CN115896560A - High-performance aluminum alloy material and preparation method thereof - Google Patents

High-performance aluminum alloy material and preparation method thereof Download PDF

Info

Publication number
CN115896560A
CN115896560A CN202211534468.XA CN202211534468A CN115896560A CN 115896560 A CN115896560 A CN 115896560A CN 202211534468 A CN202211534468 A CN 202211534468A CN 115896560 A CN115896560 A CN 115896560A
Authority
CN
China
Prior art keywords
temperature
aluminum alloy
aluminum
degassing
alloy material
Prior art date
Legal status (The legal status 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 status listed.)
Granted
Application number
CN202211534468.XA
Other languages
Chinese (zh)
Other versions
CN115896560B (en
Inventor
孙大永
崔国荣
姜华茂
范艳会
邱文娟
张营
王英睿
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zhongke Lixiang Technology Co ltd
Original Assignee
Zhongke Lixiang Technology Co ltd
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 Zhongke Lixiang Technology Co ltd filed Critical Zhongke Lixiang Technology Co ltd
Priority to CN202211534468.XA priority Critical patent/CN115896560B/en
Publication of CN115896560A publication Critical patent/CN115896560A/en
Application granted granted Critical
Publication of CN115896560B publication Critical patent/CN115896560B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P10/00Technologies related to metal processing
    • Y02P10/20Recycling

Landscapes

  • Manufacture And Refinement Of Metals (AREA)

Abstract

The invention belongs to the technical field of material processing, and particularly relates to a high-performance aluminum alloy material and a preparation method thereof, wherein the high-performance aluminum alloy material comprises the following chemical components in percentage by mass: 6.5 to 7.5 percent of Si, 0.52 to 0.58 percent of Mg, 0.10 to 0.20 percent of Ti and 0.000 to 0.2000 percent of Fe, and the amount of the alloy consists of Al and inevitable impurities. The preparation method of the high-performance aluminum alloy material provided by the invention is scientific and reasonable in design, the range of the element Mg is narrowed within the range of the components required by the national standard, and on the basis, a corresponding smelting process is established, wherein the smelting process comprises smelting temperature, components, a refining process and the like, so that the high-performance aluminum alloy material has a high-performance chemical basis; on the basis, by setting a reasonable solid solution aging treatment process, the high-performance aluminum alloy material with excellent mechanical property is obtained, and the requirements of the aerospace field on the mechanical property of the aluminum alloy material are met.

