CN112024872B - Method for preparing composite powder for laser 3D printing by sol coating method - Google Patents
Method for preparing composite powder for laser 3D printing by sol coating method Download PDFInfo
- Publication number
- CN112024872B CN112024872B CN202010945029.2A CN202010945029A CN112024872B CN 112024872 B CN112024872 B CN 112024872B CN 202010945029 A CN202010945029 A CN 202010945029A CN 112024872 B CN112024872 B CN 112024872B
- Authority
- CN
- China
- Prior art keywords
- powder
- laser
- composite powder
- tio
- sol
- 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
- 239000000843 powder Substances 0.000 title claims abstract description 154
- 239000002131 composite material Substances 0.000 title claims abstract description 90
- 238000000034 method Methods 0.000 title claims abstract description 42
- 238000010146 3D printing Methods 0.000 title claims abstract description 39
- 238000000576 coating method Methods 0.000 title claims abstract description 28
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 claims abstract description 68
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 22
- 239000000956 alloy Substances 0.000 claims abstract description 22
- 238000000498 ball milling Methods 0.000 claims abstract description 19
- 230000007062 hydrolysis Effects 0.000 claims abstract description 18
- 238000006460 hydrolysis reaction Methods 0.000 claims abstract description 18
- 239000003112 inhibitor Substances 0.000 claims abstract description 18
- 229910003407 AlSi10Mg Inorganic materials 0.000 claims abstract description 15
- 239000002243 precursor Substances 0.000 claims abstract description 15
- 239000004408 titanium dioxide Substances 0.000 claims abstract description 14
- 229910000838 Al alloy Inorganic materials 0.000 claims abstract description 13
- 239000000919 ceramic Substances 0.000 claims abstract description 13
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 13
- 239000008367 deionised water Substances 0.000 claims abstract description 12
- 229910021641 deionized water Inorganic materials 0.000 claims abstract description 12
- QTBSBXVTEAMEQO-UHFFFAOYSA-N Acetic acid Chemical compound CC(O)=O QTBSBXVTEAMEQO-UHFFFAOYSA-N 0.000 claims description 32
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 claims description 25
- 238000000227 grinding Methods 0.000 claims description 23
- 239000002245 particle Substances 0.000 claims description 20
- 229960000583 acetic acid Drugs 0.000 claims description 16
- 239000012362 glacial acetic acid Substances 0.000 claims description 16
- 238000002156 mixing Methods 0.000 claims description 14
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 claims description 11
- 238000004519 manufacturing process Methods 0.000 claims description 10
- 239000000203 mixture Substances 0.000 claims description 10
- 238000003756 stirring Methods 0.000 claims description 10
- 239000000654 additive Substances 0.000 claims description 9
- 230000000996 additive effect Effects 0.000 claims description 9
- 230000032683 aging Effects 0.000 claims description 7
- 239000011248 coating agent Substances 0.000 claims description 7
- 239000010936 titanium Substances 0.000 claims description 7
- 239000011156 metal matrix composite Substances 0.000 claims description 6
- GRYLNZFGIOXLOG-UHFFFAOYSA-N Nitric acid Chemical compound O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 0.000 claims description 5
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 5
- 238000001035 drying Methods 0.000 claims description 5
- 229910017604 nitric acid Inorganic materials 0.000 claims description 5
- FPCJKVGGYOAWIZ-UHFFFAOYSA-N butan-1-ol;titanium Chemical compound [Ti].CCCCO.CCCCO.CCCCO.CCCCO FPCJKVGGYOAWIZ-UHFFFAOYSA-N 0.000 claims description 4
- JMXKSZRRTHPKDL-UHFFFAOYSA-N titanium ethoxide Chemical group [Ti+4].CC[O-].CC[O-].CC[O-].CC[O-] JMXKSZRRTHPKDL-UHFFFAOYSA-N 0.000 claims description 3
- -1 propyl titanate Chemical compound 0.000 claims description 2
- 239000000463 material Substances 0.000 abstract description 15
- 238000002360 preparation method Methods 0.000 abstract description 12
- 238000011065 in-situ storage Methods 0.000 abstract description 11
- 230000009286 beneficial effect Effects 0.000 abstract description 5
- 239000000126 substance Substances 0.000 abstract description 5
- 230000002787 reinforcement Effects 0.000 abstract description 3
- 238000003980 solgel method Methods 0.000 abstract description 3
- 229910010413 TiO 2 Inorganic materials 0.000 abstract 2
- 230000003014 reinforcing effect Effects 0.000 description 11
- 229910052782 aluminium Inorganic materials 0.000 description 8
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 8
- 239000011159 matrix material Substances 0.000 description 8
- 239000010935 stainless steel Substances 0.000 description 8
- 229910001220 stainless steel Inorganic materials 0.000 description 8
- 229910033181 TiB2 Inorganic materials 0.000 description 5
- 238000006243 chemical reaction Methods 0.000 description 5
- 238000000889 atomisation Methods 0.000 description 4
- 108010025899 gelatin film Proteins 0.000 description 4
- 238000005266 casting Methods 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 230000000630 rising effect Effects 0.000 description 3
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 230000004927 fusion Effects 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 229910052748 manganese Inorganic materials 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 239000002105 nanoparticle Substances 0.000 description 2
- 229910052718 tin Inorganic materials 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- 229910052725 zinc Inorganic materials 0.000 description 2
- QYEXBYZXHDUPRC-UHFFFAOYSA-N B#[Ti]#B Chemical compound B#[Ti]#B QYEXBYZXHDUPRC-UHFFFAOYSA-N 0.000 description 1
- 229910020491 K2TiF6 Inorganic materials 0.000 description 1
- 229910007948 ZrB2 Inorganic materials 0.000 description 1
- MCMNRKCIXSYSNV-UHFFFAOYSA-N ZrO2 Inorganic materials O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 239000000274 aluminium melt Substances 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- VWZIXVXBCBBRGP-UHFFFAOYSA-N boron;zirconium Chemical compound B#[Zr]#B VWZIXVXBCBBRGP-UHFFFAOYSA-N 0.000 description 1
- 229910052681 coesite Inorganic materials 0.000 description 1
- 229910052906 cristobalite Inorganic materials 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000003912 environmental pollution Methods 0.000 description 1
- 150000004673 fluoride salts Chemical class 0.000 description 1
- 238000010309 melting process Methods 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 239000011259 mixed solution Substances 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 230000005501 phase interface Effects 0.000 description 1
- 238000004663 powder metallurgy Methods 0.000 description 1
- 238000010298 pulverizing process Methods 0.000 description 1
- 239000000376 reactant Substances 0.000 description 1
- 239000003870 refractory metal Substances 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 229910021332 silicide Inorganic materials 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 229910052682 stishovite Inorganic materials 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 230000035882 stress Effects 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
- 238000001308 synthesis method Methods 0.000 description 1
- 238000003786 synthesis reaction Methods 0.000 description 1
- 230000002194 synthesizing effect Effects 0.000 description 1
- 150000003568 thioethers Chemical class 0.000 description 1
- 231100000331 toxic Toxicity 0.000 description 1
- 230000002588 toxic effect Effects 0.000 description 1
- 229910052905 tridymite Inorganic materials 0.000 description 1
Images
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
- B22F1/16—Metallic particles coated with a non-metal
-
- B22F1/0003—
-
- 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
- B33Y70/10—Composites of different types of material, e.g. mixtures of ceramics and polymers or mixtures of metals and biomaterials
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Civil Engineering (AREA)
- Composite Materials (AREA)
- Structural Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
- Powder Metallurgy (AREA)
Abstract
本发明涉及一种溶胶包覆法制备激光3D打印用复合粉末的方法，属于复合粉末制备技术领域。本发明通过溶胶‑凝胶法以二氧化钛前驱体和水解抑制剂在去离子水中反应得到TiO2溶胶，将TiO2溶胶均匀包覆在B粉表面制备成TiO2@B包覆型复合粉末，再将TiO2@B包覆型复合粉末与铝合金粉末进行真空球磨处理即得激光3D打印用复合粉末。本发明方法制备的粉末材料，用于激光3D打印工艺时，TiO2与B可在AlSi10Mg合金熔体中充分接触并反应，原位生成TiB2及B2O3陶瓷增强体；不仅可以提高铝合金粉末对激光的利用率，有利于复合材料综合性能的提高，而且在粉末制备过程中不产生对环境造成污染的物质。
The invention relates to a method for preparing composite powder for laser 3D printing by a sol coating method, and belongs to the technical field of composite powder preparation. In the present invention, a TiO2 sol is obtained by reacting a titanium dioxide precursor and a hydrolysis inhibitor in deionized water by a sol-gel method, and the TiO2 sol is uniformly coated on the surface of the B powder to prepare a TiO2 @B-coated composite powder. The composite powder for laser 3D printing was obtained by vacuum ball milling the TiO 2 @B coated composite powder and the aluminum alloy powder. When the powder material prepared by the method of the invention is used in the laser 3D printing process, TiO 2 and B can fully contact and react in the AlSi10Mg alloy melt, and TiB 2 and B 2 O 3 ceramic reinforcements are formed in situ; The utilization ratio of the alloy powder to the laser is beneficial to the improvement of the comprehensive performance of the composite material, and no substances that cause pollution to the environment are produced during the powder preparation process.
Description
Technical Field
The invention relates to a method for preparing composite powder for laser 3D printing by a sol coating method, and belongs to the technical field of composite powder preparation.
Background
The ceramic reinforced aluminum-based composite material combines excellent specific strength and specific rigidity of a metal matrix and excellent high-temperature mechanical property and wear resistance of a ceramic phase, and is widely applied to the fields of aerospace, automobile manufacturing, nuclear energy equipment and the like. With increasingly complex service conditions and more severe requirements on the performance and efficiency of structural members, structural materials must simultaneously meet various performance requirements, and the production and application of traditional composite materials are limited to a certain extent.
In the prior art, ceramic particles are selected from refractory metal borides, carbides, nitrides, silicides and sulfides, a plurality of reinforcement mixed reinforced metal matrix composite materials are prepared by a powder metallurgy technology, and the ceramic particles are formed in situ in a metal matrix of the composite reinforced material. It can also be prepared by introducing various nano-reinforcing particles such as Al during atomization powder preparation process2O3、SiC、TiB2、BN、AlN、SiO2、ZrB2、ZrO2The combination of two or more than two kinds of the components makes the atomization pulverization and the nano-particle strengthening completed synchronously, and the matrix and the nano-particle are metallurgically combined, thus realizing the preparation of the multiphase reinforced aluminum matrix composite powder. For laser additive manufacturing, the in-situ synthesis method is still limited to generate a single ceramic phase, and for the preparation of a two-phase composite material, an additional method is mostly adopted. Due to the higher phase interface mismatching degree of the added ceramic phase and the metal matrix and the inevitable stress concentration, the post-treatment cost is greatly increased, which is not beneficial to the rapid preparation of the two-phase composite material.
In addition, the TiB is prepared by combining traditional fusion casting and atomization2A method for reinforcing aluminium-based composite powders, based on the main principle of using a mixed fluoride salt (KBF)4+K2TiF6) Reaction method, in-situ self-producing TiB in aluminium melt2Reinforcing phase to produce TiB2Reinforcing aluminum-based composite material casting blank, and preparing TiB from the casting blank by an atomization method2A reinforced aluminum matrix composite powder. This method is due to KBF in the preparation process4It is decomposed at high temperature or quickly hydrolyzed by water vapor to generate a great amount of toxic smog and cause environmental pollution. In addition, the reinforcing phase in the aluminum matrix composite material prepared by the method is often larger in size and easy to agglomerate, and the improvement of the comprehensive performance of the composite material is not facilitated.
Disclosure of Invention
The invention aims at the problems that the double reinforced phases of the laser additive manufacturing composite material in the prior art can not be synthesized simultaneously and the prior TiB2The problem of the preparation method of the reinforced aluminum-based composite material powder is to provide a sol coating methodThe invention discloses a method for preparing composite powder for laser 3D printing, which is characterized in that a titanium dioxide precursor and a hydrolysis inhibitor react in deionized water by a sol-gel method to obtain TiO2Sol of TiO2The sol is evenly coated on the surface of the B powder to prepare TiO2Coating the composite powder with @ B, and adding TiO2And carrying out vacuum ball milling treatment on the @ B coated composite powder and the aluminum alloy powder to obtain the composite powder for laser 3D printing. The powder material prepared by the method is used for the laser additive manufacturing process, and TiO is used2B can be fully contacted and reacted in an AlSi10Mg alloy melt to generate TiB in situ2And B2O3A ceramic reinforcement; the method can improve the utilization rate of the aluminum alloy powder to laser, is beneficial to improving the comprehensive performance of the composite material, and does not generate substances which pollute the environment in the powder preparation process.
A method for preparing composite powder for laser 3D printing by a sol coating method comprises the following specific steps:
(1) slowly dropping a titanium dioxide precursor and a hydrolysis inhibitor into deionized water, uniformly mixing, adjusting the pH value of a system to 2-3 by using dilute nitric acid under the stirring condition, and stirring for reacting for 8-10 h to obtain TiO2Sol;
(2) adding pure B powder to TiO2Mixing the sol evenly to make TiO2Uniformly coating the sol on the surface of pure B powder, aging at room temperature, drying and grinding to obtain TiO2@ B coated composite powder;
(3) adding TiO into the mixture2And carrying out ball milling treatment on the @ B coated composite powder and aluminum alloy powder to obtain the composite powder for laser 3D printing.
The titanium dioxide precursor in the step (1) is titanate, and the titanate is ethyl titanate, propyl titanate or butyl titanate.
The hydrolysis inhibitor in the step (1) is a mixture of glacial acetic acid and absolute ethyl alcohol, the glacial acetic acid accounts for 10-20% of the total volume of the glacial acetic acid and the absolute ethyl alcohol, and the volume ratio of the titanium dioxide precursor to the hydrolysis inhibitor to the deionized water is 1:3.5: 2-1: 4: 2.
The pure B powder in the step (2) is amorphous powder, and the particle size of the pure B powder is 1 to E5μm，TiO2TiO in @ B coated composite powder2The mass ratio of B to B was 11: 5.
And (3) ageing at room temperature for 2-3 days.
Preferably, the grinding process in the step (2) is carried out in a horizontal or planetary ball mill, the ratio of stainless steel grinding balls to phi 5 to phi 10 is 2 to 1, the ball-to-material ratio is 10 to 1, the fixed rotation speed is 150-250 rpm, the ball milling is carried out for 20min each time, the suspension time is 10min, and the total grinding time is 3-4 h;
the aluminum alloy powder in the step (3) is spherical powder, the particle size of the aluminum alloy powder is 15-105 micrometers, and preferably, the particle size of the powder used in the selective laser melting process is 15-53 micrometers; the particle size of the powder used in the laser near-net forming process is 53-105 μm;
TiO in composite powder for laser 3D printing2The mass fraction of the @ B coated powder is 1-10%.
Further, the aluminum alloy powder is AlSi10Mg alloy powder, AlSi7Mg alloy powder or other aluminum alloy powder for laser additive manufacturing.
Furthermore, the AlSi10Mg alloy powder comprises, by mass, 9-11% of Si, 0.2-0.45% of Mg, less than or equal to 0.55% of Fe, less than or equal to 0.45% of Mn, less than or equal to 0.05% of Cu, less than or equal to 0.15% of Ti, less than or equal to 0.1% of Zn, less than or equal to 0.05% of Sn, and the balance of Al.
Further, the AlSi7Mg alloy powder comprises, by mass, 6.5-7.5% of Si, 0.25-0.45% of Mg, less than or equal to 0.5% of Fe, less than or equal to 0.35% of Mn, less than or equal to 0.2% of Cu, less than or equal to 0.25% of Ti, less than or equal to 0.3% of Zn, less than or equal to 0.01% of Sn, and the balance of Al;
preferably, in the ball milling process in the step (3), the ratio of stainless steel milling balls phi 5 to phi 10 is 3 to 1, the ball-material ratio is 5 to 1, the fixed rotation speed is 200-300 rpm, and the ball milling mixing time is 2-3 h;
the TiO is2The powder is anatase type TiO2Powder or rutile TiO2And (3) powder.
The reaction equation of the in-situ synthesis related to the invention is
In which the mole ratioThe ratio is n (TiO)2) N (B) 3:10, molar mass ratio M (TiO)2) M (B) 79.9:10.81, M (TiO) is determined as mass ratio of reactants according to the mass relation of substances, M is n.M2):m(B)＝11:5。
The composite powder prepared by the method is used for laser 3D printing of ceramic reinforced metal matrix composite material, TiO2The @ B coated composite powder can be subjected to in-situ chemical reaction under the action of laser beam, and can be used for simultaneously synthesizing two required reinforcing phases TiB2And B2O3And the content of the reinforcing phase can be accurately regulated and controlled according to the stoichiometric ratio of the chemical reaction.
Preparation principle of composite powder for laser 3D printing: titanate as TiO2The precursor of (1) and the mixed solution of glacial acetic acid and absolute ethyl alcohol are used as hydrolysis inhibitors, and a layer of TiO is coated on the surface of pure B particles by a chemical method (sol-gel method)2Gel film, and dispersing it uniformly in AlSi10Mg alloy powder to obtain composite powder for additive manufacturing, and prepared TiO2In the process of laser forming of the @ B coated composite powder particle, TiO on the surface2The gel film is burnt with B particles in an AlSi10Mg alloy melt to synthesize dual-enhanced-phase TiB2And B2O3。
The invention has the beneficial effects that:
(1) in the composite powder for laser 3D printing, TiO2The gel film is tightly coated on the surface of the pure B particles, the gel film and the pure B particles are fully contacted and do not react with AlSi10Mg melt in the laser processing process, and the pollution to a matrix phase is effectively reduced while the in-situ reaction rate is improved;
(2) the invention relates to TiO coated on the surface of B powder in composite powder for laser 3D printing2The gel film can greatly increase the absorption rate of a powder material system to infrared laser, thereby improving the utilization rate of the aluminum alloy powder to the laser and improving the fusion quality of the composite material;
(3) the method of the invention does not generate substances which pollute the environment all the time in the preparation process, and the prepared composite material has small reinforcing phase size, thereby being beneficial to improving the comprehensive performance of the composite material.
Drawings
FIG. 1 is a flow chart of a process for preparing composite powder for laser 3D printing;
fig. 2 is a microstructure morphology of an aluminum-based composite material prepared from the composite powder for laser 3D printing in example 1.
Detailed Description
The present invention is further described in detail below with reference to specific examples, which will assist those skilled in the art in further understanding the present invention, but are not intended to limit the present invention in any way. It should be noted that various modifications and improvements can be made without departing from the spirit of the invention and still fall within the scope of the invention.
Example 1: a method for preparing composite powder for laser 3D printing by a sol coating method (see figure 1) comprises the following specific steps:
(1) slowly dripping a titanium dioxide precursor (butyl titanate) and a hydrolysis inhibitor into deionized water, uniformly mixing, adjusting the pH value of a system to 2.5 by adopting dilute nitric acid under the condition of vigorous stirring, and stirring and reacting for 8 hours at the temperature of 50 ℃ to obtain yellow and transparent TiO2Sol; wherein the hydrolysis inhibitor is a mixture of glacial acetic acid and absolute ethyl alcohol, the glacial acetic acid accounts for 10% of the total volume of the glacial acetic acid and the absolute ethyl alcohol, and the volume ratio of the titanium dioxide precursor to the hydrolysis inhibitor to the deionized water is 1:4: 2;
(2) adding pure B powder to TiO2Mixing the sol evenly to make TiO2Uniformly coating the sol on the surface of pure B powder, aging at room temperature for 48h, drying at 80 deg.C, and grinding to obtain TiO2@ B coated composite powder; wherein the pure B powder is amorphous powder, has purity of not less than 99.99%, average particle diameter of 2 μm, and TiO2TiO in @ B coated composite powder2The mass ratio of the B to the B is 11: 5; the grinding process is carried out in a planetary ball mill, the ratio of stainless steel grinding balls phi 5 to phi 10 is 2 to 1, the ball-material ratio is 10 to 1, the fixed rotation speed is 250rpm, the ball milling is carried out for 20min every time, the grinding is suspended for 10min, the powder temperature is prevented from rising, and the total grinding time is 3 h;
(3) adding TiO into the mixture2The @ B coated composite powder and the AlSi10Mg alloy powder are placedPerforming ball milling treatment in a planetary ball mill to obtain composite powder for laser 3D printing; wherein the TiO in the composite powder for laser 3D printing2The mass fraction of the @ B coated composite powder was 1%, the AlSi10Mg alloy powder was a spherical powder having an average particle diameter of 33.5 μm, and in mass percentage, the AlSi10Mg alloy powder contained 9.87% Si, 0.3% Mg, 0.09% Fe, 0.036% Mn, 0.019% Cu, 0.014% Ti, 0.01% Zn, 0.01% Sn, and the balance Al; in the ball milling process, the ratio of stainless steel grinding balls phi 5 to phi 10 is 3 to 1, the ball-material ratio is 5 to 1, the fixed rotation speed is 200rpm, and the ball milling mixing time is 2 hours;
in this example, the composite powder for laser 3D printing is processed by laser to form in-situ authigenic reinforcing phase (TiB)2+B2O3) The mass content of (A) is 1%;
the microstructure and morphology of the ceramic reinforced metal matrix composite prepared from the composite powder by laser additive manufacturing in the embodiment is shown in fig. 2, and as can be seen from fig. 2, the composite powder generates fine needle-like TiB under the action of high-energy laser2And B2O3And (4) a reinforcing phase.
Example 2: a method for preparing composite powder for laser 3D printing by a sol coating method (see figure 1) comprises the following specific steps:
(1) slowly dripping a titanium dioxide precursor (ethyl titanate) and a hydrolysis inhibitor into deionized water, uniformly mixing, adjusting the pH value of a system to 2 by adopting dilute nitric acid under the condition of vigorous stirring, and stirring and reacting for 10 hours at the temperature of 60 ℃ to obtain yellow and transparent TiO2Sol; wherein the hydrolysis inhibitor is a mixture of glacial acetic acid and absolute ethyl alcohol, the glacial acetic acid accounts for 20% of the total volume of the glacial acetic acid and the absolute ethyl alcohol, and the volume ratio of the titanium dioxide precursor to the hydrolysis inhibitor to the deionized water is 1:3.5: 2;
(2) adding pure B powder to TiO2Mixing the sol evenly to make TiO2Uniformly coating the sol on the surface of pure B powder, aging at room temperature for 72h, drying at 80 deg.C, and grinding to obtain TiO2@ B coated composite powder; wherein the pure B powder is amorphous powder, has purity of not less than 99.99%, average particle diameter of 5 μm, and TiO content2@ B coated compositeTiO in powder2The mass ratio of the B to the B is 11: 5; the grinding process is carried out in a planetary ball mill, the ratio of stainless steel grinding balls phi 5 to phi 10 is 2 to 1, the ball-material ratio is 10 to 1, the fixed rotation speed is 250rpm, the ball milling is carried out for 20min every time, the grinding is suspended for 10min, the powder temperature is prevented from rising, and the total grinding time is 3 h;
(3) adding TiO into the mixture2Putting the @ B coated composite powder and AlSi7Mg alloy powder into a planetary ball mill for ball milling treatment to obtain composite powder for laser 3D printing; wherein the TiO in the composite powder for laser 3D printing2The mass fraction of the @ B-coated composite powder was 10%, the AlSi7Mg alloy powder was a spherical powder having an average particle diameter of 77.5 μm, and 6.97% by mass of Si, 0.35% by mass of Mg, 0.05% by mass of Fe, 0.025% by mass of Mn, 0.015% by mass of Cu, 0.015% by mass of Ti, 0.1% by mass of Zn, 0.01% by mass of Sn, and the balance of Al in the AlSi7Mg alloy powder; in the ball milling process, the ratio of stainless steel grinding balls phi 5 to phi 10 is 3 to 1, the ball-material ratio is 5 to 1, the fixed rotation speed is 200rpm, and the ball milling mixing time is 3 hours;
in this example, the composite powder for laser 3D printing is processed by laser to form in-situ authigenic reinforcing phase (TiB)2+B2O3) The mass content of (A) is 10%;
the microstructure morphology of the ceramic reinforced metal matrix composite prepared from the composite powder through laser additive in the embodiment can be known, and the composite powder generates fine acicular TiB under the action of high-energy laser2And B2O3And (4) a reinforcing phase.
Example 3: a method for preparing composite powder for laser 3D printing by a sol coating method (see figure 1) comprises the following specific steps:
(1) slowly dripping a titanium dioxide precursor (butyl titanate) and a hydrolysis inhibitor into deionized water, uniformly mixing, adjusting the pH value of a system to 3 by adopting dilute nitric acid under the condition of vigorous stirring, and stirring and reacting for 7 hours at the temperature of 55 ℃ to obtain yellow and transparent TiO2Sol; wherein the hydrolysis inhibitor is a mixture of glacial acetic acid and absolute ethyl alcohol, the glacial acetic acid accounts for 15% of the total volume of the glacial acetic acid and the absolute ethyl alcohol, and the volume ratio of the titanium dioxide precursor to the hydrolysis inhibitor to the deionized water is 1:3.7: 2;
(2) will be pureB powder addition to TiO2Mixing the sol evenly to make TiO2Uniformly coating the sol on the surface of pure B powder, aging at room temperature for 60h, drying at 80 deg.C, and grinding to obtain TiO2@ B coated composite powder; wherein the pure B powder is amorphous powder, has purity of not less than 99.99%, average particle diameter of 3 μm, and TiO content2TiO in @ B coated composite powder2The mass ratio of the B to the B is 11: 5; the grinding process is carried out in a planetary ball mill, the ratio of stainless steel grinding balls phi 5 to phi 10 is 2 to 1, the ball-material ratio is 10 to 1, the fixed rotation speed is 250rpm, the ball milling is carried out for 20min every time, the grinding is suspended for 10min, the powder temperature is prevented from rising, and the total grinding time is 3 h;
(3) adding TiO into the mixture2Putting the @ B coated composite powder and AlSi10Mg alloy powder into a planetary ball mill for ball milling treatment to obtain composite powder for laser 3D printing; wherein the TiO in the composite powder for laser 3D printing2The mass fraction of the @ B coated composite powder was 4%, the AlSi10Mg alloy powder was a spherical powder having an average particle diameter of 33.5 μm, and in mass percentage, the AlSi10Mg alloy powder contained 9.87% Si, 0.3% Mg, 0.09% Fe, 0.036% Mn, 0.019% Cu, 0.014% Ti, 0.01% Zn, 0.01% Sn, and the balance Al; in the ball milling process, the ratio of stainless steel grinding balls phi 5 to phi 10 is 3 to 1, the ball-material ratio is 5 to 1, the fixed rotation speed is 200rpm, and the ball milling mixing time is 3 hours;
in this example, the composite powder for laser 3D printing is processed by laser to form in-situ authigenic reinforcing phase (TiB)2+B2O3) The mass content of (A) is 4%;
the microstructure morphology of the ceramic reinforced metal matrix composite prepared from the composite powder through laser additive in the embodiment can be known, and the composite powder generates fine acicular TiB under the action of high-energy laser2And B2O3And (4) a reinforcing phase.
While particular embodiments of the present invention have been described, it is to be understood that the invention is not limited to the precise embodiments described, and that various changes and modifications may be effected therein by one skilled in the art within the scope of the appended claims and the scope of the invention is to be accorded the full scope of the claims.
Claims (9)
1. A method for preparing composite powder for laser 3D printing by a sol coating method is characterized by comprising the following specific steps:
(1) slowly dropping a titanium dioxide precursor and a hydrolysis inhibitor into deionized water, uniformly mixing, adjusting the pH value of a system to 2-3 by using dilute nitric acid under the stirring condition, and stirring for reacting for 8-10 h to obtain TiO2Sol;
(2) adding pure B powder to TiO2Mixing the sol evenly to make TiO2Uniformly coating the sol on the surface of pure B powder, aging at room temperature, drying and grinding to obtain TiO2@ B coated composite powder;
(3) adding TiO into the mixture2And carrying out ball milling treatment on the @ B coated composite powder and aluminum alloy powder to obtain the composite powder for laser 3D printing.
2. The method for preparing the composite powder for laser 3D printing according to the sol coating method of claim 1, wherein the sol coating method comprises the following steps: the titanium dioxide precursor in the step (1) is titanate, and the titanate is ethyl titanate, propyl titanate or butyl titanate.
3. The method for preparing the composite powder for laser 3D printing according to the sol coating method of claim 1, wherein the sol coating method comprises the following steps: the hydrolysis inhibitor in the step (1) is a mixture of glacial acetic acid and absolute ethyl alcohol, the glacial acetic acid accounts for 10-20% of the total volume of the glacial acetic acid and the absolute ethyl alcohol, and the volume ratio of the titanium dioxide precursor to the hydrolysis inhibitor to the deionized water is 1:3.5: 2-1: 4: 2.
4. The method for preparing the composite powder for laser 3D printing according to the sol coating method of claim 1, wherein the sol coating method comprises the following steps: the pure B powder in the step (2) is amorphous powder, the particle size of the pure B powder is 1-5 mu m, and TiO is2TiO in @ B coated composite powder2The mass ratio of B to B was 11: 5.
5. The method for preparing the composite powder for laser 3D printing according to the sol coating method of claim 1, wherein the sol coating method comprises the following steps: and (3) ageing at room temperature for 2-3 days.
6. The method for preparing the composite powder for laser 3D printing according to the sol coating method of claim 1, wherein the sol coating method comprises the following steps: the aluminum alloy powder in the step (3) is spherical powder, the particle size of the aluminum alloy powder is 15-105 mu m, and TiO in the composite powder for laser 3D printing2The mass fraction of the @ B coated powder is 1-10%.
7. The method for preparing the composite powder for laser 3D printing according to the sol coating method of claim 1 or 6, wherein: the aluminum alloy powder is AlSi10Mg alloy powder or AlSi7Mg alloy powder.
8. The method for preparing the composite powder for laser 3D printing according to the sol coating method of claim 7, wherein the method comprises the following steps: by mass percentage, 9-11% of Si, 0.2-0.45% of Mg, less than or equal to 0.55% of Fe, less than or equal to 0.45% of Mn, less than or equal to 0.05% of Cu, less than or equal to 0.15% of Ti, less than or equal to 0.1% of Zn, less than or equal to 0.05% of Sn and the balance of Al in the AlSi10Mg alloy powder; 6.5-7.5% of Si, 0.25-0.45% of Mg, less than or equal to 0.5% of Fe, less than or equal to 0.35% of Mn, less than or equal to 0.2% of Cu, less than or equal to 0.25% of Ti, less than or equal to 0.3% of Zn, less than or equal to 0.01% of Sn and the balance of Al in the AlSi7Mg alloy powder.
9. The composite powder prepared by the method of any one of claims 1 to 8 is used for laser additive manufacturing of ceramic reinforced metal matrix composites.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010945029.2A CN112024872B (en) | 2020-09-10 | 2020-09-10 | Method for preparing composite powder for laser 3D printing by sol coating method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010945029.2A CN112024872B (en) | 2020-09-10 | 2020-09-10 | Method for preparing composite powder for laser 3D printing by sol coating method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN112024872A CN112024872A (en) | 2020-12-04 |
| CN112024872B true CN112024872B (en) | 2021-06-08 |
Family
ID=73585314
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010945029.2A Active CN112024872B (en) | 2020-09-10 | 2020-09-10 | Method for preparing composite powder for laser 3D printing by sol coating method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112024872B (en) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114985727B (en) * | 2022-03-09 | 2023-06-02 | 武汉大学 | A kind of in-situ synthesis enhanced additive composite powder, preparation method and application |
| CN115846624B (en) * | 2023-02-28 | 2023-04-28 | 昆明理工大学 | Preparation method of ceramic/iron-based honeycomb structural composite material |
| CN116288337B (en) * | 2023-03-28 | 2025-02-14 | 中北大学 | A method for high-speed laser cladding TiO2/graphene surface dual-phase reinforced ZL101 |
| CN117756535A (en) * | 2023-12-29 | 2024-03-26 | 武汉理工大学 | A light-curing 3D printing zirconium diboride-based ultra-high temperature ceramic slurry and its preparation method and application |
| CN118976907A (en) * | 2024-08-06 | 2024-11-19 | 盐城工业职业技术学院 | A preparation process of high-performance aluminum-based composite materials based on laser additive |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20030054077A (en) * | 2001-12-24 | 2003-07-02 | 서울대학교 공과대학 교육연구재단 | Method to coat ceramic powder with TiO2 and Method to improve wettability of B4C-Al composite material |
| CN1710125A (en) * | 2005-05-27 | 2005-12-21 | 哈尔滨工业大学 | Preparation method of in-situ self-generated aluminum matrix composites by reactive hot pressing |
| US9138806B2 (en) * | 2012-12-19 | 2015-09-22 | King Saud University | In-situ combustion synthesis of titanium carbide (TiC) reinforced aluminum matrix composite |
| CN105728734A (en) * | 2016-03-24 | 2016-07-06 | 西安工业大学 | High-strength ultra-fine (TixBy-TiC)/7075Al composite material and its preparation method |
| CN107760933A (en) * | 2017-09-11 | 2018-03-06 | 南京航空航天大学 | A kind of 3D printing strengthens Al alloy powder and preparation method thereof with in-situ nano complex phase ceramic |
| CN108754242A (en) * | 2018-06-15 | 2018-11-06 | 淮阴工学院 | A kind of in-situ endogenic is micro-/receive across scale ceramic phase collaboration reinforced aluminum matrix composites and its manufacturing process |
| CN110512111A (en) * | 2018-04-11 | 2019-11-29 | 上海交通大学 | Preparation method of in situ aluminum matrix composite |
| CN111118323A (en) * | 2020-01-07 | 2020-05-08 | 昆明理工大学 | Preparation method of metal ceramic composite powder for laser 3D printing |
-
2020
- 2020-09-10 CN CN202010945029.2A patent/CN112024872B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20030054077A (en) * | 2001-12-24 | 2003-07-02 | 서울대학교 공과대학 교육연구재단 | Method to coat ceramic powder with TiO2 and Method to improve wettability of B4C-Al composite material |
| CN1710125A (en) * | 2005-05-27 | 2005-12-21 | 哈尔滨工业大学 | Preparation method of in-situ self-generated aluminum matrix composites by reactive hot pressing |
| US9138806B2 (en) * | 2012-12-19 | 2015-09-22 | King Saud University | In-situ combustion synthesis of titanium carbide (TiC) reinforced aluminum matrix composite |
| CN105728734A (en) * | 2016-03-24 | 2016-07-06 | 西安工业大学 | High-strength ultra-fine (TixBy-TiC)/7075Al composite material and its preparation method |
| CN107760933A (en) * | 2017-09-11 | 2018-03-06 | 南京航空航天大学 | A kind of 3D printing strengthens Al alloy powder and preparation method thereof with in-situ nano complex phase ceramic |
| CN110512111A (en) * | 2018-04-11 | 2019-11-29 | 上海交通大学 | Preparation method of in situ aluminum matrix composite |
| CN108754242A (en) * | 2018-06-15 | 2018-11-06 | 淮阴工学院 | A kind of in-situ endogenic is micro-/receive across scale ceramic phase collaboration reinforced aluminum matrix composites and its manufacturing process |
| CN111118323A (en) * | 2020-01-07 | 2020-05-08 | 昆明理工大学 | Preparation method of metal ceramic composite powder for laser 3D printing |
Non-Patent Citations (3)
| Title |
|---|
| Al 6061-TiB2 Metal Matrix Composite Synthesized with Different Reaction Holding Times by In-Situ Method;Lawrance C. A.等;《International Journal of Composite Materials》;20151231;第5卷(第5期);第97-101页 * |
| In situ TiB2 reinforced Al alloy composites;L Lü等;《Scripta Materialia》;20011107;第45卷(第9期);第1017-1023页 * |
| 激光选区熔化成形原位自生TiB2/Al-Si复合材料的微观组织和力学性能;章敏立等;《复合材料学报》;20181130;第35卷(第11期);第3114-3121页 * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN112024872A (en) | 2020-12-04 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN112024872B (en) | Method for preparing composite powder for laser 3D printing by sol coating method | |
| Gao et al. | Selective laser melting of nano-TiN modified AlSi10Mg composite powder with low laser reflectivity | |
| Yang et al. | Fabrication and characterization of electroless Ni–P–ZrO 2 nano-composite coatings | |
| Zhao et al. | Fabrication of magnesium-coated graphene and its effect on the microstructure of reinforced AZ91 magnesium-matrix composites | |
| CN101608270A (en) | A high-efficiency and low-cost aluminum and aluminum alloy refiner and preparation method thereof | |
| CN102102158A (en) | Micro-nano particle reinforced aluminum-based composite material and preparation method thereof | |
| CN109704770B (en) | Self-lubricating ceramic tool material with nickel-coated hexagonal boron nitride nanosheet composite powder and preparation method thereof | |
| CN111206166A (en) | A kind of preparation method of in-situ ternary nanoparticle reinforced aluminum matrix composite material | |
| CN114985727B (en) | A kind of in-situ synthesis enhanced additive composite powder, preparation method and application | |
| CN109295347A (en) | A kind of aluminum alloy material that can be used for online hydrogen supply | |
| CN105568101A (en) | High-strength magnalium alloy and preparation method thereof | |
| CN108817409A (en) | A kind of preparation method of enhancement metal metal-matrix composite material | |
| CN109014182A (en) | Increasing material manufacturing 7000 line aluminium alloy powder and preparation method thereof | |
| CN111118323A (en) | Preparation method of metal ceramic composite powder for laser 3D printing | |
| FR2649973A1 (en) | PROCESS FOR THE PREPARATION OF COMPOSITE CERAMIC POWDERS AND POWDERS OBTAINED BY THE PROCESS | |
| CN113308630A (en) | In-situ CNTs @ Ti hybrid reinforced aluminum matrix composite and preparation method thereof | |
| CN102251130B (en) | Preparation method of superfine grain cemented carbide | |
| CN1995418A (en) | Preparation method of granule-mixed reinforced aluminium-based composite material | |
| CN104628385A (en) | Boric nano titanium carbonitride solid solution powder and preparation method thereof | |
| CN1226438C (en) | Method for preparing aluminium base alloy of containing T10 and AL2O3 particles | |
| CN1078257C (en) | Melting-casting process of preparing metal-base composite material through in-situ reaction and spray formation | |
| CN100376700C (en) | Al-Zr-B-O reaction system for the synthesis of high-performance aluminum-based in-situ composites and its new materials | |
| Yu et al. | Effect of processing techniques on interface bonding of graphene reinforced metal matrix composites: a review | |
| JPH10102163A (en) | Intermetallic compound reinforced magnesium base composite material and its production | |
| CN1865473A (en) | Nickel-silicon-boron intermediate alloy and process for preparing same |
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 | ||
| OL01 | Intention to license declared | ||
| OL01 | Intention to license declared |