[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

CN106735212B - 3D printing integrated structure exhaust insert mold core method and exhaust insert mold core - Google Patents

3D printing integrated structure exhaust insert mold core method and exhaust insert mold core Download PDF

Info

Publication number
CN106735212B
CN106735212B CN201611187874.8A CN201611187874A CN106735212B CN 106735212 B CN106735212 B CN 106735212B CN 201611187874 A CN201611187874 A CN 201611187874A CN 106735212 B CN106735212 B CN 106735212B
Authority
CN
China
Prior art keywords
mold core
laser beam
exhaust insert
layer
exhaust
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201611187874.8A
Other languages
Chinese (zh)
Other versions
CN106735212A (en
Inventor
向绪平
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.)
Dongguan Cangming 3d Tech Co ltd
Original Assignee
Dongguan Cangming 3d Tech Co ltd
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 Dongguan Cangming 3d Tech Co ltd filed Critical Dongguan Cangming 3d Tech Co ltd
Priority to CN201611187874.8A priority Critical patent/CN106735212B/en
Publication of CN106735212A publication Critical patent/CN106735212A/en
Application granted granted Critical
Publication of CN106735212B publication Critical patent/CN106735212B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/10Formation of a green body
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/20Direct sintering or melting
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/30Process control
    • B22F10/36Process control of energy beam parameters
    • B22F10/366Scanning parameters, e.g. hatch distance or scanning strategy
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/80Data acquisition or data processing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C45/00Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
    • B29C45/17Component parts, details or accessories; Auxiliary operations
    • B29C45/26Moulds
    • B29C45/34Moulds having venting means
    • B29C45/345Moulds having venting means using a porous mould wall or a part thereof, e.g. made of sintered metal
    • 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
    • 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
    • B33Y80/00Products made by additive manufacturing
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Mechanical Engineering (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)

Abstract

The invention discloses a 3D printing integrated structure exhaust insert mold core method, which comprises the following steps: (1) establishing a three-dimensional modeling model of a mold core and an exhaust insert of an integrated structure through CAD auxiliary software, wherein the exhaust insert is positioned in the middle of the mold core; (2) processing the three-dimensional modeling model by CAD (computer-aided design) modeling and layered slicing software to obtain data of each layer required by a 3D printer of the mold insert and the exhaust insert, wherein the data of each layer comprises a mold insert laser sintering area and an exhaust insert laser sintering area; importing each layer of data into a 3D printer, and respectively setting scanning parameters of a mold core laser sintering area and an exhaust insert laser sintering area in the 3D printer; (3) scanning layer by layer according to the data of each layer of laser scanning, forming a compact-structure mold core in a mold core laser sintering area, forming an exhaust insert with a plurality of clearance hole structures in a laser sintering area of the exhaust insert, and integrating the exhaust insert and the mold core into a whole. The invention also discloses an exhaust insert mold core.

Description

3D打印一体结构排气镶件模仁方法及排气镶件模仁3D printing integral structure exhaust insert mold core method and exhaust insert mold core

技术领域technical field

本发明涉及模具制备的技术领域,具体涉及一种3D打印一体结构排气镶件模仁方法,及实施该方法的排气镶件模仁。The invention relates to the technical field of mold preparation, in particular to a method for 3D printing an integrated structure exhaust insert mold core, and the exhaust insert mold core for implementing the method.

背景技术Background technique

由于注塑模具需要排气系统,特别是深骨位的区域。目前很多模具制造都是在困气的地方采用做镶件的形式来解决困气问题,由于镶件和模仁是2个分开的个体,在模具装配时会产生间隙,在注塑时由于压力很大,经常会在镶件与模仁间隙的地方产生披锋,影响注塑产品的外观而达不到客户的要求。Because injection molds require an exhaust system, especially in deep bone areas. At present, many mold manufacturers use the form of inserts to solve the problem of trapped air in the place where the air is trapped. Since the insert and the mold core are two separate entities, there will be a gap when the mold is assembled, and the pressure is very high during injection molding. If it is too large, it will often produce a front in the gap between the insert and the mold core, which will affect the appearance of the injection molded product and fail to meet the customer's requirements.

发明内容Contents of the invention

本项发明是针对现行技术不足,提供一种3D打印一体结构排气镶件模仁方法,通过3D打印技术制造一体结构的模仁与排气镶件,改善模具排气及防止披锋产生,提高注塑品质。This invention is aimed at the deficiencies of the current technology, and provides a method for 3D printing an integrated structure exhaust insert mold core, and manufactures an integrated structure mold core and exhaust insert through 3D printing technology to improve the exhaust of the mold and prevent the generation of the front. Improve injection molding quality.

本发明还提供一种实施该制备方法的排气镶件模仁。The invention also provides a vent insert mold core implementing the preparation method.

