WO2001026498A1 - Die manufacturing - Google Patents

Die manufacturing Download PDF

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Publication number
WO2001026498A1
WO2001026498A1 PCT/ZA2000/000182 ZA0000182W WO0126498A1 WO 2001026498 A1 WO2001026498 A1 WO 2001026498A1 ZA 0000182 W ZA0000182 W ZA 0000182W WO 0126498 A1 WO0126498 A1 WO 0126498A1
Authority
WO
WIPO (PCT)
Prior art keywords
casting
die
cad model
oversize
facility
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.)
Ceased
Application number
PCT/ZA2000/000182
Other languages
English (en)
French (fr)
Inventor
Robert James Bond
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.)
RAPID DESIGN TECHNOLOGIES Pty Ltd
Original Assignee
RAPID DESIGN TECHNOLOGIES Pty 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 RAPID DESIGN TECHNOLOGIES Pty Ltd filed Critical RAPID DESIGN TECHNOLOGIES Pty Ltd
Priority to HK03104511.9A priority Critical patent/HK1052280B/zh
Priority to CA002382750A priority patent/CA2382750C/en
Priority to DE60020725T priority patent/DE60020725T2/de
Priority to JP2001529296A priority patent/JP2003527977A/ja
Priority to AU78876/00A priority patent/AU771152C/en
Priority to AT00969047T priority patent/ATE297142T1/de
Priority to US10/089,944 priority patent/US6691763B1/en
Priority to EP00969047A priority patent/EP1220625B1/en
Publication of WO2001026498A1 publication Critical patent/WO2001026498A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C39/00—Shaping by casting, i.e. introducing the moulding material into a mould or between confining surfaces without significant moulding pressure; Apparatus therefor
    • B29C39/02—Shaping by casting, i.e. introducing the moulding material into a mould or between confining surfaces without significant moulding pressure; Apparatus therefor for making articles of definite length, i.e. discrete articles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C33/00—Moulds or cores; Details thereof or accessories therefor
    • B29C33/38—Moulds or cores; Details thereof or accessories therefor characterised by the material or the manufacturing process
    • B29C33/3835—Designing moulds, e.g. using CAD-CAM
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C64/00—Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
    • B29C64/30—Auxiliary operations or equipment
    • B29C64/386—Data acquisition or data processing for additive manufacturing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2793/00—Shaping techniques involving a cutting or machining operation
    • B29C2793/0009—Cutting out
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2793/00—Shaping techniques involving a cutting or machining operation
    • B29C2793/009—Shaping techniques involving a cutting or machining operation after shaping
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0037—Other properties
    • B29K2995/0094—Geometrical properties
    • 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
    • B33Y80/00—Products made by additive manufacturing
    • C—CHEMISTRY; METALLURGY
    • C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D1/00—Electroforming

Definitions

  • This invention relates to a system and to a method for the manufacture and production of dies and, more specifically, but not exclusively, to a system and to a method for the production and manufacture of dies to be utilised in a wide range of production processes, such as injection moulding, gravity die casting and the like.
  • a method and a system for producing a metal article such as a die is disclosed in applicant's South African Patent Application No. 99/2209, which is incorporated herein in its entirety by reference.
  • the disclosed ' method of producing a die includes the steps of: providing a CAD model of the die to be formed; rapid prototyping a three-dimensional patterns of the die from the CAD model thereof; producing mould of the die from the three-dimensional pattern thereof; and casting the die from the mould.
  • the applicant's method is effective and allows for the rapid production of new tooling, a number of difficulties have emerged.
  • the castings produced in the casting step of the method exhibit a degree of metal shrinkage which is difficult to predict and which affects the accuracy of a final article which is to be produced by means of the die.
  • a method for producing a die comprising the steps of: providing a reference CAD model of the die of desired dimensions; producing an oversized casting of the die from a mould thereof; measuring the actual dimensions of the oversized casting; comparing the measured dimensions of the oversized die against the reference
  • an oversize casting of the die by the steps of: providing an oversize CAD model of the die; including in the oversize CAD model a number of reference points sufficient to define a three-dimensional co-ordinate system relative to the CAD model; rapid prototyping a three-dimensional pattern of the die from the oversize CAD model thereof; producing a mould of the die from the three-dimensional pattern thereof; and casting the oversize die from the mould. Still further features of the invention provide for measuring the actual dimensions of the oversize casting by the steps of: imaging the oversize casting to obtain the co-ordinates of the surface of the oversize casting relative to the three dimensional co-ordinate system defined by the number of reference points on the casting; and converting the co-ordinates into a measured CAD model.
  • Yet further features of the invention provide for ablating the oversize casting by any one of the methods of laser ablation , machining or spark erosion, and for imaging the oversize casting by means of a laser-based, alternatively a contact-based imaging system.
  • the method includes the additional step of texturing at least a portion of the surface of the casting; and texturing at least a portion of the surface of the casting by: providing a reference CAD model of the desired texture to be applied to the surface of the casting; identifying the portion of the surface of the casting to be textured as a function of the co-ordinates of each one of the number of reference points on the casting; and ablating the identified portion of the surface of the casting in accordance with the reference CAD model of the desired texture to be applied to the casting.
  • the invention extends to a system for producing a die comprising: means for generating a reference CAD model of a die of desired dimensions to be produced; a production facility arranged to produce an oversized casting of the die from a mould thereof; measuring means for measuring the actual dimensions of the oversized casting; comparator means for comparing the measured dimensions of the oversized die against the reference CAD model; and an ablating facility adapted to machine the oversized casting until its dimensions are substantially the same as those of the reference CAD model.
  • the production facility to include: means for generating an oversize CAD model of the die, containing a number of reference points sufficient to define a three-dimensional co-ordinate system relative to the CAD model; a rapid prototyping facility arranged to produce a three-dimensional pattern of the die from the oversize CAD model thereof; and a production means for producing a mould of the die from the three-dimensional pattern thereof, and for casting the die from the mould thereof.
  • the measuring means prefferably be an imaging system adapted to obtain the co-ordinates of the surface of the oversize casting relative to the three-dimensional co-ordinate system defined by the number of reference points on the casting, and to convert the co-ordinates into a measured CAD model.
  • the ablating facility to be any one of a laser ablating facility, a machining facility or a spark erosion facility and for the imaging system to be a laser-based, alternatively a contact-based imaging system.
  • the system includes a texturing means for texturing at least a portion of the surface of the casting, and for the texturing means to include: means for generating a reference CAD model of a desired texture to be applied to the surface of the casting; identification means for identifying the portion of the surface of the casting to be textured, as a function of the co-ordinates of each one of the number reference points on the casting; and an ablating facility adapted to ablate the identified portion of the surface of the casting in accordance with the reference CAD model of the desired texture to be applied to the casting.
  • the ablating facility prefferably be a laser machining facility.
  • the oversize casting to include at least one integral pathway therethrough and for the pathway to include a hollow back and a baffle to direct a flow of coolant therethrough.
  • FIG.1 is a schematic representation of a system for producing a die, according to the invention.
  • a system for producing a die is indicated generally by reference numeral (1 ).
  • the system (1 ) includes a rapid prototyping facility indicated generally by reference numeral (2) and a production facility (3).
  • the rapid prototyping facility (2) includes a
  • CAD processor (not shown) and a Stereo Lithography (SL) machine (9).
  • SL Stereo Lithography
  • the CAD processor (7) produces data relating to a three-dimensional model of a die which is to be manufactured.
  • the CAD model includes a number, preferably three, of reference points on the die sufficient to define a three-dimensional co-ordinate system relative to the die. These reference points are used as a basis for measuring the physical dimensions of a die produced in accordance with the CAD model as will be described in more detail below.
  • the production facility (3) includes a electroforming bath, an investment casting facility and a flash fire furnace (not shown), which are well known in the art.
  • the system (1) includes further a measuring means (4) in the form of a laser imaging system, which is commercially available from Brenckmann GmbH of Germany as well as an ablation facility (5) in the form of a laser machining system of the type which are well known in the art and which are commercially available from HK Technologies Laser Systems of the United Kingdom or LANG GmbH and Co. of Germany.
  • a measuring means (4) in the form of a laser imaging system, which is commercially available from Brenckmann GmbH of Germany as well as an ablation facility (5) in the form of a laser machining system of the type which are well known in the art and which are commercially available from HK Technologies Laser Systems of the United Kingdom or LANG GmbH and Co. of Germany.
  • a CAD model (7) is produced by the CAD processor (not shown) of a die of desired dimensions to be manufactured by the system.
  • the CAD processor also produces an oversized CAD model (8) of the die to compensate for nominal shrinking during a casting step of the production process which will be described in greater detail below.
  • a three-dimensional pattern of the oversized die is produced from the oversized CAD model (8) thereof by means of the SL machine (9).
  • a mould of the die is then produced by the investment casting facility from the oversized three-dimensional pattern of the die, and a casting of the oversized die is produced from the mould by casting techniques which are well known in the art.
  • the dimensions of the oversized casting are measured by the laser imaging system (4) and converted to a CAD representation which is compared, at (10) with the nominally sized CAD model (7) of the die produced by the CAD processor to determine the deviation therefrom.
  • the deviation, or error is used as a control input for the ablation facility (5) to machine and remove material from the oversize casting until its dimensions conform to those of the desired size as reflected by the reference CAD model (7).
  • the system (1 ) may be conveniently utilised to achieve such a result.
  • the system provides for the CAD processor (not shown) to generate a reference CAD model (11) of a desired texture to be applied to the surface of the casting.
  • the imaging system (4) is also employed to identify a desired portion of the surface of the casting to be textured, as a function of the co-ordinates of each of the three reference points on the casting.
  • the CAD processor is then used to compute the depth and scale of the texture to be applied to the surface of the casting and to control the laser head of the laser machining system (5) to ablate the identified portion of the surface of the casting such that the desired texture is applied to the casting as required.
  • the imaging system (4) may be a contact- based rather than a laser-based imaging system
  • the laser machining system used for size reduction of the oversized casting maybe three-dimensional laser machining system, while that employed for texturing of the nominally sized casting may be a two-dimensional rather than a three-dimensional laser machining system.
  • size reduction of the oversize casting may be achieved by conventional machining or by spark erosion instead of laser ablation.
  • the oversize casting may be produced to include one or more integral pathways therethrough, each pathway having a hollow back and a baffle to direct a flow of coolant therethrough. When such hollow back dies are used in a production process, they will allow a shorter cycle time of the die to be achieved.
  • the invention therefore provides a system and a method for the production of dies which eliminates the need for accurate prediction and compensation of shrinkage during casting in prior art methods.

Landscapes

  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Optics & Photonics (AREA)
  • Physics & Mathematics (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
  • Extrusion Moulding Of Plastics Or The Like (AREA)
  • Mounting, Exchange, And Manufacturing Of Dies (AREA)
  • Macromolecular Compounds Obtained By Forming Nitrogen-Containing Linkages In General (AREA)
  • Polymers With Sulfur, Phosphorus Or Metals In The Main Chain (AREA)
  • Acyclic And Carbocyclic Compounds In Medicinal Compositions (AREA)
  • Formation And Processing Of Food Products (AREA)
PCT/ZA2000/000182 1999-10-08 2000-10-06 Die manufacturing Ceased WO2001026498A1 (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
HK03104511.9A HK1052280B (zh) 1999-10-08 2000-10-06 制造模具的方法和系统
CA002382750A CA2382750C (en) 1999-10-08 2000-10-06 Die manufacturing
DE60020725T DE60020725T2 (de) 1999-10-08 2000-10-06 Herstellung einer form
JP2001529296A JP2003527977A (ja) 1999-10-08 2000-10-06 金型製造
AU78876/00A AU771152C (en) 1999-10-08 2000-10-06 Die manufacturing
AT00969047T ATE297142T1 (de) 1999-10-08 2000-10-06 Herstellung einer form
US10/089,944 US6691763B1 (en) 1999-10-08 2000-10-06 Die manufacturing
EP00969047A EP1220625B1 (en) 1999-10-08 2000-10-06 Die manufacturing

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ZA99/6374 1999-10-08
ZA996374 1999-10-08

Publications (1)

Publication Number Publication Date
WO2001026498A1 true WO2001026498A1 (en) 2001-04-19

Family

ID=25587949

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/ZA2000/000182 Ceased WO2001026498A1 (en) 1999-10-08 2000-10-06 Die manufacturing

Country Status (10)

Country Link
US (1) US6691763B1 (enExample)
EP (1) EP1220625B1 (enExample)
JP (1) JP2003527977A (enExample)
CN (1) CN1177551C (enExample)
AT (1) ATE297142T1 (enExample)
AU (1) AU771152C (enExample)
CA (1) CA2382750C (enExample)
DE (1) DE60020725T2 (enExample)
HK (1) HK1052280B (enExample)
WO (1) WO2001026498A1 (enExample)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1321063A3 (en) * 2001-12-20 2004-06-23 High Prototyping S.a.s. Wax pattern, process for setting precious and non-precious stones and jewel obtained
EP2918387A1 (en) * 2014-03-12 2015-09-16 Reydel Automotive B.V. Method for molding interior and exterior members of vehicles

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6354836B1 (en) * 1998-08-20 2002-03-12 Jeneric/Pentron, Inc. Methods of producing dental restorations using CAD/CAM and manufactures thereof
DE102005037308B4 (de) * 2005-08-04 2018-12-20 Werkzeugbau Siegfried Hofmann Gmbh Entlüftetes, mit einem Werkstoff befüllbares Spritzwerkzeug
DE102006038795A1 (de) * 2006-08-18 2008-03-20 Fft Edag Produktionssysteme Gmbh & Co. Kg Überwachungsvorrichtung für eine Laserbearbeitungsvorrichtung
US8784723B2 (en) * 2007-04-01 2014-07-22 Stratasys Ltd. Method and system for three-dimensional fabrication
CN103192612B (zh) * 2013-04-09 2015-09-16 中国科学院重庆绿色智能技术研究院 基于磁流变材料的3d打印机器人系统及打印方法
CN103286454A (zh) * 2013-06-08 2013-09-11 爱司帝光电科技(苏州)有限公司 激光精密加工系统及激光去除毛边方法
CN103862597B (zh) * 2014-02-24 2016-05-04 锦丰科技（深圳）有限公司 一种注塑模具制造方法
WO2015167965A1 (en) * 2014-04-30 2015-11-05 Cummins Inc. Creation of injection molds via additive manufacturing
CN105921626B (zh) * 2016-04-23 2018-02-27 大连顶金通用设备制造股份有限公司 一种多动模具装置及其制造方法
CN107014973B (zh) * 2017-03-30 2019-01-29 华中科技大学 一种基于动态压强的重力铸造缩孔缺陷检测方法
CN109895341A (zh) * 2017-12-11 2019-06-18 财团法人金属工业研究发展中心 自由曲面镜片的模仁补偿方法
CN113524686B (zh) * 2020-12-17 2023-03-28 浙江闪铸三维科技有限公司 3d打印模型分区方法

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US5823778A (en) * 1996-06-14 1998-10-20 The United States Of America As Represented By The Secretary Of The Air Force Imaging method for fabricating dental devices
US5837960A (en) * 1995-08-14 1998-11-17 The Regents Of The University Of California Laser production of articles from powders
WO1999039889A1 (en) * 1998-02-06 1999-08-12 Express Tool, Inc. Thermally efficient mold apparatus and method

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US5837960A (en) * 1995-08-14 1998-11-17 The Regents Of The University Of California Laser production of articles from powders
US5823778A (en) * 1996-06-14 1998-10-20 The United States Of America As Represented By The Secretary Of The Air Force Imaging method for fabricating dental devices
WO1999039889A1 (en) * 1998-02-06 1999-08-12 Express Tool, Inc. Thermally efficient mold apparatus and method

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1321063A3 (en) * 2001-12-20 2004-06-23 High Prototyping S.a.s. Wax pattern, process for setting precious and non-precious stones and jewel obtained
EP2918387A1 (en) * 2014-03-12 2015-09-16 Reydel Automotive B.V. Method for molding interior and exterior members of vehicles
US10059040B2 (en) 2014-03-12 2018-08-28 Reydel Automotive B.V. Method for molding interior and exterior members of vehicles

Also Published As

Publication number Publication date
AU7887600A (en) 2001-04-23
CN1177551C (zh) 2004-12-01
CA2382750C (en) 2008-12-23
DE60020725T2 (de) 2006-03-23
EP1220625A1 (en) 2002-07-10
AU771152B2 (en) 2004-03-18
HK1052280B (zh) 2005-05-06
US6691763B1 (en) 2004-02-17
DE60020725D1 (de) 2005-07-14
CN1390099A (zh) 2003-01-08
HK1052280A1 (en) 2003-09-11
AU771152C (en) 2005-04-14
JP2003527977A (ja) 2003-09-24
ATE297142T1 (de) 2005-06-15
EP1220625B1 (en) 2005-06-08
CA2382750A1 (en) 2001-04-19

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