Description

High-performance aluminum alloy material and preparation method thereof
Technical Field
The invention belongs to the technical field of material processing, and particularly relates to a high-performance aluminum alloy material and a preparation method thereof.
Background
The development of light weight structure is promoted by increasing energy crisis and environmental pollution, and the application of aluminum alloy to various structural products instead of steel materials is a great trend. The development of modern science and technology puts forward higher and higher requirements on material performance, particularly, airplanes, satellites and the like which are light, flexible and excellent in performance need to be manufactured in the field of aerospace, and the aluminum alloy and the composite material thereof just can meet the requirements in the aspect. With the expansion of the application range of the aluminum alloy, higher requirements are also placed on the mechanical property and the processing property of the aluminum alloy.
At present, most researchers mainly take the solution aging process, and improve the performance of the aluminum alloy by optimizing the solution aging process, in the aluminum alloy, as precipitates of different types and different sizes are precipitated in the whole solution aging process, different reactions are generated to dislocations, generally, dislocations bypass the mechanism when passing through the precipitates with larger sizes, and cut the mechanism when passing through the precipitates with smaller sizes, and the different strengthening mechanisms enable the alloy to have different strengthening performances, so the types, sizes and distribution of the precipitates have important influence on the mechanical performance of the alloy.
The ZL114A aluminum alloy is a product developed by increasing the content of alloy element magnesium on the basis of ZL101A, and has excellent casting performance. Its corrosion resistance and other technological properties are similar to those of ZL 101. The existing ZL114A aluminum alloy has the problem of unsatisfactory mechanical property, and is difficult to meet the requirements of the aerospace field on the mechanical property of the aluminum alloy material.
Therefore, how to develop a new and high-performance ZL114A aluminum alloy material to meet the mechanical property of the aluminum alloy material in the aerospace field becomes a problem to be solved urgently.
Disclosure of Invention
The invention aims to overcome the problems in the prior art and provides a high-performance aluminum alloy material and a preparation method thereof.
In order to achieve the technical purpose and achieve the technical effect, the invention is realized by the following technical scheme:
the invention provides a high-performance aluminum alloy material, which comprises the following chemical components in percentage by mass:
Figure BDA0003977041020000021
the balance is made up of Al and unavoidable impurities.
Further, in the high-performance aluminum alloy material, the high-performance aluminum alloy material comprises the following chemical components in percentage by mass:
Figure BDA0003977041020000022
the balance is made up of Al and unavoidable impurities.
Further, in the high-performance aluminum alloy material, the high-performance aluminum alloy material comprises the following chemical components in percentage by mass:
Figure BDA0003977041020000023
the balance is made up of Al and unavoidable impurities.
The invention provides a preparation method of a high-performance aluminum alloy material, which is characterized by comprising the following steps of:
1) Solution treatment: putting the aluminum alloy into a solution furnace, raising the temperature to 530-540 ℃ at a constant speed within 1-3 h, then preserving the temperature for 10-14 h, and carrying out solution treatment;
2) Quenching: carrying out water-cooling quenching on the aluminum alloy after the solid solution, wherein the quenching time is 10-20 min;
3) First time aging treatment: raising the temperature of the quenched aluminum alloy to 118-122 ℃ at a constant speed within 0.2-0.5 h, and carrying out primary aging treatment at the temperature for 2.5-3.5 h; after the first time effect treatment is finished, air cooling to room temperature;
4) And (3) secondary aging treatment: raising the temperature of the aluminum alloy subjected to air cooling to 158-162 ℃ at a constant speed within 0.4-0.8 h, and carrying out secondary aging treatment at the temperature for 4-5 h; and after the second aging treatment is finished, air cooling to room temperature.
Further, in the step 1), the batching and smelting process of the aluminum alloy ingot comprises the following steps:
1) Setting the temperature of the aluminum liquid: setting the molten aluminum in the crucible furnace at 760 ℃, and controlling the temperature of furnace gas at a corresponding temperature;
2) Adding silicon until the aluminum liquid in the crucible reaches 700 ℃, starting to add the crystalline silicon, immediately stirring after adding the crystalline silicon until the alloy is completely wrapped by the aluminum liquid, wherein the melting time of the alloy is 30-40 min, and stirring once every 10-15 min within the melting time;
6) Adding magnesium: when the temperature of the aluminum liquid reaches 680 ℃, pressing a magnesium block into the aluminum liquid by using a preheated bell jar, and prohibiting the bell jar from leaving the liquid level during the melting of the magnesium block;
7) Adding a titanium agent: when the temperature of the aluminum liquid reaches 730 ℃, adding a titanium agent, fully reacting the aluminum liquid on the surface of the aluminum liquid, fully stirring after 30min, and controlling the temperature of the aluminum liquid at 760 ℃;
8) Melting the alloy: keeping the temperature at 760 ℃ for 30-40 min until all the alloy elements are melted;
9) Primary degassing: the gas flow valve is opened at first, the flow is adjusted to be small at this moment, and the equipment automatically runs and then is adjusted to be proper; degassing parameter setting: the distance between the rotor and the crucible bottom is 100-150 mm; degassing gas is liquid argon, or the degassing parameters of argon on two sides of degassing are set as follows: the time is 40min, and the flow rate is 1.2-1.5 m 3 Setting the rotating speed at 400r/min and the gas outlet pressure at 0.03-0.07 Mpa;
