GB2458745A - Grooved support for selective sintering or melting process - Google Patents
Grooved support for selective sintering or melting process Download PDFInfo
- Publication number
- GB2458745A GB2458745A GB0901686A GB0901686A GB2458745A GB 2458745 A GB2458745 A GB 2458745A GB 0901686 A GB0901686 A GB 0901686A GB 0901686 A GB0901686 A GB 0901686A GB 2458745 A GB2458745 A GB 2458745A
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- GB
- United Kingdom
- Prior art keywords
- support
- channels
- article
- platen
- grooves
- 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
Links
- 238000010309 melting process Methods 0.000 title claims abstract description 26
- 238000005245 sintering Methods 0.000 title claims abstract description 24
- 239000000843 powder Substances 0.000 claims abstract description 59
- 238000000034 method Methods 0.000 claims abstract description 57
- 238000005520 cutting process Methods 0.000 claims description 7
- 239000000463 material Substances 0.000 claims description 5
- 230000015572 biosynthetic process Effects 0.000 abstract 1
- 239000007787 solid Substances 0.000 description 20
- 238000000149 argon plasma sintering Methods 0.000 description 6
- 238000004132 cross linking Methods 0.000 description 3
- 238000010894 electron beam technology Methods 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 230000035882 stress Effects 0.000 description 3
- 241001634884 Cochlicopa lubricella Species 0.000 description 2
- 230000032798 delamination Effects 0.000 description 2
- 238000009760 electrical discharge machining Methods 0.000 description 2
- 239000000835 fiber Substances 0.000 description 2
- 239000000314 lubricant Substances 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 230000008646 thermal stress Effects 0.000 description 2
- 229910000684 Cobalt-chrome Inorganic materials 0.000 description 1
- 229910001069 Ti alloy Inorganic materials 0.000 description 1
- 229910001315 Tool steel Inorganic materials 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 239000010952 cobalt-chrome Substances 0.000 description 1
- 238000005137 deposition process Methods 0.000 description 1
- 239000010432 diamond Substances 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 231100001261 hazardous Toxicity 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 238000001465 metallisation Methods 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 239000012254 powdered material Substances 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 238000010079 rubber tapping Methods 0.000 description 1
- 238000000110 selective laser sintering Methods 0.000 description 1
- 239000011343 solid material Substances 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 238000007514 turning Methods 0.000 description 1
- 238000009736 wetting Methods 0.000 description 1
- 238000009763 wire-cut EDM Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
-
- 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
- B29C64/10—Processes of additive manufacturing
- B29C64/141—Processes of additive manufacturing using only solid materials
- B29C64/153—Processes of additive manufacturing using only solid materials using layers of powder being selectively joined, e.g. by selective laser sintering or melting
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/20—Direct sintering or melting
- B22F10/28—Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM]
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/40—Structures for supporting workpieces or articles during manufacture and removed afterwards
-
- B22F3/008—
-
- B22F3/1055—
-
- 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
- B29C64/40—Structures for supporting 3D objects during manufacture and intended to be sacrificed after completion thereof
-
- 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
- B29C67/00—Shaping techniques not covered by groups B29C39/00 - B29C65/00, B29C70/00 or B29C73/00
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F12/00—Apparatus or devices specially adapted for additive manufacturing; Auxiliary means for additive manufacturing; Combinations of additive manufacturing apparatus or devices with other processing apparatus or devices
- B22F12/60—Planarisation devices; Compression devices
- B22F12/67—Blades
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P10/00—Technologies related to metal processing
- Y02P10/25—Process efficiency
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Mechanical Engineering (AREA)
- Plasma & Fusion (AREA)
- Powder Metallurgy (AREA)
Abstract
A method of forming a support for use in a selective sintering or melting process comprises the formation of a support 6 on a platen 3, wherein the support has a plurality of generally parallel grooves or channels 6a which are open at least at one end. The invention is also directed toward a method of forming an article 1 which comprises the aforementioned method and subsequently building an article on top of said support, removing loose powder 2 from the grooves, through the open ends, and heat treating the article. The support may be made by forming layers of powder using a powder recoater blade 7 which traverses the platen and wherein the grooves are aligned with the direction of travel of the blade. In another aspect, the method of forming a support is characterised in that the grooves are defined between walls which are formed in a criss-cross web.
Description
1 2458745
A METHOD OF FORMING AN ARTICLE
This invention relates to a method of forming an article.
The laser or electron beam sinteringlmelting of powdered materials to form solid parts is now well known-though not so well known as for there to be an established nomenclature. In particular there are commercial powder bed Selective Laser Sintering'/'Selective Laser Melting' (SLS/SLM) machines such as the M270 produced by Electron Optical Systems (EOS) M270 and the Realizer II marketed by MCP. These take metal powders under an inert atmosphere and direct a CO2 or fibre laser onto a layer of powder.
There are also other similar powder bed machines sometimes using an electron beam and somewhat related processes where there is no bed of powder, but the powder is ejected from a nozzle proximate the laser such as in the Trumpf DMD 505. These processes are called such things as Direct Laser Fabrication' or Direct Metal Deposition'.
In the powder bed' processes a point source of energy such as a laser or electron beam is selectively applied to a layer of powder and in related processes a powder/thermal source is directed as required on a layer by layer basis to build up a 3D part from a slicing' of a design file. In both cases the heat from the thermal source melts or sinters the powder layer by layer to form a solid that may be further processed to fully solidify or render useful by various means
not relevant to this disclosure.
In these methods whilst it is possible to build complex parts it is however not possible to commence the building of a part in the bulk of a powder bed or free space-the powder must be melted and fused to a solid structure. And in the case of building a free standing object (as opposed to repairing an existing object by adding material) this commences with a platen upon which powder is melted/sintered and fused.
There are numerous well known reasons why the desired part must start at a solid object and these include: 1. The as-built part contains significant thermally induced stresses capable of bending a 36mm thick 250mm by 250mm tool steel platen-or delaminating the built part away from the platen if the interface is not sufficiently strong.
2. Addressing the point source of heat to a bed of powder causes the powder to locally melt and then ball up into weld spatter' unless it is able to wet and adhere to an existing solid object.
This also means that certain shapes require scaffolding' of supports extending from a solid part to enable wetting and mechanical stability.
Given that the desired part to be built must be attached to a platen then there must also be an intermediate layer which provides a thickness in which a cut can take place to separate the part, once built, from the platen. It is therefore the case that the prior art includes support structures and these have consisted of solid material, hollow shells and a cross hatched structure of discrete walls called EOSTYLE' supports.
After completing the build of a part there may be voids containing unmelted powder contained between the formed shape made of melted powder and the platen. And in the case of non solid supports there will be unmelted powder contained within them. This unmelted powder presents numerous problems to subsequent processing.
Firstly, to remove the stresses inherent in the as-built part a thermal process is needed for all but the smallest parts (such as dental inlays) whilst the part is still firmly attached to the platen. Some desirable thermal processes are sufficiently hot as to melt the loose powder thereby solidifying it in enclosed voids.
Secondly, to cut the part from the platen may require a wire Electrical Discharge Machining (EDM) process, particularly for hard alloys such as cobalt chrome. Loose powder contained within voids shorts out the wire in the EDM process presenting significant difficulties and additional costs for this process.
Thirdly, if cutting with a saw, lubricant may be used and the loose powder then mixes with the lubricant creating difficulties.
Fourthly, the metal powder may be hazardous to health, or valuable (such as in the case of titanium alloys). Hazard control and powder recycling is best performed prior to further processing.
For these and other reasons it is therefore advantageous to have a method of removing powder contained within voids whilst the built part is still attached to the base plate and before heating or cutting operations-and yet the part must be firmly attached to the base plate because of the thermal stresses inherent in the process.
It is not trivial to conceive of support structures that meet the requirement of: 1. Enabling substantially all trapped loose powder to be removed by e.g. gravity, tapping, vacuum or blowing and, 2. Providing a sufficiently firm anchorage during building of the part to the platen to resist delamination and, 3. Not being a solid -(which is time consuming to build and negates much of the benefit of the process-cutting a solid support from a complex solid shape is difficult and costly and negates a benefit of the powder process) and, 4. Is capable of being reliably produced by the laser sintering/melting process.
In particular it should also be understood that the laser sintering/melting process is not capable of making any and all structures and in particular cannot reliably make free standing thin pillars.
From one aspect the invention is an intermediate grooved or channelled solid layer that is built by the laser sintering/melting process between the platen and the desired part built.
This built channelled layer is either an intermediate layer below the prior art supports and/or is at least a part of the support itself including an entirely solid support with channels. If the deposition process is a powder bed process (using a recoater blade) then preferably the grooves/channels are built to lie in the line of traverse of the recoater blade. The grooves/channels are sufficiently wide as to allow loose powder to be removed whilst the built part is still attached to the base plate and before any further processing.
Typically the powder used in a laser sintering/melting process is spherical and of a D50 of 20-1 00 microns and in particular has a mean diameter of about 50 microns. A groove or channel that can be reliably built by the process is of the order of 0.5mm in width.
A preferable grooved structure is of a 0.5mm wall/rib thickness and 0.5mm gap giving a 50% solid upper surface.
Surprisingly a 50/50 0.5mm rib/gap structure is both physically sufficient to build solid parts upon (i.e. the laser sintering/meting process can bridge the gaps) and strong enough to prevent delamination of built parts from the platen either during the build process or during a subsequent heat treatment. Also, the 0.5mm walls of the support are relatively easy to remove from the built parts.
From another aspect the invention consists in a method of forming a support for use in a selective sintering or melting process including forming a body on a platen having a plurality of generally parallel channels each channel being open at at least one end. The base of the channels may be formed by the platen. Preferably the support is formed by a selective sintering or melting process.
According to a further aspect the invention includes a support for use in the selective sintering or melting process including a plurality of spaced generally parallel walls defining grooves or channels therebetween each groove or channel being open at least one end thereof.
From a still further aspect the invention consists in a method of forming an article utilising a selective sintering or melting process including: (a) building by means of a selective sintering or melting process a support defining a plurality of generally parallel channels open at least one end on a platen; (b) building an article on top of the support; (c) removing loose material from the channels through the open ends; and (d) heat treating the article.
The method may further include cutting the support from the platen and subsequently removing the article from the support. The article and support may be formed, in part, contemporaneously.
The support may be made using a method including forming layers of powder using a powder recoater blade which traverses the platen and wherein the channels or grooves are substantially aligned with the direction of travel of the blade.
This alignment in particularly beneficial because it reduces any lateral forces applied to the walls by the blade.
The arrangement described above is suitable for forming many objects, but when the article has a significant length in one dimension it has been found that the internal stress in the support can cause the walls, which define the grooves, to be pulled inwardly.
Thus from another aspect the invention consists in a method of forming a support for use in a selective sintering or melting process including forming, on a platen, a support having a plurality of generally grooves or channels, each groove or channel being open at at least one end.
Preferably by a selective sintering or melting process.
The invention also includes a support for use in a selective sintering or melting process including a plurality of spaced generally parallel walls defining grooves or channels therebetween each groove or channel being open at at least one end thereof. Alternatively the support may be formed in a criss cross web. For example the web may be made up of two sets of parallel walls, the sets being mutually inclined so that they intersect periodically.
The invention also consists in a method of forming an article utilising a selective sintering or melting process including: (a) building by means of a selective sintering or melting process a support defining a plurality of generally parallel grooves or channels open at at least one end of a platen; (b) building an article on top of the support; (c) removing loose material from the channels through the open ends; and (d) heat treating the article.
In this method the support may be as defined above or formed by the method set out above or below in any event the article and the support may be formed in part contemporaneously.
The support may be made using a method including forming layers of powder using a powder re-coater blade which traverses the platen and wherein the channels or grooves are substantially aligned with the direction of travel of the blade.
From a further aspect the invention may include a method of forming a support for use in sintering including forming on a platen a support defining plurality of generally parallel grooves or channels each being open at at least one end wherein the grooves are defined between walls which are progressively formed in a criss cross web.
The web may be made up of two sets of parallel walls, the sets being mutually inclined so that they intersect periodically.
The method may include building a series of aligned blocks of supports with a gap between adjacent ends of the support such that the channels or grooves debouch into the gaps.
The face of at least one support, which defines one wall of the gap may be inclined relative to the length of the groove or channel such that a re-coater blade travelling in the direction of the face with not impinge on the full width of the support simultaneously. The angle of inclination may be about 5°.
Although the invention has been defined 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 specific embodiments will now be described, by way of example, with reference to the accompanying drawings, in which: Figure 1 is a side view of part of selective sinter or melt powder forming apparatus with a formed article shown; Figure 2 is a corresponding article with a different support structure; Figures 3 and 4 are respective plan and side views of prior art support structures; Figure 5 is a schematic view from below of a support structure of the invention with a prior art support structure mounted on top thereof, for example as indicated in Figure 2; Figure 6 which is of a second embodiment of a support.
Figure 7 is a view taken of such a support from one end and shown aligned with further such supports; and Figure 8 is a view of an assembly such as illustrated in Figure 7 looking along the length of the grooves.
Figure 1 is a diagrammatic view at the completion of the build of a solid object 1 formed by the solidification of powder 2 by the application of a point source of heat (not shown) in a layer wise process. The building commences at a platen 3 bolted by bolt 4 to an elevator platform 5 within a powder bed machine. To enable the solid object to be built and allow a cutting gap between the object and the platen a support structure is needed. The support structure of the invention is shown at 6 being a solid support with grooves or channels 6a that contain loose powder 2. The grooves or channels are orientated such that they line along the line of traverse of the powder recoater blade 7. The grooves or channels are open at at least one end so that powder can be removed from them, e.g. by vacuum, prior to heat treatment of the article or object 1.
Figure 2 again shows a support structure of an embodiment of the invention at 6 as a discrete layer below a support structure 8 of the prior art. A plan view of this prior art support 8 is shown at Figure 3 (prior art). Here is shown an "EOSTYLE" support generated by a module within the "Magics" software produced by Materialise, Leuven, Belgium. The software generates a Manhattan' style of support consisting of thin walls 12 and contained voids 10.
Around blocks of walls there can be selectable gaps 11 and the whole is enclosed by a selectable outer wall 9. The distance between the walls 12 is also selectable and is typically 1mm. The purpose of the gaps 11 is to enable the Manhattan' blocks made of thin walls 12 to be easily snapped off the built part I by hand or using hand tools.
The trapping of powder is a known problem and the intended solution within the EOSTYLE support is shown at figure 4 (prior art). This is a view of a wall 9/12 of the EOSTYLE support 8 of the prior art with the platen 3 and the built part 1. holes 13 of a diamond or square shape can be added for the intended purpose of releasing powder. Unfortunately it is impractical to get the powder from an enclosed solid support 8 through these holes and if the hole size is enlarged the support structure does not build reliably.
As shown in figure 5, the structure of support 6 allows powder to drain vertically down the relatively large gaps 10 of the prior art support 8 into the grooves 6a of support 6 where it can readily be removed through the open ends rather than having to attempt to have it pass laterally through multiple walls 12
via holes 13 as in the prior art.
As these walls of support 8 are typically at 1mm spacing (and need to be frequent to act as a sufficient support to resist thermal stresses in part I as it is built and attempts to delaminate from platen 3) then a 100mm wide part will have -100 walls 12 with holes 13 for powder to pass if it is to drain from the prior art support structure 8. In practice the powder is not substantially removed in an economic time scale.
It should also be understood that it is not possible in this software to select solid blocks. Experimentally solid blocks have been created by other means to attempt to form an array of pillars (as they are layer-wise constructed vertically). These pillars do not build successfully In the powder bed equipment, presumably due to the interaction of the recoater blade 7 and powder 2 knocking them over mid build. In a blown powder system thin pillars are impracticable as they would require extremely rapid laser switching and/or powder switching as the laser head scanned across a surface.
Turning to Figures 6 to 8 embodiments are described, which are particularly suitable for use in constructing an article of significant length in one direction.
It should be understood that the most useful supporting structures are not only functional but also quick to form on commercially available equipment. Most laser sintering/melting systems use a galvometer to scan the laser beam, though a Cartesian system of xly motion with a mounted laser or laser projecting device such as a mirror or fibre optic is also used. These systems are all much faster to scan a laser beam along one axis than to draw complex shapes such as crosses, circles etc. that require complex computation and motion along two axis.
Figure 6 shows a variant of the invention being a crisscrossed structure formed by tipping the walls 12 on their side such that they cross vertically.
Figures 7 and 8 shows from 2 directions the same support of Figure 6 of this invention for a generally curved object and illustrates the level of contact and cross linking of this support structure under a curved object 1 to be supported (against mechanical and thermally driven forces) during building and further thermal processing if required.
It has been found when making parts with high internal structures e.g. greater than 50mm that the support walls of the invention are improved by tipping them at an angle to create cross linking e.g. as shown in figure 6. This structure, whilst it can look complex, is still formed by scanning only a single axis.
This crisscrossed support provides both stability during building high structures and also against shrinkage in the cross-wise direction of the attached built part e.g. during thermal processing. This criss-cross supporting of walls does not need to extend throughout the full height of the support to be effective.
Clearly the interIm king of the walls will now block the downward flow of loose powder necessary to allow its removal, and therefore the cross linking is not continuous and indeed all or part of the support structures may be broken into blocks of between 5mm and 100mm, typically 20mm to allow the loose powder to be removed via a gap 15 of 0.3mm and 5mm, typically 1mm.
The interlinking thin walls 12 of structure 14 have a section thickness of between 0.3mm to 5mm, typically 0.5mm. The line' spacing is 1-2 mm, typically 1mm or less and preferably between 0.3mm to 5mm. The angle of the line taken by the interlinking structures is between 5 deg and 35 deg from vertical, typically deg.
The grooves/walls are set at an angle of typically 5 deg to the motion of the re-coater blade 7 to distribute the forces more evenly.
The grooves/walls may extend outside the footprint of the object I and in which case their top leading edge may be rounded off-to help avoid them being chipped off by the re-coater blade 7 and driven into the object I during build.
The thin walls of the invention, whilst drawn as straight lines in the vertical axis may be curved, wavy or angular and the gaps thereby formed may take on any geometric shape, though the structures as shown are preferred and those familiar with the art will understand the limitations the technology places on the forming of various unsupported geometric shapes. In particular, shallow angles (from horizontal) e.g. the tops of circles are not well formed, whereas sharp points as illustrated build well.
Claims (20)
- CLAIMS1. A method of forming a support for use in a selective sintering or melting process including forming on a platen a support having a plurality of generally parallel grooves or channels, each groove or channel being open at at least one end.
- 2. A method as claimed in Claim 1, wherein the support is formed by a selective sintering or melting process.
- 3. A support for use in a selective sintering or melting process including a plurality of spaced generally parallel walls defining grooves or channels therebetween, each groove or channel being open at at least one end thereof.
- 4. A method of forming an article utilising a selective sintering or melting process including: (a) building by means of a selective sintering or melting process a support defining a plurality of generally parallel grooves or channels open at least one end on a platen; (b) building an article on top of the support; (C) removing loose material from the channels through the open ends; and (d) heat treating the article.
- 5. A method as claimed in Claim 4 including cutting the support from the platen and subsequently removing the article from the support.
- 6. A method as claimed in Claim 4 or Claim 5, wherein the article and the support are formed in part contemporaneously.
- 7. A method as claimed in any one of the preceding Claims, wherein the support is made using a method including forming layers of powder using a powder recoater blade which traverses the platen and wherein the channels or grooves are substantially aligned with the direction of travel of the blade.
- 8. A method as claimed in any one of claims 4 to claim 6 wherein the support is formed by the method of any one of claims 1 to 3 or claims 9 to 12.
- 9 A method of forming a support for use in a selective sintering or melting process including forming on a platen a support having a plurality of generally parallel grooves or channels, each groove or channel being open at at leastone end.
- 10. A method as claimed in Claim 9, wherein the support is formed by a selective sintering or melting process.
- 11. A support for use in a selective sintering or melting process including a plurality of spaced generally parallel walls defining grooves or channels therebetween, each groove or channel being open at at least one end thereof.
- 12. A method of forming an article utilising a selective sintering or melting process including: (a) building by means of a selective sintering or melting process a support defining a plurality of generally parallel grooves or channels open at least one end on a platen; (b) building an article on top of the support; (C) removing loose material from the channels through the open ends; and (d) heat treating the article.
- 13. A method as claimed in Claim 12 including cutting the support from the platen and subsequently removing the article from the support.
- 14. A method as claimed in Claim 12 or Claim 13, wherein the article and the support are formed in part contemporaneously.
- 15. A method as claimed in any one of the preceding Claims, wherein the support is made using a method including forming layers of powder using a powder re-coater blade which traverses the platen and wherein the channels or grooves are substantially aligned with the direction of travel of the blade.
- 16. A method as claimed in any one of claims 4 to 6 wherein the support is formed by the method of any one of claims 9 to 11 or claims 17 to 20.
- 17. A method of forming a support for use in sintering including forming on a platen a support defining a plurality of generally parallel grooves or channels each being open at at least on end wherein the grooves are defined between walls which are progressively formed in a criss cross web.
- 18. A method as claimed in claim 17 wherein the web is made up of two sets of parallel walls the sets being mutually inclined so that they intersect periodically.
- 19. A method as claimed in claim 17 or claim 18 wherein a series of aligned blocks of supports are formed with a gap between adjacent ends of the supports such that the channels of grooves debouch into the gaps.
- 20. A method as claimed in claim 19 wherein a face of at least one support which defines one wall of the gap is inclined relative to the length of the groove or channel such that a re-coater blade travelling in the direction of the face will not impinge on the full width of the support simultaneously.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0802601A GB0802601D0 (en) | 2008-02-13 | 2008-02-13 | A method of forming article |
GB0813438A GB0813438D0 (en) | 2008-07-23 | 2008-07-23 | A Method of forming a support |
Publications (3)
Publication Number | Publication Date |
---|---|
GB0901686D0 GB0901686D0 (en) | 2009-03-11 |
GB2458745A true GB2458745A (en) | 2009-10-07 |
GB2458745B GB2458745B (en) | 2013-03-20 |
Family
ID=40469458
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0901686.6A Active GB2458745B (en) | 2008-02-13 | 2009-02-04 | A method of forming an article |
Country Status (1)
Country | Link |
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GB (1) | GB2458745B (en) |
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Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0686480A2 (en) * | 1988-04-18 | 1995-12-13 | 3D Systems, Inc. | Stereolithographic supports |
US5595703A (en) * | 1994-03-10 | 1997-01-21 | Materialise, Naamloze Vennootschap | Method for supporting an object made by means of stereolithography or another rapid prototype production method |
US20030043360A1 (en) * | 2001-08-30 | 2003-03-06 | Farnworth Warren M. | Methods and apparatus for stereolithographic processing of components and assemblies |
US20040031780A1 (en) * | 2002-05-03 | 2004-02-19 | Bego Medical Ag | Method for making products by freeform laser sintering |
EP1486318A2 (en) * | 2003-06-02 | 2004-12-15 | Hewlett-Packard Development Company, L.P. | Methods and system for producing an object through solid freeform fabrication |
US20060208377A1 (en) * | 2005-03-21 | 2006-09-21 | Chen Jack C | Method of making a ceramic composite |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6464636B1 (en) * | 2000-10-18 | 2002-10-15 | Koninklijke Philips Electronics N.V. | Configuration tool for use in ultrasound imaging device |
-
2009
- 2009-02-04 GB GB0901686.6A patent/GB2458745B/en active Active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0686480A2 (en) * | 1988-04-18 | 1995-12-13 | 3D Systems, Inc. | Stereolithographic supports |
US5595703A (en) * | 1994-03-10 | 1997-01-21 | Materialise, Naamloze Vennootschap | Method for supporting an object made by means of stereolithography or another rapid prototype production method |
US20030043360A1 (en) * | 2001-08-30 | 2003-03-06 | Farnworth Warren M. | Methods and apparatus for stereolithographic processing of components and assemblies |
US20040031780A1 (en) * | 2002-05-03 | 2004-02-19 | Bego Medical Ag | Method for making products by freeform laser sintering |
EP1486318A2 (en) * | 2003-06-02 | 2004-12-15 | Hewlett-Packard Development Company, L.P. | Methods and system for producing an object through solid freeform fabrication |
US20060208377A1 (en) * | 2005-03-21 | 2006-09-21 | Chen Jack C | Method of making a ceramic composite |
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