CN111876829B - Optimization method for technological parameters of pulse laser 3D printing of single crystal superalloy - Google Patents

Optimization method for technological parameters of pulse laser 3D printing of single crystal superalloy Download PDF

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CN111876829B
CN111876829B CN202010750272.9A CN202010750272A CN111876829B CN 111876829 B CN111876829 B CN 111876829B CN 202010750272 A CN202010750272 A CN 202010750272A CN 111876829 B CN111876829 B CN 111876829B
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printing
single crystal
cladding layer
process parameters
parameters
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CN111876829A (en
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梁静静
慈世伟
李金国
周亦胄
孙晓峰
张宏伟
郑璇
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Taizhou Xinma Technology Industry Development Co ltd
Institute of Metal Research of CAS
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Institute of Metal Research of CAS
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    • CCHEMISTRY; METALLURGY
    • C30CRYSTAL GROWTH
    • C30BSINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
    • C30B29/00Single crystals or homogeneous polycrystalline material with defined structure characterised by the material or by their shape
    • C30B29/10Inorganic compounds or compositions
    • C30B29/52Alloys
    • 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
    • B33Y10/00Processes of additive manufacturing
    • 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
    • C30CRYSTAL GROWTH
    • C30BSINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
    • C30B30/00Production of single crystals or homogeneous polycrystalline material with defined structure characterised by the action of electric or magnetic fields, wave energy or other specific physical conditions
    • 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 invention provides a preferable method for pulse laser 3D printing of single crystal superalloy process parameters, which comprises the following steps: preparing a metal substrate and metal powder; designing an orthogonal test according to the process range; printing the metal powder on the metal substrate to form a single-channel alloy cladding layer, wherein test process parameters are adjusted in the printing process; obtaining the size of the single-channel alloy cladding layer; obtaining an epitaxial single crystal growth index according to the size of the single-channel alloy cladding layer; forming a mapping function by taking the test process parameters as independent variables and the epitaxial single crystal growth indexes as dependent variables, and obtaining correlation parameters of the independent variables and the dependent variables through linear fitting; and acquiring the influence trend of the independent variable on the dependent variable through the correlation parameter. By establishing the relationship between the process parameters and the epitaxial single crystal growth indexes, the invention can shorten the preparation process flow period of the high-temperature alloy, reduce the manufacturing cost and improve the operation efficiency.

Description

Optimization method for technological parameters of pulse laser 3D printing of single crystal superalloy
Technical Field
The invention belongs to the technical field of laser 3D printing, and particularly relates to an optimal selection method for technological parameters of pulse laser 3D printing of single crystal superalloy.
Background
The single crystal high temperature alloy is the first choice material of the turbine blade of the current cash aeroengine. The service environment of the single crystal blade is severe, the preparation cost is high, if the damaged blade can be repaired by adopting a proper method, the blade replacement is reduced, and the method has great economic significance and engineering significance. Laser melt molding (LMF) is a 3D printing method that uses a coaxial powder feed mode, which is widely used to produce and repair formed parts due to low heat input and high cooling rate. When LMF is applied to repair or manufacture of Single Crystal (SC) superalloy components, particularly SC turbine blades, it is necessary to ensure epitaxial growth of dendrites and control the formation of stray grains in front of the solid-liquid interface, i.e., to avoid the occurrence of single crystal to equiaxed crystal transformation (CET), because when CET occurs, stray crystals are formed, which affect the performance of the repair zone.
In addition, the production efficiency and powder utilization of the LMF process are also critical to the manufacture or repair of the actual single crystal. Although single crystal superalloy can be prepared by pulsed laser, the processing microstructure relation between the pulsed laser parameters and the CET, the production efficiency and the powder use efficiency is not systematically researched, so that a preferred method for 3D printing of the single crystal superalloy process parameters by the pulsed laser is needed.