10 Add slag-removing agent: after the degasser is started for 1-2 min, uniformly scattering G5550 granular deslagging agent on the surface of the aluminum liquid;
11 ) degassing is finished: after 40min, after the warning light is turned on after degassing is finished, cleaning the slag on the rotor, moving out the degassing machine, and then closing the gas valve;
12 Slagging: lightly stirring the surface of the aluminum liquid by using a preheated slag fishing tool, then collecting the aluminum slag together, and fishing out the slag by using the slag fishing tool;
13 Secondary degassing): setting parameters: the time is 20min, the flow is 1.2-1.5m3// h, the rotating speed is set to be 400r/min, and the air outlet pressure is 0.03-0.07 Mpa;
14 Addition of alterants and refiners: immediately putting the preheated aluminum-strontium alloy and TCB seed crystal alloy into the aluminum liquid after degassing starting;
15 Add slag-removing agent: after the degasser is started for 1-2 min, uniformly scattering 200G of G5550 granular deslagging agent on the surface of the molten aluminum;
16 Stirring and slag removing: lightly stirring the surface of the aluminum liquid by using a preheated slag fishing tool, then collecting the aluminum slag together, and fishing out the slag by using the slag fishing tool;
17 Chemical composition analysis of the sample: if the chemical components are unqualified, the method for adjusting the added elements is the same as the above method, and then degassing and stirring are carried out until the chemical components are qualified.
Further, in the step 1), the temperature is raised to 535 ℃ at a constant speed within 1-3 h, and then the temperature is kept for 10-14 h, and the solution treatment is carried out.
Further, in the step 1), the temperature is uniformly increased to 535 ℃ within 2h, and then the temperature is kept for 12h for solution treatment.
Further, in the step 2), water-cooling quenching is carried out by using room temperature water at 50-60 ℃, and the quenching time is 15min.
Further, in the step 3), the quenched aluminum alloy is heated to 120 ℃ within 0.2-0.5 h at a constant speed, and the first aging treatment is carried out at the temperature for 3h; and after the first time effect treatment is finished, air cooling to room temperature.
Further, in the step 4), the aluminum alloy after air cooling is heated to 160 ℃ at a constant speed within 0.4-0.8 h, and secondary aging treatment is carried out at the temperature for 4.5h.
The invention has the beneficial effects that:
the preparation method of the high-performance aluminum alloy material provided by the invention is scientific and reasonable in design, and firstly, in the range of the national standard required components, the range of the element Mg is narrowed through parameter matching, and the content of the element Mg is limited to be 0.52-0.58% from the range of 0.45-0.75%; on the basis, corresponding smelting processes including smelting temperature, components, refining processes and the like are established, so that the smelting process has a high-performance chemical basis. On the basis, by setting a reasonable solution aging treatment process, the high-performance aluminum alloy material with excellent mechanical properties (the tensile strength is more than or equal to 350MPa, and the elongation after fracture is more than or equal to 6%) is obtained, and the requirements of the aerospace field on the mechanical properties of the aluminum alloy material are met.
Of course, it is not necessary for any product to achieve all of the above advantages at the same time in the practice of the invention.
Detailed Description
The technical solutions will be described clearly and completely in the following with reference to the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the 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.
A high-performance aluminum alloy material comprises the following chemical components in percentage by mass:
Figure BDA0003977041020000051
the balance is made up of Al and unavoidable impurities.
The preparation method of the high-performance aluminum alloy material comprises the following steps:
1) Solution treatment: placing the aluminum alloy ingot into a solution furnace, raising the temperature to 530-540 ℃ at a constant speed within 1-3 h, then preserving the temperature for 10-14 h, and carrying out solution treatment;
2) Quenching: carrying out water cooling quenching on the aluminum alloy ingot after the solid solution treatment at 50-60 ℃, wherein the quenching time is 10-20 min;
3) First time aging treatment: raising the temperature of the quenched aluminum alloy ingot to 118-122 ℃ within 0.2-0.5 h at a constant speed, and carrying out primary aging treatment at the temperature for 2.5-3.5 h; after the first time effect treatment is finished, air cooling to room temperature; and (3) before the aging treatment is carried out, the furnace temperature is confirmed to be less than or equal to 100 ℃, and after the aging time reaches the specified time, the aluminum alloy cast ingot is immediately lifted out and is forbidden to stay in the aging furnace.
4) And (3) secondary aging treatment: raising the temperature of the aluminum alloy ingot after air cooling to 158-162 ℃ at a constant speed within 0.4-0.8 h, and carrying out secondary aging treatment at the temperature for 4-5 h; and after the second aging treatment is finished, air cooling to room temperature. And (3) confirming that the furnace temperature is less than or equal to 100 ℃ before the aging treatment is carried out, immediately hoisting the aluminum alloy cast ingot out after the aging time reaches the specified time, and forbidding the aluminum alloy cast ingot to stay in the aging furnace.
The specific batching and smelting process of the aluminum alloy ingot as the object to be subjected to solid solution aging treatment comprises the following steps:
