CN116219234A - High-strength aluminum alloy section bar for energy storage device and preparation method thereof - Google Patents
High-strength aluminum alloy section bar for energy storage device and preparation method thereof Download PDFInfo
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- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 35
- 238000004146 energy storage Methods 0.000 title claims abstract description 15
- 238000002360 preparation method Methods 0.000 title abstract description 9
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 26
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 26
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 20
- 239000000956 alloy Substances 0.000 claims abstract description 20
- 238000010438 heat treatment Methods 0.000 claims abstract description 20
- 230000032683 aging Effects 0.000 claims abstract description 18
- 238000001125 extrusion Methods 0.000 claims abstract description 15
- 239000000126 substance Substances 0.000 claims abstract description 5
- 238000000034 method Methods 0.000 claims description 17
- 239000007789 gas Substances 0.000 claims description 9
- 230000008018 melting Effects 0.000 claims description 9
- 238000002844 melting Methods 0.000 claims description 9
- 238000005266 casting Methods 0.000 claims description 8
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 8
- 239000002893 slag Substances 0.000 claims description 8
- 229910052802 copper Inorganic materials 0.000 claims description 7
- 238000000265 homogenisation Methods 0.000 claims description 7
- 229910052710 silicon Inorganic materials 0.000 claims description 7
- 229910052804 chromium Inorganic materials 0.000 claims description 6
- 238000002485 combustion reaction Methods 0.000 claims description 6
- 238000001816 cooling Methods 0.000 claims description 6
- 229910052742 iron Inorganic materials 0.000 claims description 6
- 230000035882 stress Effects 0.000 claims description 6
- 229910052725 zinc Inorganic materials 0.000 claims description 6
- 238000004321 preservation Methods 0.000 claims description 5
- 229910052726 zirconium Inorganic materials 0.000 claims description 5
- 238000007872 degassing Methods 0.000 claims description 4
- 239000007788 liquid Substances 0.000 claims description 4
- 239000000155 melt Substances 0.000 claims description 4
- 239000000203 mixture Substances 0.000 claims description 4
- 239000003345 natural gas Substances 0.000 claims description 4
- 239000002994 raw material Substances 0.000 claims description 4
- 238000007670 refining Methods 0.000 claims description 4
- 229910052719 titanium Inorganic materials 0.000 claims description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 4
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 claims description 3
- 238000004880 explosion Methods 0.000 claims description 3
- 239000003546 flue gas Substances 0.000 claims description 3
- 230000002431 foraging effect Effects 0.000 claims description 3
- 229910052751 metal Inorganic materials 0.000 abstract description 9
- 239000002184 metal Substances 0.000 abstract description 6
- 238000005728 strengthening Methods 0.000 abstract description 5
- 239000013078 crystal Substances 0.000 abstract description 3
- 239000004615 ingredient Substances 0.000 abstract description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 10
- 230000007797 corrosion Effects 0.000 description 8
- 238000005260 corrosion Methods 0.000 description 8
- 239000010949 copper Substances 0.000 description 7
- 239000011777 magnesium Substances 0.000 description 7
- 239000011651 chromium Substances 0.000 description 6
- 239000011701 zinc Substances 0.000 description 6
- 239000011572 manganese Substances 0.000 description 5
- 238000001953 recrystallisation Methods 0.000 description 5
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 4
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 4
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 4
- 229910052749 magnesium Inorganic materials 0.000 description 4
- 229910052748 manganese Inorganic materials 0.000 description 4
- 239000010703 silicon Substances 0.000 description 4
- 239000010936 titanium Substances 0.000 description 4
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 3
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 3
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 150000002739 metals Chemical class 0.000 description 3
- 238000009864 tensile test Methods 0.000 description 3
- 238000003723 Smelting Methods 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
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- 238000005275 alloying Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 229910002056 binary alloy Inorganic materials 0.000 description 1
- 229910052729 chemical element Inorganic materials 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
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- 230000004927 fusion Effects 0.000 description 1
- 230000009931 harmful effect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000005551 mechanical alloying Methods 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 229910052755 nonmetal Inorganic materials 0.000 description 1
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- 238000005245 sintering Methods 0.000 description 1
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- 229910002058 ternary alloy Inorganic materials 0.000 description 1
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- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
- C22C21/08—Alloys based on aluminium with magnesium as the next major constituent with silicon
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- C21—METALLURGY OF IRON
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- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
- C22C1/026—Alloys based on aluminium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/047—Changing 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
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Abstract
Description
技术领域technical field
本发明属于合金型材和合金制备工艺技术领域,具体涉及一种储能高强铝合金型材及其制备方法。The invention belongs to the technical field of alloy profile and alloy preparation technology, and in particular relates to an energy storage high-strength aluminum alloy profile and a preparation method thereof.
