CN110142402B - Powder metallurgy aluminum-based material and preparation method thereof - Google Patents
Powder metallurgy aluminum-based material and preparation method thereof Download PDFInfo
- Publication number
- CN110142402B CN110142402B CN201910478418.6A CN201910478418A CN110142402B CN 110142402 B CN110142402 B CN 110142402B CN 201910478418 A CN201910478418 A CN 201910478418A CN 110142402 B CN110142402 B CN 110142402B
- Authority
- CN
- China
- Prior art keywords
- powder
- aluminum
- sintering
- based material
- magnesium hydride
- 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
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title claims abstract description 61
- 229910052782 aluminium Inorganic materials 0.000 title claims abstract description 59
- 238000004663 powder metallurgy Methods 0.000 title claims abstract description 46
- 239000000463 material Substances 0.000 title claims abstract description 34
- 238000002360 preparation method Methods 0.000 title claims abstract description 9
- 239000000843 powder Substances 0.000 claims abstract description 199
- 238000005245 sintering Methods 0.000 claims abstract description 103
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims abstract description 80
- 229910012375 magnesium hydride Inorganic materials 0.000 claims abstract description 68
- 239000002994 raw material Substances 0.000 claims abstract description 58
- 229910000838 Al alloy Inorganic materials 0.000 claims abstract description 42
- 238000002156 mixing Methods 0.000 claims abstract description 32
- 239000011159 matrix material Substances 0.000 claims abstract description 27
- 238000000034 method Methods 0.000 claims abstract description 26
- 238000010438 heat treatment Methods 0.000 claims abstract description 22
- 239000002131 composite material Substances 0.000 claims abstract description 8
- 239000000126 substance Substances 0.000 claims abstract description 4
- 239000006104 solid solution Substances 0.000 claims description 32
- 230000032683 aging Effects 0.000 claims description 30
- 239000002245 particle Substances 0.000 claims description 29
- 238000000498 ball milling Methods 0.000 claims description 26
- 238000004321 preservation Methods 0.000 claims description 22
- 239000000314 lubricant Substances 0.000 claims description 17
- 230000001681 protective effect Effects 0.000 claims description 13
- 238000003825 pressing Methods 0.000 claims description 12
- 239000011812 mixed powder Substances 0.000 claims description 9
- 238000004519 manufacturing process Methods 0.000 abstract description 12
- 238000001816 cooling Methods 0.000 description 17
- 239000000956 alloy Substances 0.000 description 14
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 13
- 239000001301 oxygen Substances 0.000 description 13
- 229910052760 oxygen Inorganic materials 0.000 description 13
- 229910001094 6061 aluminium alloy Inorganic materials 0.000 description 12
- 238000007723 die pressing method Methods 0.000 description 11
- 239000000758 substrate Substances 0.000 description 7
- 229910000974 2014 aluminium alloy Inorganic materials 0.000 description 6
- 229910001008 7075 aluminium alloy Inorganic materials 0.000 description 6
- 229910045601 alloy Inorganic materials 0.000 description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- 235000021355 Stearic acid Nutrition 0.000 description 4
- QIQXTHQIDYTFRH-UHFFFAOYSA-N octadecanoic acid Chemical compound CCCCCCCCCCCCCCCCCC(O)=O QIQXTHQIDYTFRH-UHFFFAOYSA-N 0.000 description 4
- OQCDKBAXFALNLD-UHFFFAOYSA-N octadecanoic acid Natural products CCCCCCCC(C)CCCCCCCCC(O)=O OQCDKBAXFALNLD-UHFFFAOYSA-N 0.000 description 4
- 239000012188 paraffin wax Substances 0.000 description 4
- 239000008117 stearic acid Substances 0.000 description 4
- 229910001250 2024 aluminium alloy Inorganic materials 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 3
- XOOUIPVCVHRTMJ-UHFFFAOYSA-L zinc stearate Chemical compound [Zn+2].CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O XOOUIPVCVHRTMJ-UHFFFAOYSA-L 0.000 description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 2
- CSDREXVUYHZDNP-UHFFFAOYSA-N alumanylidynesilicon Chemical compound [Al].[Si] CSDREXVUYHZDNP-UHFFFAOYSA-N 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 239000001257 hydrogen Substances 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 239000007791 liquid phase Substances 0.000 description 2
- 239000011777 magnesium Substances 0.000 description 2
- 229910052749 magnesium Inorganic materials 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 238000010923 batch production Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 229910052593 corundum Inorganic materials 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 235000013350 formula milk Nutrition 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 238000013038 hand mixing Methods 0.000 description 1
- 238000011031 large-scale manufacturing process Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000004570 mortar (masonry) Substances 0.000 description 1
- 235000020610 powder formula Nutrition 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 238000012876 topography Methods 0.000 description 1
- 238000009736 wetting Methods 0.000 description 1
- 229910001845 yogo sapphire Inorganic materials 0.000 description 1
Images
Classifications
-
- B22F1/0003—
-
- 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
- B22F3/02—Compacting only
-
- 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
- B22F3/1003—Use of special medium during sintering, e.g. sintering aid
- B22F3/1007—Atmosphere
-
- 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
- B22F3/24—After-treatment of workpieces or articles
-
- 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
-
- 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
- B22F3/24—After-treatment of workpieces or articles
- B22F2003/248—Thermal after-treatment
-
- 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
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
- B22F2998/10—Processes characterised by the sequence of their steps
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Powder Metallurgy (AREA)
Abstract
The invention relates to a powder metallurgy aluminum-based material, which comprises raw material powder and aluminum matrix powder, wherein the raw material powder comprises 0.001-3% of magnesium hydride powder by mass percentage, and the balance is the aluminum matrix powder, and the aluminum matrix powder is aluminum simple substance powder or aluminum alloy powder or aluminum matrix composite powder. The invention also relates to a preparation method for preparing the powder metallurgy aluminum-based material, which comprises the following steps of (a) mixing powder; (b) forming; (c) sintering; (d) and (6) heat treatment. The powder metallurgy aluminum-based material has small sintering deformation; the preparation method has the advantages of simple process, high production efficiency and suitability for mass production.
Description
Technical Field
The invention relates to the field of powder metallurgy, in particular to a powder metallurgy aluminum-based material and a preparation method thereof.
Background
The aluminum alloy is a light material with low density and high specific strength, is beneficial to reducing self weight, saving energy and reducing emission after replacing iron-based and copper-based parts, and has been widely applied to the fields of aerospace, automobiles, mechanical manufacturing, ships, chemical industry and the like. For example, the cross beam, high pressure cylinder, automobile cantilever member, engine blade, casing and cylinder sleeve, automobile engine and gear box parts of supersonic fighter are widely made of aluminum alloy. However, many parts require not only light weight and good mechanical properties such as hardness, strength, wear resistance, thermal expansion coefficient, high temperature mechanical properties, etc., but also high dimensional accuracy. In particular, structural parts, such as transmission mechanism parts of a gearbox, have extremely high requirements on dimensional accuracy. This puts high demands on the manufacturing accuracy of the aluminium alloy parts.
The powder metallurgy process is energy-saving, material-saving and near-net-shape forming, is a green manufacturing technology and is suitable for large-scale production. The powder metallurgy aluminum alloy part combines the advantages of powder metallurgy and aluminum alloy, has enough mechanical property, can partially replace the traditional iron-based and copper-based parts, and is beneficial to promoting the development of light weight. But the liquid phase sintering characteristic of the aluminum alloy causes the sintering deformation of the aluminum alloy to be serious, and the problem of sintering deformation is solved by the design of a common die in the field of powder metallurgy at present; however, the sintering deformation of the aluminum alloy has non-uniformity and randomness, and is difficult to eliminate through the design of the die. Sintering deformation is one of the key technical problems of powder metallurgy aluminum-based materials, and the mass production of the materials is seriously hindered. Therefore, there is a need for a powder metallurgy aluminum-based material and a method of making the same that can address this sintering distortion problem in other ways.
Disclosure of Invention
The invention aims to provide a powder metallurgy aluminum-based material with smaller sintering deformation aiming at the current situation of the prior art.
The invention aims to solve another technical problem of providing a preparation method which is used for preparing the powder metallurgy aluminum-based material and has the advantages of simple process, high production efficiency and suitability for mass production aiming at the current situation of the prior art.
The technical scheme adopted by the invention for solving the technical problems is as follows: the powder metallurgy aluminum-based material comprises raw material powder and aluminum matrix powder, wherein the raw material powder comprises 0.001-3% of magnesium hydride powder by mass percent, and the balance is the aluminum matrix powder, and the aluminum matrix powder is aluminum simple substance powder or aluminum alloy powder or aluminum matrix composite powder.
Preferably, the mass percentage of the magnesium hydride powder is 0.06% -0.85%.
Preferably, the purity of the magnesium hydride powder is 90-98%.
The preparation method for preparing the powder metallurgy aluminum-based material comprises the following steps:
(a) mixing powder: uniformly mixing aluminum matrix powder and magnesium hydride powder according to the component proportion to obtain raw material powder;
(b) forming: pressing and forming the powder obtained in the step (a) to obtain a blank body;
(c) and (3) sintering: sintering the green body obtained in the step (2) under a protective atmosphere to obtain a sintered part;
(d) and (3) heat treatment: sequentially carrying out solid solution treatment and artificial aging heat treatment on the sintered piece obtained in the step (c);
and (d) not performing the step (d) on the sintered part which is a pure aluminum matrix or an aluminum alloy matrix which cannot be strengthened by heat treatment.
Preferably, the protective atmosphere is N2,H2Or an Ar atmosphere.
Preferably, the sintering temperature of the sintering in the step (c) is 550-660 ℃, the heat preservation time is 5-60 min, and further preferably, the cooling time is 0.5-3 h.
Preferably, the solid solution temperature of the solid solution treatment in the step (d) is 450-580 ℃, the solid solution time is 0.5-6 h, the artificial aging temperature is 100-200 ℃, and the artificial aging time is 3-24 h.
In order to facilitate demoulding and forming, in the powder mixing process in the step (a), a lubricant is added into the raw material powder, wherein the lubricant accounts for 0.5-2% of the raw material powder by mass. The lubricant can be selected from stearic acid lubricant or paraffin, and other common lubricants. The lubricant is added by hand mixing or mixer mixing, wherein the mixer mixing is preferably any one of a ball mill, a V-shaped mixer, a conical mixer, a wine barrel mixer and a screw mixer.
In order to prevent the composite material from being influenced by the lubricant, the blank is dewaxed before sintering in the step (c), wherein the dewaxing temperature is 350-450 ℃, and the dewaxing time is 20-50 min.
Preferably, the aluminum matrix powder has an average particle size of 30 to 100 μm, and the magnesium hydride powder has an average particle size of 0.1 to 100 μm. More preferably, the aluminum matrix powder has an average particle size of 60 to 80 μm, the magnesium hydride powder has an average particle size of 1 to 45 μm,
preferably, the powder mixture in the step (a) is mixed by a ball mill, the rotating speed of the ball mill is 50-140 r/min, and the ball milling time is 5-10 h. Preferably, the rotating speed of the ball mill is 80-110 r/min, and the ball milling time is 6-9 h.
Preferably, the raw material powder in the step (b) is pressed and formed by die pressing, and the forming pressure is 150-500 MPa.
Compared with the prior art, the invention has the advantages that: magnesium hydride is added in the aluminum-based powder metallurgy formula, so that the sintering deformation can be obviously reduced, the size after sintering is stabilized, and the near-net-shape forming advantage is favorably kept. The factors causing sintering deformation are many, and proper addition of magnesium hydride can release hydrogen at high temperature, remove oxygen in a sintering blank, facilitate formation of a good sintering neck and avoid sintering deformation caused by poor sintering. And secondly, the magnesium hydride releases hydrogen along with the temperature rise, so that the wetting of the sintering liquid relative to the solid particles is weakened in a proper amount, the mutual influence of the liquid phase and the solid particle framework is reduced, and the sintering deformation is reduced to a certain extent. In addition, magnesium is an important element for effective sintering of aluminum alloy powder metallurgy, and is helpful for breaking oxide films on the surfaces of aluminum particles, active magnesium left after the added magnesium hydride is dehydrogenated is also beneficial for forming a sintering neck, and the mechanical property of a sintered part can be improved to a certain extent. The cost of adding a small amount of magnesium hydride is not high, the adding mode is simple, and the method is suitable for batch production;
the invention solves the problem of sintering deformation when the aluminum alloy is prepared by adopting the powder metallurgy method by improving the component proportion of the powder metallurgy aluminum-based material from the viewpoint of the raw material powder formula, the method does not need to greatly improve production equipment and process, is convenient to use, has lower cost and higher production efficiency, can carry out mass production, and solves the long-standing technical problem of aluminum alloy sintering deformation by adopting a simple and convenient method.
Drawings
FIG. 1 is a microscopic morphology of magnesium hydride particles in example 9 of the present invention;
FIG. 2 is a fracture morphology graph of a sintered part in example 10 of the present invention;
FIG. 3 is a micro-topography of the mixed powder in example 1 of the present invention.
Detailed Description
The following detailed description of embodiments of the present invention is provided in connection with the accompanying drawings and examples.
Example 1:
in this embodiment, a method for preparing a powder metallurgy aluminum-based material is described by taking a pure aluminum substrate as an example, and specifically includes the following steps:
(1) mixing powder: and grinding and uniformly mixing the aluminum elementary powder with the average particle size of 90 mu m and the magnesium hydride powder with the average particle size of 45 mu m by using a mortar to obtain raw material powder, wherein the mass fraction of the magnesium hydride powder in the raw material powder is 0.001%, and the balance is the aluminum elementary powder. The magnesium hydride powder used in this step may preferably have a purity of 98%.
(2) Forming: and (2) carrying out die pressing forming on the powder obtained in the step (1), wherein the pressing pressure is 150MPa, and the pressure maintaining time is 15 s.
(3) And (3) sintering: sintering by adopting a tube furnace under the protective atmosphere of high-purity N2The sintering temperature is 650 ℃, the sintering heat preservation time is 60min, and furnace cooling is carried out after the heat preservation is finished. The sintering environment for this step may preferably be below 10ppm oxygen and dew point below-40 ℃.
Tests show that the strength of the pure aluminum powder without the hydrogenated magnesium powder after sintering is 68MPa, and the sintering deformation reaches 3 percent; after 0.001 percent of magnesium hydride powder is added into pure aluminum powder, the strength of the sintered aluminum-based material of powder metallurgy is 70MPa, and the sintering deformation is 2.98 percent.
Example 2:
in this embodiment, taking 2014 aluminum alloy matrix as an example, a method for preparing a powder metallurgy aluminum-based material is described, which specifically includes the following steps:
(1) mixing powder: mixing 2014 aluminum alloy powder with the average particle size of 78 microns and magnesium hydride powder with the average particle size of 10 microns to obtain raw material powder, ball-milling the raw material powder on a planetary ball mill with the rotating speed of 95r/min for 8 hours, and uniformly mixing, wherein the mass fraction of the magnesium hydride powder in the raw material powder is 0.51%, and the balance is 2014 aluminum alloy powder. The magnesium hydride powder used in this step is preferably 95% pure.
(2) Forming: mixing the powder obtained in the step (1) with zinc stearate accounting for 0.5 wt% of the raw material powder as a lubricant by using a V-shaped mixer, uniformly mixing, and then carrying out die pressing on the powder, wherein the pressing pressure is 400MPa, and the pressure maintaining time is 20 s;
(3) and (3) sintering: sintering by adopting a mesh belt type continuous furnace, wherein the sintering protective atmosphere is high-purity N2Dewaxing at 350 deg.C for 30 min; the sintering temperature is 595 ℃, the sintering heat preservation time is 40min, furnace cooling is carried out after the heat preservation is finished, and the cooling speed is controlled to reduce the temperature to the room temperature within 2h, so that the sintered part is obtained. The sintering environment for this step of sintering may preferably be less than 10ppm oxygen with a dew point of less than-40 ℃.
(4) And (3) heat treatment: and sequentially carrying out solid solution and artificial aging heat treatment on the sintered piece, wherein the solid solution temperature is 510 ℃, the solid solution time is 1h, the artificial aging temperature is 180 ℃, and the artificial aging time is 15 h.
Through tests, the 2014 aluminum alloy powder without the hydrogenated magnesium powder has the strength of 235MPa after sintering, and the deformation amount reaches 1.63%; after 0.51 percent of magnesium hydride powder is added into 2014 aluminum alloy powder, the intensity of the sintered magnesium hydride modified powder metallurgy 2014 aluminum alloy material is 226MPa, and the deformation is 0.48 percent.
Example 3:
in this embodiment, a 7039 aluminum alloy substrate is taken as an example to illustrate a method for preparing a powder metallurgy aluminum-based material, which specifically includes the following steps:
(1) mixing powder: mixing 7039 aluminum alloy powder with the average particle size of 45 microns and magnesium hydride powder with the average particle size of 16 microns to obtain raw material powder, ball-milling the raw material powder on a planetary ball mill with the rotating speed of 50r/min for 10 hours, and uniformly mixing, wherein the mass fraction of the magnesium hydride powder in the raw material powder is 3%, and the balance is 7039 aluminum alloy powder. The magnesium hydride powder used in this step may preferably have a purity of 90%.
(2) Forming: mixing zinc stearate accounting for 0.8% of the mass fraction of the raw material powder into the powder obtained in the step (1) by using a spiral mixer as a lubricant, uniformly mixing, and then carrying out die pressing on the powder to form the powder, wherein the pressing pressure is 180MPa, and the pressure maintaining time is 15 s;
(3) and (3) sintering: by usingSintering in a mesh belt type continuous furnace under the protective atmosphere of high-purity N2Dewaxing at 350 deg.C for 22 min; the sintering temperature is 550 ℃, the sintering heat preservation time is 5min, furnace cooling is carried out after the heat preservation is finished, and the cooling speed is controlled to reduce the temperature to the room temperature within 0.5h, so that a sintered part is obtained. The sintering environment for this step of sintering may preferably be less than 10ppm oxygen with a dew point of less than-40 ℃.
(4) And (3) heat treatment: and sequentially carrying out solid solution and artificial aging heat treatment on the sintered piece, wherein the solid solution temperature is 450 ℃, the solid solution time is 0.8h, the artificial aging temperature is 150 ℃, and the artificial aging time is 3 h.
Tests show that after being sintered, the 7039 aluminum alloy powder without the hydrogenated magnesium powder has the strength of 134MPa and the deformation amount of 0.75 percent; after 3 percent of magnesium hydride powder is added into 7039 aluminum alloy powder, the strength of the sintered magnesium hydride modified powder metallurgy 7039 aluminum alloy material is 90MPa, and the deformation reaches 0.21 percent.
Example 4:
in this embodiment, a 6061 aluminum alloy substrate is taken as an example to illustrate a method for preparing a powder metallurgy aluminum-based material, which specifically includes the following steps:
(1) mixing powder: 6061 aluminum alloy powder with the average particle size of 80 mu m and magnesium hydride powder with the average particle size of 0.1 mu m are mixed to obtain raw material powder, wherein the magnesium hydride powder accounts for 0.2 percent of the mass fraction of the raw material powder, and the balance is 6061 aluminum alloy powder. Ball-milling the raw material powder for 5.5h on a planetary ball mill with the rotating speed of 100r/min, adding stearic acid accounting for 1.5 percent of the mass fraction of the raw material powder into the raw material powder as a lubricant for 0.5h before the ball-milling is finished, and obtaining mixed powder after the ball-milling is finished. The magnesium hydride powder used in this step may preferably have a purity of 98%.
(2) Forming: and (2) carrying out die pressing forming on the powder obtained in the step (1), wherein the pressing pressure is 200MPa, and the pressure maintaining time is 10 s.
(3) And (3) sintering: sintering by adopting a push rod type continuous furnace in a protective atmosphere of high-purity N2The oxygen content of the sintering environment is lower than 10ppm, the dew point is lower than minus 40 ℃, the dewaxing temperature is 450 ℃, and the dewaxing time is 20 min; the sintering temperature is 590 ℃, the sintering heat preservation time is 60min, and a heat preservation junction is formedAnd cooling the sintered piece along with the furnace after the end, and controlling the cooling speed to reduce the temperature to the room temperature within 3 hours to obtain the sintered piece. The sintering environment for this step is preferably below 10ppm oxygen and dew point below-40 ℃.
(4) And (3) heat treatment: sequentially carrying out solid solution and artificial aging heat treatment on the sintered piece, wherein the solid solution temperature is 580 ℃, and the solid solution time is 0.5 h; the artificial aging temperature is 160 ℃, and the artificial aging time is 24 h.
Tests show that the strength of the 6061 aluminum alloy powder without the hydrogenated magnesium powder after sintering is 127MPa, and the deformation can reach 1.58%; after 0.2 percent of magnesium hydride powder is added into 6061 aluminum alloy powder, the strength of the sintered magnesium hydride modified powder metallurgy 6061 aluminum alloy material is 112MPa, and the deformation reaches 0.51 percent.
Example 5:
in this embodiment, a 6061 aluminum alloy substrate is taken as an example to illustrate a method for preparing a powder metallurgy aluminum-based material, which specifically includes the following steps:
(1) mixing powder: 6061 aluminum alloy powder with the average particle size of 75 microns and magnesium hydride powder with the average particle size of 35 microns are mixed to obtain raw material powder, wherein the magnesium hydride powder accounts for 0.03 percent of the mass fraction of the raw material powder, and the balance is 6061 aluminum alloy powder. Ball-milling the raw material powder for 5 hours on a planetary ball mill with the rotating speed of 140r/min, adding stearic acid accounting for 1.8 percent of the mass fraction of the raw material powder into the raw material powder as a lubricant for 0.5 hour before the ball-milling is finished, and obtaining mixed powder after the ball-milling is finished. The magnesium hydride powder used in this step may preferably have a purity of 95%.
(2) Forming: and (2) carrying out die pressing forming on the powder obtained in the step (1), wherein the pressing pressure is 350MPa, and the pressure maintaining time is 25 s.
(3) And (3) sintering: sintering by adopting a push rod type continuous furnace in a protective atmosphere of high-purity N2The oxygen content of the sintering environment is lower than 10ppm, the dew point is lower than minus 40 ℃, the dewaxing temperature is 370 ℃, and the dewaxing time is 45 min; the sintering temperature is 660 ℃, the sintering heat preservation time is 55min, furnace cooling is carried out after the heat preservation is finished, and the cooling speed is controlled to reduce the temperature to the room temperature within 2.5h, so that the sintered part is obtained. The sintering environment for this step is preferably below 10ppm oxygen and dew point below-40 ℃.
(4) And (3) heat treatment: sequentially carrying out solid solution and artificial aging heat treatment on the sintered piece, wherein the solid solution temperature is 550 ℃, and the solid solution time is 3.5 h; the artificial aging temperature is 200 ℃, and the artificial aging time is 15 h.
Tests show that the strength of the 6061 aluminum alloy powder without the hydrogenated magnesium powder after sintering is 193MPa, and the deformation reaches 1.96 percent; the strength of the 6061 aluminum alloy material modified by the magnesium hydride is 191MPa and the deformation reaches 1.25 percent after the 6061 aluminum alloy powder is added with 0.03 percent of magnesium hydride powder.
Example 6:
in this embodiment, a 7075 aluminum alloy substrate is taken as an example to illustrate a method for preparing a powder metallurgy aluminum-based material, which specifically includes the following steps:
(1) mixing powder: 7075 aluminum alloy powder having an average particle diameter of 100 μm was mixed with magnesium hydride powder having an average particle diameter of 1 μm to obtain raw material powder, wherein the mass fraction of the magnesium hydride powder in the raw material powder was 0.06%, and the balance was 7075 aluminum alloy powder. Ball-milling the raw material powder for 7 hours on a planetary ball mill with the rotation speed of 110r/min, adding paraffin accounting for 2% of the mass fraction of the raw material powder into the raw material powder as a lubricant 0.5 hour before the ball-milling is finished, and obtaining mixed powder after the ball-milling is finished. The magnesium hydride powder used in this step may preferably have a purity of 95%.
(2) Forming: and (2) carrying out die pressing forming on the powder obtained in the step (1), wherein the pressing pressure is 450MPa, and the pressure maintaining time is 30 s.
(3) And (3) sintering: sintering by adopting a push rod type continuous furnace in a protective atmosphere of high-purity N2Dewaxing at 350 deg.C for 50 min; the sintering temperature is 620 ℃, the sintering heat preservation time is 30min, the furnace is cooled after the heat preservation is finished, and the cooling speed is controlled to reduce the temperature to the room temperature within 3h, so that the sintered part is obtained. The sintering environment for this step of sintering may preferably be less than 10ppm oxygen with a dew point of less than-40 ℃.
(4) And (3) performing solid solution and artificial aging heat treatment on the sintered piece in sequence, wherein the solid solution temperature is 460 ℃, the solid solution time is 6 hours, the artificial aging temperature is 100 ℃, and the artificial aging time is 8 hours.
Tests show that after being sintered, the 7075 aluminum alloy powder without the hydrogenated magnesium powder has the strength of 241MPa and the deformation amount of 1.70 percent; after 0.06% of magnesium hydride powder is added into 7075 aluminum alloy powder, the strength of the sintered 7075 aluminum alloy material obtained by magnesium hydride modified powder metallurgy is 238MPa, and the deformation reaches 0.92%.
Example 7:
in this embodiment, a method for preparing a powder metallurgy aluminum-based material is described by taking a high silicon aluminum alloy 4a11 aluminum alloy matrix as an example, and specifically includes the following steps:
(1) mixing powder: the raw material powder was obtained by mixing 4A11 aluminum alloy powder having an average particle size of 30 μm with magnesium hydride powder having an average particle size of 100 μm, wherein the mass fraction of the magnesium hydride powder in the raw material powder was 0.05%, and the balance was 4A11 aluminum alloy powder. Ball-milling the raw material powder for 6 hours on a planetary ball mill with the rotating speed of 125r/min, adding stearic acid accounting for 1.5 percent of the mass fraction of the raw material powder into the raw material powder 0.5 hour before the ball-milling is finished, and obtaining mixed powder after the ball-milling is finished. The magnesium hydride powder used in this step may preferably have a purity of 98%.
(2) Forming: and (2) carrying out die pressing forming on the powder obtained in the step (1), wherein the pressing pressure is 250MPa, and the pressure maintaining time is 10 s.
(3) And (3) sintering: sintering by adopting a tube furnace under the protective atmosphere of high-purity N2Dewaxing at 400 ℃ for 35 min; the sintering temperature is 610 ℃, the sintering heat preservation time is 50min, the furnace is cooled after the heat preservation is finished, and the cooling speed is controlled to reduce the temperature to the room temperature within 1h, so that the sintered part is obtained. The sintering environment for this step of sintering may preferably be less than 10ppm oxygen with a dew point of less than-40 ℃.
(4) And (3) heat treatment: and (3) sequentially carrying out solid solution and artificial aging heat treatment on the sintered piece, wherein the solid solution temperature is 525 ℃, the solid solution time is 1.5h, the artificial aging temperature is 175 ℃, and the artificial aging time is 10 h.
Through tests, the strength of the 4A11 aluminum alloy powder without the hydrogenated magnesium powder after sintering is 186MPa, and the deformation can reach 2.10%; after 0.05 percent of magnesium hydride powder is added into the 4A11 aluminum alloy powder, the strength of the sintered magnesium hydride modified powder metallurgy 4A11 aluminum alloy material is 179MPa, and the deformation reaches 1.43 percent.
Example 8:
in this embodiment, a method for preparing a powder metallurgy aluminum-based material is described by taking a high silicon aluminum alloy Al-10Si substrate as an example, and specifically includes the following steps:
(1) mixing powder: mixing Al-10Si aluminum alloy powder with the average grain diameter of 60 mu m and magnesium hydride powder with the average grain diameter of 62 mu m to obtain raw material powder, wherein the mass fraction of the magnesium hydride powder in the raw material powder is 0.6 percent, and the balance is Al-10Si aluminum alloy powder. Ball-milling the raw material powder for 6.5h on a planetary ball mill with the rotating speed of 90r/min, adding paraffin accounting for 1.5 percent of the mass fraction of the raw material powder into the raw material powder as a lubricant for 0.5h before the ball-milling is finished, and obtaining mixed powder after the ball-milling is finished. The magnesium hydride powder used in this step may preferably have a purity of 95%.
(2) Forming: and (2) carrying out die pressing forming on the powder obtained in the step (1), wherein the pressing pressure is 250MPa, and the pressure maintaining time is 10 s.
(3) And (3) sintering: sintering by adopting a mesh belt type continuous furnace, wherein the sintering protective atmosphere is high-purity N2Dewaxing at 380 deg.C for 40 min; the sintering temperature is 595 ℃, the sintering heat preservation time is 45min, furnace cooling is carried out after the heat preservation is finished, and the cooling speed is controlled to reduce the temperature to the room temperature within 3h, so that the sintered part is obtained. The sintering environment for this step of sintering may preferably be less than 10ppm oxygen with a dew point of less than-40 ℃.
(4) And (3) heat treatment: and sequentially carrying out solid solution and artificial aging heat treatment on the sintered piece, wherein the solid solution temperature is 520 ℃, the solid solution time is 2 hours, the artificial aging temperature is 170 ℃, and the artificial aging time is 10 hours.
Through tests, the strength of the Al-10Si aluminum alloy powder without the hydrogenated magnesium powder after sintering is 130MPa, and the deformation can reach 1.89%; after 0.6 percent of magnesium hydride powder is added into the Al-10Si aluminum alloy powder, the strength of the sintered magnesium hydride modified powder metallurgy Al-10Si aluminum alloy material is 105MPa, and the deformation reaches 0.84 percent.
Example 9:
this example is Al reinforced with ceramic particles2O3-2024 aluminum matrix composite matrix as an example, for powdersThe preparation method of the metallurgical aluminum-based material is explained, and specifically comprises the following steps:
(1) mixing powder: al having an average particle diameter of 85 μm2O3-2024 mixing the aluminum matrix composite powder with magnesium hydride powder having an average particle diameter of 15 μm to obtain a raw material powder, wherein the mass fraction of the magnesium hydride powder in the raw material powder is 0.85%, and the balance is Al2O3-2024 aluminum matrix composite powder. Ball-milling the raw material powder for 7 hours on a planetary ball mill with the rotating speed of 80r/min, adding zinc stearate accounting for 1% of the raw material powder by mass as a lubricant into the raw material powder 0.5 hour before the ball-milling is finished, and obtaining mixed powder after the ball-milling is finished. The magnesium hydride powder used in this step may preferably have a purity of 95%.
(2) Forming: and (2) carrying out die pressing forming on the powder obtained in the step (1), wherein the pressing pressure is 300MPa, and the pressure maintaining time is 20 s.
(3) And (3) sintering: sintering by adopting a mesh belt type continuous furnace, wherein the sintering protective atmosphere is high-purity N2The dewaxing temperature is 440 ℃, and the dewaxing time is 25 min; the sintering temperature is 580 ℃, the sintering heat preservation time is 40min, the furnace is cooled after the heat preservation is finished, and the cooling speed is controlled to reduce the temperature to the room temperature within 2h, so that the sintered part is obtained. The sintering environment for this step of sintering may preferably be less than 10ppm oxygen with a dew point of less than-40 ℃.
(4) And (3) heat treatment: and carrying out solid solution and artificial aging heat treatment on the sintered part, wherein the solid solution temperature is 490 ℃, the solid solution time is 1h, the artificial aging temperature is 190 ℃, and the artificial aging time is 20 h.
The Al of the unhydrogenated magnesium powder was tested2O3The strength of the-2024 powder after sintering is 226MPa, and the deformation can reach 1.50%; al (Al)2O3-2024 powder, adding 0.85% magnesium hydride powder, and sintering to obtain magnesium hydride modified Al2O3The strength of the-2024 aluminum matrix composite is 187MPa, and the deformation amount reaches 0.57%.
Example 10:
this example illustrates a method for preparing a powder metallurgy aluminum-based material by heat treating a non-strengthenable 3003 aluminum alloy substrate, which specifically comprises the following steps:
(1) mixing powder: a3003 aluminum alloy powder having an average particle size of 70 μm and a magnesium hydride powder having an average particle size of 70 μm were mixed to obtain a raw material powder, wherein the mass fraction of the magnesium hydride powder in the raw material powder was 1.2%, and the balance was the 3003 aluminum alloy powder. Ball-milling the raw material powder for 9 hours on a planetary ball mill with the rotating speed of 70r/min, adding paraffin accounting for 1.5 percent of the mass fraction of the raw material powder into the raw material powder as a lubricant for 0.5 hour before the ball-milling is finished, and obtaining mixed powder after the ball-milling is finished. The magnesium hydride powder used in this step may preferably have a purity of 98%.
(2) And (3) forming, namely performing die pressing forming on the product obtained in the step (1), wherein the pressing pressure is 500MPa, and the pressure maintaining time is 10 s.
(3) And (3) sintering: sintering by adopting a push rod type continuous furnace in a protective atmosphere of high-purity N2Dewaxing at 400 deg.C for 30 min; the sintering temperature is 570 ℃, the sintering heat preservation time is 40min, furnace cooling is carried out after the heat preservation is finished, and the cooling speed is controlled to reduce the temperature to the room temperature within 3h, so that the sintered part is obtained. The sintering environment for this step of sintering may preferably be less than 10ppm oxygen with a dew point of less than-40 ℃. As shown in FIG. 2, the sintered part of the magnesium hydride modified powder metallurgy 3003 aluminum alloy material realizes good metallurgical bonding and has higher mechanical property.
Tests show that the strength of the 3003 aluminum alloy powder without the hydrogenated magnesium powder after sintering is 112MPa, and the deformation can reach 0.80%; after 1.2 percent of magnesium hydride powder is added into the 3003 aluminum alloy powder, the strength of the sintered magnesium hydride modified 3003 aluminum alloy material is 83MPa, and the deformation reaches 0.39 percent.
Claims (8)
1. A preparation method of powder metallurgy aluminum-based material is characterized by comprising the following steps:
(a) mixing powder: uniformly mixing aluminum matrix powder and magnesium hydride powder according to the component proportion to obtain raw material powder; the raw material powder comprises 0.001-3% of magnesium hydride powder by mass percentage, and the balance of aluminum matrix powder, wherein the aluminum matrix powder is aluminum simple substance powder or aluminum alloy powder or aluminum matrix composite powder;
(b) forming: pressing and forming the powder obtained in the step (a) to obtain a blank body;
(c) and (3) sintering: sintering the green body obtained in the step (b) in a protective atmosphere to obtain a sintered part; the sintering temperature is 550-660 ℃, and the heat preservation time is 5-60 min;
(d) and (3) heat treatment: sequentially carrying out solid solution treatment and artificial aging heat treatment on the sintered piece obtained in the step (c);
and (d) not performing the step (d) on the sintered part which is a pure aluminum matrix or an aluminum alloy matrix which cannot be strengthened by heat treatment.
2. The method of preparing a powder metallurgy aluminum-based material of claim 1, wherein: the mass percentage of the magnesium hydride powder is 0.06% -0.85%.
3. The method of preparing a powder metallurgy aluminum-based material of claim 1 or 2, wherein: the purity of the magnesium hydride powder is 90-98%.
4. The method of preparing a powder metallurgy aluminum-based material of claim 1, wherein: in the powder mixing process of the step (a), a lubricant is added into the raw material powder, wherein the lubricant accounts for 0.5-2% of the raw material powder by mass.
5. The method of preparing a powder metallurgy aluminum-based material of claim 1, wherein: the solid solution temperature of the solid solution treatment in the step (d) is 450-580 ℃, the solid solution time is 0.5-6 h, the artificial aging temperature is 100-200 ℃, and the artificial aging time is 3-24 h.
6. The method of preparing a powder metallurgy aluminum-based material of claim 1, wherein: dewaxing the blank before sintering in the step (c), wherein the dewaxing temperature is 350-450 ℃, and the dewaxing time is 20-50 min.
7. The method of preparing a powder metallurgy aluminum-based material of claim 1, wherein: the aluminum matrix powder has an average particle size of 30 to 100 μm, and the magnesium hydride powder has an average particle size of 0.1 to 100 μm.
8. The method of preparing a powder metallurgy aluminum-based material of claim 1, wherein: and (b) mixing the mixed powder in the step (a) by adopting a ball mill, wherein the rotating speed of the ball mill is 50-140 r/min, and the ball milling time is 5-10 h.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201910478418.6A CN110142402B (en) | 2019-06-03 | 2019-06-03 | Powder metallurgy aluminum-based material and preparation method thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201910478418.6A CN110142402B (en) | 2019-06-03 | 2019-06-03 | Powder metallurgy aluminum-based material and preparation method thereof |
Publications (2)
Publication Number | Publication Date |
---|---|
CN110142402A CN110142402A (en) | 2019-08-20 |
CN110142402B true CN110142402B (en) | 2022-01-25 |
Family
ID=67590267
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201910478418.6A Active CN110142402B (en) | 2019-06-03 | 2019-06-03 | Powder metallurgy aluminum-based material and preparation method thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN110142402B (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112828292A (en) * | 2021-01-05 | 2021-05-25 | 西安交通大学 | Powder metallurgy duplex gear manufacturing and processing method |
CN113564398A (en) * | 2021-07-06 | 2021-10-29 | 北京科技大学 | Preparation method of powder metallurgy lithium-containing aluminum-based composite material added with sintering activator |
CN113637881A (en) * | 2021-07-13 | 2021-11-12 | 海安金隆金属科技有限公司 | Aluminum alloy for mountain bicycle frame tube and preparation method thereof |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5972285A (en) * | 1997-06-10 | 1999-10-26 | Th. Goldschmidt Ag | Foamable metal articles |
JP2008527167A (en) * | 2005-01-10 | 2008-07-24 | ハー ツェー シュタルク ゲゼルシャフト ミット ベシュレンクテル ハフツング ウント コンパニー コマンデイトゲゼルシヤフト | Metal powder mixture |
CN103436759A (en) * | 2013-09-10 | 2013-12-11 | 株洲硬质合金集团有限公司 | Zr element-toughened WC-Ni3Al hard alloy and preparation method thereof |
CN104294070A (en) * | 2014-11-11 | 2015-01-21 | 安徽工业大学 | Method for preparing aluminum alloy containing magnesium through low temperature sintering |
CN106191493A (en) * | 2016-07-15 | 2016-12-07 | 湖南大学 | A kind of preparation method of powder metallurgy titanium alloy |
CN106498211A (en) * | 2016-11-29 | 2017-03-15 | 华南理工大学 | The preparation method of the steady nanometer phase composite construction Al Sn alloys of nano alumina particles In-sltu reinforcement hyperpyrexia |
CN109763012A (en) * | 2019-01-22 | 2019-05-17 | 山东理工大学 | The preparation method of flux foaming enhancing foamed aluminium composite foamable agent |
-
2019
- 2019-06-03 CN CN201910478418.6A patent/CN110142402B/en active Active
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5972285A (en) * | 1997-06-10 | 1999-10-26 | Th. Goldschmidt Ag | Foamable metal articles |
JP2008527167A (en) * | 2005-01-10 | 2008-07-24 | ハー ツェー シュタルク ゲゼルシャフト ミット ベシュレンクテル ハフツング ウント コンパニー コマンデイトゲゼルシヤフト | Metal powder mixture |
CN103436759A (en) * | 2013-09-10 | 2013-12-11 | 株洲硬质合金集团有限公司 | Zr element-toughened WC-Ni3Al hard alloy and preparation method thereof |
CN104294070A (en) * | 2014-11-11 | 2015-01-21 | 安徽工业大学 | Method for preparing aluminum alloy containing magnesium through low temperature sintering |
CN106191493A (en) * | 2016-07-15 | 2016-12-07 | 湖南大学 | A kind of preparation method of powder metallurgy titanium alloy |
CN106498211A (en) * | 2016-11-29 | 2017-03-15 | 华南理工大学 | The preparation method of the steady nanometer phase composite construction Al Sn alloys of nano alumina particles In-sltu reinforcement hyperpyrexia |
CN109763012A (en) * | 2019-01-22 | 2019-05-17 | 山东理工大学 | The preparation method of flux foaming enhancing foamed aluminium composite foamable agent |
Also Published As
Publication number | Publication date |
---|---|
CN110142402A (en) | 2019-08-20 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN110142402B (en) | Powder metallurgy aluminum-based material and preparation method thereof | |
CN110273092B (en) | CoCrNi particle reinforced magnesium-based composite material and preparation method thereof | |
CN110358941B (en) | Tungsten-based alloy material and preparation method thereof | |
CN109023013B (en) | Preparation method of corrosion-resistant high-strength AlCoCrFeNi-Cu high-entropy alloy | |
CN110257684B (en) | Preparation process of FeCrCoMnNi high-entropy alloy-based composite material | |
CN108251695B (en) | Preparation method of titanium-aluminum-niobium-zirconium-molybdenum alloy | |
CN111118325B (en) | Preparation method of fine-grain niobium-titanium alloy | |
CN108504916B (en) | High-wear-resistance tungsten alloy powder metallurgy material for precision instrument and preparation method thereof | |
CN106967900A (en) | A kind of titanium-based metal glass particle reinforced aluminum matrix composites and preparation method thereof | |
CN110216276B (en) | Powder metallurgy aluminum-based material and preparation method thereof | |
CN111471896B (en) | Preparation method of nano hafnium oxide reinforced NiAl composite material | |
CN113333752A (en) | Titanium and titanium alloy injection molding feed product and preparation method thereof | |
CN110216275B (en) | Powder metallurgy aluminum-based material and preparation method thereof | |
CN110184487B (en) | Powder metallurgy aluminum-based material and preparation method thereof | |
CN110157930B (en) | Powder metallurgy aluminum-based material and preparation method thereof | |
CN110983152B (en) | Fe-Mn-Si-Cr-Ni based shape memory alloy and preparation method thereof | |
CN113385856A (en) | Ternary boride Mo2NiB2Alloy welding material and production process thereof | |
CN113604720B (en) | Large-size deformation-resistant molybdenum alloy bar and preparation method thereof | |
CN114959379B (en) | Heat-resistant high-strength aluminum alloy suitable for selective laser melting and preparation method thereof | |
CN114605158A (en) | Nitride composite refractory material for titanium alloy smelting and preparation method thereof | |
CN112941391B (en) | NbC-containing high-density composite metal ceramic material and preparation method thereof | |
CN110484786B (en) | High-densification core-shell structure particle reinforced Al-based composite material and preparation method thereof | |
CN109487124B (en) | Aluminum-based wear-resistant material under sulfur-containing corrosion working condition and preparation method thereof | |
CN113957294A (en) | CrCoNi intermediate entropy alloy reinforced Al-based composite material and preparation method thereof | |
US20190185974A1 (en) | Method for Preparing Nano-SiO2 Reinforced Aluminum Matrix Composites |
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 | ||
CB02 | Change of applicant information |
Address after: No. 1508, Jingjiang Road, Yinzhou Industrial Park, Ningbo City, Zhejiang Province Applicant after: MBTM New Materials Group Co.,Ltd. Address before: 315191 No.8 Jingjiang Road, Yinzhou Industrial Park, Ningbo, Zhejiang Province Applicant before: MBTM New Materials Group Co.,Ltd. |
|
CB02 | Change of applicant information | ||
GR01 | Patent grant | ||
GR01 | Patent grant |