1) And (3) calculating the burden ratio: the proportion of the aluminum ingot is 100 percent, the mass silicon crystallized silicon is less than or equal to 30 multiplied by 30mm, the mass silicon is less than or equal to 30g, and the silicon powder is discarded; b. recording the weight of the ingredients in an ingredient list and recording the serial numbers; c. the used materials are dried in the air and then used; d. the ingredients are calculated according to the mass percentage of the chemical components.
2) Weighing alloy materials: a. calculating the weight of each aluminum ingot; b, weighing the reclaimed materials by using an electronic scale; weighing crystalline silicon, magnesium ingot, titanium agent, aluminum-strontium alloy and TCB seed crystal alloy by using an electronic scale; c. a tolerance range of ± 0.5% of the weight is allowed.
3) Checking equipment: a. if the crucible is damaged, the crucible is immediately replaced if the crucible is damaged; b. whether the ammeter data are normal or not; c. whether the thermocouple and the protection tube are normal or not; d. whether the deaerator operates normally or not; e. the diameter of the rotor is less than 180mm, and the slag stopping plate is damaged seriously and is replaced immediately.
4) Setting the temperature of the aluminum liquid: the molten aluminum in the crucible furnace is set at 760 ℃, and the temperature of furnace gas is controlled at a corresponding temperature. Feeding materials into the crucible, adding the recycled materials, cleaning, strictly preventing iron, sand, oil stain, aluminum scraps and the like from entering melting, and then feeding aluminum ingots. Safety measures are as follows: the recycled materials are gently thrown into the crucible, the crucible is easily broken due to overlarge impact, the recycled materials with moisture are dried and thrown into the crucible again, and aluminum liquid in the crucible is splashed to hurt people due to the moisture. Before adding the aluminum ingot, the aluminum ingot needs to be ensured to have no moisture, the aluminum ingot is put into a crucible furnace to enter lightly, and a large impact crucible is easy to break to cause the overflow of aluminum liquid. When a drop of water drops meets the aluminum liquid with the temperature of 700 ℃, the drop of water drops instantly expands to 6000 times of volume to generate aluminum liquid explosion, and the drop of water drops is dried before aluminum ingots and recycled materials are fed, so that no moisture is ensured. The tool contacting the aluminum liquid needs to be fully dried and is allowed to be used.
5) Adding silicon until the aluminum liquid in the crucible reaches 700 ℃, starting to add the crystalline silicon, immediately stirring after adding the crystalline silicon until the alloy is completely wrapped by the aluminum liquid, wherein the melting time of the alloy is 30-40 min, and stirring once every 10-15 min within the melting time to achieve the purpose of homogenizing the aluminum liquid alloy.
6) Adding magnesium: when the temperature of the aluminum liquid reaches 680 ℃, the preheated bell jar is used for pressing the magnesium block into the aluminum liquid for melting, the time is about 10min, and the bell jar is forbidden to leave the liquid surface during the melting of the magnesium block.
7) Adding a titanium agent: when the temperature of the aluminum liquid reaches 730 ℃, adding the titanium agent, fully reacting the aluminum liquid on the surface of the aluminum liquid (not moving the aluminum liquid), and fully stirring after 30min, wherein the temperature of the aluminum liquid is controlled at 760 ℃.
8) Melting the alloy: keeping the temperature of 760 ℃ for 30-40 min until all the alloy elements are melted.
9) Preparation before degassing: the degassing machine is pushed to the front end of the crucible, the degassing rotor is over against the center of the crucible for standby pushing of the degassing machine at the center of the crucible, attention is paid to whether a barrier is arranged in front of the rotor and the height of the rotor needs to be adjusted, and whether interference exists between the baffle and the edge of the crucible when the baffle falls is confirmed.
10 Degassing parameter settings: the distance between the rotor and the bottom of the crucible is 100 to 150mm, preferably 120 mm. Degassing gas is liquid argon or argon degassing parameters at two sides of degassing are set; for the first time: the time is 40min, and the flow rate is 1.2-1.5 m 3 The rotating speed is set to be 400r/min, and the air outlet pressure is 0.03-0.07 Mpa.
11 Primary degassing): the gas flow valve is opened firstly, the flow is reduced at the moment, and the equipment automatically runs and then is adjusted to the proper flow.
12 Add slag-removing agent: after the degasser is started for 1-2 min, 200G of G5550 granular deslagging agent is uniformly scattered on the surface of the aluminum liquid.
13 ) degassing is finished: after 40min, after the warning light lights after degassing, the degassing machine is moved out after the rotor slag is cleaned up, and then the gas valve is closed, if the gas source is closed in advance, the rotor hole is easily blocked by aluminum.
14 Slagging: lightly stirring the aluminum liquid surface by using a preheated slag fishing tool, then collecting the aluminum slag together, and fishing the slag by using the slag fishing tool.
15 Secondary degassing): setting parameters: the time is 20min, and the flow rate is 1.2-1.5 m 3 The rotating speed is set to be 400r/min, and the air outlet pressure is 0.03-0.07 Mpa.
16 Addition of alterants and refiners: and immediately putting the preheated aluminum-strontium alloy and TCB seed crystal alloy into the aluminum liquid after degassing starting.
17 Add slag-removing agent: after the degasser is started for 1-2 min, 200G of G5550 granular deslagging agent is uniformly scattered on the surface of the aluminum liquid.
18 Stirring and slag removing: lightly stirring the aluminum liquid surface by using a preheated slag fishing tool, then collecting the aluminum slag together, and fishing the slag by using the slag fishing tool.
19 Chemical composition analysis of the sample: if the chemical components are unqualified, the element adding method is adjusted according to the aluminum liquid unqualified adjusting method, and degassing and stirring are carried out until the chemical components are qualified.
