CN114645180B - Double-phase reinforced aluminum alloy and preparation method thereof - Google Patents
Double-phase reinforced aluminum alloy and preparation method thereof Download PDFInfo
- Publication number
- CN114645180B CN114645180B CN202210153260.7A CN202210153260A CN114645180B CN 114645180 B CN114645180 B CN 114645180B CN 202210153260 A CN202210153260 A CN 202210153260A CN 114645180 B CN114645180 B CN 114645180B
- Authority
- CN
- China
- Prior art keywords
- phase
- aluminum alloy
- reinforced aluminum
- entropy alloy
- strengthening
- 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.)
- Active
Links
- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 59
- 238000002360 preparation method Methods 0.000 title claims abstract description 13
- 239000000956 alloy Substances 0.000 claims abstract description 42
- 239000000843 powder Substances 0.000 claims abstract description 42
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 40
- 238000005728 strengthening Methods 0.000 claims abstract description 31
- 239000000919 ceramic Substances 0.000 claims abstract description 28
- 239000002245 particle Substances 0.000 claims abstract description 23
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 20
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 18
- 239000011159 matrix material Substances 0.000 claims abstract description 17
- 229910018072 Al 2 O 3 Inorganic materials 0.000 claims abstract description 14
- 238000010438 heat treatment Methods 0.000 claims abstract description 12
- 238000002156 mixing Methods 0.000 claims abstract description 6
- 238000000498 ball milling Methods 0.000 claims description 24
- 239000000463 material Substances 0.000 claims description 20
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 18
- 230000003014 reinforcing effect Effects 0.000 claims description 11
- 238000005245 sintering Methods 0.000 claims description 11
- 238000000034 method Methods 0.000 claims description 10
- 229910052786 argon Inorganic materials 0.000 claims description 9
- 230000003068 static effect Effects 0.000 claims description 9
- 238000001035 drying Methods 0.000 claims description 8
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 6
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 6
- 229910000831 Steel Inorganic materials 0.000 claims description 6
- 238000000227 grinding Methods 0.000 claims description 6
- 238000005551 mechanical alloying Methods 0.000 claims description 6
- 239000010959 steel Substances 0.000 claims description 6
- 238000009768 microwave sintering Methods 0.000 claims description 4
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 3
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 3
- 229910052804 chromium Inorganic materials 0.000 claims description 3
- 239000011651 chromium Substances 0.000 claims description 3
- 229910017052 cobalt Inorganic materials 0.000 claims description 3
- 239000010941 cobalt Substances 0.000 claims description 3
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 3
- 238000001816 cooling Methods 0.000 claims description 3
- 229910052742 iron Inorganic materials 0.000 claims description 3
- 229910052748 manganese Inorganic materials 0.000 claims description 3
- 239000011572 manganese Substances 0.000 claims description 3
- 229910052759 nickel Inorganic materials 0.000 claims description 3
- 239000012798 spherical particle Substances 0.000 claims description 3
- 238000001291 vacuum drying Methods 0.000 claims description 3
- 238000005303 weighing Methods 0.000 claims description 3
- 238000005275 alloying Methods 0.000 claims description 2
- 239000007789 gas Substances 0.000 claims description 2
- 230000001788 irregular Effects 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 claims 1
- 239000002131 composite material Substances 0.000 abstract description 18
- 230000002787 reinforcement Effects 0.000 abstract description 8
- 230000000694 effects Effects 0.000 abstract description 4
- 239000006185 dispersion Substances 0.000 abstract description 3
- 230000002195 synergetic effect Effects 0.000 abstract description 3
- 238000003723 Smelting Methods 0.000 abstract description 2
- 230000007547 defect Effects 0.000 abstract description 2
- 238000009826 distribution Methods 0.000 abstract description 2
- 238000000713 high-energy ball milling Methods 0.000 abstract description 2
- 230000006872 improvement Effects 0.000 abstract description 2
- 239000007769 metal material Substances 0.000 abstract description 2
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 abstract description 2
- 239000013078 crystal Substances 0.000 abstract 2
- 238000009694 cold isostatic pressing Methods 0.000 abstract 1
- 230000001360 synchronised effect Effects 0.000 abstract 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N Alumina Chemical compound [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 6
- 239000010935 stainless steel Substances 0.000 description 6
- 229910001220 stainless steel Inorganic materials 0.000 description 6
- AFCARXCZXQIEQB-UHFFFAOYSA-N N-[3-oxo-3-(2,4,6,7-tetrahydrotriazolo[4,5-c]pyridin-5-yl)propyl]-2-[[3-(trifluoromethoxy)phenyl]methylamino]pyrimidine-5-carboxamide Chemical compound O=C(CCNC(=O)C=1C=NC(=NC=1)NCC1=CC(=CC=C1)OC(F)(F)F)N1CC2=C(CC1)NN=N2 AFCARXCZXQIEQB-UHFFFAOYSA-N 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 238000011160 research Methods 0.000 description 3
- 238000001878 scanning electron micrograph Methods 0.000 description 3
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 238000011049 filling Methods 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 239000011812 mixed powder Substances 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- LDXJRKWFNNFDSA-UHFFFAOYSA-N 2-(2,4,6,7-tetrahydrotriazolo[4,5-c]pyridin-5-yl)-1-[4-[2-[[3-(trifluoromethoxy)phenyl]methylamino]pyrimidin-5-yl]piperazin-1-yl]ethanone Chemical compound C1CN(CC2=NNN=C21)CC(=O)N3CCN(CC3)C4=CN=C(N=C4)NCC5=CC(=CC=C5)OC(F)(F)F LDXJRKWFNNFDSA-UHFFFAOYSA-N 0.000 description 1
- YLZOPXRUQYQQID-UHFFFAOYSA-N 3-(2,4,6,7-tetrahydrotriazolo[4,5-c]pyridin-5-yl)-1-[4-[2-[[3-(trifluoromethoxy)phenyl]methylamino]pyrimidin-5-yl]piperazin-1-yl]propan-1-one Chemical compound N1N=NC=2CN(CCC=21)CCC(=O)N1CCN(CC1)C=1C=NC(=NC=1)NCC1=CC(=CC=C1)OC(F)(F)F YLZOPXRUQYQQID-UHFFFAOYSA-N 0.000 description 1
- DEXFNLNNUZKHNO-UHFFFAOYSA-N 6-[3-[4-[2-(2,3-dihydro-1H-inden-2-ylamino)pyrimidin-5-yl]piperidin-1-yl]-3-oxopropyl]-3H-1,3-benzoxazol-2-one Chemical compound C1C(CC2=CC=CC=C12)NC1=NC=C(C=N1)C1CCN(CC1)C(CCC1=CC2=C(NC(O2)=O)C=C1)=O DEXFNLNNUZKHNO-UHFFFAOYSA-N 0.000 description 1
- 238000002441 X-ray diffraction Methods 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 229910000905 alloy phase Inorganic materials 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000008188 pellet Substances 0.000 description 1
- 238000011056 performance test Methods 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- 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
- C22C32/001—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 only oxides
- C22C32/0015—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 only oxides with only single oxides as main non-metallic constituents
- C22C32/0036—Matrix based on Al, Mg, Be or alloys thereof
-
- 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
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/10—Sintering only
- B22F3/105—Sintering only by using electric current other than for infrared radiant energy, laser radiation or plasma ; by ultrasonic bonding
-
- 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
- B22F9/00—Making metallic powder or suspensions thereof
- B22F9/02—Making metallic powder or suspensions thereof using physical processes
- B22F9/04—Making metallic powder or suspensions thereof using physical processes starting from solid material, e.g. by crushing, grinding or milling
-
- 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
- C22C1/05—Mixtures of metal powder with non-metallic powder
-
- 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
-
- 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
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/10—Sintering only
- B22F3/105—Sintering only by using electric current other than for infrared radiant energy, laser radiation or plasma ; by ultrasonic bonding
- B22F2003/1054—Sintering only by using electric current other than for infrared radiant energy, laser radiation or plasma ; by ultrasonic bonding by microwave
-
- 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
- B22F9/00—Making metallic powder or suspensions thereof
- B22F9/02—Making metallic powder or suspensions thereof using physical processes
- B22F9/04—Making metallic powder or suspensions thereof using physical processes starting from solid material, e.g. by crushing, grinding or milling
- B22F2009/041—Making metallic powder or suspensions thereof using physical processes starting from solid material, e.g. by crushing, grinding or milling by mechanical alloying, e.g. blending, milling
-
- 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
- B22F9/00—Making metallic powder or suspensions thereof
- B22F9/02—Making metallic powder or suspensions thereof using physical processes
- B22F9/04—Making metallic powder or suspensions thereof using physical processes starting from solid material, e.g. by crushing, grinding or milling
- B22F2009/043—Making metallic powder or suspensions thereof using physical processes starting from solid material, e.g. by crushing, grinding or milling by ball milling
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P10/00—Technologies related to metal processing
- Y02P10/25—Process efficiency
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Manufacturing & Machinery (AREA)
- Powder Metallurgy (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Abstract
The invention discloses a two-phase particle reinforced aluminum alloy and a preparation method thereof, belonging to the field of metal materials. The two-phase particles are respectively FeCoNiCrMn high-entropy alloy strengthening phase and Al 2 O 3 The ceramic strengthening phase particles and the matrix are pure aluminum. The preparation method comprises the steps of preparing high-entropy alloy powder by high-energy ball milling; fully mixing pure aluminum powder, high-entropy alloy powder and aluminum oxide particles, obtaining a green body through cold isostatic pressing, and heating the green body in a microwave smelting furnace to obtain a FeCoNiCrMn high-entropy alloy strengthening phase and Al 2 O 3 An aluminum alloy with ceramic strengthening phase dual-phase strengthening. The advantages of the invention are: the reinforced phase of the double-phase reinforcement reserves the reinforcement characteristics and advantages of a single reinforced phase, has obvious synergistic reinforcement effect, eliminates the cluster defect of a particle phase by virtue of a synergistic mixing effect, and refines crystal grains at the aluminum crystal boundary by virtue of dispersion distribution, thereby realizing the synchronous improvement of the properties such as the hardness, the strength and the plasticity of the composite material, and meeting the application in the fields of aerospace and transportation.
Description
Technical Field
The invention belongs to the field of metal materials, and particularly relates to a two-phase particle reinforced aluminum alloy and a preparation method thereof.
Background
The multiphase composite reinforced aluminum alloy has excellent high-temperature mechanical property, good wear resistance, low thermal expansion coefficient, simple preparation process and low reinforcement cost, and thus becomes the research focus of high-end aluminum materials. The ceramic phase has excellent performances such as high temperature resistance, wear resistance, high strength and hardness, but the ceramic phase has high brittleness, so that the ceramic phase is poor in wettability with a matrix interface, low in interface bonding strength and the like when used as a reinforcement, the hardness and strength of the aluminum material are improved, and the plasticity and toughness of the material are inevitably reduced, so that the application range of the aluminum alloy in high-end fields is limited.
As an innovative alloy system, the high-entropy alloy is an alloy consisting of 5 or more than 5 elements and composed according to an equal molar ratio or an approximately equal molar ratio, and researches of numerous scholars find that the high-entropy alloy has more ideal properties compared with the traditional alloy, such as high toughness, high temperature resistance, good corrosion resistance, good wear resistance and the like, so that the high-entropy alloy is valued in the field of materials science. Researches find that the thermal expansion coefficients of the high-entropy alloy and the aluminum matrix are similar, and the natural interface bonding characteristic between metal and metal is realized, so that the interface wettability and the interface compatibility of the high-entropy alloy and the aluminum matrix are good. The high-entropy alloy is added to cooperate with the hard ceramic particles while the strength and the hardness of the material are not reduced, so that the interface combination between the reinforcement and the matrix can be obviously improved, and the performances of the material, such as plastic toughness, wear resistance, elastic modulus and the like, can be improved.
At present, a dual-phase or multi-phase hybrid reinforced aluminum alloy material is reported, but a high-entropy alloy and ceramic combination is not reported as a composite reinforced phase for preparing a dual-phase reinforced aluminum alloy, so that in order to continuously improve the performance of an aluminum alloy material and expand the high-end application range of the aluminum alloy, a new system and a new method aiming at aluminum alloy reinforcement and performance improvement are necessary to be developed, and a high-strength and high-toughness aluminum alloy with higher performance is prepared, so that the method has important significance in the fields of aerospace, transportation and the like.
Disclosure of Invention
The invention aims to provide an aluminum alloy reinforced by combining a high-entropy alloy reinforcing phase and a ceramic particle reinforcing phase and a preparation method thereof.
The invention is realized by the following technical scheme:
the double-phase reinforced aluminum alloy is characterized in that a reinforcing phase of the double-phase reinforced aluminum alloy is a FeCoNiCrMn high-entropy alloy reinforcing phase and Al 2 O 3 A ceramic strengthening phase, wherein the FeCoNiCrMn high-entropy alloy strengthening phase accounts for 15 percent of the total mass fraction of the dual-phase strengthened aluminum alloy, and Al 2 O 3 The ceramic strengthening phase accounts for 2-8% of the total mass fraction of the two-phase reinforced aluminum alloy, and the matrix of the two-phase reinforced aluminum alloy is aluminum.
Further, the FeCoNiCrMn high-entropy alloy strengthening phase is in a sheet shape in an aluminum matrix, and the Al is 2 O 3 The ceramic reinforcing phase is spherical.
Further, the aluminum alloy has a hardness of 109.3 to 128.5HV, a yield strength of 291.5 to 319.2MPa, and an elongation of 41.2 to 46.7%.
The preparation method of the double-phase reinforced aluminum alloy is characterized by comprising the following steps of:
(1) Preparing materials: weighing 15% and 2% -8% of FeCoNiCrMn high-entropy alloy strengthening phase powder and Al 2 O 3 Ceramic powders, and pure aluminum powders;
(2) Preparing two-phase reinforced aluminum alloy powder: after mixing the weighed powders, mechanically alloying the powders by adopting a planetary ball mill under the protection of argon gas, and drying the powders to prepare the two-phase reinforced aluminum alloy powder with the average grain diameter of 5 mu m;
(3) Preparing a green compact: placing the prepared two-phase reinforced aluminum alloy powder in a die, and carrying out static pressure forming, wherein the static pressure is 500MPa, and the static pressure time is 10s, so as to obtain a green body;
(5) Microwave sintering: and (3) placing the green body in a microwave heating furnace, sintering under the protection of argon, keeping the sintering temperature at 460-500 ℃ for 1-3 h, and then cooling to below 200 ℃ along with the furnace to complete sintering to obtain the biphase reinforced aluminum alloy.
Further, the FeCoNiCrMn high-entropy alloy strengthening phase is prepared from iron, cobalt, nickel, chromium and manganese powders with the purity of more than 99.9% according to an equal molar ratio, and is prepared into the high-entropy alloy powder with the particle size range of 5-15 mu m and irregular sheet shape by adopting a planetary ball mill mechanical alloying method under the protection of argon.
Further, the mechanical alloying parameters of the FeCoNiCrMn high-entropy alloy powder are as follows: pre-ball milling for 4 to 6 hours at the rotating speed of 120r/min; setting the ball milling time to be 72 to 96h, and setting the rotating speed to be 280 to 360r/min; the ball-milling jar and the ball of grinding are the steel, and the ball material ratio is 5.
Further, said Al 2 O 3 The ceramic reinforcing phase is 1 to 3 mu m in size and is a regular spherical particle.
Further, the mechanical alloying parameters of the dual-phase reinforced aluminum alloy powder in the step (2) are as follows: setting the ball milling time to be 6-10 h, setting the rotating speed to be 120-160r/min, wherein the ball milling tank and the grinding balls are made of steel, and the ball-to-material ratio is 5.
Further, the drying process of the double-phase reinforced aluminum alloy powder in the step (2) is completed in a vacuum drying oven, and the drying temperature is 70-75 ℃.
Further, the heating rate of the microwave oven in the step (5) for sintering is 40 to 55 ℃/min.
The main advantages of the invention are: the high-entropy alloy with metal characteristics and the alumina ceramic with typical ceramic characteristics are combined to be used as the composite strengthening phase of the aluminum alloy, the two strengthening phases can keep the advantages of the two strengthening phases when the aluminum alloy is strengthened, the effects of synergistic strengthening and hybrid strengthening are achieved, and the performance of the material is greatly improved.
The action mechanism of the high-entropy alloy and ceramic composite reinforced aluminum alloy is as follows:
(1) Adding high entropy alloy can balance Al 2 O 3 The deformation nonuniformity between the ceramic particles and the Al matrix provides a good bonding interface, and when the material is acted by external force, the load can be effectively transferred to the particles, so that the stress concentration on the matrix is released, the possibility of Al matrix fracture is reduced, and the mechanical property of the composite material is improved.
(2) Due to Al 2 O 3 The ceramic particles have excellent performance, the tensile strength, the compressive strength and the bending strength of the material are improved by adding the ceramic particles, and the alumina ceramic particles are hard in texture and also serve as grinding agents to a certain extent in the ball milling process, so that the ceramic particles have positive effects on grain refinement and particle dispersion distribution.
(3) The reinforcing phase and the aluminum matrix have good wettability, smooth and clean interface, no obvious reaction layer and high interface bonding strength.
(4) The FeCoNiCrMn high-entropy alloy phase and the alumina ceramic phase reinforce the aluminum alloy, and various strengthening mechanisms exist, including fine grain strengthening, particle strengthening, dislocation strengthening, interface strengthening and the like. FeCoNiCrMn and Al 2 O 3 The elastic modulus of the composite material is higher, so that the composite material has higher elastic modulus, and the plasticity and toughness potential of the particle reinforced aluminum-based composite material are fully exerted.
(5) The preparation method can prepare FeCoNiCrMn high-entropy alloy and Al with uniform particle dispersion and fine microstructure 2 O 3 The ceramic reinforced aluminum alloy has good hardness, strength and wear resistance, and can meet the application in the fields of aerospace and transportation.
Meanwhile, the microwave sintering heating technology adopted by the invention has the characteristics of rapid heating, uniform heating and the like. The sintering temperature is combined with the thermal expansion characteristics of the high-entropy alloy, the aluminum oxide and the aluminum matrix, the dual-phase reinforced aluminum alloy obtained under the adopted sintering temperature condition has higher density, and under the temperature range, the phenomena of element diffusion, grain growth, grain interface stripping and the like during sintering are avoided to a great extent, and the positive influence is exerted on the performance of the composite material.
Drawings
FIG. 1 is FeCoNiCrMn + Al obtained in example 1 2 O 3 XRD pattern of the two-phase reinforced aluminum alloy.
FIG. 2 is FeCoNiCrMn + Al obtained in example 1 2 O 3 SEM image of the two-phase reinforced aluminum alloy.
FIG. 3 is FeCoNiCrMn + Al obtained in example 2 2 O 3 SEM image of the two-phase reinforced aluminum alloy.
FIG. 4 is FeCoNiCrMn + Al obtained in example 3 2 O 3 SEM image of the two-phase reinforced aluminum alloy.
Detailed Description
In order to make the technical solutions of the present invention better understood, the present invention is further described in detail below with reference to the accompanying drawings. It will be understood that these examples are intended to illustrate the invention, and are not intended to limit the scope of the invention in any way; in the following examples, various procedures and methods not described in detail are conventional methods well known in the art.
Example 1:
preparation ofFeCoNiCrMn high-entropy alloy and Al 2 O 3 The ceramic phase composite reinforced aluminum alloy comprises 15 percent of FeCoNiCrMn high-entropy alloy reinforcing phase and Al, wherein the addition amount of the FeCoNiCrMn high-entropy alloy reinforcing phase accounts for the total mass fraction of the dual-phase reinforced aluminum alloy 2 O 3 The ceramic strengthening phase accounts for 2 percent of the total mass fraction of the two-phase reinforced aluminum alloy, and the matrix of the two-phase reinforced aluminum alloy is aluminum.
The preparation process of the two-phase reinforced aluminum alloy comprises the following steps:
step 1: mixing iron, cobalt, nickel, chromium and manganese powders with the purity of more than 99.9 percent according to an equal molar ratio, and then filling the mixture into a stainless steel ball milling tank, wherein the weight ratio of the ball powders is 5:1, adding stainless steel balls, wherein the stainless steel balls are divided into three sizes of 15mm, 10mm and 5mm according to a mass ratio of 1:3:5 weigh the large and medium size pellets. Adding anhydrous ethanol into the ball milling tank in an amount of 60 wt% of the mixed powder to ensure the uniformity of the powder in the ball milling tank, vacuumizing the ball milling tank, and performing ball milling for 5 hours in advance by using a planetary ball mill under the protection of argon at a rotating speed of 120r/min; setting the ball milling time to be 96h and the rotating speed to be 360r/min; the ball milling tank and the milling balls are made of steel, the ball-to-material ratio is 5.
Step 2: weighing the FeCoNiCrMn high-entropy alloy powder obtained in the step 1 and alumina according to the mass percentages of 15wt.% and 2wt.%, and the balance being pure aluminum. The alumina is regular spherical particles with the particle diameter of 1-3 mu m.
And step 3: preparing composite powder by high-energy ball milling: mixing the weighed two types of reinforcement powder with matrix aluminum powder, and then filling the mixture into a stainless steel ball milling tank, wherein the weight ratio of the ball powder is 5:1, adding stainless steel balls, wherein the stainless steel balls are divided into three sizes of 15mm, 10mm and 5mm according to a mass ratio of 1:2:4. the amount of absolute ethyl alcohol added into the ball-milling tank is 60wt.% of the mixed powder so as to ensure the uniformity of the powder in the ball-milling tank, then the ball-milling tank is vacuumized, a planetary ball mill is adopted under the protection of argon, the ball-milling time is set to 10 hours, the rotating speed is 160r/min, the ball-milling tank and the grinding balls are made of steel, the ball-to-material ratio is 5 2 O 3 ) The average particle size of the p/Al composite powder was 5 μm. Then a vacuum drying oven is adopted for carrying outDrying, and setting the temperature of a drying oven at 73 ℃.
And 4, step 4: preparing a green compact: drying the composite powder obtained in the step (3), placing the dried composite powder into a mold, and carrying out static pressure forming, wherein the static pressure is 450MPa, and the static pressure time is 10s, so as to obtain a green body;
and 5: microwave sintering: and (4) placing the green body obtained in the step (4) into a microwave smelting furnace, heating to 490 ℃ at the heating rate of 45 ℃/min, preserving the heat for 2 hours, carrying out the heating process under the protection of argon, and slowly cooling to below 200 ℃ to obtain the two-phase reinforced aluminum alloy.
And (3) detection results: feCoNiCrMn + Al prepared in example 1 2 O 3 The XRD and SEM of the two-phase reinforced aluminum alloy are shown in figures 1 and 2, and the figures show that particles of the obtained material are dispersedly distributed at the grain boundary of an aluminum matrix, the interface is smooth and clean, no obvious reaction layer exists, the pores and defects are low, and the results of standard performance tests show that the hardness of the two-phase reinforced aluminum alloy reaches 109.3HV, the yield strength is 291.5MPa, the elongation is 41.2%, the performance of the material is greatly improved, and the material has obvious technical effects.
In the embodiment 2 and the embodiment 3, the FeCoNiCrMn high-entropy alloy is kept accounting for 15 percent of the total mass fraction of the dual-phase reinforced aluminum alloy, and Al is added 2 O 3 Mass fraction of ceramic strengthening phase, and the same process and parameters as in example 1 were used to prepare FeCoNiCrMn + Al 2 O 3 A composite material. FeCoNiCrMn + Al obtained in examples 1 to 3 2 O 3 The performance index of the composite material is shown in table 1.
TABLE 1
Examples | Al 2 O 3 Content of (A)wt.%) | Hardness (HV) | Yield strength (MPa) | Elongation (%) |
Example 1 | 2 | 109.3 | 291.5 | 41.2 |
Example 2 | 5 | 120.0 | 311.6 | 45.0 |
Example 3 | 8 | 128.5 | 319.2 | 46.7 |
From the test data shown in Table 1, it is shown that FeCoNiCrMn + Al prepared according to the present invention 2 O 3 The hardness, yield strength and elongation of the composite material are all improved along with the increase of the alumina ceramic reinforcing phase.
The examples are preferred embodiments of the present invention, but the present invention is not limited to the above embodiments, and any obvious modifications, substitutions or variations can be made by those skilled in the art without departing from the spirit of the present invention.
Claims (8)
1. A dual-phase reinforced aluminum alloy is characterized in that the dual-phase reinforced aluminum alloy is reinforcedThe phases are FeCoNiCrMn high-entropy alloy strengthening phase and Al 2 O 3 A ceramic strengthening phase, wherein the FeCoNiCrMn high-entropy alloy strengthening phase accounts for 15 percent of the total mass fraction of the dual-phase strengthened aluminum alloy, and Al 2 O 3 The ceramic strengthening phase accounts for 2-8% of the total mass fraction of the dual-phase reinforced aluminum alloy, and the matrix of the dual-phase reinforced aluminum alloy is aluminum;
the FeCoNiCrMn high-entropy alloy strengthening phase is in a sheet shape in an aluminum matrix, and the Al is 2 O 3 The ceramic strengthening phase is spherical;
the hardness of the aluminum alloy reaches 109.3 to 128.5HV, the yield strength is 291.5 to 319.2MPa, and the elongation is 41.2 to 46.7%.
2. A method for producing a dual-phase reinforced aluminum alloy as recited in claim 1, comprising the steps of:
(1) Preparing materials: weighing FeCoNiCrMn high-entropy alloy strengthening phase powder and Al according to the mass percent of 15 percent and 2-8 percent 2 O 3 Ceramic powders, and pure aluminum powders;
(2) Preparing two-phase reinforced aluminum alloy powder: after mixing the weighed powders, mechanically alloying the powders by adopting a planetary ball mill under the protection of argon gas, and drying the powders to prepare the two-phase reinforced aluminum alloy powder with the average grain diameter of 5 mu m;
(3) Preparing a green compact: placing the prepared two-phase reinforced aluminum alloy powder in a mold, and carrying out static pressure forming, wherein the static pressure is 350 to 500MPa, and the static pressure time is 10s, so as to obtain a green body;
(5) Microwave sintering: and (3) placing the green body in a microwave heating furnace, sintering under the protection of argon, keeping the sintering temperature at 460-500 ℃ for 1-3 h, and then cooling to below 200 ℃ along with the furnace to complete sintering to obtain the biphase reinforced aluminum alloy.
3. The preparation method of the FeCoNiCrMn high-entropy alloy powder is characterized in that the FeCoNiCrMn high-entropy alloy strengthening phase is prepared from iron, cobalt, nickel, chromium and manganese powders with the purity of more than 99.9% according to an equimolar ratio, and the high-entropy alloy powder with the particle size range of 5-15 μm and irregular sheet shapes is prepared by a mechanical alloying method of a planetary ball mill under the protection of argon.
4. The preparation method according to claim 3, wherein the FeCoNiCrMn high entropy alloy powder mechanical alloying parameters are as follows: pre-ball milling for 4 to 6 hours at the rotating speed of 120r/min; setting the ball milling time to be 72 to 96h, and setting the rotating speed to be 280 to 360r/min; the ball-milling jar and the ball of grinding are the steel, and the ball material ratio is 5.
5. The method of claim 2, wherein: the Al is 2 O 3 The ceramic reinforcing phase has a size of 1-3 μm and is in the form of regular spherical particles.
6. The method of claim 2, wherein: the mechanical alloying parameters of the double-phase reinforced aluminum alloy powder in the step (2) are as follows: setting the ball milling time to be 6-10 h, setting the rotating speed to be 120-160r/min, wherein the ball milling tank and the grinding balls are made of steel, and the ball-to-material ratio is 5.
7. The method of claim 2, wherein: and (3) completing the drying process of the double-phase reinforced aluminum alloy powder in the step (2) in a vacuum drying box, wherein the drying temperature is 70-75 ℃.
8. The method of claim 2, wherein: and (5) the heating rate of the sintering in the microwave heating furnace is 40-55 ℃/min.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202210153260.7A CN114645180B (en) | 2022-02-18 | 2022-02-18 | Double-phase reinforced aluminum alloy and preparation method thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202210153260.7A CN114645180B (en) | 2022-02-18 | 2022-02-18 | Double-phase reinforced aluminum alloy and preparation method thereof |
Publications (2)
Publication Number | Publication Date |
---|---|
CN114645180A CN114645180A (en) | 2022-06-21 |
CN114645180B true CN114645180B (en) | 2023-03-21 |
Family
ID=81993273
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202210153260.7A Active CN114645180B (en) | 2022-02-18 | 2022-02-18 | Double-phase reinforced aluminum alloy and preparation method thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN114645180B (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115044808B (en) * | 2022-06-30 | 2023-03-21 | 江苏大学 | Composite reinforced heat-resistant wear-resistant aluminum alloy and preparation method thereof |
CN115491547B (en) * | 2022-09-28 | 2023-04-18 | 山东创新精密科技有限公司 | Multiphase reinforced aluminum alloy material and preparation method thereof |
CN117305829B (en) * | 2023-11-10 | 2024-03-12 | 西安工程大学 | Preparation method of nano ceramic particle reinforced high-entropy alloy-based composite powder suitable for cold spraying |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110438493A (en) * | 2019-09-05 | 2019-11-12 | 山东建筑大学 | A method of preparing CNTs enhancing high-entropy alloy laser deposition composite material |
CN112549848A (en) * | 2020-11-26 | 2021-03-26 | 江苏珀然股份有限公司 | Wheel hub made of high-entropy alloy reinforced aluminum-based gradient material and manufacturing method thereof |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4735656A (en) * | 1986-12-29 | 1988-04-05 | United Technologies Corporation | Abrasive material, especially for turbine blade tips |
CN100478474C (en) * | 2002-07-31 | 2009-04-15 | 北京有色金属研究总院 | Particle reinforced aluminium-based composite material and workpiece therefrom and its forming process |
TW200724492A (en) * | 2005-12-16 | 2007-07-01 | Rui-Kai Chen | Bi-liquid phase sintering process for manufacturing of Al2O3 super hard ceramic metal using cryolite and binding alloy |
CN104388764B (en) * | 2014-11-06 | 2016-05-04 | 华南理工大学 | Aluminum matrix composite that a kind of high-entropy alloy strengthens and preparation method thereof |
CN104862510B (en) * | 2015-06-03 | 2016-09-07 | 华中科技大学 | A kind of high-entropy alloy particle enhanced aluminum-based composite material and preparation method thereof |
CN105478724B (en) * | 2015-12-23 | 2017-08-29 | 华南理工大学 | A kind of high-entropy alloy particle enhanced aluminum-based composite material and its stirring casting preparation technology |
US20170314097A1 (en) * | 2016-05-02 | 2017-11-02 | Korea Advanced Institute Of Science And Technology | High-strength and ultra heat-resistant high entropy alloy (hea) matrix composites and method of preparing the same |
CN108588501B (en) * | 2018-05-21 | 2020-05-05 | 江苏理工学院 | Aluminum alloy composite material with solid self-lubricating property and preparation method thereof |
CN108624829B (en) * | 2018-05-21 | 2020-05-05 | 江苏理工学院 | High-elasticity aluminum-based composite material and preparation method thereof |
CN108660352B (en) * | 2018-05-31 | 2019-08-30 | 太原理工大学 | A kind of enhanced AlCoCrFeNi2The preparation method and application of high-entropy alloy-base neutron absorber material |
CN109338172A (en) * | 2018-12-11 | 2019-02-15 | 西安工业大学 | A kind of 2024 aluminum matrix composites and preparation method thereof of high-entropy alloy enhancing |
CN109439951B (en) * | 2018-12-27 | 2020-07-03 | 吉林大学 | Method for strengthening aluminum-silicon alloy based on multiphase mixed scale ceramic particle enhancer |
US12012647B2 (en) * | 2019-06-21 | 2024-06-18 | United States Government Administrator Of Nasa | Additively manufactured oxide dispersion strengthened medium entropy alloys for high temperature applications |
CN110273078B (en) * | 2019-06-28 | 2021-01-15 | 江苏大学 | Magnetic (FeCoNi)1.5CuBmREn)PAl composite material and preparation method thereof |
US11840746B2 (en) * | 2019-07-19 | 2023-12-12 | University Of Florida Research Foundation, Inc. | High temperature lightweight Al—Fe—Si based alloys |
CN110523997B (en) * | 2019-08-19 | 2022-05-20 | 江苏大学 | High-entropy alloy particle reinforced subzero treatment aluminum-based composite material and preparation method thereof |
US11565318B2 (en) * | 2019-09-03 | 2023-01-31 | Ut-Battelle, Llc | Reactive matrix infiltration of powder preforms |
CN111394667B (en) * | 2020-03-25 | 2021-09-10 | 江苏大学 | Regulation (FeCoNiCrAlCu)pMethod for interface of/2024A 1 composite material |
CN111961906B (en) * | 2020-07-29 | 2021-11-05 | 济南大学 | Preparation method of high-strength high-toughness corrosion-resistant nickel-based composite material and obtained product |
CN112626403A (en) * | 2020-12-07 | 2021-04-09 | 湘潭大学 | TiB2-FeCoNiCrMn aluminum liquid corrosion resistant material |
CN112899531B (en) * | 2021-01-19 | 2021-11-23 | 江苏大学 | High-entropy alloy particle reinforced aluminum-based composite material and magnetic field auxiliary preparation method |
CN113789464B (en) * | 2021-08-16 | 2022-08-26 | 东南大学 | Ceramic phase reinforced refractory high-entropy alloy and preparation method thereof |
-
2022
- 2022-02-18 CN CN202210153260.7A patent/CN114645180B/en active Active
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110438493A (en) * | 2019-09-05 | 2019-11-12 | 山东建筑大学 | A method of preparing CNTs enhancing high-entropy alloy laser deposition composite material |
CN112549848A (en) * | 2020-11-26 | 2021-03-26 | 江苏珀然股份有限公司 | Wheel hub made of high-entropy alloy reinforced aluminum-based gradient material and manufacturing method thereof |
Also Published As
Publication number | Publication date |
---|---|
CN114645180A (en) | 2022-06-21 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN114645180B (en) | Double-phase reinforced aluminum alloy and preparation method thereof | |
US11731178B2 (en) | Rolled (FeCoNiCrRn/Al)-2024Al composite panel and fabrication method thereof | |
CN110273092B (en) | CoCrNi particle reinforced magnesium-based composite material and preparation method thereof | |
CN112647009B (en) | High-strength high-wear-resistance medium-entropy alloy and preparation method thereof | |
CN108251695B (en) | Preparation method of titanium-aluminum-niobium-zirconium-molybdenum alloy | |
CN110396632A (en) | A kind of Ti (C, N) based ceramic metal and preparation method thereof with homogeneous ring core structure | |
CN113088733B (en) | Ti-W heterogeneous metal-metal composite material and preparation method thereof | |
CN114150238B (en) | Ti-Al-Nb-based composite material and preparation method thereof | |
CN113549801A (en) | Second-phase reinforced high-entropy binder hard alloy and preparation method thereof | |
CN111304479A (en) | Preparation method of VCrNbMoW refractory high-entropy alloy | |
CN114959406A (en) | Oscillatory pressure sintering ultrahigh-temperature medium-entropy ceramic reinforced refractory fine-grain medium-entropy alloy composite material | |
CN110438384A (en) | A kind of Ni-based ultra-fine cemented carbide of iron and preparation method thereof | |
CN112143925A (en) | Preparation method of high-strength high-plasticity titanium-magnesium composite material | |
CN110373593B (en) | Microwave sintering process of titanium carbonitride-based composite metal ceramic material | |
CN109468494B (en) | Wear-resistant net-shaped Cr3C2Preparation method of reinforced NiAl alloy | |
CN115353395B (en) | Preparation of Ti 2 AlC/B 4 Method for C complex phase ceramic | |
CN110791693A (en) | High-entropy alloy with low Al content, high strength and toughness and acid corrosion resistance and preparation method thereof | |
CN112941391B (en) | NbC-containing high-density composite metal ceramic material and preparation method thereof | |
CN113816747A (en) | TiC enhanced MAX phase high-entropy ceramic matrix composite material and preparation method thereof | |
CN113020604A (en) | High-strength wear-resistant high-temperature-resistant titanium-aluminum oxide alloy material and preparation method thereof | |
CN115921874B (en) | TiAl-based composite material with two-stage reinforced three-dimensional network structure and preparation method thereof | |
CN115747610B (en) | SiC-doped high-entropy alloy and preparation method and application thereof | |
CN115305388B (en) | Nickel-based high-entropy alloy material with unequal atomic ratio and preparation method thereof | |
CN115637365B (en) | High specific gravity alloy of medium entropy alloy binder and preparation method thereof | |
CN113774265B (en) | High-entropy intermetallic compound with high strength and wide-temperature-range wear-resistant characteristics |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |