CN112809003A - Novel optical coaxial powder feeding laser composite additive manufacturing method and device - Google Patents
Novel optical coaxial powder feeding laser composite additive manufacturing method and device Download PDFInfo
- Publication number
- CN112809003A CN112809003A CN202011582642.9A CN202011582642A CN112809003A CN 112809003 A CN112809003 A CN 112809003A CN 202011582642 A CN202011582642 A CN 202011582642A CN 112809003 A CN112809003 A CN 112809003A
- Authority
- CN
- China
- Prior art keywords
- laser
- additive manufacturing
- control system
- coaxial powder
- metal
- 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.)
- Withdrawn
Links
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 57
- 239000000843 powder Substances 0.000 title claims abstract description 52
- 239000000654 additive Substances 0.000 title claims abstract description 39
- 230000000996 additive effect Effects 0.000 title claims abstract description 39
- 230000003287 optical effect Effects 0.000 title claims abstract description 23
- 239000002131 composite material Substances 0.000 title claims abstract description 20
- 239000002184 metal Substances 0.000 claims abstract description 50
- 238000005242 forging Methods 0.000 claims abstract description 32
- 230000000007 visual effect Effects 0.000 claims abstract description 22
- 238000000034 method Methods 0.000 claims abstract description 21
- 238000004372 laser cladding Methods 0.000 claims abstract description 14
- 239000000758 substrate Substances 0.000 claims abstract description 7
- 230000009471 action Effects 0.000 claims abstract description 5
- 239000007788 liquid Substances 0.000 claims description 18
- 230000035939 shock Effects 0.000 claims description 12
- 238000005253 cladding Methods 0.000 claims description 6
- 238000012545 processing Methods 0.000 claims description 5
- 230000007547 defect Effects 0.000 abstract description 10
- 230000008901 benefit Effects 0.000 abstract description 6
- 238000005516 engineering process Methods 0.000 description 19
- 239000013078 crystal Substances 0.000 description 9
- 239000000463 material Substances 0.000 description 8
- 230000008569 process Effects 0.000 description 8
- 238000002844 melting Methods 0.000 description 4
- 230000008018 melting Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 2
- 230000004927 fusion Effects 0.000 description 2
- 239000007769 metal material Substances 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 230000005855 radiation Effects 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 238000003756 stirring Methods 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 230000002159 abnormal effect Effects 0.000 description 1
- 238000009825 accumulation Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000010894 electron beam technology Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 238000007712 rapid solidification Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000003746 surface roughness Effects 0.000 description 1
- 230000001360 synchronised effect Effects 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
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/10—Sintering only
- B22F3/105—Sintering only by using electric current other than for infrared radiant energy, laser radiation or plasma ; by ultrasonic bonding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B33—ADDITIVE MANUFACTURING TECHNOLOGY
- B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
- B33Y10/00—Processes of additive manufacturing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B33—ADDITIVE MANUFACTURING TECHNOLOGY
- B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
- B33Y30/00—Apparatus for additive manufacturing; Details thereof or accessories therefor
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P10/00—Technologies related to metal processing
- Y02P10/25—Process efficiency
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Mechanical Engineering (AREA)
- Laser Beam Processing (AREA)
Abstract
The invention provides a novel optical coaxial powder feeding laser composite additive manufacturing method, which comprises the following steps of 110: the method comprises the steps of obtaining a three-dimensional CAD model of a part to be processed, and slicing and layering the three-dimensional CAD model according to an additive manufacturing process to obtain two-dimensional contour data information of each section; step 120: importing the two-dimensional profile data information of each section into a control system, and setting a specific scanning route through the control system; step 130: the control system controls the six-axis robot to drive the visual workbench to move according to the scanning route; step 140: the control system controls the continuous laser to provide a stable molten pool for the action of the substrate, and simultaneously controls the pulse laser to directly act on the metal surface of the molten pool in a molten state of a laser cladding layer; when laser cladding is carried out, the micro-forging laser carries out impact vibration on a molten pool, so that the defects of shrinkage porosity, air holes, cracks, tensile stress and the like generated in the additive manufacturing process are further reduced, the quality of parts is improved, and the economic benefit is improved.
Description
Technical Field
The invention relates to the technical field of additive manufacturing, in particular to a novel optical coaxial powder feeding laser composite additive manufacturing method and device.
Background
An Additive Manufacturing (AM) technology is a novel manufacturing technology for directly manufacturing a digital model into a solid part by adopting a material layer-by-layer accumulation method based on a layered manufacturing principle. Compared with the traditional manufacturing technology, the additive manufacturing technology has a series of advantages of high flexibility, no mold, short period, no limitation of part structures and materials and the like, and is widely applied to the fields of aerospace, automobiles, electronics, medical treatment, military industry and the like.
The metal material additive manufacturing technology, which is the most advanced and difficult technology in the whole additive manufacturing system, is an important development direction of advanced manufacturing technology. For metal material additive manufacturing technologies, laser additive manufacturing, electron beam additive manufacturing, arc additive manufacturing, and the like can be mainly classified according to the type of heat source. The Laser Additive Manufacturing (LAM) technology is an integrated Manufacturing technology that meets the requirements of precise forming and high-performance forming, and is also the most reliable and feasible method for metal additive Manufacturing at present.
The laser additive manufacturing technology is classified according to the forming principle, and most representative laser selective Melting (SLM) technology and Laser Metal Direct Forming (LMDF) technology are Selective Laser Melting (SLM) technology and synchronous powder feeding technology. The laser selective melting (SLM) technology can be used for directly manufacturing a terminal metal product, the integrated design and manufacturing of materials, structures and functions are realized, complex metal parts which cannot be processed by the traditional manufacturing method, such as a light dot matrix sandwich structure, a space curved surface porous structure, a complex cavity runner structure and the like, can be processed, the technical problems that complex metal components are difficult to process, long in period, high in cost and the like are solved, and the metal parts have high dimensional accuracy and good surface roughness and do not need secondary processing. But the mechanical property of the SLM printing component can only reach or be better than that of a cast or forged piece, and the complexity of a formed piece is basically not limited but the formed size is small. The Laser Metal Direct Forming (LMDF) technology integrates the advantages of a laser cladding technology and a rapid forming technology, a mould is not needed, the manufacture of a complex structure can be realized, and a corresponding supporting structure is required to be added to the cantilever structure. The forming size is not limited, and the manufacture of large-size parts can be realized. Can realize the mixed processing of different materials and the manufacture of gradient materials. And the damaged parts are quickly repaired. The forming structure is uniform, the mechanical property is good, and the manufacture of the oriented structure can be realized.
Although much research is currently being conducted on the process of laser additive manufacturing, many problems still exist in the forming process of parts. In the SLM forming process, complicated physical, chemical, metallurgical and other processes are accompanied, and defects such as shrinkage porosity, air holes, cracks and the like are easily generated. In the LMDF forming process, along with the long-time periodical violent heating and cooling of a high-energy laser beam, the rapid solidification shrinkage of a moving molten pool under the strong constraint of the pool bottom and the associated short-time non-equilibrium cycle solid-state phase change, great tensile stress is generated inside a part, and the part is easy to deform and crack seriously.
Disclosure of Invention
The invention aims to at least solve one of the problems in the prior art, and provides a novel optical coaxial powder feeding laser composite additive manufacturing method and device.
A novel optical coaxial powder feeding laser composite additive manufacturing method is provided, and comprises the following steps:
step 110: the method comprises the steps of obtaining a three-dimensional CAD model of a part to be processed, and slicing and layering the three-dimensional CAD model according to an additive manufacturing process to obtain two-dimensional contour data information of each section;
step 120: importing the two-dimensional profile data information of each section into a control system, and setting a specific scanning route through the control system;
step 130: starting the continuous laser and the pulse laser, and simultaneously controlling the six-axis robot to drive the visual workbench to move according to the scanning route by the control system;
step 140: the control system controls the continuous laser to act on a substrate to provide a stable molten pool, and simultaneously controls the pulse laser to directly act on the metal surface of the molten pool in a laser cladding layer molten state, and shock waves generated by the pulse laser are utilized to carry out liquid micro-forging on the metal in the molten state to form pressure and vibration on the metal in the molten state area;
step 150, the control system acquires a state image of an area acted by the pulse laser fed back by the image sensor, and adjusts parameters of the pulse laser in real time according to the state image so as to keep a laser cladding layer stable until a section of the part to be processed is formed;
step 160, repeating the step 130 and the step 150, and simultaneously controlling the six-axis robot by the control system to control the visual workbench to descend by the height of the cladding layer until the part to be processed is processed and formed.
Further, the method further comprises: the continuous laser and the laser beam of the pulse laser are kept confocal, and the continuous laser and the pulse laser cooperate with each other and keep the position unchanged all the time in the whole manufacturing process.
Further, the method also comprises the steps of selecting single or multiple kinds of metal powder for cladding according to the performance requirements of the part to be processed, and controlling the metal powder flow and the laser beam generated by the continuous laser to be coaxially output during processing.
The invention also provides a novel optical coaxial powder feeding laser composite additive manufacturing device, which comprises,
the device comprises an optical coaxial powder feeding laser system, a pulse laser, an image sensor, a control system, a six-axis robot and a visual workbench;
the optical coaxial powder feeding laser system comprises a metal powder box, a continuous laser and a coaxial powder feeding device;
the laser system, the pulse laser, the image sensor and the six-axis robot are all arranged above the visual workbench, the six-axis robot is fixed below the visual workbench and clamps the visual workbench, the continuous laser is coaxial with the coaxial powder feeding device, the coaxial powder feeding device is communicated with the metal powder box, and the laser system, the pulse laser, the image sensor and the six-axis robot are all connected with and controlled by a control system;
the continuous laser is used for providing a stable molten pool for the action of a substrate, and the pulse laser is used for generating shock waves to carry out liquid micro-forging on metal in a molten state of the molten pool and form pressure and vibration on the metal in a molten state area.
Further, the six-axis robot controls the visual workbench to move along any direction.
Further, the laser energy of the laser beam generated by the pulse laser is in a HaoJ level.
Compared with the prior art, the novel optical coaxial powder feeding laser composite additive manufacturing method provided by the invention has the following beneficial effects:
the invention provides a novel optical coaxial powder feeding laser composite additive manufacturing method, which is characterized in that a continuous laser of an optical coaxial powder feeding laser system and a metal powder box are matched to form a molten pool at a base body, a pulse laser directly acts on the metal surface of a molten pool in a laser cladding layer molten state, shock waves generated by the pulse laser are utilized to carry out liquid micro-forging on metal in the molten state, pressure and vibration are formed on the metal in the molten state area, and the micro-forging laser carries out shock vibration on the molten pool during laser cladding, so that the defects of shrinkage porosity, air holes, cracks, tensile stress and the like generated in the additive manufacturing process are further reduced, the quality of parts is improved, and the economic benefit is improved.
Drawings
In order to more clearly illustrate the technical solutions in the examples of the present invention, the drawings used in the description of the examples will be briefly introduced below, it is obvious that the drawings in the following description are only some examples of the present invention, and that other drawings can be obtained by those skilled in the art without inventive effort, wherein:
fig. 1 is a flow chart of a novel optical coaxial powder feeding laser composite additive manufacturing method provided by the invention;
FIG. 2 is a functional schematic diagram of a continuous laser and a pulse laser of the novel optical coaxial powder-feeding laser composite additive manufacturing method provided by the invention;
fig. 3 is a schematic diagram of the novel optical coaxial powder feeding laser composite additive manufacturing device provided by the invention.
Detailed Description
The technical solutions in the examples of the present invention will be clearly and completely described below with reference to the drawings in the examples of the present invention, and it is obvious that the described examples are only a part of the examples of the present invention, and not all examples.
With reference to fig. 1 and fig. 2, embodiment 1 is a novel method for manufacturing a composite additive by using coaxial powder feeding laser in light, the method including the following steps:
step 110: the method comprises the steps of obtaining a three-dimensional CAD model of a part to be processed, and slicing and layering the three-dimensional CAD model according to an additive manufacturing process to obtain two-dimensional contour data information of each section;
step 120: importing the two-dimensional profile data information of each section into a control system 1, and setting a specific scanning route through the control system 1;
step 130: starting the continuous laser 4 and the pulse laser 3, and simultaneously controlling the six-axis robot 9 to drive the visual workbench 8 to move according to the scanning route by the control system 1;
step 140: the control system 1 controls the continuous laser 4 to act on a substrate to provide a stable molten pool d, meanwhile, the control system 1 controls the pulse laser 3 to directly act on the metal surface of the molten pool d in a molten state of a laser cladding layer a, and shock waves generated by pulse lasers are utilized to carry out liquid micro-forging on the metal in the molten state to form pressure and vibration on the metal in a molten state area;
step 150, the control system 1 acquires a state image of an area acted by the pulse laser 3 and fed back by the image sensor 2, and adjusts parameters of the pulse laser 3 in real time according to the state image so as to keep the laser cladding layer a stable until a section of the part to be processed is formed;
step 160, repeating the step 130 and the step 150, and simultaneously controlling the six-axis robot 9 by the control system 1 to control the visual workbench 8 to descend by the height of the cladding layer a until the part to be processed is formed.
A molten pool d is formed at a base body through the matching of a continuous laser 4 of an optical inner coaxial powder feeding laser system 6 and a metal powder box 7, the pulse laser 3 directly acts on the metal surface of a molten layer a of the molten pool d in a molten state, the metal in the molten state is subjected to liquid micro-forging by using shock waves generated by the pulse laser, pressure and vibration are formed on the metal in the molten state area, and the micro-forging laser performs shock vibration on the molten pool d during laser cladding, so that the defects of shrinkage porosity, air holes, cracks, tensile stress and the like generated in the material increase manufacturing process are further reduced, the quality of parts is improved, and the economic benefit is improved.
As a preferred embodiment of the present invention, the method further comprises: the laser beam c of the continuous laser 4 and the laser beam b of the pulse laser 3 are kept confocal, and the two are cooperated to work, and the positions are always kept unchanged in the whole manufacturing process.
As a preferred embodiment of the invention, the method further comprises the steps of selecting single or multiple metal powders for cladding according to the performance requirements of the part to be processed, and controlling the metal powder flow to be coaxially output with the laser beam generated by the continuous laser 4 during processing. The metal liquid is mixed more uniformly, pores and shrinkage porosity are eliminated, and crystal grains are refined.
The invention also provides a novel optical coaxial powder feeding laser composite additive manufacturing device, which comprises,
the device comprises an optical coaxial powder feeding laser system 6, a pulse laser 3, an image sensor 2, a control system 1, a six-axis robot 9 and a visual workbench 8;
the optical coaxial powder feeding laser system 6 comprises a metal powder box 7, a continuous laser 4 and a coaxial powder feeding device 5;
the in-light coaxial powder feeding laser system 6, the pulse laser 3 and the image sensor 2 are all arranged above a visual workbench 8, the six-axis robot 9 is fixed below the visual workbench 8 and clamps the visual workbench 8 tightly, the continuous laser 4 is coaxial with the coaxial powder feeding device 5, the coaxial powder feeding device 5 is communicated with a metal powder box 7, and the in-light coaxial powder feeding laser system 6, the pulse laser 3, the image sensor 2 and the six-axis robot 9 are all connected with the control system 1 and controlled by the control system 1;
the continuous laser 4 is used for providing a stable molten pool d for the action of a substrate, and the pulse laser 3 is used for generating shock waves to carry out liquid micro-forging on metal in a molten state of the molten pool d and form pressure and vibration on the metal in a molten state area.
After the device utilizes the method, a molten pool d can be formed at the position of a base body through the matching of the continuous laser 4 of the optical coaxial powder feeding laser system 6 and the metal powder box 7, the pulse laser 3 directly acts on the metal surface of the molten pool d in the molten state of the laser cladding layer a, the metal in the molten state is subjected to liquid micro-forging by using the shock wave generated by the pulse laser, pressure and vibration are formed on the metal in the molten state area, and the micro-forging laser performs shock vibration on the molten pool d during laser cladding, so that the defects of shrinkage porosity, air holes, cracks, tensile stress and the like generated in the material increase manufacturing process are further reduced, the quality of parts is improved, and the economic benefit is improved.
As a preferred embodiment of the present invention, the six-axis robot 9 controls the visual table 8 to move in either direction.
In a preferred embodiment of the present invention, the laser energy of the second laser light generated by the second laser is at a high power level. By adopting the laser micro-forging mode, the laser energy of the second laser is greatly reduced, and the requirement can be met only by a high-power level.
The impact forging and the liquid micro forging are essentially described as follows:
the liquid micro-forging is to improve the welding defect by an impact stirring action in a metal melting state, the impact forging is to perform the impact forging on the optimal plastic forming state of the metal and to perform the process strengthening on the solid welding seam,
in terms of crystal grains, impact forging mainly plays a role in performing impact forging on formed coarse crystal grains to refine the crystal grains and increase the grain boundary, so that the hardness and the metal strength are improved to a certain extent; the liquid micro-forging is to guide the growth direction of crystal grains, the crystal grains grow from columnar crystal to isometric crystal, and the components in the d area of the molten pool are not uniform and reduced.
So to speak, forging changes the state of the crystal grains; liquid micro-forging directs grain growth toward refined grains and equiaxed.
For the air holes, the impact forging is used for forging the air holes, the impact stirring is used for reducing and inhibiting the generation of the air holes, and the liquid micro-forging also has a pressing effect on the air holes;
the impact forging only improves the defects of cracks, air holes and the like, the liquid micro-forging inhibits the defects, and the liquid micro-forging also improves the defects.
In the case of performing liquid micro-forging, attention should be paid to the following points,
1. the accuracy of a monitoring system, the fusion standard fluctuation curves of different materials under different working conditions need multiple experiments, and the calculation of big data statistics is carried out to obtain the fusion standard fluctuation curves;
2. selecting different parameters of the forging laser corresponding to different abnormal conditions of the fluctuation signal;
the laser acts when the metal is in a molten state, and the specific acting position and energy are determined according to the real-time state of the monitored molten pool d;
3. defects are determined by monitoring the light radiation fed back from the molten pool d and the fluctuation of the heat radiation value.
The above description is only an example of the present invention and is not intended to limit the scope of the present invention, and all modifications of equivalent structures and equivalent processes, which are made by the present invention in the specification, or directly or indirectly applied to other related technical fields, are included in the scope of the present invention.
Claims (6)
1. The novel optical coaxial powder feeding laser composite additive manufacturing method is characterized by comprising the following steps:
step 110: the method comprises the steps of obtaining a three-dimensional CAD model of a part to be processed, and slicing and layering the three-dimensional CAD model according to an additive manufacturing process to obtain two-dimensional contour data information of each section;
step 120: importing the two-dimensional profile data information of each section into a control system, and setting a specific scanning route through the control system;
step 130: starting the continuous laser and the pulse laser, and simultaneously controlling the six-axis robot to drive the visual workbench to move according to the scanning route by the control system;
step 140: the control system controls the continuous laser to act on a substrate to provide a stable molten pool, and simultaneously controls the pulse laser to directly act on the metal surface of the molten pool in a laser cladding layer molten state, and shock waves generated by the pulse laser are utilized to carry out liquid micro-forging on the metal in the molten state to form pressure and vibration on the metal in the molten state area;
step 150, the control system acquires a state image of an area acted by the pulse laser fed back by the image sensor, and adjusts parameters of the pulse laser in real time according to the state image so as to keep a laser cladding layer stable until a section of the part to be processed is formed;
step 160, repeating the step 130 and the step 150, and simultaneously controlling the six-axis robot by the control system to control the visual workbench to descend by the height of the cladding layer until the part to be processed is processed and formed.
2. The novel in-light coaxial powder-feeding laser composite additive manufacturing method according to claim 1, further comprising: the continuous laser and the laser beam of the pulse laser are kept confocal, and the continuous laser and the pulse laser cooperate with each other and keep the position unchanged all the time in the whole manufacturing process.
3. The novel in-light coaxial powder-feeding laser composite additive manufacturing method according to claim 1, further comprising the steps of selecting single or multiple metal powders for cladding according to the performance requirements of the part to be processed, and controlling the metal powder flow to be coaxially output with the laser beam generated by the continuous laser during processing.
4. The novel laser composite additive manufacturing device with coaxial powder feeding in light is characterized by comprising,
the device comprises an optical coaxial powder feeding laser system, a pulse laser, an image sensor, a control system, a six-axis robot and a visual workbench;
the optical coaxial powder feeding laser system comprises a metal powder box, a continuous laser and a coaxial powder feeding device;
the laser system, the pulse laser, the image sensor and the six-axis robot are all arranged above the visual workbench, the six-axis robot is fixed below the visual workbench and clamps the visual workbench, the continuous laser is coaxial with the coaxial powder feeding device, the coaxial powder feeding device is communicated with the metal powder box, and the laser system, the pulse laser, the image sensor and the six-axis robot are all connected with and controlled by a control system;
the continuous laser is used for providing a stable molten pool for the action of a substrate, and the pulse laser is used for generating shock waves to carry out liquid micro-forging on metal in a molten state of the molten pool and form pressure and vibration on the metal in a molten state area.
5. The novel in-light coaxial powder feeding laser composite additive manufacturing device according to claim 4, wherein the six-axis robot controls the visual workbench to move in any direction.
6. The novel in-light coaxial powder-feeding laser composite additive manufacturing device according to claim 4, wherein laser energy of a laser beam generated by the pulse laser is at a HaoJoule level.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202011582642.9A CN112809003A (en) | 2020-12-28 | 2020-12-28 | Novel optical coaxial powder feeding laser composite additive manufacturing method and device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202011582642.9A CN112809003A (en) | 2020-12-28 | 2020-12-28 | Novel optical coaxial powder feeding laser composite additive manufacturing method and device |
Publications (1)
Publication Number | Publication Date |
---|---|
CN112809003A true CN112809003A (en) | 2021-05-18 |
Family
ID=75854217
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202011582642.9A Withdrawn CN112809003A (en) | 2020-12-28 | 2020-12-28 | Novel optical coaxial powder feeding laser composite additive manufacturing method and device |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN112809003A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114561637A (en) * | 2022-01-21 | 2022-05-31 | 北京航空航天大学 | Laser cladding method and device for surface modification of shaft parts |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107378251A (en) * | 2017-05-31 | 2017-11-24 | 广东工业大学 | A kind of destressing laser-impact of band large-scale metal part forges surface repairing method and device |
CN107914013A (en) * | 2017-11-14 | 2018-04-17 | 广东工业大学 | Double excitation impact forges titanium alloy fixator for catagmatic lower leg manufacture device and method |
CN112276083A (en) * | 2020-10-26 | 2021-01-29 | 广东镭奔激光科技有限公司 | Novel optical coaxial powder feeding laser composite additive manufacturing method and device |
-
2020
- 2020-12-28 CN CN202011582642.9A patent/CN112809003A/en not_active Withdrawn
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107378251A (en) * | 2017-05-31 | 2017-11-24 | 广东工业大学 | A kind of destressing laser-impact of band large-scale metal part forges surface repairing method and device |
CN107914013A (en) * | 2017-11-14 | 2018-04-17 | 广东工业大学 | Double excitation impact forges titanium alloy fixator for catagmatic lower leg manufacture device and method |
CN112276083A (en) * | 2020-10-26 | 2021-01-29 | 广东镭奔激光科技有限公司 | Novel optical coaxial powder feeding laser composite additive manufacturing method and device |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114561637A (en) * | 2022-01-21 | 2022-05-31 | 北京航空航天大学 | Laser cladding method and device for surface modification of shaft parts |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN112276083B (en) | Laser composite additive manufacturing method and device with coaxial powder feeding in light | |
CA3065982C (en) | Method for controlling deformation and precision of parts in parallel during additive manufacturing process | |
US10682716B2 (en) | Method for rapidly forming a part using combination of arc deposition and laser shock forging and device implementing same | |
Dezaki et al. | A review on additive/subtractive hybrid manufacturing of directed energy deposition (DED) process | |
CN109746441B (en) | Laser shock peening assisted laser additive manufacturing composite processing method | |
Ahmed | Direct metal fabrication in rapid prototyping: A review | |
Li et al. | Review of wire arc additive manufacturing for 3D metal printing | |
US11110513B2 (en) | Combined ultrasonic micro-forging device for improving microstructure and mechanical properties of additive manufactured metal parts, and a related additive manufacturing method | |
Zhang et al. | Hybrid direct manufacturing method of metallic parts using deposition and micro continuous rolling | |
CN109396434B (en) | Method for preparing titanium alloy part based on selective laser melting technology | |
CN109202082B (en) | Additive, equal-material and subtractive composite metal 3D laser forming device and method thereof | |
Mandil et al. | Building new entities from existing titanium part by electron beam melting: microstructures and mechanical properties | |
CN102179517A (en) | Laser-induction hybrid melting direct forming method and device | |
Ye et al. | Study of hybrid additive manufacturing based on pulse laser wire depositing and milling | |
Su et al. | An investigation into direct fabrication of fine-structured components by selective laser melting | |
EP3427870B1 (en) | Three-dimensional molded object production method | |
CN108620588B (en) | Laser metal 3D printing method without periodic layer band effect | |
CN108339984B (en) | Method for growing complex structure on surface of cast-forged piece based on wire 3D printing | |
Ruan et al. | A review of layer based manufacturing processes for metals | |
CN112809003A (en) | Novel optical coaxial powder feeding laser composite additive manufacturing method and device | |
CN108907191A (en) | 30CrMnSiA metal pattern increasing material manufacturing method suitable for high wind tunnel testing | |
Rao et al. | Effect of process parameters on powder bed fusion maraging steel 300: a review | |
Jing et al. | Application of selective laser melting technology based on titanium alloy in aerospace products | |
CN109128172B (en) | Method for manufacturing titanium alloy crystal grains by refining and adding materials | |
Yerubayeva et al. | Recent advances and application of Selective Laser Melting (SLM) technology in the aerospace industry |
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 | ||
WW01 | Invention patent application withdrawn after publication |
Application publication date: 20210518 |
|
WW01 | Invention patent application withdrawn after publication |