20 Record sample block number: the oil pen is used for clearly and accurately writing on the sample according to the serial number of the dosage list.
21 Pin hole density experiments were done: and (5) standing the aluminum liquid for 10min. And (4) operating according to a pinhole density experimental specification, and judging that the product is qualified when the standard grade is more than 2. Density determination standard (not less than 2.63 g/cm) 3 Qualified).
The following embodiments are relevant to the present invention:
example 1
The embodiment provides a high-performance aluminum alloy material, and chemical components in the high-performance aluminum alloy material are shown in the following table 1:
TABLE 1
Figure BDA0003977041020000081
The preparation method of the high-performance aluminum alloy material comprises the following steps:
1) Solution treatment: placing the aluminum alloy ingot in a solution furnace, raising the temperature to 535 ℃ at a constant speed within 2h, then preserving the temperature for 12h, and carrying out solution treatment;
2) Quenching: carrying out water-cooling quenching at 55 ℃ on the aluminum alloy ingot after the solid solution, wherein the quenching time is 15min;
3) First time aging treatment: raising the temperature of the quenched aluminum alloy ingot to 120 ℃ within 0.25h at a constant speed, and carrying out primary aging treatment at the temperature for 3h; after the first time effect treatment is finished, air cooling to room temperature;
4) And (3) secondary aging treatment: raising the temperature of the aluminum alloy ingot after air cooling to 160 ℃ within 0.5h at a constant speed, and carrying out secondary aging treatment at the temperature for 4.5h; and after the second aging treatment is finished, air cooling to room temperature.
Example 2
This example provides a high-performance aluminum alloy material, which contains the chemical components as in example 1.
The preparation method of the high-performance aluminum alloy material comprises the following steps:
1) Solution treatment: placing the aluminum alloy ingot in a solution furnace, raising the temperature to 530 ℃ at a constant speed within 2.5h, then preserving the temperature for 12h, and carrying out solution treatment;
2) Quenching: carrying out water-cooling quenching at 55 ℃ on the aluminum alloy ingot after solid solution, wherein the quenching time is 10min;
3) First time aging treatment: raising the temperature of the quenched aluminum alloy ingot to 118 ℃ within 0.25h at a constant speed, and carrying out primary aging treatment at the temperature for 3.5h; after the first time effect treatment is finished, air cooling to room temperature;
4) And (3) secondary aging treatment: raising the temperature of the aluminum alloy ingot after air cooling to 158 ℃ at a constant speed within 0.5h, and carrying out secondary aging treatment at the temperature for 5h; and after the second aging treatment is finished, air cooling to room temperature.
Example 3
This embodiment provides a high-performance aluminum alloy material, which contains the chemical components as in embodiment 1.
The preparation method of the high-performance aluminum alloy material comprises the following steps:
1) Solution treatment: placing the aluminum alloy ingot in a solution furnace, raising the temperature to 540 ℃ at a constant speed within 2.5h, then preserving the temperature for 12h, and carrying out solution treatment;
2) Quenching: carrying out water-cooling quenching at 55 ℃ on the aluminum alloy ingot after the solid solution, wherein the quenching time is 20min;
3) First time aging treatment: raising the temperature of the quenched aluminum alloy ingot to 122 ℃ within 0.25h at a constant speed, and carrying out primary aging treatment at the temperature for 2.5h; after the first time effect treatment is finished, air cooling to room temperature;
4) And (3) secondary aging treatment: raising the temperature of the aluminum alloy ingot after air cooling to 162 ℃ within 0.5h at a constant speed, and carrying out secondary aging treatment at the temperature for 4h; and after the second aging treatment is finished, air cooling to room temperature.
Example 4
The embodiment provides a high-performance aluminum alloy material, and chemical components in the high-performance aluminum alloy material are shown in the following table 2:
TABLE 2
Figure BDA0003977041020000101
The preparation method of the high-performance aluminum alloy material comprises the following steps:
1) Solution treatment: placing the aluminum alloy ingot in a solution furnace, raising the temperature to 535 ℃ at a constant speed within 2h, then preserving the temperature for 12h, and carrying out solution treatment;
2) Quenching: carrying out water-cooling quenching at 55 ℃ on the aluminum alloy ingot after solid solution, wherein the quenching time is 15min;
3) First aging treatment: raising the temperature of the quenched aluminum alloy ingot to 120 ℃ within 0.25h at a constant speed, and carrying out primary aging treatment at the temperature for 3h; after the first time effect treatment is finished, air cooling to room temperature;
4) And (3) secondary aging treatment: raising the temperature of the aluminum alloy ingot after air cooling to 160 ℃ within 0.5h at a constant speed, and carrying out secondary aging treatment at the temperature for 4.5h; and after the second aging treatment is finished, air cooling to room temperature.
Example 5
The embodiment provides a high-performance aluminum alloy material, and the chemical components of the high-performance aluminum alloy material are as in embodiment 2.
The preparation method of the high-performance aluminum alloy material comprises the following steps:
1) Solution treatment: placing the aluminum alloy ingot in a solution furnace, raising the temperature to 530 ℃ at a constant speed within 2.5h, then preserving the temperature for 12h, and carrying out solution treatment;
2) Quenching: carrying out water-cooling quenching at 55 ℃ on the aluminum alloy ingot after solid solution, wherein the quenching time is 10min;
3) First time aging treatment: raising the temperature of the quenched aluminum alloy ingot to 118 ℃ within 0.25h at a constant speed, and carrying out primary aging treatment at the temperature for 3.5h; after the first time effect treatment is finished, air cooling to room temperature;
4) And (3) secondary aging treatment: raising the temperature of the aluminum alloy ingot after air cooling to 158 ℃ at a constant speed within 0.5h, and carrying out secondary aging treatment at the temperature for 5h; and after the second aging treatment is finished, air cooling to room temperature.
Example 6
The embodiment provides a high-performance aluminum alloy material, and the chemical components of the high-performance aluminum alloy material are as in embodiment 2.
The preparation method of the high-performance aluminum alloy material comprises the following steps:
1) Solution treatment: placing the aluminum alloy ingot in a solution furnace, raising the temperature to 540 ℃ at a constant speed within 2.5h, then preserving the temperature for 12h, and carrying out solution treatment;
2) Quenching: carrying out water-cooling quenching at 55 ℃ on the aluminum alloy ingot after the solid solution, wherein the quenching time is 20min;
3) First aging treatment: raising the temperature of the quenched aluminum alloy ingot to 122 ℃ within 0.25h at a constant speed, and carrying out primary aging treatment at the temperature for 2.5h; after the first time effect treatment is finished, air cooling to room temperature;
4) And (3) secondary aging treatment: raising the temperature of the aluminum alloy ingot after air cooling to 162 ℃ within 0.5h at a constant speed, and carrying out secondary aging treatment at the temperature for 4h; and after the second aging treatment is finished, air cooling to room temperature.
Example 7
The embodiment provides a high-performance aluminum alloy material, and chemical components in the high-performance aluminum alloy material are shown in the following table 3:
TABLE 3
Figure BDA0003977041020000121
The preparation method of the high-performance aluminum alloy material comprises the following steps:
1) Solution treatment: placing the aluminum alloy ingot in a solution furnace, raising the temperature to 535 ℃ at a constant speed within 2h, then preserving the temperature for 12h, and carrying out solution treatment;
2) Quenching: carrying out water-cooling quenching at 55 ℃ on the aluminum alloy ingot after the solid solution, wherein the quenching time is 15min;
3) First aging treatment: raising the temperature of the quenched aluminum alloy ingot to 120 ℃ within 0.25h at a constant speed, and carrying out primary aging treatment at the temperature for 3h; after the first time effect treatment is finished, air cooling to room temperature;
4) And (3) secondary aging treatment: raising the temperature of the aluminum alloy ingot after air cooling to 160 ℃ within 0.5h at a constant speed, and carrying out secondary aging treatment at the temperature for 4.5h; and after the second aging treatment is finished, air cooling to room temperature.
Example 8
This example provides a high-performance aluminum alloy material, which contains the chemical components as in example 7.
The preparation method of the high-performance aluminum alloy material comprises the following steps:
1) Solution treatment: placing the aluminum alloy ingot in a solution furnace, raising the temperature to 530 ℃ at a constant speed within 2.5h, then preserving the temperature for 12h, and carrying out solution treatment;
2) Quenching: carrying out water-cooling quenching at 55 ℃ on the aluminum alloy ingot after the solid solution, wherein the quenching time is 10min;
3) First aging treatment: raising the temperature of the quenched aluminum alloy ingot to 118 ℃ within 0.25h at a constant speed, and carrying out primary aging treatment at the temperature for 3.5h; after the first time effect treatment is finished, air cooling to room temperature;
4) And (3) secondary aging treatment: raising the temperature of the aluminum alloy ingot after air cooling to 158 ℃ at a constant speed within 0.5h, and carrying out secondary aging treatment at the temperature for 5h; and after the second aging treatment is finished, air cooling to room temperature.
Example 9
This example provides a high-performance aluminum alloy material, which contains the same chemical components as in example 7.
The preparation method of the high-performance aluminum alloy material comprises the following steps:
1) Solution treatment: placing the aluminum alloy ingot in a solution furnace, raising the temperature to 540 ℃ at a constant speed within 2.5h, then preserving the temperature for 12h, and carrying out solution treatment;
2) Quenching: carrying out water-cooling quenching at 55 ℃ on the aluminum alloy ingot after the solid solution, wherein the quenching time is 20min;
3) First aging treatment: raising the temperature of the quenched aluminum alloy ingot to 122 ℃ within 0.25h at a constant speed, and carrying out primary aging treatment at the temperature for 2.5h; after the first time effect treatment is finished, air cooling to room temperature;
4) And (3) secondary aging treatment: raising the temperature of the aluminum alloy ingot after air cooling to 162 ℃ within 0.5h at a constant speed, and carrying out secondary aging treatment at the temperature for 4h; and after the second aging treatment is finished, air cooling to room temperature.
The performance tests of the aluminum alloy materials subjected to solution aging treatment in examples 1 to 9 were carried out according to GB/T15115 to 2016, and the test results are shown in Table 4:
TABLE 4
Figure BDA0003977041020000141
The preferred embodiments of the invention disclosed above are intended to be illustrative only. The preferred embodiments are not intended to be exhaustive or to limit the invention to the precise embodiments disclosed. Obviously, many modifications and variations are possible in light of the above teaching. The embodiments were chosen and described in order to best explain the principles of the invention and the practical application, to thereby enable others skilled in the art to best understand the invention for and utilize the invention. The invention is limited only by the claims and their full scope and equivalents.

