WO2022160457A1 - Heat treatment strengthening process for aluminum and magnesium as-cast alloy and application thereof - Google Patents

Heat treatment strengthening process for aluminum and magnesium as-cast alloy and application thereof Download PDF

Info

Publication number
WO2022160457A1
WO2022160457A1 PCT/CN2021/084380 CN2021084380W WO2022160457A1 WO 2022160457 A1 WO2022160457 A1 WO 2022160457A1 CN 2021084380 W CN2021084380 W CN 2021084380W WO 2022160457 A1 WO2022160457 A1 WO 2022160457A1
Authority
WO
WIPO (PCT)
Prior art keywords
alloy
aluminum
treatment
magnesium
temperature
Prior art date
Application number
PCT/CN2021/084380
Other languages
French (fr)
Chinese (zh)
Inventor
刘洪涛
齐志峰
晁延吉
周吉学
李涛
刘运腾
杨化冰
吴建华
王娜娜
李航
马百常
王西涛
Original Assignee
山东省科学院新材料研究所
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 山东省科学院新材料研究所 filed Critical 山东省科学院新材料研究所
Publication of WO2022160457A1 publication Critical patent/WO2022160457A1/en

Links

Images

Classifications

    • 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
    • C22F1/02Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working in inert or controlled atmosphere or vacuum
    • 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
    • C22F1/06Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of magnesium or alloys based thereon

Definitions

  • the invention relates to the technical field of heat treatment of non-ferrous metals, in particular to a heat treatment strengthening process of aluminum and magnesium as-cast alloys and its application.
  • Aluminum alloys and magnesium alloys are the lightest metal structural materials at present. They have the advantages of low density, high specific strength, and easy forming. They are widely used in aerospace, automotive electronics and other fields. In the automotive field, aluminum alloys and magnesium alloys can be used not only as instrument panel bases, seat frames, steering wheel shafts, gearbox casings, etc., but also in key parts such as engines and car chassis, and have broad application prospects in the automotive field.
  • alloy casting is an indispensable key link, and the quality of casting has a significant impact on the engineering parts of aluminum alloy and magnesium alloy. Due to the physical and chemical properties of aluminum alloys and magnesium alloys, casting defects are easily generated, resulting in reduced mechanical properties of castings. For example: (1) During the melting and casting process of aluminum alloys and magnesium alloys, entrainment is very likely to occur, and the buoyancy of the involved nitrogen bubbles and hydrogen bubbles is small, which makes it difficult for a large amount of hydrogen and nitrogen to escape. The form remains in the casting, and the pores will become the source of crack propagation during the service of the casting; (2) The aluminum alloy and magnesium alloy will shrink in volume during the casting process. (3) During the casting process of aluminum alloy and magnesium alloy, due to the inconsistent solidification time of different parts, large residual thermal stress will be generated, and even hot cracking will occur. This problem is especially obvious for castings with complex structures;
  • the present invention proposes a heat treatment strengthening process for aluminum and magnesium as-cast alloys and its application.
  • This process is suitable for ageing-strengthened aluminum alloys or magnesium alloys.
  • One ultra-low temperature treatment, followed by warm isostatic pressing at the alloy solution temperature, followed by a second ultra-low temperature treatment, and finally aging strengthening treatment, can greatly improve the mechanical properties of aluminum and magnesium alloy castings.
  • a first aspect of the present invention provides a heat treatment strengthening process of aluminum and magnesium as-cast alloys, which specifically includes:
  • the alloy material is taken out from the aging furnace and air-cooled;
  • the second aspect of the present invention provides the application of the above-mentioned heat treatment strengthening process of aluminum and magnesium as-cast alloys in the preparation of as-cast alloys.
  • the present invention discloses a heat treatment strengthening process for aluminum and magnesium as-cast alloys.
  • the aluminum alloy and magnesium alloy are subjected to multiple processes such as primary ultra-low temperature treatment, warm isostatic pressing solution treatment, secondary ultra-low temperature treatment and aging treatment.
  • the combined treatment greatly reduces the casting defects such as pores and shrinkage porosity in the aluminum alloy structure, the residual stress, and the precipitation strengthening phase distribution is more dispersed, and the aging strengthening effect is more ideal.
  • the strength and elongation of aluminum and magnesium as-cast alloys are obvious. improve.
  • the first ultra-low temperature treatment is mainly based on the volume shrinkage effect, which reduces the atomic spacing, shrinks the lattice, reduces the size of hole defects, and even closes some tiny voids directly, laying the foundation for the next warm isostatic pressing treatment;
  • the warm isostatic pressing treatment causes plastic flow diffusion inside the casting, bonding and bridging of the microstructure holes, and the as-cast structure is more uniform and dense, and the space occupied by defects such as pores and shrinkage porosity is extremely limited on the macroscopic level, so it will not change.
  • the size or shape of the casting is more uniform and dense, and the space occupied by defects such as pores and shrinkage porosity is extremely limited on the macroscopic level, so it will not change.
  • the size or shape of the casting is sized or shape of the casting.
  • the second ultra-low temperature treatment There are two purposes of the second ultra-low temperature treatment. One is to generate a large internal stress inside the material, which induces a large number of dislocations and sub-crystals. The strength and toughness of the alloy are improved. Second, a large number of supersaturated point defects (vacancies) can be obtained at ultra-low temperature. The interaction between vacancies and solute atoms makes the next aging precipitate more dispersed and the volume fraction increases.
  • the aging strengthening is carried out on the basis of the second ultra-low temperature treatment. Since there are more dislocations and vacancies in the microstructure, it is more conducive to the diffusion of solute atoms, and the formed strengthening phase is more dispersed, and the aging strengthening effect is more effective. ideal.
  • Figure 1 is a comparison of the tensile properties of the ZL109 as-cast aluminum alloy in Example 1(a) after the treatment of the present invention and the conventional heat treatment in Comparative Example 1(b).
  • Figure 2 is a comparison of the tensile properties of the AZ91 as-cast magnesium alloy in Example 2(a) after the treatment of the present invention and the conventional heat treatment in Comparative Example 2(b).
  • the present invention proposes a heat treatment strengthening process for aluminum and magnesium as-cast alloys, which specifically includes:
  • the alloy material is taken out from the aging furnace and air-cooled.
  • the temperature of the cavity is controlled by pumping liquid nitrogen, the temperature control accuracy is ⁇ 1°C, and the cooling rate is controlled at 10-20°C/min, So that the cavity temperature can be adjusted in the range of room temperature to -190 °C;
  • the temperature range of the first ultra-low temperature treatment is -120 to -180°C, and the ultra-low temperature treatment time is determined according to the type of alloy. , the treatment time is 5-7h, and when aluminum alloy is used, the treatment time is 6-8h.
  • the inert protective gas is argon or nitrogen, and the vacuum degree must be evacuated to below 10 mPa before introducing the inert protective gas;
  • the static gas pressure in the step (2), in the process of filling the cavity with the inert protective gas, is first controlled at about 70 MPa, and the required solid solution temperature of the alloy is equal to After stabilization, adjust the static pressure to 100-200MPa;
  • the time of the warm isostatic pressing is determined according to the type of alloy.
  • the processing time is 9-10h, and when aluminum is used When alloying, the treatment time is 4-5h.
  • step (2) the water temperature does not exceed 65°C, and the transfer time does not exceed 20s;
  • the cooling rate is controlled at 50-60°C/min
  • the temperature of the second ultra-low temperature treatment is -130--190°C
  • the treatment time is based on the alloy.
  • the treatment time is 15-17h
  • the treatment time is 13-15h.
  • the aging treatment process of the alloy is reasonably determined according to the corresponding national standards of different grades or relevant literature.
  • the second aspect of the present invention provides the application of the above-mentioned heat treatment strengthening process of aluminum and magnesium as-cast alloys in the preparation of as-cast alloys.
  • the alloy material is taken out from the aging furnace and air-cooled;
  • the alloy material is taken out from the aging furnace and air-cooled;

