CN111872386B - 3D printing process method of high-strength aluminum-magnesium alloy - Google Patents
3D printing process method of high-strength aluminum-magnesium alloy Download PDFInfo
- Publication number
- CN111872386B CN111872386B CN202010616674.XA CN202010616674A CN111872386B CN 111872386 B CN111872386 B CN 111872386B CN 202010616674 A CN202010616674 A CN 202010616674A CN 111872386 B CN111872386 B CN 111872386B
- Authority
- CN
- China
- Prior art keywords
- printing
- magnesium alloy
- aluminum
- powder
- strength aluminum
- 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
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F1/00—Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
- B22F1/06—Metallic powder characterised by the shape of the particles
- B22F1/065—Spherical particles
-
- 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
-
- 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
- B22F9/06—Making metallic powder or suspensions thereof using physical processes starting from liquid material
- B22F9/08—Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying
- B22F9/082—Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying atomising using a fluid
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B33—ADDITIVE MANUFACTURING TECHNOLOGY
- B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
- B33Y10/00—Processes of additive manufacturing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B33—ADDITIVE MANUFACTURING TECHNOLOGY
- B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
- B33Y50/00—Data acquisition or data processing for additive manufacturing
- B33Y50/02—Data acquisition or data processing for additive manufacturing for controlling or regulating additive manufacturing processes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B33—ADDITIVE MANUFACTURING TECHNOLOGY
- B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
- B33Y70/00—Materials specially adapted for additive manufacturing
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
- C22C21/08—Alloys based on aluminium with magnesium as the next major constituent with silicon
-
- 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
-
- 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)
- Materials Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Nanotechnology (AREA)
- Powder Metallurgy (AREA)
Abstract
The invention relates to a 3D printing process method of a high-strength aluminum-magnesium alloy, and belongs to the technical field of 3D printing. Firstly, heating and melting a high-strength aluminum-magnesium alloy raw material to uniformly mix the raw material; then preparing high-quality aluminum-magnesium alloy powder from the molten high-strength aluminum-magnesium alloy by adopting an air atomization technology, and drying to obtain aluminum-magnesium alloy powder for 3D printing; and adjusting printing parameters, and performing 3D printing in a printing device filled with inert gas according to the three-dimensional model data of the part to obtain a 3D printing product taking the high-strength aluminum-magnesium alloy as the raw material. Compared with the prior art, the relative density of the product printed by the process method can reach more than 99 percent, the Vickers hardness can reach more than 110HV, the tensile strength can reach more than 430MPa, the elongation can reach 21 percent, the Vickers hardness of the sample can reach more than 150HV through proper heat treatment, the tensile strength can be further improved to more than 520MPa, and the elongation can be kept at 17 percent or more.
Description
Technical Field
The invention belongs to the technical field of 3D printing, and particularly relates to a 3D printing process method of a high-strength aluminum-magnesium alloy.
Background
The 3D printing is a preparation technology for obtaining a product with a complex shape by using three-dimensional model data in a layer-by-layer accumulation mode. Compared with the traditional preparation method of plastics, ceramics, metals, alloys and composite materials, the 3D printing technology has a series of advantages of being capable of preparing products with high precision and complex shapes, saving raw materials, saving cost and the like, and has good application prospects. Currently, common 3D printing methods include direct three-dimensional printing and forming technology (3DP), selective laser melting technology (SLM), stereo light curing technology (SLA), fused deposition technology (FDM), etc., wherein the selective laser melting technology (SLM) is widely applied to 3D printing of metal powder. The metals and alloys which can be used for SLM at present mainly comprise stainless steel, titanium alloy, aluminum alloy and the like, and are mainly applied to aerospace and automobile industries.
The aluminum alloy is a material which is widely concerned in the 3D printing manufacturing technology, has the characteristics of light weight, low melting point, high plasticity and the like, the weight density of the aluminum is 1.7 times lighter than that of the titanium, and the total weight of parts can be greatly reduced by using the aluminum alloy, so the aluminum alloy has wide application prospects in the automobile lightweight and aerospace industries. However, there are still many technical difficulties in producing aluminum alloys by selective laser melting methods: higher laser radiation power is required compared to titanium or steel SLM due to the high thermal conductivity and reflectivity of aluminum and aluminum alloys. The aluminum alloy powder is easily oxidized, and the sintering of the powder particles is prevented by an oxide film on the powder particles, so that the printed product may have a high porosity. Also because of these technical difficulties, none of the currently SLM printed aluminum alloys have high strength, even up to cast aluminum alloys of the same composition, but at a much higher cost than the latter. Therefore, although the industry has a high interest in 3D printing aluminum alloy, the 3D printing aluminum alloy products in the market are limited, and most aluminum alloy parts are produced by traditional processes such as casting.
Currently, a great deal of aluminum-silicon alloys with better casting performance, such as AlSi10Mg, AlSi12 and the like, are used for 3D printing of aluminum alloys. The aluminum-silicon alloy prepared by the SLM technology has the highest tensile strength of about 450MPa, the elongation of about 4 percent, moderate tensile strength and low elongation. Wrought aluminum alloys with higher strength and better ductility often suffer from a large number of cracks during SLM processing, resulting in poor product performance far from comparable to conventionally manufactured aluminum alloys. At present, ductility of the aluminum-silicon alloy prepared by SLM is slightly increased after heat treatment, but tensile property is greatly reduced, the effect of heat treatment on performance improvement is limited, and fine microstructure of the aluminum-silicon alloy is damaged to cause performance reduction. Aiming at the current research situation of the SLM aluminum alloy, designing and optimizing the special SLM aluminum alloy is an effective way for preparing the high-performance aluminum alloy through the SLM.
Researches find that rare earth elements such as Sc and the like are added into the alloy, so that the cracking problem of the wrought aluminum alloy caused by high cooling rate in the SLM process can be effectively solved, and a product with a smooth surface and no cracks is prepared. Meanwhile, Sc can also form nano Al3And the Sc precipitates further improve the strength of the SLM aluminum alloy. However, the rare earth element content is low, the price is high, and the large-scale popularization and application are not facilitated.
Disclosure of Invention
The invention aims to provide a 3D printing process method of a high-strength aluminum-magnesium alloy.
The invention relates to a 3D printing process method for obtaining a near-compact crack-free high-strength aluminum-magnesium alloy product by controlling the powder quality, adjusting the printing parameters and improving the printing and heat treatment processes.
The purpose of the invention can be realized by the following technical scheme:
the invention provides a 3D printing process method of a high-strength aluminum-magnesium alloy, which comprises the following steps of:
heating and melting the high-strength aluminum-magnesium alloy raw material to uniformly mix the raw material;
preparing high-quality aluminum-magnesium alloy powder from the molten high-strength aluminum-magnesium alloy by adopting a gas atomization technology, and drying to obtain aluminum-magnesium alloy powder for 3D printing;
and adjusting printing parameters, and performing 3D printing in a printing device filled with inert gas according to the three-dimensional model data of the part to obtain a 3D printing product taking the high-strength aluminum-magnesium alloy as the raw material.
In one embodiment of the present invention, the chemical composition of the aluminum magnesium alloy powder for 3D printing is: mg content of 1.00-8.00 wt%, Zr content of 0.10-3.00 wt%, Si content of 0.05-2.00 wt%, Mn content of 0.01-2.00 wt%, Zn content of 0.01-1.50 wt%, and the rest is Al.
In one embodiment of the present invention, the aluminum magnesium alloy powder for 3D printing has a particle size of 10 to 60 μm, 90% or more of the powder particles are spherical or spheroidal, the powder particles have uniform size and good flowability, and are not oxidized during the preparation process, so that the powder quality is excellent.
In one embodiment of the invention, the gas atomization technology refers to gas atomization by using a supersonic atomizing nozzle combining a laval structure and a hartmann structure. The specific structure of the supersonic atomizing nozzle combining the laval and hartmann structures can refer to the supersonic atomizing nozzle combining the laval and hartmann structures disclosed in chinese patent CN201410553284.7, the supersonic atomizing nozzle combining the two-stage laval and hartmann structures disclosed in chinese patent CN201410553271.x, and the supersonic atomizing nozzle combining the single-stage laval and hartmann structures disclosed in chinese patent CN 201410553799.7.
In one embodiment of the invention, the inert gas is selected from high purity argon.
In one embodiment of the invention, the 3D printing method is Selective Laser Melting (SLM), the printing apparatus is SLM printing apparatus, and includes a laser generation device and a chamber containing a powder cylinder and a forming cylinder, the chamber is sealed during printing, an inert gas is introduced to prevent the powder from being oxidized during sintering as much as possible after the oxygen content in the chamber is lower than 0.2%, the substrate subjected to sand blasting is preheated by laser, selective laser sintering is performed according to a three-dimensional model of a part, the diameter of a laser beam spot selected for sintering is 40-70 μm, and then the printing of the product is started.
In one embodiment of the present invention, the drying is performed for 5 to 24 hours under vacuum.
In one embodiment of the invention, during printing, the powder spreading layer thickness of the first 0-3 layers is 0, at this time, the laser repeatedly scans the substrate for preheating, and then powder spreading printing is started according to the three-dimensional model of the part; the adjusted printing parameters are set to be that the laser power is between 150W and 500W, the scanning speed is between 200 and 1800mm/s, the printing layer thickness is 20 to 60 mu m, the scanning interval is 100 and 180 mu m, and the scanning strategy is a checkerboard or a bar.
In one embodiment of the invention, the 3D printed product printed from the high strength aluminum magnesium alloy is heat treated to further improve performance by solid solution strengthening and/or precipitation strengthening.
In one embodiment of the present invention, the heat treatment is selected from aging or annealing at 100-.
The relative density of the product printed by the process method can reach more than 99 percent, the Vickers hardness can reach more than 110HV, the tensile strength can reach more than 430MPa, the elongation can reach 21 percent, the Vickers hardness of the sample can reach more than 150HV through proper heat treatment, the tensile strength can be further improved to more than 520MPa, and the elongation can be kept at 17 percent or more.
Compared with the prior art, the invention has the beneficial effects that:
(1) the invention adopts the self-made gas atomization aluminum magnesium alloy powder, can obtain high-quality 3D printing metal powder in a large scale at low cost, is beneficial to improving the performance of the product and promotes the wider application of the product.
(2) The aluminum-magnesium alloy powder raw material used by the invention is added with a small amount of Zr element, and can form fine Al in the aluminum-magnesium alloy3Zr deposition is close to deposition containing Sc, which can improve SLM performance of alloy, reduce generation of hot crack, refine microstructure of SLM product, and improve strength and ductility (existing research shows that adding Sc forms Al3Sc,Al3Zr acts like this, Al3More than 20 interfaces of Zr and the main face-centered cubic aluminum phase are matched, and the crystal lattice mismatch and the atomic density change are less than 0.52 percent and less than 1 percent, so that ideal low-energy heterogeneous nucleation sites are provided, the supercooling critical quantity required by the growth of equiaxed grains is reduced by providing high-density low-barrier heterogeneous nucleation sites at the solidification front, the formation of fine equiaxed grain tissues is facilitated, and the generation of columnar grains which easily cause thermal cracks is reduced. Al (Al)3Zr particles are homogeneously bonded toIn the structure, due to the pinning effect, the strength can be improved, the grain growth is hindered, the strength and the ductility of a printed product are improved due to the generation of fine equiaxed grains and the reduction of hot cracks), the effects of Sc and Zr in the aspect of improving the alloy performance are similar, but the Sc is more expensive, so that the powder cost is reduced by replacing Sc with Zr;
(3) the raw materials of the aluminum magnesium alloy powder used in the invention also contain Mg, Si, Zn and Mn elements, in the SLM process, the solid solubility in Al is increased, and the lattice distortion is increased due to the increase of the solid solubility of other elements in the Al phase, so that the dislocation is more strongly hindered, and the strength and the hardness of the aluminum magnesium alloy are further improved;
in addition, the Si element has small linear expansion coefficient and can improve the fluidity of alloy liquid, the melting temperature can be reduced by adding the element into the aluminum magnesium alloy, the solidification shrinkage rate of the alloy is reduced, the thermal expansion coefficient is reduced, the fluidity is improved, the crack sensitivity is favorably reduced, and the SLM (melt extrusion) processability of the aluminum magnesium alloy can be favorably improved by adding a proper amount of Si for producing compact crack-free aluminum magnesium alloy. Moreover, the alloy can generate precipitates in the heat treatment process, and the performance of the alloy is further improved through precipitation strengthening;
(4) the invention controls the powder particle size to be within the range of 10-60 mu m in the SLM printing process, ensures the powder particles to have high sphericity, controls the powder particle size range and the spherical shape, ensures the powder to have good fluidity and is convenient for uniformly spreading the powder in the SLM printing process; the powder contains water, hydrogen pores can be formed, the bonding condition of the powder and a matrix is deteriorated after the powder is oxidized, impurities are easy to form and the like, so that the invention controls the powder particles to have the lowest possible water content, and simultaneously sintering is carried out under the condition of lower oxygen content, thereby avoiding the powder oxidation as much as possible. The series of measures can effectively reduce the generation of defects such as holes, cracks and the like and improve the mechanical properties such as the strength of printed products.
(5) According to the invention, by continuously adjusting the printing parameters, the generation of defects such as holes and cracks is reduced, the high-strength aluminum magnesium alloy is printed, the obtained aluminum magnesium alloy has compact structure and excellent mechanical property, and meanwhile, the complex post-treatment process is reduced, the energy is saved, and the cost is reduced. The method is also suitable for printing complex aluminum magnesium alloy parts and has obvious technical advantages.
(6) The invention can adjust the microstructure of the aluminum magnesium alloy by continuously adjusting the printing process parameters, particularly change the grain size of the alloy, and the refined grains can further improve the properties of the alloy, such as strength and the like.
Detailed Description
The invention provides a 3D printing process method of a high-strength aluminum-magnesium alloy, which comprises the following steps of:
heating and melting the high-strength aluminum-magnesium alloy raw material to uniformly mix the raw material;
preparing high-quality aluminum-magnesium alloy powder from the molten high-strength aluminum-magnesium alloy by adopting a gas atomization technology, and drying to obtain aluminum-magnesium alloy powder for 3D printing;
and adjusting printing parameters, and performing 3D printing in a printing device filled with inert gas according to the three-dimensional model data of the part to obtain a 3D printing product taking the high-strength aluminum-magnesium alloy as the raw material.
In one embodiment of the present invention, the chemical composition of the aluminum magnesium alloy powder for 3D printing is: mg content of 1.00-8.00 wt%, Zr content of 0.10-3.00 wt%, Si content of 0.05-2.00 wt%, Mn content of 0.01-2.00 wt%, Zn content of 0.01-1.50 wt%, and the rest is Al.
In one embodiment of the present invention, the aluminum magnesium alloy powder for 3D printing has a particle size of 10 to 60 μm, 90% or more of the powder particles are spherical or spheroidal, the powder particles have uniform size and good flowability, and are not oxidized during the preparation process, so that the powder quality is excellent.
In one embodiment of the invention, the gas atomization technology refers to gas atomization by using a supersonic atomizing nozzle combining a laval structure and a hartmann structure. The specific structure of the supersonic atomizing nozzle combining the laval and hartmann structures can refer to the supersonic atomizing nozzle combining the laval and hartmann structures disclosed in chinese patent CN201410553284.7, the supersonic atomizing nozzle combining the two-stage laval and hartmann structures disclosed in chinese patent CN201410553271.x, and the supersonic atomizing nozzle combining the single-stage laval and hartmann structures disclosed in chinese patent CN 201410553799.7.
In one embodiment of the invention, the inert gas is selected from high purity argon.
In one embodiment of the invention, the 3D printing method is Selective Laser Melting (SLM), the printing apparatus is SLM printing apparatus, and includes a laser generation device and a chamber containing a powder cylinder and a forming cylinder, the chamber is sealed during printing, an inert gas is introduced to prevent the powder from being oxidized during sintering as much as possible after the oxygen content in the chamber is lower than 0.2%, the substrate subjected to sand blasting is preheated by laser, selective laser sintering is performed according to a three-dimensional model of a part, the diameter of a laser beam spot selected for sintering is 40-70 μm, and then the printing of the product is started.
In one embodiment of the present invention, the drying is performed for 5 to 24 hours under vacuum.
In one embodiment of the invention, during printing, the powder spreading layer thickness of the first 0-3 layers is 0, at this time, the laser repeatedly scans the substrate for preheating, and then powder spreading printing is started according to the three-dimensional model of the part; the adjusted printing parameters are set to be that the laser power is between 150W and 500W, the scanning speed is between 200 and 1800mm/s, the printing layer thickness is 20 to 60 mu m, the scanning interval is 100 and 180 mu m, and the scanning strategy is a checkerboard or a bar.
In one embodiment of the invention, the 3D printed product printed from the high strength aluminum magnesium alloy is heat treated to further improve performance by solid solution strengthening and/or precipitation strengthening.
In one embodiment of the present invention, the heat treatment is selected from aging or annealing at 100-.
The present invention will be described in detail with reference to specific examples.
Example 1
Carrying out gas atomization to obtain aluminum magnesium alloy powder, wherein the aluminum magnesium alloy powder comprises the following chemical components: mg content 5.72 wt%, Zr content 1.48 wt%, Si content 1.24 wt%, Mn content 0.62 wt%, Zn content 0.43 wt%, and the balance Al. The average particle diameter of the powder is 25.95 μm, more than 90% of the powder particles are spherical or spheroidal, and the powder has good fluidity. The powder is dried in a vacuum drying oven at 70 ℃ for 12 hours, then the powder is added into a cavity of a Hanbang HBD-SLM100 printer (the diameter of a laser beam spot is about 50 mu m), high-purity argon is introduced to enable the oxygen content in the cavity to be lower than 0.1%, then laser scanning is carried out for 2 times to preheat a substrate, and then powder spreading and printing are carried out according to a three-dimensional model of a part. The printing parameters are set to be 200W of laser power, 750mm/s of scanning speed, 30 mu m of printing layer thickness, 130 mu m of scanning interval and checkerboard scanning strategy. The printed sample has smooth surface without cracks, the relative density is more than 99.6 percent, the average Vickers hardness is 114HV, the tensile strength at room temperature is about 435MPa, and the elongation is about 21 percent. And carrying out heat treatment on the obtained sample, carrying out aging treatment at 400 ℃ for 12h, and then carrying out air cooling, wherein the Vickers hardness average value of the heat-treated sample is increased to 153HV, the tensile strength is increased to 526MPa, and the elongation is about 17%. Compared with other common SLM aluminum alloys, the prepared aluminum-magnesium alloy has certain advantages in strength and ductility, and can further improve the performance through heat treatment, so that the use requirement on the aluminum alloy under most conditions can be met, the complex post-treatment process of the wrought aluminum alloy is reduced, and the energy and the cost are saved.
Example 2
The embodiment provides a 3D printing process method of a high-strength aluminum-magnesium alloy, which comprises the following steps:
heating and melting high-strength aluminum-magnesium alloy raw materials (chemical composition: Mg content is 4.00 wt%, Zr content is 1.50 wt%, Si content is 1.00 wt%, Mn content is 1.00 wt%, Zn content is 1.00 wt%, and the balance is Al) to uniformly mix;
preparing high-quality aluminum-magnesium alloy powder from a molten high-strength aluminum-magnesium alloy by adopting a gas atomization technology, and drying the high-quality aluminum-magnesium alloy powder for 15 hours in vacuum to obtain the aluminum-magnesium alloy powder for 3D printing, wherein the particle size of the aluminum-magnesium alloy powder for 3D printing is 10-60 mu m, more than 90% of powder particles are spherical or spheroidal, the powder particles are uniform in size and good in flowability, and cannot be oxidized in the preparation process, and the powder quality is excellent;
adjusting printing parameters, performing 3D printing according to three-dimensional model data of a part in printing equipment with high-purity argon gas introduced, wherein the 3D printing method is Selective Laser Melting (SLM), the printing equipment is SLM printing equipment and comprises a laser generating device and a cavity containing a powder cylinder and a forming cylinder, the cavity is closed during printing, inert gas is introduced to prevent powder from being oxidized during sintering as much as possible after the oxygen content in the cavity is lower than 0.2%, the substrate subjected to sand blasting treatment is preheated by laser, selective laser sintering is performed according to the three-dimensional model of the part, the diameter of a laser beam spot selected for sintering is 55 mu m, printing of a product is started, the powder spreading layer thickness of the first 0-3 layers is 0 during printing, the laser scans the substrate repeatedly for preheating at the moment, and then powder spreading and printing are started according to the three-dimensional model of the part; the adjusted printing parameters are set to be that the laser power is 350W, the scanning speed is 1000mm/s, the printing layer thickness is 40 mu m, the scanning interval is 140 mu m, and the scanning strategy is a checkerboard or a strip, so that the 3D printing product taking the high-strength aluminum-magnesium alloy as the raw material is obtained.
In this embodiment, the atomization technique is atomization using a supersonic atomizing nozzle with a laval and hartmann structure. The specific structure of the supersonic atomizing nozzle combining the laval structure and the hartmann structure can refer to the supersonic atomizing nozzle combining the laval structure and the hartmann structure disclosed in chinese patent CN 201410553284.7.
In the embodiment, the 3D printed product with the high-strength aluminum-magnesium alloy as the raw material is subjected to heat treatment, wherein the heat treatment is performed by aging or annealing at 200 ℃ for 50 hours, and the performance is further improved by solid solution strengthening and/or precipitation strengthening.
Example 3
The embodiment provides a 3D printing process method of a high-strength aluminum-magnesium alloy, which comprises the following steps:
heating and melting high-strength aluminum-magnesium alloy raw materials (chemical composition: Mg content is 1.00 wt%, Zr content is 3.00 wt%, Si content is 0.05 wt%, Mn content is 2.00 wt%, Zn content is 0.01 wt%, and the balance is Al) to uniformly mix;
preparing high-quality aluminum-magnesium alloy powder from a molten high-strength aluminum-magnesium alloy by adopting a gas atomization technology, and drying the high-quality aluminum-magnesium alloy powder for 5 hours in vacuum to obtain the aluminum-magnesium alloy powder for 3D printing, wherein the particle size of the aluminum-magnesium alloy powder for 3D printing is 10-60 mu m, more than 90% of powder particles are spherical or spheroidal, the powder particles are uniform in size and good in flowability, and cannot be oxidized in the preparation process, and the powder quality is excellent;
adjusting printing parameters, performing 3D printing according to three-dimensional model data of a part in printing equipment with high-purity argon gas introduced, wherein the 3D printing method is Selective Laser Melting (SLM), the printing equipment is SLM printing equipment and comprises a laser generating device and a cavity containing a powder cylinder and a forming cylinder, the cavity is closed during printing, inert gas is introduced to prevent powder from being oxidized during sintering as much as possible after the oxygen content in the cavity is lower than 0.2%, the substrate subjected to sand blasting treatment is preheated by laser, selective laser sintering is performed according to the three-dimensional model of the part, the diameter of a laser beam spot selected for sintering is 40 mu m, printing of a product is started, the powder spreading layer thickness of the first 0-3 layers is 0 during printing, the laser scans the substrate repeatedly for preheating at the moment, and then powder spreading and printing are started according to the three-dimensional model of the part; the adjusted printing parameters are set to be that the laser power is 150W, the scanning speed is 200mm/s, the printing layer thickness is 20 micrometers, the scanning interval is 100 micrometers, and the scanning strategy is checkerboard or bar-shaped, so that the 3D printing product taking the high-strength aluminum-magnesium alloy as the raw material is obtained.
In this embodiment, the atomization technique is atomization using a supersonic atomizing nozzle with a laval and hartmann structure. The specific structure of the supersonic atomizing nozzle fusing the laval structure and the hartmann structure can refer to the supersonic atomizing nozzle fusing the secondary laval structure and the hartmann structure disclosed in chinese patent No. cn201410553271.
In the embodiment, the 3D printed product with the high-strength aluminum-magnesium alloy as the raw material is subjected to heat treatment, wherein the heat treatment is selected from aging treatment or annealing treatment at 100 ℃ for 200 hours, and the performance is further improved through solid solution strengthening and/or precipitation strengthening.
Example 4
The embodiment provides a 3D printing process method of a high-strength aluminum-magnesium alloy, which comprises the following steps:
heating and melting high-strength aluminum-magnesium alloy raw materials (chemical composition: Mg content 8.00 wt%, Zr content 0.10 wt%, Si content 2.00 wt%, Mn content 0.01 wt%, Zn content 1.50 wt%, and the balance of Al) to uniformly mix;
preparing high-quality aluminum-magnesium alloy powder from a molten high-strength aluminum-magnesium alloy by adopting a gas atomization technology, and drying the high-quality aluminum-magnesium alloy powder in vacuum for 24 hours to obtain the aluminum-magnesium alloy powder for 3D printing, wherein the particle size of the aluminum-magnesium alloy powder for 3D printing is 10-60 mu m, more than 90% of powder particles are spherical or spheroidal, the powder particles are uniform in size and good in flowability, and cannot be oxidized in the preparation process, and the powder quality is excellent;
adjusting printing parameters, performing 3D printing according to three-dimensional model data of a part in printing equipment with high-purity argon gas introduced, wherein the 3D printing method is Selective Laser Melting (SLM), the printing equipment is SLM printing equipment and comprises a laser generating device and a cavity containing a powder cylinder and a forming cylinder, the cavity is closed during printing, inert gas is introduced to prevent powder from being oxidized during sintering as much as possible after the oxygen content in the cavity is lower than 0.2%, the substrate subjected to sand blasting treatment is preheated by laser, selective laser sintering is performed according to the three-dimensional model of the part, the diameter of a laser beam spot selected for sintering is 70 mu m, printing of a product is started, the powder spreading layer thickness of the first 0-3 layers is 0 during printing, the laser scans the substrate repeatedly for preheating at the moment, and then powder spreading and printing are started according to the three-dimensional model of the part; the adjusted printing parameters are set to be that the laser power is 500W, the scanning speed is 1800mm/s, the printing layer thickness is 60 mu m, the scanning interval is 180 mu m, and the scanning strategy is a checkerboard or a bar shape, so that the 3D printing product taking the high-strength aluminum-magnesium alloy as the raw material is obtained.
In this embodiment, the atomization technique is atomization using a supersonic atomizing nozzle with a laval and hartmann structure. The specific structure of the supersonic atomizing nozzle combining the laval structure and the hartmann structure can refer to the supersonic atomizing nozzle combining the laval structure and the hartmann structure in a single stage disclosed in chinese patent CN 201410553799.7.
In the embodiment, the 3D printed product printed with the high-strength aluminum-magnesium alloy as the raw material is subjected to heat treatment, wherein the heat treatment is selected from aging treatment or annealing treatment at 400 ℃ for 1 hour, and the performance is further improved through solid solution strengthening and/or precipitation strengthening.
The embodiments described above are described to facilitate an understanding and use of the invention by those skilled in the art. It will be readily apparent to those skilled in the art that various modifications to these embodiments may be made, and the generic principles described herein may be applied to other embodiments without the use of the inventive faculty. Therefore, the present invention is not limited to the above embodiments, and those skilled in the art should make improvements and modifications within the scope of the present invention based on the disclosure of the present invention.
Claims (3)
1. A3D printing process method of a high-strength aluminum-magnesium alloy is characterized by comprising the following steps:
heating and melting the high-strength aluminum-magnesium alloy raw material to uniformly mix the raw material;
preparing high-quality aluminum-magnesium alloy powder from the molten high-strength aluminum-magnesium alloy by adopting an air atomization technology, and drying to obtain the aluminum-magnesium alloy powder for 3D printing, wherein the air atomization technology is air atomization by adopting a supersonic speed atomization nozzle fusing laval and hartmann structures;
adjusting printing parameters, and performing 3D printing in a printing device filled with inert gas according to the three-dimensional model data of the part to obtain a 3D printing product taking the high-strength aluminum-magnesium alloy as a raw material;
the 3D printing method is selective laser melting, the printing equipment is SLM printing equipment and comprises a laser generating device and a cavity containing a powder cylinder and a forming cylinder, the cavity is closed during printing, inert gas is introduced, after the oxygen content in the cavity is lower than 0.1%, the substrate subjected to sand blasting treatment is preheated by laser, selective laser sintering is carried out according to a three-dimensional model of a part, the diameter of a selected laser beam spot is 50 microns, and then the product is printed;
during printing, laser scanning is carried out for 2 times to preheat the substrate, then powder spreading printing is carried out according to the three-dimensional model of the part, the printing parameters are set to be 200W of laser power, the scanning speed is 750mm/s, the printing layer thickness is 30 micrometers, the scanning interval is 130 micrometers, and the scanning strategy is a checkerboard;
after a 3D printing product taking high-strength aluminum-magnesium alloy as a raw material is obtained, carrying out heat treatment, carrying out aging treatment at 400 ℃ for 12 hours, and then carrying out air cooling;
the aluminum magnesium alloy powder for 3D printing comprises the following chemical compositions: mg content of 5.72 wt%, Zr content of 1.48 wt%, Si content of 1.24 wt%, Mn content of 0.62 wt%, Zn content of 0.43 wt%, and the balance of Al;
the average particle diameter of the powder is 25.95 μm, and more than 90% of the powder particles are spherical or spheroidal.
2. The 3D printing process of a high strength aluminum magnesium alloy according to claim 1 wherein the inert gas is selected from high purity argon.
3. The 3D printing process method of the high-strength aluminum-magnesium alloy according to claim 1, wherein the drying is performed for 5-24h under vacuum.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202010616674.XA CN111872386B (en) | 2020-06-30 | 2020-06-30 | 3D printing process method of high-strength aluminum-magnesium alloy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202010616674.XA CN111872386B (en) | 2020-06-30 | 2020-06-30 | 3D printing process method of high-strength aluminum-magnesium alloy |
Publications (2)
Publication Number | Publication Date |
---|---|
CN111872386A CN111872386A (en) | 2020-11-03 |
CN111872386B true CN111872386B (en) | 2021-12-31 |
Family
ID=73157580
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202010616674.XA Active CN111872386B (en) | 2020-06-30 | 2020-06-30 | 3D printing process method of high-strength aluminum-magnesium alloy |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN111872386B (en) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112536446B (en) * | 2020-11-20 | 2022-03-08 | 中国科学院金属研究所 | Laser additive and heat treatment composite process for preparing high-strength and high-toughness aluminum-silicon alloy or composite material thereof |
CN112893871B (en) * | 2021-01-20 | 2022-09-27 | 贵州大学 | Method for continuously manufacturing aluminum-magnesium alloy 3D printing component |
CN113042748B (en) * | 2021-03-09 | 2022-10-11 | 中北大学 | Method for preparing high-strength high-elongation Al-Cu-Mg alloy by SLM |
CN113430422B (en) * | 2021-06-25 | 2022-04-22 | 中南大学 | High-strength high-toughness heat-resistant aluminum-iron alloy and 3D printing method thereof |
CN113684403A (en) * | 2021-08-17 | 2021-11-23 | 北京工业大学 | High-strength aluminum alloy powder for 3D printing and preparation method thereof |
CN113755726B (en) * | 2021-08-30 | 2022-05-31 | 上海交通大学 | High-modulus high-toughness aluminum-based composite material and preparation method thereof |
CN116174733B (en) * | 2023-04-27 | 2023-07-28 | 宁波众远新材料科技有限公司 | Alloy powder, preparation method and application thereof, and part model |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104368820A (en) * | 2014-10-17 | 2015-02-25 | 同济大学 | Laval and hartmann structure integrated type supersonic-speed atomizing nozzle |
CN106801171A (en) * | 2015-11-04 | 2017-06-06 | 空中客车防务和空间有限责任公司 | For the Al Mg Si alloys with scandium of the unitary construction of ALM structures |
CN108465807A (en) * | 2018-03-20 | 2018-08-31 | 中南大学 | A kind of high intensity Al-Mg-Sc alloy powders, preparation method, the application in 3D printing and its 3D printing method |
CN108486433A (en) * | 2018-06-11 | 2018-09-04 | 江苏科技大学 | Selective laser melting process Al-Mg-Sc-Zr line aluminium alloys composition and molded part preparation method |
CN109576536A (en) * | 2019-01-22 | 2019-04-05 | 中南大学 | A kind of dedicated alumal power formulations of 3D printing and preparation method thereof and Method of printing |
CN109844150A (en) * | 2016-07-05 | 2019-06-04 | 纳诺尔有限责任公司 | Band and powder from high-strength corrosion-resisting aluminium alloy |
CN110724891A (en) * | 2019-10-24 | 2020-01-24 | 中车工业研究院有限公司 | Heat treatment method for controlling strength and elongation of additive manufactured aluminum alloy |
CN108796320B (en) * | 2018-09-19 | 2020-03-17 | 湖南东方钪业股份有限公司 | Aluminum alloy powder for 3D printing and preparation method thereof |
WO2020095009A2 (en) * | 2019-01-24 | 2020-05-14 | C-Tec Constellium Technology Center | Method for manufacturing an aluminum alloy part |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
PL3623488T3 (en) * | 2018-05-21 | 2021-10-25 | Obshchestvo S Ogranichennoy Otvetstvennost'yu "Obedinennaya Kompaniya Rusal Inzhenerno-Tekhnologicheskiy Tsentr" | Aluminum alloy powder for additive techniques and parts produced from the powder |
US11421310B2 (en) * | 2018-10-17 | 2022-08-23 | GM Global Technology Operations LLC | High strength aluminum alloy |
CN109487126B (en) * | 2018-12-19 | 2020-06-02 | 中车工业研究院有限公司 | Aluminum alloy powder for 3D printing and preparation method and application thereof |
FR3092119B1 (en) * | 2019-01-24 | 2020-12-25 | C Tec Constellium Tech Center | Process for manufacturing an aluminum alloy part, the alloy comprising at least zirconium and magnesium |
CN110405206A (en) * | 2019-07-23 | 2019-11-05 | 同济大学 | A method of aluminium alloy monomer structure is prepared using 3D printing |
-
2020
- 2020-06-30 CN CN202010616674.XA patent/CN111872386B/en active Active
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104368820A (en) * | 2014-10-17 | 2015-02-25 | 同济大学 | Laval and hartmann structure integrated type supersonic-speed atomizing nozzle |
CN106801171A (en) * | 2015-11-04 | 2017-06-06 | 空中客车防务和空间有限责任公司 | For the Al Mg Si alloys with scandium of the unitary construction of ALM structures |
CN109844150A (en) * | 2016-07-05 | 2019-06-04 | 纳诺尔有限责任公司 | Band and powder from high-strength corrosion-resisting aluminium alloy |
CN108465807A (en) * | 2018-03-20 | 2018-08-31 | 中南大学 | A kind of high intensity Al-Mg-Sc alloy powders, preparation method, the application in 3D printing and its 3D printing method |
CN108486433A (en) * | 2018-06-11 | 2018-09-04 | 江苏科技大学 | Selective laser melting process Al-Mg-Sc-Zr line aluminium alloys composition and molded part preparation method |
CN108796320B (en) * | 2018-09-19 | 2020-03-17 | 湖南东方钪业股份有限公司 | Aluminum alloy powder for 3D printing and preparation method thereof |
CN109576536A (en) * | 2019-01-22 | 2019-04-05 | 中南大学 | A kind of dedicated alumal power formulations of 3D printing and preparation method thereof and Method of printing |
WO2020095009A2 (en) * | 2019-01-24 | 2020-05-14 | C-Tec Constellium Technology Center | Method for manufacturing an aluminum alloy part |
CN110724891A (en) * | 2019-10-24 | 2020-01-24 | 中车工业研究院有限公司 | Heat treatment method for controlling strength and elongation of additive manufactured aluminum alloy |
Non-Patent Citations (1)
Title |
---|
高强Al_Mg合金钨极氩弧双丝增材制造工艺与组织性能;何杰等;《焊接学报》;20190731;第40卷(第7期);第109-113页 * |
Also Published As
Publication number | Publication date |
---|---|
CN111872386A (en) | 2020-11-03 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN111872386B (en) | 3D printing process method of high-strength aluminum-magnesium alloy | |
CN111659889A (en) | 3D printing process method of high-strength aluminum-manganese alloy | |
CN112935252B (en) | Method for preparing high-toughness eutectic high-entropy alloy based on selective laser melting technology | |
CN111673085A (en) | 3D printing process method of high-strength aluminum-magnesium-silicon alloy | |
CN111850332A (en) | 3D printing process method of high-strength aluminum-zinc alloy | |
CN110983262B (en) | Preparation method of aluminum-scandium alloy target material | |
CN108330344A (en) | A kind of 3D printing 7xxx aluminium alloys and preparation method thereof | |
US20240123502A1 (en) | Titanium alloy powder for selective laser melting 3d printing, selective laser melted titanium alloy and preparation thereof | |
CN110791686A (en) | Aluminum alloy powder material for additive manufacturing, and preparation method and application thereof | |
JP2019516861A (en) | Titanium, aluminum, vanadium and iron BCC materials and products made therefrom | |
CN109022920A (en) | A kind of 4D printing Ti-Ni marmem of flawless and preparation method thereof | |
CN113042748B (en) | Method for preparing high-strength high-elongation Al-Cu-Mg alloy by SLM | |
CN111455216A (en) | TC 4-like titanium alloy for laser additive manufacturing application | |
CN114411035B (en) | Precipitation strengthening type medium-entropy alloy suitable for laser additive manufacturing and preparation method thereof | |
CN110711862A (en) | Preparation method of special alloy for 3D printing of 6-series aluminum alloy | |
CN111659882A (en) | Aluminum magnesium alloy powder for 3D printing and preparation method thereof | |
CN111531172B (en) | 3D printing process method of high-strength aluminum-silicon alloy | |
CN111872404A (en) | Aluminum-copper alloy powder for 3D printing and preparation method thereof | |
CN111842914A (en) | 3D printing process method of high-strength aluminum-copper alloy | |
CN114351029A (en) | SLM CoCrNi alloy based on grain boundary segregation enhancement and preparation method thereof | |
CN114457267B (en) | Special high-strength aluminum alloy for SLM (Selective laser melting) and SLM forming method thereof | |
CN113020585B (en) | Low-melting-point multi-component alloy additive for laser additive manufacturing of aluminum alloy | |
CN113681028A (en) | Method and device for additive manufacturing of aluminum alloy in static magnetic field | |
CN111842913A (en) | Aluminum-zinc alloy powder for 3D printing and preparation method thereof | |
CN116426784B (en) | Method for preparing particle reinforced eutectic high-entropy alloy based on laser powder bed melting technology |
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 |