CN110052615A - A kind of method that precinct laser fusion prepares high strength alumin ium alloy - Google Patents

A kind of method that precinct laser fusion prepares high strength alumin ium alloy Download PDF

Info

Publication number
CN110052615A
CN110052615A CN201810906410.0A CN201810906410A CN110052615A CN 110052615 A CN110052615 A CN 110052615A CN 201810906410 A CN201810906410 A CN 201810906410A CN 110052615 A CN110052615 A CN 110052615A
Authority
CN
China
Prior art keywords
high strength
alumin ium
ium alloy
strength alumin
laser fusion
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.)
Pending
Application number
CN201810906410.0A
Other languages
Chinese (zh)
Inventor
李欣蔚
朱强
胡小刚
卢宏兴
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Southwest University of Science and Technology
Southern University of Science and Technology
Original Assignee
Southwest University of Science and Technology
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Southwest University of Science and Technology filed Critical Southwest University of Science and Technology
Priority to CN201810906410.0A priority Critical patent/CN110052615A/en
Publication of CN110052615A publication Critical patent/CN110052615A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/20Direct sintering or melting
    • B22F10/28Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM]
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F1/00Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
    • B22F1/05Metallic powder characterised by the size or surface area of the particles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/30Process control
    • B22F10/32Process control of the atmosphere, e.g. composition or pressure in a building chamber
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/30Process control
    • B22F10/34Process control of powder characteristics, e.g. density, oxidation or flowability
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/30Process control
    • B22F10/36Process control of energy beam parameters
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F9/00Making metallic powder or suspensions thereof
    • B22F9/02Making metallic powder or suspensions thereof using physical processes
    • B22F9/04Making metallic powder or suspensions thereof using physical processes starting from solid material, e.g. by crushing, grinding or milling
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B33ADDITIVE MANUFACTURING TECHNOLOGY
    • B33YADDITIVE 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
    • B33Y50/00Data acquisition or data processing for additive manufacturing
    • B33Y50/02Data acquisition or data processing for additive manufacturing for controlling or regulating additive manufacturing processes
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/04Making non-ferrous alloys by powder metallurgy
    • C22C1/0408Light metal alloys
    • C22C1/0416Aluminium-based alloys
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/04Making non-ferrous alloys by powder metallurgy
    • C22C1/05Mixtures of metal powder with non-metallic powder
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F9/00Making metallic powder or suspensions thereof
    • B22F9/02Making metallic powder or suspensions thereof using physical processes
    • B22F9/04Making metallic powder or suspensions thereof using physical processes starting from solid material, e.g. by crushing, grinding or milling
    • B22F2009/043Making metallic powder or suspensions thereof using physical processes starting from solid material, e.g. by crushing, grinding or milling by ball milling
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P10/00Technologies related to metal processing
    • Y02P10/25Process efficiency

Abstract

The present invention provides a kind of methods that precinct laser fusion prepares high strength alumin ium alloy; the following steps are included: providing high strength alumin ium alloy spherical powder and function and service particle; the function and service particle is the mixture of hard phase and alloying element phase; by the high strength alumin ium alloy spherical powder and the function and service particle mixed processing, mixed powder is obtained;Under inert atmosphere conditions, using precinct laser fusion equipment in laser power 190-220W, 70 μm of lasing beam diameter, scanning speed 115-155mm/s, 40-80 μm of sweep span, 70 μm of powder layer thickness, powder preheats under conditions of 150-250 DEG C, precinct laser fusion forming, natural cooling prepare high strength alumin ium alloy workpiece after coming out.

