CN110396629B - A kind of 800MPa grade aluminum alloy extruded profile and preparation method thereof - Google Patents
A kind of 800MPa grade aluminum alloy extruded profile and preparation method thereof Download PDFInfo
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- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 36
- 238000002360 preparation method Methods 0.000 title claims abstract description 8
- 238000000034 method Methods 0.000 claims abstract description 38
- 239000000956 alloy Substances 0.000 claims abstract description 23
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 22
- 238000001125 extrusion Methods 0.000 claims abstract description 22
- 238000010438 heat treatment Methods 0.000 claims abstract description 12
- 229910052706 scandium Inorganic materials 0.000 claims abstract description 5
- 229910052726 zirconium Inorganic materials 0.000 claims abstract description 5
- 239000012535 impurity Substances 0.000 claims abstract description 3
- 229910052742 iron Inorganic materials 0.000 claims abstract 2
- 238000005266 casting Methods 0.000 claims description 54
- 238000000265 homogenisation Methods 0.000 claims description 38
- 238000004321 preservation Methods 0.000 claims description 34
- 239000006104 solid solution Substances 0.000 claims description 27
- 238000007670 refining Methods 0.000 claims description 26
- 230000008569 process Effects 0.000 claims description 21
- 238000002844 melting Methods 0.000 claims description 18
- 230000008018 melting Effects 0.000 claims description 18
- 238000001816 cooling Methods 0.000 claims description 16
- 229910052751 metal Inorganic materials 0.000 claims description 12
- 239000002184 metal Substances 0.000 claims description 12
- 230000032683 aging Effects 0.000 claims description 11
- 238000001192 hot extrusion Methods 0.000 claims description 9
- 239000000126 substance Substances 0.000 claims description 7
- 238000007599 discharging Methods 0.000 claims description 6
- 229910052802 copper Inorganic materials 0.000 claims description 5
- 239000000463 material Substances 0.000 claims description 5
- 230000004927 fusion Effects 0.000 claims description 2
- 229910052725 zinc Inorganic materials 0.000 claims 1
- 238000009749 continuous casting Methods 0.000 abstract description 5
- 239000007769 metal material Substances 0.000 abstract description 2
- 239000004615 ingredient Substances 0.000 abstract 1
- 239000002994 raw material Substances 0.000 abstract 1
- 229910052782 aluminium Inorganic materials 0.000 description 8
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 8
- 229910018182 Al—Cu Inorganic materials 0.000 description 4
- 239000003795 chemical substances by application Substances 0.000 description 4
- 238000003756 stirring Methods 0.000 description 4
- 229910018580 Al—Zr Inorganic materials 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 238000004663 powder metallurgy Methods 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- 238000006467 substitution reaction Methods 0.000 description 2
- 239000013585 weight reducing agent Substances 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000000694 effects Effects 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
- C22C21/10—Alloys based on aluminium with zinc as the next major constituent
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/053—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with zinc as the next major constituent
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Abstract
一种800MPa级铝合金挤压型材及其制备方法。本发明属于金属材料技术领域，提供一种可用于半连续铸造法制备的大尺寸800MPa级铝合金挤压型材，按重量百分比计算成分为：Zn 9.0～12.5％，Mg 2.5～3.5％，Cu 0.8～1.5％，Zr 0.08～0.15％，Sc 0.05～0.25％，Fe≤0.10％，Si≤0.10％，其它杂质单个≤0.05％，总量≤0.15％，余量为Al。按合金成分配料，将原料熔化，经炉内精炼、静置后，采用半连续铸造法浇注成所需规格的合金锭；经进行三级均匀化工艺处理及挤压工艺成形，挤压型材厚度不小于40mm，宽度不小于150mm，经热处理后可供使用。本发明的新型铝合金挤压型材显微组织均匀、性能稳定，L向抗拉强度可达800MPa以上，屈服强度达750MPa，延伸率高于8％；LT向抗拉强度可达750MPa，屈服强度达700MPa，延伸率高于6％，制备的型材可广泛应用于航空、航天、核工业、交通运输、兵器等领域。An 800MPa grade aluminum alloy extruded profile and a preparation method thereof. The invention belongs to the technical field of metal materials, and provides a large-size 800MPa-grade aluminum alloy extruded profile that can be prepared by a semi-continuous casting method. ～1.5%, Zr 0.08～0.15%, Sc 0.05～0.25%, Fe≤0.10%, Si≤0.10%, other impurities individually≤0.05%, the total amount≤0.15%, and the balance is Al. According to the alloy ingredients, the raw materials are melted, refined in the furnace and allowed to stand, and then cast into alloy ingots of the required specifications by the semi-continuous casting method; Not less than 40mm, width not less than 150mm, available after heat treatment. The new aluminum alloy extrusion profile of the invention has uniform microstructure and stable performance, the L-direction tensile strength can reach more than 800MPa, the yield strength can reach 750MPa, and the elongation is higher than 8%; the LT-direction tensile strength can reach 750MPa, and the yield strength can reach 750MPa. Up to 700MPa, the elongation rate is higher than 6%, the prepared profiles can be widely used in aviation, aerospace, nuclear industry, transportation, weapons and other fields.
Description
Technical Field
The invention belongs to the technical field of metal materials, relates to an aluminum alloy extruded section, and particularly relates to a large-size 800 MPa-level aluminum alloy extruded section prepared by a semi-continuous casting method.
Background
With the increasing demand of ultra-light structure and low cost of future weaponry, the demand of high-strength aluminum alloy materials is strong. At present, small-size 800 MPa-grade aluminum alloy manufactured by adopting a semi-continuous casting technology and 800 MPa-grade aluminum alloy manufactured by adopting a powder metallurgy technology appear in China. The small-size 800MPa aluminum alloy cannot meet the application of weaponry due to size limitation; the ultra-high strength aluminum alloy prepared by the powder metallurgy method is difficult to be applied industrially due to the cost limitation. The large-size 800 MPa-grade low-cost aluminum alloy with stable performance and prepared by adopting the semi-continuous casting method has wide application prospect in the fields of aviation, aerospace, nuclear industry, transportation, weaponry and the like.
Currently, the industrially applied ultrahigh-strength aluminum alloy is 600 MPa-level aluminum alloy, and mainly comprises 7150 aluminum alloy (Al-7.6% of Zn-1.8% of Mg-2.0% of Cu-0.10% of Zr), 7055 aluminum alloy (Al-8% of Zn-2.0% of Mg-2.2% of Cu-0.10% of Zr) and the like. The invention relates to a preparation method of 800 MPa-grade aluminum alloy, which has a remarkable weight-reducing effect when replacing 600 MPa-grade aluminum alloy.
Disclosure of Invention
The purpose of the invention is: aiming at the practical application of the weight reduction requirement of the existing weapon, an 800 MPa-grade aluminum alloy section and a preparation method thereof are provided.
In order to solve the technical problem, the technical scheme of the invention is as follows:
in a first aspect, an 800MPa grade aluminum alloy extruded profile is provided, wherein the alloy comprises the following chemical components in percentage by weight: 9.0-12.5% of Zn, 2.5-3.5% of Mg, 0.8-1.5% of Cu, less than or equal to 0.10% of Fe, less than or equal to 0.10% of Si, less than or equal to 0.05% of other impurities, less than or equal to 0.15% of total amount, and the balance of Al.
1-2 of Zr and Sc are added in the chemical components of the alloy, and the weight percentage is as follows: zr0.08-0.15% and Sc 0.05-0.25%.
On the other hand, the preparation method of the 800 MPa-grade aluminum alloy extruded section comprises the following steps:
step one, preparing materials according to the chemical components and weight percentage of alloy, casting to obtain a semi-continuous ingot, wherein the size of the ingot is
Step two, carrying out three-stage homogenization treatment on the semicontinuous ingot casting, which comprises the following specific steps:
the first-stage homogenization temperature is 390-410 ℃, and the heat preservation time is 20-24 h; the second-stage homogenization temperature is 460-470 ℃; the heat preservation time is 15-24 h; the third-stage homogenization temperature is 470-478 ℃, the heat preservation time is 15-24 h, and the total heat preservation time is more than 50 h;
step three, performing hot extrusion after the homogenized cast ingot is peeled, wherein the extrusion ratio is controlled to be 20 or more, and the thickness of the final extruded section is not less than 40mm, and the width is not less than 150 mm;
and step four, carrying out solid solution and aging heat treatment on the section.
Preferably, the second step is started within 3h after the fusion casting in the first step is finished. And the cast ingot is prevented from cracking in the placing process.
The casting process in the first step is as follows:
(1) melting in a melting furnace, wherein the melting temperature is 700-780 ℃;
(2) refining the completely melted metal, wherein the temperature of the metal is maintained within the range of 690-730 ℃ during refining;
(3) fully standing for at least 30min after refining;
(4) and (3) starting casting after fully standing, wherein the casting temperature is 690-700 ℃, the casting speed is 15-22 mm/min, and the casting pressure is 0.03-0.08 MPa.
And step two, after homogenization is finished, cooling along with the furnace to below 150 ℃, discharging and air cooling.
Preferably, the parameters in the process of the step three hot extrusion technology are as follows: the blank temperature is 350-375 ℃, and the extrusion speed is 1-4 m/min.
Preferably, the solid solution in the fourth step adopts two-stage solid solution, the first-stage solid solution temperature is 455-460 ℃, and the second-stage solid solution temperature is: 465 to 477 ℃.
Preferably, the aging in the fourth step adopts peak aging, and the process comprises the following steps: keeping the temperature at 90-125 ℃ for 10-72 h.
The invention has the beneficial effects that:
the sectional material prepared by the method has the size thickness not less than 40mm and the width not less than 150mm, the L-direction tensile strength of the material can reach more than 800MPa, the yield strength reaches 750MPa, and the elongation is higher than 8 percent; the LT tensile strength can reach 750MPa, the yield strength can reach 700MPa, and the elongation is higher than 6%. The aluminum alloy weight reduction efficiency of the section bar can reach more than 20% by replacing 600MPa grade 7150 and 7055 aluminum alloy, and the section bar has wide application prospect.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the following description will clearly and completely describe the embodiments. It is to be understood that the embodiments described are only a few embodiments of the present invention, and not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Features of various aspects of embodiments of the invention will be described in detail below. In the following detailed description, numerous specific details are set forth in order to provide a thorough understanding of the present invention. It will be apparent, however, to one skilled in the art that the present invention may be practiced without these specific details. The following description of the embodiments is merely intended to better understand the present invention by illustrating examples thereof. The present invention is not limited to any particular arrangement or method provided below, but rather covers all product structures, any modifications, alterations, etc. of the method covered without departing from the spirit of the invention.
In the following description, well-known structures and techniques are not shown to avoid unnecessarily obscuring the present invention.
Example 1:
the preparation process of the alloy comprises the following steps:
(1) the alloy proportion is Zn: 9.0%, Mg: 2.5%, Cu: 0.8 percent; preparing 99.99 percent of refined Al ingot, pure Zn ingot, pure Mg ingot and Al-Cu intermediate alloy according to the weight percentage;
(2) melting in a melting furnace, wherein the melting temperature is 700-780 ℃;
(3) adding a refining agent into the completely melted metal, continuously stirring for refining, wherein the refining is carried out in batches, and the metal temperature is maintained within the range of 690-750 ℃ during refining;
(4) after refining, standing in vacuum, vacuumizing to 1000-1200 Pa, and standing for 30-35 min;
(5) the casting is started after the aluminum base is fully stood, the thickness of the pure aluminum base is not less than 100mm, the casting temperature is 690-700 ℃, the casting speed is 15-22 mm/min, and the casting pressure is controlled at 0.03-0.08 MPa;
(6) casting to obtain semi-continuous cast ingot with the size of the cast ingot
(7) Homogenizing the cast ingot within 3 hours after the casting is finished;
(8) the ingot casting adopts a three-level homogenization process,
the ingot casting homogenization process comprises the following steps: the first-stage homogenization temperature is 390 ℃, and the heat preservation time is 20 h; the second-stage homogenization temperature is 460 ℃; the heat preservation time is 15 h; the third-stage homogenization temperature is 470 ℃, and the heat preservation time is 15 hours;
(9) after homogenization, cooling along with the furnace to below 150 ℃, discharging and air cooling;
(10) peeling the homogenized cast ingot, and casting the ingot with the diameter after peeling
(11) Selecting a mould to carry out hot extrusion on the cast ingot, wherein the extrusion ratio is 20, and the size of the mould is 40 multiplied by 150 mm;
(12) in the extrusion process, the initial heating temperature of the cast ingot is 360 ℃, the temperature of the cast ingot in the extrusion process is controlled to be 350-375 ℃, and the extrusion speed is controlled to be 1-4 m/min;
(13) the extruded section is subjected to two-stage solid solution, and the solid solution system is as follows: the first-stage solid solution temperature is 455 ℃, the heat preservation time is 2 hours, and the second-stage solid solution temperature is as follows: keeping the temperature at 470 ℃ for 4 h;
(14) the extruded section is subjected to peak aging heat treatment, and the heat preservation temperature is as follows: keeping the temperature at 90 ℃ for 72h, and cooling with air in the furnace.
The room temperature tensile properties of the profile obtained in example 1 are shown in Table 1 below, where σ isbFor tensile strength, σ0.2For yield strength, δ is elongation.
TABLE 1
Example 2:
(1) the alloy proportion is Zn: 10.5%, Mg: 3.0%, Cu: 1.1%, Zr: 0.11 percent; preparing 99.99 percent of refined Al ingot, pure Zn ingot, pure Mg ingot, Al-Cu intermediate alloy and Al-Zr intermediate alloy according to the weight percentage;
(2) melting in a melting furnace, wherein the melting temperature is 700-780 ℃;
(3) adding a refining agent into the completely melted metal, continuously stirring for refining, wherein the refining is carried out in batches, and the metal temperature is maintained within the range of 690-750 ℃ during refining;
(4) after refining, standing in vacuum, vacuumizing to 1000-1200 Pa, and standing for 30-35 min;
(5) the casting is started after the aluminum base is fully stood, the thickness of the pure aluminum base is not less than 100mm, the casting temperature is 690-700 ℃, the casting speed is 15-22 mm/min, and the casting pressure is controlled at 0.03-0.08 MPa;
(6) casting to obtain semi-continuous cast ingot with the size of the cast ingot
(7) Homogenizing the cast ingot within 3 hours after the casting is finished;
(8) the ingot casting adopts a three-level homogenization process,
the ingot casting homogenization process comprises the following steps: the first-stage homogenization temperature is 400 ℃, and the heat preservation time is 22 h; the second-stage homogenization temperature is 465 ℃; the heat preservation time is 20 h; the third-stage homogenization temperature is 474 ℃ and the heat preservation time is 20 hours;
(9) after homogenization, cooling along with the furnace to below 150 ℃, discharging and air cooling;
(10) peeling the homogenized cast ingot, and casting the ingot with the diameter after peeling
(11) Selecting a mould to carry out hot extrusion on the cast ingot, wherein the extrusion ratio is 25, and the size of the mould is 45 multiplied by 175 mm;
(12) in the extrusion process, the initial heating temperature of the cast ingot is 360 ℃, the temperature of the cast ingot in the extrusion process is controlled to be 350-375 ℃, and the extrusion speed is controlled to be 1-4 m/min;
(13) the extruded section is subjected to two-stage solid solution, and the solid solution system is as follows: the first-stage solid solution temperature is 458 ℃, the heat preservation time is 2 hours, and the second-stage solid solution temperature is as follows: 471 ℃, and the heat preservation time is 4 hours;
(14) the extruded section is subjected to peak aging heat treatment, and the heat preservation temperature is as follows: keeping the temperature at 110 ℃ for 32h, and cooling with air in the furnace.
The room temperature tensile properties of the profile obtained in example 2 are shown in Table 2 below, where σ isbFor tensile strength, σ0.2The yield strength, delta the elongation,
TABLE 2
Example 3:
(1) the alloy proportion is Zn: 11.0%, Mg: 3.0%, Cu: 1.1%, Sc: 0.15 percent; preparing 99.99 percent of refined Al ingot, pure Zn ingot, pure Mg ingot, Al-Cu intermediate alloy and Al-Zr intermediate alloy according to the weight percentage;
(2) melting in a melting furnace, wherein the melting temperature is 700-780 ℃;
(3) adding a refining agent into the completely melted metal, continuously stirring for refining, wherein the refining is carried out in batches, and the metal temperature is maintained within the range of 690-750 ℃ during refining;
(4) after refining, standing in vacuum, vacuumizing to 1000-1200 Pa, and standing for 30-35 min;
(5) the casting is started after the aluminum base is fully stood, the thickness of the pure aluminum base is not less than 100mm, the casting temperature is 690-700 ℃, the casting speed is 15-22 mm/min, and the casting pressure is controlled at 0.03-0.08 MPa;
(6) casting to obtain semi-continuous cast ingot with the size of the cast ingot
(7) Homogenizing the cast ingot within 3 hours after the casting is finished;
(8) the ingot casting adopts a three-level homogenization process,
the ingot casting homogenization process comprises the following steps: the first-stage homogenization temperature is 400 ℃, and the heat preservation time is 22 h; the second-stage homogenization temperature is 465 ℃; the heat preservation time is 20 h; the third-stage homogenization temperature is 474 ℃ and the heat preservation time is 20 hours;
(9) after homogenization, cooling along with the furnace to below 150 ℃, discharging and air cooling;
(10) peeling the homogenized cast ingot, and casting the ingot with the diameter after peeling
(11) Selecting a mould to carry out hot extrusion on the cast ingot, wherein the extrusion ratio is 20, and the size of the mould is 40 multiplied by 150 mm;
(12) in the extrusion process, the initial heating temperature of the cast ingot is 360 ℃, the temperature of the cast ingot in the extrusion process is controlled to be 350-375 ℃, and the extrusion speed is controlled to be 1-4 m/min;
(13) the extruded section is subjected to two-stage solid solution, and the solid solution system is as follows: the first-stage solid solution temperature is 458 ℃, the heat preservation time is 2 hours, and the second-stage solid solution temperature is as follows: 471 ℃, and the heat preservation time is 4 hours;
(14) the extruded section is subjected to peak aging heat treatment, and the heat preservation temperature is as follows: keeping the temperature at 110 ℃ for 32h, and cooling with air in the furnace.
The room temperature tensile properties of the profile obtained in example 3 are shown in Table 3 below, where σ isbFor tensile strength, σ0.2The yield strength, delta the elongation,
TABLE 3
Example 4:
(1) the alloy proportion is Zn: 12.5%, Mg: 3.5%, Cu: 1.5%, Zr: 0.15 percent and Sc 0.25 percent; preparing 99.99 percent of refined Al ingot, pure Zn ingot, pure Mg ingot, Al-Cu intermediate alloy, Al-Zr intermediate alloy and Al-Sc intermediate alloy according to the weight percentage;
(2) melting in a melting furnace, wherein the melting temperature is 700-780 ℃;
(3) adding a refining agent into the completely melted metal, continuously stirring for refining, wherein the refining is carried out in batches, and the metal temperature is maintained within the range of 690-750 ℃ during refining;
(4) after refining, standing in vacuum, vacuumizing to 1000-1200 Pa, and standing for 30-35 min;
(5) the casting is started after the aluminum base is fully stood, the thickness of the pure aluminum base is not less than 100mm, the casting temperature is 690-700 ℃, the casting speed is 15-22 mm/min, and the casting pressure is controlled at 0.03-0.08 MPa;
(6) casting to obtain semi-continuous cast ingot with the size of the cast ingot
(7) Homogenizing the cast ingot within 3 hours after the casting is finished;
(8) the ingot casting adopts a three-level homogenization process,
the ingot casting homogenization process comprises the following steps: the first-stage homogenization temperature is 410 ℃, and the heat preservation time is 24 hours; the second-stage homogenization temperature is 470 ℃; the heat preservation time is 24 h; the third-stage homogenization temperature is 478 ℃, and the heat preservation time is 24 hours;
(9) after homogenization, cooling along with the furnace to below 150 ℃, discharging and air cooling;
(10) peeling the homogenized cast ingot, and casting the ingot with the diameter after peeling
(11) Selecting a mould to carry out hot extrusion on the cast ingot, wherein the extrusion ratio is 30, and the size of the mould is 40 multiplied by 150 mm;
(12) in the extrusion process, the initial heating temperature of the cast ingot is 360 ℃, the temperature of the cast ingot in the extrusion process is controlled to be 350-375 ℃, and the extrusion speed is controlled to be 1-4 m/min;
(13) the extruded section is subjected to two-stage solid solution, and the solid solution system is as follows: the first-stage solid solution temperature is 460 ℃, the heat preservation time is 2h, and the second-stage solid solution temperature is: 477 ℃, and keeping the temperature for 4 hours;
(14) the extruded section is subjected to peak aging heat treatment, and the heat preservation temperature is as follows: keeping the temperature at 125 ℃ for 10h, and cooling with air in the furnace.
The room temperature tensile properties of the profile obtained in example 4 are shown in Table 4 below, where σ isbFor tensile strength, σ0.2The yield strength, delta the elongation,
TABLE 4 tensile Properties at room temperature of the profiles
From the performance analysis, the large-size 800 MPa-grade aluminum alloy section provided by the invention has stable performance, the L-directional ultimate tensile strength is stable and reaches more than 800MPa, the elongation is higher than 8%, the LT-directional performance tensile strength is stable and reaches more than 750MPa, the elongation is higher than 6%, the anisotropy difference is small, and the large-size 800 MPa-grade aluminum alloy section has a wide application prospect in the fields of aviation, aerospace, nuclear industry, transportation, weaponry and the like.
Finally, it should be noted that: the above embodiments are only for illustrating the technical solutions of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art can easily conceive various equivalent modifications or substitutions within the technical scope of the present invention, and these modifications or substitutions should be covered within the scope of the present invention.
Claims (9)
1. An 800 MPa-level aluminum alloy extruded section is characterized in that: the alloy comprises the following chemical components in percentage by weight: 10.5 to 12.5 percent of Zn, 3.0 to 3.5 percent of Mg, 0.8 to 1.5 percent of Cu, less than or equal to 0.10 percent of Fe, less than or equal to 0.10 percent of Si, less than or equal to 0.05 percent of other impurities, less than or equal to 0.15 percent of total amount, and the balance of Al;
the 800 MPa-grade aluminum alloy extruded section is prepared by the following method:
step one, preparing materials according to the chemical components and weight percentage of alloy, casting to obtain a semi-continuous ingot, wherein the size of the ingot is
Step two, carrying out three-stage homogenization treatment on the semicontinuous ingot casting, which comprises the following specific steps:
the first-stage homogenization temperature is 390-410 ℃, and the heat preservation time is 20-24 h; the second-stage homogenization temperature is 460-470 ℃; the heat preservation time is 15-24 h; the third-stage homogenization temperature is 470-478 ℃, the heat preservation time is 15-24 h, and the total heat preservation time is more than 50 h;
step three, performing hot extrusion after the homogenized cast ingot is peeled, wherein the extrusion ratio is controlled to be 20 or more, and the thickness of the final extruded section is not less than 40mm, and the width is not less than 150 mm;
and step four, carrying out solid solution and aging heat treatment on the section.
2. The 800MPa grade aluminum alloy extruded profile of claim 1, wherein: 1-2 of Zr and Sc are added in the chemical components of the alloy, and the weight percentage is as follows: 0.08-0.15% of Zr and 0.05-0.25% of Sc.
3. A method for preparing an 800MPa grade aluminium alloy extruded profile according to claim 1 or 2, characterized in that: the preparation method comprises the following steps:
step one, preparing materials according to the chemical components and weight percentage of alloy, casting to obtain a semi-continuous ingot, wherein the size of the ingot is
Step two, carrying out three-stage homogenization treatment on the semicontinuous ingot casting, which comprises the following specific steps:
the first-stage homogenization temperature is 390-410 ℃, and the heat preservation time is 20-24 h; the second-stage homogenization temperature is 460-470 ℃; the heat preservation time is 15-24 h; the third-stage homogenization temperature is 470-478 ℃, the heat preservation time is 15-24 h, and the total heat preservation time is more than 50 h;
step three, performing hot extrusion after the homogenized cast ingot is peeled, wherein the extrusion ratio is controlled to be 20 or more, and the thickness of the final extruded section is not less than 40mm, and the width is not less than 150 mm;
and step four, carrying out solid solution and aging heat treatment on the section.
4. The method for preparing the 800MPa grade aluminum alloy extruded profile according to claim 3, characterized in that: and the second step is started within 3h after the fusion casting in the first step is finished.
5. The method for preparing the 800MPa grade aluminum alloy extruded profile according to claim 3, characterized in that: the casting process in the first step is as follows:
(1) melting in a melting furnace, wherein the melting temperature is 700-780 ℃;
(2) refining the completely melted metal, wherein the temperature of the metal is maintained within the range of 690-730 ℃ during refining;
(3) standing for at least 30min after refining;
(4) and (3) starting casting after standing, wherein the casting temperature is 690-700 ℃, the casting speed is 15-22 mm/min, and the casting pressure is 0.03-0.08 MPa.
6. The method for preparing the 800MPa grade aluminum alloy extruded profile according to claim 3, characterized in that: and step two, after homogenization is finished, cooling along with the furnace to below 150 ℃, discharging and air cooling.
7. The method for preparing the 800MPa grade aluminum alloy extruded profile according to claim 3, characterized in that: the parameters in the hot extrusion technological process in the third step are as follows: the blank temperature is 350-375 ℃, and the extrusion speed is 1-4 m/min.
8. The method for preparing the 800MPa grade aluminum alloy extruded profile according to claim 3, characterized in that: in the fourth step, two-stage solid solution is adopted for solid solution, the first-stage solid solution temperature is 455-460 ℃, and the second-stage solid solution temperature is: 465 to 477 ℃.
9. The method for preparing the 800MPa grade aluminum alloy extruded profile according to claim 3, characterized in that: the aging in the fourth step adopts peak aging, and the process comprises the following steps: keeping the temperature at 90-125 ℃ for 10-72 h.
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| CN110863128B (en) * | 2019-12-28 | 2021-06-04 | 东北轻合金有限责任公司 | Preparation method of 640 MPa-grade aluminum alloy extruded material for aviation |
| CN112522559A (en) * | 2020-12-03 | 2021-03-19 | 江阴金属材料创新研究院有限公司 | High intergranular corrosion resistance aircraft landing gear aluminum alloy and preparation method thereof |
| CN113215458B (en) * | 2021-07-02 | 2023-02-24 | 中国航发北京航空材料研究院 | Aluminum alloy and manufacturing method thereof |
| CN113737068B (en) * | 2021-08-19 | 2022-10-04 | 中铝材料应用研究院有限公司 | High-strength and high-toughness corrosion-resistant 7xxx series aluminum alloy and processing method thereof |
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| CN115008063A (en) * | 2022-05-20 | 2022-09-06 | 江苏科技大学 | A kind of aluminum alloy welding wire containing scandium and preparation method thereof |
| CN115233055B (en) * | 2022-07-25 | 2023-09-22 | 安徽工业大学 | Aluminum extrusion profile convenient to recycle and preparation method thereof |
| CN117127071A (en) * | 2023-10-27 | 2023-11-28 | 中铝材料应用研究院有限公司 | Aluminum alloy material and preparation method thereof |
| CN117127130B (en) * | 2023-10-27 | 2024-02-20 | 中铝材料应用研究院有限公司 | Multistage homogenization treatment method for aluminum alloy and aluminum alloy |
| CN117904500B (en) * | 2023-11-15 | 2024-09-13 | 东北轻合金有限责任公司 | 800 MPa-grade ultrahigh-strength aluminum alloy round ingot and preparation method thereof |
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