Claims (10)

1. The high-performance aluminum alloy material is characterized in that the high-performance aluminum alloy material comprises the following chemical components in percentage by mass:
Figure FDA0003977041010000011
the balance is made up of Al and unavoidable impurities.
2. The high-performance aluminum alloy material according to claim 1, which is characterized in that the high-performance aluminum alloy material comprises the following chemical components in percentage by mass:
Figure FDA0003977041010000012
the balance of Al and unavoidable impurities.
3. The high-performance aluminum alloy material of claim 2, wherein the high-performance aluminum alloy material comprises the following chemical components in percentage by mass:
Figure FDA0003977041010000013
the balance is made up of Al and unavoidable impurities.
4. The production method of a high-performance aluminum alloy material according to any one of claims 1 to 3, comprising the steps of:
1) Solution treatment: putting the aluminum alloy ingot into a solid solution furnace, raising the temperature to 530-540 ℃ at a constant speed within 1-3 h, then preserving the temperature for 10-14 h, and carrying out solid solution treatment;
2) Quenching: carrying out water-cooling quenching on the aluminum alloy ingot after the solid solution treatment, wherein the quenching time is 10-20 min;
3) First aging treatment: raising the temperature of the quenched aluminum alloy ingot to 118-122 ℃ at a constant speed within 0.2-0.5 h, and carrying out primary aging treatment at the temperature for 2.5-3.5 h; after the first time effect treatment is finished, air cooling to room temperature;
4) And (3) secondary aging treatment: raising the temperature of the aluminum alloy ingot after air cooling to 158-162 ℃ at a constant speed within 0.4-0.8 h, and carrying out secondary aging treatment at the temperature for 4-5 h; and after the second aging treatment is finished, air cooling to room temperature.
5. The preparation method of claim 4, wherein in the step 1), the batching and smelting process of the aluminum alloy ingot comprises the following steps:
1) Setting the temperature of the aluminum liquid: setting the molten aluminum in the crucible furnace at 760 ℃, and controlling the temperature of furnace gas at a corresponding temperature;
2) Adding silicon until the aluminum liquid in the crucible reaches 700 ℃, starting to add the crystalline silicon, immediately stirring after adding the crystalline silicon until the alloy is completely wrapped by the aluminum liquid, wherein the melting time of the alloy is 30-40 min, and stirring once every 10-15 min within the melting time;
6) Adding magnesium: when the temperature of the aluminum liquid reaches 680 ℃, pressing a magnesium block into the aluminum liquid by using a preheated bell jar, and prohibiting the bell jar from leaving the liquid level during the melting of the magnesium block;
7) Adding a titanium agent: when the temperature of the aluminum liquid reaches 730 ℃, adding a titanium agent, fully reacting the titanium agent on the surface of the aluminum liquid, fully stirring after 30min, and controlling the temperature of the aluminum liquid at 760 ℃;
8) Melting the alloy: keeping the temperature at 760 ℃ for 30-40 min until all the alloy elements are melted;
9) Primary degassing: the gas flow valve is opened at first, the flow is adjusted to be small at this moment, and the equipment automatically runs and then is adjusted to be proper; degassing parameter setting: the distance between the rotor and the crucible bottom is 100-150 mm; degassing gas is liquid argon, or the degassing parameters of argon on two sides of degassing are set as follows: the time is 40min, and the flow rate is 1.2-1.5 m 3 V/h, setting the rotating speed at 400r/min and the air outlet pressure at 0.03-0.07 Mpa;
10 Add slag-removing agent: after the degasser is started for 1-2 min, uniformly scattering G5550 granular deslagging agent on the surface of the aluminum liquid;
11 ) degassing is finished: after 40min, after the warning light is turned on after degassing, the degassing machine is moved out after the rotor slag is cleaned up, and then the gas valve is closed;
12 Slagging: lightly stirring the surface of the aluminum liquid by using a preheated slag fishing tool, then collecting the aluminum slag together, and fishing out the slag by using the slag fishing tool;
13 Secondary degassing): setting parameters: the time is 20min, the flow is 1.2-1.5m3// h, the rotating speed is set to be 400r/min, and the air outlet pressure is 0.03-0.07 Mpa;
14 Addition of alterants and refiners: immediately putting the preheated aluminum-strontium alloy and TCB seed crystal alloy into the aluminum liquid after degassing starting;
15 Add slag-removing agent: after the degasser is started for 1-2 min, 200G of G5550 granular deslagging agent is uniformly scattered on the surface of the aluminum liquid;
16 Stirring and slag fishing: lightly stirring the surface of the aluminum liquid by using a preheated slag fishing tool, then collecting the aluminum slag together, and fishing out the slag by using the slag fishing tool;
17 Chemical composition analysis of the sample: if the chemical components are unqualified, the method for adjusting the added elements is the same as the above method, and then degassing and stirring are carried out until the chemical components are qualified.
6. The preparation method according to claim 4, characterized in that in the step 1), the temperature is uniformly raised to 535 ℃ within 1-3 h, and then the temperature is kept for 10-14 h for solution treatment.
7. The preparation method according to claim 5, wherein in the step 1), the temperature is uniformly raised to 535 ℃ within 2 hours, and then the temperature is kept for 12 hours for solution treatment.
8. The preparation method according to claim 4, wherein in the step 2), water-cooling quenching is performed by using room-temperature water at 50-60 ℃, and the quenching time is 15min.
9. The preparation method according to claim 4, wherein in the step 3), the quenched aluminum alloy ingot is heated to 120 ℃ at a constant speed within 0.2-0.5 h, and the first aging treatment is carried out at the temperature for 3h; and after the first time effect treatment is finished, air cooling to room temperature.
10. The preparation method according to claim 4, characterized in that in the step 4), the temperature of the aluminum alloy ingot after air cooling is raised to 160 ℃ at a constant speed within 0.4-0.8 h, and the second aging treatment is carried out at the temperature for 4.5h.
CN202211534468.XA 2022-12-02 2022-12-02 High-performance aluminum alloy material and preparation method thereof Active CN115896560B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202211534468.XA CN115896560B (en) 2022-12-02 2022-12-02 High-performance aluminum alloy material and preparation method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202211534468.XA CN115896560B (en) 2022-12-02 2022-12-02 High-performance aluminum alloy material and preparation method thereof