Description

A kind of method that precinct laser fusion prepares high strength alumin ium alloy
Technical field
The invention belongs to metal material 3D printing fields more particularly to a kind of precinct laser fusion to prepare high strength alumin ium alloy Method.
Background technique
Selective laser melting process is the important branch in metal 3D printing family, can utilize the direct local melting gold of laser Belong to powder, realize the fast precise forming of complex parts, and has been achieved with stainless steel, high-strength steel, titanium alloy, high temperature alloy, casting Make the forming of the materials such as aluminium alloy, cochrome.But it is being widely used in aerospace, weaponry, auto industry and electricity The high strength alumin ium alloy complex precise component manufacture view of the high-end fields such as son, cannot but play a role well.Because of high-strength aluminium The alloying level of alloy is high, and freezing range is big, and hot tearing sensibility is high, the high temperature generated during precinct laser fusion Under (3000 DEG C or more), micro- molten bath (20-120 μm), rapid cooling curing condition (solidification rate is up to 5m/s), easily because of solidification Shrink generate hole and through entire crystal grain fire check defect and along crystal boundary extend, seriously affect the formability and power of the alloy Learn performance.
The isometric crystal structure of fine uniform, which can accommodate, to be strained and prevents crackle.Increased in melt process of setting Cold degree is the key point for obtaining ideal isometric crystal structure, however, diffusion coefficient when due to aluminothermy conductance height, alloying element liquid Greatly, the solidification rate and temperature gradient that precinct laser fusion is formed are difficult to generate big degree of supercooling.Before solidification front, height is provided Density, the heterogeneous nucleation mass point of low energy barrier, degree of supercooling needed for isometric crystals growth capable of being reduced.
Although currently having carried out both at home and abroad some by crystal grain refinement improvement precinct laser fusion forming high strength alumin ium alloy heat The research work split simultaneously obtains certain achievement, but research emphasis is focusing only on adjusting process parameter and additional/interior raw nanoscale The heterogeneous nucleation mass point of mono-/multi- phase adds mono-/multi- kind alloying element only to refine crystal grain, and there are still hole or heat for gained alloy The problems such as crack defect, and mechanical property is very poor.As American scholar (Nature, 2017,549,365-369.) is thin using ZrH2 The 7075 high strength alumin ium alloy crystal grain for changing precinct laser fusion forming, although solving the problems, such as hot tearing to a certain extent, institute The tensile strength of drip molding is obtained less than 400MPa, far below casting-deformation conventional method acquisition alloy (580MPa or more).Than Sharp Shi Xuezhe (J.Mater.Process Tech., 2016,238,437-445.) adds Si element in the powder, can refine choosing The crystal grain of the Al-Zn-Mg-Cu high strength alumin ium alloy of area's laser fusing forming, but alloy consistency is very low.
Summary of the invention
The purpose of the present invention is to provide a kind of methods that precinct laser fusion prepares high strength alumin ium alloy, it is intended to solve existing Technology precinct laser fusion shape high strength alumin ium alloy method, generate hole and through entire crystal grain fire check defect and along crystalline substance The problem of boundary extends, and seriously affects the formability and mechanical property of the alloy.
For achieving the above object, The technical solution adopted by the invention is as follows:
One aspect of the present invention provides a kind of method that precinct laser fusion prepares high strength alumin ium alloy, comprising the following steps:
High strength alumin ium alloy spherical powder and function and service particle are provided, the function and service particle is hard phase and alloy member The high strength alumin ium alloy spherical powder and the function and service particle mixed processing are obtained mixed powder by the mixture of plain phase;
Under inert atmosphere conditions, using precinct laser fusion equipment in laser power 190-220W, 70 μm of lasing beam diameter, Scanning speed 115-155mm/s, 40-80 μm of sweep span, 70 μm of powder layer thickness, under conditions of powder preheats 150-250 DEG C, choosing Area's laser fusing, rear natural cooling to be formed, prepares high strength alumin ium alloy workpiece.
Preferably, the granularity of the high strength alumin ium alloy spherical powder is 200 mesh, and D90 is 40-50 μm;
The partial size of the hard phase is 30-50nm;The partial size of the alloying element phase is 30-50 μm.
Preferably, the partial size of the hard phase is 40nm;The partial size of the alloying element phase is 40 μm.
Preferably, in the function and service particle, the volume ratio of the hard phase and the alloying element phase is 1:1.
Preferably, the hard phase be selected from one of titanium carbide, titanium carbonitride, the alloying element be mutually selected from Ti, Hf, One of Sc, Y, Zr, Sr.
Preferably, the hard phase is titanium carbide, and the alloying element is mutually Ti.
Preferably, the mass ratio of the high strength alumin ium alloy spherical powder and the function and service particle is 100:(0.01- 10)。
Preferably, the mass ratio of the high strength alumin ium alloy spherical powder and the function and service particle is 100:(1-2).
Preferably, the function and service particle the preparation method comprises the following steps: the hard phase and the alloying element are mixed Afterwards, it is placed in ball mill, ball-milling treatment is carried out using the microballoon of 2-16mm, obtains function and service particle.
Preferably, in the step of precinct laser fusion, the intracorporal vacuum degree of precinct laser fusion equipment cavity is 10- 3Pa。
The method that precinct laser fusion provided by the invention prepares high strength alumin ium alloy will have and dive as heterogeneous forming core core The hard phase of power and the alloying element that can be reacted in molten aluminum mix the function and service particle and the high-strength aluminium of composition Precinct laser fusion is carried out after the mixing of alloy spherical powder, it is high that precinct laser fusion forming may be implemented in the function and service particle Strength aluminum alloy crystal grain refinement, the high strength alumin ium alloy for shaping precinct laser fusion have the equiaxed grain structure that can accommodate strain, keep away Exempt from hot tearing and hole defect, improve the mechanical property of alloy, it is hereby achieved that uniform small grains, without obvious crackle, densification The precinct laser fusion forming high strength alumin ium alloy test specimen of degree height, good mechanical performance, has practical application value.In addition, this hair The precinct laser fusion of bright offer prepares the method and process advantages of simple of high strength alumin ium alloy, high production efficiency, in high strength alumin ium alloy There are good industrial applications potentiality in terms of 3D printing.
Detailed description of the invention
Fig. 1 is the microscopic appearance figure for the Al-Zn-Mg-Cu high strength alumin ium alloy drip molding that comparative example 1 of the present invention provides;
Fig. 2 is the microscopic appearance figure for the Al-Zn-Mg-Cu high strength alumin ium alloy drip molding that the embodiment of the present invention 1 provides.
Specific embodiment
In order to which technical problems, technical solutions and advantageous effects to be solved by the present invention are more clearly understood, below in conjunction with Embodiment, the present invention will be described in further detail.It should be appreciated that specific embodiment described herein is only used to explain The present invention is not intended to limit the present invention.
In the description of the present invention, it is to be understood that, term " first ", " second " are used for description purposes only, and cannot It is interpreted as indication or suggestion relative importance or implicitly indicates the quantity of indicated technical characteristic.Define as a result, " the One ", the feature of " second " can explicitly or implicitly include one or more of the features.In the description of the present invention, The meaning of " plurality " is two or more, unless otherwise specifically defined.
The embodiment of the invention provides a kind of methods that precinct laser fusion prepares high strength alumin ium alloy, comprising the following steps:
S01. high strength alumin ium alloy spherical powder and function and service particle are provided, the function and service particle is hard phase and conjunction The mixture of gold element phase is mixed the high strength alumin ium alloy spherical powder and the function and service particle mixed processing Powder;
S02. under inert atmosphere conditions, using precinct laser fusion equipment in laser power 190-220W, lasing beam diameter 70 μm, scanning speed 115-155mm/s, 40-80 μm of sweep span, 70 μm of powder layer thickness, powder preheats 150-250 DEG C of condition Under, precinct laser fusion, rear natural cooling to be formed prepares high strength alumin ium alloy workpiece.
The method that precinct laser fusion provided in an embodiment of the present invention prepares high strength alumin ium alloy will have as heterogeneous forming core The hard phase of core potentiality and the alloying element that can be reacted in molten aluminum mix the function and service particle of composition with it is described Precinct laser fusion is carried out after the mixing of high strength alumin ium alloy spherical powder, precinct laser fusion may be implemented in the function and service particle High strength alumin ium alloy crystal grain refinement is shaped, the high strength alumin ium alloy for shaping precinct laser fusion has the equiax crystal group that can accommodate strain Knit, avoid hot tearing and hole defect, improve the mechanical property of alloy, it is hereby achieved that uniform small grains, without obvious crackle, The precinct laser fusion forming high strength alumin ium alloy test specimen of consistency height, good mechanical performance, has practical application value.In addition, Precinct laser fusion provided in an embodiment of the present invention prepares the method and process advantages of simple of high strength alumin ium alloy, high production efficiency, There are good industrial applications potentiality in terms of high strength alumin ium alloy 3D printing.
In above-mentioned steps S01, the function and service particle is the function and service particle for refining high strength alumin ium alloy crystal grain. Specifically, the function and service particle is the mixture of hard phase and alloying element phase, wherein the hard phase can be used as heterogeneous The refinement of Al crystal grain in forming core core refining aluminum alloy, crystal grain can improve hot tearing and improve alloy mechanical property, strengthen and close Gold;The alloying element can mutually occur to melt and chemically react with Al in molten bath, and suction/heat release of these reactions can make to melt Pond melt amount of localized heat is unevenly distributed, and forms violent thermal convection, and hard phase dispersion and alloying element atom is promoted to be evenly distributed.Its In, the dispersion of hard phase promotes grain refining effect further;Alloying element atom, which is uniformly distributed, can make it be easier to be solid-solution in In Al matrix, reinforced alloys improve the mechanical property of alloy.
In the embodiment of the present invention, described hard phase fusing point itself is high, thermal stability is good but the wetting between molten aluminum Difference is difficult to refine Al crystal grain directly as heterogeneous forming core core.In consideration of it, further, hard phase is coated on alloying element phase Surface.The hard phase and the alloying element are mutually combined, mutually melted using alloying element or chemistry occurs with Al The thermal change generated is reacted, the wetability between Lai Gaishan hard phase and molten aluminum can more fully play its forming core work With.
In the embodiment of the present invention, the partial size of the hard phase is 30-50nm;The partial size of the alloying element phase is 30-50 μ m.The hard phase it is undersized when, cost is higher, and the dimensional effect of nano particle is significant, easy to reunite, can't be The heterogeneous forming core core of effect;When oversized, the tensile strength of aluminium alloy can be substantially reduced.The alloying element it is undersized When, it is not easy to adhere to nanoscale hard phase uniformly on the surface thereof;When oversized, alloying element atom is in precinct laser fusion There is no enough time evenly dispersed in the fusing-process of setting of processing extremely fast.
Specific preferred, the partial size of the hard phase is 40nm;The partial size of the alloying element phase is 40 μm, is used for constituency When laser fusing prepares high strength alumin ium alloy, obtained high strength alumin ium alloy " uniform small grains, without obvious crackle, consistency is high, power The effect of function admirable " is more preferable.
Preferably, the hard phase be selected from one of titanium carbide, titanium carbonitride, the alloying element be mutually selected from Ti, Hf, One of Sc, Y, Zr, Sr.The titanium carbide, titanium carbonitride are identical as Al crystal structure of element, lattice equations are less than or equal to 9%, it is easy to the heterogeneous forming core core as Al, and then heterogeneous forming core Al, refinement Al crystal grain, hot tearing is solved by crystal grain refinement and is asked Topic, and further increase the mechanical property of alloy.
Preferred alloying element can react in molten bath, and under high temperature, reaction product is unstable.These features make to melt Pond melt amount of localized heat is unevenly distributed, and forms violent thermal convection, and hard phase dispersion and alloying element atom is promoted to be evenly distributed.Firmly The dispersion of matter phase promotes grain refining effect further;Alloying element atom, which is uniformly distributed, can make it be easier to be solid-solution in Al matrix In, reinforced alloys improve the mechanical property of alloy.
Specific preferred, the hard phase is titanium carbide, and the alloying element is mutually Ti.
Preferably, in the function and service particle, the volume ratio of the hard phase and the alloying element phase is 1:1.
