GB2453774A - A method of making an article with a re-entrant by reversibly bonding underlying powder - Google Patents

A method of making an article with a re-entrant by reversibly bonding underlying powder Download PDF

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Publication number
GB2453774A
GB2453774A GB0720449A GB0720449A GB2453774A GB 2453774 A GB2453774 A GB 2453774A GB 0720449 A GB0720449 A GB 0720449A GB 0720449 A GB0720449 A GB 0720449A GB 2453774 A GB2453774 A GB 2453774A
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United Kingdom
Prior art keywords
article
powder
layer
bonding
entrant
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.)
Granted
Application number
GB0720449A
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GB0720449D0 (en
GB2453774B (en
Inventor
Trevor Illston
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.)
Materials Solutions Ltd
Original Assignee
Materials Solutions 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 Materials Solutions Ltd filed Critical Materials Solutions Ltd
Priority to GB0720449.8A priority Critical patent/GB2453774B/en
Publication of GB0720449D0 publication Critical patent/GB0720449D0/en
Publication of GB2453774A publication Critical patent/GB2453774A/en
Application granted granted Critical
Publication of GB2453774B publication Critical patent/GB2453774B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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
    • B29C64/00Additive 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
    • B29C64/10Processes of additive manufacturing
    • B29C64/141Processes of additive manufacturing using only solid materials
    • B29C64/153Processes of additive manufacturing using only solid materials using layers of powder being selectively joined, e.g. by selective laser 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
    • B22F5/00Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
    • B22F5/10Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of articles with cavities or holes, not otherwise provided for in the preceding subgroups
    • 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
    • B22F10/20Direct sintering or melting
    • B22F10/28Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM]
    • 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
    • B22F10/60Treatment of workpieces or articles after build-up
    • B22F10/68Cleaning or washing
    • B22F3/1055
    • 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
    • B29C64/00Additive 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
    • B29C64/40Structures for supporting 3D objects during manufacture and intended to be sacrificed after completion thereof
    • 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
    • B33Y40/00Auxiliary operations or equipment, e.g. for material handling
    • B33Y40/20Post-treatment, e.g. curing, coating or polishing
    • 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

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  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Plasma & Fusion (AREA)
  • Optics & Photonics (AREA)
  • Powder Metallurgy (AREA)

Abstract

A method of making an article 10 using selective laser sintering, wherein the object 10 has at least one re-entrant or overhanging feature 16, comprises the steps of forming a layer of metal powder 15 on a base 12 and selectively laser fusing portions of the layer to form the object 10 such that process continues until the "overhang" feature 16 occurs whereby the unfused metal powder 15 in the preceding or underlying layer is reversely bonded making it stable under the application of the laser. By reversibly bonding the powder, balling up and weld spatter is avoided thus enabling complex objects containing overhangs, hollows and voids to be created. The unfused powder is bonded using an adhesive and the bonding is reversed by the application of solvent, heat and/or electromagnetic energy. The unfused powder can then be removed from the article.

Description

I
A method of making an article This invention relates to a method of making an article having at least one re-entrant surface.
Rapid Prototyping of plastics by various techniques is well known and more recently metal powders have been processed by laser in layers. It is equally well known that support structures (scaffolding') are frequently required and these may be provide in the same material or by a secondary material that may be e.g. water soluble or melts at a lower temperature to the primary material used to build the desired prototype article. It is also known to form an article by using adhesive droplets deposited on each thin powder layer to create bonding. Such a process is "3D printing" as described in US patent 6589471.
Aiso known is where a green' article is first formed e.g. in Metal Injection Moulding whereby metal powder is bonded together by a binder which is then fired to form the nominally solid article. These are inherently never 100% dense and are not useful for many applications-particularly where internal voids can precipitate fatigue cracking. Such bonding/firing techniques may be used to form metal parts from a metal/polymer powder raw material where firstly the polymer is melted/sintered by selective application of a laser to form a green' article that is subsequently fired to metal and join together the metal powder. Alternatively the article formed of powder may not be fully dense and it is subsequently infiltrated with a liquid that hardens to make a solid object.
More particularly it is known to manufacture articles by laying down successive layers of metal powder, and, after each layer has been laid down, solidifying selected portions of the layer by suitable operation of a scanning laser so that an article of simple or complex shape can be built up. Some form of support or scaffold' is frequently required to support a layer of the article during build and there is a significant problem with any structure in which the solidified portion is not supported by a solidified portion in the preceding layer, because if the laser is applied to a bulk of unsolidified metal powder, that powder simply balls up into clumps analogous to weld splatter'. Such solid supports of certain complex structures, particularly where they are located one above another, present great difficulty. Whilst they can be built, their subsequent removal to complete the article may be difficult or impossible. An example is where two rows of vanes are to be built one above another within a double walled casing.
From one aspect the invention consists in a method of making an article having at ieast one re-entrant surface including the steps of: (a) forming a layer of metal powder on a base; (b) selectively laser fusing portions of the layer; and (c) repeating steps (a) and (b) to form the article, each step (a) being performed on the preceding layer characterised in that prior to performing step (a) in a layer which will initiate the formation of a re-entrant feature reversibly bonding at least some of the unfused underlying powder such that it is stable under the application of the laser.
The applicants have realised that by bonding such powder in a reversible way, they are able to prevent balling up of the powder, but still be able to reverse the bonding allowing subsequent removal of the powder from the article.
Typically the undersurface of the re-entrant feature in the build orientation will be at least substantially parallel to the layer.
The unfused powder may be bonded using an adhesive. This is a surprising finding as it might reasonably be expected that the heat of the laser when fusing the metal powder would also destroy the adhesive. The bonding step may subsequently be reversed, for example, by solvent, heat and/or the application of electro-magnetic energy or any other suitable process. Preferably the adhesive is a hydrocarbon with low reactivity with the powdered metal.
The loose powder is preferably removed from the article subsequent to the bonding reversal e.g. by heating to a temperature below a metal hardening temperature and the article may, for example, be at least partially hollow.
Although the invention has been described above it is to be understood it includes any inventive combination of the features set out above or in the
following description.
The invention may be performed in various ways and a specific embodiment will now be described by way of example, with reference to the accompanying drawing in which Figure Ia is a side view of a part of a notional article 10 and Figure lb. The drawing is a scrap cross-sectional view of the notional article 10 along the line A-A. As will be well understood by persons skilled in the art, the article portion 11 can readily be built up by the use of standard selective laser sintering processes in which a layer of material is formed on a base plate 12, selectively sintered using a scanning laser and then covered by a further layer as the base plate 12 descends by the intended layer thickness. Typically such articles contain voids, as illustrated at 13 and 14 and these remain filled with unfused powder 15.
If it is then desired to form a re-entrant surface, such as indicated at 16 as part of a further portion 17 of the article 10, then this will prove to be impossible, because the powder 15 will simply ball up as soon as the laser is applied to it.
Accordingly the applicants bond the powder 15 by stopping the build immediately before the layer 16 that would commence building feature 17 and applying an adhesive such as super glue' for at least a depth which is sufficient to prevent balling to take place. Thus far it has been found unnecessary to bond all the powder 15 and even where a portion 17 can be built without this technique the undersurface of portion 17 at 16 is improved by this technique-due to the absence of adhered weld splatter'-like material created by laser penetration into the powder 15. Without the glue the undersurface at 16 is rough and the geometry of the article 10 may present a difficulty in access for polishing to be suitable for good airflow. With the glue the surface at 16 is smooth enough not to require polishing.
In some articles, it may be acceptable to retain the bonded powder during the life of the article, but in general it will be desirable to reverse the bonding so that the powder can be removed. This may be done by the use of solvents, heat, the application of electro-magnetic energy or any other suitable process.
This technique has experimentally been performed using stainless steel powder and it is expected to work with other metal powders such as high temperature metal alloys widely used in aerospace.

Claims (6)

  1. Claims 1. A method of making an article having at least one re-entrant surface including the steps of: (a) forming a layer of metal powder on a base; (b) selectively laser fusing portions of the layer; and (C) repeating steps (a) and (b) to form the article, each step (a) being performed on the preceding layer characterised in that prior to performing step (a) in a layer which wifi initiate the formation of a re-entrant feature reversibly bonding at least some of the unfused underlying powder such that it is stable under the application of the laser.
  2. 2. A method as claimed in Claim 1 wherein the undersurface of the re-entrant feature in a build orientation is at least substantially parallel to the layer.
  3. 3. A method as claimed in claim I or 2 wherein the unfused powder is bonded using an adhesive.
  4. 4. A method as claimed in any one of the preceding claims wherein the bonding step is reversed, for example, by solvent, heat and/or the application of electromagnetic energy.
  5. 5. A method as claimed in claim 4 wherein the loose powder is removed from the article subsequent to bonding reversal.
  6. 6. A method as claimed in any one of the preceding claims wherein the article is at least partially hollow.
GB0720449.8A 2007-10-19 2007-10-19 A method of making an article Active GB2453774B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB0720449.8A GB2453774B (en) 2007-10-19 2007-10-19 A method of making an article

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0720449.8A GB2453774B (en) 2007-10-19 2007-10-19 A method of making an article

Publications (3)

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GB0720449D0 GB0720449D0 (en) 2007-11-28
GB2453774A true GB2453774A (en) 2009-04-22
GB2453774B GB2453774B (en) 2013-02-20

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Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9739161B2 (en) 2013-02-27 2017-08-22 Rolls-Royce Plc Vaned structure and a method of manufacturing a vaned structure
US9925797B2 (en) 2014-08-07 2018-03-27 Orbotech Ltd. Lift printing system
GB2556661A (en) * 2016-09-21 2018-06-06 Bae Systems Plc Improved additive layer manufacturing
US10193004B2 (en) 2014-10-19 2019-01-29 Orbotech Ltd. LIFT printing of conductive traces onto a semiconductor substrate
US10471538B2 (en) 2015-07-09 2019-11-12 Orbotech Ltd. Control of lift ejection angle
US10629442B2 (en) 2013-10-14 2020-04-21 Orbotech Ltd. Lift printing of multi-composition material structures
US10633758B2 (en) 2015-01-19 2020-04-28 Orbotech Ltd. Printing of three-dimensional metal structures with a sacrificial support
US10688692B2 (en) 2015-11-22 2020-06-23 Orbotech Ltd. Control of surface properties of printed three-dimensional structures
US11881466B2 (en) 2017-05-24 2024-01-23 Orbotech Ltd. Electrical interconnection of circuit elements on a substrate without prior patterning

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11833749B2 (en) * 2017-12-19 2023-12-05 Stratasys, Inc. Method for producing a treated, 3D printed object

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5555481A (en) * 1993-11-15 1996-09-10 Rensselaer Polytechnic Institute Method of producing solid parts using two distinct classes of materials
WO2001038061A1 (en) * 1999-10-26 2001-05-31 University Of Southern California Process of making a three-dimensional object
US20040018107A1 (en) * 2002-07-23 2004-01-29 Behrokh Khoshnevis Metallic parts fabrication using selective inhibition of sintering (SIS)
WO2004058487A1 (en) * 2002-12-20 2004-07-15 University Of Southern California Methods for reduction of powder waste in selective inhibition of sintering (sis)
US20040137228A1 (en) * 2002-09-21 2004-07-15 Degussa Ag Polymer powders for SIB processes
EP1775104A1 (en) * 2005-10-14 2007-04-18 Northrop Grumman Corporation Method for enhancing density of a three-dimensional object

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5555481A (en) * 1993-11-15 1996-09-10 Rensselaer Polytechnic Institute Method of producing solid parts using two distinct classes of materials
WO2001038061A1 (en) * 1999-10-26 2001-05-31 University Of Southern California Process of making a three-dimensional object
US20040018107A1 (en) * 2002-07-23 2004-01-29 Behrokh Khoshnevis Metallic parts fabrication using selective inhibition of sintering (SIS)
US20040137228A1 (en) * 2002-09-21 2004-07-15 Degussa Ag Polymer powders for SIB processes
WO2004058487A1 (en) * 2002-12-20 2004-07-15 University Of Southern California Methods for reduction of powder waste in selective inhibition of sintering (sis)
EP1775104A1 (en) * 2005-10-14 2007-04-18 Northrop Grumman Corporation Method for enhancing density of a three-dimensional object

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9739161B2 (en) 2013-02-27 2017-08-22 Rolls-Royce Plc Vaned structure and a method of manufacturing a vaned structure
US10629442B2 (en) 2013-10-14 2020-04-21 Orbotech Ltd. Lift printing of multi-composition material structures
US9925797B2 (en) 2014-08-07 2018-03-27 Orbotech Ltd. Lift printing system
US10193004B2 (en) 2014-10-19 2019-01-29 Orbotech Ltd. LIFT printing of conductive traces onto a semiconductor substrate
US10633758B2 (en) 2015-01-19 2020-04-28 Orbotech Ltd. Printing of three-dimensional metal structures with a sacrificial support
US10471538B2 (en) 2015-07-09 2019-11-12 Orbotech Ltd. Control of lift ejection angle
US10688692B2 (en) 2015-11-22 2020-06-23 Orbotech Ltd. Control of surface properties of printed three-dimensional structures
GB2556661A (en) * 2016-09-21 2018-06-06 Bae Systems Plc Improved additive layer manufacturing
US11881466B2 (en) 2017-05-24 2024-01-23 Orbotech Ltd. Electrical interconnection of circuit elements on a substrate without prior patterning

Also Published As

Publication number Publication date
GB0720449D0 (en) 2007-11-28
GB2453774B (en) 2013-02-20

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