背景技术Background technique
合金,是由两种或两种以上的金属与金属或非金属经一定方法所合成的具有金属特性的物质。一般通过熔合成均匀液体和凝固而得。根据组成元素的数目,可分为二元合金、三元合金和多元合金,常将两种或两种以上的金属元素或以金属为基添加其他非金属元素通过合金化工艺(熔炼、机械合金化、烧结、气相沉积等等)而形成的具有金属特性的金属材料叫做合金。但合金可能只含有一种金属元素,如钢。Alloys are substances with metallic properties that are synthesized by two or more metals and metals or nonmetals by a certain method. It is generally obtained by melting into a homogeneous liquid and solidifying. According to the number of constituent elements, it can be divided into binary alloys, ternary alloys and multi-component alloys. Usually, two or more metal elements or other non-metallic elements are added based on metals through alloying processes (smelting, mechanical alloying) Metal materials with metallic properties formed by melting, sintering, vapor deposition, etc.) are called alloys. But alloys may contain only one metallic element, such as steel.
现有技术中的缺陷:Defects in the prior art:
1、现有技术通过配比形成的合金,由于硅、铜、锰和铬含量的调配,在力学性能、耐腐蚀性、流动性、机械性能上,参数都不够均匀,影响合金的使用,对于锌、铝的用量多少,可能会产生缩孔,影响整体的强度。1. The alloy formed by proportioning in the prior art, due to the deployment of silicon, copper, manganese and chromium content, the parameters in terms of mechanical properties, corrosion resistance, fluidity and mechanical properties are not uniform enough, which affects the use of the alloy. For The amount of zinc and aluminum used may cause shrinkage and affect the overall strength.
2、现有制备工艺,使用单一温度加热,无温度梯度和等温挤压,导致生产的合金,金属流速不均匀,晶粒变化大,表面色质不均匀,力学性能偏差大,且单次失效工艺,导致其强度差,拉伸、抗压性能差,对储能装置的质量产品影响。2. The existing preparation process uses single temperature heating, no temperature gradient and isothermal extrusion, resulting in the production of alloys with uneven metal flow rate, large grain changes, uneven surface color quality, large deviation in mechanical properties, and single failure process, resulting in poor strength, poor tensile and compressive properties, which have an impact on the quality of energy storage devices.
附图说明Description of drawings
附图用来提供对本发明的进一步理解,并且构成说明书的一部分,与本发明的实施例一起用于解释本发明,并不构成对本发明的限制。The accompanying drawings are used to provide a further understanding of the present invention, and constitute a part of the description, and are used together with the embodiments of the present invention to explain the present invention, and do not constitute a limitation to the present invention.
图1为本发明实施例一拉伸实验报告曲线图;Fig. 1 is a curve diagram of a tensile test report of an embodiment of the present invention;
图2为本发明实施例二拉伸实验报告曲线图;Fig. 2 is the graph of report of tensile test of embodiment two of the present invention;
图3为本发明实施例三拉伸实验报告曲线图。Fig. 3 is a curve diagram of a tensile test report in Example 3 of the present invention.
具体实施方式Detailed ways
本发明的目的在于提供一种储能高强铝合金型材及其制备方法,以解决上述背景技术中提出的问题。The object of the present invention is to provide an energy storage high-strength aluminum alloy profile and a preparation method thereof, so as to solve the problems raised in the above-mentioned background technology.