本发明为实现上述目的所采用的技术方案是:The technical scheme that the present invention adopts for realizing the above object is:

一种3D打印一体结构排气镶件模仁方法,其特征在于,其包括以下步骤:A method for 3D printing an integral structure exhaust insert mold core, characterized in that it comprises the following steps:

(1)通过CAD辅助软件建立一体结构的模仁与排气镶件的三维建模模型,所述排气镶件位于模仁中间部位;(1) Establish the three-dimensional modeling model of the mold core and the exhaust insert of an integrated structure by CAD auxiliary software, and the exhaust insert is located at the middle part of the mold core;

(2)设置激光烧结的3D打印机,将步骤(1)的三维建模模型经过CAD建模及分层切片软件处理,获得一体结构的模仁以及排气镶件的3D打印机所需的各层数据,各层数据中包括模仁激光烧结区域及排气镶件激光烧结区域;将各层数据导入至3D打印机中,并在3D打印机中分别设置模仁激光烧结区域及排气镶件激光烧结区域的扫描参数;(2) Set up a 3D printer for laser sintering, and process the 3D modeling model in step (1) through CAD modeling and layered slicing software to obtain a mold core with an integrated structure and each layer required by the 3D printer for exhaust inserts Data, each layer of data includes the laser sintering area of the mold core and the laser sintering area of the exhaust insert; import the data of each layer into the 3D printer, and set the laser sintering area of the mold core and the laser sintering of the exhaust insert in the 3D printer The scan parameters of the area;

(3)根据步骤(2)的激光扫描各层数据进行逐层扫描,模仁激光烧结区域形成致密结构的模仁,排气镶件的激光烧结区域形成有多个间隙孔结构的排气镶件,排气镶件与模仁为一体结构。(3) Carry out layer-by-layer scanning according to the laser scanning data of each layer in step (2), the laser sintering area of the mold core forms a mold core with a dense structure, and the laser sintering area of the exhaust insert forms an exhaust insert with multiple interstitial hole structures Parts, the exhaust insert and the mold core are integrated.

作为进一步改进,所述步骤(3)中,逐层扫描的过程包括以下步骤:As a further improvement, in the step (3), the process of layer-by-layer scanning includes the following steps:

(31)在激光束进行扫描一层时,激光束对模仁激光烧结区域进行扫描时,激光束以同为横向或同为纵向的方向进行逐行扫描,并且后一行激光束扫描轨迹与前一行激光束扫描轨迹设有重叠部分;(31) When the laser beam scans one layer, when the laser beam scans the laser sintering area of the mold core, the laser beam scans line by line in the same horizontal or vertical direction, and the laser beam scanning track of the next line is the same as that of the previous line. A row of laser beam scanning tracks is provided with overlapping parts;

激光束对排气镶件的激光烧结区域进行扫描时,激光束以同为横向或同为纵向的方向进行逐行扫描,并且后一行激光束扫描轨迹与前一行激光束扫描轨迹之间设有间隙;When the laser beam scans the laser sintering area of the exhaust insert, the laser beam scans line by line in the same horizontal or vertical direction, and there is an gap;

(32)当激光束完成前一激光束扫描层扫描后,进行后一激光束扫描层扫描时,(32) When the laser beam scans the previous laser beam scanning layer and scans the next laser beam scanning layer,

激光束对模仁激光烧结区域进行扫描时,激光束以同为横向或同为纵向的方向进行逐行扫描,并且后一行激光束扫描轨迹与前一行激光束扫描轨迹设有重叠部分;When the laser beam scans the laser sintering area of the mold core, the laser beam scans line by line in the same horizontal or vertical direction, and the laser beam scanning track of the next line overlaps with the scanning track of the previous line of laser beam;

激光束对排气镶件的激光烧结区域进行扫描时,激光束以同为横向或同为纵向的方向进行逐行扫描,并且后一行激光束扫描轨迹与前一行激光束扫描轨迹之间设有间隙,When the laser beam scans the laser sintering area of the exhaust insert, the laser beam scans line by line in the same horizontal or vertical direction, and there is an gap,

后一激光束扫描层的排气镶件激光烧结区域的激光束扫描方向与前一激光束扫描层的排气镶件激光烧结区域的激光束扫描方向交叉;前一激光束扫描层中各行激光束扫描轨迹之间的间隙与后一激光束扫描层中各行激光束扫描轨迹之间的间隙交错重叠,形成间隙孔,该间隙孔为排气镶件的排气孔。The laser beam scanning direction of the exhaust insert laser sintering area of the latter laser beam scanning layer crosses the laser beam scanning direction of the exhaust insert laser sintering area of the previous laser beam scanning layer; each row of laser beams in the previous laser beam scanning layer The gaps between beam scanning tracks overlap with the gaps between each row of laser beam scanning tracks in the subsequent laser beam scanning layer to form a gap hole, which is the exhaust hole of the exhaust insert.