Publications (2)

Publication Number Publication Date
CN115896560A true CN115896560A (en) 2023-04-04
CN115896560B CN115896560B (en) 2023-06-06

Family

ID=86495270

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202211534468.XA Active CN115896560B (en) 2022-12-02 2022-12-02 High-performance aluminum alloy material and preparation method thereof

Country Status (1)

Country Link
CN (1) CN115896560B (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060198754A1 (en) * 2005-03-03 2006-09-07 The Boeing Company Method for preparing high-temperature nanophase aluminum-alloy sheets and aluminum-alloy sheets prepared thereby
WO2010031255A1 (en) * 2008-09-17 2010-03-25 北京有色金属研究总院 An al alloy material suitable for manufacturing main supporting structural components with large section
CN108193096A (en) * 2017-12-11 2018-06-22 南昌大学 A kind of hypoeutectic silumin alloy of high-strength and high ductility and preparation method thereof
CN111032897A (en) * 2017-08-14 2020-04-17 伦敦布鲁内尔大学 Method of forming cast aluminum alloy
CN111020316A (en) * 2019-12-20 2020-04-17 福建祥鑫股份有限公司 High-performance 7XXX aluminum alloy capable of being quenched on line and preparation method thereof

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060198754A1 (en) * 2005-03-03 2006-09-07 The Boeing Company Method for preparing high-temperature nanophase aluminum-alloy sheets and aluminum-alloy sheets prepared thereby
WO2010031255A1 (en) * 2008-09-17 2010-03-25 北京有色金属研究总院 An al alloy material suitable for manufacturing main supporting structural components with large section
CN111032897A (en) * 2017-08-14 2020-04-17 伦敦布鲁内尔大学 Method of forming cast aluminum alloy
CN108193096A (en) * 2017-12-11 2018-06-22 南昌大学 A kind of hypoeutectic silumin alloy of high-strength and high ductility and preparation method thereof
CN111020316A (en) * 2019-12-20 2020-04-17 福建祥鑫股份有限公司 High-performance 7XXX aluminum alloy capable of being quenched on line and preparation method thereof

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
吴护林: "轻质材料环境适应性数据手册:铝合金、钛合金及防护工艺", 国防工业出版社, pages: 179 *
王刚;孙一苇;祝伟忠;徐群峰;: "轻量化汽车承载用铝合金挤压型材的研制", 轻合金加工技术, no. 02, pages 179 *

Also Published As

Publication number Publication date
CN115896560B (en) 2023-06-06

Similar Documents

Publication Publication Date Title
CN108866404B (en) Preparation method of large-size high-strength high-toughness 7000 series aluminum alloy round ingot
CN105886855B (en) A kind of aluminium alloy thick plate and its production method
CN106811635A (en) A kind of 6 line aluminium alloy materials and preparation method thereof
CN112430767B (en) Large-size hollow ingot casting and ingot casting method
CN111440974B (en) High-strength aluminum alloy and manufacturing method thereof
CN109468503A (en) A kind of aluminum alloy materials and its production technology
CN107779704A (en) A kind of 2 line aluminium alloys and its melting and casting method
CN108950325B (en) High-strength aluminum alloy material and production process thereof
CN107815575A (en) A kind of magnesium alloy ingot casting
CN114351017A (en) Casting method and application of high-toughness high-heat-conductivity aluminum alloy ingot
CN1087787C (en) Fireproof cast magnesium alloy and its smelting and casting process
JPS591650A (en) Metal alloy manufacture
CN106544561A (en) A kind of casting method of aluminum alloy plate materials
CN108118215A (en) A kind of 6 line aluminium alloys and preparation method thereof
CN115896560A (en) High-performance aluminum alloy material and preparation method thereof
CN116219233B (en) High-heat-conductivity cast aluminum alloy and preparation method thereof
CN112159917A (en) Large-size high-purity homogeneous fine-grain aluminum alloy ingot and casting method
CN111304498A (en) Method for producing 8021 aluminum alloy for lithium battery by casting method
CN108796318B (en) High-strength and high-toughness near-eutectic aluminum-silicon-copper-magnesium alloy and preparation method thereof
CN111139386A (en) Preparation method of high-strength soluble magnesium alloy material
CN110438378A (en) A kind of 2 line aluminium alloy melting and casting methods
CN1102667C (en) Pressure-cast fireproof magnesium alloy and its smelting and pressure casting process
CN114231804A (en) 7050 alloy ingot casting material and preparation method thereof
CN106591640A (en) Abrasion-resisting aluminum alloy
CN107805736B (en) Preparation method of dezincification-resistant lead-free bismuth-arsenic extruded brass bar

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant