WO2023035831A1 - Alliage d'aluminium pour extrusion et procédé de préparation associé - Google Patents
Alliage d'aluminium pour extrusion et procédé de préparation associé Download PDFInfo
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- WO2023035831A1 WO2023035831A1 PCT/CN2022/110595 CN2022110595W WO2023035831A1 WO 2023035831 A1 WO2023035831 A1 WO 2023035831A1 CN 2022110595 W CN2022110595 W CN 2022110595W WO 2023035831 A1 WO2023035831 A1 WO 2023035831A1
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- WIPO (PCT)
- Prior art keywords
- aluminum
- extrusion
- aluminum alloy
- temperature
- refining
- Prior art date
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- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 60
- 238000001125 extrusion Methods 0.000 title claims abstract description 49
- 238000002360 preparation method Methods 0.000 title claims description 14
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 55
- 238000007670 refining Methods 0.000 claims abstract description 45
- 239000012535 impurity Substances 0.000 claims abstract description 21
- 238000005096 rolling process Methods 0.000 claims abstract description 16
- 238000000034 method Methods 0.000 claims abstract description 15
- 238000009749 continuous casting Methods 0.000 claims abstract description 7
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 54
- 238000005266 casting Methods 0.000 claims description 23
- 239000000956 alloy Substances 0.000 claims description 22
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 20
- 239000007788 liquid Substances 0.000 claims description 20
- 229910052725 zinc Inorganic materials 0.000 claims description 16
- 229910052790 beryllium Inorganic materials 0.000 claims description 13
- 239000003795 chemical substances by application Substances 0.000 claims description 13
- 239000000203 mixture Substances 0.000 claims description 12
- 229910052691 Erbium Inorganic materials 0.000 claims description 11
- 229910052748 manganese Inorganic materials 0.000 claims description 11
- 229910052757 nitrogen Inorganic materials 0.000 claims description 10
- 229910045601 alloy Inorganic materials 0.000 claims description 9
- 229910052742 iron Inorganic materials 0.000 claims description 9
- 229910052720 vanadium Inorganic materials 0.000 claims description 9
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 8
- 238000001914 filtration Methods 0.000 claims description 8
- 229910052719 titanium Inorganic materials 0.000 claims description 8
- 239000002893 slag Substances 0.000 claims description 7
- 239000000498 cooling water Substances 0.000 claims description 5
- 238000007872 degassing Methods 0.000 claims description 5
- 239000011148 porous material Substances 0.000 claims description 5
- 238000003756 stirring Methods 0.000 claims description 5
- 229910052786 argon Inorganic materials 0.000 claims description 4
- 235000012438 extruded product Nutrition 0.000 claims description 4
- 238000002844 melting Methods 0.000 claims description 2
- 230000008018 melting Effects 0.000 claims description 2
- 229910052710 silicon Inorganic materials 0.000 claims 1
- 239000000463 material Substances 0.000 abstract description 10
- 238000000137 annealing Methods 0.000 abstract description 9
- 230000007797 corrosion Effects 0.000 abstract description 9
- 238000005260 corrosion Methods 0.000 abstract description 9
- 238000003723 Smelting Methods 0.000 abstract description 6
- 238000005275 alloying Methods 0.000 abstract description 4
- 238000001816 cooling Methods 0.000 abstract 1
- 230000002035 prolonged effect Effects 0.000 abstract 1
- 230000000052 comparative effect Effects 0.000 description 28
- 239000011572 manganese Substances 0.000 description 19
- 239000011701 zinc Substances 0.000 description 14
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 8
- 238000010438 heat treatment Methods 0.000 description 7
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 6
- -1 aluminum-manganese Chemical compound 0.000 description 6
- 239000000047 product Substances 0.000 description 6
- 239000010936 titanium Substances 0.000 description 6
- 239000000839 emulsion Substances 0.000 description 5
- 238000004519 manufacturing process Methods 0.000 description 5
- 238000005204 segregation Methods 0.000 description 5
- 239000004615 ingredient Substances 0.000 description 4
- 239000011159 matrix material Substances 0.000 description 4
- 239000006104 solid solution Substances 0.000 description 4
- YIWGJFPJRAEKMK-UHFFFAOYSA-N 1-(2H-benzotriazol-5-yl)-3-methyl-8-[2-[[3-(trifluoromethoxy)phenyl]methylamino]pyrimidine-5-carbonyl]-1,3,8-triazaspiro[4.5]decane-2,4-dione Chemical compound CN1C(=O)N(c2ccc3n[nH]nc3c2)C2(CCN(CC2)C(=O)c2cnc(NCc3cccc(OC(F)(F)F)c3)nc2)C1=O YIWGJFPJRAEKMK-UHFFFAOYSA-N 0.000 description 3
- 229910000952 Be alloy Inorganic materials 0.000 description 3
- 229910001371 Er alloy Inorganic materials 0.000 description 3
- 229910000640 Fe alloy Inorganic materials 0.000 description 3
- 229910000914 Mn alloy Inorganic materials 0.000 description 3
- 229910001069 Ti alloy Inorganic materials 0.000 description 3
- 229910000756 V alloy Inorganic materials 0.000 description 3
- 229910001297 Zn alloy Inorganic materials 0.000 description 3
- UQZIWOQVLUASCR-UHFFFAOYSA-N alumane;titanium Chemical compound [AlH3].[Ti] UQZIWOQVLUASCR-UHFFFAOYSA-N 0.000 description 3
- SOWHJXWFLFBSIK-UHFFFAOYSA-N aluminum beryllium Chemical compound [Be].[Al] SOWHJXWFLFBSIK-UHFFFAOYSA-N 0.000 description 3
- CYUOWZRAOZFACA-UHFFFAOYSA-N aluminum iron Chemical compound [Al].[Fe] CYUOWZRAOZFACA-UHFFFAOYSA-N 0.000 description 3
- HIMLGVIQSDVUJQ-UHFFFAOYSA-N aluminum vanadium Chemical compound [Al].[V] HIMLGVIQSDVUJQ-UHFFFAOYSA-N 0.000 description 3
- FJMNNXLGOUYVHO-UHFFFAOYSA-N aluminum zinc Chemical compound [Al].[Zn] FJMNNXLGOUYVHO-UHFFFAOYSA-N 0.000 description 3
- 238000004945 emulsification Methods 0.000 description 3
- 239000000155 melt Substances 0.000 description 3
- 238000001556 precipitation Methods 0.000 description 3
- 230000003068 static effect Effects 0.000 description 3
- 230000002301 combined effect Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- 230000002195 synergetic effect Effects 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000004512 die casting Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
Images
Classifications
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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
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/0075—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for rods of limited length
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22B—PRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
- C22B21/00—Obtaining aluminium
- C22B21/06—Obtaining aluminium refining
- C22B21/066—Treatment of circulating aluminium, e.g. by filtration
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22B—PRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
- C22B9/00—General processes of refining or remelting of metals; Apparatus for electroslag or arc remelting of metals
- C22B9/10—General processes of refining or remelting of metals; Apparatus for electroslag or arc remelting of metals with refining or fluxing agents; Use of materials therefor, e.g. slagging or scorifying agents
-
- C—CHEMISTRY; METALLURGY
- 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
-
- C—CHEMISTRY; METALLURGY
- 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
- C22C1/03—Making non-ferrous alloys by melting using master alloys
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/06—Making non-ferrous alloys with the use of special agents for refining or deoxidising
-
- 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
Definitions
- the invention relates to the field of aluminum alloy die-casting processing, in particular to an aluminum alloy for extrusion and a preparation method thereof.
- Aluminum alloy extrusion products are widely used in automobiles, airplanes, home appliances and other fields.
- the processing cost due to die loss accounts for 30% of the total cost, and the average production of 3.5 tons of extruded products
- Existing aluminum alloy materials have poor fluidity and ductility, and wall breakage often occurs when extruding thin-walled products, resulting in cost losses.
- problems such as poor structural continuity, poor corrosion resistance, and coarse grains leading to poor toughness of aluminum alloy materials. Therefore, there is still a need for an aluminum alloy material to improve the extrusion performance of the material, which is suitable for extrusion products with complex structures or thin-wall structures, and prolongs the service life of extrusion dies.
- the present invention provides an aluminum alloy for extrusion and a preparation method thereof, which have significantly improved corrosion resistance, material strength, fluidity and tissue continuity.
- the present invention claims to protect an aluminum alloy for extrusion, its components and the mass percentage of each component are: Si 0.1-0.2%, Fe 0.15-0.25%, Mn 1.8-2.4%, Zn 0.05-0.18%, Er 0.03 -0.06%, Ti 0.008-0.04%, Be 0.04-0.08%, V 0.01-0.02%, the rest are Al and unavoidable impurities, and the total amount of impurities does not exceed 0.015%.
- the components of the aluminum alloy for extrusion and the mass percent of each component are: Si 0.18%, Fe 0.23%, Mn 2.23%, Zn 0.14%, Er 0.05%, Ti 0.02%, Be 0.06%, V 0.015 %, the rest is Al and unavoidable impurities, the total amount of impurities is not more than 0.015%.
- the preparation method of aluminum alloy for extrusion of the present invention comprises the following steps:
- S2 Add an intermediate alloy to the first aluminum liquid in the holding furnace, stir for 25-35 minutes, and obtain the second aluminum liquid; wherein, the temperature of the holding furnace is 780-800°C, and the intermediate alloy is one or more types, containing Si , Fe, Mn, Zn, Er, Ti, Be and V;
- the medium-strength aluminum alloy materials used for extrusion in the industry mainly use Mn as the main element.
- Mn has the advantages of improving strength and corrosion resistance of materials, but there are the following problems: (1) High slag content, extrusion The material has very strict requirements on the slag content of the structure. During the extrusion process, these impurities will form hard spots, which will increase the wear of the mold, and will destroy the continuity of the structure and affect the quality of the extruded product; (2) The structure is not uniform , High manganese element is easy to segregate, grain growth is uneven after annealing, material properties are unstable, aluminum sticking and wall breaking are easy to occur during extrusion, which reduces mold life and product quality.
- the present invention obtains a high-strength, high-fluidity, high-ductility and corrosion-resistant aluminum alloy material by improving the raw material composition and proportion of the aluminum alloy, and cooperating with the production process and heat treatment process.
- step S1 the time for one refining is 35-45 minutes.
- step S1 or S3 a refining agent is added at a rate of 2-3 kg/t of aluminum liquid.
- the pore size of the second filter is 60 mesh, and the pore size of the first filter is smaller than 60 mesh, preferably 40 mesh.
- step S5 the speed of feeding the AlTiC wire is 1.5-2.0 m/min.
- AlTiC is selected as the refiner to avoid the formation of hard phase, thereby reducing the loss of the die during the extrusion process and increasing the continuity of the product.
- the titanium content in the molten aluminum can be kept fluctuating within 0.008-0.04%.
- step S5 horizontal casting is performed on the fourth molten aluminum.
- step S5 the pore size of the casting filter is 16 mesh.
- step S6 the flow rate of the rolling emulsion is 35-38 m 3 /h, the pressure is 180-200 kPa, and the final rolling temperature can be adjusted by the flow rate and pressure of the rolling emulsion.
- step S7 keep warm for 90-96h.
- the present invention also claims extruded products prepared using the aforementioned aluminum alloys.
- the present invention has at least the following advantages:
- Mn can improve the corrosion resistance of aluminum alloys. Its maximum solid solubility in aluminum is 1.82%. Excessive Mn content can easily lead to intragranular segregation. The content of Mn in the medium can achieve corrosion resistance. By adding Fe, it can form FeMnAl 6 phase with Mn, reduce the solid solution of Mn in the aluminum matrix, and improve the ductility of the alloy. At the same time, cooperate with Zn and Er to further reduce the solid solution of Mn And reduce the segregation phenomenon, refine the coarse phase in the structure, and significantly improve the mechanical properties of the material.
- the present invention matches the heat treatment process of the present invention by adding Er, Si, and Be to heat treatment at low temperature for a long time, so that the compound dissolved in the aluminum matrix is slowly precipitated, the amount of manganese element precipitation is promoted, and the growth of the precipitated phase is suppressed at the same time.
- Large, to realize the fine and dispersed distribution of the second phase improve the extrusion fluidity of the alloy material, avoid the coarse grains caused by high temperature annealing, and provide an alloy material with excellent toughness.
- Figure 1 shows the aluminum alloys prepared in Example 1 and Comparative Examples 2, 8, and 9.
- the components of aluminum alloy for extrusion and the mass percentage of each component are: Si 0.18%, Fe 0.23%, Mn 2.23%, Zn 0.14%, Er 0.05%, Ti 0.02%, Be 0.06%, V 0.015%, the rest Al and unavoidable impurities, the total amount of impurities is not more than 0.015%.
- the preparation method of aluminum alloy for extrusion comprises the following steps:
- the components of the aluminum alloy for extrusion and the mass percentage of each component are: Si 0.1%, Fe 0.16%, Mn 1.8%, Zn 0.18%, Er 0.06%, Ti 0.015%, Be 0.08%, V 0.02%, the rest Al and unavoidable impurities, the total amount of impurities is not more than 0.015%.
- the preparation method of aluminum alloy for extrusion comprises the following steps:
- S5 Continuously cast the molten aluminum after the online treatment of S4, adopt horizontal casting, and add a 16-mesh casting filter to filter the scale at the gate, control the casting temperature to 710°C, the casting speed to 6.5t/h, and the cooling water temperature 35°C, and the billet temperature is 520°C.
- the components of aluminum alloy for extrusion and the mass percentage of each component are: Si 0.2%, Fe 0.2%, Mn 2%, Zn 0.05%, Er 0.03%, Ti 0.04%, Be 0.04%, V 0.01%, the rest Al and unavoidable impurities, the total amount of impurities is not more than 0.015%.
- the preparation method of aluminum alloy for extrusion comprises the following steps:
- a filter plate which is respectively the 40 mesh filter plate of the front channel and the 60 mesh filter plate of the rear channel, performs double-stage filtration.
- S5 Continuously cast the molten aluminum after S4 on-line treatment, adopt horizontal casting, and add a 16-mesh casting filter to filter the scale at the gate, control the casting temperature to 720°C, the casting speed to 7.5t/h, and the cooling water temperature 25°C, and the billet temperature is 550°C.
- Si is not added to the composition of the aluminum alloy for extrusion, and the rest is the same as in Example 1.
- the temperature during the annealing treatment in S7 was 560° C., and the rest were the same as in Example 1.
- the time during the annealing treatment in S7 was 85h (a) and 103h (b), and the rest were the same as in Example 1.
- Example 1 has increased respectively compared with Comparative Examples 1-9: 9.52%, 8.49%, 8.49%, 16.16%, 7.48%, 9.52%, 17.35%, 15%, 15% (a), 12.75% (b); From elongation aspect, embodiment 1 has improved respectively compared with example 1-9: 30.56%, 34.29%, 30.56%, 56.67%, 27.03%, 38.24%, 56.67%, 38.24% %, 42.42% (a), 38.24% (b); from the aspect of product qualified rate, the unqualified rate of embodiment 1 has reduced respectively compared with comparative example 1-9: 82.76%, 79.17%, 81.48%, 84.38%, 79.17% %, 80%, 82.76%, 77.27%, 82.14% (a), 82.76% (b); from the aspect of mold life, embodiment 1 has improved respectively compared with comparative example 1-9: 27.91%, 25%, 22.22%, 197.3%, 26.44%,
- embodiment 1 has improved 2.4 compared with comparative example 1, and embodiment 1 has improved 2.2 compared with comparative example 2, and embodiment 1 has improved 2 compared with comparative example 3, and embodiment 1 has improved 7.3 compared with comparative example 4 , the difference sum of comparative examples 1-3 and embodiment 1 is 6.4 (7.3 less than the difference value 7.3 of comparative example 4 and embodiment 1), it can be seen that the combined effect of Er, Si and Be improves the sum of the effect of using separately than respectively up 10.61%.
- the present invention increases the content of manganese element, forms FeMnAl 6 phase by adding Zn, Fe, Er, reduces the solid solution of Mn in the aluminum matrix, and improves the ductility of the alloy. At the same time, it cooperates with Zn and Er to further reduce the solid solution of Mn and reduce the segregation phenomenon, refine the coarse phase in the structure, and solve the problem of high segregation and unevenness of Mn element.
- Zn and Er can assist in the elimination of Si element Existing broken wall or shrinkage porosity problem, Zn, Fe, Er can significantly improve the processing performance of aluminum alloy material; From the above table we can know (also taking extrusion die life as an example), embodiment 1 has improved 2.4% compared with comparative example 1 , embodiment 1 has improved 2.3 compared with comparative example 5, and embodiment 1 has improved 2.1 compared with comparative example 6, and embodiment 1 has improved 7.5 compared with comparative example 7, and the difference sum of comparative examples 1,5,6 and embodiment 1 is 6.8 (7.5 less than the difference between Comparative Example 7 and Example 1), it can be seen that the combined effect of Er, Fe and Zn is 10.29% higher than the sum of the effects of separate use. Therefore, there is a synergistic effect among various elements in the present invention, which improves the comprehensive performance of the aluminum alloy material, and each component is indispensable.
- the present invention improves the performance of the material by optimizing the production process and heat treatment process: during the production process, refining is carried out in both the smelting furnace and the holding furnace, two-stage filtration is added and casting filter screens are added to filter most of the impurities, and the substrate is purified with Er and other elements; the heat treatment process Among them, the inventors have found through a large number of experiments that the optimal heat treatment condition is to keep warm at 450-460°C for 88-100h, and the grains grow uniformly after annealing, as shown in Figure 1 (A is the aluminum alloy prepared in Example 1, and B is the The aluminum alloy prepared in Example 8, C is the aluminum alloy b prepared in Comparative Example 9, and D is the aluminum alloy prepared in Comparative Example 2), the grain size in A is uniform, while the extruded walls of B-D are uneven, and C is due to the excessive holding time Long, coarse grains, and segregation phenomenon occurs in the preparation process, the material performance is unstable during extrusion, and aluminum sticking and wall breaking appear.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacturing & Machinery (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Extrusion Of Metal (AREA)
- Continuous Casting (AREA)
Abstract
La présente invention concerne un alliage d'aluminium destiné à l'extrusion. Les constituants de l'alliage d'aluminium et le pourcentage en masse de chaque constituant sont les suivants : 0,1-0,2 % de Si, 0,15-0,25 % de Fe, 1,8-2,4 % de Mn, 0,05-0,18 % de Zn, 0,03-0,06 % d'Er, 0,008-0,04 % de Ti, 0,04-0,08 % de Be et 0,01-0,02 % de V, le reste étant de l'Al et des impuretés inévitables, la quantité totale des impuretés étant inférieure ou égale à 0,015 %. L'alliage d'aluminium est préparé au moyen des étapes du processus comprenant la fusion, l'alliage, l'affinage, le traitement en ligne de l'aluminium fondu, la coulée continue, le laminage continu, le refroidissement et la reprise, le traitement de recuit, etc. L'alliage d'aluminium de la présente invention est amélioré considérablement quant à la résistance à la corrosion, la résistance du matériau, la fluidité et la continuité structurale, de sorte que la capacité de support de pression d'un matériau d'extrusion préparé soit améliorée considérablement, et que sa durée de vie soit prolongée.
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CN202111050518.2 | 2021-09-08 | ||
CN202111050518.2A CN113846249B (zh) | 2021-09-08 | 2021-09-08 | 一种挤压用铝合金及其制备方法 |
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CN116555606A (zh) * | 2023-05-15 | 2023-08-08 | 上海萨新东台热传输材料有限公司 | 一种耐磨型铝合金管道的制备方法 |
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- 2021-09-08 CN CN202111050518.2A patent/CN113846249B/zh active Active
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EP2177638A1 (fr) * | 2008-10-15 | 2010-04-21 | "Impexmetal" S.A. | Alliage d'aluminium, en particulier pour la fabrication d'échangeurs thermiques |
CN102286679A (zh) * | 2011-09-02 | 2011-12-21 | 上海交通大学 | 用于热交换器的稀土铝合金及其制备方法 |
CN103103404A (zh) * | 2013-01-28 | 2013-05-15 | 华峰铝业股份有限公司 | 一种耐蚀铝锰合金及其制备方法 |
JP2018178170A (ja) * | 2017-04-06 | 2018-11-15 | 三菱アルミニウム株式会社 | 耐エロージョン性に優れる薄肉フィン材、耐エロージョン性に優れる薄肉フィン材の製造方法および熱交換器の製造方法 |
CN108977699A (zh) * | 2018-08-17 | 2018-12-11 | 江苏亨通电力特种导线有限公司 | 一种挤压成型用铝材的制备方法及对应的铝合金材料 |
CN109371295A (zh) * | 2018-11-23 | 2019-02-22 | 沈阳航空航天大学 | 一种高Mn含量Al-Mn合金及其制备方法 |
CN113846249A (zh) * | 2021-09-08 | 2021-12-28 | 江苏亨通电力特种导线有限公司 | 一种挤压用铝合金及其制备方法 |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
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CN116555606A (zh) * | 2023-05-15 | 2023-08-08 | 上海萨新东台热传输材料有限公司 | 一种耐磨型铝合金管道的制备方法 |
CN116555606B (zh) * | 2023-05-15 | 2024-01-02 | 上海萨新东台热传输材料有限公司 | 一种耐磨型铝合金管道的制备方法 |
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CN113846249B (zh) | 2022-07-08 |
CN113846249A (zh) | 2021-12-28 |
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