Landscapes

  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Powder Metallurgy (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)

Abstract

A heat treatment strengthening process for an aluminum and magnesium as-cast alloy and an application thereof. The aluminum alloy and the magnesium alloy are subjected to multi-process combined treatment such as primary ultralow-temperature treatment, warm isostatic pressing solution treatment, secondary ultralow-temperature treatment, and aging treatment; casting defects such as air holes and shrinkage porosity in an aluminum alloy structure are greatly reduced, residual stress and precipitation strengthening phase distribution is more dispersed, and the aging strengthening effect is more ideal, the strength and elongation of the aluminum and magnesium as-cast alloy are obviously improved. The process steps are simple, the process parameters of warm isostatic pressing and ultralow-temperature treatment can be adjusted according to different as-cast alloy types, the problems of air holes, shrinkage porosity, residual stress and the like in the casting process of the as-cast alloy are effectively solved, and the microstructure and mechanical properties of the aluminum and magnesium as-cast alloy are greatly improved. Moreover, the process steps are simple, the process parameters of warm isostatic pressing and ultralow-temperature treatment can be adjusted according to different as-cast alloy types, the problems of air holes, shrinkage porosity, residual stress and the like in the casting process of the as-cast alloy are effectively solved, and the microstructure and mechanical properties of the aluminum and magnesium as-cast alloy are greatly improved. The heat treatment strengthening process has important significance for expanding the engineering application of the aluminum and magnesium as-cast alloy.

