CN110885941A - High-toughness aluminum alloy material and preparation method thereof - Google Patents
High-toughness aluminum alloy material and preparation method thereof Download PDFInfo
- Publication number
- CN110885941A CN110885941A CN201911396674.7A CN201911396674A CN110885941A CN 110885941 A CN110885941 A CN 110885941A CN 201911396674 A CN201911396674 A CN 201911396674A CN 110885941 A CN110885941 A CN 110885941A
- Authority
- CN
- China
- Prior art keywords
- percent
- aluminum alloy
- alloy material
- temperature
- furnace
- 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
Links
Images
Classifications
-
- 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
- C22C21/02—Alloys based on aluminium with silicon as the next major constituent
-
- 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
- C22C1/06—Making non-ferrous alloys with the use of special agents for refining or deoxidising
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Continuous Casting (AREA)
- Treatment Of Steel In Its Molten State (AREA)
Abstract
The invention discloses a high-toughness aluminum alloy material, which comprises the following components in percentage by mass: si: 10-13%, Fe: 0.8-1%, Cr: 0.15-0.35%, Mn: 0.45-0.65%, Mg: 0.1-0.3%, Cu: 2.5-3.2%, Zn: 0.15-0.35%, Zr: 1.5-3%, Hf: 0.25-0.35%, Nb: 0.1-0.2%, Ta: 0.1-0.2%, Sr: 0.01-0.03%, the total amount of impurity elements is less than or equal to 0.15%, and the balance is Al. The high-toughness aluminum alloy material disclosed by the invention has higher elongation and improves the toughness of the aluminum alloy material while not reducing the tensile strength of the aluminum alloy material.
Description
Technical Field
The invention relates to the technical field of aluminum alloy preparation, in particular to a high-toughness aluminum alloy material and a preparation method thereof.
Background
Aluminum alloy is a non-ferrous metal structural material which is most widely applied in industry, and is widely applied in the industries of aerospace, automobiles, mechanical manufacturing, ships and the like. Aluminum alloys have a low density but a relatively high strength, which is close to or exceeds that of high-quality steels, can be processed into various shapes, have excellent electrical conductivity, thermal conductivity and corrosion resistance, and are widely used industrially.
However, the existing aluminum alloy has single function, although the existing aluminum alloy has high hardness, the existing aluminum alloy has poor plasticity and poor elongation, and the hardness and the strength cannot have larger breakthrough, so that the application of the aluminum alloy is limited to a certain extent. Therefore, there is a need for an aluminum alloy material that satisfies the high strength requirements and has high toughness.
The Chinese patent document CN110564993A discloses a high-performance automobile die casting aluminum alloy material, which comprises the following components in percentage by mass: si: 8-9%, Fe: 0.5-0.8%, Cu: 3.2% -3.8%, Mn: 0.15-0.40%, less than or equal to 0.3% of Mg, less than or equal to 1.5% of Zn, Sr: 0.008-0.02%. The aluminum alloy material has the tensile strength of more than 330MPa, the elongation of more than 3.5 percent, the hardness of more than 95HBW and higher strength, but the toughness of the aluminum alloy material is still to be further improved.
Disclosure of Invention
The invention aims to provide a high-toughness aluminum alloy material and a preparation method thereof aiming at the defects of the prior art, so that the high-toughness aluminum alloy material has higher elongation and improves the toughness of the aluminum alloy material while the tensile strength is not reduced.
In order to achieve the purpose, the technical scheme adopted by the invention is as follows:
a high-toughness aluminum alloy material comprises the following components in percentage by mass: si: 10-13%, Fe: 0.8-1%, Cr: 0.15-0.35%, Mn: 0.45-0.65%, Mg: 0.1-0.3%, Cu: 2.5-3.2%, Zn: 0.15-0.35%, Zr: 1.5-3%, Hf: 0.25-0.35%, Nb: 0.1-0.2%, Ta: 0.1-0.2%, Sr: 0.01-0.03%, the total amount of impurity elements is less than or equal to 0.15%, and the balance is Al.
Further, the aluminum alloy material comprises the following components in percentage by mass: the aluminum alloy material comprises the following components in percentage by mass: si: 11%, Fe: 0.9%, Cr: 0.15%, Mn: 0.6%, Mg: 0.1%, Cu: 2.9%, Zn: 0.25%, Zr: 1.5%, Hf: 0.25%, Nb: 0.1%, Ta: 0.1%, Sr: 0.03 percent, less than or equal to 0.15 percent of impurity elements and the balance of Al.
Further, the aluminum alloy material comprises the following components in percentage by mass: 11%, Fe: 0.9%, Cr: 0.15%, Mn: 0.6%, Mg: 0.1%, Cu: 2.9%, Zn: 0.25%, Zr: 2.5%, Hf: 0.28%, Nb: 0.15%, Ta: 0.15%, Sr: 0.03 percent, less than or equal to 0.15 percent of impurity elements and the balance of Al.
Further, the aluminum alloy material comprises the following components in percentage by mass: si: 11%, Fe: 0.9%, Cr: 0.15%, Mn: 0.6%, Mg: 0.1%, Cu: 2.9%, Zn: 0.25%, Zr: 3%, Hf: 0.35%, Nb: 0.2%, Ta: 0.2%, Sr: 0.03 percent, less than or equal to 0.15 percent of impurity elements and the balance of Al.
A preparation method of a high-toughness aluminum alloy material comprises the following steps:
1) adding raw material aluminum into a melting furnace, heating to the temperature of 700-800 ℃, stirring to completely melt the added aluminum, and keeping the aluminum in a molten state or a liquid state in the furnace;
2) to the molten aluminium prepared, 10-13% Si, Fe: 0.8-1%, Cr: 0.15 to 0.35 percent of Mn, 0.45 to 0.65 percent of Mn and 0.1 to 0.3 percent of Mg, preserving the heat for 1 to 2 hours at the temperature of 800 plus 880 ℃, and fully stirring to prepare an alloying system;
3) blowing 1-2% of refining agent of the total weight of the raw materials into a furnace by using nitrogen, refining for 30-60min, and carrying out refining degassing and deslagging treatment in the furnace;
4) adding the first material into the alloy system, reducing the temperature to 700-800 ℃, and keeping the temperature for 45-75 min;
5) adding a second material into the alloy system, keeping the temperature at 750-850 ℃, and preserving the heat for 60-80min to form a functional compound;
6) regulating the temperature to 650-700 ℃, blowing a refining agent accounting for 1-2% of the total weight of the raw materials into the furnace by using nitrogen, refining for 30-60min, and refining, degassing and deslagging in the furnace again;
7) and pouring the refined alloy system into a mold, and cooling and forming.
Further, the purity of the raw material aluminum is more than 99%.
Further, the first material comprises 2.5-3.2% of Cu and 0.15-0.35% of Zn.
Further, the second material comprises 1.5-3% of Zr, 0.25-0.35% of Hf, 0.1-0.2% of Nb, 0.1-0.2% of Ta and 0.01-0.03% of Sr.
Further, the chemical formula of the functional compound is represented by AlxSry[Zr1-x(HfaNbbTa)1-a-b]1-x-yWherein x is more than 0 and less than or equal to 1, y is more than 0.1 and less than or equal to 0.5, a is more than 0 and less than or equal to 0.08, and b is more than 0 and less than or equal to 0.03.
According to the invention, by adding Si with a reasonable percentage, the fluidity of the aluminum alloy is improved, and the mechanical property of the aluminum alloy is ensured.
Too high Fe content increases the brittleness of the alloy, and too low Fe content makes the alloy not easy to demould.
Cr plays roles of precipitation strengthening and dispersion strengthening, can reduce the harmful effect of Fe, and improves the stress corrosion crack resistance of the alloy.
Mg can greatly improve the mechanical property of the alloy. Mg and Si can generate a strengthening phase Mg2Si, which can effectively improve the performance of the alloy, but the excessively high Mg content can reduce the elongation of the alloy.
Cu can improve the strength of the alloy and improve the high-temperature performance of the alloy, but the corrosion resistance and the casting performance of the alloy are reduced due to the excessively high Cu content.
Zn can improve the solubility and the dissolution speed of Cu in the aluminum alloy so as to improve the plasticity of the alloy, and can also form a strengthening phase Mg/Zn with Mg2And the tensile strength and the yield strength of the alloy are enhanced.
Zr plays a role in refining grains, the chemical properties of Hf and Zr are close, the corrosion resistance of Zr is close to those of Nb and Ta, and Sr can improve the plastic processability of the alloy. The aluminum alloy material of the invention forms a functional compound Al in the preparationxSry[Zr1-x(HfaNbbTa)1-a-b]1-x-yAnd the toughness of the alloy material is improved.
Compared with the prior art, the invention has the following advantages:
1. according to the invention, the alloy material with sufficient strength is obtained by optimizing the component proportion of each component, so that the high-strength requirement on the aluminum alloy material is met.
2. The invention uses Zr, Hf, Nb, Ta, Sr and Al to form a special functional compound AlxSry[Zr1-x(HfaNbbTa)1-a-b]1-x-yThe toughness of the alloy material is greatly improved, the elongation of the aluminum alloy material is larger than 12%, the optimal proportion value is obtained by optimizing the proportion of each component of Zr, Hf, Nb, Ta and Sr, and the elongation of the aluminum alloy material can reach 16.37% under the optimal proportion value.
3 in the preparation process, the invention is beneficial to obtaining the optimal conditions of each component through step-by-step addition and multiple times of refining, and plays the optimal role in an aluminum alloy system.
Drawings
Fig. 1 is a comparative line graph of tensile strengths of aluminum alloy materials of examples and comparative examples.
Fig. 2 is a comparative line graph of the yield strengths of the aluminum alloy materials of the examples and comparative examples.
FIG. 3 is a comparative line graph of elongation for the aluminum alloy materials of the example and the comparative example.
Detailed Description
The present invention will be further described with reference to the following examples.
The purity of the raw material aluminum used in the present example is greater than 99%.
Example 1
A high-toughness aluminum alloy material comprises the following components in percentage by mass: si: 11%, Fe: 0.9%, Cr: 0.15%, Mn: 0.6%, Mg: 0.1%, Cu: 2.9%, Zn: 0.25%, Zr: 1.5%, Hf: 0.25%, Nb: 0.1%, Ta: 0.1%, Sr: 0.03 percent, less than or equal to 0.15 percent of impurity elements and the balance of Al.
The preparation method of the high-toughness aluminum alloy material comprises the following steps:
1) adding raw material aluminum into a melting furnace, heating to 750 ℃, stirring to completely melt the added aluminum, and keeping the aluminum in a molten state or a liquid state in the furnace;
2) to the molten aluminium prepared, 11% Si, Fe: 0.9%, Cr: 0.15 percent of Mn, 0.6 percent of Mn and 0.1 percent of Mg, preserving the heat for 1 hour at the temperature of 850 ℃, and fully stirring to prepare an alloying system;
3) blowing a refining agent accounting for 2 percent of the total weight of the raw materials into the furnace by using nitrogen, refining for 40min, and carrying out refining, degassing and deslagging treatment in the furnace;
4) adding a first material which comprises 2.9 percent of Cu and 0.25 percent of Zn into an alloy system, reducing the temperature to 750 ℃, and preserving the temperature for 60 min;
5) adding a second material comprising 1.5 percent of Zr, 0.25 percent of Hf, 0.1 percent of Nb, 0.1 percent of Ta and 0.03 percent of Sr into an alloy system, keeping the temperature at 800 ℃, and preserving the temperature for 70min to form a functional compound with a chemical formula of Al0.3Sr0.4[Zr0.7(Hf0.05Nb0.03Ta)0.92]0.3；
6) Adjusting the temperature to 650 ℃, blowing a refining agent accounting for 2 percent of the total weight of the raw materials into the furnace by using nitrogen, refining for 45min, and refining, degassing and deslagging in the furnace again;
7) and pouring the refined alloy system into a mold, and cooling and forming.
Example 2
A high-toughness aluminum alloy material comprises the following components in percentage by mass: si: 11%, Fe: 0.9%, Cr: 0.15%, Mn: 0.6%, Mg: 0.1%, Cu: 2.9%, Zn: 0.25%, Zr: 3%, Hf: 0.35%, Nb: 0.2%, Ta: 0.2%, Sr: 0.03 percent, less than or equal to 0.15 percent of impurity elements and the balance of Al.
The preparation method of the high-toughness aluminum alloy material comprises the following steps:
1) adding raw material aluminum into a melting furnace, heating to 750 ℃, stirring to completely melt the added aluminum, and keeping the aluminum in a molten state or a liquid state in the furnace;
2) to the molten aluminium prepared, 11% Si, Fe: 0.9%, Cr: 0.15 percent of Mn, 0.6 percent of Mn and 0.1 percent of Mg, preserving the heat for 1 hour at the temperature of 850 ℃, and fully stirring to prepare an alloying system;
3) blowing a refining agent accounting for 2 percent of the total weight of the raw materials into the furnace by using nitrogen, refining for 40min, and carrying out refining, degassing and deslagging treatment in the furnace;
4) adding a first material which comprises 2.9 percent of Cu and 0.25 percent of Zn into an alloy system, reducing the temperature to 750 ℃, and preserving the temperature for 60 min;
5) adding a second material comprising 3% of Zr, 0.35% of Hf, 0.2% of Nb, 0.2% of Ta and 0.03% of Sr into an alloy system, keeping the temperature at 800 ℃, and keeping the temperature for 70min to form a functional compound with a chemical formula of Al0.2Sr0.4[Zr0.8(Hf0.08Nb0.01Ta)0.91]0.4；
6) Adjusting the temperature to 650 ℃, blowing a refining agent accounting for 2 percent of the total weight of the raw materials into the furnace by using nitrogen, refining for 45min, and refining, degassing and deslagging in the furnace again;
7) and pouring the refined alloy system into a mold, and cooling and forming.
Example 3
A high-toughness aluminum alloy material comprises the following components in percentage by mass: : si: 11%, Fe: 0.9%, Cr: 0.15%, Mn: 0.6%, Mg: 0.1%, Cu: 2.9%, Zn: 0.25%, Zr: 2.25%, Hf: 0.28%, Nb: 0.15%, Ta: 0.15%, Sr: 0.02 percent, less than or equal to 0.15 percent of impurity elements and the balance of Al.
The preparation method of the high-toughness aluminum alloy material comprises the following steps:
1) adding raw material aluminum into a melting furnace, heating to 750 ℃, stirring to completely melt the added aluminum, and keeping the aluminum in a molten state or a liquid state in the furnace;
2) to the molten aluminum prepared, 12% Si, 11% Si, Fe: 0.9%, Cr: 0.15 percent of Mn, 0.6 percent of Mn and 0.1 percent of Mg, preserving the heat for 1 hour at the temperature of 850 ℃, and fully stirring to prepare an alloying system;
3) blowing a refining agent accounting for 2 percent of the total weight of the raw materials into the furnace by using nitrogen, refining for 40min, and carrying out refining, degassing and deslagging treatment in the furnace;
4) adding a first material which comprises 2.9 percent of Cu and 0.25 percent of Zn into an alloy system, reducing the temperature to 750 ℃, and preserving the temperature for 60 min;
5) adding a second material comprising 2.25% of Zr, 0.28% of Hf, 0.15% of Nb, 0.15% of Ta and 0.02% of Sr into an alloy system, keeping the temperature at 800 ℃, and keeping the temperature for 70min to form a functional compound with a chemical formula of Al0.5Sr0.3[Zr0.5(Hf0.02Nb0.01Ta)0.97]0.2；
6) Adjusting the temperature to 650 ℃, blowing a refining agent accounting for 2 percent of the total weight of the raw materials into the furnace by using nitrogen, refining for 45min, and refining, degassing and deslagging in the furnace again;
7) and pouring the refined alloy system into a mold, and cooling and forming.
Example 4
A high-toughness aluminum alloy material comprises the following components in percentage by mass: si: 11%, Fe: 0.9%, Cr: 0.15%, Mn: 0.6%, Mg: 0.1%, Cu: 2.9%, Zn: 0.25%, Zr: 2.5%, Hf: 0.28%, Nb: 0.15%, Ta: 0.15%, Sr: 0.03 percent, less than or equal to 0.15 percent of impurity elements and the balance of Al.
The preparation method of the high-toughness aluminum alloy material comprises the following steps:
1) adding raw material aluminum into a melting furnace, heating to 750 ℃, stirring to completely melt the added aluminum, and keeping the aluminum in a molten state or a liquid state in the furnace;
2) to the molten aluminium prepared, 11% Si, Fe: 0.9%, Cr: 0.15 percent of Mn, 0.6 percent of Mn and 0.1 percent of Mg, preserving the heat for 1 hour at the temperature of 850 ℃, and fully stirring to prepare an alloying system;
3) blowing a refining agent accounting for 2 percent of the total weight of the raw materials into the furnace by using nitrogen, refining for 40min, and carrying out refining, degassing and deslagging treatment in the furnace;
4) adding a first material which comprises 2.9 percent of Cu and 0.25 percent of Zn into an alloy system, reducing the temperature to 750 ℃, and preserving the temperature for 60 min;
5) adding a second material comprising 2.5 percent of Zr, 0.28 percent of Hf, 0.15 percent of Nb, 0.15 percent of Ta and 0.03 percent of Sr into an alloy system, keeping the temperature at 800 ℃, and preserving the temperature for 70min to form a functional compound with a chemical formula of Al0.6Sr0.3[Zr0.4(Hf0.07Nb0.02Ta)0.91]0.1；
6) Adjusting the temperature to 650 ℃, blowing a refining agent accounting for 2 percent of the total weight of the raw materials into the furnace by using nitrogen, refining for 45min, and refining, degassing and deslagging in the furnace again;
7) and pouring the refined alloy system into a mold, and cooling and forming.
Example 5
A high-toughness aluminum alloy material comprises the following components in percentage by mass: si: 11%, Fe: 0.9%, Cr: 0.15%, Mn: 0.6%, Mg: 0.1%, Cu: 2.9%, Zn: 0.25%, Zr: 2.0%, Hf: 0.25%, Nb: 0.1%, Ta: 0.1%, Sr: 0.03 percent, less than or equal to 0.15 percent of impurity elements and the balance of Al.
The preparation method of the high-toughness aluminum alloy material comprises the following steps:
1) adding raw material aluminum into a melting furnace, heating to 750 ℃, stirring to completely melt the added aluminum, and keeping the aluminum in a molten state or a liquid state in the furnace;
2) to the molten aluminium prepared, 11% Si, Fe: 0.9%, Cr: 0.15 percent of Mn, 0.6 percent of Mn and 0.1 percent of Mg, preserving the heat for 1 hour at the temperature of 850 ℃, and fully stirring to prepare an alloying system;
3) blowing a refining agent accounting for 2 percent of the total weight of the raw materials into the furnace by using nitrogen, refining for 40min, and carrying out refining, degassing and deslagging treatment in the furnace;
4) adding a first material which comprises 2.9 percent of Cu and 0.25 percent of Zn into an alloy system, reducing the temperature to 750 ℃, and preserving the temperature for 60 min;
5) adding a second material comprising 2.0 percent of Zr, 0.25 percent of Hf, 0.1 percent of Nb, 0.1 percent of Ta and 0.03 percent of Sr into an alloy system, keeping the temperature at 800 ℃, and preserving the temperature for 70min to form a functional compound with a chemical formula of Al0.8Sr0.1[Zr0.2(Hf0.04Nb0.01Ta)0.95]0.1；
6) Adjusting the temperature to 650 ℃, blowing a refining agent accounting for 2 percent of the total weight of the raw materials into the furnace by using nitrogen, refining for 45min, and refining, degassing and deslagging in the furnace again;
7) and pouring the refined alloy system into a mold, and cooling and forming.
Comparative example 1
The aluminum alloy material of the comparative example comprises the following components in percentage by mass: si: 11%, Fe: 0.9%, Cr: 0.15%, Mn: 0.6%, Mg: 0.1%, Cu: 2.9%, Zn: 0.25 percent, less than or equal to 0.15 percent of impurity elements and the balance of Al.
The preparation method of the high-toughness aluminum alloy material comprises the following steps:
1) adding raw material aluminum into a melting furnace, heating to 750 ℃, stirring to completely melt the added aluminum, and keeping the aluminum in a molten state or a liquid state in the furnace;
2) to the molten aluminium prepared, 12% Si, Fe: 0.9%, Cr: 0.15 percent of Mn, 0.6 percent of Mn and 0.1 percent of Mg, preserving the heat for 1 hour at the temperature of 850 ℃, and fully stirring to prepare an alloying system;
3) blowing a refining agent accounting for 2 percent of the total weight of the raw materials into the furnace by using nitrogen, refining for 40min, and carrying out refining, degassing and deslagging treatment in the furnace;
4) adding a first material which comprises 2.9 percent of Cu and 0.25 percent of Zn into an alloy system, reducing the temperature to 750 ℃, and preserving the temperature for 60 min;
5) adjusting the temperature to 650 ℃, blowing a refining agent accounting for 2 percent of the total weight of the raw materials into the furnace by using nitrogen, refining for 45min, and refining, degassing and deslagging in the furnace again;
6) and pouring the refined alloy system into a mold, and cooling and forming.
Various performance tests were performed on the aluminum alloy materials of the different examples and comparative examples, and the test results are shown in table 1.
TABLE 1
Although the present invention has been described with reference to the preferred embodiments, it is not intended to be limited thereto. Those skilled in the art can make various changes and modifications without departing from the spirit and scope of the invention. Therefore, the protection scope of the present invention should be determined by the appended claims.
Claims (9)
1. A high-toughness aluminum alloy material is characterized in that: the aluminum alloy material comprises the following components in percentage by mass: si: 10-13%, Fe: 0.8-1%, Cr: 0.15-0.35%, Mn: 0.45-0.65%, Mg: 0.1-0.3%, Cu: 2.5-3.2%, Zn: 0.15-0.35%, Zr: 1.5-3%, Hf: 0.25-0.35%, Nb: 0.1-0.2%, Ta: 0.1-0.2%, Sr: 0.01-0.03%, the total amount of impurity elements is less than or equal to 0.15%, and the balance is Al.
2. The high-toughness aluminum alloy material according to claim 1, characterized in that: the aluminum alloy material comprises the following components in percentage by mass: si: 11%, Fe: 0.9%, Cr: 0.15%, Mn: 0.6%, Mg: 0.1%, Cu: 2.9%, Zn: 0.25%, Zr: 1.5%, Hf: 0.25%, Nb: 0.1%, Ta: 0.1%, Sr: 0.03 percent, less than or equal to 0.15 percent of impurity elements and the balance of Al.
3. The high-toughness aluminum alloy material according to claim 1, characterized in that: the aluminum alloy material comprises the following components in percentage by mass: si: 11%, Fe: 0.9%, Cr: 0.15%, Mn: 0.6%, Mg: 0.1%, Cu: 2.9%, Zn: 0.25%, Zr: 2.5%, Hf: 0.28%, Nb: 0.15%, Ta: 0.15%, Sr: 0.03 percent, less than or equal to 0.15 percent of impurity elements and the balance of Al.
4. The high-toughness aluminum alloy material according to claim 1, characterized in that: the aluminum alloy material comprises the following components in percentage by mass: si: 11%, Fe: 0.9%, Cr: 0.15%, Mn: 0.6%, Mg: 0.1%, Cu: 2.9%, Zn: 0.25%, Zr: 3%, Hf: 0.35%, Nb: 0.2%, Ta: 0.2%, Sr: 0.03 percent, less than or equal to 0.15 percent of impurity elements and the balance of Al.
5. A method for producing a high-toughness aluminum alloy material according to any one of claims 1 to 4, wherein: the preparation method comprises the following steps:
1) adding raw material aluminum into a melting furnace, heating to the temperature of 700-800 ℃, stirring to completely melt the added aluminum, and keeping the aluminum in a molten state or a liquid state in the furnace;
2) to the molten aluminium prepared, 10-13% Si, Fe: 0.8-1%, Cr: 0.15 to 0.35 percent of Mn, 0.45 to 0.65 percent of Mn and 0.1 to 0.3 percent of Mg, preserving the heat for 1 to 2 hours at the temperature of 800 plus 880 ℃, and fully stirring to prepare an alloying system;
3) blowing 1-2% of refining agent of the total weight of the raw materials into a furnace by using nitrogen, refining for 30-60min, and carrying out refining degassing and deslagging treatment in the furnace;
4) adding the first material into the alloy system, reducing the temperature to 700-800 ℃, and keeping the temperature for 45-75 min;
5) adding a second material into the alloy system, keeping the temperature at 750-850 ℃, and preserving the heat for 60-80min to form a functional compound;
6) regulating the temperature to 650-700 ℃, blowing a refining agent accounting for 1-2% of the total weight of the raw materials into the furnace by using nitrogen, refining for 30-60min, and refining, degassing and deslagging in the furnace again;
7) and pouring the refined alloy system into a mold, and cooling and forming.
6. The method for producing a high-toughness aluminum alloy material according to claim 5, characterized in that: the purity of the raw material aluminum is more than 99%.
7. The method for producing a high-toughness aluminum alloy material according to claim 5, characterized in that: the first material comprises 2.5-3.2% of Cu and 0.15-0.35% of Zn.
8. The method for producing a high-toughness aluminum alloy material according to claim 5, characterized in that: the second material comprises 1.5-3% of Zr, 0.25-0.35% of Hf, 0.1-0.2% of Nb, 0.1-0.2% of Ta and 0.01-0.03% of Sr.
9. The method for producing a high-toughness aluminum alloy material according to claim 8, characterized in that: the chemical formula of the functional compound is AlxSry[Zr1-x(HfaNbbTa)1-a-b]1-x-yWherein x is more than 0 and less than or equal to 1, y is more than 0.1 and less than or equal to 0.5, a is more than 0 and less than or equal to 0.08, and b is more than 0 and less than or equal to 0.03.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911396674.7A CN110885941B (en) | 2019-12-30 | 2019-12-30 | High-toughness aluminum alloy material and preparation method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911396674.7A CN110885941B (en) | 2019-12-30 | 2019-12-30 | High-toughness aluminum alloy material and preparation method thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN110885941A true CN110885941A (en) | 2020-03-17 |
| CN110885941B CN110885941B (en) | 2021-05-18 |
Family
ID=69753429
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201911396674.7A Active CN110885941B (en) | 2019-12-30 | 2019-12-30 | High-toughness aluminum alloy material and preparation method thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110885941B (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113151703A (en) * | 2021-05-17 | 2021-07-23 | 王小飞 | Preparation method of high-strength anti-cracking aluminum alloy |
| CN117089748A (en) * | 2023-09-06 | 2023-11-21 | 威海科米沃新材料有限公司 | Preparation method of high-elongation aluminum alloy material |
| CN117721358A (en) * | 2023-12-15 | 2024-03-19 | 山东昊瑞得智能科技有限公司 | SiCp particles for aluminum-based composite material, composite material and preparation method |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005163100A (en) * | 2003-12-02 | 2005-06-23 | Sumitomo Denko Shoketsu Gokin Kk | Heat resistant/high toughness aluminum alloy, its production method, and engine component |
| CN102864349A (en) * | 2011-07-05 | 2013-01-09 | 浙江艾默樱零部件有限公司 | High-temperature resistant aluminium alloy and preparation method thereof |
| CN108913961A (en) * | 2018-08-13 | 2018-11-30 | 文登皇利压铸化工材料有限公司 | The piston aluminium ingot used for turbocharging automobile |
| CN110195176A (en) * | 2019-06-25 | 2019-09-03 | 山东裕隆金和精密机械有限公司 | A kind of high tough pack alloy and preparation method thereof |
| CN110564993A (en) * | 2019-10-16 | 2019-12-13 | 南通众福新材料科技有限公司 | High-performance automobile die casting aluminum alloy material and preparation method thereof |
-
2019
- 2019-12-30 CN CN201911396674.7A patent/CN110885941B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005163100A (en) * | 2003-12-02 | 2005-06-23 | Sumitomo Denko Shoketsu Gokin Kk | Heat resistant/high toughness aluminum alloy, its production method, and engine component |
| CN102864349A (en) * | 2011-07-05 | 2013-01-09 | 浙江艾默樱零部件有限公司 | High-temperature resistant aluminium alloy and preparation method thereof |
| CN108913961A (en) * | 2018-08-13 | 2018-11-30 | 文登皇利压铸化工材料有限公司 | The piston aluminium ingot used for turbocharging automobile |
| CN110195176A (en) * | 2019-06-25 | 2019-09-03 | 山东裕隆金和精密机械有限公司 | A kind of high tough pack alloy and preparation method thereof |
| CN110564993A (en) * | 2019-10-16 | 2019-12-13 | 南通众福新材料科技有限公司 | High-performance automobile die casting aluminum alloy material and preparation method thereof |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113151703A (en) * | 2021-05-17 | 2021-07-23 | 王小飞 | Preparation method of high-strength anti-cracking aluminum alloy |
| CN117089748A (en) * | 2023-09-06 | 2023-11-21 | 威海科米沃新材料有限公司 | Preparation method of high-elongation aluminum alloy material |
| CN117089748B (en) * | 2023-09-06 | 2024-04-26 | 威海科米沃新材料有限公司 | Preparation method of high-elongation aluminum alloy material |
| CN117721358A (en) * | 2023-12-15 | 2024-03-19 | 山东昊瑞得智能科技有限公司 | SiCp particles for aluminum-based composite material, composite material and preparation method |
Also Published As
| Publication number | Publication date |
|---|---|
| CN110885941B (en) | 2021-05-18 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN110885941B (en) | High-toughness aluminum alloy material and preparation method thereof | |
| CN110885940B (en) | Rare earth aluminum alloy material and preparation method thereof | |
| CN108396204B (en) | Hypoeutectic aluminum-silicon alloy casting and process method for improving performance thereof | |
| CN103667825A (en) | Ultra-strong strength, high-toughness and anticorrosive aluminum alloy and preparation method for same | |
| CN111411274B (en) | High-strength heat-conducting aluminum alloy material and preparation method thereof | |
| CN114086040B (en) | Aluminum-magnesium-silicon-scandium-zirconium alloy and preparation method thereof | |
| CN109022983B (en) | Sc-containing high-strength high-toughness magnesium alloy and preparation method thereof | |
| CN101906554A (en) | Mg-containing high-strength deforming zinc-copper alloy and preparation method thereof | |
| CN109161730B (en) | Aluminum alloy conductor material for bus duct and preparation method thereof | |
| CN109487135A (en) | A kind of low-cost high-strength high-toughness magnesium alloy and preparation method thereof | |
| CN115094278A (en) | 6-series aluminum alloy material with good thermal stability and preparation method thereof | |
| CN114250387A (en) | Aluminum alloy and preparation method thereof | |
| CN110423928B (en) | High-strength flame-retardant magnesium alloy | |
| WO2020052129A1 (en) | Rare-earth aluminum alloy material having high ductility and high strength and preparation method therefor | |
| CN110616356A (en) | Er-containing magnesium alloy and preparation method thereof | |
| CN116179910A (en) | High-strength Al-Zn-Mg alloy with excellent comprehensive performance and preparation method thereof | |
| CN111455233B (en) | High-thermal-conductivity aluminum alloy material and preparation method thereof | |
| CN113862529B (en) | Aluminum alloy and preparation method thereof | |
| CN114703409A (en) | High-strength corrosion-resistant aluminum alloy and casting method thereof | |
| CN116411208A (en) | Die-casting aluminum alloy and preparation method thereof | |
| CN110016595B (en) | Aluminum alloy foil and preparation method thereof | |
| CN113278827A (en) | Medium-strength easily-extruded 5-series aluminum alloy ingot | |
| CN111996419A (en) | Iron-containing hypoeutectic aluminum-silicon alloy and preparation method thereof | |
| CN111705248A (en) | Al-4.5Cu aluminum-copper alloy material and preparation method thereof | |
| CN115896574B (en) | Die-casting magnesium alloy and preparation method thereof |
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 |