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EP3331687A1 - Procédé et dispositif de fabrication d'un objet tridimensionnel - Google Patents

Procédé et dispositif de fabrication d'un objet tridimensionnel

Info

Publication number
EP3331687A1
EP3331687A1 EP16763444.3A EP16763444A EP3331687A1 EP 3331687 A1 EP3331687 A1 EP 3331687A1 EP 16763444 A EP16763444 A EP 16763444A EP 3331687 A1 EP3331687 A1 EP 3331687A1
Authority
EP
European Patent Office
Prior art keywords
region
envelope
building material
envelope region
dimensional object
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Withdrawn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
EP16763444.3A
Other languages
German (de)
English (en)
Inventor
Thomas Hoferer
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.)
EOS GmbH
Original Assignee
EOS 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 EOS GmbH filed Critical EOS GmbH
Publication of EP3331687A1 publication Critical patent/EP3331687A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • 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
    • B33Y10/00—Processes of 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
    • B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/40—Structures for supporting workpieces or articles during manufacture and removed afterwards
    • B22F10/47—Structures for supporting workpieces or articles during manufacture and removed afterwards characterised by structural features
    • 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
    • B22F10/60—Treatment of workpieces or articles after build-up
    • B22F10/66—Treatment of workpieces or articles after build-up by mechanical means
    • 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
    • B22F10/30—Process control
    • B22F10/36—Process control of energy beam parameters
    • 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
    • B22F10/30—Process control
    • B22F10/36—Process control of energy beam parameters
    • B22F10/366—Scanning parameters, e.g. hatch distance or scanning strategy
    • 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 present invention relates to a method and apparatus for producing a three-dimensional object by selective. Stratified solidification of build material.
  • Methods and devices of this type are used, for example, in rapid prototyping, rapid tooling or additive manufacturing.
  • An example of such a method is known as "selective laser sintering or laser melting".
  • selective laser sintering or laser melting In this case, a thin layer of a build-up material is applied repeatedly and the build-up material in each layer is selectively solidified by selective irradiation with a laser beam.
  • the object is advantageous to produce the object on a building platform to which the building material adheres during solidification.
  • a building platform to which the building material adheres during solidification.
  • Such a method is known from DE 195 11 772 C2. The steep After completion, the three-dimensional object can be separated from the building platform, or the construction platform forms an integral part of the object.
  • the separation of the support structure is carried out in known methods by a suitable tool such as a pair of pliers, saw or file.
  • a suitable tool such as a pair of pliers, saw or file.
  • the object of the present invention is to provide an alternative, preferably improved method for producing a three-dimensional object, as well as a device which is suitable for carrying out the method, wherein in particular the object to be produced is well supported during the production process and the support structure in a simple manner and way of the finished manufactured object can be removed.
  • the method according to the invention for producing a three-dimensional object by layering and selectively strengthening a building material comprises the steps of applying a layer of the building material to a construction field by means of a coater, selectively solidifying the applied layer at locations corresponding to the cross section of the object in the respective layer and repeating the steps of applying and selectively solidifying at the cross section of an envelope region until the object and the envelope region are completed.
  • the build-up material is solidified in such a way that the envelope region encloses the object at least in sections, wherein the points corresponding to the envelope region are less strongly solidified than the points corresponding to the three-dimensional object.
  • an envelope region is solidified around the object, which encloses the object at least in sections and thus supports it. This makes it possible to produce filigree components and objects with internal cavities. Since the envelope region is less strongly solidified than the three-dimensional object, the finished object can be easily separated from the envelope region.
  • the envelope region encloses the three-dimensional
  • the enclosing in at least 2 spatial directions can refer to one or more layers or arbitrarily selected cross sections of the object, preferably on all layers or cross sections.
  • Enclosing in all three directions in space analogously also means a partial three-dimensional encircling of the object, preferably a complete encircling of the object such that all of its outer surfaces directly or indirectly adjoin the enveloping region. This allows uniform support and, if necessary, protection of the object to be manufactured across all areas of construction, thus offering good stability. Furthermore, it is prevented by the envelope region that the object to be produced is deformed by internal stress and thermal effects.
  • the envelope region substantially encloses the object or the part of the object in a form-fitting manner. This provides a good connection of the object to the envelope area and thus good stability of the object.
  • the method according to the invention may further include the following step: removal of the envelope area after completion of the
