CN107267823B - A kind of aviation alloyed aluminium - Google Patents
A kind of aviation alloyed aluminium Download PDFInfo
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- CN107267823B CN107267823B CN201710550009.3A CN201710550009A CN107267823B CN 107267823 B CN107267823 B CN 107267823B CN 201710550009 A CN201710550009 A CN 201710550009A CN 107267823 B CN107267823 B CN 107267823B
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/10—Alloys based on aluminium with zinc as the next major constituent
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/001—Continuous casting of metals, i.e. casting in indefinite lengths of specific alloys
- B22D11/003—Aluminium alloys
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- 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
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- 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
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/053—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with zinc as the next major constituent
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Abstract
The invention discloses a kind of aviation alloyed aluminium, which is made of the element of following mass percent：Si 0.01-0.1%, Fe 0.15-0.2%, Cu 4.6-5.5%, Mn 0.3-0.5%, Mg 1.1-2.2%, Cr 0.01-0.04%, Zn 7.4-8.4%, Zr 0.15-0.2%, Ti 0.01-0.1%, Cd 0.1-0.2%, B 0.01-0.2%, Sc 0.1-0.2%, Ce 0.15-0.3%, V 0.05-0.1%, Re 0.05-0.2%, surplus Al.Aluminum alloy materials performance of the present invention protrudes, and manufacturing cost is low, while having excellent intensity, toughness and heat resistance.
Description
Technical field
The invention belongs to aluminum alloy materials field more particularly to a kind of aviation Al-Zn-Mg-Cu aluminum alloys.
Background technology
Aluminium alloy is most widely used one kind non-ferrous metal structural material in industry, in Aeronautics and Astronautics, automobile, machinery
It has been widely applied in manufacture, ship and chemical industry.It is ultrahigh-strength aluminum alloy that Al-Zn-Mg-Cu aluminum alloy, which belongs to 7, this is
Row alloy yield tensile ratio and specific strength are very high, have very high room temperature intensity, good corrosion resistance and high toughness, are answered extensively
For aerospace field.Currently, having had developed a series of superhigh intensity aluminium such as 7050,7055,7068,7150 both at home and abroad
Alloy, however, with the fast development of aeronautical and space technology, at present for Al-Zn-Mg-Cu aluminum alloy intensity, toughness,
More stringent requirements are proposed in terms of heat resistance and manufacturing cost.
Invention content
The purpose of the present invention is to provide one kind have high intensity, high tenacity, high-fire resistance and manufacturing method it is easy to operate,
Lower-cost Al-Zn-Mg-Cu systems ultrahigh-strength aluminum alloy.
The purpose of the present invention is achieved through the following technical solutions：
A kind of aviation alloyed aluminium, component and mass percentage are as follows：
Si 0.01~0.1%
Fe 0.15~0.2%
Cu 4.6~5.5%
Mn 0.3~0.5%
Mg 1.1~2.2%
Cr 0.01~0.04%
Zn 7.4-8.4%
Zr 0.15-0.2%
Ti 0.01~0.1%
Cd 0.1~0.2%
B 0.01~0.2%
Sc 0.1~0.2%
Ce 0.15~0.3%
V 0.05~0.1%
Re 0.05~0.2%.
Further, component and mass percentage are as follows：
Si 0.01%
Fe 0.15%
Cu 4.6%
Mn 0.3%
Mg 1.1%
Cr 0.01%
Zn 7.4%
Zr 0.15%
Ti 0.01%
Cd 0.1%
B 0.01%
Sc 0.1%
Ce 0.15%
V 0.05%
Re 0.05%
Al surpluses.
Optionally, component and mass percentage are as follows：
Si 0.1%
Fe 0.2%
Cu 5.5%
Mn 0.5%
Mg 2.2%
Cr 0.04%
Zn 8.4%
Zr 0.2%
Ti 0.1%
Cd 0.2%
B 0.2%
Sc 0.2%
Ce 0.3%
V 0.1%
Re 0.2%
Al surpluses.
Further, the preparation method of the aviation alloyed aluminium is：
(1) melting：Fine aluminium ingot, pure magnesium ingot, pure zinc ingot, tough cathode input smelting furnace are subjected to melting, smelting temperature 725-
765 DEG C, be sufficiently stirred using magnetic stirrer in fusion process, then put into Si, Fe, Mn, Cr, Zr, Ti, Cd, B, Sc,
Each intermediate alloy raw material of Ce, V, Re, adjustment temperature are 745-770 DEG C, until completely melted sampling analysis chemical composition, and seeing is
It is no to meet Composition Control requirement, Composition Control is carried out if necessary to be adjusted to obtain aluminium alloy melt；
(2) it refines：Refining agent is added to refine melt, to eliminate gas in melt, oxidation film and field trash；
(3) it skims and stirs：Aluminium alloy melt is stirred after skimming, and then stands 25-45 minutes, waits for casting
It makes；
(4) it casts：It is cast using semi-continuous casting method, semi-continuous casting temperature is 730 DEG C~750 DEG C, casting speed
Degree is 40mm/min~60mm/min, and cooling water intensity is 0.06MPa~0.12MPa, and electromagnetic induction is arranged in crystallizer
The frequency of coil, magnetic field is 1000~3000Hz, and the magnetic field intensity of crystallizer center is 15~25mT；
(5) Homogenization Treatments：Homogenization Treatments are carried out to ingot casting to rise to first with the heating rate of 100-130 DEG C/h
300-320 DEG C, keep the temperature 3-4h, then with the heating rate of 50-70 DEG C/h, rise to 450-480 DEG C, keep the temperature 4-6h, then it is air-cooled extremely
250-290 DEG C, 2-3h is kept the temperature, room temperature is then air-cooled to, then with the heating rate of 100-150 DEG C/h, rise to 480-500 DEG C, protects
Warm 5-8h is down to 150-180 DEG C with the rate of temperature fall of 140-180 DEG C/h, keeps the temperature 1-2h, water cooling to room temperature, then with 100-
The heating rate of 150 DEG C/h rises to 300-330 DEG C, keeps the temperature 1-3h, comes out of the stove and be air-cooled to room temperature；
(6) ingot casting after Homogenization Treatments is subjected to hot extrusion, hot rolling or forging technology as needed, be processed into specified
The semi-finished product of shape；
(7) semi-finished product are quenched, aging strengthening model can be obtained aviation alloyed aluminium.
Further, the fine aluminium ingot described in step (1), pure magnesium ingot, pure zinc ingot purity are all higher than 99.99%.
Further, step (2) refining carries out in enclosed environment, refining time 5-10min.
Further, step (4) semi-continuous casting is tapered using crystallizer graphite liner band, and cooling water hole center line
It it is 20-40 ° with cavity centerlines.
The fine aluminium ingot, pure magnesium ingot, pure zinc ingot purity are all higher than 99.99%.
High intensity of the present invention, high tenacity, the composition design of high-fire resistance aluminium alloy are according to as follows：
Si elements are the main components for improving mobile performance, and best mobility can be obtained from eutectic to hypereutectic.Separately
Outside, intensity when Si can improve tensile strength, hardness, machinability and high temperature, and elongation percentage is made to reduce, and Si can also be with Mg shapes
At Mg-Si metallic compounds, improve the hot property of aluminium alloy.
The effect of addition Fe elements is that Al can form Al with Fe3Fe, the Al of precipitation3Fe diffusing particles inhibit aluminium alloy
The deformation of creep, and improve the stability of connection.In addition Fe can also improve the tensile strength of aluminium base, yield limit and heat-resisting
Performance improves the plasticity of aluminium alloy.When Fe in alloy content 0.1% hereinafter, to aluminium base performance change very little, but containing
Fe elements are added in the alloy of Mn or Cr, work as Fe>When 0.3%, since Fe and Mn or Cr forms insoluble intermetallic compound, from
And reduce the content of Mn and Cr in solid solution, to reduce quenching effect and timeliness effect.
Mn elements can form Al with Al and Cu2Mn2Cu phases are precipitated with small and dispersed particle, hinder dislocation motion, are improved and are closed
Golden room temperature intensity and elevated temperature strength, addition Mn can improve quenching effect and timeliness effect, when the additive amount of Mn is 0.3-0.5%
When, quenching effect increases apparent.
(CrFe) A that Cr elements are formed in Al17(CrMn) Al13Equal intermetallic compounds, can crystal grain thinning, resistance
Only recrystallization and crystal grain are grown up, and have certain invigoration effect to alloy, moreover it is possible to be improved alloy ductility and be reduced stress corrosion sensitivity
Property.But when Cr contents are high, quenching sensitive is reinforced, and drop is low-alloyed from hardenability, in order to make the quenching degree from quenching property and thick member
Well, Cr contents should be controlled.
Zr elements form ZrAl as addition element, Zr and Al3Compound can hinder recrystallization process, refinement recrystallization
Crystal grain, on the other hand, Zr form complicated alloy cpd with Fe, Cu and Al, can improve the anti-fatigue performance of aluminium alloy.And
In Al-Zn-Mg-Cu aluminum alloy, influence ratio Cr's and Mn due to Zr to quenching sensitive is small, is preferably replaced with Zr
Part Cr and Mn refine recrystallized structure.
Sc has a significant impact the tissue and performance of aluminium alloy, and meeting is in solid solution or ag(e)ing process after Sc is added in Al alloy
The disperse phase with matrix coherence is precipitated, with ZrAl3There is similar effect, but better, in addition Al3Sc fine uniforms itself, can
With refined cast structure, so as to improve the welding performance of alloy.
Ce has the function of refining as-cast grain size, reduces the failure procedure precipitate speed of growth.
Ti only micro need to be such that mechanical performance improves in aluminium alloy, can be formed with multiple elements such as Fe, Mg, Cu, RE
Aluminium base complex compound, effective crystallization of refinement.
B and Cd elements：Cd has significant impact, Cd that can inhibit the low of made of Al-Cu alloy the ag(e)ing process of made of Al-Cu alloy
Warm hardening promotes the high-temperature aging of alloy so that the time that alloy reaches timeliness hardness and strength peak value shortens, and timeliness peak value carries
It is high.B and Cd can play refining alloy tissue simultaneously, improve the plasticity of alloy, micro Cd can be increased sharply the surrender of alloy
Intensity reduces elongation percentage, and when Cd is more than 0.3%, then there are the free Cd of more low melting point, and casting quenching easily to be caused to be opened for crystal boundary
It splits.
V element：Compound can be formed in aluminium alloy melt with elements such as Fe, Cu, RE to be distributed in aluminium base, and there is high temperature
The effect of reinforcing can also reduce the tendency to form pin hole while improving heat resistance, improve compactness.
RE：Rare earth element, which is added in aluminium alloy, can play the role of microalloying；In addition, the gases such as it and hydrogen and many
It is nonmetallic to have stronger affinity, the high compound of fusing point can be generated, therefore it has certain dehydrogenation, refining, catharsis；Together
When, Rare-Earth Element Chemistry activity is extremely strong, it can selectively be adsorbed on the crystal grain boundary grown up, and hinder the growth of crystal grain,
As a result lead to crystal grain refinement, play the role of rotten.
Beneficial effects of the present invention：
1. the present invention is redesigned by the ingredient to traditional Al-Zn-Mg-Cu aluminum alloy, lot of trace is added
Element adjusts the relative amount of Zn, Mg, Cu, and is strictly controlled the content of each addition trace element so that the aluminium of manufacture
Alloy structure is uniform, tiny, while improving the intensity, toughness and heat resistance of aluminium alloy.
2. the preparation method of the aviation alloyed aluminium of the present invention is easy to operate, manufacturing cost is low, by melting, refines, takes off
Slag, semi-continuous casting ensure that the purity of aluminium alloy cast ingot；By to the well-designed of Homogenization Treatments, making mixed with lot of trace
The aluminum alloy organization of element tends to be uniform, ensure that its good mechanical property.
3. the aviation alloyed aluminium tensile strength of the present invention is more than 700MPa, yield strength be more than 640MPa,
Elongation percentage is more than 9.0%, and can be used above at 250 DEG C for a long time.
Specific implementation mode
The technical solution work of the aviation alloyed aluminium of the present invention is further explained below by way of specific three embodiments
It states.
Embodiment 1
(1) dispensing：The mass percent of the aviation alloyed aluminium each element is：Si0.01%, Fe0.15%,
Cu4.6%, Mn0.3%, Mg1.1%, Cr0.01%, Zn7.4%, Zr0.15%, Ti0.01%, Cd0.1%, B0.01%,
Sc0.1%, Ce0.15%, V0.05%, Re0.05%, surplus Al, according to above-mentioned mass percent dispensing, wherein Al, Mg,
Zn and Cu prepares raw material in the form of fine aluminium ingot, pure magnesium ingot, pure zinc ingot, tough cathode, Si, Fe, Mn, Cr, Zr, Ti, Cd, B, Sc,
Ce, V, Re prepare raw material in the form of intermediate alloy；
(2) melting：Fine aluminium ingot, pure magnesium ingot, pure zinc ingot, tough cathode input smelting furnace are subjected to melting, smelting temperature 765
DEG C, be sufficiently stirred using magnetic stirrer in fusion process, then put into Si, Fe, Mn, Cr, Zr, Ti, Cd, B, Sc, Ce,
V, each intermediate alloy raw material of Re, adjustment temperature is 770 DEG C, and sampling analysis chemical composition, sees whether meet until completely melted
Composition Control requirement carries out Composition Control and adjusts to obtain aluminium alloy melt if necessary；
(3) it refines：Refining agent is added to refine melt, to eliminate gas in melt, oxidation film and field trash；
(4) it skims and stirs：Aluminium alloy melt is stirred after skimming, and then stands 30 minutes, is waited to be cast；
(5) it casts：It is cast using semi-continuous casting method, semi-continuous casting temperature is 750 DEG C, and casting speed is
50mm/min, cooling water intensity is 0.1MPa, and electromagnetic induction coil is arranged in crystallizer, and the frequency in magnetic field is 2000Hz,
The magnetic field intensity of crystallizer center is 25mT.
(6) Homogenization Treatments：Homogenization Treatments are carried out to ingot casting and rise to 320 DEG C first with the heating rate of 130 DEG C/h,
4h is kept the temperature, then with the heating rate of 70 DEG C/h, rises to 480 DEG C, 6h is kept the temperature, then air-cooled to 290 DEG C, keeps the temperature 3h, it is then air-cooled
To room temperature, then with the heating rate of 150 DEG C/h, 500 DEG C being risen to, heat preservation 8h is down to 180 DEG C with the rate of temperature fall of 180 DEG C/h,
2h is kept the temperature, water cooling to room temperature rises to 330 DEG C then with the heating rate of 150 DEG C/h, keeps the temperature 3h, come out of the stove and be air-cooled to room temperature；
(7) ingot casting after Homogenization Treatments is subjected to hot extrusion as needed, is processed into the semi-finished product of designated shape；
(8) semi-finished product are quenched, aging strengthening model obtains high intensity, high tenacity, high-fire resistance aviation are closed with aluminium
Golden material.
Embodiment 2
(1) dispensing：The mass percent of the aluminum alloy materials each element is：Si0.1%, Fe0.2%, Cu5.5%,
Mn0.5%, Mg2.2%, Cr0.04%, Zn8.4%, Zr0.2%, Ti0.1%, Cd0.2%, B0.2%, Sc0.2%,
Ce0.3%, V0.1%, Re0.2%, surplus Al, according to above-mentioned mass percent dispensing, wherein Al, Mg, Zn and Cu are with fine aluminium
The form preparation raw material of ingot, pure magnesium ingot, pure zinc ingot, tough cathode, Si, Fe, Mn, Cr, Zr, Ti, Cd, B, Sc, Ce, V, Re are with centre
The form of alloy prepares raw material；
(2) melting：Fine aluminium ingot, pure magnesium ingot, pure zinc ingot, tough cathode input smelting furnace are subjected to melting, smelting temperature 725
DEG C, be sufficiently stirred using magnetic stirrer in fusion process, then put into Si, Fe, Mn, Cr, Zr, Ti, Cd, B, Sc, Ce,
V, each intermediate alloy raw material of Re, adjustment temperature is 745 DEG C, and sampling analysis chemical composition, sees whether meet until completely melted
Composition Control requirement carries out Composition Control and adjusts to obtain aluminium alloy melt if necessary；
(3) it refines：Refining agent is added to refine melt, to eliminate gas in melt, oxidation film and field trash；
(4) it skims and stirs：Aluminium alloy melt is stirred after skimming, and then stands 30 minutes, is waited to be cast；
(5) it casts：It is cast using semi-continuous casting method, semi-continuous casting temperature is 730 DEG C, and casting speed is
50mm/min, cooling water intensity is 0.1MPa, and electromagnetic induction coil is arranged in crystallizer, and the frequency in magnetic field is 2000Hz,
The magnetic field intensity of crystallizer center is 25mT.
(6) Homogenization Treatments：Homogenization Treatments are carried out to ingot casting and rise to 300 DEG C first with the heating rate of 100 DEG C/h,
3h is kept the temperature, then with the heating rate of 50 DEG C/h, rises to 450 DEG C, 4h is kept the temperature, then air-cooled to 250 DEG C, keeps the temperature 2h, it is then air-cooled
To room temperature, then with the heating rate of 100 DEG C/h, 480 DEG C being risen to, heat preservation 5h is down to 150 DEG C with the rate of temperature fall of 140 DEG C/h,
1h is kept the temperature, water cooling to room temperature rises to 300 DEG C then with the heating rate of 100 DEG C/h, keeps the temperature 1h, come out of the stove and be air-cooled to room temperature；
(7) ingot casting after Homogenization Treatments is subjected to hot rolling as needed, is processed into the semi-finished product of designated shape；
(8) semi-finished product are quenched, aging strengthening model obtains high intensity, high tenacity, high-fire resistance aviation are closed with aluminium
Golden material.
Embodiment 3
(1) dispensing：The mass percent of the aluminum alloy materials each element is：Si0.01%, Fe0.18%, Cu5.0%,
Mn0.4%, Mg1.8%, Cr0.02%, Zn8.0%, Zr0.2%, Ti0.05%, Cd0.15%, B0.1%, Sc0.15%,
Ce0.2%, V0.07%, Re0.1%, surplus is Al and impurity, according to above-mentioned mass percent dispensing, wherein Al, Mg, Zn and
Cu prepares raw material in the form of fine aluminium ingot, pure magnesium ingot, pure zinc ingot, tough cathode, Si, Fe, Mn, Cr, Zr, Ti, Cd, B, Sc, Ce, V,
Re prepares raw material in the form of intermediate alloy；
(2) melting：Fine aluminium ingot, pure magnesium ingot, pure zinc ingot, tough cathode input smelting furnace are subjected to melting, smelting temperature 745
DEG C, be sufficiently stirred using magnetic stirrer in fusion process, then put into Si, Fe, Mn, Cr, Zr, Ti, Cd, B, Sc, Ce,
V, each intermediate alloy raw material of Re, adjustment temperature is 760 DEG C, and sampling analysis chemical composition, sees whether meet until completely melted
Composition Control requirement carries out Composition Control and adjusts to obtain aluminium alloy melt if necessary；
(3) it refines：Refining agent is added to refine melt, to eliminate gas in melt, oxidation film and field trash；
(4) it skims and stirs：Aluminium alloy melt is stirred after skimming, and then stands 30 minutes, is waited to be cast；
(5) it casts：It is cast using semi-continuous casting method, semi-continuous casting temperature is 745 DEG C, and casting speed is
50mm/min, cooling water intensity is 0.11MPa, and electromagnetic induction coil is arranged in crystallizer, and the frequency in magnetic field is 2000Hz,
The magnetic field intensity of crystallizer center is 20mT.
(6) Homogenization Treatments：Homogenization Treatments are carried out to ingot casting and rise to 310 DEG C first with the heating rate of 120 DEG C/h,
3h is kept the temperature, then with the heating rate of 60 DEG C/h, rises to 470 DEG C, 4h is kept the temperature, then air-cooled to 280 DEG C, keeps the temperature 3h, it is then air-cooled
To room temperature, then with the heating rate of 150 DEG C/h, 500 DEG C being risen to, heat preservation 7h is down to 150 DEG C with the rate of temperature fall of 175 DEG C/h,
1h is kept the temperature, water cooling to room temperature rises to 320 DEG C then with the heating rate of 140 DEG C/h, keeps the temperature 2h, come out of the stove and be air-cooled to room temperature；
(7) ingot casting after Homogenization Treatments is subjected to forging technology as needed, is processed into the semi-finished product of designated shape；
(8) semi-finished product are quenched, aging strengthening model can be obtained high intensity, high tenacity, high-fire resistance aviation aluminium
Alloy material.
Not only intensity is high for the aluminium alloy that manufacturing method according to the invention obtains, good toughness, and heat-resist (being shown in Table 1),
It is easy to be cast, extrusion molding and subsequent machining disclosure satisfy that harshness of the aerospace field for material property
It is required that.
1 each embodiment of table manufactures the mechanical experimental results of aluminum alloy materials
Above-mentioned specific implementation can by those skilled in the art under the premise of without departing substantially from the principle of the invention and objective with difference
Mode carry out local directed complete set to it, protection scope of the present invention is subject to claims and not by above-mentioned specific implementation institute
Limit, each implementation within its scope is by the constraint of the present invention.
Claims (6)
1. a kind of aviation alloyed aluminium, which is characterized in that its component and mass percentage are as follows：
Preparation method is as follows：
(1) melting：Fine aluminium ingot, pure magnesium ingot, pure zinc ingot, tough cathode input smelting furnace are subjected to melting, smelting temperature 725-765
DEG C, be sufficiently stirred using magnetic stirrer in fusion process, then put into Si, Fe, Mn, Cr, Zr, Ti, Cd, B, Sc, Ce,
V, each intermediate alloy raw material of Re, adjustment temperature are 745-770 DEG C, sampling analysis chemical composition until completely melted, see whether
Meet Composition Control requirement, carries out Composition Control if necessary and adjust to obtain aluminium alloy melt；
(2) it refines：Refining agent is added to refine melt, to eliminate gas in melt, oxidation film and field trash；
(3) it skims and stirs：Aluminium alloy melt is stirred after skimming, and then stands 25-45 minutes, is waited to be cast；
(4) it casts：It is cast using semi-continuous casting method, semi-continuous casting temperature is 730 DEG C~750 DEG C, and casting speed is
40mm/min~60mm/min, cooling water intensity is 0.06MPa~0.12MPa, and electromagnetic induction coil is arranged in crystallizer,
The frequency in magnetic field is 1000~3000Hz, and the magnetic field intensity of crystallizer center is 15~25mT；
(5) Homogenization Treatments：Homogenization Treatments are carried out to ingot casting and rise to 300- first with the heating rate of 100-130 DEG C/h
320 DEG C, 3-4h is kept the temperature, then with the heating rate of 50-70 DEG C/h, rise to 450-480 DEG C, keep the temperature 4-6h, it is then air-cooled to 250-
290 DEG C, 2-3h is kept the temperature, room temperature is then air-cooled to, then with the heating rate of 100-150 DEG C/h, rise to 480-500 DEG C, keeps the temperature 5-
8h is down to 150-180 DEG C with the rate of temperature fall of 140-180 DEG C/h, keeps the temperature 1-2h, water cooling to room temperature, then with 100-150 DEG C/
The heating rate of h rises to 300-330 DEG C, keeps the temperature 1-3h, comes out of the stove and be air-cooled to room temperature；
(6) ingot casting after Homogenization Treatments is subjected to hot extrusion, hot rolling or forging technology as needed, is processed into designated shape
Semi-finished product；
(7) semi-finished product are quenched, aging strengthening model can be obtained aviation alloyed aluminium.
2. aviation alloyed aluminium as described in claim 1, which is characterized in that its component and mass percentage are as follows：
3. aviation alloyed aluminium as described in claim 1, which is characterized in that its component and mass percentage are as follows：
4. aviation alloyed aluminium according to claim 1, it is characterised in that：The fine aluminium ingot, pure magnesium ingot, pure zinc ingot are pure
Degree is all higher than 99.99%.
5. aviation alloyed aluminium according to claim 1, it is characterised in that：Refining carries out in enclosed environment, refines
Time is 5-10min.
6. aviation alloyed aluminium according to claim 1, it is characterised in that：Semi-continuous casting uses crystallizer graphite liner
With tapered, and cooling water hole center line and cavity centerlines are 20-40 °.
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| CN100410406C (en) * | 2006-08-14 | 2008-08-13 | 吉林大学 | High strength high toughness casting aluminum alloy |
| CN101733393A (en) * | 2008-11-04 | 2010-06-16 | 吴江市天龙机械有限公司 | Method for preparing high-performance aluminum alloy accurate die casting |
| CN103114229A (en) * | 2013-02-21 | 2013-05-22 | 东北轻合金有限责任公司 | Aluminum-alloy rivet wire for aerospace and manufacturing method thereof |
| CN106521197B (en) * | 2016-11-16 | 2018-07-17 | 山东南山铝业股份有限公司 | A kind of aviation alloyed aluminium and its production technology |
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