CN109338171B - A kind of Zn-containing cast aluminum-magnesium-lithium alloy and heat treatment method thereof - Google Patents
A kind of Zn-containing cast aluminum-magnesium-lithium alloy and heat treatment method thereof Download PDFInfo
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- 239000001989 lithium alloy Substances 0.000 title claims abstract description 53
- 229910000733 Li alloy Inorganic materials 0.000 title claims abstract description 38
- 238000010438 heat treatment Methods 0.000 title claims abstract description 17
- 238000000034 method Methods 0.000 title abstract description 33
- VCHVXUQQZMQWIY-UHFFFAOYSA-N [AlH3].[Mg].[Li] Chemical compound [AlH3].[Mg].[Li] VCHVXUQQZMQWIY-UHFFFAOYSA-N 0.000 title abstract description 31
- 230000032683 aging Effects 0.000 claims abstract description 22
- 239000012535 impurity Substances 0.000 claims abstract description 9
- 229910052744 lithium Inorganic materials 0.000 claims abstract description 8
- 229910052749 magnesium Inorganic materials 0.000 claims abstract description 8
- 229910052725 zinc Inorganic materials 0.000 claims abstract description 7
- 229910045601 alloy Inorganic materials 0.000 claims description 49
- 239000000956 alloy Substances 0.000 claims description 49
- 238000005266 casting Methods 0.000 claims description 6
- 229910052742 iron Inorganic materials 0.000 claims description 6
- 238000002360 preparation method Methods 0.000 claims description 6
- 229910001051 Magnalium Inorganic materials 0.000 claims 5
- 238000002844 melting Methods 0.000 claims 1
- 230000008018 melting Effects 0.000 claims 1
- 238000010129 solution processing Methods 0.000 claims 1
- 230000008569 process Effects 0.000 abstract description 25
- 238000004321 preservation Methods 0.000 abstract description 4
- 239000000243 solution Substances 0.000 description 30
- 230000000052 comparative effect Effects 0.000 description 18
- 239000006104 solid solution Substances 0.000 description 17
- 239000011777 magnesium Substances 0.000 description 15
- 229910001148 Al-Li alloy Inorganic materials 0.000 description 8
- JFBZPFYRPYOZCQ-UHFFFAOYSA-N [Li].[Al] Chemical compound [Li].[Al] JFBZPFYRPYOZCQ-UHFFFAOYSA-N 0.000 description 8
- 229910019400 Mg—Li Inorganic materials 0.000 description 7
- 238000003723 Smelting Methods 0.000 description 7
- 238000005728 strengthening Methods 0.000 description 7
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 6
- 239000011159 matrix material Substances 0.000 description 6
- 239000000203 mixture Substances 0.000 description 6
- 230000000694 effects Effects 0.000 description 5
- 229910052782 aluminium Inorganic materials 0.000 description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 4
- 239000002893 slag Substances 0.000 description 4
- 229910052786 argon Inorganic materials 0.000 description 3
- 239000002994 raw material Substances 0.000 description 3
- 238000007670 refining Methods 0.000 description 3
- 229910000838 Al alloy Inorganic materials 0.000 description 2
- 229910017073 AlLi Inorganic materials 0.000 description 2
- -1 aluminum-copper-lithium Chemical compound 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 229910052748 manganese Inorganic materials 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- AHLBNYSZXLDEJQ-FWEHEUNISA-N orlistat Chemical compound CCCCCCCCCCC[C@H](OC(=O)[C@H](CC(C)C)NC=O)C[C@@H]1OC(=O)[C@H]1CCCCCC AHLBNYSZXLDEJQ-FWEHEUNISA-N 0.000 description 2
- 238000001556 precipitation Methods 0.000 description 2
- 230000001737 promoting effect Effects 0.000 description 2
- 238000011160 research Methods 0.000 description 2
- 229910052709 silver Inorganic materials 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- NIPNSKYNPDTRPC-UHFFFAOYSA-N N-[2-oxo-2-(2,4,6,7-tetrahydrotriazolo[4,5-c]pyridin-5-yl)ethyl]-2-[[3-(trifluoromethoxy)phenyl]methylamino]pyrimidine-5-carboxamide Chemical compound O=C(CNC(=O)C=1C=NC(=NC=1)NCC1=CC(=CC=C1)OC(F)(F)F)N1CC2=C(CC1)NN=N2 NIPNSKYNPDTRPC-UHFFFAOYSA-N 0.000 description 1
- AFCARXCZXQIEQB-UHFFFAOYSA-N N-[3-oxo-3-(2,4,6,7-tetrahydrotriazolo[4,5-c]pyridin-5-yl)propyl]-2-[[3-(trifluoromethoxy)phenyl]methylamino]pyrimidine-5-carboxamide Chemical compound O=C(CCNC(=O)C=1C=NC(=NC=1)NCC1=CC(=CC=C1)OC(F)(F)F)N1CC2=C(CC1)NN=N2 AFCARXCZXQIEQB-UHFFFAOYSA-N 0.000 description 1
- 230000018199 S phase Effects 0.000 description 1
- 230000002159 abnormal effect Effects 0.000 description 1
- SNAAJJQQZSMGQD-UHFFFAOYSA-N aluminum magnesium Chemical compound [Mg].[Al] SNAAJJQQZSMGQD-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 230000005496 eutectics Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000005272 metallurgy Methods 0.000 description 1
- 238000013508 migration Methods 0.000 description 1
- 230000005012 migration Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—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
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Abstract
本发明公开了一种含Zn铸造铝镁锂合金及其热处理方法;所述铝镁锂合金包括如下各组分:2.1~2.5wt%Mg,3.1~3.5wt%Li,0.1~1.0wt%Zn,杂质元素总量小于0.15wt%,余量为Al。本发明还涉及前述含Zn铸造铝镁锂合金的热处理方法,包括三级固溶处理和单级时效处理两个工艺,其中三级固溶处理工艺为:在430~440℃下固溶处理20~30h,再在500~510℃下固溶处理10~20h,最后在560~570℃下固溶处理20~30h。单级时效处理工艺为175~200℃下保温8~128h。本发明工艺简单,成本低廉,制得的铸造铝镁锂合金可应用于汽车、航空航天、军工等领域。
The invention discloses a Zn-containing cast aluminum-magnesium-lithium alloy and a heat treatment method thereof; the aluminum-magnesium-lithium alloy comprises the following components: 2.1-2.5wt% Mg, 3.1-3.5wt% Li, 0.1-1.0wt% Zn , the total amount of impurity elements is less than 0.15wt%, and the balance is Al. The present invention also relates to the heat treatment method of the aforementioned Zn-containing cast aluminum-magnesium-lithium alloy, including two processes of three-stage solution treatment and single-stage aging treatment, wherein the three-stage solution treatment process is: solution treatment at 430-440°C for 20 ~30h, then solution treatment at 500~510°C for 10~20h, and finally solution treatment at 560~570°C for 20~30h. The single-stage aging treatment process is heat preservation at 175-200°C for 8-128 hours. The invention has simple process and low cost, and the prepared cast aluminum-magnesium-lithium alloy can be applied to the fields of automobile, aerospace, military industry and the like.
Description
技术领域technical field
本发明涉及金属材料类及冶金领域,具体地,涉及一种含Zn铸造铝镁锂合金及其热处理方法。The invention relates to the field of metal materials and metallurgy, in particular to a Zn-containing cast aluminum-magnesium-lithium alloy and a heat treatment method thereof.
背景技术Background technique
随着能源和环境意识的不断增强,人类对轻质结构材料的需求愈发迫切。铝锂合金具有密度小、比强度和比刚度高等优点,是一种在汽车、航空航天、军工等领域具有广阔应用前景的结构材料。With the continuous enhancement of energy and environmental awareness, the human demand for lightweight structural materials is becoming more and more urgent. Aluminum-lithium alloy has the advantages of low density, high specific strength and specific stiffness, and is a structural material with broad application prospects in automotive, aerospace, military and other fields.
塑性变形可以赋予铝锂合金更高的强度,因此目前商业牌号的铝锂合金绝大多数属于变形合金。美国镁铝公司公开了一种改进的铝镁锂合金及其制作方法(公开号:CN105143492),该合金由以下成分组成:2~3.9wt%Mg,0.1~1.8wt%Li,最多至1.5wt%Cu,最多至2wt%Zn,最多至1wt%Ag,最多至1.5wt%Mn,最多至0.5wt%Si,最多至0.35wt%Fe,以及一些次要元素,余量为Al。上述合金为变形铝镁锂合金,为避免裂纹扩展反常偏移,Li元素的添加量通常不高于1.8wt%,以减小Al3Li相的含量,降低平面滑移程度。另外,在变形铝镁锂合金中,由于Li元素含量较低,形成的晶间化合物较少,热处理温度通常较低,例如在法国肯联铝业公开的变形铝镁锂合金(公开号:CN103687971)中,固溶温度为300~430℃,时效温度为150℃,但是,对于Li含量较高的铸造铝镁锂合金,该固溶温度过低,晶界上富集的大量初生相无法充分固溶入基体当中,导致合金塑韧性差,同时该时效温度过低,时效强化效果较差。Plastic deformation can give aluminum-lithium alloys higher strength, so most of the current commercial grades of aluminum-lithium alloys are deformed alloys. American Magnesium Aluminum Company discloses an improved aluminum-magnesium-lithium alloy and its production method (publication number: CN105143492), the alloy is composed of the following components: 2-3.9wt% Mg, 0.1-1.8wt% Li, up to 1.5wt% % Cu, up to 2wt% Zn, up to 1wt% Ag, up to 1.5wt% Mn, up to 0.5wt% Si, up to 0.35wt% Fe, and some minor elements, the balance being Al. The above alloy is a deformed aluminum-magnesium-lithium alloy. In order to avoid abnormal migration of crack propagation, the addition amount of Li element is usually not higher than 1.8wt%, so as to reduce the content of Al 3 Li phase and reduce the degree of plane slip. In addition, in the deformed aluminum-magnesium-lithium alloy, due to the low content of Li element, there are few intergranular compounds formed, and the heat treatment temperature is usually low, such as the deformed aluminum-magnesium-lithium alloy disclosed by the French Kenlian Aluminum Industry (publication number: CN103687971 ), the solid solution temperature is 300-430°C, and the aging temperature is 150°C. However, for cast aluminum-magnesium-lithium alloys with high Li content, the solid solution temperature is too low, and a large number of primary phases enriched on the grain boundaries cannot fully Solid solution into the matrix leads to poor plasticity and toughness of the alloy. At the same time, the aging temperature is too low, and the aging strengthening effect is poor.
目前,变形铝锂合金已在诸多领域得到了广泛的应用,然而某些形状复杂的结构件如涡轮发动机叶轮和马达活塞等需要通过铸造方式生产。因此,国内外相继开展了铸造铝锂合金的研究。铸造铝锂合金按照合金成分可分为铸造铝铜锂合金及铸造铝镁锂合金,上海交通大学公开了一种轻质高强铸造铝锂合金及其制备方法(公开号:CN105648283),所述合金由以下成分组成:3~3.5wt%Li,1~2wt%Cu,0.5~2wt%Mg,0.4~0.8wt%Ag,0.14~0.2wt%Zr,0.3~0.8wt%Mn,杂质元素总量小于0.25wt%,余量为Al。该合金属于铸造铝铜锂合金范畴,向Al合金中添加Cu元素,可促进时效过程中θ′相、T1相及S相的析出,因此该合金具有较高的强度,但同时Cu元素的存在也导致合金具有较差的抗腐蚀性及较高的密度。本课题组在前期工作的基础上,通过优化合金成分及热处理方法,获得了一种具有较好的抗腐蚀性,较低密度的含Zn铸造铝镁锂合金,这对于推动铸造铝锂合金的应用具有重要意义。At present, deformed aluminum-lithium alloys have been widely used in many fields, but some structural parts with complex shapes, such as turbine engine impellers and motor pistons, need to be produced by casting. Therefore, researches on casting aluminum-lithium alloys have been carried out successively at home and abroad. Cast aluminum-lithium alloys can be divided into cast aluminum-copper-lithium alloys and cast aluminum-magnesium-lithium alloys according to the alloy composition. Shanghai Jiaotong University discloses a light-weight high-strength cast aluminum-lithium alloy and its preparation method (public number: CN105648283). It consists of the following components: 3-3.5wt% Li, 1-2wt% Cu, 0.5-2wt% Mg, 0.4-0.8wt% Ag, 0.14-0.2wt% Zr, 0.3-0.8wt% Mn, the total amount of impurity elements is less than 0.25wt%, the balance is Al. This alloy belongs to the category of cast aluminum-copper-lithium alloy. Adding Cu element to Al alloy can promote the precipitation of θ′ phase, T 1 phase and S phase during the aging process, so the alloy has high strength, but at the same time the Cu element The presence of Al also results in alloys with poorer corrosion resistance and higher density. On the basis of the previous work, the research group obtained a Zn-containing cast aluminum-magnesium-lithium alloy with better corrosion resistance and lower density by optimizing the alloy composition and heat treatment method, which is conducive to promoting the development of cast aluminum-lithium alloys Applications are important.
发明内容Contents of the invention
针对现有技术中的缺陷,本发明的目的是提供一种含Zn铸造铝镁锂合金及其热处理方法。通过优化合金成分以及热处理工艺,获得性能优良,制备工艺简单,成本低廉的铸造铝镁锂合金,这对于铸造铝镁锂合金在汽车、航空航天、军工等领域的推广应用具有重要意义。Aiming at the defects in the prior art, the object of the present invention is to provide a Zn-containing cast aluminum-magnesium-lithium alloy and a heat treatment method thereof. By optimizing the alloy composition and heat treatment process, a cast aluminum-magnesium-lithium alloy with excellent performance, simple preparation process and low cost is obtained, which is of great significance for the promotion and application of cast aluminum-magnesium-lithium alloy in the fields of automobile, aerospace, military industry and so on.
本发明的目的是通过以下技术方案来实现的:The purpose of the present invention is achieved through the following technical solutions:
第一方面,本发明涉及一种含Zn铸造铝镁锂合金,所述合金包括如下重量百分比含量的各组分:2.1~2.5wt%Mg,3.1~3.5wt%Li,0.1~1.0wt%Zn,杂质元素总量小于0.15wt%,余量为Al。在本发明的体系中,如Mg的含量高于2.5wt%,则会在合金内部产生大量初生相,很难通过固溶处理溶入基体,危害合金的力学性能,如Mg的含量低于2.1wt%,则Mg元素的固溶强化效果不明显;如Li的含量高于3.5wt%,则会导致合金在熔炼过程中极易吸气,造成氧化夹渣等铸造缺陷,如Li的含量低于3.1wt%,则无法充分发挥Li元素提高Al合金比强度、比刚度的作用;如Zn的含量高于1.0wt%则会明显增加合金密度,如Zn的含量低于0.1wt%则无法对合金的微观组织和力学性能造成影响。In the first aspect, the present invention relates to a cast aluminum-magnesium-lithium alloy containing Zn. The alloy includes the following components in weight percent: 2.1-2.5wt% Mg, 3.1-3.5wt% Li, 0.1-1.0wt% Zn , the total amount of impurity elements is less than 0.15wt%, and the balance is Al. In the system of the present invention, if the content of Mg is higher than 2.5wt%, a large number of primary phases will be produced inside the alloy, which is difficult to dissolve into the matrix through solid solution treatment, which will endanger the mechanical properties of the alloy. If the content of Mg is lower than 2.1 wt%, the solid solution strengthening effect of Mg element is not obvious; if the Li content is higher than 3.5wt%, it will cause the alloy to absorb gas easily during the smelting process, resulting in casting defects such as oxidation slag inclusions, such as low Li content If the content of Zn is higher than 3.1wt%, the effect of Li element on improving the specific strength and specific stiffness of the Al alloy cannot be fully exerted; if the content of Zn is higher than 1.0wt%, the density of the alloy will be significantly increased, and if the content of Zn is lower than 0.1wt%, it will not be able to The microstructure and mechanical properties of the alloy are affected.
优选地,所述杂质元素包括Fe、Si、K和Na中的一种或几种。Preferably, the impurity elements include one or more of Fe, Si, K and Na.
第二方面,本发明还涉及一种含Zn铸造铝镁锂合金的热处理方法,包括三级固溶处理和单级时效处理。In the second aspect, the present invention also relates to a heat treatment method for cast aluminum-magnesium-lithium alloy containing Zn, including three-stage solid solution treatment and single-stage aging treatment.
优选地,所述三级固溶处理包括:将所述含Zn铸造铝镁锂合金在430~440℃下固溶处理20~30h,再在500~510℃下固溶处理10~20h,最后在560~570℃下固溶处理20~30h。在本发明的体系中,如各阶段固溶处理温度低于上述温度范围,则由于温度过低,无法起到使相应初生相Al17Mg12,Al2MgLi,AlLi等溶入基体的作用,如各阶段固溶处理温度高于上述温度范围,则由于温度过高,容易使合金过烧或晶粒过度长大。Preferably, the three-stage solution treatment includes: solution treating the Zn-containing cast aluminum-magnesium-lithium alloy at 430-440°C for 20-30h, then solution-treating at 500-510°C for 10-20h, and finally Solution treatment at 560-570°C for 20-30 hours. In the system of the present invention, if the solution treatment temperature at each stage is lower than the above temperature range, the corresponding primary phases Al 17 Mg 12 , Al 2 MgLi, AlLi, etc. cannot be dissolved into the matrix because the temperature is too low. If the solution treatment temperature at each stage is higher than the above temperature range, the alloy is likely to be over-burned or the grains grow excessively due to the high temperature.
优选地,所述单级时效处理为175~200℃下保温8~128h。Preferably, the single-stage aging treatment is carried out at 175-200° C. for 8-128 hours.
与现有技术相比,本发明具有如下的有益效果:Compared with the prior art, the present invention has the following beneficial effects:
(1)Li是最轻的金属元素,密度只有0.53g cm-3,并且是少数几种在Al中具有较高固溶度的元素之一,在共熔温度(602℃)下,约有4.2wt%的Li可以溶解在Al中,此外,在时效过程中,Li元素能够以Al3Li相的形式析出,起到时效强化效果。本专利设计的Li元素含量为3.1~3.5wt%,可极大的降低合金密度并改善合金强度。(1) Li is the lightest metal element with a density of only 0.53g cm -3 , and it is one of the few elements with high solid solubility in Al. At the eutectic temperature (602°C), about 4.2wt% of Li can be dissolved in Al. In addition, during the aging process, the Li element can be precipitated in the form of Al 3 Li phase, which plays an aging strengthening effect. The Li element content designed in this patent is 3.1-3.5 wt%, which can greatly reduce the alloy density and improve the alloy strength.
(2)Mg元素的添加不仅可以进一步降低合金密度,还可以起到固溶强化的作用,同时降低Li在Al中的溶解度,促进主要强化相Al3Li相的析出,增加时效强化效果。(2) The addition of Mg element can not only further reduce the alloy density, but also play the role of solid solution strengthening, while reducing the solubility of Li in Al, promoting the precipitation of the main strengthening phase Al 3 Li phase, and increasing the aging strengthening effect.
(3)Zn元素的添加不仅可以起到固溶强化的作用,还可以细化晶粒,改善合金力学性能。(3) The addition of Zn element can not only play the role of solid solution strengthening, but also refine the grains and improve the mechanical properties of the alloy.
(4)采用三级固溶工艺,使Al8Mg5相在较低的第一级温度下固溶入基体中,Al2MgLi相在第二级温度下溶解,AlLi相在最高的第三级温度下溶解,解决了低温单级固溶条件下初生相难以溶解,高温单级固溶条件下合金严重过烧的难题,同时有效避免了晶粒尺寸的过度增长。(4) Three-stage solid solution process is adopted, so that the Al 8 Mg 5 phase is solid-dissolved into the matrix at the lower first-stage temperature, the Al 2 MgLi phase is dissolved at the second-stage temperature, and the AlLi phase is dissolved at the highest third-stage temperature. It dissolves at the low-grade temperature, which solves the problem that the primary phase is difficult to dissolve under the low-temperature single-stage solid solution condition, and the alloy is severely over-burned under the high-temperature single-stage solid solution condition, and at the same time, it effectively avoids the excessive growth of the grain size.
附图说明Description of drawings
通过阅读参照以下附图对非限制性实施例所作的详细描述,本发明的其它特征、目的和优点将会变得更明显:Other characteristics, objects and advantages of the present invention will become more apparent by reading the detailed description of non-limiting embodiments made with reference to the following drawings:
图1为实施例1中合金金相组织照片,其中图1(a)为铸态金相组织照片,图1(b)为固溶态金相组织照片;Fig. 1 is alloy metallographic structure photo in embodiment 1, and wherein Fig. 1 (a) is as-cast metallographic structure photo, Fig. 1 (b) is solid solution state metallographic structure photo;
图2为实施例2中合金金相组织照片,其中图2(a)为铸态金相组织照片,图2(b)为固溶态金相组织照片;Fig. 2 is alloy metallographic structure photo in embodiment 2, and wherein Fig. 2 (a) is as-cast metallographic structure photo, Fig. 2 (b) is solid solution state metallographic structure photo;
图3为对比例1及对比例2中合金金相组织照片,其中图3(a)为对比例1中合金固溶态金相组织照片,图3(b)为对比例2中合金固溶态金相组织照片。Fig. 3 is the metallographic structure photo of the alloy in comparative example 1 and comparative example 2, wherein Fig. 3 (a) is the metallographic structure photo of the alloy in the comparative example 1, and Fig. 3 (b) is the alloy solid solution in the comparative example 2 state metallographic structure photos.
图4为对比例3中合金金相组织照片。Figure 4 is a photo of the metallographic structure of the alloy in Comparative Example 3.
具体实施方式Detailed ways
下面结合具体实施例对本发明进行详细说明。以下实施例将有助于本领域的技术人员进一步理解本发明,但不以任何形式限制本发明。应当指出的是,对本领域的普通技术人员来说,在不脱离本发明构思的前提下,还可以做出若干变化和改进。这些都属于本发明的保护范围。The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several changes and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.
实施例1Example 1
本实施例涉及一种含Zn铸造铝镁锂合金,所述合金包括如下重量百分比含量的各组分:2.1wt%Mg,3.1wt%Li,0.1wt%Zn,杂质元素Fe、Si、K和Na总量小于0.15wt%,余量为Al。This embodiment relates to a Zn-containing cast aluminum-magnesium-lithium alloy. The alloy includes the following components in weight percent: 2.1wt% Mg, 3.1wt% Li, 0.1wt% Zn, impurity elements Fe, Si, K and The total amount of Na is less than 0.15wt%, and the balance is Al.
所述含Zn铸造铝镁锂合金的制备方法分为熔炼和热处理两个工艺。The preparation method of the Zn-containing cast Al-Mg-Li alloy is divided into two processes of smelting and heat treatment.
所述熔炼工艺包括如下步骤:Described smelting process comprises the steps:
1、按所述含Zn铸造铝镁锂合金的重量百分比准备原料;1. Prepare raw materials according to the weight percentage of the Zn-containing cast aluminum-magnesium-lithium alloy;
2、将纯铝放入坩埚中熔化,待炉温升高至760~780℃,加入纯Zn;2. Put the pure aluminum into the crucible and melt it. After the furnace temperature rises to 760-780°C, add pure Zn;
3、待炉温下降至730~740℃加入纯Mg;3. Add pure Mg when the furnace temperature drops to 730-740°C;
4、温度继续下降到700~710℃时在氩气保护下加入纯Li;4. Add pure Li under argon protection when the temperature continues to drop to 700-710°C;
5、控制炉温回升至720~730℃,精炼,扒渣,浇注得到含Zn铸造铝镁锂合金铸锭。5. Controlling the furnace temperature to rise to 720-730°C, refining, removing slag, and pouring to obtain Zn-containing cast aluminum-magnesium-lithium alloy ingots.
图1(a)为本实施例中合金铸态金相组织照片,可以看出,铸态合金晶粒呈树枝状,粗大的初生相呈网状分布于晶界。Figure 1(a) is a photograph of the as-cast metallographic structure of the alloy in this example. It can be seen that the grains of the as-cast alloy are dendritic, and the coarse primary phases are distributed in the grain boundary in the form of a network.
所述热处理工艺包括三级固溶处理和单级时效处理两个步骤:The heat treatment process includes two steps of three-stage solution treatment and single-stage aging treatment:
所述三级固溶处理工艺包括:将所述含Zn铸造铝镁锂合金在430℃下固溶处理20h,再在500℃下固溶处理10h,最后在560℃下固溶处理20h。图1(b)为本实施例中合金固溶态金相组织照片,从图中可以看出,经三级固溶处理后,合金中的初生相已充分溶于基体。The three-stage solution treatment process includes: solution treating the Zn-containing cast Al-Mg-Li alloy at 430° C. for 20 hours, then solution treating it at 500° C. for 10 hours, and finally performing solution treatment at 560° C. for 20 hours. Figure 1(b) is a photograph of the metallographic structure of the alloy in solid solution state in this example. It can be seen from the figure that after three-stage solution treatment, the primary phase in the alloy has been fully dissolved in the matrix.
所述单级时效处理工艺为175℃下保温64h。The single-stage aging treatment process is heat preservation at 175° C. for 64 hours.
实施例2Example 2
本实施例涉及一种含Zn铸造铝镁锂合金,所述合金包括如下重量百分比含量的各组分:2.1wt%Mg,3.1wt%Li,1.0wt%Zn,杂质元素Fe、Si、K和Na总量小于0.15wt%,余量为Al。This embodiment relates to a Zn-containing cast aluminum-magnesium-lithium alloy. The alloy includes the following components in weight percent: 2.1wt% Mg, 3.1wt% Li, 1.0wt% Zn, impurity elements Fe, Si, K and The total amount of Na is less than 0.15wt%, and the balance is Al.
所述含Zn铸造铝镁锂合金的制备方法分为熔炼和热处理两个工艺。The preparation method of the Zn-containing cast Al-Mg-Li alloy is divided into two processes of smelting and heat treatment.
所述熔炼工艺包括如下步骤:Described smelting process comprises the steps:
1、按所述含Zn铸造铝镁锂合金的重量百分比准备原料;1. Prepare raw materials according to the weight percentage of the Zn-containing cast aluminum-magnesium-lithium alloy;
2、将纯铝放入坩埚中熔化,待炉温升高至760~780℃,加入纯Zn;2. Put the pure aluminum into the crucible and melt it. After the furnace temperature rises to 760-780°C, add pure Zn;
3、待炉温下降至730~740℃加入纯Mg;3. Add pure Mg when the furnace temperature drops to 730-740°C;
4、温度继续下降到700~710℃时在氩气保护下加入纯Li;4. Add pure Li under argon protection when the temperature continues to drop to 700-710°C;
5、控制炉温回升至720~730℃,精炼,扒渣,浇注得到含Zn铸造铝镁锂合金铸锭。5. Controlling the furnace temperature to rise to 720-730°C, refining, removing slag, and pouring to obtain Zn-containing cast aluminum-magnesium-lithium alloy ingots.
图2(a)为本实施例中合金铸态金相组织照片,铸态合金晶粒为等轴晶,与图1(a)所示的实施例1中合金铸态金相组织对比,可以看出,提高Zn元素含量能有效细化晶粒。Fig. 2 (a) is the metallographic structure photograph of alloy in the as-cast state in the present embodiment, and the as-cast alloy crystal grain is equiaxed grain, compares with the metallographic structure of alloy as-cast state in the embodiment 1 shown in Fig. 1 (a), can It can be seen that increasing the Zn element content can effectively refine the grains.
所述热处理工艺包括三级固溶处理和单级时效处理两个步骤:The heat treatment process includes two steps of three-stage solution treatment and single-stage aging treatment:
所述三级固溶处理工艺包括:将所述含Zn铸造铝镁锂合金在430℃下固溶处理20h,再在510℃下固溶处理20h,最后在560℃下固溶处理20h。图2(b)为本实施例中合金固溶态金相组织照片,从图中可以看出,经三级固溶处理后,合金中的初生相已充分溶于基体。The three-stage solution treatment process includes: solution treating the Zn-containing cast Al-Mg-Li alloy at 430° C. for 20 hours, then solution treating it at 510° C. for 20 hours, and finally performing solution treatment at 560° C. for 20 hours. Figure 2(b) is a photograph of the metallographic structure of the alloy in solid solution state in this example. It can be seen from the figure that after three-stage solution treatment, the primary phase in the alloy has been fully dissolved in the matrix.
所述单级时效处理工艺为175℃下保温128h。The single-stage aging treatment process is heat preservation at 175° C. for 128 hours.
实施例3Example 3
本实施例涉及一种含Zn铸造铝镁锂合金,所述合金包括如下重量百分比含量的各组分:2.5wt%Mg,3.5wt%Li,0.5wt%Zn,杂质元素Fe、Si、K和Na总量小于0.15wt%,余量为Al。This embodiment relates to a Zn-containing cast aluminum-magnesium-lithium alloy. The alloy includes the following components in weight percent: 2.5wt% Mg, 3.5wt% Li, 0.5wt% Zn, impurity elements Fe, Si, K and The total amount of Na is less than 0.15wt%, and the balance is Al.
所述含Zn铸造铝镁锂合金的制备方法分为熔炼和热处理两个工艺。The preparation method of the Zn-containing cast Al-Mg-Li alloy is divided into two processes of smelting and heat treatment.
所述熔炼工艺包括如下步骤:Described smelting process comprises the steps:
1、按所述含Zn铸造铝镁锂合金的重量百分比准备原料;1. Prepare raw materials according to the weight percentage of the Zn-containing cast aluminum-magnesium-lithium alloy;
2、将纯铝放入坩埚中熔化,待炉温升高至760~780℃,加入纯Zn;2. Put the pure aluminum into the crucible and melt it. After the furnace temperature rises to 760-780°C, add pure Zn;
3、待炉温下降至730~740℃加入纯Mg;3. Add pure Mg when the furnace temperature drops to 730-740°C;
4、温度继续下降到700~710℃时在氩气保护下加入纯Li;4. Add pure Li under argon protection when the temperature continues to drop to 700-710°C;
5、控制炉温回升至720~730℃,精炼,扒渣,浇注得到含Zn铸造铝镁锂合金铸锭。5. Controlling the furnace temperature to rise to 720-730°C, refining, removing slag, and pouring to obtain Zn-containing cast aluminum-magnesium-lithium alloy ingots.
