CN107739907A - Aluminium nickel copper-manganese lanthanum alloy intermediate and its application for preparing aluminium alloy - Google Patents
Aluminium nickel copper-manganese lanthanum alloy intermediate and its application for preparing aluminium alloy Download PDFInfo
- Publication number
- CN107739907A CN107739907A CN201711213347.4A CN201711213347A CN107739907A CN 107739907 A CN107739907 A CN 107739907A CN 201711213347 A CN201711213347 A CN 201711213347A CN 107739907 A CN107739907 A CN 107739907A
- Authority
- CN
- China
- Prior art keywords
- parts
- aluminium
- alloy
- manganese
- copper
- 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.)
- Pending
Links
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
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
- C22C1/026—Alloys based on aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
- C22C1/03—Making non-ferrous alloys by melting using master alloys
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/06—Making non-ferrous alloys with the use of special agents for refining or deoxidising
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
Abstract
The invention discloses a kind of aluminium nickel copper-manganese lanthanum alloy intermediate and its application of aluminium alloy is prepared, belongs to technical field of aluminium alloy preparation.Described aluminium nickel copper-manganese lanthanum alloy intermediate, in units of parts by weight, including following raw material：60 80 parts of aluminium, 25 parts of nickel, 48 parts of manganese, 25 parts of copper, 1 1.6 parts of lanthanum.Aluminium alloy is prepared using the aluminium nickel copper-manganese lanthanum alloy intermediate of the present invention, tensile strength, the elongation percentage of aluminum alloy materials can be improved.
Description
Technical field
The invention belongs to technical field of aluminium alloy preparation, and in particular to a kind of aluminium-nickel-manganese-copper-lanthanum alloy intermediate and its
Prepare the application of aluminium alloy.
Background technology
High strength alumin ium alloy has intensity high, and plasticity is good, and solderability is good, the features such as fine corrosion resistance, is widely used
It is many at present dual-use winged in the structural member and the high high stress corrosion resistance structure part of other intensity requirements of various aircrafts
Machine, indispensable important feature material in transport facility.As space flight and aviation technology develops to material requirements increasingly
Improve, researcher is just putting forth effort that mining inetesity is higher, the high intensity and high ductility aluminium alloy of high comprehensive performance.At present, it is raising riveting
The combination property of the high strength alumin ium alloy connect, mainly while material high intensity is pursued, reduce and resisted because intensity improves
Stress corrosion performance, fracture toughness and fatigue strength etc. have undesirable effect.Meanwhile requirement day of the every profession and trade to high strength alumin ium alloy
Benefit improves, and proposes a systems such as top load, lighting, high-strength, high-ductility, high-modulus, good corrosion resisting property and welding performance
Row require, and existing high strength alumin ium alloy accessory size caused by fracture toughness difference or low intensity is thicker, can not meet top load,
Lighting, low cost require that there is an urgent need to Novel light high-strength aluminium alloy to be updated the replacement.
In the world high strength alumin ium alloy development substantially along high intensity, low toughness → high intensity, high tenacity → high intensity,
High tenacity, corrosion-resistant direction are developed.The former Soviet Union and the U.S. successively find to add in toward high strength alumin ium alloy Sc elements can reduce due to
Addition Cu elements cause the hot cracking tendency in alloy welding process, hence it is evident that improve the intensity and welding performance of alloy, be this phase
After developing the high strength alumin ium alloy containing Sc.
In recent years, Russia takes the method that Sc and Zr is added into Al-Zn-Mg alloy, develops anti-fatigue performance, weldering
Connect high strength alumin ium alloy 1975,1970 of performance and good toughness etc..Domestic high strength alumin ium alloy development course is identical with foreign countries, at present
Also the laboratory trial-production of solderable high strength alumin ium alloy has been carried out in the country.But height is pursued in China when studying high-strength/tenacity aluminum alloy
Strength high toughness but ignores the production cost for reducing material, while the water that the existing high-strength/tenacity aluminum alloy in China can reach
It is flat to go back.
Chinese patent literature " a kind of rare earth modified aluminum alloy materials and preparation method thereof " (patent No.：
ZL201510310462.8 a kind of preparation method of rare earth modified aluminum alloy materials) is disclosed, it is completely molten by melting Al simple substance
Change temperature up to 850 DEG C, then add Cu, intermediate alloy is added after having melted, it is mono- that intermediate alloy includes Mn, Ni, Cr, Ti, Zr, Er, Yb
Matter, finally add Mg, Zn simple substance successively；Degasification removes the gred again after being completely melt, stands, casting of being cast when solution temperature is up to 750 DEG C
Ingot；Ingot casting is removed into top layer 1-2mm, is then placed in homogenization stove, 24h is incubated at 410 DEG C, then is cooled to less than 120 DEG C, is gone out
Stove air cooling, obtain homogenizing ingot casting；Homogenization ingot casting is subjected to hot rolling and hot extrusion at 450 DEG C, control total deformation is not small
In 60%, obtain deforming ingot casting；Deformation ingot casting is incubated 4h water quenchings immediately at 470 DEG C, then at 120 DEG C after timeliness 24h
Air cooling, obtain rare earth modified aluminum alloy materials.Aluminium alloy made from the invention has inexpensive, excellent impact flexibility, but deposits
Tensile strength, elongation percentage is relatively low the problem of.
The content of the invention
It is an object of the invention to provide a kind of aluminium-nickel-manganese-copper-lanthanum alloy intermediate and its application of aluminium alloy is prepared, with
Solve in Chinese patent literature " a kind of rare earth modified aluminum alloy materials and preparation method thereof the " (patent No.：
ZL201510310462.8 on the basis of aluminium alloy material material formula disclosed in), how to optimize component, dosage, method etc., improve aluminium and close
The tensile strength of gold, elongation percentage.
In order to solve the above technical problems, the present invention uses following technical scheme：
A kind of aluminium-nickel-manganese-copper-lanthanum alloy intermediate, in units of parts by weight, including following raw material：Aluminium 60-80 parts, nickel
2-5 parts, manganese 4-8 parts, copper 2-5 parts, lanthanum 1-1.6 parts.
Preferably, described aluminium-nickel-manganese-copper-lanthanum alloy intermediate, in units of parts by weight, including following raw material：Aluminium
70 parts, 4 parts of nickel, 6 parts of manganese, 3 parts of copper, 1.5 parts of lanthanum.
The present invention also provides a kind of aluminium-nickel-manganese-copper-application of the lanthanum alloy intermediate in aluminium alloy is prepared, described aluminium
Alloy, include the raw material of following mass percent：Zinc 3.2%-5.6%, magnesium 0.02%-0.18%, copper 0.03%-0.7%, manganese
0.1%-0.3%, nickel 0.1%-0.29%, zirconium 0.1%-0.9%, titanium 1.5%-1.8%, iron 0.4%-0.8%, chromium
0.02%-0.06%, rare earth element 1.2%-3%, refining agent 0.8%-1.5%, sldium lauryl sulfate 0.6%-1.2%, crystalline substance
Grain fining agent 2%-3.2%, remaining is aluminium；
Described grain refiner, in units of parts by weight, including following raw material：Aluminium-nickel-manganese-copper-lanthanum alloy intermediate
10-18 parts, aluminium-titanium-zirconium-cerium alloy intermediate 4-9 parts.
Preferably, described grain refiner, in units of parts by weight, including following raw material：Aluminium-nickel-manganese-copper-lanthanum closes
Golden 15 parts of intermediate, aluminium-titanium-zirconium -6 parts of cerium alloy intermediate.
Preferably, the aluminium-titanium-zirconium-cerium alloy intermediate is in units of parts by weight, including following raw material：Aluminium 40-75
Part, titanium 1.8-2.5 parts, zirconium 1-1.5 parts, cerium 0.5-0.8 parts.
Preferably, the rare earth element is in units of parts by weight, including following raw material：Lanthanum 1.5-2.5 parts, praseodymium 1-2 parts, neodymium
0.5-1.2 parts, dysprosium 0.6-0.9 parts, holmium 1.2-1.8 parts, ytterbium 0.3-0.9 parts.
Preferably, the rare earth element is in units of parts by weight, including following raw material：2 parts of lanthanum, 1.6 parts of praseodymium, 0.9 part of neodymium,
0.8 part of dysprosium, 1.7 parts of holmium, 0.8 part of ytterbium.
Preferably, the refining agent is in units of parts by weight, including following raw material：Sodium fluoride 18-25 parts, graphene 10-
15 parts, calcirm-fluoride 6-12 parts.
Preferably, the refining agent is in units of parts by weight, including following raw material：122 parts of sodium fluoride, 14 parts of graphene,
9 parts of calcirm-fluoride.
Preferably, the preparation method of the aluminium alloy, comprises the following steps：
S1：Add aluminium ingot in electromagnetic induction furnace, rise temperature makes its fusing to 880-920 DEG C, and addition is wrapped up with aluminium foil
The nickel of weight ratio, manganese, copper, the melting of lanthanum powder, and alloy melt is stirred, after stirring 15-20min, carries out degasification
Processing, stand, be then ultrasonically treated, obtain aluminium-nickel-manganese-copper-lanthanum alloy intermediate, the temperature of supersound process is 800-
820 DEG C, ultrasonic power 20-25KW, processing time 25-30min；Aluminium-titanium-zirconium-cerium alloy is prepared using identical method
Intermediate；Crystal grain refinement is made in aluminium-nickel-manganese-copper-lanthanum alloy intermediate and aluminium-titanium-zirconium-cerium alloy intermediate by weight
Agent, the size of the grain refiner is less than 12 μm；
S2：Zinc, magnesium, copper, manganese, nickel, zirconium, titanium, iron, chromium, rare earth element are put into smelting furnace by mass percentage and melted
Melt, obtain molten aluminium alloy；
S3：After molten aluminium alloy is warming up into 730-780 DEG C, the grain refiner stirring of mass percent is added；
S4：Refining agent, sldium lauryl sulfate are added in the liquation of gained in step s3, while is passed through inert gas, no
Disconnected stirring is refined, and it is 720-760 DEG C to control refining temperature, and liquation is carried out after refining to take off Slag treatment, is then cooled down, is stood
25-35min；
S5：The molten aluminium alloy of gained in step S3 is subjected to casting；
S6：450-500 DEG C, 5-8h solution treatment are carried out to casting, aluminium alloy is made.
The invention has the advantages that：
(1) from embodiment 1-3 and the data of comparative example 5, the tension of aluminum alloy materials is strong made from embodiment 1-3
Degree, elongation percentage are significantly higher than the tensile strength of aluminum alloy materials, elongation percentage made from comparative example 5；Simultaneously by embodiment 1-3 number
According to visible, embodiment 2 is optimum embodiment.
(2) existed from embodiment 2 and comparative example 1-4 data, rare earth element, sldium lauryl sulfate, grain refiner
Prepare and synergy is served in aluminum alloy materials, significantly improve tensile strength, the elongation percentage of aluminum alloy materials；This may
It is：1) addition of rare-earth elements of lanthanum, praseodymium, neodymium, dysprosium, holmium, ytterbium, compound that can be high with the gas such as hydrogen or nonmetallic generation fusing point,
There are certain dehydrogenation, refining and catharsis, so as to realize the tensile strength for improving aluminum alloy materials, elongation percentage；2) laruyl alcohol
Sodium sulphate is used together with the rare earth element of this formula, can improve the intensity and yield limit of aluminum alloy materials, improves aluminium conjunction
The tensile strength of golden material, elongation percentage；3) grain refiner is added in aluminum alloy materials, dispensing and bath composition can be reduced
Charging quantity, be advantageous to skim clean, so as to strengthen tensile strength, and overcome in the prior art using aluminium-titanium-
The problem of easily aggregation of chromium intermediate and slag inclusion；, can be in crystalline substance meanwhile grain refiner is used together with the rare earth element of this formula
Grain optionally adsorbs on interface, hinders the growth of crystal grain so that aluminum grain refinement, be advantageous to aluminum alloy materials and be broken
Crack initiation position and expansion path change in journey so that aluminum alloy materials obtain toughening, so as to improve aluminum alloy materials
Tensile strength, elongation percentage.
Embodiment
For ease of more fully understanding the present invention, it is illustrated by following instance, these examples belong to the protection of the present invention
Scope, but do not limit the scope of the invention.
In embodiment, the aluminium alloy, include the raw material of following mass percent：Zinc 3.2%-5.6%, magnesium
0.02%-0.18%, copper 0.03%-0.7%, manganese 0.1%-0.3%, nickel 0.1%-0.29%, zirconium 0.1%-0.9%, titanium
1.5%-1.8%, iron 0.4%-0.8%, chromium 0.02%-0.06%, rare earth element 1.2%-3%, refining agent 0.8%-
1.5%th, sldium lauryl sulfate 0.6%-1.2%, grain refiner 2%-3.2%, remaining is aluminium；
The rare earth element is in units of parts by weight, including following raw material：Lanthanum 1.5-2.5 parts, praseodymium 1-2 parts, neodymium 0.5-1.2
Part, dysprosium 0.6-0.9 parts, holmium 1.2-1.8 parts, ytterbium 0.3-0.9 parts；
The refining agent is in units of parts by weight, including following raw material：Sodium fluoride 18-25 parts, graphene 10-15 parts, fluorine
Change calcium 6-12 parts；
The grain refiner is in units of parts by weight, including following raw material：Aluminium-nickel-manganese-copper-lanthanum alloy intermediate 10-
18 parts, aluminium-titanium-zirconium-cerium alloy intermediate 4-9 parts；Aluminium-nickel-manganese-copper-lanthanum alloy the intermediate is in units of parts by weight, bag
Include following raw material：Aluminium 60-80 parts, nickel 2-5 parts, manganese 4-8 parts, copper 2-5 parts, lanthanum 1-1.6 parts；In the aluminium-titanium-zirconium-cerium alloy
Mesosome is in units of parts by weight, including following raw material：Aluminium 40-75 parts, titanium 1.8-2.5 parts, zirconium 1-1.5 parts, cerium 0.5-0.8 parts；
The preparation method of the aluminium alloy, comprises the following steps：
S1：Add aluminium ingot in electromagnetic induction furnace, rise temperature makes its fusing to 880-920 DEG C, and addition is wrapped up with aluminium foil
The nickel of weight ratio, manganese, copper, the melting of lanthanum powder, and alloy melt is stirred, after stirring 15-20min, carries out degasification
Processing, stand, be then ultrasonically treated, obtain aluminium-nickel-manganese-copper-lanthanum alloy intermediate, the temperature of supersound process is 800-
820 DEG C, ultrasonic power 20-25KW, processing time 25-30min；Aluminium-titanium-zirconium-cerium alloy is prepared using identical method
Intermediate；Crystal grain refinement is made in aluminium-nickel-manganese-copper-lanthanum alloy intermediate and aluminium-titanium-zirconium-cerium alloy intermediate by weight
Agent, the size of the grain refiner is less than 12 μm；
S2：Zinc, magnesium, copper, manganese, nickel, zirconium, titanium, iron, chromium, rare earth element are put into smelting furnace by mass percentage and melted
Melt, obtain molten aluminium alloy；
S3：After molten aluminium alloy is warming up into 730-780 DEG C, the grain refiner stirring of mass percent is added；
S4：Refining agent, sldium lauryl sulfate are added in the liquation of gained in step s3, while is passed through inert gas, no
Disconnected stirring is refined, and it is 720-760 DEG C to control refining temperature, and liquation is carried out after refining to take off Slag treatment, is then cooled down, is stood
25-35min；
S5：The molten aluminium alloy of gained in step S3 is subjected to casting；
S6：450-500 DEG C, 5-8h solution treatment are carried out to casting, aluminium alloy is made.
Below by more specific embodiment, the present invention will be described.
Embodiment 1
A kind of aluminium alloy, include the raw material of following mass percent：Zinc 3.5%, magnesium 0.06%, copper 0.03%-0.7%,
Manganese 0.1%, nickel 0.1%, zirconium 0.1%, titanium 1.5%, iron 0.4%, chromium 0.02%, rare earth element 1.2%, refining agent 0.8%, the moon
Lauryl sulfate 0.6%, grain refiner 2%, remaining is aluminium；
The rare earth element is in units of parts by weight, including following raw material：1.5 parts of lanthanum, praseodymium 1-2 parts, 0.5 part of neodymium, dysprosium 0.6
Part, 1.3 parts of holmium, 0.3 part of ytterbium；
The refining agent is in units of parts by weight, including following raw material：18 parts of sodium fluoride, 10 parts of graphene, calcirm-fluoride 6
Part；
The grain refiner is in units of parts by weight, including following raw material：Aluminium-nickel-manganese-copper-lanthanum alloy intermediate 10
Part, aluminium-titanium-zirconium -4 parts of cerium alloy intermediate；Aluminium-nickel-manganese-copper-lanthanum alloy the intermediate in units of parts by weight, including with
Lower raw material：60 parts of aluminium, 2 parts of nickel, 4 parts of manganese, 2 parts of copper, 1 part of lanthanum；Aluminium-titanium-zirconium-cerium alloy the intermediate is using parts by weight to be single
Position, including following raw material：40 parts of aluminium, 1.8 parts of titanium, 1 part of zirconium, 0.5 part of cerium；
The preparation method of the aluminium alloy, comprises the following steps：
S1：Add aluminium ingot in electromagnetic induction furnace, rise temperature makes its fusing, the weight that addition is wrapped up with aluminium foil to 880 DEG C
Nickel, manganese, copper, the lanthanum powder for measuring part ratio melt, and alloy melt are stirred, and after stirring 20min, carry out degassing processing, quiet
Put, be then ultrasonically treated, obtain aluminium-nickel-manganese-copper-lanthanum alloy intermediate, the temperature of supersound process is 800 DEG C, ultrasonic work(
Rate is 20KW, processing time 30min；Aluminium-titanium-zirconium-cerium alloy intermediate is prepared using identical method；By aluminium-nickel-manganese-
Grain refiner is made in copper-lanthanum alloy intermediate and aluminium-titanium-zirconium-cerium alloy intermediate by weight, the grain refiner
Size is less than 12 μm；
S2：Zinc, magnesium, copper, manganese, nickel, zirconium, titanium, iron, chromium, rare earth element are put into smelting furnace by mass percentage and melted
Melt, obtain molten aluminium alloy；
S3：After molten aluminium alloy is warming up into 730 DEG C, the grain refiner stirring of mass percent is added；
S4：Refining agent, sldium lauryl sulfate are added in the liquation of gained in step s3, while is passed through inert gas, no
Disconnected stirring is refined, and it is 720 DEG C to control refining temperature, and liquation is carried out after refining to take off Slag treatment, is then cooled down, is stood
35min；
S5：The molten aluminium alloy of gained in step S3 is subjected to casting；
S6：450 DEG C, 8h solution treatment are carried out to casting, aluminium alloy is made.
Embodiment 2
A kind of aluminium alloy, include the raw material of following mass percent：Zinc 4.5%, magnesium 0.1%, copper 0.32%, manganese 0.2%,
Nickel 0.16%, zirconium 0.5%, titanium 1.7%, iron 0.6%, chromium 0.05%, rare earth element 2.5%, refining agent 1.2%, laruyl alcohol sulphur
Sour sodium 0.9%, grain refiner 2.8%, remaining is aluminium；
The rare earth element is in units of parts by weight, including following raw material：2 parts of lanthanum, 1.6 parts of praseodymium, 0.9 part of neodymium, dysprosium 0.8
Part, 1.7 parts of holmium, 0.8 part of ytterbium；
The refining agent is in units of parts by weight, including following raw material：122 parts of sodium fluoride, 14 parts of graphene, calcirm-fluoride 9
Part；
The grain refiner is in units of parts by weight, including following raw material：Aluminium-nickel-manganese-copper-lanthanum alloy intermediate 15
Part, aluminium-titanium-zirconium -6 parts of cerium alloy intermediate；Aluminium-nickel-manganese-copper-lanthanum alloy the intermediate in units of parts by weight, including with
Lower raw material：70 parts of aluminium, 4 parts of nickel, 6 parts of manganese, 3 parts of copper, 1.5 parts of lanthanum；Aluminium-titanium-zirconium-cerium alloy the intermediate is using parts by weight to be single
Position, including following raw material：65 parts of aluminium, 2 parts of titanium, 1.2 parts of zirconium, 0.7 part of cerium；
The preparation method of the aluminium alloy, comprises the following steps：
S1：Add aluminium ingot in electromagnetic induction furnace, rise temperature makes its fusing, the weight that addition is wrapped up with aluminium foil to 900 DEG C
Nickel, manganese, copper, the lanthanum powder for measuring part ratio melt, and alloy melt are stirred, and after stirring 18min, carry out degassing processing, quiet
Put, be then ultrasonically treated, obtain aluminium-nickel-manganese-copper-lanthanum alloy intermediate, the temperature of supersound process is 815 DEG C, ultrasonic work(
Rate is 23KW, processing time 28min；Aluminium-titanium-zirconium-cerium alloy intermediate is prepared using identical method；By aluminium-nickel-manganese-
Grain refiner is made in copper-lanthanum alloy intermediate and aluminium-titanium-zirconium-cerium alloy intermediate by weight, the grain refiner
Size is less than 12 μm；
S2：Zinc, magnesium, copper, manganese, nickel, zirconium, titanium, iron, chromium, rare earth element are put into smelting furnace by mass percentage and melted
Melt, obtain molten aluminium alloy；
S3：After molten aluminium alloy is warming up into 760 DEG C, the grain refiner stirring of mass percent is added；
S4：Refining agent, sldium lauryl sulfate are added in the liquation of gained in step s3, while is passed through inert gas, no
Disconnected stirring is refined, and it is 740 DEG C to control refining temperature, and liquation is carried out after refining to take off Slag treatment, is then cooled down, is stood
32min；
S5：The molten aluminium alloy of gained in step S3 is subjected to casting；
S6：480 DEG C, 7h solution treatment are carried out to casting, aluminium alloy is made.
Embodiment 3
A kind of aluminium alloy, include the raw material of following mass percent：Zinc 2.5%, magnesium 0.18%, copper 0.7%, manganese 0.3%,
Nickel 0.29%, zirconium 0.9%, titanium 1.8%, iron 0.8%, chromium 0.06%, rare earth element 3%, refining agent 1.5%, laruyl alcohol sulfuric acid
Sodium 1.2%, grain refiner 3.2%, remaining is aluminium；
The rare earth element is in units of parts by weight, including following raw material：2.5 parts of lanthanum, 2 parts of praseodymium, 1.2 parts of neodymium, dysprosium 0.9
Part, 1.8 parts of holmium, 0.9 part of ytterbium；
The refining agent is in units of parts by weight, including following raw material：25 parts of sodium fluoride, 15 parts of graphene, calcirm-fluoride 12
Part；
The grain refiner is in units of parts by weight, including following raw material：Aluminium-nickel-manganese-copper-lanthanum alloy intermediate 18
Part, aluminium-titanium-zirconium -9 parts of cerium alloy intermediate；Aluminium-nickel-manganese-copper-lanthanum alloy the intermediate in units of parts by weight, including with
Lower raw material：80 parts of aluminium, 5 parts of nickel, 8 parts of manganese, 5 parts of copper, 1.6 parts of lanthanum；Aluminium-titanium-zirconium-cerium alloy the intermediate is using parts by weight to be single
Position, including following raw material：75 parts of aluminium, 2.5 parts of titanium, 1.5 parts of zirconium, 0.8 part of cerium；
The preparation method of the aluminium alloy, comprises the following steps：
S1：Add aluminium ingot in electromagnetic induction furnace, rise temperature makes its fusing, the weight that addition is wrapped up with aluminium foil to 920 DEG C
Nickel, manganese, copper, the lanthanum powder for measuring part ratio melt, and alloy melt are stirred, and after stirring 15min, carry out degassing processing, quiet
Put, be then ultrasonically treated, obtain aluminium-nickel-manganese-copper-lanthanum alloy intermediate, the temperature of supersound process is 820 DEG C, ultrasonic work(
Rate is 25KW, processing time 25min；Aluminium-titanium-zirconium-cerium alloy intermediate is prepared using identical method；By aluminium-nickel-manganese-
Grain refiner is made in copper-lanthanum alloy intermediate and aluminium-titanium-zirconium-cerium alloy intermediate by weight, the grain refiner
Size is less than 12 μm；
S2：Zinc, magnesium, copper, manganese, nickel, zirconium, titanium, iron, chromium, rare earth element are put into smelting furnace by mass percentage and melted
Melt, obtain molten aluminium alloy；
S3：After molten aluminium alloy is warming up into 780 DEG C, the grain refiner stirring of mass percent is added；
S4：Refining agent, sldium lauryl sulfate are added in the liquation of gained in step s3, while is passed through inert gas, no
Disconnected stirring is refined, and it is 760 DEG C to control refining temperature, and liquation is carried out after refining to take off Slag treatment, is then cooled down, is stood
25min；
S5：The molten aluminium alloy of gained in step S3 is subjected to casting；
S6：500 DEG C, 5h solution treatment are carried out to casting, aluminium alloy is made.
Comparative example 1
It is essentially identical with the preparation technology of embodiment 2, have only unlike prepare and lack rare earth member in the raw material of aluminium alloy
Element, sldium lauryl sulfate, grain refiner.
Comparative example 2
It is essentially identical with the preparation technology of embodiment 2, have only unlike prepare and lack rare earth member in the raw material of aluminium alloy
Element.
Comparative example 3
It is essentially identical with the preparation technology of embodiment 2, have only unlike prepare in the raw material of aluminium alloy and lack laruyl alcohol
Sodium sulphate.
Comparative example 4
It is essentially identical with the preparation technology of embodiment 2, have only unlike prepare that to lack crystal grain in the raw material of aluminium alloy thin
Agent.
Comparative example 5
Using Chinese patent literature " a kind of rare earth modified aluminum alloy materials and preparation method thereof the " (patent No.：
ZL201510310462.8) technique of effect example 1 prepares aluminum alloy materials.
Aluminum alloy materials made from embodiment 1-3 and comparative example 1-5 are carried out with performance test, it is as a result as shown in the table.Its
In, the test of tensile strength and elongation percentage is by (the embodiment and right of aluminum alloy plate materials made from embodiment 1-3 and comparative example 1-5
The sample board dimension of ratio is 12.26mm × 4.22mm) carry out performance test by standard GB/T/T228-2010.
As seen from the above table：(1) from embodiment 1-3 and the data of comparative example 5, aluminium alloy material made from embodiment 1-3
The tensile strength of material, elongation percentage are significantly higher than the tensile strength of aluminum alloy materials, elongation percentage made from comparative example 5；Simultaneously by reality
It is visible to apply the data of a 1-3, embodiment 2 is optimum embodiment.
(2) existed from embodiment 2 and comparative example 1-4 data, rare earth element, sldium lauryl sulfate, grain refiner
Prepare and synergy is served in aluminum alloy materials, significantly improve tensile strength, the elongation percentage of aluminum alloy materials；This may
It is：1) addition of rare-earth elements of lanthanum, praseodymium, neodymium, dysprosium, holmium, ytterbium, compound that can be high with the gas such as hydrogen or nonmetallic generation fusing point,
There are certain dehydrogenation, refining and catharsis, so as to realize the tensile strength for improving aluminum alloy materials, elongation percentage；2) laruyl alcohol
Sodium sulphate is used together with the rare earth element of this formula, can improve the intensity and yield limit of aluminum alloy materials, improves aluminium conjunction
The tensile strength of golden material, elongation percentage；3) grain refiner is added in aluminum alloy materials, dispensing and bath composition can be reduced
Charging quantity, be advantageous to skim clean, so as to strengthen tensile strength, and overcome in the prior art using aluminium-titanium-
The problem of easily aggregation of chromium intermediate and slag inclusion；, can be in crystalline substance meanwhile grain refiner is used together with the rare earth element of this formula
Grain optionally adsorbs on interface, hinders the growth of crystal grain so that aluminum grain refinement, be advantageous to aluminum alloy materials and be broken
Crack initiation position and expansion path change in journey so that aluminum alloy materials obtain toughening, so as to improve aluminum alloy materials
Tensile strength, elongation percentage.
The preferred embodiments of the present invention are the foregoing is only, are not intended to limit the invention, for the skill of this area
For art personnel, the present invention can have various modifications and variations.Within the spirit and principles of the invention, that is made any repaiies
Change, equivalent substitution, improvement etc., should be included in the scope of the protection.
Claims (10)
- A kind of 1. aluminium-nickel-manganese-copper-lanthanum alloy intermediate, it is characterised in that in units of parts by weight, including following raw material：Aluminium 60-80 parts, nickel 2-5 parts, manganese 4-8 parts, copper 2-5 parts, lanthanum 1-1.6 parts.
- 2. aluminium-nickel-manganese-copper-lanthanum alloy intermediate according to claim 1, it is characterised in that in units of parts by weight, Including following raw material：70 parts of aluminium, 4 parts of nickel, 6 parts of manganese, 3 parts of copper, 1.5 parts of lanthanum.
- 3. a kind of aluminium-nickel-manganese-copper-lanthanum alloy intermediate according to any one of claim 1 or 2 is in aluminium alloy is prepared Application, it is characterised in that described aluminium alloy, include the raw material of following mass percent：Zinc 3.2%-5.6%, magnesium 0.02%-0.18%, copper 0.03%-0.7%, manganese 0.1%-0.3%, nickel 0.1%-0.29%, zirconium 0.1%-0.9%, titanium 1.5%-1.8%, iron 0.4%-0.8%, chromium 0.02%-0.06%, rare earth element 1.2%-3%, refining agent 0.8%- 1.5%th, sldium lauryl sulfate 0.6%-1.2%, grain refiner 2%-3.2%, remaining is aluminium；Described grain refiner, in units of parts by weight, including following raw material：Aluminium-nickel-manganese-copper-lanthanum alloy intermediate 10- 18 parts, aluminium-titanium-zirconium-cerium alloy intermediate 4-9 parts.
- 4. aluminium-nickel-manganese-copper-application of the lanthanum alloy intermediate in aluminium alloy is prepared according to claim 1, its feature It is, described grain refiner, in units of parts by weight, including following raw material：Aluminium-nickel-manganese-copper-lanthanum alloy intermediate 15 Part, aluminium-titanium-zirconium -6 parts of cerium alloy intermediate.
- 5. aluminium-nickel-manganese-copper-application of the lanthanum alloy intermediate in aluminium alloy is prepared according to claim 4, its feature It is, the aluminium-titanium-zirconium-cerium alloy intermediate is in units of parts by weight, including following raw material：Aluminium 40-75 parts, titanium 1.8-2.5 Part, zirconium 1-1.5 parts, cerium 0.5-0.8 parts.
- 6. aluminium-nickel-manganese-copper-application of the lanthanum alloy intermediate in aluminium alloy is prepared according to claim 3, its feature It is, the rare earth element is in units of parts by weight, including following raw material：Lanthanum 1.5-2.5 parts, praseodymium 1-2 parts, neodymium 0.5-1.2 parts, Dysprosium 0.6-0.9 parts, holmium 1.2-1.8 parts, ytterbium 0.3-0.9 parts.
- 7. aluminium-nickel-manganese-copper-application of the lanthanum alloy intermediate in aluminium alloy is prepared according to claim 6, its feature It is, the rare earth element is in units of parts by weight, including following raw material：2 parts of lanthanum, 1.6 parts of praseodymium, 0.9 part of neodymium, 0.8 part of dysprosium, holmium 1.7 parts, 0.8 part of ytterbium.
- 8. aluminium-nickel-manganese-copper-application of the lanthanum alloy intermediate in aluminium alloy is prepared according to claim 3, its feature It is, the refining agent is in units of parts by weight, including following raw material：Sodium fluoride 18-25 parts, graphene 10-15 parts, calcirm-fluoride 6-12 parts.
- 9. application of the grain refiner according to claim 8 in aluminium alloy is prepared, it is characterised in that the refining agent In units of parts by weight, including following raw material：122 parts of sodium fluoride, 14 parts of graphene, 9 parts of calcirm-fluoride.
- 10. application of the grain refiner according to claim any one of 3-9 in aluminium alloy is prepared, it is characterised in that The preparation method of the aluminium alloy, comprises the following steps：S1：Add aluminium ingot in electromagnetic induction furnace, rise temperature makes its fusing, the weight that addition is wrapped up with aluminium foil to 880-920 DEG C Nickel, manganese, copper, the lanthanum powder for measuring part ratio melt, and alloy melt are stirred, and after stirring 15-20min, carry out degassing processing, Standing, be then ultrasonically treated, obtain aluminium-nickel-manganese-copper-lanthanum alloy intermediate, the temperature of supersound process is 800-820 DEG C, Ultrasonic power is 20-25KW, processing time 25-30min；Aluminium-titanium-zirconium-cerium alloy intermediate is prepared using identical method； Grain refiner is made in aluminium-nickel-manganese-copper-lanthanum alloy intermediate and aluminium-titanium-zirconium-cerium alloy intermediate by weight, it is described The size of grain refiner is less than 12 μm；S2：Zinc, magnesium, copper, manganese, nickel, zirconium, titanium, iron, chromium, rare earth element are put into smelting furnace melt by mass percentage, is obtained Molten aluminium alloy；S3：After molten aluminium alloy is warming up into 730-780 DEG C, the grain refiner stirring of mass percent is added；S4：Refining agent, sldium lauryl sulfate are added in the liquation of gained in step s3, while is passed through inert gas, is constantly stirred Mix and refined, it is 720-760 DEG C to control refining temperature, and liquation is carried out after refining to take off Slag treatment, then cools down, stands 25- 35min；S5：The molten aluminium alloy of gained in step S3 is subjected to casting；S6：450-500 DEG C, 5-8h solution treatment are carried out to casting, aluminium alloy is made.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711213347.4A CN107739907A (en) | 2017-11-28 | 2017-11-28 | Aluminium nickel copper-manganese lanthanum alloy intermediate and its application for preparing aluminium alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711213347.4A CN107739907A (en) | 2017-11-28 | 2017-11-28 | Aluminium nickel copper-manganese lanthanum alloy intermediate and its application for preparing aluminium alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107739907A true CN107739907A (en) | 2018-02-27 |
Family
ID=61239567
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711213347.4A Pending CN107739907A (en) | 2017-11-28 | 2017-11-28 | Aluminium nickel copper-manganese lanthanum alloy intermediate and its application for preparing aluminium alloy |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107739907A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101693956A (en) * | 2009-10-12 | 2010-04-14 | 江阴裕华铝业有限公司 | Preparation process of high-strength and high-plasticity 6061 and 6063 aluminum alloy and sectional material thereof |
| CN102041405A (en) * | 2009-10-09 | 2011-05-04 | 韦斌 | Strengthening technique of alloy elements in automobile wheel hub |
| CN102312135A (en) * | 2010-06-30 | 2012-01-11 | 通用汽车环球科技运作有限责任公司 | Improved y alloy y |
| CN103103415A (en) * | 2012-12-11 | 2013-05-15 | 芜湖恒坤汽车部件有限公司 | Smelting and preparation method of aluminum alloy profile |
| CN103710592A (en) * | 2013-12-17 | 2014-04-09 | 芜湖万润机械有限责任公司 | Preparation method of aluminum alloy profile for high speed train body |
| CN105039798A (en) * | 2014-04-30 | 2015-11-11 | 通用汽车环球科技运作有限责任公司 | Cast aluminum alloy components |
-
2017
- 2017-11-28 CN CN201711213347.4A patent/CN107739907A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102041405A (en) * | 2009-10-09 | 2011-05-04 | 韦斌 | Strengthening technique of alloy elements in automobile wheel hub |
| CN101693956A (en) * | 2009-10-12 | 2010-04-14 | 江阴裕华铝业有限公司 | Preparation process of high-strength and high-plasticity 6061 and 6063 aluminum alloy and sectional material thereof |
| CN102312135A (en) * | 2010-06-30 | 2012-01-11 | 通用汽车环球科技运作有限责任公司 | Improved y alloy y |
| CN103103415A (en) * | 2012-12-11 | 2013-05-15 | 芜湖恒坤汽车部件有限公司 | Smelting and preparation method of aluminum alloy profile |
| CN103710592A (en) * | 2013-12-17 | 2014-04-09 | 芜湖万润机械有限责任公司 | Preparation method of aluminum alloy profile for high speed train body |
| CN105039798A (en) * | 2014-04-30 | 2015-11-11 | 通用汽车环球科技运作有限责任公司 | Cast aluminum alloy components |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| AU2010239014B2 (en) | High-elongation rate aluminum alloy material for cable and preparation method thereof | |
| CN102978449B (en) | Al-Fe-Sb-RE aluminum alloy, and preparation method and power cable thereof | |
| CN102978448B (en) | Al-Fe-Ba-RE aluminum alloy, and preparation method and power cable thereof | |
| CN106834846B (en) | A kind of multicomponent heat-resistant corrosion-resistant magnesium alloy and preparation method | |
| CN102816959B (en) | Large-specification aluminum alloy round bar and casting method thereof | |
| CN106148786B (en) | High-strength casting magnesium lithium alloy and preparation method thereof | |
| CN112143945B (en) | High-strength and high-toughness cast aluminum-silicon alloy containing multiple composite rare earth elements and preparation method thereof | |
| WO2011035652A1 (en) | High-strength heat-proof aluminum alloy material containing lithium and rare earth and producing method thereof | |
| CN107447150B (en) | A kind of corrosion resistance structure aluminium alloy and preparation method | |
| CN101445886A (en) | High-strength high-toughness aluminum alloy pre-tensioned thick plate and preparation method thereof | |
| CN103572106B (en) | Aluminum alloy materials | |
| CN107587012A (en) | A kind of lightweight casting Al Si Li alloy materials and preparation method thereof | |
| CN109252073A (en) | High-strength tenacity aluminium alloy space material and preparation method thereof | |
| CN109628805A (en) | A kind of aluminium alloy and preparation method thereof | |
| CN110229984A (en) | A kind of high intensity Mg-Gd-Er-Y magnesium alloy and preparation method thereof | |
| CN107828999A (en) | The heat treatment method and die-cast aluminum alloy material of a kind of pack alloy | |
| CN107354349A (en) | A kind of tank body material is with high-performance containing nearly cocrystallized Al-Si alloys of Zn and preparation method thereof | |
| CN107460380B (en) | A kind of anticorodal and preparation method thereof | |
| CN106967910B (en) | A kind of high intensity Al-Zn-Mg line aluminium alloys and preparation method thereof | |
| CN107739866A (en) | Grain refiner and its application in rare earth aluminum alloy material is prepared | |
| CN107937745A (en) | Aluminium titanium zirconium cerium alloy intermediate, aluminum alloy materials and preparation method thereof | |
| CN107974577A (en) | A kind of aluminium alloys for automobile body sheets containing rare earth and preparation method thereof | |
| CN107099710A (en) | A kind of aluminium copper and its casting method | |
| CN114717453B (en) | High-toughness cast aluminum-silicon alloy and preparation method thereof | |
| CN107739907A (en) | Aluminium nickel copper-manganese lanthanum alloy intermediate and its application for preparing aluminium alloy |
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 | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180227 |