In the embodiment of the present invention, it is preferred that the function and service particle the preparation method comprises the following steps: by the hard phase and described It after alloying element mixes, is placed in ball mill, ball-milling treatment is carried out using the microballoon of 2-16mm, obtains function and service particle. By ball-milling treatment, nanoscale hard phase can be preferably coated on to the surface of micron-sized alloying element phase.Certainly, should Understand, in addition to ball-milling treatment, can also be realized using modes such as electrostatic treatments hard phase in the attachment of alloying element phase surface, but Effect is good not as good as ball-milling treatment, in addition, equipment needed for the modes such as electrostatic treatment, price, energy consumption are high.
In the embodiment of the present invention, it is preferred that the granularity of the high strength alumin ium alloy spherical powder is 200 mesh, and D90 is 40-50 μ m.The high strength alumin ium alloy powder of the grain size intervals is easy to precinct laser fusion forming.When powder size is excessive, drip molding porosity Height, poor quality;When powder size is too small, powder flowbility is poor, and powdering performance is poor, easily forms crackle and hole.
Preferably, the mass ratio of the high strength alumin ium alloy spherical powder and the function and service particle is 100:(1-5), it is right The grain refining effect of aluminium alloy is preferable.Specifically, composite particles ratio is too low, sufficient Grain Refinement Effect is not had, no It can effectively solve hot tearing problem, it is even more impossible to improve alloy mechanical property;Ratio is excessively high, multiple in precinct laser fusion process Closing can reunite agglomeration, alloying element of nanometer hard phase contained in particle not can be uniformly dispersed in aluminum substrate.
Specifically, the embodiment of the present invention by granularity be 200 mesh, D90 be 40-50 μm high strength alumin ium alloy spherical powder with adopt The composite particles (40nm hard phase with 40 μm of alloying element phases) prepared with ball-milling method are uniformly mixed, and improve powder on powder bed Powdering ability.Specifically, powdering ability is related with powder flowbility for metal powder, the powder paving of good fluidity Powder ability is strong.Micron order alloying element phase mobility selected by the present invention is better than the Al alloy powder with scale, therefore, with aluminium Mixed-powder mobility after alloy powder mixes is better than simple Al alloy powder.In addition, alloying element phase surface adheres to There are nanoscale hard-phase particles, be equivalent to and mutually load onto one layer of idler wheel to alloying element.Therefore, powder is easier to flow, more Easy powdering.
In above-mentioned steps S02, under inert atmosphere conditions, using precinct laser fusion equipment in laser power 190-220W, 70 μm of lasing beam diameter, scanning speed 115-155mm/s, 40-80 μm of sweep span, 70 μm of powder layer thickness, powder preheats 150- Under conditions of 250 DEG C, precinct laser fusion, rear natural cooling to be formed prepares high strength alumin ium alloy workpiece.Under this technique It can get grain fine uniform, the precinct laser fusion without obvious crackle, consistency height, good mechanical performance shapes high strength alumin ium alloy Test specimen.
Wherein, it can be protected using argon gas in forming cavity.After part forming, the natural cooling in forming cavity, to reduce Residual stress improves formability.Preferably, in the step of precinct laser fusion, the precinct laser fusion equipment cavity is intracorporal Vacuum degree is 10-3Pa。
It is illustrated combined with specific embodiments below.
Embodiment 1
The method of the precinct laser fusion forming of Al-Zn-Mg-Cu high strength alumin ium alloy, comprising the following steps:
The spherical powder (200 mesh of granularity, D90 be 40 μm) that material is Al-Zn-Mg-Cu high strength alumin ium alloy is provided, and it is compound Particle (hard phase titanium carbide of 40nm and 40 μm of alloying element titanium, volume ratio 1:1) is packed into after mixing according to weight ratio 100:2 Powder drum.
10 are evacuated down in precinct laser fusion equipment cavity-3After Pa, it is filled with high-purity argon gas, 3 times repeatedly.In powder bed Powder, powdering basal plate preheating is to 150 DEG C.
Precinct laser fusion technological parameter: laser power 210w, 80 μm of laser diameter, scanning speed 135mm/s, between scanning Away from 50 μm, 70 μm of lift height.After part forming, the Slow cooling in forming cavity, to prevent Quench from cracking.
Al-Zn-Mg-Cu high strength alumin ium alloy as a comparison case 1 using the forming of common process precinct laser fusion is provided.This The common process at place refers to, compared to comparative example, is not added with composite particles, other process conditions are identical.
Fig. 1 and Fig. 2 is respectively Al-Zn-Mg-Cu high strength alumin ium alloy drip molding prepared by comparative example 1 and the embodiment of the present invention 1 Microscopic appearance figure, sample pass through mechanical lapping polishing treatment, obtained by optical microphotograph sem observation.Wherein, Pores indicates hole Hole, Carcks indicate crackle.
It is measured and is calculated, compared with comparative example, the Al-Zn-Mg-Cu high strength alumin ium alloy drip molding of the preparation of embodiment 1 Average grain size is reduced to 1.1 μm by 75 μm, and crackle, hole defect substantially reduce, and consistency is increased to by 96.3% 99.6%, and tensile strength, microhardness are increased to 419MPa, 171HV by 76MPa, 149HV respectively.
Embodiment 2
The method of the precinct laser fusion forming of Al-Si-Mg-Cu high strength alumin ium alloy, comprising the following steps:
The spherical powder (200 mesh of granularity, D90 be 40 μm) that material is Al-Si-Mg-Cu high strength alumin ium alloy is provided, and it is compound Particle (hard phase titanium carbide of 40nm and 40 μm of alloying element strontium, volume ratio 1:1) is packed into after mixing according to weight ratio 100:1 Powder drum.
10 are evacuated down in precinct laser fusion equipment cavity-3After Pa, it is filled with high-purity argon gas, 3 times repeatedly.In powder bed Powder, powdering basal plate preheating is to 150 DEG C.
Precinct laser fusion technological parameter: laser power 210w, 80 μm of laser diameter, scanning speed 135mm/s, between scanning Away from 50 μm, 70 μm of lift height.After part forming, the Slow cooling in forming cavity, to prevent Quench from cracking.
Al-Si-Mg-Cu high strength alumin ium alloy as a comparison case 2 using the forming of common process precinct laser fusion is provided.This The common process at place refers to, compared to comparative example 2, is not added with composite particles, other process conditions are identical.It is measured and is calculated, Compared with comparative example, the average grain size of Al-Si-Mg-Cu high strength alumin ium alloy drip molding prepared by embodiment 1 is reduced by 45 μm To 9.8 μm, crackle, hole defect are substantially reduced, and consistency is increased to 99.1%, and tensile strength, microhardness point by 95% 303MPa, 162HV are not increased to by 211MPa, 123HV.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all in essence of the invention Made any modifications, equivalent replacements, and improvements etc., should all be included in the protection scope of the present invention within mind and principle.

Claims (10)

1. a kind of method that precinct laser fusion prepares high strength alumin ium alloy, which comprises the following steps:
High strength alumin ium alloy spherical powder and function and service particle are provided, the function and service particle is hard phase and alloying element phase Mixture the high strength alumin ium alloy spherical powder and the function and service particle mixed processing are obtained into mixed powder;
Under inert atmosphere conditions, using precinct laser fusion equipment in laser power 190-220W, 70 μm of lasing beam diameter, scan Speed 115-155mm/s, 40-80 μm of sweep span, 70 μm of powder layer thickness, under conditions of powder preheats 150-250 DEG C, constituency is swashed Light fusing, rear natural cooling to be formed, prepares high strength alumin ium alloy workpiece.
2. the method that precinct laser fusion as described in claim 1 prepares high strength alumin ium alloy, which is characterized in that the high-strength aluminium The granularity of alloy spherical powder is 200 mesh, and D90 is 40-50 μm;
The partial size of the hard phase is 30-50nm;The partial size of the alloying element phase is 30-50 μm.
3. the method that precinct laser fusion as claimed in claim 2 prepares high strength alumin ium alloy, which is characterized in that the hard phase Partial size be 40nm;The partial size of the alloying element phase is 40 μm.
4. the method that precinct laser fusion as claimed in claim 3 prepares high strength alumin ium alloy, which is characterized in that the function is multiple It closes in particle, the volume ratio of the hard phase and the alloying element phase is 1:1.
5. the method that precinct laser fusion according to any one of claims 1-4 prepares high strength alumin ium alloy, which is characterized in that institute State hard phase be selected from one of titanium carbide, titanium carbonitride, the alloying element mutually in Ti, Hf, Sc, Y, Zr, Sr one Kind.
6. the method that precinct laser fusion as claimed in claim 5 prepares high strength alumin ium alloy, which is characterized in that the hard phase For titanium carbide, the alloying element is mutually Ti.
7. the method that precinct laser fusion according to any one of claims 1-4 prepares high strength alumin ium alloy, which is characterized in that institute The mass ratio for stating high strength alumin ium alloy spherical powder and the function and service particle is 100:(1-5).
8. the method that precinct laser fusion as claimed in claim 7 prepares high strength alumin ium alloy, which is characterized in that the high-strength aluminium The mass ratio of alloy spherical powder and the function and service particle is 100:(0.01-10).
9. the method that precinct laser fusion according to any one of claims 1-4 prepares high strength alumin ium alloy, which is characterized in that institute State function and service particle the preparation method comprises the following steps: the hard phase and the alloying element are mixed after, be placed in ball mill, adopt Ball-milling treatment is carried out with the microballoon of 2-16mm, obtains function and service particle.
10. the method that precinct laser fusion according to any one of claims 1-4 prepares high strength alumin ium alloy, which is characterized in that In the step of precinct laser fusion, the intracorporal vacuum degree of precinct laser fusion equipment cavity is 10-3Pa。
CN201810906410.0A 2018-08-10 2018-08-10 A kind of method that precinct laser fusion prepares high strength alumin ium alloy Pending CN110052615A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810906410.0A CN110052615A (en) 2018-08-10 2018-08-10 A kind of method that precinct laser fusion prepares high strength alumin ium alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810906410.0A CN110052615A (en) 2018-08-10 2018-08-10 A kind of method that precinct laser fusion prepares high strength alumin ium alloy

Publications (1)

Publication Number Publication Date
CN110052615A true CN110052615A (en) 2019-07-26

Family

ID=67315245

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810906410.0A Pending CN110052615A (en) 2018-08-10 2018-08-10 A kind of method that precinct laser fusion prepares high strength alumin ium alloy

Country Status (1)

Country Link
CN (1) CN110052615A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110744047A (en) * 2019-11-01 2020-02-04 昆明理工大学 Preparation method of aluminum-based composite material
CN111272872A (en) * 2020-02-14 2020-06-12 南方科技大学 Crack detection method and device and additive manufacturing system
CN111957960A (en) * 2020-08-12 2020-11-20 南方科技大学 Selective laser melting forming method for heat crack-free precipitation strengthening high-temperature alloy
CN112207278A (en) * 2020-08-20 2021-01-12 南京航空航天大学 Selective laser melting additive manufacturing and discharge combined machining method for aluminum alloy gear
CN113430432A (en) * 2021-06-29 2021-09-24 哈尔滨工业大学 Preparation method of high-Zn light high-strength aluminum alloy
CN114107756A (en) * 2021-10-20 2022-03-01 汕头大学 Aluminum alloy capable of inhibiting 3D printing solidification cracks and processing method thereof
WO2022067554A1 (en) * 2020-09-29 2022-04-07 西门子股份公司 3d printing powder and 3d printing method
CN114729424A (en) * 2019-11-18 2022-07-08 Eos有限公司电镀光纤系统 Weldable aluminium alloy containing Zn as the main alloying element for direct metal laser sintering
CN114871450A (en) * 2022-03-31 2022-08-09 南京航空航天大学 Preparation method for manufacturing thermal crack sensitive material through laser material increase based on infrared ray auxiliary preheating
WO2022193487A1 (en) * 2021-03-15 2022-09-22 上海交通大学 High-strength and toughness, heat-resistant aluminum alloy armature material and preparation method therefor

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02149682A (en) * 1988-11-30 1990-06-08 Showa Alum Corp Production of aluminum alloy material having superior wear resistance
JPH02205664A (en) * 1988-12-15 1990-08-15 Komatsu Ltd Laser cladding method
CN104404508A (en) * 2014-11-24 2015-03-11 桂林电子科技大学 Laser additive manufacturing method for aluminium alloy structural part
CN104805450A (en) * 2015-03-20 2015-07-29 南京航空航天大学 Three-phase Al-Ti-Cu microparticle enhanced Al alloy protective coating and preparation method
CN105112708A (en) * 2015-09-16 2015-12-02 华中科技大学 Rapid manufacturing method for laser remelting scanning carbide dispersion strengthened aluminum alloy
CN105328186A (en) * 2015-10-30 2016-02-17 南京航空航天大学 Aluminum-based in-situ composite material formed based on laser 3D printing and preparation method of aluminum-based in-situ composite material
CN105583401A (en) * 2015-12-25 2016-05-18 华中科技大学 Method for preparing composite powder for 3D printing, product and application
CN105803271A (en) * 2016-03-18 2016-07-27 南京航空航天大学 Aluminium-based nanocomposite based on SLM forming and preparation method of nanocomposite
CN107254610A (en) * 2017-06-12 2017-10-17 吉林大学 Raw nano-sized particles reinforced aluminium alloy material preparation method in a kind of
CN107774996A (en) * 2017-10-11 2018-03-09 华中科技大学 A kind of integral forming method of the part of more material gradient lattice structures
CN107812941A (en) * 2017-10-20 2018-03-20 华中科技大学 A kind of in-situ preparation method of laser gain material manufacture aluminium alloy and products thereof

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02149682A (en) * 1988-11-30 1990-06-08 Showa Alum Corp Production of aluminum alloy material having superior wear resistance
JPH02205664A (en) * 1988-12-15 1990-08-15 Komatsu Ltd Laser cladding method
CN104404508A (en) * 2014-11-24 2015-03-11 桂林电子科技大学 Laser additive manufacturing method for aluminium alloy structural part
CN104805450A (en) * 2015-03-20 2015-07-29 南京航空航天大学 Three-phase Al-Ti-Cu microparticle enhanced Al alloy protective coating and preparation method
CN105112708A (en) * 2015-09-16 2015-12-02 华中科技大学 Rapid manufacturing method for laser remelting scanning carbide dispersion strengthened aluminum alloy
CN105328186A (en) * 2015-10-30 2016-02-17 南京航空航天大学 Aluminum-based in-situ composite material formed based on laser 3D printing and preparation method of aluminum-based in-situ composite material
CN105583401A (en) * 2015-12-25 2016-05-18 华中科技大学 Method for preparing composite powder for 3D printing, product and application
CN105803271A (en) * 2016-03-18 2016-07-27 南京航空航天大学 Aluminium-based nanocomposite based on SLM forming and preparation method of nanocomposite
CN107254610A (en) * 2017-06-12 2017-10-17 吉林大学 Raw nano-sized particles reinforced aluminium alloy material preparation method in a kind of
CN107774996A (en) * 2017-10-11 2018-03-09 华中科技大学 A kind of integral forming method of the part of more material gradient lattice structures
CN107812941A (en) * 2017-10-20 2018-03-20 华中科技大学 A kind of in-situ preparation method of laser gain material manufacture aluminium alloy and products thereof

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
BINGYI ZHAO等: "Efect of TiC Nanoparticles Supported by Ti Powders on the Solidifcation Behavior and Microstructure of Pure Aluminum", 《METALS AND MATERIALS INTERNATIONAL》 *
王运赣等: "《三维打印技术》", 31 July 2013 *
雷仕湛等: "《激光智能制造技术》", 30 June 2018 *

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110744047A (en) * 2019-11-01 2020-02-04 昆明理工大学 Preparation method of aluminum-based composite material
CN114729424A (en) * 2019-11-18 2022-07-08 Eos有限公司电镀光纤系统 Weldable aluminium alloy containing Zn as the main alloying element for direct metal laser sintering
CN114729424B (en) * 2019-11-18 2024-02-20 Eos有限公司电镀光纤系统 Weldable aluminium alloy containing Zn as main alloying element for direct metal laser sintering
CN111272872A (en) * 2020-02-14 2020-06-12 南方科技大学 Crack detection method and device and additive manufacturing system
CN111957960A (en) * 2020-08-12 2020-11-20 南方科技大学 Selective laser melting forming method for heat crack-free precipitation strengthening high-temperature alloy
CN112207278A (en) * 2020-08-20 2021-01-12 南京航空航天大学 Selective laser melting additive manufacturing and discharge combined machining method for aluminum alloy gear
WO2022067554A1 (en) * 2020-09-29 2022-04-07 西门子股份公司 3d printing powder and 3d printing method
WO2022193487A1 (en) * 2021-03-15 2022-09-22 上海交通大学 High-strength and toughness, heat-resistant aluminum alloy armature material and preparation method therefor
CN113430432A (en) * 2021-06-29 2021-09-24 哈尔滨工业大学 Preparation method of high-Zn light high-strength aluminum alloy
CN113430432B (en) * 2021-06-29 2022-03-01 哈尔滨工业大学 Preparation method of high-Zn light high-strength aluminum alloy
CN114107756A (en) * 2021-10-20 2022-03-01 汕头大学 Aluminum alloy capable of inhibiting 3D printing solidification cracks and processing method thereof
CN114871450B (en) * 2022-03-31 2023-12-01 南京航空航天大学 Preparation method for manufacturing thermal cracking sensitive material by laser additive based on infrared auxiliary preheating
CN114871450A (en) * 2022-03-31 2022-08-09 南京航空航天大学 Preparation method for manufacturing thermal crack sensitive material through laser material increase based on infrared ray auxiliary preheating

Similar Documents

Publication Publication Date Title
CN110052615A (en) A kind of method that precinct laser fusion prepares high strength alumin ium alloy
Li et al. Synthesis of AlxCoCrFeNi high-entropy alloys by high-gravity combustion from oxides
Kalaiselvan et al. Production and characterization of AA6061–B4C stir cast composite
Ravi et al. Characterization of aluminium matrix composites (AA6061/B4C) fabricated by stir casting technique
EP2065108B1 (en) Metal particles, process for manufacturing the same, and process for manufacturing vehicle components therefrom
Wolf et al. Recent developments on fabrication of Al‐matrix composites reinforced with quasicrystals: from metastable to conventional processing
CN108746625A (en) A kind of preparation method of aluminum-base nano composite material
CN109175391B (en) Method for in-situ synthesis of nano-oxide particle dispersion strengthened alloy
Venkatesh et al. Mechanical properties of metal matrix composites (Al/SiCp) particles produced by powder metallurgy
CN104593652A (en) Quasicrystal and alumina mixed particle reinforced magnesium-based composite material and manufacturing method thereof
CN110438379B (en) Preparation method of lithium-containing magnesium/aluminum-based composite material
CN110423914B (en) Preparation method of rare earth magnesium alloy composite material
Mazahery et al. Effect of coated B4C reinforcement on mechanical properties of squeeze cast A356 composites
Huashun et al. Preparation of Al-Al3Ti in situ composites by direct reaction method
Lin et al. Sol-gel MgO coating on glass microspheres for inhibiting excessive interfacial reaction in Al-Mg matrix syntactic foam
US20210062315A1 (en) Preparation method of a lithium-containing magnesium/aluminum matrix composite
CN109576522B (en) Silicon carbide reinforced aluminum-based composite material and preparation method thereof
CN102864343B (en) Preparation method for in-situ aluminium base composite material inoculant
Gui et al. Microstructure and mechanical properties of Mg–Al9Zn/SiCp composite produced by vacuum stir casting process
Jayalakshmi et al. Light metal matrix composites
Nie Patents of methods to prepare intermetallic matrix composites: A Review
CN104625081A (en) Method for preparing aluminum alloy powder through salt melting method
CN112705717A (en) Preparation method of in-situ generated nitride enhanced high-entropy alloy-based powder material
CN102560204A (en) Silicon-aluminum bicontinuous composite material and preparation method thereof
Baghchesara et al. Fractography of stir casted Al-ZrO2 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
RJ01 Rejection of invention patent application after publication

Application publication date: 20190726

RJ01 Rejection of invention patent application after publication