CN107267817B - A kind of high-strength anti-fatigue in-situ nano-strengthened aluminum alloy and its die-casting method - Google Patents
A kind of high-strength anti-fatigue in-situ nano-strengthened aluminum alloy and its die-casting method Download PDFInfo
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- 238000004512 die casting Methods 0.000 title claims abstract description 76
- 238000011065 in-situ storage Methods 0.000 title claims abstract description 34
- 238000000034 method Methods 0.000 title claims abstract description 31
- 230000002929 anti-fatigue Effects 0.000 title claims abstract description 23
- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 16
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 125
- 239000000956 alloy Substances 0.000 claims abstract description 125
- 238000013016 damping Methods 0.000 claims abstract description 24
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 10
- 229910052742 iron Inorganic materials 0.000 claims abstract description 10
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 10
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 9
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 9
- 239000002131 composite material Substances 0.000 claims abstract description 8
- 230000000694 effects Effects 0.000 claims abstract description 8
- 229910052749 magnesium Inorganic materials 0.000 claims abstract description 8
- 229910018084 Al-Fe Inorganic materials 0.000 claims abstract description 7
- 229910018192 Al—Fe Inorganic materials 0.000 claims abstract description 7
- 229910052725 zinc Inorganic materials 0.000 claims abstract description 7
- 239000011159 matrix material Substances 0.000 claims abstract description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 29
- 239000011777 magnesium Substances 0.000 claims description 28
- 230000032683 aging Effects 0.000 claims description 25
- 238000007670 refining Methods 0.000 claims description 24
- 238000003756 stirring Methods 0.000 claims description 18
- 239000000919 ceramic Substances 0.000 claims description 17
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 16
- 238000007872 degassing Methods 0.000 claims description 16
- 229910002804 graphite Inorganic materials 0.000 claims description 16
- 239000010439 graphite Substances 0.000 claims description 16
- 238000002347 injection Methods 0.000 claims description 15
- 239000007924 injection Substances 0.000 claims description 15
- 239000000155 melt Substances 0.000 claims description 15
- 239000013078 crystal Substances 0.000 claims description 11
- 230000002787 reinforcement Effects 0.000 claims description 11
- 229910052691 Erbium Inorganic materials 0.000 claims description 10
- 230000008569 process Effects 0.000 claims description 9
- 239000007789 gas Substances 0.000 claims description 8
- 239000000203 mixture Substances 0.000 claims description 8
- 239000002245 particle Substances 0.000 claims description 8
- 230000006911 nucleation Effects 0.000 claims description 7
- 238000010899 nucleation Methods 0.000 claims description 7
- 238000005728 strengthening Methods 0.000 claims description 7
- 238000004321 preservation Methods 0.000 claims description 6
- 229910052796 boron Inorganic materials 0.000 claims description 5
- 238000006243 chemical reaction Methods 0.000 claims description 5
- 238000011049 filling Methods 0.000 claims description 5
- 239000001257 hydrogen Substances 0.000 claims description 5
- 229910052739 hydrogen Inorganic materials 0.000 claims description 5
- 125000004435 hydrogen atom Chemical class [H]* 0.000 claims description 5
- 239000002893 slag Substances 0.000 claims description 5
- 229910018131 Al-Mn Inorganic materials 0.000 claims description 4
- 229910018461 Al—Mn Inorganic materials 0.000 claims description 4
- 229910018580 Al—Zr Inorganic materials 0.000 claims description 4
- 230000015572 biosynthetic process Effects 0.000 claims description 4
- 239000011261 inert gas Substances 0.000 claims description 4
- 238000003786 synthesis reaction Methods 0.000 claims description 4
- 239000003795 chemical substances by application Substances 0.000 claims description 3
- 239000006185 dispersion Substances 0.000 claims description 3
- 239000000243 solution Substances 0.000 claims description 3
- 239000000126 substance Substances 0.000 claims description 3
- 229910016343 Al2Cu Inorganic materials 0.000 claims description 2
- 229910018176 Al—(Mn, Fe)—Si Inorganic materials 0.000 claims description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 2
- 229910019752 Mg2Si Inorganic materials 0.000 claims description 2
- UYAHIZSMUZPPFV-UHFFFAOYSA-N erbium Chemical compound [Er] UYAHIZSMUZPPFV-UHFFFAOYSA-N 0.000 claims description 2
- 238000005429 filling process Methods 0.000 claims description 2
- 230000008595 infiltration Effects 0.000 claims description 2
- 238000001764 infiltration Methods 0.000 claims description 2
- 239000011572 manganese Substances 0.000 claims description 2
- 230000005012 migration Effects 0.000 claims description 2
- 238000013508 migration Methods 0.000 claims description 2
- 230000009467 reduction Effects 0.000 claims description 2
- 239000007787 solid Substances 0.000 claims description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims 15
- 239000011701 zinc Substances 0.000 claims 9
- 238000001556 precipitation Methods 0.000 claims 6
- 229910052726 zirconium Inorganic materials 0.000 claims 3
- 238000003723 Smelting Methods 0.000 claims 2
- 239000002244 precipitate Substances 0.000 claims 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims 1
- 238000005275 alloying Methods 0.000 claims 1
- 230000005496 eutectics Effects 0.000 claims 1
- 230000002349 favourable effect Effects 0.000 claims 1
- 238000002156 mixing Methods 0.000 claims 1
- 239000002114 nanocomposite Substances 0.000 claims 1
- 239000000843 powder Substances 0.000 claims 1
- 239000000047 product Substances 0.000 claims 1
- 238000007711 solidification Methods 0.000 claims 1
- 230000008023 solidification Effects 0.000 claims 1
- 230000007847 structural defect Effects 0.000 claims 1
- 238000005266 casting Methods 0.000 abstract description 15
- 238000005457 optimization Methods 0.000 abstract description 9
- 229910007948 ZrB2 Inorganic materials 0.000 abstract description 8
- 239000000470 constituent Substances 0.000 abstract description 8
- 230000008859 change Effects 0.000 abstract description 2
- 230000003014 reinforcing effect Effects 0.000 abstract description 2
- 230000035939 shock Effects 0.000 description 19
- 230000008018 melting Effects 0.000 description 9
- 238000002844 melting Methods 0.000 description 7
- 238000013329 compounding Methods 0.000 description 6
- 238000005516 engineering process Methods 0.000 description 6
- 238000004458 analytical method Methods 0.000 description 5
- 238000012669 compression test Methods 0.000 description 5
- 230000004907 flux Effects 0.000 description 5
- 238000004519 manufacturing process Methods 0.000 description 5
- 239000002994 raw material Substances 0.000 description 5
- 238000005070 sampling Methods 0.000 description 5
- 238000002791 soaking Methods 0.000 description 5
- 238000013019 agitation Methods 0.000 description 4
- 206010016256 fatigue Diseases 0.000 description 4
- 239000004411 aluminium Substances 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 239000003921 oil Substances 0.000 description 3
- 238000010792 warming Methods 0.000 description 3
- 230000000052 comparative effect Effects 0.000 description 2
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 2
- 229910052737 gold Inorganic materials 0.000 description 2
- 239000010931 gold Substances 0.000 description 2
- 238000010309 melting process Methods 0.000 description 2
- 230000008520 organization Effects 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 239000006104 solid solution Substances 0.000 description 2
- 229910000863 Ferronickel Inorganic materials 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- HGHPQUIZVKPZEU-UHFFFAOYSA-N boranylidynezirconium Chemical compound [B].[Zr] HGHPQUIZVKPZEU-UHFFFAOYSA-N 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 229910001325 element alloy Inorganic materials 0.000 description 1
- 238000007373 indentation Methods 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 229910001338 liquidmetal Inorganic materials 0.000 description 1
- 239000010705 motor oil Substances 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 230000035882 stress Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Classifications
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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
- B22D21/00—Casting non-ferrous metals or metallic compounds so far as their metallurgical properties are of importance for the casting procedure; Selection of compositions therefor
- B22D21/002—Castings of light metals
- B22D21/007—Castings of light metals with low melting point, e.g. Al 659 degrees C, Mg 650 degrees C
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D17/00—Pressure die casting or injection die casting, i.e. casting in which the metal is forced into a mould under high pressure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D21/00—Casting non-ferrous metals or metallic compounds so far as their metallurgical properties are of importance for the casting procedure; Selection of compositions therefor
- B22D21/02—Casting exceedingly oxidisable non-ferrous metals, e.g. in inert atmosphere
- B22D21/04—Casting aluminium or magnesium
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F1/00—Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
- B22F1/07—Metallic powder characterised by particles having a nanoscale microstructure
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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
- C22C1/04—Making non-ferrous alloys by powder metallurgy
- C22C1/0408—Light metal alloys
- C22C1/0416—Aluminium-based 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
- C22C1/10—Alloys containing non-metals
- C22C1/1036—Alloys containing non-metals starting from a melt
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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
- C22C1/10—Alloys containing non-metals
- C22C1/1036—Alloys containing non-metals starting from a melt
- C22C1/1047—Alloys containing non-metals starting from a melt by mixing and casting liquid metal matrix composites
- C22C1/1052—Alloys containing non-metals starting from a melt by mixing and casting liquid metal matrix composites by mixing and casting metal matrix composites with reaction
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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
- C22C1/10—Alloys containing non-metals
- C22C1/1036—Alloys containing non-metals starting from a melt
- C22C1/1068—Making hard metals based on borides, carbides, nitrides, oxides or silicides
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/10—Alloys containing non-metals
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- C22C1/1073—Infiltration or casting under mechanical pressure, e.g. squeeze casting
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- C22C32/00—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ
- C22C32/0047—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents
- C22C32/0073—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents only borides
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Abstract
The present invention relates to aluminum matrix composites, refer in particular to the high-strength antifatigue in-situ nano reinforced aluminium alloy of one kind and its pressure casting method.By in-situ nano reinforcing and alloy elements regulation, and the non-linear high pressure die casting technique of optimization is combined to obtain die casting.By in-situ nano ZrB2Reinforcement and nanometer Al3Scale effect, interfacial effect, the heterogeneous forming core effect of Er precipitated phase, significantly improve intensity, anti-fatigue performance and the damping capacity of alloy;At the same time, Mg, Zn and Fe constituent content are improved, and introduces Mn and Ni element, while improving hardening constituent content, obtaining high-intensitive, refine the harmful coarse precipitated phase such as Al-Fe effectively and circle change, and ensure the good die casting performance of alloy;Thus the characteristics of showing high-strength plasticity, high antifatigue, high damping properties and good die casting performance using alloy of the present invention and its pressure casting method component produced.
Description
Technical field
The present invention relates to aluminum matrix composites, refer in particular to the high-strength antifatigue in-situ nano reinforced aluminium alloy of one kind and its die casting side
Method.
Background technique
With the development of economy and society, automobile has progressed into common people house, becomes the indispensability of people's trip life
Tool.China Association for Automobile Manufacturers's statistics display, Chinese Brand passenger car sells 1052.86 ten thousand altogether within 2016, increases by a year-on-year basis
20.50%.Heart of the engine as automobile, high efficiency, low cost and the high-performance of critical component production have become major
The core of automobile vendor's promotion product competitiveness.
High-pressure casting is gradually replaced with its high production efficiency, good economy performance, the advantage that casting accuracy is high, surface smoothness is good
For high-cost low pressure, gravitational casting, become the automobile engines such as aluminium engine cylinder body, oil pump case, cushioning members key
The main manufacture of components.However, high-pressure casting is since liquid Metal Filling type chamber speed is high, fluidised form is unstable, is produced
Casting be easy to generate stomata, cannot be heat-treated, leading to precipitated phase in casting is usually in coarse needle-shaped or laminated structure, reinforcing
Effect is unobvious, is easy to generate stress concentration, keeps its strong plasticity, anti-fatigue performance relatively low.To make high pressure die castings be difficult to
Full substitution low pressure casting, gravitational casting part, are especially dfficult to apply to middle-to-high end car engine with high performance requirements.
Summary of the invention
The object of the invention is that inclined for the existing die casting strong plasticity of typical aluminium alloy AlSi9Cu3, anti-fatigue performance
It is low, it is not able to satisfy the deficiency of high-performance enginer component high-intensitive, antifatigue, high-damping technical requirements to it especially, leads to
It crosses alloy elements regulation and in-situ nano is strengthened, and combine the non-linear pressure injection casting processes of optimization, improving alloy precipitated phase
Content, circle are changed and are refined simultaneously, realize that transgranular and crystal boundary in-situ nano ceramic phase reinforcement is strengthened, significantly improve die cast product
Strong plasticity, fatigue resistance and damping capacity.
Using the automobile engine shock bracket of the technology of the present invention production and the tensile strength of shell up to 352MPa, bend
It takes intensity and reaches 285MPa, elongation percentage is up to 10.6%.Final products carry out durability test through Special-purpose bench, minimum circulation time
Number has reached 1,000,000 times, much higher than 500,000 times of customer requirement, has reached germany volkswagen (shock bracket) DIN EN1706-
1998 standards and Japan's Mazda (shock-absorbing casing) MES MM 621-ADC12 standard, while having also exceeded using low pressure casting
Shock bracket performance (the tensile strength 300MPa, yield strength 210MPa, elongation percentage of (after solid solution+aging strengthening model) production
7.5%).
A kind of die casting in-situ nano reinforced aluminium alloy and its die casting that high-strength antifatigue and damping capacity is good of the invention
Method is strengthened by alloy elements regulation and in-situ nano, and the non-linear high pressure die casting of optimization is combined to obtain transgranular and crystal boundary
Include a large amount of and finely dispersed nanometer ZrB2Ceramic phase reinforcement, transgranular includes nanometer Al3Er precipitated phase, including common reciever,
Mg2Si phase, alloy precipitated phase including Al2Cu phase and phase containing Fe is tiny, circle die casting.By nanometer reinforcement and nanometer
The Al that the Er element of the dispersion-strengtherning of precipitated phase, interfacial damping effect and low solid solubility is generated in alloy melt3Er phase crystal grain
Refining effect significantly improves the strong plasticity of alloy components, antifatigue and damping capacity;At the same time, Mg, Zn and Fe constituent content
Raising and Mn and Ni element introduce, while ensureing good die casting performance, improving alloy strengthening phase content, make Al-Fe
Equal alloy strengthenings mutually change by effectively refinement and circle;To make alloy of the present invention component produced show high-strength plasticity, highly resistance
The characteristics of fatigability and excellent damping performance.
Preparation method of the invention the following steps are included:
(1) AlSi9Cu3 alloy melting to 750-780 DEG C and alloy melting: is kept the temperature into 10min.The AlSi9Cu3 is closed
Gold is commercial alloy, the element mass percent of specific chemical composition are as follows: Si 8.0~11.0, Cu 2.0~3.5, Zn 1.0
~1.5, Mg 0.3~0.5, Fe≤0.8, Mn 0.1~0.5, surplus Al.
(2) fabricated in situ nanometer ZrB2Nano ceramics reinforcement: it is molten that step (1) is added in Al-Zr and Al-B intermediate alloy
It refines and in the melt that keeps the temperature and is brought rapidly up to 840-860 DEG C, while using graphite stirring rotator agitation melt to promote alloy
Be sufficiently mixed, soaking time 10-15min keeps Zr in alloy and B element in situ anti-under the driving force that free energy reduces
A nanometer ZrB should be synthesized2Then ceramic phase reinforcement is cooled to 730-750 DEG C and keeps the temperature.So that zirconium boron element in step (2) alloy
Mass percent reach Zr:3.0-5.0, B:0.5-1.0.
(3) Er and Ni element is introduced, the content of Fe and Mn element in alloy is adjusted and refines degasification: by Al-Er, Al-Fe
Be added in step (2) compounding flux obtained with Al-Mn intermediate alloy and pure Ni, and use graphite stirring rotator to stir with
Promote being sufficiently mixed for alloy, the insulated and stirred time is 10-15min;Then the powdered composite refining by granularity less than 500 μm
Agent is blown into melt with inert gas by the hollow channel of graphite rotator, carries out refining degasification to melt, to remove alloy height
The hydrogen dissolved in the slag inclusion and melt generated in warm melting and reaction process, refining temperature are 730-750 DEG C, refine soaking time
For 25-30min.Finally erbium ferro-nickel element content in step (3) alloy is made to reach Er:0.1-0.15, Fe:1.0~1.5, Mn:
0.5~1.0, Ni 0.5~1.0.
(4) Mg is adjusted, the content of Zn element: the melt that step (3) obtain is cooled to 660-700 DEG C and is kept the temperature, then
By pure Mg and pure Zn using in the melt after bell jar indentation refining degasification, start graphite stirring rotator, and mix slowly, heat preservation is stirred
> 15min is mixed the time, so that Mg, Zn dissolve in alloy and avoid melt air-breathing, and reaches magnesium Zn-ef ficiency content in step (4) alloy
To Mg:0.5~1.0, Zn:1.5~2.5.
(5) non-linear high pressure die casting: in the insulated bag for the compounding flux merging die casting machine that step (4) are obtained, use is excellent
The non-linear die-casting process changed carries out die casting and obtains nano crystalline compounding die casting, and wherein injection speed is parabolic from small to large
Wire type injection slowly fills type 2.5-3m/s early period to realize, final instants high speed fills the non-linear of type and fills type (maximum injection speed
Reach 40-50m/s, die casting pressure reaches 100-150MPa).
(6) ageing treatment: the die casting that step (5) are obtained carries out ageing treatment (natrual ageing or artificial aging), with
Obtain the good in-situ nano reinforced aluminium alloy die casting of high-strength antifatigue and damping capacity.
Al-Zr, Al-B, Al-Er, Al-Fe and Al-Mn intermediate alloy, during preferred alloy constituent content is high
Between alloy, such as Al-10Zr, Al-10B, Al-20Er, Al-20Fe and Al-10Mn.
The fabricated in situ nanometer ZrB2Nano ceramics reinforcement refers to and utilizes ZrB in the multi-element alloy system2Ji
Buss free energy is low, and Zr has thermodynamics-kinetic characteristics of low solubility and low thermal diffusivity coefficient in Al, in the alloy
Introduce Zr, after B element, in the melt fabricated in situ nanoscale ZrB2Ceramic particle, having a size of 20-80nm, content is to close
The 2-6wt.% of golden amount, synthesis temperature are 840-860 DEG C.To in alloy melt process of setting: on the one hand, in-situ nano
ZrB2Ceramic particle can be used as the nucleation rate that heterogeneous forming core core improves alloy, refine crystal grain, and finally comprising being scattered in alloy
Intra-die significantly improves intensity, the anti-fatigue performance of alloy;On the other hand, do not become the nanometer ZrB of forming core core2Ceramics
Particle can be scattered in crystal boundary during crystal grain is grown up, and effectively pin crystal boundary and can hinder the migration of crystal boundary, it is strong to improve alloy
While spending, performance interfacial damping effect is maximized, improves the damping capacity of alloy.
Introducing Er and the Ni element adjusts the content of Fe and Mn element in alloy and refines degasification, refers in alloy
The Er of the 0.1-0.15wt.% of middle introducing, it is molten in alloy on the one hand by solubility (0.1wt.%) Er low in aluminium solution
Al is precipitated in body3The heterogeneous forming core core of Er improves the nucleation rate of aluminium, on the other hand refining alloy is solid-solution in Er element in alloy,
Can in alloy aging it is transgranular be precipitated it is tiny and with the good L1 of aluminum substrate Lattice Matching2Type nanometer Al3Er precipitated phase, significantly
Improve the aging strength and anti-fatigue performance of alloy pressuring casting;The purpose for increasing the content of Fe element in the alloy is to improve alloy
Middle Fe precipitated phase content further increases the anti-stick mould performance of alloy, alloy precipitated phase is avoided to contain while improving alloy strength
It measures and increases, expands demoulding hardly possible and considerable sticking problems caused by system's reduction, introduce Ni element and the purpose for improving Mn constituent content is logical
β-Fe the phase transition of gill shape in Ni, Mn and alloy is crossed into blocky or Chinese character shape α-Al (Mn, Fe) Si and α-Al (Ni, Fe) Si
Phase avoids the raising of Fe content from generating a large amount of acicular beta-Fe and mutually drops low-alloyed plasticity and toughness.
The content of adjustment Mg, the Zn element, is the content for further increasing precipitated phase in alloy, strong to improve alloy
Degree, anti-fatigue performance, and by the damping capacity of increased phase boundary raising alloy.
The non-linear high pressure die casting technique refers to the novel die casting machine controlled using die-cast rotor housing speed-programmable,
And optimize its acquisition non-linear high pressure die casting technique, with from avoid in melt cavity filling process turbulent flow and volume gas, be conducive to type chamber
The discharge of middle gas and the infiltration and dispersion for promoting nanometer reinforcement under the instantaneous high speed and high pressure full of type chamber, to obtain tissue
Defect is few, function admirable die-cast product.Wherein injection speed is parabolic injection from small to large, to realize that early period is slow
Fill type 2.5-3m/s, final instants high speed fills the non-linear of type and fills type (maximum injection speed reaches 40-50m/s, and die casting pressure reaches
To 100-150MPa).
Detailed description of the invention
Fig. 1 (a) is routine AlSi9Cu3 die casting metallographic structure figure, is (b) prepared by the present invention high-strength antifatigue and resistance
The good in-situ nano reinforced aluminium alloy shock bracket die casting metallographic structure figure of damping properties, can be seen that from two metallographic structure figures
It is disappeared using precipitated phase needle-shaped in die casting prepared by this patent, is converted into the circle precipitated phase of graininess or short-movie shape, mentions
The high disperse degree of precipitated phase, conducive to the raising of workpiece strong plasticity and fatigue behaviour.
The good in-situ nano reinforced aluminium alloy shock bracket die casting of Fig. 2 high-strength antifatigue and damping capacity prepared by the present invention
Part TEM organization chart, it can be seen from the figure that in-situ nano existing for transgranular and crystal boundary using die casting prepared by this patent
ZrB2Ceramic enhancement phase and more fine uniform nanometer Al3Er nanometer precipitated phase is conducive to the strong plasticity of workpiece, anti-fatigue performance and resistance
The comprehensive of damping properties is improved.
Specific embodiment
Further describe below in conjunction with attached drawing to embodiment of the present invention: following embodiment is being with technical solution of the present invention
Under the premise of implemented, the detailed implementation method and specific operation process are given, but protection scope of the present invention is not limited to
Following embodiments.
Embodiment 1
With Al-10Zr, Al-10B, Al-20Er, Al-20Fe, Al-10Mn intermediate alloy and pure Ni, pure Mg, pure Zn, and
AlSi9Cu3 is raw material, prepares automobile engine shock bracket using the non-linear high pressure die casting technology of optimization.
The 500Kg commercialization AlSi9Cu3 alloy (760 DEG C) of melting is transferred in moderate soak furnace, then by Al-10Zr and
Al-10B intermediate alloy is added in holding furnace and is warming up to 850 DEG C, while using graphite stirring rotator agitation melt to promote to close
Gold is sufficiently mixed, then alloy is cooled to 750 DEG C and kept the temperature by soaking time 15min;By Al-20Er, Al-20Fe and
Al-10Mn and pure Ni is added in melt, and the powdered composite refiner after stirring heat preservation 15min by partial size less than 500 μm is used
Inert gas is blown into melt by the hollow channel of graphite rotator, carries out refining degasification to melt, molten to remove alloy high-temp
The hydrogen dissolved in the slag inclusion and melt generated in refining and reaction process, refining time 30min, temperature are maintained at 750 DEG C, refining
It is cooled to 680 DEG C after degasification and pure Mg and pure Zn bell jar is pressed into the melt after refining degasification, starting graphite stirring
Rotor, and mix slowly, insulated and stirred time 18min makes the alloy ultimate constituent reach Si 9.5, Cu 3, Zr 3.5, B
0.75, Zn 1.5, Mg 0.8, Fe 1.3, Mn 1.0, Ni 0.7, Er 0.12, surplus Al, finally by the compounding flux of acquisition
Shock bracket is prepared with the non-linear high pressure die casting technique of optimization, mid-early stage is that 3m/s slowly fills type, to realize that advection fills type
And be conducive to gas in mold cavity and be smoothly discharged, it is full of the moment of (riser underfill) to type chamber, improves injection speed extremely
40m/s, and pressure is being kept to obtain die casting shock bracket to 100MPa, dwell time 15s.
The die-casting blank of dead head and overlap will be cut off, is put into heat-treatment furnace and carries out artificial aging, the 300 of aging temp
DEG C, aging time is 8 hours.
Sampling analysis shows that the hardness of shock bracket is greater than 97HBS, and tensile strength has reached 352MPa, and yield strength reaches
285MPa is arrived, elongation percentage 10.6%, the repeated tension and compression test service life is greater than 2 × 10 under 7.6kN load6It is secondary, final products
Durability test is carried out through Special-purpose bench, minimum cycle-index has reached 1,000,000 times, is much higher than customer requirement 500,000 times.Product
Reach germany volkswagen (shock bracket) DIN EN1706-1998 standard and Japan Mazda (shock-absorbing casing) MES MM 621-
ADC12 standard.It, can be with from figure as shown in Figure 1 b for using the metallographic structure figure of shock bracket prepared by the present embodiment technique
Find out and compare routine AlSi9Cu3 die casting, the needle-shaped precipitated phase in die casting prepared by this patent disappears, and is converted into particle
The circle of shape or short-movie shape precipitated phase, improves the disperse degree of precipitated phase, conducive to the raising of workpiece strong plasticity and fatigue behaviour.
Fig. 2 is shock bracket die casting TEM organization chart prepared by the present embodiment technique, it can be seen from the figure that made using this patent
There are a large amount of in-situ nano ZrB for the transgranular and crystal boundary of standby die casting2Ceramic enhancement phase and more fine uniform nanometer Al3Er
Nanometer precipitated phase, comprehensive conducive to the strong plasticity of workpiece, anti-fatigue performance and damping capacity are improved.
Embodiment 2
With Al-10Zr, Al-5B, Al-10Er, Al-10Fe, Al-10Mn intermediate alloy and pure Ni, pure Mg, pure Zn, and
AlSi9Cu3 is raw material, prepares automobile engine shock-absorbing casing (shell structure using the non-linear high pressure die casting technology of optimization
Complexity fills type and discharge gas difficulty is high, usually reduces Mg content, improves die casting pressure, improves die casting performance and yield rate).
The 500Kg commercialization AlSi9Cu3 alloy (750 DEG C) of melting is transferred in moderate soak furnace, then by Al-10Zr and
Al-5B intermediate alloy is added in holding furnace and is warming up to 840 DEG C, while using graphite stirring rotator agitation melt to promote alloy
Be sufficiently mixed, then alloy is cooled to 740 DEG C and kept the temperature by soaking time 10min;By Al-10Er, Al-10Fe and Al-
10Mn and pure Ni is added in melt, the powdered composite refiner inertia after stirring heat preservation 10min by partial size less than 500 μm
Gas is blown into melt by the hollow channel of graphite rotator, carries out refining degasification to melt, with remove alloy high-temp melting and
The hydrogen dissolved in the slag inclusion and melt generated in reaction process, refining time 25min, temperature are maintained at 740 DEG C, refine degasification
After be cooled to 660 DEG C and by pure Mg and pure Zn with bell jar be pressed into refining degasification after melt in, start graphite stirring rotator,
And mix slowly, insulated and stirred time 20min makes the alloy ultimate constituent reach Si 11, Cu 3.5, Zr 5.0, B 1.0, Zn
2.0, Mg 0.5, Fe 1.5, Mn 1.0, Ni 0.5, Er 0.15, surplus Al, finally by the compounding flux of acquisition to optimize
Non-linear high pressure die casting technique prepares shock-absorbing casing, and mid-early stage is that 5m/s slowly fills type, to realize that advection fills type and conducive to mould
Gas is smoothly discharged in tool type chamber, and the moment of (riser underfill) is full of to type chamber, improves injection speed to 50m/s, and
It keeps pressure to 150MPa, time 15s, obtains die casting shock-absorbing casing.
The die-casting blank of dead head and overlap will be cut off, is put into heat-treatment furnace and carries out artificial aging, the 250 of aging temp
DEG C, aging time is 10 hours.
Sampling analysis shows that the hardness of shock bracket is greater than 92HBS, and tensile strength has reached 315MPa, and yield strength reaches
243MPa is arrived, elongation percentage 8.9%, the repeated tension and compression test service life is greater than 1.5 × 10 under 7.6kN load6It is secondary, final products
Durability test is carried out through Special-purpose bench, minimum cycle-index has reached 1,000,000 times, is much higher than customer requirement 500,000 times.
Embodiment 3
With Al-10Zr, Al-5B, Al-20Er, Al-20Fe, Al-5Mn intermediate alloy and pure NIi, pure Mg, pure Zn, and
AlSi9Cu3 is raw material, prepares automobile engine oil pump case using the non-linear high pressure die casting technology of optimization.
The 500Kg commercialization AlSi9Cu3 alloy (780 DEG C) of melting is transferred in moderate soak furnace, then by Al-10Zr and
Al-5B intermediate alloy is added in holding furnace and is warming up to 860 DEG C, while using graphite stirring rotator agitation melt to promote alloy
Be sufficiently mixed, then alloy is cooled to 750 DEG C and kept the temperature by soaking time 15min;By Al-20Er, Al-20Fe and Al-
50Mn and pure Ni is added in melt, and ultra-fine powdered refining agent inert gas is passed through graphite after stirring heat preservation 10min
The hollow channel of rotor is blown into melt, is carried out refining degasification to melt, is produced with removing in alloy high-temp melting and reaction process
The hydrogen dissolved in raw slag inclusion and melt, refining time 30min, temperature are maintained at 750 DEG C, are cooled to after refining degasification
680 DEG C and pure Mg and pure Zn bell jar is pressed into the melt after refining degasification, starts graphite stirring rotator, and mix slowly,
Insulated and stirred time 20min makes the alloy ultimate constituent reach Si 11, Cu 2.5, Zr 5.0, B 1.0, Zn 2.5, Mg 1.0,
Fe 1.5, Mn 1.0, Ni 1.0, Er 0.1, surplus Al, the finally non-linear high pressure pressure by the compounding flux of acquisition to optimize
Casting process prepares oil pump case, and mid-early stage is that 4m/s slowly fills type, to realize that advection fills type and conducive to gas in mold cavity
Be smoothly discharged, the moment of (riser underfill) is full of to type chamber, improves injection speed to 50m/s, and is keeping pressure extremely
130MPa, time 15s obtain die casting oil pump case.
The die-casting blank of dead head and overlap will be cut off, is put into heat-treatment furnace and carries out artificial aging, the 220 of aging temp
DEG C, aging time is 15 hours.
Sampling analysis shows that the hardness of shock bracket is greater than 93HBS, and tensile strength has reached 330MPa, and yield strength reaches
250MPa is arrived, elongation percentage 7.8%, the repeated tension and compression test service life is greater than 1.2 × 10 under 7.6kN load6It is secondary, final products
Durability test is carried out through Special-purpose bench, minimum cycle-index has reached 1,000,000 times, is much higher than customer requirement 500,000 times.
Compare embodiment
Comparative example 1
Using AlSi9Cu3 alloy as raw material, automobile engine damping is prepared using the non-linear high pressure die casting technology of optimization
Bracket.
By (700 DEG C) of 500Kg commercialization AlSi9Cu3 alloy of the melting non-linear high pressure die casting technology preparations using optimization
Automobile engine shock bracket, and to excision dead head and overlap die-casting blank carry out artificial aging, the 300 of aging temp
DEG C, aging time is 8 hours.
Sampling analysis shows that the hardness of shock bracket is greater than 82HBS, and tensile strength has reached 285MPa, and yield strength reaches
193MPa is arrived, elongation percentage 6.4%, the repeated tension and compression test service life is greater than 1 × 10 under 7.6kN load6It is secondary.
Comparative example 2
With Al-10Zr, Al-10B, Al-20Er, Al-20Fe, Al-10Mn intermediate alloy and pure Ni, pure Mg, pure Zn, and
AlSi9Cu3 is raw material, prepares automobile engine shock bracket using conventional die-casting technique.
Fabricated in situ nanometer ZrB2Reinforcement and alloy elements regulation are same as Example 1, and will obtain temperature is 680 DEG C,
Ingredient be Si 9.5, Cu 3, Zr 3.5, B 0.75, Zn 1.5, Mg 0.8, Fe 1.3, Mn 1.0, Ni 0.7, Er 0.12, it is remaining
Amount is the alloy melt of Al, obtains die casting shock bracket using conventional die-casting process.
Ageing treatment is carried out to die casting using the identical aging technique of embodiment 1.
Sampling analysis shows that the hardness of shock bracket is greater than 93HBS, and tensile strength has reached 335MPa, and yield strength reaches
263MPa is arrived, elongation percentage 9.2%, the repeated tension and compression test service life is greater than 1.8 × 10 under 7.6kN load6It is secondary.
Claims (6)
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PCT/CN2018/080114 WO2018214631A1 (en) | 2017-05-25 | 2018-03-23 | High-strength anti-fatigue in-situ nano strengthening aluminium alloy for vibration-damping part of automobile engine, and high-density die-casting method therefor |
CH00580/19A CH714442B1 (en) | 2017-05-25 | 2018-03-23 | Aluminum alloy for a vibration damping component of an automobile engine and die casting process. |
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CN108342606B (en) * | 2018-01-19 | 2020-01-24 | 江苏大学 | A method for improving the microstructure and properties of in-situ aluminum matrix composites with mixed rare earths |
CN108672702A (en) * | 2018-05-21 | 2018-10-19 | 宁波市奇强精密冲件有限公司 | Damper knuckle support |
CN111074113B (en) * | 2020-01-02 | 2021-12-24 | 苏州先准电子科技有限公司 | Production process for in-situ generation of zirconium boride particle reinforced aluminum-silicon-based composite material |
CN111647785A (en) * | 2020-06-17 | 2020-09-11 | 帅翼驰新材料集团有限公司 | High-strength die-casting aluminum alloy and preparation method thereof |
CN114438376A (en) * | 2022-02-17 | 2022-05-06 | 江西理工大学 | A kind of aluminum-cerium-erbium heat-resistant cast aluminum alloy and preparation method thereof |
CN114959372B (en) * | 2022-03-08 | 2023-06-27 | 山东金马汽车装备科技有限公司 | Aluminum-based composite hub and manufacturing method thereof |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104451236A (en) * | 2014-11-07 | 2015-03-25 | 江苏大学 | A kind of in-situ preparation method of nano ZrB2 particle reinforced aluminum matrix composite |
CN104874772A (en) * | 2015-05-20 | 2015-09-02 | 柳州市百田机械有限公司 | Preparation method of highly dense pressure casting aluminum alloy |
CN105256185A (en) * | 2015-11-11 | 2016-01-20 | 天津爱田汽车部件有限公司 | Cast aluminum alloy high in thermal conductivity |
CN105861887A (en) * | 2016-04-01 | 2016-08-17 | 江苏大学 | Anti-fatigue in-situ aluminum-based composite for heavy-load hubs and preparation method thereof |
CN106282685A (en) * | 2016-08-31 | 2017-01-04 | 中车戚墅堰机车车辆工艺研究所有限公司 | A kind of high strength cast aluminum alloys and preparation method thereof |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2001252754A (en) * | 2000-03-09 | 2001-09-18 | Hitachi Metals Ltd | Aluminum wheel and its manufacturing method |
CN107267817B (en) * | 2017-05-25 | 2019-04-19 | 江苏大学 | A kind of high-strength anti-fatigue in-situ nano-strengthened aluminum alloy and its die-casting method |
-
2017
- 2017-05-25 CN CN201710376448.7A patent/CN107267817B/en active Active
-
2018
- 2018-03-23 CH CH00580/19A patent/CH714442B1/en unknown
- 2018-03-23 WO PCT/CN2018/080114 patent/WO2018214631A1/en active Application Filing
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104451236A (en) * | 2014-11-07 | 2015-03-25 | 江苏大学 | A kind of in-situ preparation method of nano ZrB2 particle reinforced aluminum matrix composite |
CN104874772A (en) * | 2015-05-20 | 2015-09-02 | 柳州市百田机械有限公司 | Preparation method of highly dense pressure casting aluminum alloy |
CN105256185A (en) * | 2015-11-11 | 2016-01-20 | 天津爱田汽车部件有限公司 | Cast aluminum alloy high in thermal conductivity |
CN105861887A (en) * | 2016-04-01 | 2016-08-17 | 江苏大学 | Anti-fatigue in-situ aluminum-based composite for heavy-load hubs and preparation method thereof |
CN106282685A (en) * | 2016-08-31 | 2017-01-04 | 中车戚墅堰机车车辆工艺研究所有限公司 | A kind of high strength cast aluminum alloys and preparation method thereof |
Non-Patent Citations (2)
Title |
---|
"Er、Zr、B对耐热导电铝合金组织和性能的影响";侯雅尘 等;《特种铸造及有色合金》;20170520;第37卷(第5期);第550-553页 |
"离合器壳体压铸工艺优化——瑞士布勒H-1100B压铸机调试与应用";胡济川;《特种铸造及有色合金》;19940620(第3期);第27页 |
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