Description

一种铝、镁铸态合金的热处理强化工艺及其应用A kind of heat treatment strengthening process of aluminum and magnesium as-cast alloy and its application 技术领域technical field
本发明涉及有色金属热处理技术领域,具体涉及一种铝、镁铸态合金的热处理强化工艺及其应用。The invention relates to the technical field of heat treatment of non-ferrous metals, in particular to a heat treatment strengthening process of aluminum and magnesium as-cast alloys and its application.
背景技术Background technique
公开该背景技术部分的信息仅仅旨在增加对本发明的总体背景的理解,而不必然被视为承认或以任何形式暗示该信息构成已经成为本领域一般技术人员所公知的现有技术。The disclosure of information in this Background section is only for enhancement of understanding of the general background of the invention and should not necessarily be taken as an acknowledgement or any form of suggestion that this information forms the prior art already known to a person of ordinary skill in the art.
能源短缺和环境污染是当今世界的突出问题,减轻自身重量成为汽车、航空航天等领域减少环境污染和节约能源的有效方法。据统计汽车质量每降低100千克,油耗就可减少0.7升。在航空航天器中,结构件重量的降低带来燃油费用的减少,则是汽车工业的100倍。铝合金和镁合金是目前最轻的金属结构材料,具有密度小、比强度高、易于成形等优点,在航空航天、汽车电子等领域应用广泛。在汽车领域,铝合金和镁合金除可用作仪表盘基座、座位框架、方向盘轴、变速箱外壳等外,还可用于发动机、汽车底盘等关键部位,在汽车领域具有广阔的应用前景。Energy shortage and environmental pollution are prominent problems in today's world. Reducing one's own weight has become an effective way to reduce environmental pollution and save energy in the fields of automobiles, aerospace and other fields. According to statistics, the fuel consumption can be reduced by 0.7 liters for every 100 kg reduction in the mass of the car. In aerospace vehicles, the reduction in structural weight reduces fuel costs by a factor of 100 compared to the automotive industry. Aluminum alloys and magnesium alloys are the lightest metal structural materials at present. They have the advantages of low density, high specific strength, and easy forming. They are widely used in aerospace, automotive electronics and other fields. In the automotive field, aluminum alloys and magnesium alloys can be used not only as instrument panel bases, seat frames, steering wheel shafts, gearbox casings, etc., but also in key parts such as engines and car chassis, and have broad application prospects in the automotive field.
在铝合计和镁合金工程化应用过程中,合金熔铸是不可或缺的关键环节,铸件的质量对铝合金和镁合金的工程化零部件具有显著影响。由于铝合金和镁合金自身的物理化学性质,极易产生铸造缺陷,导致铸件的机械性能降低。譬如:(1)铝合金和镁合金在熔铸过程中,都非常容易发生卷气,卷入的氮气泡和氢气泡受到的浮力较小,致使大量的氢和氮逸出困难,最终以气孔的形式残留 在铸件中,气孔将成为铸件服役过程中的裂纹扩展源;(2)铝合金和镁合金在铸造过程中会发生体积收缩,若不能及时补缩,极易形成缩孔、缩松;(3)铝合金和镁合金在铸造过程中,由于不同部位凝固时间不一致,会产生较大残余热应力,甚至产生热裂,这个问题对于结构复杂的铸件尤其明显;In the process of aluminum alloy and magnesium alloy engineering application, alloy casting is an indispensable key link, and the quality of casting has a significant impact on the engineering parts of aluminum alloy and magnesium alloy. Due to the physical and chemical properties of aluminum alloys and magnesium alloys, casting defects are easily generated, resulting in reduced mechanical properties of castings. For example: (1) During the melting and casting process of aluminum alloys and magnesium alloys, entrainment is very likely to occur, and the buoyancy of the involved nitrogen bubbles and hydrogen bubbles is small, which makes it difficult for a large amount of hydrogen and nitrogen to escape. The form remains in the casting, and the pores will become the source of crack propagation during the service of the casting; (2) The aluminum alloy and magnesium alloy will shrink in volume during the casting process. (3) During the casting process of aluminum alloy and magnesium alloy, due to the inconsistent solidification time of different parts, large residual thermal stress will be generated, and even hot cracking will occur. This problem is especially obvious for castings with complex structures;
由上可知,由于铝合金和镁合金的物理特性与钢铁等金属材料差别较大,使得其熔铸过程中气孔、缩松和残余应力等问题非常突出,铸态组织极易产生各种缺陷,导致铸件性能降低。从保证铸件的完整性、制造工艺的合理性以及使用过程的可靠性等角度来看,这种由气孔、缩松缺陷和残余应力引发的工程组件变形断裂、失效等,已严重限制了铝合金和镁合金铸件的工程化应用。因此,如何有效消除各种铸造组织缺陷,有力增强铝合金和镁合金的铸件质量,提高其服役性能,已成为制约铝合金和镁合金工程化应用的瓶颈技术和急待解决的关键技术之一。It can be seen from the above that the physical properties of aluminum alloys and magnesium alloys are quite different from those of metal materials such as steel, which makes the problems of pores, shrinkage porosity and residual stress very prominent during the casting process. Casting performance is reduced. From the perspective of ensuring the integrity of the casting, the rationality of the manufacturing process, and the reliability of the use process, the deformation, fracture, and failure of engineering components caused by pores, shrinkage defects and residual stress have seriously limited aluminum alloys. and engineering application of magnesium alloy castings. Therefore, how to effectively eliminate various casting microstructure defects, effectively enhance the casting quality of aluminum alloys and magnesium alloys, and improve their service performance has become one of the bottleneck technologies that restrict the engineering application of aluminum alloys and magnesium alloys and one of the key technologies to be solved urgently. .
发明内容SUMMARY OF THE INVENTION
为了解决现有技术的不足,本发明提出一种铝、镁铸态合金的热处理强化工艺及其应用,本工艺适用于可时效强化的铝合金或镁合金,对铝合金或镁合金铸件先进行一次超低温处理,再在合金固溶温度下进行温等静压处理,之后再进行二次超低温处理,最后进行时效强化处理,可大幅提升铝、镁合金铸件的机械性能。In order to solve the deficiencies of the prior art, the present invention proposes a heat treatment strengthening process for aluminum and magnesium as-cast alloys and its application. This process is suitable for ageing-strengthened aluminum alloys or magnesium alloys. One ultra-low temperature treatment, followed by warm isostatic pressing at the alloy solution temperature, followed by a second ultra-low temperature treatment, and finally aging strengthening treatment, can greatly improve the mechanical properties of aluminum and magnesium alloy castings.
为实现上述目的,本发明第一方面提供一种铝、镁铸态合金的热处理强化工艺,具体包括:In order to achieve the above object, a first aspect of the present invention provides a heat treatment strengthening process of aluminum and magnesium as-cast alloys, which specifically includes:
(1)将需要处理的铝或镁等轻质合金放入密闭腔体中,将腔体环境温度逐渐冷却至超低温,进行第一次超低温处理;(1) Put the light alloys such as aluminum or magnesium to be treated into a closed cavity, gradually cool the ambient temperature of the cavity to an ultra-low temperature, and perform the first ultra-low temperature treatment;
(2)铝合金或镁合金第一次超低温处理完成后,将温度缓慢恢复至室温, 再放入温等静压设备中,在合金材料固溶温度下通入惰性保护气体进行气体加压热处理;温等静压处理过程结束后,铝合金或镁合金随炉恢复至室温,释放惰性保护气体,降低腔体静压力,逐渐恢复至常压;静气压力降到常压后,将铝合金或镁合金快速转移浸入水中,直至其彻底冷却;(2) After the first ultra-low temperature treatment of the aluminum alloy or magnesium alloy is completed, the temperature is slowly returned to room temperature, and then placed in a warm isostatic pressing equipment, and an inert protective gas is introduced at the solid solution temperature of the alloy material for gas pressure heat treatment ; After the warm isostatic pressing process, the aluminum alloy or magnesium alloy will return to room temperature with the furnace, release the inert protective gas, reduce the static pressure of the cavity, and gradually return to normal pressure; after the static gas pressure drops to normal pressure, the aluminum alloy Or the magnesium alloy is quickly transferred and immersed in water until it is completely cooled;
(3)铝合金或镁合金温等静压处理完成后,将腔体环境温度逐渐冷却,进行第二次超低温处理;(3) After the temperature isostatic pressing of the aluminum alloy or magnesium alloy is completed, the ambient temperature of the cavity is gradually cooled, and the second ultra-low temperature treatment is performed;
(4)铝合金或镁合金二次超低温处理结束后,将铝合金或镁合金放入时效炉中进行时效处理;(4) After the secondary ultra-low temperature treatment of aluminum alloy or magnesium alloy is completed, the aluminum alloy or magnesium alloy is put into an aging furnace for aging treatment;
(5)时效过程结束后,将合金材料从时效炉中取出,空冷;(5) After the aging process is finished, the alloy material is taken out from the aging furnace and air-cooled;
本发明第二方面提供上述铝、镁铸态合金的热处理强化工艺在铸态合金制备中的应用。The second aspect of the present invention provides the application of the above-mentioned heat treatment strengthening process of aluminum and magnesium as-cast alloys in the preparation of as-cast alloys.
本发明的一个或多个实施方式至少具有以下有益效果:One or more embodiments of the present invention have at least the following beneficial effects:
(1)本发明公开了一种铝、镁铸态合金的热处理强化工艺,通过对铝合金、镁合金进行一次超低温处理、温等静压固溶处理、二次超低温处理及时效处理等多工艺组合处理,大幅消减了铝合金组织中的气孔、缩松等铸造缺陷、残余应力、析出强化相分布更为弥散,时效强化效果更为理想,铝、镁铸态合金的强度与延伸率均明显提高。(1) The present invention discloses a heat treatment strengthening process for aluminum and magnesium as-cast alloys. The aluminum alloy and magnesium alloy are subjected to multiple processes such as primary ultra-low temperature treatment, warm isostatic pressing solution treatment, secondary ultra-low temperature treatment and aging treatment. The combined treatment greatly reduces the casting defects such as pores and shrinkage porosity in the aluminum alloy structure, the residual stress, and the precipitation strengthening phase distribution is more dispersed, and the aging strengthening effect is more ideal. The strength and elongation of aluminum and magnesium as-cast alloys are obvious. improve.
其中,第一次超低温处理主要基于体积收缩效应,使得原子间距减少,晶格产生收缩,孔洞缺陷尺寸减小,部分微小空隙甚至直接弥合,为下一步的温等静压处理打下基础;Among them, the first ultra-low temperature treatment is mainly based on the volume shrinkage effect, which reduces the atomic spacing, shrinks the lattice, reduces the size of hole defects, and even closes some tiny voids directly, laying the foundation for the next warm isostatic pressing treatment;
温等静压处理使得铸件内部发生塑性流动扩散,微观组织孔洞发生粘结弥合,铸态组织更加均匀、致密,且由于气孔、缩松等缺陷所占空间在宏观上极为有限,故不会改变铸件的尺寸或外形。The warm isostatic pressing treatment causes plastic flow diffusion inside the casting, bonding and bridging of the microstructure holes, and the as-cast structure is more uniform and dense, and the space occupied by defects such as pores and shrinkage porosity is extremely limited on the macroscopic level, so it will not change. The size or shape of the casting.
第二次超低温处理的目的有两个,一是在材料内部产生很大的内应力,诱发大量位错和亚晶,在内应力作用下,位错发生增殖,通过自身的像话缠绕和钉扎提高了合金的强韧性,二是在超低温下还可获得大量的过饱和点缺陷(空位),空位与溶质原子相互作用,使得下一步的时效析出相更加的弥散,体积分数增加。There are two purposes of the second ultra-low temperature treatment. One is to generate a large internal stress inside the material, which induces a large number of dislocations and sub-crystals. The strength and toughness of the alloy are improved. Second, a large number of supersaturated point defects (vacancies) can be obtained at ultra-low temperature. The interaction between vacancies and solute atoms makes the next aging precipitate more dispersed and the volume fraction increases.
时效强化是在第二次超低温处理的基础上进行,由于微观组织内部具有了更多的,位错和空位,更加有利于溶质原子的扩散,形成的强化相也更加的弥散,时效强化效果更加的理想。The aging strengthening is carried out on the basis of the second ultra-low temperature treatment. Since there are more dislocations and vacancies in the microstructure, it is more conducive to the diffusion of solute atoms, and the formed strengthening phase is more dispersed, and the aging strengthening effect is more effective. ideal.
(2)本发明步骤简单,可根据不同的铸态合金类型调整温等静压和超低温处理的工艺参数,有效解决铸态合金熔铸过程中气孔、缩松和残余应力等问题,大幅提高铝、镁铸态合金的微观组织和力学性能,对于扩大铝、镁铸态合金的工程应用具有重要的意义。(2) The steps of the present invention are simple, and the process parameters of temperature isostatic pressing and ultra-low temperature treatment can be adjusted according to different as-cast alloy types, effectively solving the problems of pores, shrinkage porosity and residual stress during the casting process of the as-cast alloy, greatly improving aluminum, The microstructure and mechanical properties of magnesium as-cast alloys are of great significance for expanding the engineering applications of aluminum and magnesium as-cast alloys.
附图说明Description of drawings
构成本发明的一部分的说明书附图用来提供对本发明的进一步理解,本发明的示意性实施例及其说明用于解释本发明,并不构成对本发明的不当限定。The accompanying drawings forming a part of the present invention are used to provide further understanding of the present invention, and the exemplary embodiments of the present invention and their descriptions are used to explain the present invention, and do not constitute an improper limitation of the present invention.
图1为实施例1(a)中ZL109铸态铝合金经本发明处理与对比例1(b)中经常规热处理后的拉伸性能对比。Figure 1 is a comparison of the tensile properties of the ZL109 as-cast aluminum alloy in Example 1(a) after the treatment of the present invention and the conventional heat treatment in Comparative Example 1(b).
图2为实施例2(a)中AZ91铸态镁合金经本发明处理与对比例2(b)中经常规热处理后的拉伸性能对比。Figure 2 is a comparison of the tensile properties of the AZ91 as-cast magnesium alloy in Example 2(a) after the treatment of the present invention and the conventional heat treatment in Comparative Example 2(b).
具体实施方式Detailed ways
应该指出,以下详细说明都是示例性的,旨在对本发明提供进一步的说明。除非另有指明,本文使用的所有技术和科学术语具有与本发明所属技术领域的普通技术人员通常理解的相同含义。It should be noted that the following detailed description is exemplary and intended to provide further explanation of the invention. Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs.
需要注意的是,这里所使用的术语仅是为了描述具体实施方式,而非意图限制根据本发明的示例性实施方式。如在这里所使用的,除非上下文另外明确指出,否则单数形式也意图包括复数形式,此外,还应当理解的是,当在本说明书中使用术语“包含”和/或“包括”时,其指明存在特征、步骤、操作、器件、组件和/或它们的组合。It should be noted that the terminology used herein is for the purpose of describing specific embodiments only, and is not intended to limit the exemplary embodiments according to the present invention. As used herein, unless the context clearly dictates otherwise, the singular is intended to include the plural as well, furthermore, it is to be understood that when the terms "comprising" and/or "including" are used in this specification, it indicates that There are features, steps, operations, devices, components and/or combinations thereof.
正如背景技术所介绍的,现有技术中铝、镁铸态合金熔铸过程中气孔、缩松和残余应力等问题非常突出,铸态组织极易产生各种缺陷,导致铸件性能降低,为了解决如上的技术问题,本发明提出了一种铝、镁铸态合金的热处理强化工艺,具体包括:As described in the background art, in the prior art, problems such as pores, shrinkage porosity and residual stress during the melting and casting of aluminum and magnesium as-cast alloys are very prominent. The present invention proposes a heat treatment strengthening process for aluminum and magnesium as-cast alloys, which specifically includes:
(1)将需要处理的铝或镁等轻质合金放入密闭腔体中,将腔体环境温度逐渐冷却至超低温,进行第一次超低温处理;(1) Put the light alloys such as aluminum or magnesium to be treated into a closed cavity, gradually cool the ambient temperature of the cavity to an ultra-low temperature, and perform the first ultra-low temperature treatment;
(2)铝合金或镁合金第一次超低温处理完成后,将温度缓慢恢复至室温,再放入温等静压设备中,在合金材料固溶温度下通入惰性保护气体进行气体加压热处理;温等静压处理过程结束后,铝合金或镁合金随炉恢复至室温,释放惰性保护气体,降低腔体静压力,逐渐恢复至常压;静气压力降到常压后,将铝合金或镁合金快速转移浸入水中,直至其彻底冷却;(2) After the first ultra-low temperature treatment of the aluminum alloy or magnesium alloy is completed, the temperature is slowly returned to room temperature, and then placed in a warm isostatic pressing equipment, and an inert protective gas is introduced at the solid solution temperature of the alloy material for gas pressure heat treatment ; After the warm isostatic pressing process, the aluminum alloy or magnesium alloy will return to room temperature with the furnace, release the inert protective gas, reduce the static pressure of the cavity, and gradually return to normal pressure; after the static gas pressure drops to normal pressure, the aluminum alloy Or the magnesium alloy is quickly transferred and immersed in water until it is completely cooled;
(3)铝合金或镁合金温等静压处理完成后,将腔体环境温度逐渐冷却至合金所需超低温,进行第二次超低温处理;(3) After the temperature isostatic pressing of the aluminum alloy or magnesium alloy is completed, the ambient temperature of the cavity is gradually cooled to the ultra-low temperature required by the alloy, and the second ultra-low temperature treatment is performed;
(4)铝合金或镁合金二次超低温处理结束后,将铝合金或镁合金放入时效炉中进行时效处理;(4) After the secondary ultra-low temperature treatment of aluminum alloy or magnesium alloy is completed, the aluminum alloy or magnesium alloy is put into an aging furnace for aging treatment;
(5)时效过程结束后,将合金材料从时效炉中取出,空冷。(5) After the aging process is completed, the alloy material is taken out from the aging furnace and air-cooled.
在本发明的一个或多个实施方式中,所述步骤(1)中,通过泵入液氮来控制腔体温度,温控精度为±1℃,降温速率控制在10~20℃/min,使得腔体温 度可在室温至-190℃范围内进行调节;In one or more embodiments of the present invention, in the step (1), the temperature of the cavity is controlled by pumping liquid nitrogen, the temperature control accuracy is ±1°C, and the cooling rate is controlled at 10-20°C/min, So that the cavity temperature can be adjusted in the range of room temperature to -190 ℃;
在本发明的一个或多个实施方式中,所述步骤(1)中,第一次超低温处理的温度范围为-120~-180℃,超低温处理时间根据合金的类型来确定,当采用镁合金时,处理时间为5-7h,当采用铝合金时,处理时间为6-8h。In one or more embodiments of the present invention, in the step (1), the temperature range of the first ultra-low temperature treatment is -120 to -180°C, and the ultra-low temperature treatment time is determined according to the type of alloy. , the treatment time is 5-7h, and when aluminum alloy is used, the treatment time is 6-8h.
在本发明的一个或多个实施方式中,所述步骤(2)中,惰性保护气体为氩气或氮气,在通入惰性保护气体之前要先将真空度抽至10mPa以下;In one or more embodiments of the present invention, in the step (2), the inert protective gas is argon or nitrogen, and the vacuum degree must be evacuated to below 10 mPa before introducing the inert protective gas;
在本发明的一个或多个实施方式中,所述步骤(2)中,在往腔体充入惰性保护气体的过程中,先将静气压力控制在70MPa左右,等合金所需固溶温度稳定后,再将静气压力调节至100~200MPa;In one or more embodiments of the present invention, in the step (2), in the process of filling the cavity with the inert protective gas, the static gas pressure is first controlled at about 70 MPa, and the required solid solution temperature of the alloy is equal to After stabilization, adjust the static pressure to 100-200MPa;
在本发明的一个或多个实施方式中,所述步骤(2)中,温等静压处理的时间根据合金的类型来确定,当采用镁合金时,处理时间为9-10h,当采用铝合金时,处理时间为4-5h。In one or more embodiments of the present invention, in the step (2), the time of the warm isostatic pressing is determined according to the type of alloy. When magnesium alloy is used, the processing time is 9-10h, and when aluminum is used When alloying, the treatment time is 4-5h.
在本发明的一个或多个实施方式中,所属步骤(2)中,水温不超过65℃,转移时间不超过20s;In one or more embodiments of the present invention, in step (2), the water temperature does not exceed 65°C, and the transfer time does not exceed 20s;
在本发明的一个或多个实施方式中,所述步骤(3)中,降温速率控制在50~60℃/min,第二次超低温处理温度为-130~-190℃,处理的时间根据合金的类型来确定,当采用镁合金时,处理时间为15-17h,当采用铝合金时,处理时间为13-15h。In one or more embodiments of the present invention, in the step (3), the cooling rate is controlled at 50-60°C/min, the temperature of the second ultra-low temperature treatment is -130--190°C, and the treatment time is based on the alloy. To determine the type, when using magnesium alloy, the treatment time is 15-17h, when using aluminum alloy, the treatment time is 13-15h.
所述步骤(4)中,合金的时效处理工艺,依据不同牌号相应的国家标准或相关文献合理确定。In the step (4), the aging treatment process of the alloy is reasonably determined according to the corresponding national standards of different grades or relevant literature.
本发明第二方面提供上述铝、镁铸态合金的热处理强化工艺在铸态合金制备中的应用。The second aspect of the present invention provides the application of the above-mentioned heat treatment strengthening process of aluminum and magnesium as-cast alloys in the preparation of as-cast alloys.
为了使得本领域技术人员能够更加清楚地了解本发明的技术方案,以下将 结合具体的实施例详细说明本发明的技术方案。In order to enable those skilled in the art to understand the technical solutions of the present invention more clearly, the technical solutions of the present invention will be described in detail below in conjunction with specific embodiments.
实施例1Example 1
利用本发明的热处理方法对ZL109铸态铝合金进行强化处理:Utilize the heat treatment method of the present invention to carry out strengthening treatment to ZL109 as-cast aluminum alloy:
(1)将ZL109铝合金放入密闭腔体中,通入液氮,逐渐冷却至-165℃,降温速率为20℃/min,处理时间7h;(1) Put the ZL109 aluminum alloy into a closed cavity, pass in liquid nitrogen, and gradually cool to -165°C, the cooling rate is 20°C/min, and the treatment time is 7h;
(2)超低温处理结束后,将温度缓慢恢复至室温,将ZL109铸态铝合金放入温等静压设备中,通入氮气加压,先将静气压力控制在70MPa,等处理温度稳定到495℃,将静气压力调至150MPa,处理时间4h;温等静压处理过程结束后,ZL109铝合金随炉恢复至室温,释放保护气体,降低腔体静压力,在此过程中温度保持不变;静气压力降到常压后,将ZL109铝合金快速转移浸入65℃的水中,转移时间不超过20s;(2) After the ultra-low temperature treatment is completed, the temperature is slowly returned to room temperature, the ZL109 as-cast aluminum alloy is put into the warm isostatic pressing equipment, and nitrogen is introduced to pressurize. 495 ℃, the static gas pressure was adjusted to 150MPa, and the treatment time was 4h; after the warm isostatic pressing process, the ZL109 aluminum alloy was returned to room temperature with the furnace, and the protective gas was released to reduce the static pressure of the cavity. During this process, the temperature remained constant. After the static pressure drops to normal pressure, the ZL109 aluminum alloy is quickly transferred and immersed in water at 65 °C, and the transfer time does not exceed 20s;
(3)ZL109铝合金温等静压处理完成后,进行二次超低温处理,将腔体环境温度以50℃/min的速度,快速冷却至-180℃,处理10h;(3) After the ZL109 aluminum alloy temperature isostatic pressing treatment is completed, a second ultra-low temperature treatment is performed, and the ambient temperature of the cavity is rapidly cooled to -180 °C at a speed of 50 °C/min, and treated for 10 hours;
(4)二次超低温处理结束后,将ZL109铝合金放入时效炉中,时效处理温度180℃,处理时间14h;(4) After the secondary ultra-low temperature treatment is completed, put the ZL109 aluminum alloy into the aging furnace, the aging treatment temperature is 180°C, and the treatment time is 14h;
(5)时效过程结束后,将合金材料从时效炉中取出,空冷;(5) After the aging process is finished, the alloy material is taken out from the aging furnace and air-cooled;
处理结束后,对ZL109铝合金进行拉伸性能测试,抗拉强度达到了305.7MPa,测试结果如图1(a)所示。After the treatment, the tensile properties of ZL109 aluminum alloy were tested, and the tensile strength reached 305.7MPa. The test results are shown in Figure 1(a).
实施例2Example 2
利用本发明的热处理方法对AZ91铸态镁合金进行强化处理:Utilize the heat treatment method of the present invention to carry out strengthening treatment to AZ91 as-cast magnesium alloy:
(1)将AZ91镁合金放入密闭腔体中,通入液氮,逐渐冷却至-145℃,降温速率为15℃/min,处理时间6h;(1) Put the AZ91 magnesium alloy into a closed cavity, pour liquid nitrogen, and gradually cool it to -145°C, the cooling rate is 15°C/min, and the treatment time is 6h;
(2)超低温处理结束后,将温度缓慢恢复至室温,将AZ91镁合金放入 温等静压设备中,通入氮气加压,先将静气压力控制在70MPa,等处理温度稳定到410℃,将静气压力调至120MPa,处理时间10h;温等静压处理过程结束后,AZ91镁合金随炉恢复至室温,释放保护气体,降低腔体静压力,在此过程中温度保持不变;静气压力降到常压后,将AZ91镁合金快速转移浸入室温的水中,转移时间不超过20s;(2) After the ultra-low temperature treatment is completed, the temperature is slowly returned to room temperature, the AZ91 magnesium alloy is put into the warm isostatic pressing equipment, and nitrogen is introduced to pressurize. , the static gas pressure was adjusted to 120MPa, and the treatment time was 10h; after the warm isostatic pressing process, the AZ91 magnesium alloy was returned to room temperature with the furnace, the protective gas was released, and the static pressure of the cavity was reduced, and the temperature remained unchanged during this process; After the static pressure dropped to normal pressure, the AZ91 magnesium alloy was quickly transferred and immersed in water at room temperature, and the transfer time did not exceed 20s;
(3)AZ91镁合金温等静压处理完成后,进行二次超低温处理,将腔体环境温度以50℃/min的速度,快速冷却至-170℃,处理8h;(3) After the warm isostatic pressing of AZ91 magnesium alloy is completed, a second ultra-low temperature treatment is performed, and the ambient temperature of the cavity is rapidly cooled to -170 °C at a speed of 50 °C/min, and treated for 8 hours;
(4)二次超低温处理结束后,将AZ91镁合金放入时效炉中,时效处理温度220℃,处理时间16h;(4) After the secondary ultra-low temperature treatment, put the AZ91 magnesium alloy into the aging furnace, the aging treatment temperature is 220 °C, and the treatment time is 16 h;
(5)时效过程结束后,将合金材料从时效炉中取出,空冷;(5) After the aging process is finished, the alloy material is taken out from the aging furnace and air-cooled;
处理结束后,对AZ91镁合金进行拉伸性能测试,抗拉强度达到了285.9MPa,测试结果如图2(a)所示。After the treatment, the tensile properties of the AZ91 magnesium alloy were tested, and the tensile strength reached 285.9 MPa. The test results are shown in Figure 2(a).
对比例1Comparative Example 1
依据国家标准GB/T 25745-2010,对同批次、同规格的ZL109铸态铝合金采用常规的热处理,495℃,固溶处理4h,水冷后在180℃下,时效处理时间14h。常规的热处理结束后,再对其进行拉伸性能测试,结果如图1(b)所示。在实施例1中得到的ZL109铸态铝合金抗拉强度达到了305.7MPa,而对比例1得到的ZL109抗拉强度只有247.6MPa,同实施例1相比,抗拉强度明显偏低。因此,与常规热处理方法相比,经本发明工艺处理的ZL109铸态铝合金拉伸性能得到显著提升。According to the national standard GB/T 25745-2010, conventional heat treatment is used for the ZL109 as-cast aluminum alloys of the same batch and specification, at 495 °C, solution treatment for 4 hours, and then water-cooled at 180 °C for 14 hours of aging treatment time. After the conventional heat treatment, the tensile properties were tested, and the results are shown in Fig. 1(b). The ZL109 as-cast aluminum alloy obtained in Example 1 has a tensile strength of 305.7 MPa, while the ZL109 obtained in Comparative Example 1 has a tensile strength of only 247.6 MPa. Compared with Example 1, the tensile strength is significantly lower. Therefore, compared with the conventional heat treatment method, the tensile properties of the ZL109 as-cast aluminum alloy treated by the process of the present invention are significantly improved.
对比例2Comparative Example 2
参考相关文献,对同批次、同规格的AZ91铸态镁合金采用常规的热处理,410℃,固溶处理10h,水冷后在220℃下,时效处理时间16h。常规热处理后, 对其进行拉伸性能测试,结果如图2(b)所示。在实施例2中AZ91拉强度达到了285.9MPa,而对比例2得到的AZ91抗拉强度只有234.1MPa,同实施例1相比,抗拉强度明显偏低。因此,与常规热处理方法相比,经本发明工艺处理的AZ91铸态镁合金拉伸性能得到显著提升。Referring to relevant literature, conventional heat treatment was used for AZ91 as-cast magnesium alloys of the same batch and specification, at 410 °C, solution treatment for 10 h, and after water cooling at 220 °C, the aging treatment time was 16 h. After conventional heat treatment, the tensile properties were tested, and the results are shown in Fig. 2(b). In Example 2, the tensile strength of AZ91 reached 285.9 MPa, while the tensile strength of AZ91 obtained in Comparative Example 2 was only 234.1 MPa. Compared with Example 1, the tensile strength was significantly lower. Therefore, compared with the conventional heat treatment method, the tensile properties of the AZ91 as-cast magnesium alloy treated by the process of the present invention are significantly improved.
以上所述仅为本发明的优选实施例而已,并不用于限制本发明,对于本领域的技术人员来说,本发明可以有各种更改和变化。凡在本发明的精神和原则之内,所作的任何修改、等同替换、改进等,均应包含在本发明的保护范围之内。The above descriptions are only preferred embodiments of the present invention, and are not intended to limit the present invention. For those skilled in the art, the present invention may have various modifications and changes. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention shall be included within the protection scope of the present invention.

Claims (10)

  1. 一种铝、镁铸态合金的热处理强化工艺,其特征在于:具体包括:A heat treatment strengthening process for aluminum and magnesium as-cast alloys, which is characterized in that: it specifically includes:
    (1)将需要处理的铝或镁轻质合金放入密闭腔体中,将腔体环境温度逐渐冷却至超低温,进行第一次超低温处理;(1) Put the aluminum or magnesium light alloy to be treated into a closed cavity, gradually cool the ambient temperature of the cavity to an ultra-low temperature, and perform the first ultra-low temperature treatment;
    (2)铝合金或镁合金第一次超低温处理完成后,将温度缓慢恢复至室温,再放入温等静压设备中,在合金材料固溶温度下通入惰性保护气体进行气体加压热处理;温等静压处理过程结束后,铝合金或镁合金随炉恢复至室温,释放惰性保护气体,降低腔体静压力,逐渐恢复至常压;静气压力降到常压后,将铝合金或镁合金快速转移浸入水中,直至其彻底冷却;(2) After the first ultra-low temperature treatment of the aluminum alloy or magnesium alloy is completed, the temperature is slowly returned to room temperature, and then placed in a warm isostatic pressing equipment, and an inert protective gas is introduced at the solid solution temperature of the alloy material for gas pressure heat treatment ; After the warm isostatic pressing process, the aluminum alloy or magnesium alloy will return to room temperature with the furnace, release the inert protective gas, reduce the static pressure of the cavity, and gradually return to normal pressure; after the static gas pressure drops to normal pressure, the aluminum alloy Or the magnesium alloy is quickly transferred and immersed in water until it is completely cooled;
    (3)铝合金或镁合金温等静压处理完成后,将腔体环境温度逐渐冷却至合金所需超低温,进行第二次超低温处理;(3) After the temperature isostatic pressing of the aluminum alloy or magnesium alloy is completed, the ambient temperature of the cavity is gradually cooled to the ultra-low temperature required by the alloy, and the second ultra-low temperature treatment is performed;
    (4)铝合金或镁合金二次超低温处理结束后,将铝合金或镁合金放入时效炉中进行时效处理;(4) After the secondary ultra-low temperature treatment of aluminum alloy or magnesium alloy is completed, the aluminum alloy or magnesium alloy is put into an aging furnace for aging treatment;
    (5)时效过程结束后,将合金材料从时效炉中取出,空冷。(5) After the aging process is completed, the alloy material is taken out from the aging furnace and air-cooled.
  2. 如权利要求1所述的工艺,其特征在于:所述步骤(1)中,通过泵入液氮,来控制腔体温度,温控精度为±1℃,降温速率控制在10~20℃/min,使得腔体温度在室温至-190℃范围内进行调节。The process of claim 1, wherein: in the step (1), the temperature of the cavity is controlled by pumping liquid nitrogen, the temperature control accuracy is ±1°C, and the cooling rate is controlled at 10-20°C/ min, so that the chamber temperature can be adjusted in the range of room temperature to -190 °C.
  3. 如权利要求1所述的工艺,其特征在于:所述步骤(1)中,第一次超低温处理的温度范围为-120~-180℃,超低温处理时间根据合金的类型来确定,当采用镁合金时,处理时间为5-7h,当采用铝合金时,处理时间为6-8h。The process according to claim 1, wherein: in the step (1), the temperature range of the first ultra-low temperature treatment is -120~-180°C, and the ultra-low temperature treatment time is determined according to the type of alloy. When the alloy is used, the treatment time is 5-7h, and when the aluminum alloy is used, the treatment time is 6-8h.
  4. 如权利要求1所述的工艺,其特征在于:所述步骤(2)中,所述惰性保护气体为氩气或氮气,在通入惰性保护气体之前要先将真空度抽至10mPa以下。The process according to claim 1, characterized in that: in the step (2), the inert protective gas is argon or nitrogen, and the vacuum degree must be evacuated to below 10 mPa before the inert protective gas is introduced.
  5. 如权利要求1所述的工艺,其特征在于:所述步骤(2)中,在往腔体充入惰性保护气体的过程中,先将静气压力控制在70MPa,等合金所需固溶温度稳定后,再将静气压力调节至100~200MPa。The process according to claim 1, characterized in that: in the step (2), in the process of filling the cavity with the inert protective gas, the static gas pressure is first controlled at 70 MPa, which is equal to the required solid solution temperature of the alloy. After stabilization, the static pressure was adjusted to 100-200MPa.
  6. 如权利要求1所述的工艺,其特征在于:所述步骤(2)中,温等静压处理的时间根据合金的类型来确定,当采用镁合金时,处理时间为9-10h,当采用铝合金时,处理时间为4-5h。The process according to claim 1, characterized in that: in the step (2), the time of the warm isostatic pressing is determined according to the type of the alloy, when a magnesium alloy is used, the processing time is 9-10h, when the For aluminum alloys, the treatment time is 4-5h.
  7. 如权利要求1所述的工艺,其特征在于:所述步骤(2)中,水温不超过65℃,转移时间不超过20s。The process of claim 1, wherein in the step (2), the water temperature does not exceed 65°C, and the transfer time does not exceed 20s.
  8. 如权利要求1所述的工艺,其特征在于:所述步骤(3)中,降温速率控制在50~60℃/min。The process according to claim 1, characterized in that: in the step (3), the cooling rate is controlled at 50-60°C/min.
  9. 如权利要求1所述的工艺,其特征在于:所述步骤(3)中,第二次超低温处理温度为-130~-190℃,处理的时间根据合金的类型来确定,当采用镁合金时,处理时间为15-17h,当采用铝合金时,处理时间为13-15h。The process according to claim 1, characterized in that: in the step (3), the temperature of the second ultra-low temperature treatment is -130 to -190°C, and the treatment time is determined according to the type of alloy. When magnesium alloy is used , the treatment time is 15-17h, and when aluminum alloy is used, the treatment time is 13-15h.
  10. 权利要求1-8任一项所述的铝、镁铸态合金的热处理强化工艺在铸态合金制备中的应用。Application of the heat treatment strengthening process of aluminum and magnesium as-cast alloys according to any one of claims 1 to 8 in the preparation of as-cast alloys.
PCT/CN2021/084380 2021-01-29 2021-03-31 Heat treatment strengthening process for aluminum and magnesium as-cast alloy and application thereof WO2022160457A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN202110126975.9 2021-01-29
CN202110126975.9A CN112962038B (en) 2021-01-29 2021-01-29 Heat treatment strengthening process for aluminum and magnesium as-cast alloy and application thereof

Publications (1)

Publication Number Publication Date
WO2022160457A1 true WO2022160457A1 (en) 2022-08-04

Family

ID=76272116

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2021/084380 WO2022160457A1 (en) 2021-01-29 2021-03-31 Heat treatment strengthening process for aluminum and magnesium as-cast alloy and application thereof

Country Status (2)

Country Link
CN (1) CN112962038B (en)
WO (1) WO2022160457A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115846403A (en) * 2022-09-23 2023-03-28 贵州大学 Cobalt-based alloy with long rod-shaped phase structure with large number of stacking faults and deformation nanometer twin crystals and preparation method thereof

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114150130B (en) * 2021-12-01 2023-09-08 宁波江丰热等静压技术有限公司 Heat treatment method and application of plate for hot isostatic pressing lifting appliance

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2581466B1 (en) * 2011-10-14 2015-04-01 voestalpine Metal Forming GmbH Method for producing a moulded part
CN108796313A (en) * 2018-05-24 2018-11-13 江苏大学 A kind of Al-Mg-Si systems wrought aluminium alloy and its strengthening and toughening treatment method
CN109022974A (en) * 2018-08-24 2018-12-18 重庆元和利泰镁合金制造有限公司 A kind of magnesium alloy motor casing production method and motor housing
CN109252074A (en) * 2018-11-20 2019-01-22 沈左红 A kind of automobile high-toughness high-strength aluminium alloy wheel hub and its manufacturing method

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BRPI0519400A2 (en) * 2004-12-23 2009-01-20 Commw Scient Ind Res Org heat treatment of aluminum alloy high pressure die castings
US8168015B2 (en) * 2008-10-23 2012-05-01 GM Global Technology Operations LLC Direct quench heat treatment for aluminum alloy castings
CN102605304A (en) * 2012-04-17 2012-07-25 辽宁忠旺集团有限公司 Technological method for grain refinement of aluminum alloy extruded section
CN103668014A (en) * 2013-12-10 2014-03-26 常熟柏科汽车零件再制造有限公司 Subzero treatment method of starter aluminium alloy shell
CN107419148A (en) * 2017-05-05 2017-12-01 安徽彩晶光电有限公司 Al-alloy for liquid crystal television bracket
CN111057977A (en) * 2019-12-31 2020-04-24 中南大学 Subzero treatment process and device for improving strength of 6016 aluminum alloy cold-rolled sheet

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2581466B1 (en) * 2011-10-14 2015-04-01 voestalpine Metal Forming GmbH Method for producing a moulded part
CN108796313A (en) * 2018-05-24 2018-11-13 江苏大学 A kind of Al-Mg-Si systems wrought aluminium alloy and its strengthening and toughening treatment method
CN109022974A (en) * 2018-08-24 2018-12-18 重庆元和利泰镁合金制造有限公司 A kind of magnesium alloy motor casing production method and motor housing
CN109252074A (en) * 2018-11-20 2019-01-22 沈左红 A kind of automobile high-toughness high-strength aluminium alloy wheel hub and its manufacturing method

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115846403A (en) * 2022-09-23 2023-03-28 贵州大学 Cobalt-based alloy with long rod-shaped phase structure with large number of stacking faults and deformation nanometer twin crystals and preparation method thereof
CN115846403B (en) * 2022-09-23 2023-08-15 贵州大学 Cobalt-based alloy with long rod-shaped phase structure of a large number of stacking faults and deformation nanometer twin crystals and preparation method thereof

Also Published As

Publication number Publication date
CN112962038A (en) 2021-06-15
CN112962038B (en) 2022-03-04

Similar Documents

Publication Publication Date Title
WO2022160457A1 (en) Heat treatment strengthening process for aluminum and magnesium as-cast alloy and application thereof
CN105220090B (en) A kind of vacuum high-pressure pack alloy heat treating castings method
CN101914713B (en) Oversized high-strength heatproof magnesium alloy ingot blank semicontinuous casting technique
CN111500952B (en) Hot isostatic pressing treatment process method for cast ZL101A aluminum alloy
WO2022142249A1 (en) Method for eliminating cracks in additive manufacturing metal material
CN106521378B (en) A kind of alsimay die casting efficient energy-saving heat treatment method
CN112680616B (en) Preparation method of vacuum induction melting Cu8Cr4Nb alloy
CN108149040A (en) The ingredient of evacuated die-casting process aluminium silicon magnesium-manganese alloy and optimization of Heat Treatment Process method
CN113373351A (en) Pressure casting preparation method of aluminum alloy casting part capable of avoiding heat treatment
Jiang et al. Effect of heat treatment on microstructure and dimensional stability of ZL114A aluminum alloy
CN106119621B (en) A kind of replacement aluminum alloy materials of QT450 braking automobile pump cases and its model casting forming method
WO2024017085A1 (en) High-strength and high-toughness al-cu series cast aluminum alloy, preparation method therefor, and use of same in wheel hub manufacturing
CN110565034B (en) Heat treatment method of die-casting aluminum alloy and automobile part
Zhang et al. Effect of casting methods on microstructure and mechanical properties of ZM5 space flight magnesium alloy
CN106591635A (en) Method for modifying AlSi9Cu2 cast aluminum alloy by rare-earth Y
CN112894113A (en) Aluminum-magnesium heterogeneous alloy post-welding treatment process and application thereof
CN100510150C (en) High-pressure harmonization processing method of eliminating 700 line aluminium alloy cast ingot crystallization phase
Choi et al. Effect of ultrasonic vibration on infiltration of nickel porous preform with molten aluminum alloys
CN107217181B (en) A kind of preparation method of high-strength Al-Si castings wrought alloy
Wang et al. Mechanical properties and microstructure of A356-T6 aluminum alloy wheel hub based on casting-spinning process
CN108118207A (en) A kind of cast Al-Si alloy and preparation method thereof
Wang et al. Solidification structure and mechanical properties of Al–Li–Cu–Zr cast alloys
CN115896514B (en) Preparation method of aluminum alloy casting
CN115652159B (en) High-strength and high-toughness die-casting magnesium alloy and preparation method thereof
CN117620202A (en) Laser selective melting forming method for inhibiting magnesium alloy cracks

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 21922056

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 21922056

Country of ref document: EP

Kind code of ref document: A1