为实现上述目的,本发明提供如下技术方案:一种储能高强铝合金型材及其制备方法,该铝合金化学成分按重量百分比计为Mg:1.0~1.05%,Si:0.70~0.75%,Cu:0.28~0.33%,Mn:0.05~0.1%,Cr:0.08~0.13%,Ti:0.03~0.08%,Fe:0.1~0.2%,Zn:0~0.05%,Zr:0.03~0.06%,余量为Al。In order to achieve the above object, the present invention provides the following technical solutions: an energy storage high-strength aluminum alloy profile and its preparation method, the chemical composition of the aluminum alloy is Mg: 1.0-1.05%, Si: 0.70-0.75%, Cu : 0.28~0.33%, Mn: 0.05~0.1%, Cr: 0.08~0.13%, Ti: 0.03~0.08%, Fe: 0.1~0.2%, Zn: 0~0.05%, Zr: 0.03~0.06%, balance for Al.
一种储能高强铝合金型材的制备方法,所述制备方法包括以下步骤:A method for preparing an energy-storage high-strength aluminum alloy profile, the method comprising the following steps:
步骤一:熔铸:将配好的原材料加入熔炼炉内熔化,并通过除气、除渣精炼手段将熔体内的夹渣、气体有效除去,将熔炼好的铝液通过深井铸造系统铸造成铝合金铸锭;Step 1: Melting and casting: Put the prepared raw materials into the melting furnace to melt, and effectively remove the slag inclusions and gases in the melt by means of degassing and slag removal refining, and cast the smelted aluminum liquid into aluminum through the deep well casting system alloy ingot;
步骤二:均匀化:将铝合金铸锭放置于565±5℃下进行均匀化处理,加热6-8h;Step 2: Homogenization: place the aluminum alloy ingot at 565±5°C for homogenization treatment, and heat for 6-8h;
步骤三:冷却:采用强水进行冷却,将其冷却至80±5℃;Step 3: Cooling: cooling with strong water to 80±5°C;
步骤四:挤压:将铝均匀化好的铝棒通过机械装置送入天然气铝棒加热炉内进行加热,铝棒炉内设置有四个加热区域,第一阶段设置为350℃,第二阶段设置为450℃,第三阶段设置为480℃,第四阶段设置为510℃,通过热锯装置将铸锭锯切成长度为800-1200mm的短铝棒再送入挤压机盛锭筒内进行挤压成型,挤出型材出口温度为520-540℃;Step 4: Extrusion: send the homogenized aluminum rods into the natural gas aluminum rod heating furnace for heating through a mechanical device. There are four heating areas in the aluminum rod furnace. The first stage is set at 350 °C, and the second stage The setting is 450°C, the third stage is set at 480°C, and the fourth stage is set at 510°C. The ingot is cut into short aluminum rods with a length of 800-1200mm by a hot saw device and then sent into the ingot barrel of the extruder. Extrusion molding, the outlet temperature of the extruded profile is 520-540°C;
步骤五:拉伸:按0.8%-1.2%的变形量对挤压型材进行拉伸矫直,并消除内应力;Step 5: Stretch: Stretch and straighten the extruded profile according to the deformation amount of 0.8%-1.2%, and eliminate the internal stress;
步骤六:人工时效:将拉伸之后的型材锯切装框,在8小时内送至时效炉内进行时效处理,时效分二级,一级时间温度为125±5℃,保温4h,二级时效温度160±5℃,保温2h,出炉后用轴流风机吹冷至室温即得铝合金型材成品。Step 6: Artificial aging: Cut the stretched profile into a frame and send it to the aging furnace for aging treatment within 8 hours. The aging is divided into two levels. The aging temperature is 160±5°C, heat preservation for 2 hours, and after being out of the furnace, use an axial fan to blow and cool to room temperature to obtain the finished aluminum alloy profile.
进一步而言,所述铝合金铸锭的加热方式通过热风加热方式,燃气送入热风发生炉内燃烧,燃烧生成的高温烟气和冷风混合后,由引风机通过管道送入料仓内对合金进行加热,燃气通过多组均匀布置在主管道内壁的送气管进行注入,且靠近送气管一端的位置处,通过风机进行匀速送入与混匀。其特点是受热均匀,不易烧结,且使内部各个位置的压力均匀相同,避免发生空爆。Furthermore, the aluminum alloy ingot is heated by hot air, and the gas is fed into the hot air furnace for combustion. After the high temperature flue gas generated by the combustion is mixed with the cold air, it is sent into the silo by the induced draft fan through the pipeline to cool the alloy. For heating, the gas is injected through multiple groups of air supply pipes evenly arranged on the inner wall of the main pipeline, and at a position close to one end of the air supply pipe, it is fed and mixed at a uniform speed by a fan. It is characterized by uniform heating, not easy to sinter, and makes the pressure of each position in the interior uniform and the same to avoid air explosion.
进一步而言,所述挤压机盛锭筒通过螺旋推送方式进行挤出与挤压,且该螺旋推送为多螺旋辊推送。Further, the extruding machine ingot barrel is extruded and extruded by means of spiral propulsion, and the spiral propulsion is multi-spiral roller propulsion.
本发明的有益技术效果:Beneficial technical effect of the present invention:
本发明一种储能装置用高强铝合金型材及其制备方法,通过改善配料成分,并采用梯度加热工艺,即将挤压前加热好的铝棒从前到后沿其轴线方向温度逐渐降低,形成温度梯度,实现等温挤压,使得挤压时金属流速均匀,晶粒变化小,表面色质均匀、力学性能偏差小,采用二次时效工艺,使合金强化项脱溶充分,型材的抗拉强度达到380MPa以上、屈服强度达到330MPa以上以上,大大提高了产品质量,从而改善整体储能装置的质量。The invention discloses a high-strength aluminum alloy profile for an energy storage device and a preparation method thereof. By improving the ingredients and adopting a gradient heating process, the temperature of the aluminum rod that has been heated before extrusion is gradually reduced from the front to the rear along the axis direction, forming a temperature Gradient, to achieve isothermal extrusion, so that the metal flow rate is uniform during extrusion, the grain change is small, the surface color is uniform, and the mechanical property deviation is small. The secondary aging process is adopted to make the alloy strengthening item fully desolvated, and the tensile strength of the profile reaches Above 380MPa, the yield strength reaches above 330MPa, which greatly improves the product quality, thereby improving the quality of the overall energy storage device.
具体实施方式Detailed ways
下面将结合本发明实施例,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the embodiments of the present invention. Obviously, the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
本发明提供一种基于多源网络空间的威胁情报采集融合系统技术方案:该铝合金化学成分按重量百分比计为Mg:1.0~1.05%,Si:0.70~0.75%,Cu:0.28~0.33%,Mn:0.05~0.1%,Cr:0.08~0.13%,Ti:0.03~0.08%,Fe:0.1~0.2%,Zn:0~0.05%,Zr:0.03~0.06%,余量为Al。The present invention provides a technical scheme of a threat information collection and fusion system based on multi-source network space: the chemical composition of the aluminum alloy is Mg: 1.0-1.05%, Si: 0.70-0.75%, Cu: 0.28-0.33%, Mn: 0.05-0.1%, Cr: 0.08-0.13%, Ti: 0.03-0.08%, Fe: 0.1-0.2%, Zn: 0-0.05%, Zr: 0.03-0.06%, and the balance is Al.
一种储能高强铝合金型材的制备方法,其特征在于:所述制备方法包括以下步骤:A method for preparing an energy-storage high-strength aluminum alloy profile, characterized in that the preparation method includes the following steps:
步骤一:熔铸:将配好的原材料加入熔炼炉内熔化,并通过除气、除渣精炼手段将熔体内的夹渣、气体有效除去,将熔炼好的铝液通过深井铸造系统铸造成铝合金铸锭;Step 1: Melting and casting: Put the prepared raw materials into the melting furnace to melt, and effectively remove the slag inclusions and gases in the melt by means of degassing and slag removal refining, and cast the smelted aluminum liquid into aluminum through the deep well casting system alloy ingot;
步骤二:均匀化:将铝合金铸锭放置于565±5℃下进行均匀化处理,加热6-8h;Step 2: Homogenization: place the aluminum alloy ingot at 565±5°C for homogenization treatment, and heat for 6-8h;
步骤三:冷却:采用强水进行冷却,将其冷却至80±5℃;Step 3: Cooling: cooling with strong water to 80±5°C;
步骤四:挤压:将铝均匀化好的铝棒通过机械装置送入天然气铝棒加热炉内进行加热,铝棒炉内设置有四个加热区域,第一阶段设置为350℃,第二阶段设置为450℃,第三阶段设置为480℃,第四阶段设置为510℃,通过热锯装置将铸锭锯切成长度为800-1200mm的短铝棒再送入挤压机盛锭筒内进行挤压成型,挤出型材出口温度为520-540℃;Step 4: Extrusion: send the homogenized aluminum rods into the natural gas aluminum rod heating furnace for heating through a mechanical device. There are four heating areas in the aluminum rod furnace. The first stage is set at 350 °C, and the second stage The setting is 450°C, the third stage is set at 480°C, and the fourth stage is set at 510°C. The ingot is cut into short aluminum rods with a length of 800-1200mm by a hot saw device and then sent into the ingot barrel of the extruder. Extrusion molding, the outlet temperature of the extruded profile is 520-540°C;
步骤五:拉伸:按0.8%-1.2%的变形量对挤压型材进行拉伸矫直,并消除内应力;Step 5: Stretch: Stretch and straighten the extruded profile according to the deformation amount of 0.8%-1.2%, and eliminate the internal stress;
步骤六:人工时效:将拉伸之后的型材锯切装框,在8小时内送至时效炉内进行时效处理,时效分二级,一级时间温度为125±5℃,保温4h,二级时效温度160±5℃,保温2h,出炉后用轴流风机吹冷至室温即得铝合金型材成品。Step 6: Artificial aging: Cut the stretched profile into a frame and send it to the aging furnace for aging treatment within 8 hours. The aging is divided into two levels. The aging temperature is 160±5°C, heat preservation for 2 hours, and after being out of the furnace, use an axial fan to blow and cool to room temperature to obtain the finished aluminum alloy profile.
在本实施例中,铝合金铸锭的加热方式通过热风加热方式,燃气送入热风发生炉内燃烧,燃烧生成的高温烟气和冷风混合后,由引风机通过管道送入料仓内对合金进行加热,燃气通过多组均匀布置在主管道内壁的送气管进行注入,且靠近送气管一端的位置处,通过风机进行匀速送入与混匀。其特点是受热均匀,不易烧结,且使内部各个位置的压力均匀相同,避免发生空爆。In this embodiment, the aluminum alloy ingot is heated by hot air, and the gas is fed into the hot air furnace for combustion. After the high-temperature flue gas generated by the combustion is mixed with cold air, it is sent into the silo by the induced draft fan through the pipeline to cool the alloy. For heating, the gas is injected through multiple groups of air supply pipes evenly arranged on the inner wall of the main pipeline, and at a position close to one end of the air supply pipe, it is fed and mixed at a uniform speed by a fan. It is characterized by uniform heating, not easy to sinter, and makes the pressure of each position in the interior uniform and the same to avoid air explosion.
在本实施例中,挤压机盛锭筒通过螺旋推送方式进行挤出与挤压,且该螺旋推送为多螺旋辊推送。In this embodiment, the ingot holder of the extruder is extruded and extruded by means of spiral push, and the spiral push is pushed by multiple helical rollers.
在本实施例中,本发明化学元素在铝合金中的作用如下:Mg:镁可以改善铝合金的机械性质和切削性,抗蚀性也好,并能和硅形成强化项提高力学性能。本发明镁含量控制在1.0~1.05%。Si:硅可以使铝合金流动良好,搞高抗蚀性、耐磨性和焊接性、并能和镁形成强化项提高力学性能。本发明硅含量控制在0.70~0.75%。In this embodiment, the role of the chemical elements of the present invention in the aluminum alloy is as follows: Mg: Magnesium can improve the mechanical properties and machinability of the aluminum alloy, as well as the corrosion resistance, and can form a strengthening item with silicon to improve the mechanical properties. The content of magnesium in the present invention is controlled at 1.0-1.05%. Si: Silicon can make aluminum alloy flow well, improve corrosion resistance, wear resistance and weldability, and can form strengthening items with magnesium to improve mechanical properties. The silicon content of the present invention is controlled at 0.70-0.75%.
Cu:铜可以改善铝合金的力学性能和切削性,但是耐腐蚀性和流动性变差,引起晶间腐蚀。本发明铜含量控制在0.28~0.33%。Mn:锰元素能提高再结晶温度,阻止铝合金再结晶过程,细化晶粒,减少铁的有害影响,但其添加量要根据合金中铁的含量来变化,否则会产生粗大的初晶、机械性能显著下降。本发明锰含量控制在0.05~0.1%。Cu: Copper can improve the mechanical properties and machinability of aluminum alloys, but the corrosion resistance and fluidity will deteriorate, causing intergranular corrosion. The copper content of the present invention is controlled at 0.28-0.33%. Mn: manganese element can increase the recrystallization temperature, prevent the recrystallization process of aluminum alloy, refine the grains, and reduce the harmful effects of iron, but its addition amount should be changed according to the content of iron in the alloy, otherwise coarse primary crystals, mechanical Performance drops significantly. The content of manganese in the present invention is controlled at 0.05-0.1%.
Cr:铬元素对合金有一定的强化作用,阻碍再结晶的形核和长大过程,,还能改善合金韧性和降低应力腐蚀开裂敏感性,抵消铜对抗蚀性的不利影响。本发明铬含量控制在0.08~0.13%Cr: Chromium has a certain strengthening effect on the alloy, hinders the nucleation and growth process of recrystallization, and can also improve the toughness of the alloy and reduce the sensitivity of stress corrosion cracking, offsetting the adverse effects of copper on corrosion resistance. The chromium content of the present invention is controlled at 0.08-0.13%
Ti:添加少量的钛元素可以细化铝合金铸造组织和焊缝组织的作用。本发明钛含量控制在0.03~0.08%。Ti: Adding a small amount of titanium element can refine the role of aluminum alloy casting structure and weld structure. The content of titanium in the present invention is controlled at 0.03-0.08%.
Fe:少量的铁元素可以减少铝合金的缩孔、细化晶料。本发明铁含量控制在0.1~0.2%。Fe: A small amount of iron element can reduce the shrinkage cavity of aluminum alloy and refine the crystal material. The iron content of the present invention is controlled at 0.1-0.2%.
Zn:锌元素和镁元素一起添加对铝合金产生明显的强化作用,但有应力耐腐倾向,而且添加量过多的话容易产生缩孔,应尽量降低。本发明锌含量控制在0~0.05%。Zn: Adding zinc and magnesium together can significantly strengthen the aluminum alloy, but it tends to resist stress and corrosion, and if the amount is too much, it is easy to produce shrinkage cavities, which should be reduced as much as possible. The zinc content of the present invention is controlled at 0-0.05%.
Zr:锆元素可阻碍再结晶过程,细化再结晶晶粒。本发明锆含量控制0.03~0.06%。Zr: Zirconium element can hinder the recrystallization process and refine the recrystallization grains. The content of zirconium in the present invention is controlled to be 0.03-0.06%.
实施例一:Embodiment one:
实施例二:Embodiment two:
实施例三:Embodiment three:
样件力学性能Sample Mechanical Properties
根据以上三种式样结果,其中实施例三强度最高,实施例二延伸率最佳。According to the results of the above three models, the third embodiment has the highest strength, and the second embodiment has the best elongation.
本发明的工作原理及使用流程:将配好的原材料按工艺要求加入熔炼炉内熔化,并通过除气、除渣精炼手段将熔体内的夹渣、气体有效除去,将熔炼好的铝液通过深井铸造系统铸造成铝合金铸锭,将铝合金铸锭放置于565±5℃下进行均匀化处理,加热6-8h,采用强水进行冷却,将其冷却至80±5℃,将铝均匀化好的铝棒通过机械装置送入天然气铝棒加热炉内进行加热,铝棒炉内设置有四个加热区域,第一阶段设置为350℃,第二阶段设置为450℃,第三阶段设置为480℃,第四阶段设置为510℃,通过热锯装置将铸锭锯切成长度为800-1200mm的短铝棒再送入挤压机盛锭筒内进行挤压成型,挤出型材出口温度为520-540℃,按0.8%-1.2%的变形量对挤压型材进行拉伸矫直,并消除内应力,将拉伸之后的型材锯切装框,在8小时内送至时效炉内进行时效处理,时效分二级,一级时间温度为125±5℃,保温4h,二级时效温度160±5℃,保温2h,出炉后用轴流风机吹冷至室温即得铝合金型材成品。The working principle and application process of the present invention: put the prepared raw materials into the smelting furnace for melting according to the technological requirements, and effectively remove the slag inclusions and gas in the melt by means of degassing and slag removal refining, and smelt the molten aluminum Cast aluminum alloy ingots through a deep well casting system, place the aluminum alloy ingots at 565±5°C for homogenization, heat for 6-8 hours, and cool them with strong water until they are cooled to 80±5°C. The homogenized aluminum rods are sent into the natural gas aluminum rod heating furnace for heating through mechanical devices. There are four heating zones in the aluminum rod furnace. The first stage is set at 350°C, the second stage is set at 450°C, and the third stage The setting is 480°C, and the fourth stage is set at 510°C. The ingot is sawed into short aluminum rods with a length of 800-1200mm by the hot saw device, and then sent into the ingot barrel of the extrusion machine for extrusion molding, and the extruded profile is exported The temperature is 520-540°C, and the extruded profiles are stretched and straightened according to the deformation of 0.8%-1.2%, and the internal stress is eliminated. The stretched profiles are sawed and framed, and sent to the aging furnace within 8 hours The aging treatment is carried out inside, and the aging is divided into two stages. The first-stage time temperature is 125±5°C, and the heat preservation is 4h. The second-stage aging temperature is 160±5°C, and the heat preservation is 2h. finished product.
以上为本发明较佳的实施方式,本发明所属领域的技术人员还能够对上述实施方式进行变更与修改,因此,本发明并不局限于上述的具体实施方式,凡是本领域技术人员在本发明的基础上所作的任何显而易见的改进、替换或变型均属于本发明的保护范围。The above are the preferred embodiments of the present invention, and those skilled in the art of the present invention can also change and modify the above-mentioned embodiments. Therefore, the present invention is not limited to the above-mentioned specific embodiments. Any obvious improvements, substitutions or variations made on the basis of the above-mentioned methods belong to the protection scope of the present invention.
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Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0860285A (en) * | 1994-06-16 | 1996-03-05 | Furukawa Electric Co Ltd:The | Bumper reinforcement made of aluminum alloy and its production |
CN201397013Y (en) * | 2009-01-19 | 2010-02-03 | 马鞍山钢铁股份有限公司 | Alloy roasting and drying device |
CN203333682U (en) * | 2013-06-26 | 2013-12-11 | 北京建龙重工集团有限公司 | Device for preheating coke by gradient utilization of residual heat in waste smoke gas of hot air furnace |
CN109943756A (en) * | 2018-12-19 | 2019-06-28 | 江阴东华铝材科技有限公司 | A kind of new energy car battery pallet high strength alumin ium alloy profile and preparation method thereof |
CN112952253A (en) * | 2021-01-27 | 2021-06-11 | 广西大学 | Processing technology of aluminum alloy battery tray of passenger vehicle |
-
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- 2022-12-15 CN CN202211610284.7A patent/CN116219234A/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0860285A (en) * | 1994-06-16 | 1996-03-05 | Furukawa Electric Co Ltd:The | Bumper reinforcement made of aluminum alloy and its production |
CN201397013Y (en) * | 2009-01-19 | 2010-02-03 | 马鞍山钢铁股份有限公司 | Alloy roasting and drying device |
CN203333682U (en) * | 2013-06-26 | 2013-12-11 | 北京建龙重工集团有限公司 | Device for preheating coke by gradient utilization of residual heat in waste smoke gas of hot air furnace |
CN109943756A (en) * | 2018-12-19 | 2019-06-28 | 江阴东华铝材科技有限公司 | A kind of new energy car battery pallet high strength alumin ium alloy profile and preparation method thereof |
CN112952253A (en) * | 2021-01-27 | 2021-06-11 | 广西大学 | Processing technology of aluminum alloy battery tray of passenger vehicle |
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