WO2025052064A1 - Improved device for additively manufacturing a part by means of powder bed fusion - Google Patents
Improved device for additively manufacturing a part by means of powder bed fusion Download PDFInfo
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- WO2025052064A1 WO2025052064A1 PCT/FR2024/051129 FR2024051129W WO2025052064A1 WO 2025052064 A1 WO2025052064 A1 WO 2025052064A1 FR 2024051129 W FR2024051129 W FR 2024051129W WO 2025052064 A1 WO2025052064 A1 WO 2025052064A1
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- Prior art keywords
- spreading
- tools
- powder
- tool
- scraper
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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
- B22F10/20—Direct sintering or melting
- B22F10/28—Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM]
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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
- B22F10/30—Process control
- B22F10/32—Process control of the atmosphere, e.g. composition or pressure in a building chamber
- B22F10/322—Process control of the atmosphere, e.g. composition or pressure in a building chamber of the gas flow, e.g. rate or direction
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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
- 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
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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
- 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
- B22F12/70—Gas flow means
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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
- 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
- B22F12/80—Plants, production lines or modules
- B22F12/82—Combination of additive manufacturing apparatus or devices with other processing apparatus or devices
- B22F12/84—Parallel processing within single device
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- 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
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- 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
- B29C64/20—Apparatus for additive manufacturing; Details thereof or accessories therefor
- B29C64/205—Means for applying layers
- B29C64/214—Doctor blades
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- 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
- B29C64/364—Conditioning of environment
- B29C64/371—Conditioning of environment using an environment other than air, e.g. inert gas
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- 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
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- 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
- B33Y30/00—Apparatus for additive manufacturing; Details thereof or accessories therefor
-
- 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
- B33Y50/00—Data acquisition or data processing for additive manufacturing
- B33Y50/02—Data acquisition or data processing for additive manufacturing for controlling or regulating additive manufacturing processes
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- 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
- B29C64/171—Processes of additive manufacturing specially adapted for manufacturing multiple 3D objects
- B29C64/182—Processes of additive manufacturing specially adapted for manufacturing multiple 3D objects in parallel batches
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- 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 disclosure relates to a device for the additive manufacturing of parts, in particular by powder bed fusion, and a method using such a device.
- a classic example of additive manufacturing is the manufacturing by melting or sintering powder particles using a high-energy beam.
- high-energy beams we can notably mention the laser beam and the electron beam.
- SLM selective laser melting
- LBM Laser Beam Melting
- a first layer 100a of powder of a material is deposited, for example using a spreading tool 200 (for example a roller or a scraper), on a construction plate 210 (this may be a plate alone or surmounted by a solid support, a part of another part or a support grid used to facilitate the construction of certain parts).
- a spreading tool 200 for example a roller or a scraper
- a construction plate 210 this may be a plate alone or surmounted by a solid support, a part of another part or a support grid used to facilitate the construction of certain parts.
- This powder is transferred from a feed tray 220 during a forward movement of the roller 200 then it is scraped, and possibly slightly compacted, during one (or more) return movement(s) of the roller 200.
- the powder is composed of metallic particles 110, for example comprising a nickel alloy. Excess powder is recovered in a recycling bin 230 located adjacent to the build bin 240 in which the build plate 210 moves vertically.
- a generator 300 of a laser beam 310 is also used, and a control system 320 capable of directing this beam 310 onto any region of the construction plate 210 so as to scan any region of a previously deposited powder layer.
- the shaping of the laser beam 310 and the variation of its diameter on the focal plane are carried out respectively by means of a beam dilator or focusing system 330 and a “Beam Expander” 340, the assembly constituting the optical system.
- This type of additive manufacturing process can use any high-energy beam instead of the laser beam 310, and in particular an electron beam, as long as this beam is sufficiently energetic to melt the powder particles and a portion of the material on which the particles rest.
- This scanning of the beam is carried out for example by a galvanometric head forming part of a control system 320.
- this control system comprises at least one orientable mirror 350 on which the laser beam 310 is reflected before reaching a layer of powder, each point of the surface of which is always located at the same height relative to the focusing lens, contained in the focusing system 340, the angular position of this mirror being controlled by a galvanometric head so that the laser beam scans at least one region of the first layer of powder, and thus follows a pre-established part profile.
- the galvanometric head is controlled according to the information contained in the database of the computer tool used for the computer-aided design and manufacturing of the part to be manufactured.
- the powder particles 110 of this region of the first layer 100a are melted and form a first element 120a in one piece, integral with the construction plate 210.
- the construction plate 210 is lowered by a height corresponding to the thickness of the first layer of powder 100a (20 to 100 ⁇ m and generally 30 to 50 ⁇ m).
- a second layer 100b of powder is then deposited on the first layer 100a and on this first single-piece or consolidated element 120a, then a region of the second layer 10b which is located partially or completely above this first single-piece or consolidated element 120a in the case illustrated in FIG. 1 is heated by exposure to the laser beam 310, such that the powder particles of this region of the second layer 100b are melted with at least a portion of the element 120a and form a second single-piece or consolidated element 120b, the assembly of these two elements 120a and 120b forming, in the case illustrated in FIG. 1, a single-piece block.
- a protective gas such as argon can be diffused over the layers of powder during melting, by means of a device that is independent and separate from the device described above.
- a protective gas such as argon can be diffused over the layers of powder during melting, by means of a device that is independent and separate from the device described above.
- Such a gas makes it possible to protect the powder against the harmful action of compounds in the ambient air, and in particular to limit the oxidation of the powder, which can be detrimental to the quality of the final part.
- the present disclosure relates to a device for the additive manufacturing of parts by powder bed fusion, comprising a build plate capable of supporting the part during its manufacture, a spreading device capable of spreading the powder, in successive layers, on the build plate, and at least one laser beam or electron generator capable of melting the successive layers of powder in a localized manner, the spreading device comprising a plurality of mobile spreading tools arranged one behind the other in a circular train, each of the spreading tools being capable of spreading the powder and moving jointly with the other spreading tools of the plurality of spreading tools, diffusing a protective gas, and recovering the protective gas diffused by at least one of the other spreading tools of the plurality of spreading tools.
- each spreading tool is arranged one behind the other such that each spreading tool is arranged between two other spreading tools. Furthermore, by “move jointly with the other tools” it is understood that each spreading tool moves at the same time as the other spreading tools of the plurality of spreading tools, that is to say following the same trajectory and preferably going at the same speed. It will be noted, however, that the spreading tools may not go at the same speed, this speed being able to vary.
- each spreading tool moves jointly with the spreading tool preceding it and the spreading tool following it, according to the direction of movement of the spreading tools.
- the spreading device can spread a larger surface area of powder, which is particularly advantageous for large parts.
- the circular train arrangement is also particularly suitable for large annular parts, involving for example an additive manufacturing device and an annular-shaped build plate. It is thus possible to efficiently manufacture such parts continuously.
- the device of the invention makes it possible to improve the yield and productivity during the additive manufacturing of parts by powder bed fusion.
- the spreading device and in particular the spreading tools, perform not only the spreading function, but also the function of managing the protective gases, in particular the diffusion and recovery of these gases.
- This configuration makes it possible to control the protective gas flows more efficiently, which is particularly advantageous in the context of the manufacture of large parts involving large devices as well, and thus further improve the productivity and the quality of the material of the manufactured part.
- each of the spreading tools is capable of moving along a closed-loop trajectory.
- each spreading tool returns to its starting point after completing its trajectory. This allows for spreading of the powder layers by zones, continuously without downtime and without the need for return movements of the spreading tools, thus further improving productivity.
- the shielding gas comprises a neutral gas.
- the neutral gas is argon.
- each spreading tool includes at least one outlet nozzle for diffusing the shielding gas, and at least one inlet nozzle for recovering the shielding gas, the outlet nozzle of each spreading tool being oriented towards the inlet nozzle of the spreading tool arranged downstream, according to a direction of movement of the spreading tools.
- each spreading tool can both inject a shielding gas towards the spreading tool arranged downstream of said spreading tool, and also recover the shielding gas injected by the spreading tool arranged upstream of said spreading tool.
- the presence of an outlet nozzle and an inlet nozzle on each spreading tool, oriented respectively towards the outlet nozzle and the inlet nozzle of the adjacent spreading tool, thus makes it possible to target and locate the diffusion zone of the shielding gas by each spreading tool, thus improving the control of the shielding gas flows.
- each spreading tool is a scraper, a first face of the scraper comprising a plurality of outlet nozzles distributed along said first face, and a second face opposite the first face and comprising a plurality of inlet nozzles distributed along said second face.
- outlet and inlet nozzles are preferably distributed at regular intervals along the first and second faces of the scraper respectively. This arrangement makes it possible on the one hand to improve the efficiency of the diffusion of the protective gases on the powder layers, and on the other hand to facilitate the recovery of the gases diffused by a spreading tool, by the following spreading tool.
- the spreading device comprises N spreading tools, where N>2, the spreading tool N being capable of diffusing a protective gas towards the spreading tool N+1, and of capturing a protective gas diffused by the spreading tool N-1.
- each spreading tool performs the same function, by diffusing the protective gases towards the spreading tool which follows it according to the direction of movement of the spreading tools, and by recovering the protective gases diffused by the spreading tool which precedes it.
- the spreading device comprises between six and twenty spreading tools, preferably twelve spreading tools.
- the part to be manufactured is an annular casing of an aircraft engine, such as an airplane or a helicopter.
- the present disclosure also relates to a method for additive manufacturing of a part by powder bed fusion using a device according to any one of the preceding embodiments, the method comprising the steps of:
- the manufacturing of the part layer by layer on the basis of the digital model comprising the spreading of successive layers of powder by the spreading device on the construction plate, the local melting of said layers of powder by the laser beam or electron generator
- Figure 1 represents an overview of an additive manufacturing device by selective fusion of powder beds according to the prior art
- Figure 2 schematically represents a device for the additive manufacturing of parts by powder bed fusion according to a first embodiment of the invention
- FIG. 3 schematically represents, in a top view, a spreading device of the device of Figure 2,
- FIG. 4 Figure 4 schematically represents a detailed and partial view of the spreading device of Figure 3,
- Figure 2 schematically represents a device 1 for additive manufacturing of parts by powder bed fusion.
- the elements common to the device according to the prior art described previously with reference to Figure 1 are not shown and will not be described again.
- the device 1 comprises a construction plate 10 shown in a top view.
- the construction plate 10 has, in this example, an axisymmetric annular shape around a central axis A, suitable for manufacturing parts such as turbine rings or any annular parts such as annular casings, bearing supports or flanges.
- the construction plate 10 is virtually divided into several sectors 12, in this example twelve sectors 12, corresponding to the sectors in which portions of the part are manufactured, that is to say sectors in which the successive layers of powder are melted.
- the device 1 also comprises a spreading device 20 for spreading the successive layers of powder on the construction plate 10.
- the spreading device 20 comprises a gas diffusion means 21 and a plurality of spreading tools 22 (schematically represented in FIG. 1 by an assembly 22 and described in detail below), the gas diffusion means 21 making it possible to supply the spreading tools 22 with protective gas intended to protect the layers of powder during their melting.
- the device 1 further comprises a laser beam generator 30.
- the laser beam generator 30 is configured so as to generate a plurality of laser beams 31, preferably as many laser beams as there are sectors 12 of the build plate 10, in this example twelve laser beams 31 (only two beams 31 are shown in FIG. 2). It is therefore understood that a laser beam 31 is allocated to each sector 12 and intended to locally melt the successive layers of powder in this sector.
- the laser beams 31 may be electron beams.
- FIG. 3 schematically represents, in detail, the spreading device 20, in a top view.
- the spreading device 20 comprises a plurality of spreading tools 22, in this example twelve.
- the spreading tools 22 are typically longitudinal scrapers of square section. This shape is however not limiting, the scrapers can be longitudinal of rectangular, polygonal or even circular section.
- each scraper 22 is arranged one behind the other in a circle. In other words, each scraper 22 forms a predetermined angle with the adjacent scraper 22, such that the scrapers 22 are distributed at regular intervals around the central axis A.
- each scraper 22 moves together with the scraper 22 which precedes it or which follows it, that is to say preferably at the same speed and following the same trajectory.
- This trajectory is circular, so as to form a closed-loop trajectory.
- a given scraper 22 returns to its initial position after having completed a complete revolution.
- the scrapers 22 may not move at the same speed as each other.
- the speed of movement of each scraper 22 may oscillate, such that two adjacent scrapers 22 may move towards each other temporarily and then move away, and so on.
- each scraper 22 of the spreading device 20 is arranged above the construction plate 10, such that during the additive manufacturing of the part, each scraper 22 is capable of spreading a layer of powder in a given sector 12, then in the following sector 12 after rotation of the spreading device 20, and so on.
- the device 1 may also comprise feed trays (not shown) adjacent to each sector 12, such that each scraper 22 transfers the powder from the feed tray to the sector 12 and then spreads the powder over said sector 12, in the manner described previously with reference to FIG. 1.
- feed trays not shown
- each scraper 22 transfers the powder from the feed tray to the sector 12 and then spreads the powder over said sector 12, in the manner described previously with reference to FIG. 1.
- the laser beam 31 dedicated to said sector 12 carries out a scan in the area of said sector 12, in order to melt in a localized manner the layer of powder which has just been spread by the scraper 22.
- each scraper 22 is capable of diffusing a protective gas, intended to protect the layer of powder during its melting on a given sector 12.
- a protective gas typically comprises argon, and makes it possible to protect the material constituting the powder against oxidation.
- the gas flow lines G are represented by arrows in Figures 3 and 4.
- FIG 4 shows a detailed view of the spreading device 20 of Figure 3, in which only three scrapers 22 are shown.
- Each scraper 22 comprises a plurality of outlet nozzles 24 and inlet nozzles 26.
- the outlet nozzles 24 (in this non-limiting example, six outlet nozzles 24) are distributed longitudinally along a first face 22a of the scraper 22, preferably at regular intervals. Each outlet nozzle 24 makes it possible to deliver a gas flow G in the direction of the following scraper 22, according to the direction of movement of the scrapers 22, the gas flow G diffusing over the powder bed of the corresponding sector 12.
- the inlet nozzles 26 (in this non-limiting example, six inlet nozzles 26) are distributed longitudinally along a second face 22b of the scraper 22, opposite the first face 22a and preferably at regular intervals. Each inlet nozzle 26 makes it possible to capture and recover the gas flow G coming from the previous scraper 22 after its passage over the corresponding sector 12.
- outlet nozzles 24 and the inlet nozzles 26 are shown in relief in Figure 4, this shape is not limiting, the nozzles inlet and outlet which may be simple orifices formed on the faces 22a, 22b of each scraper 22.
- the outlet nozzles 24 of each scraper 22 are oriented towards the inlet nozzles 26 of the following scraper 22, according to the direction of movement of the scrapers 22. Conversely, the inlet nozzles 26 of each scraper 22 are oriented towards the outlet nozzles 24 of the preceding scraper 22, according to the direction of movement of the scrapers 22.
- a scraper 22 (N) diffuses gas flows G towards the following scraper 22 (N+1), the latter recovering said gas flows G coming from the scraper 22 (N).
- the scraper 22N recovers the gas flows G coming from the previous scraper 22 (N-1). It will be noted that in this example comprising twelve scrapers 22, and taking into account the closed-loop arrangement of the scrapers 22, the scraper numbered “12” is arranged between the scraper numbered “11” and the scraper numbered “1”.
- the first faces 22a, and therefore the outlet nozzles 24, are oriented so as to inject the gas flows G in a direction opposite to the direction of rotation of the spreading device 20.
- the first face 22a comprising the outlet nozzles 24 is a downstream face in the direction of movement of the scraper 22, and the second face 22b comprising the inlet nozzles 26 is an upstream face.
- each scraper 22 comprises internal circuits (not shown) for the flow of the protective gas, these internal circuits being supplied by the gas diffusion means 21.
- each scraper 22 may comprise an inlet circuit and a return circuit distinct from each other.
- the gas diffusion means 21 supplies the inlet circuit with protective gas, the latter then being ejected by the outlet nozzles 24.
- the return circuit collects the protective gas recovered by the inlet nozzles 26, the collected gas then being able to be rerouted to the gas diffusion means 21.
- Figures 2 to 4 represent an embodiment in which the scrapers are arranged so as to form a circular train. This arrangement is however not limiting, other types of arrangement of the scrapers 22 can be envisaged without departing from the scope of the invention.
- a method of additive manufacturing of a part by powder bed fusion using a device 1 as described above comprises on the one hand the provision of a digital model of the part to be manufactured, and on the other hand the actual manufacturing of the part layer by layer on the basis of the digital model.
- the digital model may be a digital production file produced using suitable software.
- This file typically comprises a division into slices of given thickness produced by CAD (computer-aided design) of an object.
- the production file also comprises all the necessary instructions, such as the trajectories of the laser beams 31, so that the device 1 can manufacture the object, slice by slice.
- the actual manufacturing of the part comprises the spreading of successive layers of powder by the spreading device 20, and the local and targeted melting of said layers of powder by the laser or electron beam generator 30.
- the laser beams 31 selectively scan certain zones of the powder bed in each sector 12, corresponding to a slice of the part to be manufactured.
- the circular zones F in broken lines in figure 2 represent the local zones covered by each of the laser beams 31.
- each laser beam 31 as well as all the parameters linked to the scanning of the laser, in particular the power of the laser, the scanning speed, the spacing between two passes of the laser, are dictated to the device 1 by the aforementioned production file.
- the actual manufacturing further comprises the diffusion of the protective gas, and the capture of said protective gas, by means of the gas diffusion means 21 and the scrapers 22 of the spreading device 20.
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Abstract
Description
Description Description
Titre de l'invention : dispositif amélioré pour la fabrication additive de pièce par fusion sur lit de poudre Title of the invention: improved device for the additive manufacturing of parts by powder bed fusion
Domaine Technique Technical Field
[0001 ] Le présent exposé concerne un dispositif pour la fabrication additive de pièce, notamment par fusion sur lit de poudre, et un procédé utilisant un tel dispositif. [0001] The present disclosure relates to a device for the additive manufacturing of parts, in particular by powder bed fusion, and a method using such a device.
Technique antérieure Prior art
[0002] Il est désormais connu, dans le domaine aéronautique notamment, d’utiliser des méthodes de fabrication additive pour la réalisation de certains pièces dont la géométrie est fine ou complexe. [0002] It is now known, particularly in the aeronautical field, to use additive manufacturing methods for the production of certain parts with fine or complex geometry.
[0003] Un exemple classique de fabrication additive est la fabrication par fusion ou frittage de particules de poudre au moyen d’un faisceau de haute énergie. Parmi ces faisceaux de haute énergie, on peut mentionner notamment le faisceau laser et le faisceau d’électrons. [0003] A classic example of additive manufacturing is the manufacturing by melting or sintering powder particles using a high-energy beam. Among these high-energy beams, we can notably mention the laser beam and the electron beam.
[0004] Par "fusion sélective par laser", en anglais "Selective Laser Melting" (SLM), également connu sous le nom de procédé « Laser Beam Melting » (LBM), on entend un procédé dont les caractéristiques principales sont rappelées ci- après, en référence à la figure 1 illustrant un dispositif classique de fabrication de pièce par fusion sélective ou frittage sélectif de lits de poudre au moyen d’un faisceau laser. [0004] By "selective laser melting" (SLM), also known as the "Laser Beam Melting" (LBM) process, is meant a process whose main characteristics are recalled below, with reference to Figure 1 illustrating a conventional device for manufacturing parts by selective melting or selective sintering of powder beds using a laser beam.
[0005] On dépose, par exemple à l’aide d’un outil d’étalement 200 (par exemple un rouleau ou un racleur), une première couche 100a de poudre d'un matériau sur un plateau de construction 210 (il peut s’agir d’un plateau seul ou surmonté d’un support massif, d’une partie d’une autre pièce ou d’une grille support utilisée pour faciliter la construction de certaines pièces). [0005] A first layer 100a of powder of a material is deposited, for example using a spreading tool 200 (for example a roller or a scraper), on a construction plate 210 (this may be a plate alone or surmounted by a solid support, a part of another part or a support grid used to facilitate the construction of certain parts).
[0006] Cette poudre est transvasée depuis un bac d’alimentation 220 lors d’un mouvement aller du rouleau 200 puis elle est raclée, et éventuellement légèrement compactée, lors d’un (ou de plusieurs) mouvement(s) de retour du rouleau 200. La poudre est composée de particules 110 métalliques, comprenant par exemple un alliage de nickel. L’excédent de poudre est récupéré dans un bac de recyclage 230 situé de façon adjacente au bac de construction 240 dans lequel se déplace verticalement le plateau de construction 210. [0006] This powder is transferred from a feed tray 220 during a forward movement of the roller 200 then it is scraped, and possibly slightly compacted, during one (or more) return movement(s) of the roller 200. The powder is composed of metallic particles 110, for example comprising a nickel alloy. Excess powder is recovered in a recycling bin 230 located adjacent to the build bin 240 in which the build plate 210 moves vertically.
[0007] On utilise également un générateur 300 de faisceau laser 310, et un système de pilotage 320 apte à diriger ce faisceau 310 sur n'importe quelle région du plateau de construction 210 de façon à balayer n'importe quelle région d'une couche de poudre préalablement déposée. La mise en forme du faisceau laser 310 et la variation de son diamètre sur le plan focal se font respectivement au moyen d’un dilatateur de faisceau ou système de focalisation 330 et d’un « Beam Expander » 340, l’ensemble constituant le système optique. [0007] A generator 300 of a laser beam 310 is also used, and a control system 320 capable of directing this beam 310 onto any region of the construction plate 210 so as to scan any region of a previously deposited powder layer. The shaping of the laser beam 310 and the variation of its diameter on the focal plane are carried out respectively by means of a beam dilator or focusing system 330 and a “Beam Expander” 340, the assembly constituting the optical system.
[0008] Ensuite, on porte une région de cette première couche 100a de poudre, par balayage avec un faisceau laser 310, à une température supérieure à la température de fusion de cette poudre. [0008] Next, a region of this first layer 100a of powder is brought, by scanning with a laser beam 310, to a temperature higher than the melting temperature of this powder.
[0009] Ce type de procédé de fabrication additive peut utiliser n'importe quel faisceau de haute énergie à la place du faisceau laser 310, et notamment un faisceau d’électrons, tant que ce faisceau est suffisamment énergétique pour fondre les particules de poudre et une partie du matériau sur lequel les particules reposent. [0009] This type of additive manufacturing process can use any high-energy beam instead of the laser beam 310, and in particular an electron beam, as long as this beam is sufficiently energetic to melt the powder particles and a portion of the material on which the particles rest.
[0010] Ce balayage du faisceau est effectué par exemple par une tête galvanométrique faisant partie d’un système de pilotage 320. Par exemple ce système de pilotage comprend au moins un miroir 350 orientable sur lequel le faisceau laser 310 se réfléchit avant d'atteindre une couche de poudre dont chaque point de la surface se trouve située toujours à la même hauteur par rapport à la lentille de focalisation, contenue dans le système de focalisation 340, la position angulaire de ce miroir étant pilotée par une tête galvanométrique pour que le faisceau laser balaye au moins une région de la première couche de poudre, et suive ainsi un profil de pièce préétabli. Pour ce faire, la tête galvanométrique est commandée selon les informations contenues dans la base de données de l’outil informatique utilisé pour la conception et la fabrication assistées par ordinateur de la pièce à fabriquer. [0011 ] Ainsi, les particules de poudre 110 de cette région de la première couche 100a sont fondues et forment un premier élément 120a d'un seul tenant, solidaire avec le plateau de construction 210. A ce stade, on peut également balayer avec le faisceau laser plusieurs régions indépendantes de cette première couche pour former, après fusion et solidification de la matière, plusieurs premiers éléments 120a disjoints les uns des autres. [0010] This scanning of the beam is carried out for example by a galvanometric head forming part of a control system 320. For example, this control system comprises at least one orientable mirror 350 on which the laser beam 310 is reflected before reaching a layer of powder, each point of the surface of which is always located at the same height relative to the focusing lens, contained in the focusing system 340, the angular position of this mirror being controlled by a galvanometric head so that the laser beam scans at least one region of the first layer of powder, and thus follows a pre-established part profile. To do this, the galvanometric head is controlled according to the information contained in the database of the computer tool used for the computer-aided design and manufacturing of the part to be manufactured. [0011] Thus, the powder particles 110 of this region of the first layer 100a are melted and form a first element 120a in one piece, integral with the construction plate 210. At this stage, it is also possible to scan with the laser beam several independent regions of this first layer to form, after melting and solidification of the material, several first elements 120a separate from each other.
[0012] On abaisse le plateau de construction 210 d’une hauteur correspondant à l’épaisseur de la première couche de poudre 100a (20 à 100 pm et en général de 30 à 50 |im). [0012] The construction plate 210 is lowered by a height corresponding to the thickness of the first layer of powder 100a (20 to 100 μm and generally 30 to 50 μm).
[0013] On dépose ensuite une deuxième couche 100b de poudre sur la première couche 100a et sur ce premier élément d’un seul tenant ou consolidé 120a, puis on chauffe par exposition au faisceau laser 310 une région de la deuxième couche 10b qui est située partiellement ou complètement au-dessus de ce premier élément d’un seul tenant ou consolidé 120a dans le cas illustré à la figure 1 , de telle sorte que les particules de poudre de cette région de la deuxième couche 100b sont fondues avec au moins une partie de l’élément 120a et forment un deuxième élément d’un seul tenant ou consolidé 120b, l’ensemble de ces deux éléments 120a et 120b formant, dans le cas illustré à la figure 1 , un bloc d'un seul tenant. [0013] A second layer 100b of powder is then deposited on the first layer 100a and on this first single-piece or consolidated element 120a, then a region of the second layer 10b which is located partially or completely above this first single-piece or consolidated element 120a in the case illustrated in FIG. 1 is heated by exposure to the laser beam 310, such that the powder particles of this region of the second layer 100b are melted with at least a portion of the element 120a and form a second single-piece or consolidated element 120b, the assembly of these two elements 120a and 120b forming, in the case illustrated in FIG. 1, a single-piece block.
[0014] Une telle technique de fabrication additive assure donc un excellent contrôle de la géométrie de la pièce à fabriquer et permet de réaliser des pièces possédant une grande complexité. [0014] Such an additive manufacturing technique therefore ensures excellent control of the geometry of the part to be manufactured and makes it possible to produce parts with great complexity.
[0015] Parallèlement à la fabrication couche par couche de la pièce décrite ci- dessus, un gaz de protection tel que de l’argon peut être diffusé sur les couches de poudre lors de la fusion, par l’intermédiaire d’un dispositif autonome et distinct du dispositif décrit ci-dessus. Un tel gaz permet de protéger la poudre contre l’action néfaste des composés de l’air ambiant, et limiter notamment l’oxydation de la poudre, pouvant nuire à la qualité de la pièce finale. [0015] In parallel with the layer-by-layer manufacturing of the part described above, a protective gas such as argon can be diffused over the layers of powder during melting, by means of a device that is independent and separate from the device described above. Such a gas makes it possible to protect the powder against the harmful action of compounds in the ambient air, and in particular to limit the oxidation of the powder, which can be detrimental to the quality of the final part.
[0016] Toutefois, pour la réalisation de pièces de grande taille, impliquant par exemple des surfaces de fusion supérieures à 1500 cm2, le rendement des dispositifs de fabrication additive existant peut être limité. Par ailleurs, le fait d’augmenter la taille du plateau de construction rend plus difficile, en particulier dans le cas des pièces annulaires, la gestion du flux de gaz de protection, ce qui limite d’autant plus la productivité. [0016] However, for the production of large parts, involving for example fusion surfaces greater than 1500 cm 2 , the yield of existing additive manufacturing devices may be limited. Furthermore, the fact Increasing the size of the build plate makes it more difficult, especially in the case of annular parts, to manage the flow of shielding gas, which further limits productivity.
[0017] Il existe donc un réel besoin pour un dispositif permettant de surmonter au moins en partie les inconvénients précités. [0017] There is therefore a real need for a device making it possible to overcome at least in part the aforementioned drawbacks.
Exposé de l'invention Statement of the invention
[0018] Le présent exposé concerne un dispositif pour la fabrication additive de pièce par fusion sur lit de poudre, comprenant un plateau de construction apte à porter la pièce au cours de sa fabrication, un dispositif d’étalement apte à étaler la poudre, par couches successives, sur le plateau de construction, et au moins un générateur de faisceau laser ou d’électrons apte à faire fondre de manière localisée les couches successives de poudre, le dispositif d’étalement comprenant une pluralité d’outils d’étalement mobiles disposés les uns derrières les autres selon un train circulaire, chacun des outils d’étalement étant apte à étaler la poudre et à se déplacer conjointement aux autres outils d’étalement de la pluralité d’outils d’étalement, à diffuser un gaz de protection, et à récupérer le gaz de protection diffusé par au moins un des autres outils d’étalement de la pluralité d’outils d’étalement. [0018] The present disclosure relates to a device for the additive manufacturing of parts by powder bed fusion, comprising a build plate capable of supporting the part during its manufacture, a spreading device capable of spreading the powder, in successive layers, on the build plate, and at least one laser beam or electron generator capable of melting the successive layers of powder in a localized manner, the spreading device comprising a plurality of mobile spreading tools arranged one behind the other in a circular train, each of the spreading tools being capable of spreading the powder and moving jointly with the other spreading tools of the plurality of spreading tools, diffusing a protective gas, and recovering the protective gas diffused by at least one of the other spreading tools of the plurality of spreading tools.
[0019] On comprend que les outils d’étalement sont disposés les uns derrières les autres de telle sorte que chaque outil d’étalement est disposé entre deux autres outils d’étalement. Par ailleurs, par « se déplacer conjointement aux autres outils » on comprend que chaque outil d’étalement se déplace en même temps que les autres outils d’étalement de la pluralité d’outils d’étalement, c’est- à-dire en suivant la même trajectoire et en allant de préférence à la même vitesse. On notera toutefois que les outils d’étalement peuvent ne pas aller à la même vitesse, celle-ci pouvant varier. [0019] It is understood that the spreading tools are arranged one behind the other such that each spreading tool is arranged between two other spreading tools. Furthermore, by “move jointly with the other tools” it is understood that each spreading tool moves at the same time as the other spreading tools of the plurality of spreading tools, that is to say following the same trajectory and preferably going at the same speed. It will be noted, however, that the spreading tools may not go at the same speed, this speed being able to vary.
[0020] Ainsi, au cours du fonctionnement du dispositif d’étalement, chaque outil d’étalement se déplace conjointement à l’outil d’étalement qui le précède et l’outil d’étalement qui lui succède, selon le sens de déplacement des outils d’étalement. [0020] Thus, during operation of the spreading device, each spreading tool moves jointly with the spreading tool preceding it and the spreading tool following it, according to the direction of movement of the spreading tools.
[0021] Compte tenu de cet agencement, il est possible de diminuer l’intervalle de temps entre l’étalement de deux couches successives de poudre sur le plateau de construction. Par ailleurs, sur un intervalle de temps donné, le dispositif d’étalement peut étaler une surface plus importante de poudre, ce qui est particulièrement avantageux pour les pièces de grande taille. L’agencement en train circulaire est en outre particulièrement adapté aux pièces de grande taille annulaire, impliquant par exemple un dispositif de fabrication additive et un plateau de construction de forme annulaire. Il est ainsi possible de fabriquer efficacement, en continu, de telles pièces. En d’autres termes, le dispositif de l’invention permet d’améliorer le rendement et la productivité lors de la fabrication additive de pièces par fusion sur lit de poudre. [0021] Given this arrangement, it is possible to reduce the time interval between the spreading of two successive layers of powder on the plate. construction. Furthermore, over a given time interval, the spreading device can spread a larger surface area of powder, which is particularly advantageous for large parts. The circular train arrangement is also particularly suitable for large annular parts, involving for example an additive manufacturing device and an annular-shaped build plate. It is thus possible to efficiently manufacture such parts continuously. In other words, the device of the invention makes it possible to improve the yield and productivity during the additive manufacturing of parts by powder bed fusion.
[0022] Par ailleurs, le dispositif d’étalement, et en particulier les outils d’étalement, assurent non seulement la fonction d’étalement, mais également la fonction de gestion des gaz de protection, notamment la diffusion et la récupération de ces gaz. Cette configuration permet de maîtriser plus efficacement les flux de gaz de protection, ce qui est particulièrement avantageux dans le cadre de la fabrication de pièces de grande taille impliquant des dispositifs de grande taille également, et ainsi améliorer davantage la productivité et la qualité du matériau de la pièce fabriquée. [0022] Furthermore, the spreading device, and in particular the spreading tools, perform not only the spreading function, but also the function of managing the protective gases, in particular the diffusion and recovery of these gases. This configuration makes it possible to control the protective gas flows more efficiently, which is particularly advantageous in the context of the manufacture of large parts involving large devices as well, and thus further improve the productivity and the quality of the material of the manufactured part.
[0023] Dans certains modes de réalisation, chacun des outils d’étalement est apte à se déplacer selon une trajectoire en boucle fermée. [0023] In some embodiments, each of the spreading tools is capable of moving along a closed-loop trajectory.
[0024] En d’autres termes, chaque outil d’étalement revient à son point départ après avoir terminé sa trajectoire. Cela permet d’effectuer un étalement des couches de poudre par zones, de manière continue sans temps d’arrêt et sans nécessité des mouvements retour des outils d’étalement, améliorant ainsi davantage la productivité. [0024] In other words, each spreading tool returns to its starting point after completing its trajectory. This allows for spreading of the powder layers by zones, continuously without downtime and without the need for return movements of the spreading tools, thus further improving productivity.
[0025] Dans certains modes de réalisation, le gaz de protection comprend un gaz neutre. [0025] In some embodiments, the shielding gas comprises a neutral gas.
[0026] Dans certains modes de réalisation, le gaz neutre est de l’argon. [0026] In some embodiments, the neutral gas is argon.
[0027] Dans certains modes de réalisation, chaque outil d’étalement comprend au moins une buse de sortie pour diffuser le gaz de protection, et au moins une buse d’entrée pour récupérer le gaz de protection, la buse de sortie de chaque outil d’étalement étant orientée vers la buse d’entrée de l’outil d’étalement disposé en aval, selon un sens de déplacement des outils d’étalement. [0027] In some embodiments, each spreading tool includes at least one outlet nozzle for diffusing the shielding gas, and at least one inlet nozzle for recovering the shielding gas, the outlet nozzle of each spreading tool being oriented towards the inlet nozzle of the spreading tool arranged downstream, according to a direction of movement of the spreading tools.
[0028] En d’autres termes, chaque outil d’étalement peut à la fois injecter un gaz de protection vers l’outil d’étalement disposé en aval dudit outil d’étalement, et également récupérer le gaz de protection injecté par l’outil d’étalement disposé en amont dudit outil d’étalement. La présence d’une buse de sortie et d’une buse d’entrée sur chaque outil d’étalement, orientée respectivement vers la buse de sortie et la buse d’entrée de l’outil d’étalement adjacent, permet ainsi de cibler et de localiser la zone de diffusion du gaz de protection par chaque outil d’étalement, améliorant ainsi la maîtrise des flux de gaz de protection. [0028] In other words, each spreading tool can both inject a shielding gas towards the spreading tool arranged downstream of said spreading tool, and also recover the shielding gas injected by the spreading tool arranged upstream of said spreading tool. The presence of an outlet nozzle and an inlet nozzle on each spreading tool, oriented respectively towards the outlet nozzle and the inlet nozzle of the adjacent spreading tool, thus makes it possible to target and locate the diffusion zone of the shielding gas by each spreading tool, thus improving the control of the shielding gas flows.
[0029] Dans certains modes de réalisation, chaque outil d’étalement est un racleur, une première face du racleur comprenant une pluralité de buses de sortie réparties le long de ladite première face, et une deuxième face opposée à la première face et comprenant une pluralité de buses d’entrée réparties le long de ladite deuxième face. [0029] In some embodiments, each spreading tool is a scraper, a first face of the scraper comprising a plurality of outlet nozzles distributed along said first face, and a second face opposite the first face and comprising a plurality of inlet nozzles distributed along said second face.
[0030] Les buses de sortie et d’entrée sont de préférence réparties à intervalles réguliers le long de la première et de la deuxième face du racleur respectivement. Cet agencement permet d’une part d’améliorer l’efficacité de la diffusion des gaz de protection sur les couches de poudre, et d’autre part de faciliter la récupération des gaz diffusés par un outil d’étalement, par l’outil d’étalement suivant. [0030] The outlet and inlet nozzles are preferably distributed at regular intervals along the first and second faces of the scraper respectively. This arrangement makes it possible on the one hand to improve the efficiency of the diffusion of the protective gases on the powder layers, and on the other hand to facilitate the recovery of the gases diffused by a spreading tool, by the following spreading tool.
[0031] Dans certains modes de réalisation, le dispositif d’étalement comprend N outils d’étalement, où N>2, l’outil d’étalement N étant apte à diffuser un gaz de protection vers l’outil d’étalement N+1 , et à capter un gaz de protection diffusé par l’outil d’étalement N-1 . [0031] In certain embodiments, the spreading device comprises N spreading tools, where N>2, the spreading tool N being capable of diffusing a protective gas towards the spreading tool N+1, and of capturing a protective gas diffused by the spreading tool N-1.
[0032] En d’autres termes, chaque l’outil d’étalement rempli la même fonction, en diffusant les gaz de protection vers l’outil d’étalement qui lui succède selon le sens de déplacement des outils d’étalement, et en récupérant les gaz de protection diffusés par l’outil d’étalement qui le précède. [0032] In other words, each spreading tool performs the same function, by diffusing the protective gases towards the spreading tool which follows it according to the direction of movement of the spreading tools, and by recovering the protective gases diffused by the spreading tool which precedes it.
[0033] Dans certains modes de réalisation, le dispositif d’étalement comprend entre six et vingt outils d’étalement, de préférence douze outils d’étalement. [0034] Dans certains modes de réalisation, la pièce à fabriquer est un carter annulaire de moteur d’aéronef, tel qu’un avion ou un hélicoptère. [0033] In some embodiments, the spreading device comprises between six and twenty spreading tools, preferably twelve spreading tools. [0034] In some embodiments, the part to be manufactured is an annular casing of an aircraft engine, such as an airplane or a helicopter.
[0035] Le présent exposé concerne également un procédé de fabrication additive de pièce par fusion sur lit de poudre utilisant un dispositif selon l’un quelconque des modes de réalisation précédents, le procédé comprenant les étapes de : [0035] The present disclosure also relates to a method for additive manufacturing of a part by powder bed fusion using a device according to any one of the preceding embodiments, the method comprising the steps of:
- fourniture d'un modèle numérique de la pièce à fabriquer, - provision of a digital model of the part to be manufactured,
- la fabrication de la pièce couche par couche sur la base du modèle numérique, comprenant l’étalement de couches successives de poudre par le dispositif d’étalement sur le plateau de construction, la fusion locale desdites couches de poudre par le générateur de faisceau laser ou d’électrons - the manufacturing of the part layer by layer on the basis of the digital model, comprising the spreading of successive layers of powder by the spreading device on the construction plate, the local melting of said layers of powder by the laser beam or electron generator
- la diffusion d’un gaz de protection, et la capture dudit gaz de protection, par l’intermédiaire des outils d’étalement du dispositif d’étalement. - the diffusion of a protective gas, and the capture of said protective gas, by means of the spreading tools of the spreading device.
Brève description des dessins Brief description of the drawings
[0036] L'invention et ses avantages seront mieux compris à la lecture de la description détaillée faite ci-après de différents modes de réalisation de l'invention donnés à titre d'exemples non limitatifs. Cette description fait référence aux pages de figures annexées, sur lesquelles : [0036] The invention and its advantages will be better understood upon reading the detailed description given below of different embodiments of the invention given as non-limiting examples. This description refers to the appended pages of figures, in which:
[0037] [Fig. 1] La figure 1 représente une vue d'ensemble d'un dispositif de fabrication additive par fusion sélective de lits de poudre selon l'art antérieur,[0037] [Fig. 1] Figure 1 represents an overview of an additive manufacturing device by selective fusion of powder beds according to the prior art,
[0038] [Fig. 2] La figure 2 représente schématiquement un dispositif pour la fabrication additive de pièce par fusion sur lit de poudre selon un premier mode de réalisation de l’invention, [0038] [Fig. 2] Figure 2 schematically represents a device for the additive manufacturing of parts by powder bed fusion according to a first embodiment of the invention,
[0039] [Fig. 3] La figure 3 représente schématiquement, dans une vue de dessus, un dispositif d’étalement du dispositif de la figure 2, [0039] [Fig. 3] Figure 3 schematically represents, in a top view, a spreading device of the device of Figure 2,
[0040] [Fig. 4] La figure 4 représente schématiquement une vue détaillée et partielle du dispositif d’étalement de la figure 3, [0040] [Fig. 4] Figure 4 schematically represents a detailed and partial view of the spreading device of Figure 3,
Description des modes de réalisation Description of the embodiments
[0041] Un mode de réalisation de l’invention va être décrit dans la suite de la description en référence aux figures 2 à 4. [0042] La figure 2 représente schématiquement un dispositif 1 de fabrication additive de pièce par fusion sur lit de poudre. Les éléments communs au dispositif selon l’art antérieur décrit précédemment en référence à la figure 1 ne sont pas représentés et ne seront pas décrits à nouveau. [0041] An embodiment of the invention will be described in the remainder of the description with reference to Figures 2 to 4. [0042] Figure 2 schematically represents a device 1 for additive manufacturing of parts by powder bed fusion. The elements common to the device according to the prior art described previously with reference to Figure 1 are not shown and will not be described again.
[0043] Le dispositif 1 comprend un plateau de construction 10 représenté dans une vue de dessus. Le plateau de construction 10 présente, dans cet exemple, une forme annulaire axisymétrique autour d’un axe central A, adaptée pour fabriquer des pièces telles que des anneaux de turbine ou toutes pièces annulaires telles que des carters annulaires, des supports de palier ou des flasques. Le plateau de construction 10 est divisé virtuellement en plusieurs secteurs 12, dans cet exemple douze secteurs 12, correspondant aux secteurs dans lequel des portions de la pièce sont fabriquées, c’est-à-dire des secteurs dans lesquels les couches successives de poudre sont fondues. [0043] The device 1 comprises a construction plate 10 shown in a top view. The construction plate 10 has, in this example, an axisymmetric annular shape around a central axis A, suitable for manufacturing parts such as turbine rings or any annular parts such as annular casings, bearing supports or flanges. The construction plate 10 is virtually divided into several sectors 12, in this example twelve sectors 12, corresponding to the sectors in which portions of the part are manufactured, that is to say sectors in which the successive layers of powder are melted.
[0044] Le dispositif 1 comprend également un dispositif d’étalement 20 permettant d’étaler les couches successives de poudre sur le plateau de construction 10. Le dispositif d’étalement 20 comprend un moyen de diffusion de gaz 21 et une pluralité d’outils d’étalement 22 (représentés schématiquement sur la figure 1 par un ensemble 22 et décrits en détails ci-après), le moyen de diffusion de gaz 21 permettant d’alimenter les outils d’étalement 22 en gaz de protection destiné à protéger les couches de poudre pendant leur fusion. [0044] The device 1 also comprises a spreading device 20 for spreading the successive layers of powder on the construction plate 10. The spreading device 20 comprises a gas diffusion means 21 and a plurality of spreading tools 22 (schematically represented in FIG. 1 by an assembly 22 and described in detail below), the gas diffusion means 21 making it possible to supply the spreading tools 22 with protective gas intended to protect the layers of powder during their melting.
[0045] Le dispositif 1 comprend en outre un générateur de faisceau laser 30. Dans ce mode de réalisation, le générateur de faisceau laser 30 est configuré de telle sorte à générer une pluralité de faisceaux laser 31 , de préférence autant de faisceau laser que de secteurs 12 du plateau de construction 10, dans cet exemple douze faisceaux laser 31 (seuls deux faisceaux 31 sont représentés sur la figure 2). On comprend donc qu’un faisceau laser 31 est attribué à chaque secteur 12 et destiné à fondre localement les couches successives de poudre dans ce secteur. De manière alternative, les faisceaux laser 31 peuvent être des faisceaux d’électrons. [0045] The device 1 further comprises a laser beam generator 30. In this embodiment, the laser beam generator 30 is configured so as to generate a plurality of laser beams 31, preferably as many laser beams as there are sectors 12 of the build plate 10, in this example twelve laser beams 31 (only two beams 31 are shown in FIG. 2). It is therefore understood that a laser beam 31 is allocated to each sector 12 and intended to locally melt the successive layers of powder in this sector. Alternatively, the laser beams 31 may be electron beams.
[0046] La figure 3 représente schématiquement, de manière détaillée, le dispositif d’étalement 20, dans une vue de dessus. Le dispositif d’étalement 20 comprend une pluralité d’outils d’étalement 22, dans cet exemple douze. Les outils d’étalement 22 sont typiquement des racleurs longitudinaux de section carrée. Cette forme n’est toutefois pas limitative, les racleurs pouvant être longitudinaux de section rectangulaire, polygonale ou même circulaire. [0046] Figure 3 schematically represents, in detail, the spreading device 20, in a top view. The spreading device 20 comprises a plurality of spreading tools 22, in this example twelve. The spreading tools 22 are typically longitudinal scrapers of square section. This shape is however not limiting, the scrapers can be longitudinal of rectangular, polygonal or even circular section.
[0047] Les racleurs 22 sont agencés les uns derrière les autres en cercle. En d’autres termes, chaque racleur 22 forme un angle prédéterminé avec le racleur 22 adjacent, de telle sorte que les racleurs 22 sont répartis à intervalles réguliers autour de l’axe central A. [0047] The scrapers 22 are arranged one behind the other in a circle. In other words, each scraper 22 forms a predetermined angle with the adjacent scraper 22, such that the scrapers 22 are distributed at regular intervals around the central axis A.
[0048] Les racleurs 22 sont ainsi agencés de manière à former un train circulaire, concentrique avec le plateau de construction 10, et se déplaçant en bloc autour de l’axe central A dans un sens donné, par exemple dans le sens anti horaire représenté par les flèches courbes sur la figure 3. [0048] The scrapers 22 are thus arranged so as to form a circular train, concentric with the construction plate 10, and moving as a unit around the central axis A in a given direction, for example in the counterclockwise direction represented by the curved arrows in FIG. 3.
[0049] Par « se déplaçant en bloc », on comprend que chaque racleur 22 se déplace conjointement au racleur 22 qui le précède ou qu’il succède, c’est-à-dire de préférence à la même vitesse et suivant la même trajectoire. Cette trajectoire est circulaire, de telle sorte à former une trajectoire en boucle fermée. En d’autres termes, un racleur 22 donné revient à sa position initiale après avoir effectué un tour complet. On notera cependant que les racleurs 22 peuvent ne pas se déplacer à la même vitesse les uns des autres. Par exemple, la vitesse de déplacement de chaque racleur 22 peut osciller, de telle sorte que deux racleurs 22 adjacents peuvent se rapprocher l’un de l’autre temporairement puis s’éloigner, et ainsi de suite. [0049] By “moving as a unit”, it is understood that each scraper 22 moves together with the scraper 22 which precedes it or which follows it, that is to say preferably at the same speed and following the same trajectory. This trajectory is circular, so as to form a closed-loop trajectory. In other words, a given scraper 22 returns to its initial position after having completed a complete revolution. It will be noted, however, that the scrapers 22 may not move at the same speed as each other. For example, the speed of movement of each scraper 22 may oscillate, such that two adjacent scrapers 22 may move towards each other temporarily and then move away, and so on.
[0050] Les racleurs 22 du dispositif d’étalement 20 sont disposés au-dessus du plateau de construction 10, de telle sorte qu’au cours de la fabrication additive de la pièce, chaque racleur 22 est apte à étaler une couche de poudre dans un secteur 12 donné, puis dans le secteur 12 suivant après rotation du dispositif d’étalement 20, et ainsi de suite. [0050] The scrapers 22 of the spreading device 20 are arranged above the construction plate 10, such that during the additive manufacturing of the part, each scraper 22 is capable of spreading a layer of powder in a given sector 12, then in the following sector 12 after rotation of the spreading device 20, and so on.
[0051 ] On notera que le dispositif 1 peut également comprendre des bacs d’alimentation (non représentés) adjacents à chaque secteur 12, de telle sorte que chaque racleur 22 transfert la poudre du bac d’alimentation vers le secteur 12 puis étale la poudre sur ledit secteur 12, de la manière décrite précédemment en référence à la figure 1 . [0052] Ainsi, sur un intervalle de temps donné, une couche de poudre peut être étalée conjointement sur tous les secteurs 12 du plateau de construction 10 par l’ensemble des racleurs 22, ce qui permet d’améliorer le rendement et la productivité. [0051] It will be noted that the device 1 may also comprise feed trays (not shown) adjacent to each sector 12, such that each scraper 22 transfers the powder from the feed tray to the sector 12 and then spreads the powder over said sector 12, in the manner described previously with reference to FIG. 1. [0052] Thus, over a given time interval, a layer of powder can be spread jointly over all the sectors 12 of the construction plate 10 by all the scrapers 22, which makes it possible to improve the yield and productivity.
[0053] Par ailleurs, après le passage d’un racleur 22 sur un secteur 12 donné, et avant l’arrivée du racleur 22 suivant, le faisceau laser 31 dédié audit secteur 12 effectue un balayage dans la zone dudit secteur 12, afin de fondre de manière localisée la couche de poudre venant d’être étalée par le racleur 22. [0053] Furthermore, after the passage of a scraper 22 over a given sector 12, and before the arrival of the following scraper 22, the laser beam 31 dedicated to said sector 12 carries out a scan in the area of said sector 12, in order to melt in a localized manner the layer of powder which has just been spread by the scraper 22.
[0054] En outre, au cours de la rotation du dispositif d’étalement 20, chaque racleur 22 est apte à diffuser un gaz de protection, destiné à protéger la couche de poudre au cours de sa fusion sur un secteur 12 donné. Un tel gaz de protection comprend typiquement de l’argon, et permet de protéger le matériau constituant la poudre contre l’oxydation. Les lignes de flux de gaz G sont représentées par des flèches sur les figures 3 et 4. [0054] Furthermore, during the rotation of the spreading device 20, each scraper 22 is capable of diffusing a protective gas, intended to protect the layer of powder during its melting on a given sector 12. Such a protective gas typically comprises argon, and makes it possible to protect the material constituting the powder against oxidation. The gas flow lines G are represented by arrows in Figures 3 and 4.
[0055] La figure 4 représente une vue détaillée du dispositif d’étalement 20 de la figure 3, dans laquelle seuls trois racleurs 22 sont représentés. Chaque racleur 22 comprend une pluralité de buses de sortie 24 et de buses d’entrée 26. [0055] Figure 4 shows a detailed view of the spreading device 20 of Figure 3, in which only three scrapers 22 are shown. Each scraper 22 comprises a plurality of outlet nozzles 24 and inlet nozzles 26.
[0056] Les buses de sortie 24 (dans cet exemple non limitatif, six buses de sortie 24) sont réparties longitudinalement le long d’une première face 22a du racleur 22, de préférence à intervalles réguliers. Chaque buse de sortie 24 permet de délivrer un flux de gaz G dans la direction du racleur 22 suivant, selon le sens de déplacement des racleurs 22, le flux de gaz G se diffusant sur le lit de poudre du secteur 12 correspondant. [0056] The outlet nozzles 24 (in this non-limiting example, six outlet nozzles 24) are distributed longitudinally along a first face 22a of the scraper 22, preferably at regular intervals. Each outlet nozzle 24 makes it possible to deliver a gas flow G in the direction of the following scraper 22, according to the direction of movement of the scrapers 22, the gas flow G diffusing over the powder bed of the corresponding sector 12.
[0057] Les buses d’entrée 26 (dans cet exemple non limitatif, six buses d’entrée 26) sont réparties longitudinalement le long d’une deuxième face 22b du racleur 22, opposée à la première face 22a et de préférence à intervalles réguliers. Chaque buse d’entrée 26 permet de capter et de récupérer le flux de gaz G provenant du racleur 22 précédent après son passage sur le secteur 12 correspondant. [0057] The inlet nozzles 26 (in this non-limiting example, six inlet nozzles 26) are distributed longitudinally along a second face 22b of the scraper 22, opposite the first face 22a and preferably at regular intervals. Each inlet nozzle 26 makes it possible to capture and recover the gas flow G coming from the previous scraper 22 after its passage over the corresponding sector 12.
[0058] Bien que les buses de sortie 24 et les buses d’entrée 26 soient représentées en relief sur la figure 4, cette forme n’est pas limitative, les buses d’entrée et de sortie pouvant être de simples orifices formées sur les faces 22a, 22b de chaque racleur 22. [0058] Although the outlet nozzles 24 and the inlet nozzles 26 are shown in relief in Figure 4, this shape is not limiting, the nozzles inlet and outlet which may be simple orifices formed on the faces 22a, 22b of each scraper 22.
[0059] Compte tenu de cet agencement, les buses de sortie 24 de chaque racleur 22 sont orientées vers les buses d’entrée 26 du racleur 22 suivant, selon le sens de déplacement des racleurs 22. A l’inverse, les buses d’entrée 26 de chaque racleur 22 sont orientées vers les buses de sortie 24 du racleur 22 précédent, selon le sens de déplacement des racleurs 22. [0059] Taking into account this arrangement, the outlet nozzles 24 of each scraper 22 are oriented towards the inlet nozzles 26 of the following scraper 22, according to the direction of movement of the scrapers 22. Conversely, the inlet nozzles 26 of each scraper 22 are oriented towards the outlet nozzles 24 of the preceding scraper 22, according to the direction of movement of the scrapers 22.
[0060] Ainsi, un racleur 22 (N) diffuse des flux de gaz G en direction du racleur 22 (N+1 ) suivant, ce dernier récupérant lesdits flux de gaz G provenant du racleur 22 (N). De même, le racleur 22N récupère les flux de gaz G provenant du racleur 22 (N-1 ) précédent. On notera que dans cet exemple comprenant douze racleurs 22, et compte tenu de l’agencement en boucle fermé des racleurs 22, le racleur numéroté « 12 » est disposé entre le racleur numéroté « 11 » et le racleur numéroté « 1 ». [0060] Thus, a scraper 22 (N) diffuses gas flows G towards the following scraper 22 (N+1), the latter recovering said gas flows G coming from the scraper 22 (N). Similarly, the scraper 22N recovers the gas flows G coming from the previous scraper 22 (N-1). It will be noted that in this example comprising twelve scrapers 22, and taking into account the closed-loop arrangement of the scrapers 22, the scraper numbered “12” is arranged between the scraper numbered “11” and the scraper numbered “1”.
[0061] De préférence, les premières faces 22a, et donc les buses de sortie 24, sont orientées de telle sorte à injecter les flux de gaz G dans un sens opposé au sens de rotation du dispositif d’étalement 20. En d’autres termes, sur chaque racleur 22, la première face 22a comprenant les buses de sortie 24 est une face aval selon le sens de déplacement du racleur 22, et la deuxième face 22b comprenant les buses d’entrée 26 est une face amont. [0061] Preferably, the first faces 22a, and therefore the outlet nozzles 24, are oriented so as to inject the gas flows G in a direction opposite to the direction of rotation of the spreading device 20. In other words, on each scraper 22, the first face 22a comprising the outlet nozzles 24 is a downstream face in the direction of movement of the scraper 22, and the second face 22b comprising the inlet nozzles 26 is an upstream face.
[0062] Ainsi, sur les figure 3 et la figure 4, le dispositif d’étalement 20 tourne dans le sens anti horaire, et les flux de gaz G sont orientés dans le sens horaire (flèches G sur les figures). Chaque racleur 22 laisse ainsi dans son sillage le gaz de protection diffusé par les buses de sortie 24. Cette configuration permet de profiter de l’effet d’inertie des racleurs 22, et d’améliorer l’efficacité de la diffusion du gaz de protection sur les couches de poudre, tout en facilitant la récupération du gaz. On notera toutefois que cet agencement n’est pas limitatif, la position des buses de sortie 24 et des buses d’entrée 26 pouvant être inversée, sans sortir du cadre de l’invention, de telle sorte que les flux de gaz G soient éjectées dans le sens de rotation du dispositif d’étalement 20. [0063] Chaque racleur 22 étant apte à la fois à diffuser et à capter un gaz de protection, il est ainsi possible de diffuser le gaz de protection sur des zones locales et ciblées, correspondant à chaque secteur 12. [0062] Thus, in Figure 3 and Figure 4, the spreading device 20 rotates counterclockwise, and the gas flows G are oriented clockwise (arrows G in the figures). Each scraper 22 thus leaves in its wake the protective gas diffused by the outlet nozzles 24. This configuration makes it possible to take advantage of the inertia effect of the scrapers 22, and to improve the efficiency of the diffusion of the protective gas on the powder layers, while facilitating the recovery of the gas. It will be noted, however, that this arrangement is not limiting, the position of the outlet nozzles 24 and the inlet nozzles 26 being able to be reversed, without departing from the scope of the invention, so that the gas flows G are ejected in the direction of rotation of the spreading device 20. [0063] Each scraper 22 being capable of both diffusing and capturing a protective gas, it is thus possible to diffuse the protective gas over local and targeted areas, corresponding to each sector 12.
[0064] De préférence, chaque racleur 22 comprend des circuits internes (non représentés) d’écoulement du gaz de protection, ces circuits internes étant alimentés par le moyen de diffusion de gaz 21 . En particulier, chaque racleur 22 peut comprendre un circuit d’arrivée et un circuit de retour distinct l’un de l’autre. Le moyen de diffusion de gaz 21 alimente le circuit d’arrivée en gaz de protection, ce dernier étant ensuite éjecté par les buses de sortie 24. Le circuit de retour collecte le gaz de protection récupéré par les buses d’entrée 26, le gaz collecté pouvant ensuite être réacheminé vers le moyen de diffusion de gaz 21 . [0064] Preferably, each scraper 22 comprises internal circuits (not shown) for the flow of the protective gas, these internal circuits being supplied by the gas diffusion means 21. In particular, each scraper 22 may comprise an inlet circuit and a return circuit distinct from each other. The gas diffusion means 21 supplies the inlet circuit with protective gas, the latter then being ejected by the outlet nozzles 24. The return circuit collects the protective gas recovered by the inlet nozzles 26, the collected gas then being able to be rerouted to the gas diffusion means 21.
[0065] Les figures 2 à 4 représentent un mode de réalisation dans lequel les racleurs sont agencés de manière à former un train circulaire. Cet agencement n’est toutefois pas limitatif, d’autres types d’agencement des racleurs 22 pouvant être envisagés sans sortir du cadre de l’invention. [0065] Figures 2 to 4 represent an embodiment in which the scrapers are arranged so as to form a circular train. This arrangement is however not limiting, other types of arrangement of the scrapers 22 can be envisaged without departing from the scope of the invention.
[0066] Un procédé de fabrication additive de pièce par fusion sur lit de poudre utilisant un dispositif 1 tel que décrit ci-dessus comprend d’une part la fourniture d’un modèle numérique de la pièce à fabriquer, et d’autre part la fabrication proprement dite de la pièce couche par couche sur la base du modèle numérique. [0066] A method of additive manufacturing of a part by powder bed fusion using a device 1 as described above comprises on the one hand the provision of a digital model of the part to be manufactured, and on the other hand the actual manufacturing of the part layer by layer on the basis of the digital model.
[0067] Le modèle numérique peut être un fichier numérique de production réalisé grâce à un logiciel adapté. Ce fichier comprend typiquement un découpage en tranches d’épaisseur données réalisé par de la CAO (conception assistée par ordinateur) d’un objet. Le fichier de production comprend en outre l’ensemble des instructions nécessaires, telles que les trajectoires des faisceaux laser 31 , pour que le dispositif 1 puisse fabriquer l’objet, tranche par tranche. [0067] The digital model may be a digital production file produced using suitable software. This file typically comprises a division into slices of given thickness produced by CAD (computer-aided design) of an object. The production file also comprises all the necessary instructions, such as the trajectories of the laser beams 31, so that the device 1 can manufacture the object, slice by slice.
[0068] Par ailleurs, la fabrication proprement dite de la pièce comprend l’étalement de couches successives de poudre par le dispositif d’étalement 20, et la fusion locale et ciblée desdites couches de poudre par le générateur de faisceau laser ou d’électron 30. En particulier, les faisceaux laser 31 balayent sélectivement certaines zones du lit de poudre dans chaque secteur 12, correspondant à une tranche de la pièce à fabriquer. Les zones F circulaires en traits interrompus sur la figure 2 représentent les zones locales couvertes par chacun des faisceaux lasers 31 . [0068] Furthermore, the actual manufacturing of the part comprises the spreading of successive layers of powder by the spreading device 20, and the local and targeted melting of said layers of powder by the laser or electron beam generator 30. In particular, the laser beams 31 selectively scan certain zones of the powder bed in each sector 12, corresponding to a slice of the part to be manufactured. The circular zones F in broken lines in figure 2 represent the local zones covered by each of the laser beams 31.
[0069] Le motif de balayage de chaque faisceau laser 31 , ainsi que tous les paramètres liés au balayage du laser, notamment la puissance du laser, la vitesse de balayage, l’espacement entre deux passages du laser, sont dictés au dispositif 1 par le fichier de production précité. [0069] The scanning pattern of each laser beam 31, as well as all the parameters linked to the scanning of the laser, in particular the power of the laser, the scanning speed, the spacing between two passes of the laser, are dictated to the device 1 by the aforementioned production file.
[0070] La fabrication proprement dite comprend en outre la diffusion du gaz de protection, et la capture dudit gaz de protection, par l’intermédiaire du moyen de diffusion de gaz 21 et des racleurs 22 du dispositif d’étalement 20. [0070] The actual manufacturing further comprises the diffusion of the protective gas, and the capture of said protective gas, by means of the gas diffusion means 21 and the scrapers 22 of the spreading device 20.
[0071 ] Bien que la présente invention ait été décrite en se référant à des exemples de réalisation spécifiques, il est évident que des modifications et des changements peuvent être effectués sur ces exemples sans sortir de la portée générale de l'invention telle que définie par les revendications. En particulier, des caractéristiques individuelles des différents modes de réalisation illustrés/mentionnés peuvent être combinées dans des modes de réalisation additionnels. Par conséquent, la description et les dessins doivent être considérés dans un sens illustratif plutôt que restrictif. [0071] Although the present invention has been described with reference to specific exemplary embodiments, it is obvious that modifications and changes may be made to these examples without departing from the general scope of the invention as defined by the claims. In particular, individual features of the various illustrated/mentioned embodiments may be combined in additional embodiments. Therefore, the description and drawings should be considered in an illustrative rather than restrictive sense.
[0072] Il est également évident que toutes les caractéristiques décrites en référence à un procédé sont transposables, seules ou en combinaison, à un dispositif, et inversement, toutes les caractéristiques décrites en référence à un dispositif sont transposables, seules ou en combinaison, à un procédé. [0072] It is also obvious that all the characteristics described with reference to a method are transposable, alone or in combination, to a device, and conversely, all the characteristics described with reference to a device are transposable, alone or in combination, to a method.
Claims
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FRFR2309433 | 2023-09-07 | ||
| FR2309433A FR3152732A1 (en) | 2023-09-07 | 2023-09-07 | improved device for additive manufacturing of parts by powder bed fusion |
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| WO2025052064A1 true WO2025052064A1 (en) | 2025-03-13 |
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| PCT/FR2024/051129 Pending WO2025052064A1 (en) | 2023-09-07 | 2024-08-28 | Improved device for additively manufacturing a part by means of powder bed fusion |
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| WO (1) | WO2025052064A1 (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108177339A (en) * | 2017-12-27 | 2018-06-19 | 科大天工智能装备技术(天津)有限公司 | A kind of continuously shaped increasing material manufacturing laser formation equipment of multizone |
| CN207874862U (en) * | 2017-12-27 | 2018-09-18 | 科大天工智能装备技术(天津)有限公司 | A kind of continuously shaped increasing material manufacturing laser formation equipment of multizone |
| US20190176233A1 (en) * | 2016-04-13 | 2019-06-13 | 3D New Technologies S.R.L. | Apparatus for additive manufacturing and method of additive manufacturing |
| US20210229361A1 (en) * | 2020-01-28 | 2021-07-29 | Divergent Technologies, Inc. | 3-d printer with gas exchange mechanism for removing contaminants during re-coating |
| FR3111286A1 (en) * | 2020-06-11 | 2021-12-17 | Safran | Additive manufacturing machine with gas flow system |
| CN114682806A (en) * | 2022-03-14 | 2022-07-01 | 江南大学 | Laser powder bed melting forming device based on rotary powder laying mechanism |
-
2023
- 2023-09-07 FR FR2309433A patent/FR3152732A1/en active Pending
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2024
- 2024-08-28 WO PCT/FR2024/051129 patent/WO2025052064A1/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20190176233A1 (en) * | 2016-04-13 | 2019-06-13 | 3D New Technologies S.R.L. | Apparatus for additive manufacturing and method of additive manufacturing |
| CN108177339A (en) * | 2017-12-27 | 2018-06-19 | 科大天工智能装备技术(天津)有限公司 | A kind of continuously shaped increasing material manufacturing laser formation equipment of multizone |
| CN207874862U (en) * | 2017-12-27 | 2018-09-18 | 科大天工智能装备技术(天津)有限公司 | A kind of continuously shaped increasing material manufacturing laser formation equipment of multizone |
| US20210229361A1 (en) * | 2020-01-28 | 2021-07-29 | Divergent Technologies, Inc. | 3-d printer with gas exchange mechanism for removing contaminants during re-coating |
| FR3111286A1 (en) * | 2020-06-11 | 2021-12-17 | Safran | Additive manufacturing machine with gas flow system |
| CN114682806A (en) * | 2022-03-14 | 2022-07-01 | 江南大学 | Laser powder bed melting forming device based on rotary powder laying mechanism |
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