进行时效处理,出炉后得到所述高强Al-Mg-Si-Cu系合金挤压材,所得的挤压材力学性能见表1。S6 Aging: The quenched extruded material is heated to 160°C and kept for 24 hours for aging treatment. After being released from the furnace, the high-strength Al-Mg-Si-Cu alloy extruded material is obtained. The mechanical properties of the obtained extruded material are shown in Table 1. .

对比例1Comparative Example 1

对比例1所用的合金化学成分按质量百分比为:Si:0.85%、Fe:0.18%、Cu、1.2%、Mn:0.60%、Mg:0.90%、Cr:0.05%、Ti:0.05%,余量为Al,各成分质量百分比之和为100%;(Mg+Si)/Cu的质量比为1.46。其制备方法与实施例1相同。所得的挤压材力学性能见表1。The chemical composition of the alloy used in Comparative Example 1 is: Si: 0.85%, Fe: 0.18%, Cu, 1.2%, Mn: 0.60%, Mg: 0.90%, Cr: 0.05%, Ti: 0.05%, the remainder is Al, and the sum of the mass percentages of each component is 100%; the mass ratio of (Mg+Si)/Cu is 1.46. The preparation method is the same as that of Example 1. The mechanical properties of the obtained extruded materials are shown in Table 1.

对比例2Comparative Example 2

对比例2所用的合金化学成分按质量百分比为:Si:1.10%、Fe:0.18%、Cu、0.70%、Mn:0.50%、Mg:1.30%、Cr:0.05%、Ti:0.06%,余量为Al,各成分重量百分比之和为100%;(Mg+Si)/Cu的质量比为3.43。其熔铸、均匀化及时效工艺与实施例1相同,其挤压工艺为:铸锭加热到500℃,挤压筒温度为450℃,挤压材挤出速度8m/min;淬火温度为520℃,淬火方式为在线穿水淬火。所得的挤压材力学性能见表1。The chemical composition of the alloy used in Comparative Example 2 is: Si: 1.10%, Fe: 0.18%, Cu, 0.70%, Mn: 0.50%, Mg: 1.30%, Cr: 0.05%, Ti: 0.06%, the remainder is Al, and the sum of the weight percentages of each component is 100%; the mass ratio of (Mg+Si)/Cu is 3.43. The casting, homogenization and aging processes are the same as in Example 1, and the extrusion process is as follows: the ingot is heated to 500°C, the extrusion barrel temperature is 450°C, the extrusion speed of the extruded material is 8m/min; the quenching temperature is 520°C , the quenching method is online water quenching. The mechanical properties of the obtained extruded materials are shown in Table 1.

力学性能测试:按GBT228.1-2010金属材料拉伸试验第1部分室温试验方法所述进行检测分析。Mechanical property test: According to GBT228.1-2010 Tensile Test of Metal Materials Part 1 Room temperature test method, the test and analysis are carried out.

表1实施例1~3和对比例1~2所述挤压材的力学性能指标Table 1 Mechanical properties index of the extruded materials described in Examples 1-3 and Comparative Examples 1-2

样品sample 抗拉强度/MPaTensile strength/MPa 屈服强度/MPaYield strength/MPa 延伸率/%Elongation/% 实施例1Example 1 452452 421421 11.5%11.5% 实施例2Example 2 468468 432432 10.1%10.1% 实施例3Example 3 472472 445445 10.3%10.3% 对比例1Comparative Example 1 406406 374374 10.8%10.8% 对比例2Comparative Example 2 419419 382382 12.0%12.0%

Claims (7)

1. A preparation method of high-strength Al-Mg-Si-Cu alloy is characterized by comprising the following steps: the high-strength Al-Mg-Si-Cu alloy comprises the following components in percentage by mass: 0.75-1.10 wt.%, Fe: 0.35 wt.%, Cu: 0.75-1.0 wt.%, Mn: 0.5-0.75 wt.%, Mg: 0.85-1.30 wt.%, Cr: less than or equal to 0.05 wt.%, Ti: not more than 0.10 wt.%, the balance being Al, the sum of the mass percentages of the components being 100%, and the mass ratio of (Mg + Si)/Cu being 2.2;
the preparation method of the high-strength Al-Mg-Si-Cu alloy comprises the following steps: mixing the raw materials, smelting, casting, homogenizing, hot extruding, quenching and aging to obtain the high-strength Al-Mg-Si-Cu alloy.
2. The method of claim 1, wherein: the smelting temperature is 720-760 ℃.
3. The method of claim 1, wherein: the casting adopts a semi-continuous casting mode, the casting temperature is 690-710 ℃, and the casting speed is 45-140 mm/min.
4. The method of claim 1, wherein: the homogenizing treatment process comprises the following steps: heating the cast ingot to 530-560 ℃, preserving heat for 1-10 h, then cooling to 400-450 ℃ at a speed of not more than 15 ℃/min, and then cooling to below 180 ℃ at a speed of not less than 30 ℃/min.
5. The method of claim 1, wherein: the technological parameters of the hot extrusion are as follows: heating the ingot after homogenizing treatment to 500-530 ℃, wherein the temperature of an extrusion cylinder is 430-500 ℃, and the extrusion speed of an extrusion material is 4-20 m/min.
6. The method of claim 1, wherein: the quenching temperature is not lower than 535 ℃, and the quenching cooling medium is water.
7. The method of claim 1, wherein: the temperature of the aging treatment is 100-200 ℃, and the time is 1-48 h.
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Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4589932A (en) * 1983-02-03 1986-05-20 Aluminum Company Of America Aluminum 6XXX alloy products of high strength and toughness having stable response to high temperature artificial aging treatments and method for producing
US5858134A (en) * 1994-10-25 1999-01-12 Pechiney Rhenalu Process for producing alsimgcu alloy products with improved resistance to intercrystalline corrosion
JP2004238657A (en) * 2003-02-04 2004-08-26 Kobe Steel Ltd Method of manufacturing aluminum alloy plate for outer panel
CN102337434A (en) * 2011-08-18 2012-02-01 苏州有色金属研究院有限公司 High-strength high-toughness Al-Mg-Si-Cu wrought aluminum alloy and preparation method thereof
JP2014074213A (en) * 2012-10-05 2014-04-24 Uacj Corp High strength aluminum alloy extruded material and method of producing the same
CN109371266A (en) * 2018-12-05 2019-02-22 中南大学 A kind of production method of high-strength corrosion-resistant weldable Al-Mg-Si alloy extrusion material
CN109468508A (en) * 2018-12-26 2019-03-15 东莞市铝美铝型材有限公司 A kind of aluminum alloy materials and preparation method thereof for electric automobile power battery pallet
CN111647780A (en) * 2020-07-21 2020-09-11 军材科技(天津)有限公司 High-strength 6-series aluminum alloy and preparation method and application thereof

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4589932A (en) * 1983-02-03 1986-05-20 Aluminum Company Of America Aluminum 6XXX alloy products of high strength and toughness having stable response to high temperature artificial aging treatments and method for producing
US5858134A (en) * 1994-10-25 1999-01-12 Pechiney Rhenalu Process for producing alsimgcu alloy products with improved resistance to intercrystalline corrosion
JP2004238657A (en) * 2003-02-04 2004-08-26 Kobe Steel Ltd Method of manufacturing aluminum alloy plate for outer panel
CN102337434A (en) * 2011-08-18 2012-02-01 苏州有色金属研究院有限公司 High-strength high-toughness Al-Mg-Si-Cu wrought aluminum alloy and preparation method thereof
JP2014074213A (en) * 2012-10-05 2014-04-24 Uacj Corp High strength aluminum alloy extruded material and method of producing the same
CN109371266A (en) * 2018-12-05 2019-02-22 中南大学 A kind of production method of high-strength corrosion-resistant weldable Al-Mg-Si alloy extrusion material
CN109468508A (en) * 2018-12-26 2019-03-15 东莞市铝美铝型材有限公司 A kind of aluminum alloy materials and preparation method thereof for electric automobile power battery pallet
CN111647780A (en) * 2020-07-21 2020-09-11 军材科技(天津)有限公司 High-strength 6-series aluminum alloy and preparation method and application thereof

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