所述热处理工艺包括三级固溶处理和单级时效处理两个步骤:The heat treatment process includes two steps of three-stage solution treatment and single-stage aging treatment:
所述三级固溶处理工艺包括:将所述含Zn铸造铝镁锂合金在440℃下固溶处理30h,再在510℃下固溶处理20h,最后在570℃下固溶处理30h。The three-stage solution treatment process includes: solution treating the Zn-containing cast Al-Mg-Li alloy at 440° C. for 30 hours, then solution treating it at 510° C. for 20 hours, and finally performing solution treatment at 570° C. for 30 hours.
所述单级时效处理工艺为200℃下保温8h。The single-stage aging treatment process is heat preservation at 200° C. for 8 hours.
对比例1Comparative example 1
本对比例涉及一种含Zn铸造铝镁锂合金,所述合金的组分和时效工艺与实施例1基本相同,不同之处仅在于:本对比例中的合金采用低温单级固溶处理工艺,具体为500℃/50h。由图3(a)可以看出,由于固溶温度低,初生相难以溶解。This comparative example involves a Zn-containing cast aluminum-magnesium-lithium alloy. The composition and aging process of the alloy are basically the same as those in Example 1, the only difference being that the alloy in this comparative example adopts a low-temperature single-stage solution treatment process , specifically 500°C/50h. It can be seen from Figure 3(a) that the primary phase is difficult to dissolve due to the low solid solution temperature.
对比例2Comparative example 2
本对比例涉及一种含Zn铸造铝镁锂合金,所述合金的组分和时效工艺与实施例1基本相同,不同之处仅在于:本对比例中的合金采用高温单级固溶处理工艺,具体为560℃/50h。由图3(b)可以看出,由于固溶温度高,合金出现过烧现象。This comparative example relates to a Zn-containing cast aluminum-magnesium-lithium alloy. The composition and aging process of the alloy are basically the same as those in Example 1, the only difference being that the alloy in this comparative example adopts a high-temperature single-stage solution treatment process , specifically 560°C/50h. It can be seen from Figure 3(b) that due to the high solution temperature, the alloy appears overburned.
对比例3Comparative example 3
本对比例涉及一种含Zn铸造铝镁锂合金,所述合金的组分和时效工艺与实施例1基本相同,不同之处仅在于:本对比例中的合金采用双极固溶处理工艺,具体为:在500℃下固溶处理20h,再在560℃下固溶处理30h。由图4可以看出,由于缺少低温固溶处理步骤,合金在高温下处理时间偏长,晶粒明显长大。This comparative example relates to a Zn-containing cast aluminum-magnesium-lithium alloy. The composition and aging process of the alloy are basically the same as those in Example 1, the only difference being that the alloy in this comparative example adopts a bipolar solution treatment process. Specifically: solution treatment at 500°C for 20 hours, and then solution treatment at 560°C for 30 hours. It can be seen from Figure 4 that due to the lack of a low-temperature solution treatment step, the alloy is treated at a high temperature for a long time, and the grains grow significantly.
性能测试Performance Testing
实施例1-3和对比例1-2制备的铸造铝镁锂合金T6态室温力学性能如下表1所示:The mechanical properties of the cast Al-Mg-Li alloy T6 state at room temperature prepared in Example 1-3 and Comparative Example 1-2 are shown in Table 1 below:
表1Table 1
以上对本发明的具体实施例进行了描述。需要理解的是,本发明并不局限于上述特定实施方式,本领域技术人员可以在权利要求的范围内做出各种变化或修改,这并不影响本发明的实质内容。在不冲突的情况下,本申请的实施例和实施例中的特征可以任意相互组合。Specific embodiments of the present invention have been described above. It should be understood that the present invention is not limited to the specific embodiments described above, and those skilled in the art may make various changes or modifications within the scope of the claims, which do not affect the essence of the present invention. In the case of no conflict, the embodiments of the present application and the features in the embodiments can be combined with each other arbitrarily.
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