Disclosure of Invention
Therefore, the technical problem to be solved by the invention is to provide a preferred method for pulse laser 3D printing of single crystal superalloy process parameters, which can shorten the preparation process flow period of the superalloy, reduce the manufacturing cost and improve the operation efficiency by establishing the relationship between the process parameters and the epitaxial single crystal growth indexes.
In order to solve the above problems, the present invention provides a preferred method for 3D printing of single crystal superalloy process parameters by using pulsed laser, comprising the following steps:
preparing a metal substrate and metal powder;
designing an orthogonal test according to the process range;
printing the metal powder on the metal substrate to form a single-channel alloy cladding layer, wherein test process parameters are adjusted in the printing process;
obtaining the size of the single-channel alloy cladding layer;
obtaining an epitaxial single crystal growth index according to the size of the single-channel alloy cladding layer;
forming a mapping function by taking the test process parameters as independent variables and the epitaxial single crystal growth indexes as dependent variables, and obtaining correlation parameters of the independent variables and the dependent variables through linear fitting;
and acquiring the influence trend of the independent variable on the dependent variable through the correlation parameter.
Preferably, the test process parameters comprise at least one of laser output power P, pulse width t and powder feeding rate m; the sizes of the single-channel alloy cladding layer comprise a cladding layer height H and a deposition height HDEpitaxial growth height HEAt least one of the area S of the cladding area with the single-channel length L and the alloy density rho; the epitaxial single crystal growth index comprises a difference value (R) between an epitaxial growth ratio and a cladding ratioE-RD) Deposition height HDAt least one of the width W of the cladding layer and the utilization rate eta of the powder, wherein RE=HE/H,RD=HD/H,η=S×L×ρ÷m÷T÷6×10-13X 100%, wherein T is cladding time, H, HR, HD, HE, L, HS are all in mum, and S is in mum2P is in the unit of W, T and T are in the unit of s, m is in the unit of g/min, rho is in the unit of g/cm3
Preferably, the obtaining of the influence trend of the independent variable on the dependent variable through the correlation parameter comprises:
taking an absolute value of the correlation parameter and normalizing to form a normalized correlation parameter;
and drawing a radar chart by using the normalized correlation parameters.
Preferably, before the metal powder printing is carried out, the surface of the metal substrate is subjected to grinding and/or cleaning and drying treatment.
Preferably, the metal substrate after being cleaned and dried is placed on a constant-temperature water-cooling copper substrate workbench in a glove box under the protection of inert gas through a transition bin.
Preferably, the metal powder is dried and cooled in a vacuum oven before the metal powder printing is performed.
Preferably, before the metal powder printing is performed, the distance between the laser head of the numerical control machine and the metal substrate is adjusted to 14mm-16 mm.
Preferably, the adjustment of the test process parameters during the printing process is achieved by means of a preset program.
Preferably, the preset program is a pulsed laser 3D printing G code.
Preferably, the pulsed laser 3D printing G code is generated using Python programming.
According to the optimal selection method for the pulse laser 3D printing of the single crystal superalloy process parameters, the corresponding test process parameters are adjusted in a larger range, the adjusted test process parameters are further adopted for laser 3D printing to form the alloy cladding layer, the corresponding epitaxial single crystal growth indexes can be further known through obtaining the size of the single channel alloy cladding layer, the influence trends of the test process parameters and the epitaxial single crystal growth indexes are further clarified through the correlation parameters between the test process parameters and the epitaxial single crystal growth indexes, and an operator can clarify the selection of the relevant process parameters in the specific pulse laser 3D printing of the single crystal superalloy according to the trend, so that the preparation process flow period of the superalloy can be obviously shortened, the manufacturing cost is reduced, and the like, The technical scheme of the invention can provide the adjustment trend of the associated parameters of the large-size metal single crystal structural member with uniform longitudinal gradient performance, and provides technical support for the field of rapid manufacturing.
Drawings
FIG. 1 is a schematic step diagram of a preferred method for 3D printing parameters of a single crystal superalloy process by using a pulsed laser in a pipe forming apparatus according to an embodiment of the present invention;
FIG. 2 is a schematic size diagram of a single-pass alloy cladding layer printed according to an embodiment of the present invention;
FIG. 3 is a radar chart plotted with normalized correlation parameters in an embodiment of the present invention;
FIG. 4 is a physical diagram of a single-pass alloy cladding layer printed by using the preferred process parameters of the preferred method of the present invention;
FIG. 5 is an EBSD photograph under an electron microscope at A in FIG. 4.
Detailed Description
Referring to fig. 1 to 5 in combination, according to an embodiment of the present invention, there is provided a preferred method for 3D printing single crystal superalloy process parameters by using a pulsed laser, including the following steps:
preparing a metal substrate and metal powder;
designing an orthogonal test according to a process range, wherein the process range specifically refers to a rough range of test process parameters adopted when laser 3D printing is adopted for an alloy material of a certain material;
printing the metal powder on the metal substrate to form a single-channel alloy cladding layer, wherein test process parameters are adjusted in the printing process;
obtaining the size of the single-channel alloy cladding layer;
obtaining an epitaxial single crystal growth index according to the size of the single-channel alloy cladding layer;
forming a mapping function by taking the test process parameters as independent variables and the epitaxial single crystal growth indexes as dependent variables, and obtaining correlation parameters of the independent variables and the dependent variables through linear fitting;
and acquiring the influence trend of the independent variable on the dependent variable through the correlation parameter.
In the technical scheme, the corresponding test process parameters are adjusted in a larger range, the adjusted test process parameters are further adopted for laser 3D printing to form the alloy cladding layer, the corresponding epitaxial single crystal growth indexes can be further known through obtaining the size of the single-channel alloy cladding layer, the influence trend of the test process parameters and the epitaxial single crystal growth indexes is further clarified through the correlation parameters between the test process parameters and the epitaxial single crystal growth indexes, and an operator can clearly select the related process parameters in the specific process of 3D single crystal high-temperature alloy printing by using pulse laser according to the trend, so that the preparation process flow period of the high-temperature alloy can be obviously shortened, the manufacturing cost is reduced, the operating efficiency is improved, and further, the technical scheme of the invention can provide the adjustment trend of the correlation parameters of the large-size metal single crystal structural component with uniform longitudinal gradient performance The method provides technical support for the field of rapid manufacturing.
Further, the test process parameters comprise at least one of laser output power P, pulse width t and powder feeding speed m; as shown in FIG. 2, the dimensions of the single-pass alloy cladding layer comprise a cladding layer height H and a remelting height HRDeposition height HDEpitaxial growth height HELength L of single channel, height H of impurity crystal regionSAt least one of the area S of the cladding area and the alloy density rho; the epitaxial single crystal growth index comprises a difference value (R) between an epitaxial growth ratio and a cladding ratioE-RD) Deposition height HDAt least one of the width W of the cladding layer and the utilization rate eta of the powder, wherein RE=HE/H,RD=HD/H,η=S×L×ρ÷m÷T÷6×10-13X 100%, wherein T is the cladding time.
The acquiring the influence trend of the independent variable on the dependent variable through the correlation parameter comprises the following steps:
taking an absolute value of the correlation parameter and normalizing to form a normalized correlation parameter;
and drawing a radar chart by using the normalized correlation parameters.
According to the technical scheme, the correlation parameters are processed through normalization, the data processing process is simplified, and the influence of each influence factor (namely the test process parameters) on the epitaxial single crystal growth index can be more visual by drawing a radar chart through the normalized correlation parameters, so that the adjustment of the operator on the correlation process parameters can be more clearly guided.
Before metal powder printing, the surface of the metal substrate is polished and/or cleaned and dried, the surface roughness of the metal substrate is changed, the surface of the metal substrate is kept smooth and clean, and the quality of a single-channel alloy cladding layer formed in a subsequent printing test can be guaranteed. Specifically, for example, before the test, the metal substrate is firstly polished by different types of sand paper, the surface roughness Ra of the metal substrate is controlled to be 2.5-5.0 μm, then the polished metal substrate is washed by absolute ethyl alcohol and dried by a blower, the surface is ensured to be flat and clean, and the metal substrate is sequentially placed into a glove vacuum box comprising a CNC (computer numerical control) machine tool to prevent the oxidation of a cladding layer in the test process. The metal substrate is formed by cutting a metal material to a specification of 50mm multiplied by 10mm multiplied by 5mm, the length of 50mm can ensure enough cladding distance, and the thickness of 5mm ensures that the metal substrate cannot deform greatly in a test.
And putting the cleaned and dried metal substrate on a constant-temperature water-cooling copper substrate workbench in a glove box protected by inert gas through a transition bin, so that the heat of the metal substrate printing the single-channel alloy cladding layer can be dissipated as soon as possible.
Preferably, before printing the metal powder, the metal powder is dried and cooled in a vacuum drying oven, and the moisture in the metal powder is removed to improve the uniformity and the fluidity of the metal powder, wherein the particle size of the metal powder is 53-105 μm.
Preferably, before the metal powder printing is carried out, the distance between a laser head of the numerical control machine tool and the metal substrate is adjusted to be 14-16 mm, preferably 15mm, so as to ensure that the laser beam and the metal powder flow sent out by the coaxial four argon powder feeding pipelines are well converged.
Preferably, the test process parameters are adjusted in the printing process by a preset program, specifically, the preset program is a pulse laser 3D printing G code, and the pulse laser 3D printing G code is generated by Python programming.
To further illustrate the technical solution of the present invention, the following description is given with reference to specific examples.
Examples
(1) The metal material was cut into a size of 50mm × 10mm × 5mm to obtain a substrate required for the test, i.e., the metal substrate described above. Before testing, firstly, polishing the metal substrate by using different types of abrasive paper, controlling the surface roughness Ra of the metal substrate to be 2.5-5.0 mu m, then cleaning the polished metal substrate by using absolute ethyl alcohol, drying the metal substrate by using a blower, ensuring the surface to be flat and clean, and sequentially putting the metal substrate into a glove vacuum box comprising a CNC (computerized numerical control) machine tool to prevent a cladding layer from being oxidized in the testing process;
(2) before testing, firstly drying and cooling metal powder for printing in a vacuum drying oven, and removing moisture in the metal powder to improve the uniformity and the fluidity of the metal powder, wherein the particle size of the metal powder is 53-105 μm;
(3) putting the dried metal substrate on a constant-temperature water-cooling copper substrate workbench in a glove box under the protection of inert gas after passing through a transition bin;
(4) generating a pulse laser 3D printing G code by utilizing Python software;
(5) adjusting the distance between the laser head and the metal substrate to be controlled to be 15mm so as to ensure that the converging effect of the laser beam and the powder flow sent out by the coaxial four-way argon powder feeding pipeline is good;
(6) loading a pre-designed CNC G code in a numerical control system of the CNC numerical control machine tool; and then, adjusting test process parameters (such as those shown in table 1) to be changed on the control panel in sequence, wherein the test process parameters comprise laser output power P, pulse width t and powder feeding rate m, and then performing a printing test.
Setting P, t and m as variables, wherein the variation ranges are respectively that P is 800W-3000W, the pulse width t is 0.1-0.28 s, and the powder feeding rate is set that m is 10-20 g/min.
Table 1 experimental process parameters for which processing can be carried out
Serial number P(W) t(s) m(g/min)
1 1800 0.1 5
2 1800 0.16 10
3 1800 0.28 20
4 2200 0.1 10
5 2200 0.16 20
6 2200 0.28 5
7 2600 0.1 20
8 2600 0.16 5
9 2600 0.28 10
After the single-channel alloy cladding layer is printed, taking the longitudinal section of the cladding layer as a statistical object (as shown in figure 2), wherein the statistical parameters comprise the height H of the cladding layer and the remelting height HRDeposition height HDEpitaxial growth height HELength L of single channel, height H of impurity crystal regionSAnd the area S of the cladding area and the alloy density rho, and by combining the obtained statistical parameters with the actual time consumption T of 3D printing, the following can be obtained: powder utilization rate eta ═ SxLxrho ÷ m ÷ Tx100%
Describing the difference (R) of the process parameters P, t and m to the epitaxial growth ratio and the cladding ratio through a functional relationshipE—RD) Deposition height HDThe influence of other indexes such as the width W of the cladding layer, the utilization rate eta of the powder and the like is shown as a function formula (1):
Figure BDA0002609848080000061
wherein a, b, c, d, a1, b1, c1, d1, a2, b2, c2, d2, a3, b3, c3 and d3 are the briefly described correlation parameters and are obtained by origin software linear fitting experimental results. The fitting data are equation (2).
Figure BDA0002609848080000062
The absolute values of four groups of data of a, b, c, a1, b1, c1, a2, b2, c2, a3, b3 and c3 are taken and then normalized. The normalized correlation parameters a, b, c, a1, b1, c1, a2, b2, c2, a3, b3 and c3 are obtained, and the radar map shown in fig. 3 is drawn according to the above normalized data, wherein the marked points of various shapes in the map are represented by positive correlation in a solid way, and the hollow points are represented by negative correlation in a hollow way.
Table 2 summary of normalized data
Figure BDA0002609848080000071
In order to verify the technical effect of the method of the present invention, the inventor performed printing with optimized process parameters, P2000W, t 0.16s and m 11g/min, and as a result, referring to fig. 4, it can be seen from fig. 5 that the single crystal thin wall was formed by performing pulse laser 3D printing on the single crystal superalloy with the optimized process parameters.
It is readily understood by a person skilled in the art that the advantageous ways described above can be freely combined, superimposed without conflict.
The present invention is not limited to the above preferred embodiments, and any modifications, equivalent substitutions and improvements made within the spirit and principle of the present invention should be included in the protection scope of the present invention. The above is only a preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, several improvements and modifications can be made without departing from the technical principle of the present invention, and these improvements and modifications should also be regarded as the protection scope of the present invention.

Claims (8)

1. A preferable method for 3D printing of single crystal superalloy process parameters by pulse laser is characterized by comprising the following steps:
preparing a metal substrate and metal powder;
designing an orthogonal test according to the process range;
printing the metal powder on the metal substrate to form a single-channel alloy cladding layer, wherein test process parameters are adjusted in the printing process;
obtaining the size of the single-channel alloy cladding layer;
obtaining an epitaxial single crystal growth index according to the size of the single-channel alloy cladding layer;
forming a mapping function by taking the test process parameters as independent variables and the epitaxial single crystal growth indexes as dependent variables, and obtaining correlation parameters of the independent variables and the dependent variables through linear fitting;
acquiring the influence trend of the independent variable on the dependent variable through the correlation parameter;
the test process parameters are laser output power P, pulse width t and powder feeding speed m; the sizes of the single-channel alloy cladding layer comprise a cladding layer height H and a deposition height HDEpitaxial growth height HEAt least one of the length L of the single channel, the area S of the cladding area and the alloy density rho; the epitaxial single crystal growth index comprises a difference value (R) between an epitaxial growth ratio and a cladding ratioE-RD) Deposition height HDAt least one of the width W of the cladding layer and the utilization rate eta of the powder, wherein RE=HE/H,RD= HD/H,η= S×L×ρ÷m÷T÷6×10-13X 100%, wherein T is the cladding time;
the acquiring the influence trend of the independent variable on the dependent variable through the correlation parameter comprises the following steps:
taking an absolute value of the correlation parameter and normalizing to form a normalized correlation parameter;
and drawing a radar chart by using the normalized correlation parameters.
2. The preferred method of claim 1, wherein the surface of the metal substrate is subjected to a grinding and/or cleaning bake process prior to metal powder printing.
3. The preferable method according to claim 2, wherein the metal substrate after the cleaning and drying treatment is placed on a constant temperature water-cooled copper substrate workbench in an inert gas-protected glove box through a transition bin.
4. The preferred method of claim 1, wherein the metal powder is dried and cooled in a vacuum oven prior to printing the metal powder.
5. The preferred method according to claim 1, wherein the distance between the laser head of the numerically controlled machine tool and the metal substrate is adjusted to 14mm to 16mm before the metal powder printing is performed.
6. A preferred method according to claim 1, wherein the trial process parameters are adjusted during printing by means of a pre-set program.
7. The preferred method of claim 6, wherein the pre-set program is a pulsed laser 3D printed G-code.
8. The preferred method of claim 7, wherein the pulsed laser 3D printed G-code is generated using Python programming.
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CN113245560B (en) * 2021-06-03 2021-09-28 恒新增材制造研究中心(佛山)有限公司 Method for rapidly acquiring standard forming parameters of selective laser melting equipment
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Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105108142A (en) * 2015-06-18 2015-12-02 航星利华(北京)科技有限公司 Method for manufacturing monocrystalline and directional solidified part through laser 3D printer
CN105478768A (en) * 2016-01-06 2016-04-13 福建工程学院 3D printing die laser cladding equipment and gradation process
CN107790717A (en) * 2017-11-05 2018-03-13 湖南大学 A kind of quasi-continuous lasing metal 3D printing method for realizing the regulation and control of nickel-base alloy crystallographic texture
CN108846148A (en) * 2018-04-17 2018-11-20 山东大学 A kind of model topology optimization method and apparatus based on TPMS towards 3D printing
CN110640316A (en) * 2019-09-03 2020-01-03 温州大学 Double-beam laser welding optimization method
CN111069599A (en) * 2019-12-02 2020-04-28 西安铂力特增材技术股份有限公司 Laser beam energy online monitoring device and monitoring method for 3D printing equipment
CN111331136A (en) * 2020-02-10 2020-06-26 中国科学院金属研究所 Powder feeding laser 3D printing method for metal thin-wall parts with uniform performance
CN111360251A (en) * 2020-02-10 2020-07-03 中国科学院金属研究所 Method for repairing single crystal high-temperature alloy thin-walled workpiece through powder feeding pulse laser 3D printing

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105108142A (en) * 2015-06-18 2015-12-02 航星利华(北京)科技有限公司 Method for manufacturing monocrystalline and directional solidified part through laser 3D printer
CN105478768A (en) * 2016-01-06 2016-04-13 福建工程学院 3D printing die laser cladding equipment and gradation process
CN107790717A (en) * 2017-11-05 2018-03-13 湖南大学 A kind of quasi-continuous lasing metal 3D printing method for realizing the regulation and control of nickel-base alloy crystallographic texture
CN108846148A (en) * 2018-04-17 2018-11-20 山东大学 A kind of model topology optimization method and apparatus based on TPMS towards 3D printing
CN110640316A (en) * 2019-09-03 2020-01-03 温州大学 Double-beam laser welding optimization method
CN111069599A (en) * 2019-12-02 2020-04-28 西安铂力特增材技术股份有限公司 Laser beam energy online monitoring device and monitoring method for 3D printing equipment
CN111331136A (en) * 2020-02-10 2020-06-26 中国科学院金属研究所 Powder feeding laser 3D printing method for metal thin-wall parts with uniform performance
CN111360251A (en) * 2020-02-10 2020-07-03 中国科学院金属研究所 Method for repairing single crystal high-temperature alloy thin-walled workpiece through powder feeding pulse laser 3D printing

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