EP2318163A2 - Procédé de fabrication en couches de surfaces à forte inclinaison - Google Patents

Procédé de fabrication en couches de surfaces à forte inclinaison

Info

Publication number
EP2318163A2
EP2318163A2 EP09780110A EP09780110A EP2318163A2 EP 2318163 A2 EP2318163 A2 EP 2318163A2 EP 09780110 A EP09780110 A EP 09780110A EP 09780110 A EP09780110 A EP 09780110A EP 2318163 A2 EP2318163 A2 EP 2318163A2
Authority
EP
European Patent Office
Prior art keywords
product
layers
impact
layer
geometric data
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.)
Withdrawn
Application number
EP09780110A
Other languages
German (de)
English (en)
Inventor
Carsten Vagt
Ralf Wehning
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.)
Bego Medical GmbH
Original Assignee
Bego Medical GmbH
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 Bego Medical GmbH filed Critical Bego Medical GmbH
Publication of EP2318163A2 publication Critical patent/EP2318163A2/fr
Withdrawn legal-status Critical Current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
    • 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
    • B29C64/106—Processes of additive manufacturing using only liquids or viscous materials, e.g. depositing a continuous bead of viscous material
    • B29C64/124—Processes of additive manufacturing using only liquids or viscous materials, e.g. depositing a continuous bead of viscous material using layers of liquid which are selectively solidified
    • 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
    • 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
    • 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
    • B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/24—After-treatment of workpieces or articles
    • B22F2003/247—Removing material: carving, cleaning, grinding, hobbing, honing, lapping, polishing, milling, shaving, skiving, turning the surface
    • 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
    • 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
    • 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

Definitions

  • the invention relates to a process for the layered production of a product, comprising the steps of: (a) applying a layer of a curable material, (b) selectively curing predetermined regions of the applied layer based on geometric data of the product, (c) repeating the steps (a ) and (b) until the geometry of the product has been prepared as a cured material, (d) removing the uncured material.
  • the invention relates to a device for producing a product by layered construction, comprising means for applying a layer of a curable material and means for selectively curing predetermined areas of the applied layer based on geometric data of the product.
  • Methods and devices for producing a product by layered construction are described, for example, by DE 299 24 924 U1, EP 1 021 997 B1, DE 102 19 983 B4, DE 103 20 085 A1, EP 1 464 298 B1, WO 2005/080029 A1, EP 1 568 472 B1 and DE 10 2005 050 665 A1.
  • Methods of this type enable efficient production of geometrically complex products.
  • Such processes can be carried out, for example, with a powdery or otherwise pourable material, which can preferably be hardened by a physical bonding process, for example a fusion or sintering, and in this way can produce a loadable, three-dimensional structure.
  • Preferred methods are, for example, selective laser sintering (SLS) or selective laser melting (SLM).
  • the method mentioned at the outset is also used, for example, for highly loaded products with complex geometries, such as those used, for example, as dental prostheses, implants or dental auxiliary parts in dental technology.
  • the method of selective laser melting (SLM) is preferably used for the layered structure.
  • DE 103 20 085 A1 provides a method in which, depending on the sequence of the sintering or melting process, its boundary conditions, namely the energy density of the laser beam and / or its deflection speed and / or the track pitch and / or the strip width ( perpendicular to the track direction) are changed automatically.
  • the energy input at any time automatically adapts to the need for heat of fusion, which can be predetermined to achieve the desired density of the finished product.
  • the laser beam is controlled such that the energy is coupled in several steps in the material or the material to be cured.
  • an energy coupling takes place at a specific position of the material layer until the corresponding region of the material layer has been heated at this position to a temperature just below the melting point.
  • the laser beam then heats this area above the melting temperature, thereby fusing the material with the underlying layer.
  • the solution according to EP 1568472 B1 thus provides that each position is irradiated several times to produce the product. By such alternating irradiation, temperature equalizing operations can be performed after one irradiation process is temporarily stopped and another irradiation process is started. The danger of explosive evaporation of small material particles is considerably reduced by the fact that the beam is directed to a different position after a short time.
  • WO 2005/080029 A1 also pursues the aim of improving the product quality and dimensional stability of the surface, in particular of thin-walled products, by adapting the wall thicknesses in such a way that the desired outer contours of the product can be produced as precisely as possible in the layered structure.
  • WO 2005/080029 A1 discloses a method of the aforementioned type in which a compensation data set and / or a compensation function is determined and linked to the data set of the product target geometry, in order to generate a control data record by means of which a high-energy beam during sintering and / or or melting is performed.
  • the thickness of the product to be produced is reduced in a plane perpendicular to a plane tangent to the outer surface of the product. This is intended to reduce the effect of spherical irregularities observed when a newly applied layer extends into a region below which no portion of the product to be formed is located.
  • the mentioned methods are inadequate and can be further improved with regard to the quality of the products, in particular with regard to defects in the cured material.
  • the surface quality of the products produced in particular in the areas with complex geometries and different surface configurations in successive layers, can be further improved.
  • the complex control of the existing methods can also be further simplified.
  • the invention has for its object to provide a method and an apparatus with which / the quality of manufacture of layered products can be improved in a variety of geometries.
  • the invention is based on the finding that, during curing, for example during laser melting, the area to be cured is heated above the melting point of the material and a temperature compensation takes place via the previously hardened layer underneath, so that, for example, the occurrence of local temperature peaks leading to Evaporation of the material and thus could lead to defects in the product, avoided or reduced.
  • a temperature compensation is not or only possible with difficulty. Especially in these areas, therefore, there are difficulties to achieve optimal temperature control, so there is a risk of malformations in the product to be produced.
  • the solution according to the invention deviates from the desired product contour in a layered manner in a targeted and predetermined manner by providing an SLM in areas in which quality problems, especially with regard to the correct curing of the material or dimensional inaccuracies, can occur Manufacture contour is produced.
  • the SLM manufacturing contour is the sum of the product contour and a predetermined oversize markup.
  • an excess allowance is to be understood as meaning a volume of material which is applied as a production aid to the material volume of the actual product and must be removed again in a subsequent step in order to complete the product.
  • the areas to be cured in the corresponding layers are increased such that a re-hardened layer each extends only by a certain extent beyond the underlying, previously prepared layer addition.
  • the predetermined oversize impact prevents the angle between the axis perpendicular to the layers and the individual surface portions of the SLM manufacturing contours from exceeding a predetermined value such that malformations, such as only partially cured product areas, molten spheres, voids, etc., are caused by the occurrence of localized False temperatures, especially overheating, are avoided.
  • the predetermined value which the angle between the axis perpendicular to the layers and the individual surface portions of the product contours should not exceed is dependent on powder grain size, melting temperature, heat capacity and conductivity, and is of a grain size CoCr powder used for the production of dental parts 25 ⁇ m for example at about 45 °.
  • the oversize impact may be wedge-shaped, for example, in cross-section, since a product section with a sharply inclined surface can be produced towards a less inclined SLM production contour (or vice versa).
  • the angle of the wedge-shaped oversize impact between the product contour and the SLM production contour will be greater, depending stronger the product contour is inclined. This results in a cross-section usually widening shape of the oversize impact, which leads to a wedge shape.
  • the product contours are predominantly not rectilinear but, for example, irregular or arcuate, so that the wedge shape of the cross section of the oversize impact to be predetermined also has correspondingly irregular or arcuate contours.
  • a product portion to be over-inflated according to the invention is preferably a three-dimensional part of the product which comprises a part of the outer surface of the product.
  • a product section may be an arbitrarily shaped contiguous part of the outer surface of the product, a strip of product approximately horizontally oriented or wedge-shaped, or an annular region of the product running at a certain height of the product in the manufacturing state.
  • the excess is produced as overhang angle or minimum wall thickness in the contour outlet.
  • Product sections which are advantageously to be provided with an oversize are, for example, functional surfaces, fitting surfaces or overhangs.
  • a product may have a plurality of product sections, which according to the invention are each provided with an oversize impact, ie a product may have several oversize impacts. If reference is made to an oversized impact in the following, the statements also apply mutatis mutandis to two or more oversize surcharges.
  • the method according to the invention has the advantage that the quality of the product produced, in particular in the areas in which the area size changes greatly over the height of the product, or the contour of product sections is greatly inclined, is considerably improved. By providing an excess impact in these areas, the temperature compensation can be improved, whereby malformations due to insufficient temperature compensation, in particular overheating, can be reduced or avoided.
  • the layered production of the product can be further simplified because the requirements for the control of the temperature and thus the control of, for example, the energy input of a laser beam can be facilitated.
  • the invention is preferably further developed by the step of adjusting the geometric data of the product to selectively cure predetermined areas of the applied layer in accordance with the overcharge to be produced in a step preceding steps (a) to (d).
  • the geometric data of the product to be produced are known in advance.
  • these data are read before the start of the layered preparation, i. before applying the first layer of a curable material, then analyzing whether the product has product portions in which the angle between an axis perpendicular to the layers to be applied and at least a surface portion of a contour of the product exceeds a predetermined value.
  • the geometric data of the SLM production contour such that the angle between rule of the axes perpendicular to the layers and the outer surface in this section does not exceed the predetermined value.
  • the volume to be additionally hardened in the individual layers due to the oversized impact will be greater the more the product contour is inclined.
  • the area around which a layer to be newly hardened is intended to maximally extend beyond a previously produced layer above it is selected such that a sufficient temperature compensation is possible between the layer to be newly hardened and the previously produced layer underneath.
  • different inclinations can be realized. For example, in a CoCr powder of particle size 25 .mu.m used for the production of dental parts, the layer thickness is about 25-50 .mu.m. In product sections which exceed the permissible angle of inclination of the outer surface, a large number of layers are generally to be provided with an oversized impact.
  • the geometric data of the product are adapted such that they are optimized with regard to the layered production, for example with regard to minimum wall thicknesses, contour runouts or overhang angles.
  • the further development according to the invention has the advantage that malformations, such as, for example, only partially cured product areas, the process of layered application, selective curing and removal of the uncured material can be carried out as usual, since the geometry change has already occurred in advance.
  • the invention is further preferably developed by the step of removing the oversize mark, preferably by machining, in a subsequent step (e).
  • the product manufactured in layers with an excess allowance is freed from the oversized impact after the layered structure has been built up. In some applications, it may also be preferable to remove only one or more parts of the oversize impact.
  • the removal of the oversize impact is preferably carried out by machining, for example by milling, since in this case a high dimensional accuracy and surface quality corresponding to the product requirements can be ensured.
  • high-speed cutting which is characterized by high machining performance and surface quality, is preferred.
  • the inventive method preferably combines the advantages of the layered structure with those of the machining and on the one hand ensures that a high quality of the manufactured product can be achieved even in the critical product sections in the layered construction and on the other hand by the machining finishing a high surface area. quality and dimensional accuracy can be achieved.
  • the further development according to the invention thus has the advantage that the high surface quality, contour accuracy and dimensional accuracy made possible by the machining can be achieved even in the product sections which, due to their complex product geometry and / or different surface configurations in successive layers of the product geometry, have a layered structure Such high quality can not or can only be produced with great difficulty.
  • the method according to the invention is advantageously developed by the steps: Generating or providing geometric data of the product for removing the oversize mark, in particular geometric data of at least one surface portion of a desired product contour, in a step preceding the implementation of steps (a) to (d), and
  • these data are generated or provided before the start of the layered production of the product, ie before the application of the first layer to be cured.
  • this is done with or after fitting the geometric data of the product to selectively cure predetermined areas of the applied layer according to the overcharge to be produced according to claim 2.
  • data processing ie, for example, data generation, processing, adaptation, bundled and efficient.
  • the geometric data of the product for removing the oversized impact are transferred to a production facility, which serves to remove the oversized impact, in particular by machining, such as milling.
  • a production device may be, for example, a high-speed milling machine.
  • This transfer has the advantage that the data can be centrally generated, provided or adapted and merely transmitted to the production facility, which removes the oversized markup from the product, without this also having to be transferred. device must still take steps to generate or process data.
  • the product manufactured in layers with an oversized impact is likewise transferred to this production device, so that both the required geometrical data and the product produced in layers with the oversized impact are present to remove the oversize impact at the production facility.
  • the transfer of the product produced in layers with an excess impact occurs with the transfer of the geometric data. It may also be advantageous, depending on the particular applications, to transfer the product before or after the transfer of the geometric data.
  • the geometrical data and / or the product produced in layers with an oversized impact are provided with a referencing aid so that firstly the data can be unambiguously assigned to the product and vice versa, in particular also after the transfer of both the product and the data to the product Manufacturing device for removing the oversized impact, and on the other hand, the position of the product with respect to the manufacturing device is uniquely determined and thus the correct application of the data for removing the excess can be ensured on the product.
  • the referencing aid can be designed, for example, as metadata associated with the geometric data. Another possibility is, for example, to define a product surface as the reference surface or to provide notches or projections on the product.
  • Another aspect of the invention relates to a method of the type mentioned above or according to claim 1, which is characterized in that in one, two or more product sections in steps (a) and (b) an oversized impact is applied, as alignment and / or handling aid is formed.
  • a trained oversized impact can advantageously serve as a reference to uniquely determine the location or orientation of the product. This is particularly advantageous if, after the layered production, the product is subjected to one or more further processing steps, for example to remove excess impacts in other areas. Since the products to be produced in dental technology are usually individual, irregularly shaped individual parts, the determination of the orientation and position of the product for processing steps which follow the layered preparation, such as, for example, a subsequent machining, is of great importance.
  • An inventive overfeed impact which is designed as an alignment and / or handling aid, can advantageously continue to serve to facilitate the transport of the product between several successive processing stations by the alignment and / or handling aid has a gripping portion on which the product is simple and can be safely grasped or taken up. This has the advantage that during transport it is not necessary for the product itself to be touched with its possibly sensitive surfaces, but only for the oversize impact to be removed again later so that damage to the product by handling devices can be avoided.
  • an oversize impact as an alignment and / or handling aid in the layered structure of the product has the advantage that in this way a uniform and / or standardized section can be created, which is easier by uniform and / or standardized alignment and / or handling devices can be used as the individually different products themselves.
  • the oversized impact formed as an alignment and / or handling aid has an individualization aid.
  • Customization assistance can serve to uniquely identify the product, in particular during transport or in further processing steps, if For example, certain data can be assigned to a specific product.
  • the individualization aid can be designed, for example, as a notch or indentation sequence.
  • Another aspect of the invention relates to an apparatus for producing a product by layered construction comprising means for applying a layer of curable material and means for selectively curing predetermined areas of the applied layer based on geometrical data of the product, characterized by
  • Data processing means adapted to adjust the geometric data of the product to selectively cure predetermined regions of the coated layers prior to coating and curing the layers such that a product made from this data
  • the invention further relates to a device arrangement for producing a product by partial layered construction, comprising a device for the layered construction of a first partial volume of the product, comprising means for applying a layer of a curable material and means for selectively curing predetermined regions of the applied layer on the basis of geometric data of the product, characterized by a manufacturing device for removing an excess mark of the product.
  • the device arrangement according to the invention can be further formed according to claim 9.
  • a further aspect of the invention relates to the use of a device for the layered construction of a product for carrying out a method according to one of the preceding claims 1 to 6 or in a device arrangement according to one of the two preceding claims.
  • 1 shows schematically a section of a longitudinal section through a product to be produced in layers
  • 2 shows schematically a section of a longitudinal section of a product to be produced in layers, wherein the representation of the layers is enlarged and made exaggerated for clarification
  • FIG. 3 shows the section shown in FIG. 2 with an oversized impact
  • FIG. 4 shows a product to be produced by layered structure with an oversized impact designed as an alignment and / or handling aid.
  • a product 100 is shown with a product contour 100a, which is to be produced by layered structure.
  • the product 100 has a product portion 110 which is sharply inclined to an axis 150 perpendicular to the layers through which the product is built.
  • a measure of the inclination of the product portion 110 is the angle ⁇ between the vertical axis 150 and a tangent 11 of the contour 100a in the product portion 110.
  • the layered production of the product portion 1 10 is connected to the disadvantages mentioned above.
  • another product portion 120 has a much lower inclination, as indicated by the angle ⁇ between the vertical axis 150 and a tangent 121 of the product portion 120.
  • a product section 120 does not exhibit, or only to a small extent, the problems mentioned in the case of methods which are not according to the invention.
  • an oversize impact 130 is produced, which results in an angle ⁇ between the outer surface 140 and the vertical axis 150 in the section 110 which is smaller than the angle ⁇ and one in the contour to be produced by layered structure does not exceed the predetermined value.
  • This predetermined value is to be chosen so that a sufficient temperature compensation between the to be applied layer and the underlying, already cured layer is made possible, so that no malformations occur in the area to be cured.
  • the oversized impact extends beyond the product section 110.
  • FIG. 2 shows a product 200 to be produced by layered structure, in which likewise a section 210 is inclined to a vertical axis 250 to the layers such that the lateral projection D of the layers over the respectively preceding layer is so large that a temperature compensation in FIG these areas D is no longer adequately guaranteed.
  • the product contour of a product produced by layered construction proceeds in stages, each stage corresponding to a layer of cured material.
  • the illustration in Fig. 2 is not to scale and the steps are heavily coarsened. The contour or outer surface of the product is therefore considered as a smoothed line or surface over the steps.
  • the method according to the invention provides to reduce the regions D in which the layer to be newly cured in each case protrudes laterally beyond the previously cured layer.
  • an oversized impact 230 as shown in Fig. 3, produced.
  • it is first calculated in which areas an oversize impact is required and how the geometric data of the product are to be adapted in order to produce this oversize impact 230.
  • the result of this data adaptation provides that the individual layers are changed in their area, in particular enlarged.
  • These enlargements of the layers are shown in broken lines in FIG. Exemplary of three layers are the areas of the layers to be cured according to the product geometry with 260, which after the adaptation of the geometric data with oversize impact mark additional regions of the layers to be built up in layers with 270.
  • the first seven layers were not adjusted in their geometric data. Beginning with layer 8, the areas to be cured of the layers of curable material were successively enlarged, so that, according to the invention, lateral protrusions of the layers produced by the method according to the invention (for example, denoted by D 1 for three layers) are substantially smaller than the distances D shown in FIG. 2. This ensures that sufficient temperature compensation is ensured between the layer to be cured and the layer below it is.
  • the intermediate product thus produced is transferred to a production facility for removing the oversize impact, preferably by machining in a high-speed milling machine.
  • Data are also passed to the manufacturing facility which, together with the adaptation of the geometrical data, has been prepared prior to the layered production of the intermediate product defining the oversize to be removed so that by removing the oversize, a product having the desired product contours can be made.
  • FIG. 4 shows an intermediate product 300 to be produced by layer-by-layer construction with an oversized impact 390, which is designed as an alignment and / or handling aid.
  • the interference overrun 390 is generated by adjusting the geometrical data to selectively cure predetermined regions of the deposited layer prior to performing the layered construction.
  • the alignment and / or handling aid can serve to transport the intermediate product without damaging the relevant outer contours, and furthermore to unambiguously determine the position or orientation of the intermediate product in post-processing steps.
  • the oversize 390 of the intermediate product 300 is preferably removed again by machining, with corresponding data for removing the oversize 390 preferably already before the start of the application of the first layer a curable material have been created and before, with or after transfer of the intermediate product 300 to a manufacturing device for machining are also transferred to this.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)

Abstract

L'invention concerne un procédé de fabrication en couches d'un produit, ce procédé comprenant les étapes suivantes : (a) application d'une couche de matière durcissable, (b) durcissement sélectif de régions prédéfinies de la couche appliquée, à l'aide de données géométriques du produit, (c) répétition des étapes (a) et (b) jusqu'à obtention de la géométrie du produit en tant que matière durcie, (d) élimination de la matière non durcie. Selon l'invention, dans une, deux ou plusieurs sections du produit dans lesquelles un angle formé entre un axe perpendiculaire aux couches et au moins une section superficielle d'un contour du produit est supérieur à une valeur prédéfinie, une surépaisseur, par exemple cunéiforme en coupe transversale, est appliquée sur ladite section superficielle au cours des étapes (a) et (b) de telle sorte que l'angle entre l'axe perpendiculaire aux couches et la surface extérieure dans ladite section du produit ne dépasse pas la valeur prédéfinie.
EP09780110A 2008-07-08 2009-07-02 Procédé de fabrication en couches de surfaces à forte inclinaison Withdrawn EP2318163A2 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102008031926A DE102008031926A1 (de) 2008-07-08 2008-07-08 Verfahren zum schichtweisen Herstellen stark geneigter Flächen
PCT/EP2009/058370 WO2010003883A2 (fr) 2008-07-08 2009-07-02 Procédé de fabrication en couches de surfaces à forte inclinaison

Publications (1)

Publication Number Publication Date
EP2318163A2 true EP2318163A2 (fr) 2011-05-11

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
EP09780110A Withdrawn EP2318163A2 (fr) 2008-07-08 2009-07-02 Procédé de fabrication en couches de surfaces à forte inclinaison

Country Status (4)

Country Link
US (1) US8926879B2 (fr)
EP (1) EP2318163A2 (fr)
DE (1) DE102008031926A1 (fr)
WO (1) WO2010003883A2 (fr)

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EP2849672B1 (fr) 2012-05-10 2019-10-16 Renishaw Plc. Procédé de fabrication d'un article
GB201303428D0 (en) 2013-02-27 2013-04-10 Rolls Royce Plc A vane structure and a method of manufacturing a vane structure
DE102013203936A1 (de) * 2013-03-07 2014-09-11 Airbus Operations Gmbh Generatives Schichtaufbauverfahren zur Herstellung eines dreidimensionalen Objekts und dreidimensionales Objekt
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US20110180971A1 (en) 2011-07-28
US8926879B2 (en) 2015-01-06
WO2010003883A3 (fr) 2010-04-29
DE102008031926A1 (de) 2010-01-14

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