  • the removal of the cladding region is preferably carried out by blasting, wherein when blasting preferably hard particles, in particular ceramic particles and / or steel balls are used as a radiation medium.
  • blasting preferably hard particles, in particular ceramic particles and / or steel balls are used as a radiation medium.
  • the hardening of the building material takes place by introducing energy by means of radiation, then it is preferable to introduce less energy at the points corresponding to the envelope area than at the object itself. As a result, the envelope area becomes less strong. solidified as the three-dimensional object and thus is easily removable from this.
  • the envelope region is at least partially solidified spaced from the three-dimensional object, wherein the distance between envelope region and object is preferably greater than or equal to 0.06 mm and / or less than 0.10 mm and more preferably constant.
  • the distance between the cladding area and the object prevents the cladding area from sticking to the three-dimensional object, which improves the surface quality of the component.
  • the calculation of the geometry of the envelope region is simplified by choosing a gap of constant size.
  • the building material is a powdery material, more preferably a metal powder. Since the support of the object to be produced is particularly important in the case of metallic building materials, the use of metal powders as a building material can achieve a particularly good effect through the enveloping area.
  • the following steps are performed in advance: calculating the geometry of the three-dimensional object, calculating the geometry of a body that at least partially encloses the object, subtracting the geometry of the object from the geometry of the body, storing the generated geometry as the geometry of the envelope region, and calculating the cross-section of the object and the cross-section of the envelope region in the respective layers.
  • the geometry of the body is chosen such that the body has the smallest possible volume and / or that the body completely encloses the three-dimensional object.
  • a computer program according to the invention is loadable into a programmable control unit and comprises program code means for carrying out all the steps of the method described above when the computer program is executed on the control unit. As a result, it is possible to carry out the learning according to the invention in a simple manner by executing the computer program in a control unit.
  • a control command generating unit for a device for producing a three-dimensional object by layering and selectively solidifying a building material is designed to generate control commands for a device, so that the building material is solidified such that the envelope region encloses the object at least in sections, and the areas corresponding to the envelope area are less strongly solidified than the locations corresponding to the three-dimensional object.
  • the device comprises a coater which can be moved over a building field Applying a layer of the building material to the construction field and solidifying means for selectively solidifying the applied layer at locations corresponding to a cross-section of the object to be manufactured and a cladding area and is adapted and / or controlled to repeat the steps of application and selective solidification until the object and the envelope area are completed. This makes it possible to generate control commands which can be executed in order to carry out the method according to the invention.
  • a control unit for an apparatus for producing a three-dimensional object by layering and selectively strengthening a building material, the apparatus comprising: a field movable coater for applying a layer of building material to the building field and solidifying means for selectively solidifying the applied layers Layer at locations that correspond to a cross-section of the object to be produced and an envelope region.
  • the device is designed and / or controlled to repeat the steps of application and selective solidification until the object and the envelope region are completed.
  • the control unit is designed to control the device such that the build-up material is solidified in such a way that the envelope region encloses the object at least in sections, and the points corresponding to the envelope region are less strongly solidified than the points corresponding to the three-dimensional object. This makes it possible to carry out the method according to the invention by means of the control unit.
  • the device is designed and / or controlled to repeat the steps of application and selective solidification until the ob ect and the cladding region are completed to solidify the build material such that the cladding region encloses the object at least in sections and corresponding to the cladding region To strengthen such sites that the corresponding areas of the envelope are less strongly solidified than the corresponding three-dimensional object bodies. This makes it possible to carry out the method according to the invention by means of the device for producing a three-dimensional object.
  • Fig. 1 is a schematic, partially in section
  • Fig. 2a is a perspective view of a three-dimensional object having an envelope portion (already partially removed); and Fig. 2b is a schematic perspective view of the object shown in Fig. 2a.
  • 3a-3b are schematic, sectional views of embodiments of a three-dimensional object with an envelope region according to a method according to the invention.
  • FIG. 4 is a schematic, sectional view of a three-dimensional object having an envelope region according to a first embodiment of the method according to the invention.
  • FIG. 5 is a schematic, sectional view of a three-dimensional object having an envelope region according to a second embodiment of the method according to the invention.
  • FIGS. 6a-6c are schematic, sectional views of a three-dimensional object having a cladding region, showing the removal of the cladding region according to a method of the invention.
  • FIG. 1 is a laser sintering or laser melting apparatus 1.
  • an upwardly open container 5 is arranged with a wall 6.
  • a movable in a vertical direction V carrier 7 is arranged, on which a base plate 8 is attached, which the container 5 after concludes and thus forms its bottom.
  • the base plate 8 may be a separately formed from the carrier 7 plate which is secured to the carrier 7, or it may be integrally formed with the carrier ⁇ . 7
  • a building platform 9 may still be mounted on the base plate 8, on which the obj ect 2 and the envelope region 30 are constructed.
  • the object 2 and the envelope region 30 can also be built on the base plate 8 itself, which then serves as a construction platform.
  • the object 2 to be formed in the container 5 on the building platform 9 is shown below a working plane 10 in an intermediate state with several solidified layers surrounded by the envelope region 30 and building material 11 that has remained unconsolidated.
  • the laser sintering device 1 further contains a reservoir 12 for a build-up material 13 which can be solidified by electromagnetic radiation and a coater 14 movable in a horizontal direction H for applying the build-up material 13 to the work plane 10.
  • the wall 4 of the process chamber 3 contains a coupling window 15 for the Solidifying the building material 13 serving radiation 22.
  • the laser sintering device 1 also contains an exposure device 20 with a laser 21 which generates a laser beam 22 which is deflected by a deflection device 23 and focused by a focusing device 24 on the working plane 10 via the coupling window 15.
  • the laser sintering apparatus 1 includes a control unit 29, via the 1 ⁇ are controlled in a coordinated way for performing the building process, the individual components of the device.
  • the control unit may contain a CPU whose operation is controlled by a computer program (software).
  • the computer program can be stored separately from the device on a storage medium, from which it can be loaded into the device, in particular into the control unit 29.
  • the control unit 29 can generate control commands for the device 1 and control the device 1 by outputting the control commands to the device 1.
  • the carrier 7 is first lowered by a height which corresponds to the desired layer thickness.
  • a layer of the building material 13 is now applied.
  • the application takes place at least over the entire cross-section of the object 2 to be produced, preferably over the entire construction field, ie the region of the working plane 10 which lies within the upper opening of the container 5.
  • the cross section of the object 2 to be produced is scanned by the laser beam 22, so that the support material 13 is solidified at the points corresponding to the cross section of the object 2 to be produced.
  • FIG. 2 a shows a finished three-dimensional object 2 with an envelope region 30, which has already been partially removed, on a build platform 9 and
  • FIG. 2 b is a schematic view of the object 2 with envelope region 30 shown in FIG. 2 a.
  • the object 2 is present a ring with a radius R, which has filigree structures.
  • the envelope rich 30 is formed as a hollow cylinder with an outer radius ri and an inner radius 2, where: T2 ⁇ R ⁇ ri, so that the ring is completely enclosed by the hollow cylinder.
  • T2 ⁇ R ⁇ ri the filigree structures of the ring are well supported by the cladding region 30 during the manufacturing process.
  • the areas corresponding to the envelope region 30 are less strongly solidified during the manufacturing process than the points corresponding to the object 2. This is achieved by introducing less energy at points corresponding to the envelope region in a layer than at points corresponding to the object.
  • the laser power can be reduced and / or the distance between adjacent laser scanning lines (hatch distance) can be increased and / or the speed with which the laser beam 22 can be moved over the working plane 10 can be increased.
  • exemplary values for the exposure parameters laser power, hatch distance and speed for the solidification of the build-up material 13 are given on the object 2 and the envelope region 30 corresponding points, which cause a less strong solidification of the envelope region 30.
  • the values given in the table are only examples, other values may also be chosen. Also, only one or two of the specified parameters for the consolidation of the building material 13 at the areas corresponding to the envelope area 30 could deviate from those selected for the consolidation of the building material 13 at locations corresponding to the object 2.
  • the geometry of the object 2 to be produced is first calculated and the data thus obtained is stored. Then, the geometry of an artificial body is calculated, which completely encloses the object 2. Subsequently, the geometry of the object 2 is subtracted from the geometry of the body and the body thus obtained is stored as the geometry of the envelope region 30.
  • the cross section of the three-dimensional object 2 and the envelope region 30 in the respective layers are calculated and the data thus obtained is stored.
  • the artificial body which serves to generate the layer information of the enveloping region 30, is calculated in such a way that the body has the smallest possible volume.
  • the smallest possible volume of the body is chosen from the viewpoint that the envelope region 30 must provide a sufficiently large support function for the object 2, which is no longer the case with a body that is too small.
  • FIG. 3a shows a sectional view of an object 2 and an enveloping region 30.
  • the enveloping region 30 is calculated from a body which was not chosen from the viewpoint of the smallest possible volume.
  • FIG. 3 b shows an envelope region 30 which was calculated from a body which has the smallest possible volume.
  • the wall thickness of the envelope region is approximately constant and the envelope region has intermediate spaces 32 which are filled with structural material 11 that has remained unconsolidated.
  • FIG. 4 shows a three-dimensional object 2 with a cavity 2 a which lies inside the object 2.
  • the structure 2b located in the cavity 2a is also supported by the cladding region 30.
  • the three-dimensional object 2 is completely enclosed by the enveloping region 30.
  • “Completely enclosed” is to be understood as meaning that the envelope region 30 surrounds all surfaces (including inner ones) of the object 2.
  • the envelope region 30 can also have gaps 32 which can be filled with composition material 11 that has remained unconsolidated Cavity 2a of the object 2 is not completely filled.
  • the envelope region 30 essentially encloses the object 2 in a form-fitting manner, i. the surface of the envelope region 30 facing the object is formed to be complementary to the surface of the object 2. In this case, a contact between a surface of the object 2 and the envelope region 30 is not absolutely necessary.
  • the envelope region 30 is formed in FIG. 4 on the build platform 9. This ensures a good connection of the object 2 to the building Platform 9 guaranteed.
  • the envelope region 30 may also be formed detached from the build platform 9, or no envelope region 30 may be provided between the object 2 and the build platform 9, so that the object 2 is formed directly on the build platform 9.
  • FIG. 5 shows a sectional view of a three-dimensional object 2, which is completely enclosed by an enveloping region 30.
  • a gap 31 is provided / so that the envelope region 30 is solidified from the object 2 spaced.
  • the width of the gap 31 and thus the distance of the envelope region 30 from the object 2 is preferably approximately constant or greater than or equal to 0.06 mm and less than or equal to 0.10 mm. This prevents build material 13 belonging to the cladding region 30 from adhering to or merging with the surface of the object 2 during the construction process. This eliminates a costly reworking of the surface of the object 2.
  • the gap 31 may be filled with unverloom remained building material 11, whereby a sufficient support effect is ensured.
  • FIG. 6a-6c illustrate the steps of a method according to the invention for removing the envelope region 30 after completion of the object 2.
  • FIG. 6a shows an envelope region 30 which completely surrounds the object 2 so that it is not visible to the viewer.
  • the envelope region 30 is removed from the object by blasting. Since the building material 13 is less strongly solidified in the areas corresponding to the envelope area 30 than in the object 2 corresponding. As a result, it is possible to remove the cladding region 30 by blasting without damaging the object 2.
  • a radiation medium hard particles, such as ceramic particles or Used steel balls. Well suited particles are with a diameter of 0.3-0.6 mm, but other suitable particle sizes are conceivable.
  • the pressure of the particle beam is preferably 4-6 bar, but the method can also be carried out with deviating pressures.
  • Fig. 6b the object 2 and the envelope region 30 are shown in an intermediate state, in which the object 2 is partially enclosed by the envelope region and partially exposed. The left part of the object 2 is already exposed, the right part of the object 2 is still enclosed by the enveloping region 30.
  • 6c shows the object 2 after complete removal of the envelope region 30.
  • the object is completely enclosed by the envelope region, so that the envelope region surrounds all surfaces (including the interior) of the object.
  • the envelope region can also be solidified such that it encloses the object only in sections, so that not all surfaces of the object are surrounded by the envelope region.
  • the gap described with reference to FIG. 5, which is provided between the three-dimensional object and the envelope region, does not necessarily have to be around the entire surface of the object 2 be provided around. Rather, it is also possible to arrange the gap only in one spatial direction, for example in the vertical or horizontal direction, or in two spatial directions around the object. The gap may also be only partially solidified in one or more spatial directions around the object.
  • the envelope area does not necessarily have to be removed from the object by blasting. It is also possible to remove the envelope region by another known method, e.g. manually or mechanically applied force, such as' by hammering, rubbing (files, etc.).
  • the present invention has been described with reference to a laser sintering or laser melting apparatus, it is not limited to laser sintering or laser melting. It can be applied to any methods of manufacturing a three-dimensional object by layering and selectively solidifying a building material.
  • the laser may include, for example, a gas or solid state laser or any other type of laser.
  • any means by which energy can be applied selectively to a layer of building material can be used.
  • a laser for example, another light source, an electron beam or any other energy or radiation source can be used, which is suitable to solidify the building material.
  • the invention can also be applied to selective mask sintering using an extended light source and a mask, or to absorption sintering.
  • the selective solidification of the applied build-up material can also be done by 3D printing, for example by applying an adhesive.
  • the invention relates to the manufacture of an object by means of coating and selective solidification of a building material, regardless of the manner in which the building material is solidified.
  • various materials may be used, especially powdery materials such as metal powder, plastic powder, ceramic powder, sand, filled or mixed powder. Since the support of the object to be produced is particularly important in the case of metallic structural materials, a particularly good effect can be achieved by using metal powders as building material through the enveloping area.

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  • 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

L'invention concerne un procédé de fabrication d'un objet tridimensionnel (2) par dépôt par couches successives et solidification sélective d'un matériau de fabrication (13), comprenant les étapes de : (a) dépôt d'une couche de matériau de fabrication (13) sur une zone de fabrication au moyen d'un appareil de dépôt (14) ; (b) solidification sélective de la couche déposée à des endroits correspondant à la section transversale de l'objet (2) dans la couche respective et à des endroits correspondant à la section transversale d'une zone d'enveloppe (30) ; et (c) répétition des étapes de dépôt et de solidification sélective jusqu'à ce que l'objet (2) et la zone d'enveloppe (30) soient terminés. Le matériau de fabrication (13) est solidifié de telle sorte que la zone d'enveloppe (30) entoure l'objet (2) au moins localement, les endroits correspondants à la zone d'enveloppe (30) étant moins fortement solidifiés que les endroits correspondant à l'objet tridimensionnel (2).
EP16763444.3A 2015-09-11 2016-09-02 Procédé et dispositif de fabrication d'un objet tridimensionnel Withdrawn EP3331687A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102015217469.7A DE102015217469A1 (de) 2015-09-11 2015-09-11 Verfahren und Vorrichtung zum Herstellen eines dreidimensionalen Objekts
PCT/EP2016/001493 WO2017041882A1 (fr) 2015-09-11 2016-09-02 Procédé et dispositif de fabrication d'un objet tridimensionnel

Publications (1)

Publication Number Publication Date
EP3331687A1 true EP3331687A1 (fr) 2018-06-13

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EP16763444.3A Withdrawn EP3331687A1 (fr) 2015-09-11 2016-09-02 Procédé et dispositif de fabrication d'un objet tridimensionnel

Country Status (5)

Country Link
US (1) US20180243828A1 (fr)
EP (1) EP3331687A1 (fr)
CN (1) CN107949470A (fr)
DE (1) DE102015217469A1 (fr)
WO (1) WO2017041882A1 (fr)

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DE102017126624A1 (de) 2017-11-13 2019-05-16 Trumpf Laser- Und Systemtechnik Gmbh Schichtselektive belichtung im überhangbereich bei der generativen fertigung
US11400655B2 (en) 2018-04-30 2022-08-02 Hewlett-Packard Development Company, L.P. Fabrication of objects having different degree of solidification areas
ES2942271T3 (es) * 2018-12-03 2023-05-31 Ivoclar Vivadent Ag Procedimiento para la fabricación aditiva de cuerpos moldeados
US20220111441A1 (en) * 2019-02-14 2022-04-14 Safran Method of additive manufacturing with separation via a frangible zone
EP4049829B1 (fr) * 2021-02-25 2024-08-21 EOS GmbH Electro Optical Systems Structure de support et un objet tridimensionnel et leurs procédés de fabrication
JP7287732B1 (ja) * 2022-10-25 2023-06-06 株式会社松浦機械製作所 三次元成形方法

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US20180243828A1 (en) 2018-08-30
WO2017041882A1 (fr) 2017-03-16
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