CN107187056A - The complex parts 3D printing method and system being layered based on curved surface - Google Patents

The complex parts 3D printing method and system being layered based on curved surface Download PDF

Info

Publication number
CN107187056A
CN107187056A CN201710310420.3A CN201710310420A CN107187056A CN 107187056 A CN107187056 A CN 107187056A CN 201710310420 A CN201710310420 A CN 201710310420A CN 107187056 A CN107187056 A CN 107187056A
Authority
CN
China
Prior art keywords
complex parts
printing
curved surface
space
module
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201710310420.3A
Other languages
Chinese (zh)
Inventor
赵冬华
郭为忠
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shanghai Jiaotong University
Original Assignee
Shanghai Jiaotong University
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Shanghai Jiaotong University filed Critical Shanghai Jiaotong University
Priority to CN201710310420.3A priority Critical patent/CN107187056A/en
Publication of CN107187056A publication Critical patent/CN107187056A/en
Pending legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06TIMAGE DATA PROCESSING OR GENERATION, IN GENERAL
    • G06T17/00Three dimensional [3D] modelling, e.g. data description of 3D objects

Abstract

A kind of complex parts 3D printing method and system being layered based on curved surface, its threedimensional model is set up according to the structure and curved surface features of complex parts, and carries out structure lightened topology optimization design and space 3D slicing delaminations, generates the control data for 3D printing;Successively 3D printing is carried out after carrying out print parameters setting according to control data, the 3D printing part of complex parts is obtained;Space 3D slicing delaminations refer to:According to the design feature of the threedimensional model of complex parts, choose curved surface layered approach and carry out curved surface layering, Selective filling strategy after handling the space 3D individual-layer datas after layering carries out printing path and trajectory planning;It is of the invention to be advantageously implemented continuous lod manufacture compared with existing CNC process technologies, effectively improve the shaping surface precision of complex parts, reduce printing support.

Description

The complex parts 3D printing method and system being layered based on curved surface
Technical field
It is specifically a kind of based on answering that curved surface is layered the present invention relates to a kind of technology in complex parts 3D printing field Miscellaneous part 3D printing method and system.
Background technology
For the 3D printing of complex parts, existing layered mode is 2D layerings, i.e., based on etc. thickness, become thickness, many The mode in direction carries out hierarchy slicing.One direction printing can not solve the problems, such as support;Change layer slab mode passes through for perpendicular Nogata reduces slice thickness to improve printing precision to when having curved surface;And tangential section is for complex parts in many ways, then Huge early stage slicing treatment cost can be brought.Filling mode mainly includes Raster, Zigzag, Contour, Hybrid, Continuous, medial axis transformation etc., by the filling mode in different 2D planes, take into account filling Efficiency and printing precision.But, the lamination error of 2D plane Internal periphery errors of fitting and Z-direction remains unchanged presence.It is existing many Free degree printing device does not use 3D truly dependent on the filling Strategy in existing 2D slicing modes and 2D planes The method of section, to realize that printout surface is smooth, surface curve gradient is free and adjust connection weaker between layers.
The content of the invention
The present invention is directed to deficiencies of the prior art, proposes a kind of complex parts 3D printing being layered based on curved surface Method and system, choose curved surface layering and filling Strategy with reference to the structure of complex parts, surface and function, plan print track, And the control data progress 3D printing and post processing of printing device are converted to, so as to realize the 3D with reference to the layering of complex parts curved surface Printing.
The present invention is achieved by the following technical solutions:
The present invention sets up its threedimensional model according to the structure, curved surface features and process requirements of complex parts, and carries out structure Lightweight topology optimization design and space 3D slicing delaminations, generate the control data for 3D printing;Carried out according to control data Successively 3D printing is carried out after print parameters setting, the 3D printing part of complex parts is obtained.
The structure of described complex parts includes:Spacial special-shaped pipeline configuration, integrated labyrinth, Space Free-Form Surface Structure etc. has the structure of larger Z-direction section lamination error.The class formation is cut into slices according to existing Z-direction, the side of X/Y plane printing Formula can cause lamination error.
Described curved surface features include:Space Free-Form Surface, surface of revolution etc. are along the larger curved surface of Z-direction curvature.
Described process requirements include:Some part requirements are more excellent thus it requires printout in the tensile and compressive property of Z-direction Microstructure grows along some direction, i.e., Print direction is consistent with the direction of growth.
Described foundation, by shape, property and the process materials demand towards print object in itself, is made using three-dimensional Type software is modeled realization.
Described threedimensional model is drawn by 3D sculpting software.
Described structure lightened topology optimization design includes:Structural-functional analysis, load-carrying properties about beam analysis and stress Specificity analysis.
Described structural-functional analysis refers to:Analyzed for key structure, key function, be further ensured that structure, Function can reach design requirement.In the case where meeting structure function, structure lightened topological optimization is carried out.
Described load-carrying properties about beam analysis refers to:The load-carrying properties constraint in printout all directions itself is analyzed, should Effect of constraint value printing-forming motion mode, in the case where meeting load-carrying properties constraint, carries out structure lightened topological optimization.
Described stress characteristics analysis refers to:To printout, required stress characteristics are analyzed in itself, are meeting stress In the case of demand, structure lightened topological optimization is carried out.
Described space 3D slicing delaminations refer to:According to the design feature of the threedimensional model of complex parts, curved surface point is chosen Layer method carries out curved surface slicing delamination, and Selective filling strategy is filled after handling the space 3D individual-layer datas after layering, is entered Row printing path and trajectory planning.Fabrication orientation is, along radially, by envelope innermost layer and outermost data, then to select Suitable filling Strategy is successively printed, and along radially, layered manufacturing is carried out from outside to inside or from inside to outside.
Described selection curved surface layered approach includes but is not limited to:The direction increased according to fiber or integrated structure and song Face carries out profile-followed.
The direction of described curved surface slicing delamination can from inside to outside, from outside to inside, and thickness is equal or different.
Described control data includes but is not limited to:Between driving data and each motor for controlling each motor The time series data of linkage.
Described successively 3D printing refers to:It is layered and prints with reference to CNC machining controls forming accuracy, often prints one or more layers Afterwards reinforcing is processed by the way of being pressed along forming face normal orientation.
The present invention relates to a kind of system for realizing the above method, including:The three-dimensional modeling of complex parts, structure lightened open up Flutter optimization module, space 3D slicing delaminations module, control data generation module, print parameters setting module, data transfer and 3D Print module and post-processing module, wherein:Pass through between the three-dimensional modeling of complex parts and structure lightened topological optimization module Three-dimensional modeling data is transmitted, structure lightened topological optimization module and space 3D control data generation module slicing delamination moulds Data transfer is carried out by STL models between block, space 3D control data generation module slicing delaminations module includes space delamination And print track generation, control data generation module is by beating that space 3D control data generation module slicing delamination modules are obtained Print track is converted to the control data of each motor linkage, sets print parameters by print parameters setting module, utilizes data Transmission and 3DD print modules realize the data transfer between upper and lower machine, and by means of beating that print parameters setting module is set Print parameter is printed, so that the shaping of whole 3D control datas generation module printout is realized, with reference to post-processing module, air exercise Printed document carries out certain post processing and obtains final printout.
Technique effect
Compared with prior art, the present invention is entered using the layering of three dimensions 3D curved surfaces with reference to multiple degrees of freedom 3D printing equipment Row printing Anatomy-and-ultrastructure processed, is different from existing 2D slicing delaminations mode, i.e., in z-direction slicing delamination, successively fill;It is different from existing 2.5D layering, i.e., in different directions respectively slicing delamination, successively fill, be advantageously implemented continuous lod manufacture, reality The enhancing of existing bearing capacity, less printing support;And use structure function for complex parts and load-carrying properties to constrain with And stress characteristics analysis carries out structure lightened topology optimization design so that overall structure further optimizes, and reduces rapidoprint, Cost is reduced, efficiency is improved.
Brief description of the drawings
Fig. 1 is schematic diagram of the present invention;
Fig. 2 is the curved surface layered approach schematic diagram of complex parts;
In figure:(a) before for layering, after (b) is layering;
Fig. 3 is the schematic flow sheet of embodiment 1;
Fig. 4 is six-dimension force sensor model schematic in embodiment 1;
Fig. 5 is that six-dimension force sensor space 3D curved surfaces are layered schematic diagram;
Fig. 6 is the hierarchy schematic diagram after the structure lightened topology optimization design of six-dimension force sensor;
In figure:1 is lower platform, and 2,4 be flexible hinge, and 3 be flexible beam, and 5 be upper mounting plate.
Embodiment
Embodiments of the invention are elaborated below, the present embodiment is carried out lower premised on technical solution of the present invention Implement, give detailed embodiment and specific operating process, but protection scope of the present invention is not limited to following implementations Example.
Embodiment 1
As shown in Figures 1 to 3, the complex parts of the present embodiment are six-dimension force sensor, specifically include following steps:
Step 1, according to the structure and curved surface features of six-dimension force sensor using 3D sculpting software draw six-dimensional force sensing The threedimensional model of device elastomer.
Described six-dimension force sensor uses the form based on Stewart parallel institutions, including six-dimension force sensor is upper Platform 5, lower platform 1, flexible hinge 2,4 and flexible beam 3, wherein:Flexible hinge 2,4 is the key structure portion of six-dimension force sensor Point.
Described 3D sculpting software includes but is not limited to:Solidworks, ProE or Catia.
Step 2, the threedimensional model progress lightweight topology optimization design to being obtained in step 1, as shown in Figure 6.
The foundation of described structure lightened topology optimization design is structural-functional analysis, load-carrying properties about beam analysis and should Force characteristic is analyzed.
Described structural-functional analysis and load-carrying properties about beam analysis can using HyperMesh, HyperView, OptiStruct or HyperStudy is carried out, and stress characteristics analysis is carried out using Ansys software combinations MATLAB.
Step 3, as shown in Figure 4 and Figure 5, to optimizing in step 2 after threedimensional model carry out space 3D slicing delaminations, generation 3D printing equipment moving control data.
Described space 3D slicing delaminations are realized by corresponding software, and it based on MATLAB or C++ is kernel that the software, which is, C# is the independently developed hierarchy slicing software at interface, by being read out to threedimensional model file, obtains outline data, adjustment Corresponding parameter, and curved surface layering is carried out using modes such as offset, slicing delamination data are obtained, in conjunction with complex parts in itself Structure, curved surface features and process requirements etc., choose suitable surface filling strategy, generate the control number of surface filling According to.
Described space 3D slicing delaminations comprise the following steps:
S1:According to the design feature of the threedimensional model of six-dimension force sensor, integrated structure and the accompanying curved surface of curved surface are chosen Layered approach carries out curved surface slicing delamination, to realize the increasing material manufacturing of continuous lod.
The direction of described curved surface slicing delamination is from inside to outside.
S2:Selective filling strategy after handling the space 3D individual-layer datas after layering, with reference to printing technology demand and The performance indications of six-dimension force sensor carry out printing path and trajectory planning.
Described filling Strategy includes but is not limited to:Space zig-zag type filling, continuous space fitting a curve or spatial light Grid are filled.
S3:The 3D data for being layered and filling in space are converted to the motion control data of 3D printing equipment.
Step 4, according to motion control data carry out print parameters setting, using synchronous material be sent into increases material manufacturing technology enter Row successively 3D printing, obtains the 3D printing part of elastomer for six-dimensional force sensor.
Described synchronous material is sent into the laser that increases material manufacturing technology refers to including but not limited to coaxial or paraxonic powder feeding material Cladding, welding of synchronous wire feed material etc. possess the layered manufacturing method of spatial shaping ability.
Described successively 3D printing refers to:Successively print, with reference to CNC machining control forming accuracies, often print one layer or number Reinforcing is processed after layer by the way of being pressed along forming face normal orientation, strengthens the intensity of the part of printing.
Described 3D printing equipment possesses multiple degrees of freedom, is different from existing 3 axis movable 3D printer, such as 6DOF Stewart 3D Printer, using the Dutch 3D printer Mataerial of mechanical arm configuration, by the way of five-axle linkage German DMGMORI DMG Lasertec 65.
Described control forming accuracy realizes that printhead possesses spatial shaping energy relative to print platform by printhead Different printing technology control printing-formings can be combined in printhead, laser printing head, the welding gun of power, such as FDM, print procedure Precision.
To ensure that precision can be using increasing material manufacturing with subtracting the composite manufacturing that material manufacture is combined, such as milling, grinding.
Step 5, printout is post-processed, printing terminates.
Described post processing refers to:Intensity processing to printout is heat-treated, and the surface treatment to printout, with Further improve shaping surface quality.
Described printout carries out the filling of curved surface layering using space curve, and the lamination eliminated in existing Z-direction is missed Difference;And the printing type is based on multiple degrees of freedom 3D printing equipment, when printing the structure of similar cantilever beam, without printing support knot Structure, while less printed material, also improves printing effect.
The present embodiment is different from the method that traditional CNC fabricates six-dimension force sensor, using successively printing and successively edge The mode for forming face normal direction pressure is strengthened, while the material that subtracts that can combine milling or grinding manufactures multiple to realize Close manufacture, forming accuracy improved while high intensity, that is, improve complex parts surface accuracies, increase complex parts printing intensity, Realize that printout surface is smooth, surface curve gradient is free and adjust connection weaker between layers.
Above-mentioned specific implementation can by those skilled in the art on the premise of without departing substantially from the principle of the invention and objective with difference Mode local directed complete set is carried out to it, protection scope of the present invention is defined by claims and not by above-mentioned specific implementation institute Limit, each implementation in the range of it is by the constraint of the present invention.

Claims (9)

1. a kind of complex parts 3D printing method being layered based on curved surface, it is characterised in that according to the structure and song of complex parts Region feature sets up its threedimensional model, and carries out structure lightened topology optimization design and space 3D slicing delaminations, generates for 3D The control data of printing;Successively 3D printing is carried out after carrying out print parameters setting according to control data, the 3D of complex parts is obtained Printout;
Described space 3D slicing delaminations refer to:According to the design feature of the threedimensional model of complex parts, curved surface layering side is chosen Method carries out curved surface slicing delamination, and Selective filling strategy is filled after handling the space 3D individual-layer datas after layering, is beaten Print path and trajectory planning.
2. complex parts 3D printing method according to claim 1, it is characterized in that, described structure lightened topological optimization The foundation of design is that structural-functional analysis, load-carrying properties about beam analysis and stress characteristics are analyzed.
3. complex parts 3D printing method according to claim 1, it is characterized in that, described selection curved surface layered approach bag Include but be not limited to:The direction increased according to fiber or integrated structure and curved surface carry out profile-followed.
4. complex parts 3D printing method according to claim 1, it is characterized in that, the direction of described curved surface slicing delamination Can from inside to outside, from outside to inside, and thickness is equal or different.
5. complex parts 3D printing method according to claim 1, it is characterized in that, described successively 3D printing refers to:Knot The layering printing of CNC machining controls forming accuracy is closed, often prints and uses what is pressed along forming face normal orientation after one or more layers Mode is processed reinforcing.
6. complex parts 3D printing method according to claim 1, it is characterized in that, the structure bag of described complex parts Include:Spacial special-shaped pipeline configuration, integrated labyrinth and Space Free-Form Surface structure.
7. complex parts 3D printing method according to claim 1, it is characterized in that, described curved surface features include:Space Free form surface, surface of revolution.
8. complex parts 3D printing method according to claim 1, it is characterized in that, described foundation, by towards printing Shape, property and the process materials demand of object in itself, realization is modeled using 3D sculpting software.
9. a kind of system for realizing any of the above-described claim methods described, it is characterised in that including:The three-dimensional of complex parts is built Mould, structure lightened topological optimization module, space 3D slicing delaminations module, control data generation module, print parameters setting mould Block, data transfer and 3D printing module and post-processing module, wherein:The three-dimensional modeling of complex parts and structure lightened topology are excellent Transmitted between change module by three-dimensional modeling data, structure lightened topological optimization module is generated with space 3D control datas Data transfer, space 3D control data generation module slicing delamination moulds are carried out by STL models between module slicing delamination module Block includes space delamination and print track is generated, and control data generation module divides the section of space 3D control datas generation module The print track that layer module is obtained is converted to the control data of each motor linkage, is set and printed by print parameters setting module Parameter, realizes the data transfer between upper and lower machine, and set by means of print parameters using data transfer and 3DD print modules The print parameters of cover half block setting are printed, so that the shaping of whole 3D control datas generation module printout is realized, with reference to Post-processing module, carries out certain post processing to printout and obtains final printout.
CN201710310420.3A 2017-05-05 2017-05-05 The complex parts 3D printing method and system being layered based on curved surface Pending CN107187056A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710310420.3A CN107187056A (en) 2017-05-05 2017-05-05 The complex parts 3D printing method and system being layered based on curved surface

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710310420.3A CN107187056A (en) 2017-05-05 2017-05-05 The complex parts 3D printing method and system being layered based on curved surface

Publications (1)

Publication Number Publication Date
CN107187056A true CN107187056A (en) 2017-09-22

Family

ID=59874026

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710310420.3A Pending CN107187056A (en) 2017-05-05 2017-05-05 The complex parts 3D printing method and system being layered based on curved surface

Country Status (1)

Country Link
CN (1) CN107187056A (en)

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107901423A (en) * 2017-12-11 2018-04-13 杭州捷诺飞生物科技股份有限公司 The 3D printing method of heterogeneous filler
CN107945277A (en) * 2017-11-26 2018-04-20 中国人民解放军陆军装甲兵学院 The equidistant surface layered approach of point cloud model is remanufactured based on increasing material
CN108320327A (en) * 2018-01-16 2018-07-24 浙江大学 The wall thickness such as three period minimal surfaces of one kind being layered filling region generation method
CN109079136A (en) * 2018-07-25 2018-12-25 沈阳精合数控科技开发有限公司 A kind of 3D printing method
CN109177174A (en) * 2018-09-10 2019-01-11 西华大学 One kind being suitable for cylindrical component 3D printing method
CN109396436A (en) * 2018-12-04 2019-03-01 陕西理工大学 A kind of pure titanium 3D printing increasing material manufacturing method
CN109394410A (en) * 2018-11-13 2019-03-01 武汉必盈生物科技有限公司 Based on the personalized outer fixed 3D printing model design method of patient and slice systems
CN109759589A (en) * 2019-03-13 2019-05-17 陕西理工大学 A kind of fine copper 3D printing increasing material manufacturing method
CN110605391A (en) * 2019-09-09 2019-12-24 江西宝航新材料有限公司 3D printing additive manufacturing method of pot-shaped thin-walled workpiece
CN110696366A (en) * 2019-10-21 2020-01-17 浙江大学 Surface appearance regulation and control method for inclined plane formed by additive manufacturing technology
WO2020037732A1 (en) * 2018-08-24 2020-02-27 苏州中瑞智创三维科技股份有限公司 Shape-adapting manufacturing method for three-dimensional printing using high-viscosity material
CN111523198A (en) * 2019-01-30 2020-08-11 通用电气公司 Additive manufacturing system and method of generating a CAD model for additive printing on a workpiece
WO2020192756A1 (en) * 2019-03-27 2020-10-01 北京机科国创轻量化科学研究院有限公司 Method for planning 3d printing path of continuous fiber reinforced composite material
CN111893485A (en) * 2020-08-26 2020-11-06 江西昌河航空工业有限公司 Method for double-cylinder synchronous powder feeding, melting and depositing composite cladding layer based on 35# steel
CN111945155A (en) * 2020-08-26 2020-11-17 江西昌河航空工业有限公司 Method for double-cylinder synchronous powder feeding, melting and depositing composite cladding layer based on 30CrMnSiA steel
CN112182911A (en) * 2020-10-26 2021-01-05 同济大学 3D printing filling design method based on force flow tube load path
CN112659544A (en) * 2020-12-02 2021-04-16 西安交通大学 Thin-wall tubular model slicing method and system of five-axis 3D printer and printing method
CN112757625A (en) * 2020-12-13 2021-05-07 华融普瑞(北京)科技有限公司 Continuous carbon fiber FDM3D printing method for crus of quadruped robot
CN113366481A (en) * 2018-11-09 2021-09-07 欧特克公司 Boundary-based generative design under 2.5-axis subtractive manufacturing constraints for computer-aided design and manufacturing
CN114425626A (en) * 2020-10-29 2022-05-03 华中科技大学 Directional energy deposition manufacturing method based on curved surface cantilever structure and product
CN114986872A (en) * 2022-06-17 2022-09-02 南京航空航天大学 Multi-degree-of-freedom additive manufacturing printing method for helmet
CN115157655A (en) * 2022-07-04 2022-10-11 上海酷鹰机器人科技有限公司 Design method of 3D printing overall scheme of large-size special-shaped curved surface sample
CN115673341A (en) * 2022-07-08 2023-02-03 湖北鸿路钢结构有限公司 Printing method and system for electric arc additive manufacturing pipe-pipe intersecting area

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106202754A (en) * 2016-07-15 2016-12-07 西安交通大学 A kind of space path printed towards multiple degrees of freedom 3D generates method

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106202754A (en) * 2016-07-15 2016-12-07 西安交通大学 A kind of space path printed towards multiple degrees of freedom 3D generates method

Cited By (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107945277A (en) * 2017-11-26 2018-04-20 中国人民解放军陆军装甲兵学院 The equidistant surface layered approach of point cloud model is remanufactured based on increasing material
CN107901423A (en) * 2017-12-11 2018-04-13 杭州捷诺飞生物科技股份有限公司 The 3D printing method of heterogeneous filler
CN108320327A (en) * 2018-01-16 2018-07-24 浙江大学 The wall thickness such as three period minimal surfaces of one kind being layered filling region generation method
CN109079136A (en) * 2018-07-25 2018-12-25 沈阳精合数控科技开发有限公司 A kind of 3D printing method
CN109079136B (en) * 2018-07-25 2020-09-04 沈阳精合数控科技开发有限公司 3D printing method
WO2020037732A1 (en) * 2018-08-24 2020-02-27 苏州中瑞智创三维科技股份有限公司 Shape-adapting manufacturing method for three-dimensional printing using high-viscosity material
CN109177174A (en) * 2018-09-10 2019-01-11 西华大学 One kind being suitable for cylindrical component 3D printing method
CN113366481A (en) * 2018-11-09 2021-09-07 欧特克公司 Boundary-based generative design under 2.5-axis subtractive manufacturing constraints for computer-aided design and manufacturing
CN109394410A (en) * 2018-11-13 2019-03-01 武汉必盈生物科技有限公司 Based on the personalized outer fixed 3D printing model design method of patient and slice systems
CN109396436A (en) * 2018-12-04 2019-03-01 陕西理工大学 A kind of pure titanium 3D printing increasing material manufacturing method
CN111523198A (en) * 2019-01-30 2020-08-11 通用电气公司 Additive manufacturing system and method of generating a CAD model for additive printing on a workpiece
CN111523198B (en) * 2019-01-30 2024-02-27 通用电气公司 Additive manufacturing system and method for generating CAD models for additive printing on workpieces
CN109759589A (en) * 2019-03-13 2019-05-17 陕西理工大学 A kind of fine copper 3D printing increasing material manufacturing method
WO2020192756A1 (en) * 2019-03-27 2020-10-01 北京机科国创轻量化科学研究院有限公司 Method for planning 3d printing path of continuous fiber reinforced composite material
CN110605391A (en) * 2019-09-09 2019-12-24 江西宝航新材料有限公司 3D printing additive manufacturing method of pot-shaped thin-walled workpiece
CN110605391B (en) * 2019-09-09 2021-08-27 江西宝航新材料有限公司 3D printing additive manufacturing method of pot-shaped thin-walled workpiece
CN110696366A (en) * 2019-10-21 2020-01-17 浙江大学 Surface appearance regulation and control method for inclined plane formed by additive manufacturing technology
CN111893485A (en) * 2020-08-26 2020-11-06 江西昌河航空工业有限公司 Method for double-cylinder synchronous powder feeding, melting and depositing composite cladding layer based on 35# steel
CN111945155A (en) * 2020-08-26 2020-11-17 江西昌河航空工业有限公司 Method for double-cylinder synchronous powder feeding, melting and depositing composite cladding layer based on 30CrMnSiA steel
CN112182911A (en) * 2020-10-26 2021-01-05 同济大学 3D printing filling design method based on force flow tube load path
CN114425626A (en) * 2020-10-29 2022-05-03 华中科技大学 Directional energy deposition manufacturing method based on curved surface cantilever structure and product
CN114425626B (en) * 2020-10-29 2022-12-02 华中科技大学 Directional energy deposition manufacturing method based on curved surface cantilever structure and product
CN112659544A (en) * 2020-12-02 2021-04-16 西安交通大学 Thin-wall tubular model slicing method and system of five-axis 3D printer and printing method
CN112659544B (en) * 2020-12-02 2022-06-07 西安交通大学 Thin-wall tubular model slicing method and system of five-axis 3D printer and printing method
CN112757625A (en) * 2020-12-13 2021-05-07 华融普瑞(北京)科技有限公司 Continuous carbon fiber FDM3D printing method for crus of quadruped robot
CN114986872A (en) * 2022-06-17 2022-09-02 南京航空航天大学 Multi-degree-of-freedom additive manufacturing printing method for helmet
CN115157655A (en) * 2022-07-04 2022-10-11 上海酷鹰机器人科技有限公司 Design method of 3D printing overall scheme of large-size special-shaped curved surface sample
CN115673341A (en) * 2022-07-08 2023-02-03 湖北鸿路钢结构有限公司 Printing method and system for electric arc additive manufacturing pipe-pipe intersecting area
CN115673341B (en) * 2022-07-08 2023-09-15 湖北鸿路钢结构有限公司 Printing method and system for arc additive manufacturing tube-tube intersecting region

Similar Documents

Publication Publication Date Title
CN107187056A (en) The complex parts 3D printing method and system being layered based on curved surface
CN107825701A (en) Based on five axle print platforms without support 3D printing method
CN111037917B (en) FDM printing method, system and medium based on model splitting and splicing printing
CN106600710B (en) A kind of layer of the adjacent topological correlation of geometric mesh model cuts multiply connected domain construction method
CN108274055B (en) The processing method that elliptical vibration assists micro- V-groove layered cutting
CN107067471B (en) Self-adaptive scanning speed method for improving forming quality of pendant model
CN104057611A (en) 3D printing fill path generation method based on optimization of scanning line dip angle
CN107187030A (en) The method that sensor is made using 3D printing technique
US10906248B2 (en) Additive manufacturing method for improved core structure
CN107457995A (en) Five-axle linkage 3D printing method based on nurbs surface description
CN110561667A (en) sole forming die and metal 3D printing manufacturing method thereof
CN110962337B (en) Method for improving strength between walls in ultra-large fused deposition 3D printing
CN114986872B (en) Multi-degree-of-freedom additive manufacturing printing method for helmet
KR102171748B1 (en) A method of fabricating a rotor blade filler body, and a rotor blade filler body comprising at least one cellular assembly having closed cells
CN105799172A (en) Equipment and method for 3D printing of architectural ornaments
JP2002067175A (en) Contour smoothening method by micro-slice forming
Feng et al. Curved-layered material extrusion modeling for thin-walled parts by a 5-axis machine
CN110667109A (en) Delta mechanical arm-based photocuring 3D printer slicing method, printing method and printer
CN110696367B (en) Shell part variable-thickness curved surface layering, path planning and process control method
CN116100808B (en) Space curved surface printing path planning method based on dynamic contour bias dispersion
CN114918370B (en) Sand mold forming method suitable for manufacturing adaptive slices by increasing and decreasing materials
Zhong et al. As-continuous-as-possible extrusion-based fabrication of surface models
CN113360976B (en) Automatic generation method of composite material digital layering model
CN100999123A (en) Stage injection/carving composite fast shaping technology
CN110096761B (en) method for synchronously optimizing shape and layering sequence of free-form surface laminated shell

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication

Application publication date: 20170922

RJ01 Rejection of invention patent application after publication