作为进一步改进,所述的3D打印一体结构排气镶件模仁方法还包括以下步骤:As a further improvement, the 3D printing integrated structure exhaust insert mold core method also includes the following steps:

(4)将间隙孔内的金属粉末吸出。(4) Suck out the metal powder in the gap hole.

作为进一步改进,所述间隙孔的方向为竖直方向,从上往下贯穿排气镶件,将模仁内部与外部连通。As a further improvement, the direction of the clearance hole is a vertical direction, which penetrates the exhaust insert from top to bottom, and communicates the inside of the mold core with the outside.

作为进一步改进,步骤(32)中,后一激光束扫描层的排气镶件激光烧结区域的激光束扫描方向与前一激光束扫描层的排气镶件激光烧结区域的激光束扫描方向呈垂直交叉,或呈斜向交叉。As a further improvement, in step (32), the laser beam scanning direction of the exhaust insert laser sintering area of the latter laser beam scanning layer is in the same direction as the laser beam scanning direction of the exhaust insert laser sintering area of the previous laser beam scanning layer Cross vertically, or cross diagonally.

作为进一步改进,步骤(31)或(32)中,激光束对模仁激光烧结区域进行扫描时,激光束以同为横向或同为纵向的方向进行逐行扫描,并且后一行激光束扫描轨迹与前一行激光束扫描轨迹设有重叠部分,重叠部分为激光束扫描轨迹的30%。As a further improvement, in step (31) or (32), when the laser beam scans the laser sintering area of the mold core, the laser beam scans line by line in the same direction as the horizontal direction or the same as the vertical direction, and the last line of laser beam scanning track There is an overlapping portion with the laser beam scanning track of the previous row, and the overlapping portion is 30% of the laser beam scanning track.

一种实施上述3D打印一体结构排气镶件模仁方法的排气镶件模仁,所述排气镶件模仁为模仁与排气镶件组成的一体结构,所述排气镶件位于模仁中间部位,所述排气镶件内打印出多个间隙孔。An exhaust insert mold core for implementing the above-mentioned method of 3D printing an integrated structure exhaust insert mold core, the exhaust insert mold core is an integral structure composed of a mold core and an exhaust insert, and the exhaust insert Located in the middle of the mold core, multiple clearance holes are printed in the exhaust insert.

作为进一步改进,所述间隙孔的方向为竖直方向,从上往下贯穿排气镶件,将模仁内部与外部连通。As a further improvement, the direction of the clearance hole is a vertical direction, which penetrates the exhaust insert from top to bottom, and communicates the inside of the mold core with the outside.

作为进一步改进,所述间隙孔为垂直设置,孔内设有金属粉末。As a further improvement, the interstitial holes are arranged vertically, and metal powder is arranged in the holes.

作为进一步改进,所述间隙孔为垂直设置的通孔。As a further improvement, the clearance hole is a through hole arranged vertically.

本发明的有益效果:本发明通过3D打印制作一体结构的模仁与排气镶件,模仁与排气镶件在注塑时,即能实现排气功能,模腔内气体通过排气镶件的间隙孔顺利排出,解决困气问题,同时,由于模仁与排气镶件为一体结构,因此注塑中不会由于压力大而在排气镶件与模仁间隙的地方产生披锋,注塑产品的外观美观无瑕疵。Beneficial effects of the present invention: the present invention manufactures an integrated mold core and exhaust insert through 3D printing. When the mold core and exhaust insert are injected, the exhaust function can be realized, and the gas in the mold cavity passes through the exhaust insert. The gap holes in the hole are discharged smoothly to solve the problem of trapped air. At the same time, because the mold core and the exhaust insert are integrally structured, there will be no peaks in the gap between the exhaust insert and the mold core during injection molding due to high pressure. Injection molding The appearance of the product is beautiful and flawless.

下面结合附图与具体实施方式,对本发明进一步详细说明。The present invention will be described in further detail below in conjunction with the accompanying drawings and specific embodiments.

附图说明Description of drawings

图1为本实施例的一体结构的模仁与排气镶件的结构示意图;Fig. 1 is the schematic structural view of the mold core and exhaust insert of the integrated structure of the present embodiment;

图2为本实施例的排气镶件结构示意图;Fig. 2 is a schematic structural diagram of the exhaust insert of the present embodiment;

图3为模仁激光烧结区域激光束扫描轨迹一个激光束扫描层示意图;Fig. 3 is a schematic diagram of a laser beam scanning layer of the laser beam scanning track in the laser sintering area of the mold core;

图4为排气镶件激光烧结区域激光束扫描轨迹两个激光束扫描层示意图;Fig. 4 is a schematic diagram of two laser beam scanning layers of the laser beam scanning track in the laser sintering area of the exhaust insert;

图5为图4中A部位放大结构示意图;Fig. 5 is a schematic diagram of the enlarged structure of part A in Fig. 4;

图中:1.模仁激光烧结区域,2.排气镶件激光烧结区域,3.激光束扫描轨迹,4.重叠部分,5.间隙,6.间隙孔,7.激光束扫描层。In the figure: 1. Mold core laser sintering area, 2. Exhaust insert laser sintering area, 3. Laser beam scanning track, 4. Overlapping part, 5. Gap, 6. Gap hole, 7. Laser beam scanning layer.

具体实施方式Detailed ways

实施例,参见图1~5,本实施例提供的3D打印一体结构排气镶件模仁方法,其包括以下步骤:Embodiments, referring to Figures 1 to 5, the method for 3D printing an integrated exhaust insert mold core provided by this embodiment includes the following steps:

(1)通过CAD辅助软件建立一体结构的模仁与排气镶件的三维建模模型,所述排气镶件位于模仁中间部位;(1) Establish the three-dimensional modeling model of the mold core and the exhaust insert of an integrated structure by CAD auxiliary software, and the exhaust insert is located at the middle part of the mold core;

(2)设置激光烧结的3D打印机,将步骤(1)的三维建模模型经过CAD建模及分层切片软件处理,获得一体结构的模仁以及排气镶件的3D打印机所需的各层数据,各层数据中包括模仁激光烧结区域1及排气镶件激光烧结区域2;将各层数据导入至3D打印机中,并在3D打印机中分别设置模仁激光烧结区域1及排气镶件激光烧结区域2的扫描参数;(2) Set up a 3D printer for laser sintering, and process the 3D modeling model in step (1) through CAD modeling and layered slicing software to obtain a mold core with an integrated structure and each layer required by the 3D printer for exhaust inserts Data, each layer of data includes the laser sintering area 1 of the mold core and the laser sintering area 2 of the exhaust insert; import the data of each layer into the 3D printer, and set the laser sintering area 1 of the mold core and the exhaust insert in the 3D printer respectively. The scanning parameters of the laser sintering area 2 of the workpiece;

(3)根据步骤(2)的激光扫描各层数据进行逐层扫描,模仁激光烧结区域1形成致密结构的模仁,排气镶件的激光烧结区域形成有多个间隙孔6结构的排气镶件,排气镶件与模仁为一体结构,逐层扫描的过程包括以下步骤:(3) Carry out layer-by-layer scanning according to the laser scanning data of each layer in step (2), the laser sintering area 1 of the mold core forms a mold core with a dense structure, and the laser sintering area of the exhaust insert forms a row of multiple gap holes 6 structures Gas inserts, exhaust inserts and mold cores are integrated, and the layer-by-layer scanning process includes the following steps:

(31)在激光束进行扫描一层时,激光束对模仁激光烧结区域1进行扫描时,激光束以同为横向或同为纵向的方向进行逐行扫描,并且后一行激光束扫描轨迹3与前一行激光束扫描轨迹3设有重叠部分4;(31) When the laser beam scans one layer, when the laser beam scans the laser sintering area 1 of the mold core, the laser beam scans line by line in the same horizontal or vertical direction, and the last line of laser beam scanning track 3 An overlapping portion 4 is provided with the previous row of laser beam scanning tracks 3;

激光束对排气镶件的激光烧结区域进行扫描时,激光束以同为横向或同为纵向的方向进行逐行扫描,并且后一行激光束扫描轨迹3与前一行激光束扫描轨迹3之间设有间隙5;When the laser beam scans the laser sintering area of the exhaust insert, the laser beam scans line by line in the same horizontal or vertical direction, and the distance between the laser beam scanning track 3 in the next line and the laser beam scanning track 3 in the previous line a gap 5 is provided;

(32)当激光束完成前一激光束扫描层7扫描后,进行后一激光束扫描层7扫描时,(32) When the laser beam finishes scanning the previous laser beam scanning layer 7 and then scans the latter laser beam scanning layer 7,

激光束对模仁激光烧结区域1进行扫描时,激光束以同为横向或同为纵向的方向进行逐行扫描,并且后一行激光束扫描轨迹3与前一行激光束扫描轨迹3设有重叠部分4;When the laser beam scans the laser sintering area 1 of the mold core, the laser beam scans line by line in the same horizontal or vertical direction, and the laser beam scanning track 3 of the next line overlaps with the laser beam scanning track 3 of the previous line 4;

激光束对排气镶件的激光烧结区域进行扫描时,激光束以同为横向或同为纵向的方向进行逐行扫描,并且后一行激光束扫描轨迹3与前一行激光束扫描轨迹3之间设有间隙5,When the laser beam scans the laser sintering area of the exhaust insert, the laser beam scans line by line in the same horizontal or vertical direction, and the distance between the laser beam scanning track 3 in the next line and the laser beam scanning track 3 in the previous line with gap 5,

后一激光束扫描层7的排气镶件激光烧结区域2的激光束扫描方向与前一激光束扫描层7的排气镶件激光烧结区域2的激光束扫描方向交叉;前一激光束扫描层7中各行激光束扫描轨迹3之间的间隙5与后一激光束扫描层7中各行激光束扫描轨迹3之间的间隙5交错重叠,形成间隙孔6,该间隙孔6为排气镶件的排气孔;后一激光束扫描层7的排气镶件激光烧结区域2的激光束扫描方向与前一激光束扫描层7的排气镶件激光烧结区域2的激光束扫描方向呈垂直交叉,或呈斜向交叉;The laser beam scanning direction of the exhaust insert laser sintering area 2 of the latter laser beam scanning layer 7 intersects with the laser beam scanning direction of the exhaust insert laser sintering area 2 of the previous laser beam scanning layer 7; the previous laser beam scanning The gap 5 between each row of laser beam scanning tracks 3 in the layer 7 and the gap 5 between each row of laser beam scanning tracks 3 in the next laser beam scanning layer 7 are alternately overlapped to form a gap hole 6, which is an exhaust inlay. The exhaust hole of the part; the laser beam scanning direction of the exhaust insert laser sintering area 2 of the latter laser beam scanning layer 7 is in the same direction as the laser beam scanning direction of the exhaust insert laser sintering area 2 of the previous laser beam scanning layer 7 cross vertically, or cross diagonally;

(4)将间隙孔6内的金属粉末吸出。(4) Suck out the metal powder in the gap hole 6 .

上述步骤(31)或(32)中,激光束对模仁激光烧结区域1进行扫描时,激光束以同为横向或同为纵向的方向进行逐行扫描,并且后一行激光束扫描轨迹3与前一行激光束扫描轨迹3设有重叠部分4,重叠部分4为激光束扫描轨迹3的30%。In the above step (31) or (32), when the laser beam scans the laser sintering area 1 of the mold core, the laser beam scans line by line in the same horizontal or vertical direction, and the laser beam scanning track 3 of the last row is in line with the The previous row of laser beam scanning tracks 3 is provided with an overlapping portion 4 , and the overlapping portion 4 is 30% of the laser beam scanning track 3 .

所述间隙孔6的方向为竖直方向,从上往下贯穿排气镶件,将模仁内部与外部连通。The direction of the gap hole 6 is the vertical direction, which penetrates the exhaust insert from top to bottom, and communicates the inside of the mold core with the outside.

本实施例还提供的排气镶件模仁,所述排气镶件模仁为模仁与排气镶件组成的一体结构,所述排气镶件位于模仁中间部位,所述排气镶件内打印出多个间隙孔6。This embodiment also provides the exhaust insert mold core, the exhaust insert mold core is an integrated structure composed of the mold core and the exhaust insert, the exhaust insert is located in the middle of the mold core, and the exhaust A plurality of clearance holes 6 are printed in the insert.

所述间隙孔6的方向为竖直方向,从上往下贯穿排气镶件,将模仁内部与外部连通,将模仁内困气的地方空气导出。The direction of the gap hole 6 is the vertical direction, which penetrates the exhaust insert from top to bottom, communicates the inside of the mold core with the outside, and leads out the air trapped in the mold core.

所述间隙孔6为垂直设置,孔内设有金属粉末,或者,所述间隙孔6为垂直设置的通孔。The clearance holes 6 are arranged vertically, and metal powder is arranged in the holes, or the clearance holes 6 are through holes arranged vertically.

打印成型的模仁与排气镶件为一体结构,不可分离。The printed mold core and exhaust insert are integrated and inseparable.

本发明并不限于上述实施方式,采用与本发明上述实施例相同或近似方法或结构,而得到的其他3D打印一体结构排气镶件模仁方法及排气镶件模仁,均在本发明的保护范围之内。The present invention is not limited to the above-mentioned embodiments, and other 3D printing integrated structure exhaust insert mold core methods and exhaust insert mold cores obtained by adopting the same or similar methods or structures as the above-mentioned embodiments of the present invention are all included in the present invention. within the scope of protection.

Claims (10)

1.一种3D打印一体结构排气镶件模仁方法,其特征在于,其包括以下步骤:1. A 3D printing integrated structure exhaust insert mold kernel method, is characterized in that, it comprises the following steps: (1)通过CAD辅助软件建立一体结构的模仁与排气镶件的三维建模模型,所述排气镶件位于模仁中间部位;(1) Establish the three-dimensional modeling model of the mold core and the exhaust insert of an integrated structure by CAD auxiliary software, and the exhaust insert is located at the middle part of the mold core; (2)设置激光烧结的3D打印机,将步骤(1)的三维建模模型经过CAD建模及分层切片软件处理,获得一体结构的模仁以及排气镶件的3D打印机所需的各层数据,各层数据中包括模仁激光烧结区域及排气镶件激光烧结区域;将各层数据导入至3D打印机中,并在3D打印机中分别设置模仁激光烧结区域及排气镶件激光烧结区域的扫描参数;(2) Set up a 3D printer for laser sintering, and process the 3D modeling model in step (1) through CAD modeling and layered slicing software to obtain a mold core with an integrated structure and each layer required by the 3D printer for exhaust inserts Data, each layer of data includes the laser sintering area of the mold core and the laser sintering area of the exhaust insert; import the data of each layer into the 3D printer, and set the laser sintering area of the mold core and the laser sintering of the exhaust insert in the 3D printer The scan parameters of the area; (3)根据步骤(2)的激光扫描各层数据进行逐层扫描,模仁激光烧结区域形成致密结构的模仁,排气镶件的激光烧结区域形成有多个间隙孔结构的排气镶件,排气镶件与模仁为一体结构。(3) Carry out layer-by-layer scanning according to the laser scanning data of each layer in step (2), the laser sintering area of the mold core forms a mold core with a dense structure, and the laser sintering area of the exhaust insert forms an exhaust insert with multiple interstitial hole structures Parts, the exhaust insert and the mold core are integrated. 2.根据权利要求1所述的3D打印一体结构排气镶件模仁方法,其特征在于,所述步骤(3)中,逐层扫描的过程包括以下步骤:2. The 3D printing integrated structure exhaust insert mold core method according to claim 1, characterized in that, in the step (3), the process of layer-by-layer scanning comprises the following steps: (31)在激光束进行扫描一层时,激光束对模仁激光烧结区域进行扫描时,激光束以同为横向或同为纵向的方向进行逐行扫描,并且后一行激光束扫描轨迹与前一行激光束扫描轨迹设有重叠部分;(31) When the laser beam scans one layer, when the laser beam scans the laser sintering area of the mold core, the laser beam scans line by line in the same horizontal or vertical direction, and the laser beam scanning track of the next line is the same as that of the previous line. A row of laser beam scanning tracks is provided with overlapping parts; 激光束对排气镶件的激光烧结区域进行扫描时,激光束以同为横向或同为纵向的方向进行逐行扫描,并且后一行激光束扫描轨迹与前一行激光束扫描轨迹之间设有间隙;When the laser beam scans the laser sintering area of the exhaust insert, the laser beam scans line by line in the same horizontal or vertical direction, and there is an gap; (32)当激光束完成前一激光束扫描层扫描后,进行后一激光束扫描层扫描时,(32) When the laser beam scans the previous laser beam scanning layer and scans the next laser beam scanning layer, 激光束对模仁激光烧结区域进行扫描时,激光束以同为横向或同为纵向的方向进行逐行扫描,并且后一行激光束扫描轨迹与前一行激光束扫描轨迹设有重叠部分;When the laser beam scans the laser sintering area of the mold core, the laser beam scans line by line in the same horizontal or vertical direction, and the laser beam scanning track of the next line overlaps with the scanning track of the previous line of laser beam; 激光束对排气镶件的激光烧结区域进行扫描时,激光束以同为横向或同为纵向的方向进行逐行扫描,并且后一行激光束扫描轨迹与前一行激光束扫描轨迹之间设有间隙,When the laser beam scans the laser sintering area of the exhaust insert, the laser beam scans line by line in the same horizontal or vertical direction, and there is an gap, 后一激光束扫描层的排气镶件激光烧结区域的激光束扫描方向与前一激光束扫描层的排气镶件激光烧结区域的激光束扫描方向交叉;前一激光束扫描层中各行激光束扫描轨迹之间的间隙与后一激光束扫描层中各行激光束扫描轨迹之间的间隙交错重叠,形成间隙孔,该间隙孔为排气镶件的排气孔。The laser beam scanning direction of the exhaust insert laser sintering area of the latter laser beam scanning layer crosses the laser beam scanning direction of the exhaust insert laser sintering area of the previous laser beam scanning layer; each row of laser beams in the previous laser beam scanning layer The gaps between beam scanning tracks overlap with the gaps between each row of laser beam scanning tracks in the subsequent laser beam scanning layer to form a gap hole, which is the exhaust hole of the exhaust insert. 3.根据权利要求2所述的3D打印一体结构排气镶件模仁方法,其特征在于,其还包括以下步骤:3. The 3D printing integrated structure exhaust insert mold core method according to claim 2, characterized in that it also includes the following steps: (4)将间隙孔内的金属粉末吸出。(4) Suck out the metal powder in the gap hole. 4.根据权利要求2所述的3D打印一体结构排气镶件模仁方法,其特征在于,所述间隙孔的方向为竖直方向,从上往下贯穿排气镶件,将模仁内部与外部连通。4. The method for 3D printing an integrated structure exhaust insert mold core according to claim 2, characterized in that the direction of the clearance hole is a vertical direction, and runs through the exhaust insert from top to bottom, and the inside of the mold core is communicate with the outside world. 5.根据权利要求2所述的3D打印一体结构排气镶件模仁方法,其特征在于,步骤(32)中,后一激光束扫描层的排气镶件激光烧结区域的激光束扫描方向与前一激光束扫描层的排气镶件激光烧结区域的激光束扫描方向呈垂直交叉,或呈斜向交叉。5. The 3D printing integrated structure exhaust insert mold core method according to claim 2, characterized in that, in step (32), the laser beam scanning direction of the exhaust insert laser sintering area of the latter laser beam scanning layer The laser beam scanning direction of the exhaust insert laser sintering area of the previous laser beam scanning layer is vertically intersected, or obliquely intersected. 6.根据权利要求2所述的3D打印一体结构排气镶件模仁方法,其特征在于,步骤(31)或(32)中,激光束对模仁激光烧结区域进行扫描时,激光束以同为横向或同为纵向的方向进行逐行扫描,并且后一行激光束扫描轨迹与前一行激光束扫描轨迹设有重叠部分,重叠部分为激光束扫描轨迹的30%。6. The method for 3D printing an integrated structure exhaust insert mold core according to claim 2, characterized in that, in step (31) or (32), when the laser beam scans the laser sintering area of the mold core, the laser beam uses Both horizontal and vertical directions are scanned line by line, and the laser beam scanning track of the latter line is overlapped with the previous line of laser beam scanning track, and the overlapping portion is 30% of the laser beam scanning track. 7.一种由 权利要求1~6之一所述3D打印一体结构排气镶件模仁方法制作 的排气镶件模仁,其特征在于,所述排气镶件模仁为模仁与排气镶件组成的一体结构,所述排气镶件位于模仁中间部位,所述排气镶件内打印出多个间隙孔。7. An exhaust insert mold core made by the 3D printing integral structure exhaust insert mold core method according to one of claims 1 to 6, characterized in that, the exhaust insert mold core is a mold core and An integrated structure composed of exhaust inserts, the exhaust insert is located in the middle of the mold core, and multiple clearance holes are printed in the exhaust insert. 8.根据权利要求7所述的排气镶件模仁,其特征在于,所述间隙孔的方向为竖直方向,从上往下贯穿排气镶件,将模仁内部与外部连通。8 . The venting insert mold core according to claim 7 , wherein the direction of the clearance hole is a vertical direction, which penetrates the exhaust insert from top to bottom, and connects the inside of the mold core with the outside. 9.根据权利要求7所述的排气镶件模仁,其特征在于,所述间隙孔为垂直设置,孔内设有金属粉末。9. The exhaust insert mold core according to claim 7, characterized in that, the clearance holes are arranged vertically, and metal powder is arranged in the holes. 10.根据权利要求7所述的排气镶件模仁,其特征在于,所述间隙孔为垂直设置的通孔。10. The venting insert mold core according to claim 7, characterized in that, the clearance hole is a through hole arranged vertically.
CN201611187874.8A 2016-12-20 2016-12-20 3D printing integrated structure exhaust insert mold core method and exhaust insert mold core Active CN106735212B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611187874.8A CN106735212B (en) 2016-12-20 2016-12-20 3D printing integrated structure exhaust insert mold core method and exhaust insert mold core

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611187874.8A CN106735212B (en) 2016-12-20 2016-12-20 3D printing integrated structure exhaust insert mold core method and exhaust insert mold core

Publications (2)

Publication Number Publication Date
CN106735212A CN106735212A (en) 2017-05-31
CN106735212B true CN106735212B (en) 2018-05-08

Family

ID=58894255

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201611187874.8A Active CN106735212B (en) 2016-12-20 2016-12-20 3D printing integrated structure exhaust insert mold core method and exhaust insert mold core

Country Status (1)

Country Link
CN (1) CN106735212B (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3441162A1 (en) 2017-08-11 2019-02-13 Siemens Aktiengesellschaft Method of additively manufacturing a structure on a pre-existing component out of the powder bed
CN107498749A (en) * 2017-08-31 2017-12-22 东莞市康铭光电科技有限公司 A kind of exhaust structure and method for exhausting
CN107420721A (en) * 2017-08-31 2017-12-01 东莞市康铭光电科技有限公司 A kind of lubrication system and lubricating method
CN108099064A (en) * 2017-11-27 2018-06-01 山东豪迈机械科技股份有限公司 Mould manufacturing method and tire-mold based on 3D printing
CN108032466A (en) * 2017-11-27 2018-05-15 山东豪迈机械科技股份有限公司 A kind of tire-mold and its manufacture method
CN113183417A (en) * 2021-06-03 2021-07-30 深圳市银宝山新科技股份有限公司 Die gas circuit and die
CN116021715A (en) * 2021-10-27 2023-04-28 嘉兴海拉灯具有限公司 Mold core, injection molding system and mold core manufacturing method based on 3D printing

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103231055A (en) * 2013-05-13 2013-08-07 柳岸敏 Differential laser three-dimensional (3D) metal piece printing method
CN104399978A (en) * 2014-11-27 2015-03-11 华南理工大学 3D (Three Dimensional) forming method for large-sized porous amorphous alloy part of complex shape
CN105537588A (en) * 2016-01-21 2016-05-04 东莞市康铭光电科技有限公司 A kind of three-dimensional printing preparation method of plastic injection mold core and plastic injection mold core
CN106001568A (en) * 2016-07-07 2016-10-12 四川三阳永年增材制造技术有限公司 3D printing integrated preparation method for metal dies of gradient materials
CN106142454A (en) * 2015-04-15 2016-11-23 四川长虹电器股份有限公司 A kind of 3D prints the mould of processing
CN106182606A (en) * 2015-04-10 2016-12-07 株式会社松浦机械制作所 Resin injection molding mold

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005025779A2 (en) * 2003-09-11 2005-03-24 Ex One Corporation Layered manufactured articles having small-width fluid conduction vents and methods of making same

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103231055A (en) * 2013-05-13 2013-08-07 柳岸敏 Differential laser three-dimensional (3D) metal piece printing method
CN104399978A (en) * 2014-11-27 2015-03-11 华南理工大学 3D (Three Dimensional) forming method for large-sized porous amorphous alloy part of complex shape
CN106182606A (en) * 2015-04-10 2016-12-07 株式会社松浦机械制作所 Resin injection molding mold
CN106142454A (en) * 2015-04-15 2016-11-23 四川长虹电器股份有限公司 A kind of 3D prints the mould of processing
CN105537588A (en) * 2016-01-21 2016-05-04 东莞市康铭光电科技有限公司 A kind of three-dimensional printing preparation method of plastic injection mold core and plastic injection mold core
CN106001568A (en) * 2016-07-07 2016-10-12 四川三阳永年增材制造技术有限公司 3D printing integrated preparation method for metal dies of gradient materials

Also Published As

Publication number Publication date
CN106735212A (en) 2017-05-31

Similar Documents

Publication Publication Date Title
CN106735212B (en) 3D printing integrated structure exhaust insert mold core method and exhaust insert mold core
CN111037917B (en) FDM printing method, system and medium based on model splitting and splicing printing
CN104226996B (en) A kind of laser 3D prints the device and method of impeller of pump
CN105538712B (en) A kind of 3D printing method of laser compound-contoured scanning
EP3175972B1 (en) Method for producing a mold, and mold
CN103434137B (en) A kind of toy manufacture method based on rapid shaping technique
JP2017137563A (en) Manufacturing method of three-dimensional shape molded article
CN110744354B (en) A method for determining the timing of alternation in composite manufacturing of additive and subtractive materials
CN103121082A (en) V8 type gray cast iron cylinder body casting pouring method
US20180200795A1 (en) Method for manufacturing three-dimensional shaped object and three-dimensional shaped object
WO2022066980A8 (en) Transparent support bath for embedded 3d printing and system for in process monitoring
CN109732913A (en) A kind of 3D printing manufacturing method of shoe tree
CN103847102B (en) Laser shell mould invalid rapid forming method of film covering powder material
CN107390642B (en) The deburring cutter block of computer readable storage medium and the application medium produces lathes
CN106925776A (en) A kind of subregion scanning pattern generation method of control increasing material manufacturing stress deformation
CN111215578A (en) A casting mold preparation method based on shell mold additive and residual area filling
CN110126266A (en) A kind of three-dimension object manufacturing method
CN109635322A (en) A kind of method that automobile panel process complementary surface section line is arranged automatically
CN108213342A (en) The casting technique of the complicated smallclothes of batch production
TWI585558B (en) Three dimensional printing method
JP2001254107A (en) Three-dimensional model structure by stereolithography, object structure by stereolithography, and modeling method by stereolithography
CN104309127B (en) A kind of hollow mould Method of printing
CN106345914B (en) Structure of insert and manufacturing method
KR102127648B1 (en) Method of manufacturing salt core
CN108312545A (en) A kind of selective laser sintering part preprocess method

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant