EP3740381A1 - Dispositif de chauffage d'un matériau de composant, installation de fabrication additive et procédé de fabrication additive - Google Patents

Dispositif de chauffage d'un matériau de composant, installation de fabrication additive et procédé de fabrication additive

Info

Publication number
EP3740381A1
EP3740381A1 EP19726914.5A EP19726914A EP3740381A1 EP 3740381 A1 EP3740381 A1 EP 3740381A1 EP 19726914 A EP19726914 A EP 19726914A EP 3740381 A1 EP3740381 A1 EP 3740381A1
Authority
EP
European Patent Office
Prior art keywords
component
platform
component material
additive
heating
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Withdrawn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
EP19726914.5A
Other languages
German (de)
English (en)
Inventor
Michael Ott
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.)
Siemens Energy Global GmbH and Co KG
Original Assignee
Siemens AG
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 Siemens AG filed Critical Siemens AG
Publication of EP3740381A1 publication Critical patent/EP3740381A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • 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
    • B22F1/00—Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
    • B22F1/14—Treatment of metallic powder
    • B22F1/142—Thermal or thermo-mechanical treatment
    • 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
    • B22F10/30—Process control
    • B22F10/36—Process control of energy beam parameters
    • B22F10/362—Process control of energy beam parameters for preheating
    • 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
    • B22F12/10—Auxiliary heating means
    • B22F12/13—Auxiliary heating means to preheat the material
    • 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
    • B22F12/22—Driving 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
    • 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
    • B29C64/227—Driving 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
    • B29C64/20—Apparatus for additive manufacturing; Details thereof or accessories therefor
    • B29C64/245—Platforms or substrates
    • 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
    • B29C64/295—Heating elements
    • 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
    • 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
    • B33Y40/00—Auxiliary operations or equipment, e.g. for material handling
    • B33Y40/10—Pre-treatment
    • 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
    • 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
    • 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
    • B22F12/90—Means for process control, e.g. cameras or sensors
    • 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
    • B22F2999/00—Aspects linked to processes or compositions used in powder metallurgy
    • 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
    • B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
    • B22F5/009—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine components other than turbine blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
    • B22F5/04—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine blades
    • 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 device for, in particular selective, heating or preheating a component material in the additive production.
  • the component material is preferably a powder material for the powder-bed-based additive manufacturing of the component.
  • an aditive manufacturing plant comprising the device and a method for additive production of the component, angege ben.
  • the component is preferably intended for use in a Strö tion machine, preferably in the hot gas path of a gas turbine.
  • the component preferably consists of a nickel- or cobalt-based superalloy.
  • the alloy may be precipitation hardened or precipitation hardenable.
  • Modern gas turbines are the subject of continuous improvement to increase their efficiency. However, this leads, inter alia, to ever higher temperatures in the hot gas path.
  • the metallic materials for blades, particularly in the first stages, have recently been improved in terms of their strength, creep properties and resistance to thermo-mechanical fatigue.
  • Additive manufacturing methods include, for example, as powder bed processes, selective laser melting (SLM) or laser sintering (SLS), or electron beam melting (EBM).
  • SLM selective laser melting
  • SLS laser sintering
  • EBM electron beam melting
  • Additive manufacturing processes (English: "additive manufacturing”) have also proven to be particularly advantageous for complex or filigree-designed components, for example la rinthearth-like structures, cooling and / or lightweight structures,
  • additive manufacturing is provided by a particularly short chain Of process steps advantageous because a manufacturing or manufacturing step of a component can be done almost exclusively on the basis of a corresponding CAD file and the choice of appropriate manufacturing parameters.
  • a device which allows a simple and intelligent way a selective or local in ductile heating of the component material.
  • the solution also includes the operation of said device, for example, implemented in an additive Heinrichsan location.
  • One aspect of the present invention relates to a Vorrich device for, in particular selective, heating or preheating a component material for the additive, in particular powder bed-based, production of the component.
  • the device includes a platform with a, in particular inductive, He warming head. By this means, a high preheating temperature can be achieved particularly expediently.
  • the device further comprises a suspension, which supports or holds the platform and which is designed to move the platform, for example controlled or controlled, ent long three vertical spatial directions within a construction space of an additive manufacturing plant.
  • a suspension which supports or holds the platform and which is designed to move the platform, for example controlled or controlled, ent long three vertical spatial directions within a construction space of an additive manufacturing plant.
  • the embodiment of the suspension also makes possible a targeted or controlled movement of the platform along the vertical spatial Z-axis within the mounting space.
  • the advantages of the proposed solution relate, for example, to the possibility of local and intensive preheating at the place of processing. Accordingly, said location of the processing can be a (mobile) caused by the energy beam molten bath in the Bauteilmate material.
  • Another advantage relates to the simple possibility of flexible three-dimensional positioning of the platform, preferably at any location within a space and on the build platform.
  • reaction atmosphere can be created at the site of processing or selective solidification of the component material via the device or the platform (in situ), which has an advantageous effect on the structural properties or mechanical properties of the component to be produced (see below).
  • the heating head comprises a, in particular water-cooled, induction coil, which in particular via a high-frequency generator, such as the device, operated and / or regulated and is formed from, the component material locally to a temperature between 800 ° C and 1200 ° C, in particular of 1000 ° C or more, to heat or pre-heat for the actual additive build-up process, ie to bring to a suitable preheating tempera ture.
  • a high-frequency generator such as the device, operated and / or regulated and is formed from, the component material locally to a temperature between 800 ° C and 1200 ° C, in particular of 1000 ° C or more, to heat or pre-heat for the actual additive build-up process, ie to bring to a suitable preheating tempera ture.
  • the suspension comprises four Aktua factors, which are individually controlled and evenly, example, in a square arrangement, are mounted in the body space.
  • the actuators are preferably each made flexible in order to allow mobility of the platform along the three mutually perpendicular spatial directions.
  • the actuators are each made flexible.
  • the actuators are each controlled via a gear, a cable, a telescopic arm, pneumatic and / or hydraulic means.
  • the actuators can preferably be made particularly flexible.
  • the device comprises a tempera ture meter, such as an infrared camera or a py rometer, which is arranged and formed - example, viewed in supervision on a construction area - the tempera ture of the component material and on the construction area to mes sen and / or to regulate or to control.
  • a tempera ture meter such as an infrared camera or a py rometer
  • the device comprises a protective gas guide which is coupled to the platform and designed to guide a protective gas, for example an inert gas, laminar or parallel over and / or perpendicular to the component material during the additive production of the component.
  • a protective gas for example an inert gas, laminar or parallel over and / or perpendicular to the component material during the additive production of the component.
  • the vertical guidance of the protective gas onto the component material can be implemented, for example, by means of a showerhead-like arrangement of the protective gas guide or a corresponding gas outlet.
  • the manufacturing plant preferably further comprises a coating device and a device for irradiation, as in known additive manufacturing systems.
  • the device is in the system, example, as viewed along the construction direction of the corresponding component, arranged above a mounting surface.
  • Another aspect of the present invention relates to a method for preheating and / or additive preparation, preferably before a powder bed method, a component comprising the orders of a layer of a component material on a mounting surface with the coating device.
  • the method further comprises lowering or approaching a platform in the direction of a region of the construction surface to be irradiated.
  • the method further comprises heating the region to be irradiated by means of the heating head of the device.
  • the method further comprises irradiating the area with an energy beam for selective solidification of the construction part material according to a predetermined geometry of the construction part.
  • the method comprises - after irradiation of the area - lifting or lifting the building panel form out of an area of action of the irradiation device and then repeating the described steps of applying, lowering, heating
  • the steps of the described heating and irradiation are performed at least partially simultaneously.
  • the irradiation of the area is performed syn chronously, preferably time and / or location, with the heating men, wherein the energy beam during the additi tional structure of the component, for example, by an eye of an induction coil of the device or the heating head ge leads ,
  • the component material is heated locally to a temperature of more than 800 ° C., preferably 1000 ° C. or more, particularly preferably 1200 ° C. or more.
  • the component material is locally heated to ei ne temperature between 800 ° C and 1200 ° C, in particular 1000 ° C or more.
  • the component material is a g
  • the component has a component turned or provided in the hot gas path of a gas turbine.
  • the component material before the egg tual additive structure for example by selective laser melting, only preheated.
  • Embodiments, features and / or advantages, which relate vorlie on the device or the additive manufacturing plant, may also relate to the process for additive manufel ment or vice versa.
  • FIG. 1 indicates a powder-bed-based additive manufacturing process of a component on the basis of a schematic sectional view.
  • Figure 2 shows a simplified and schematic perspekti vische view of a device according to the invention.
  • FIG. 3 indicates method steps according to the invention on the basis of a schematic flow diagram.
  • the same or equivalent elements may each be provided with the same padszei chen.
  • the elements shown and their size ratios with each other are basically not to be considered as true to scale, but individual elements, for better presentation and / or better understanding of understanding can be shown exaggerated thick or large.
  • FIG. 1 shows an additive manufacturing plant 100.
  • the plant 100 is preferably a device for the additive manufacture of a component (cf. reference numeral 10) from a powder bed, for example by selective laser melting. zen or electron beam melting.
  • the system 100 has a substrate plate 11. On the substrate plate or the sub strate 11 is in the course of its additive production, a construction part 10 constructed, ie preferably also directly stoffschlüs sig connected or "welded".
  • the component is preferably a component which is used in the hot gas path of a turbomachine, for example a gas turbine.
  • the component may designate a rotor or vane segment, a segment or ring segment, a burner part or a burner tip, a frame, a shield, a nozzle, a gasket, a filter, a Mün or lance, a resonator, stamp or a swirler , or a corresponding transition, use, or a corresponding retrofit part.
  • the component 10 is preferably constructed in a construction space AR of the system 100.
  • the component 10 is shown in Figure 1, preferably only partially built on, for example, only two Schich th S of a component material P.
  • the component material P may be a powder of a g- and / or g'-hardened, nickel- or cobalt-based superalloy.
  • Individual layers of the material P for the layers S of the component are preferably applied over a Be Anlagenungsvorrich device 30 and then selectively melted by means of an energy beam 21 for the construction of the component 10 and solidified.
  • the energy beam is preferably emitted by an irradiation device 20, for example as a display or comprising an electron beam or a laser source.
  • the substrate plate 11 will preferably correspond to one of the layer thickness S - lowered the measure. Subsequently, a new powder layer for the construction of the component 10 is applied, for example, starting from a powder supply, which te on the left Be in Figure 1 is shown.
  • the additive buildup process is preferably carried out under an inert or inert gas atmosphere or at least in a reduced oxygen content atmosphere in order to influence corrosion, oxidation or other influences which affect the quality of the component material, ie the powder P, or the finally produced component 10 , to avoid.
  • a corresponding inert gas or inert gas guidance is not explicitly indicated in FIG. 1; However, it may be provided and designed to guide an inert gas, for example laminar, over a mounting surface AF.
  • FIG. 1 shows a camera, for example an infrared camera 50, which is preferably arranged and designed to measure and / or regulate the temperature of the component material P on the mounting surface AF.
  • a camera for example an infrared camera 50, which is preferably arranged and designed to measure and / or regulate the temperature of the component material P on the mounting surface AF.
  • FIG. 1 is already a Platt form 200 according to the invention, for example, a device 300 (see Figure 2 below), shown, via which a targeted or se lective heating of the component material P can be done.
  • the platform 200 can be stored and / or moved via a suspension 201 (also shown in FIG. 2 below).
  • a construction direction (not explicitly marked) for the component 10 corresponds in FIG. 1 to a direction pointing vertically upwards.
  • Figure 2 shows details of a device 300 and a sectionan view of the system 100, which contains the device 300 and in which the device 300 is installed, for example, as a retrofit kit.
  • the device 300 is arranged above the mounting surface AF.
  • the device 300 is preferably provided for selective heating or preheating of the component material P for the additive, in particular powder bed-based, production of a component 10.
  • the device 300 comprises a platform 200 with a, in particular in ductile, heating head L, and a suspension 201, which supports the platform 200 and which is formed
  • the device 300 in addition to a lateral movement in the X- or Y-direction, the device 300 according to the invention also enables a vertical movement of the platform 200 along the Z-axis.
  • the platform 200 may be configured, for example, annular, so that, for example, during the additive manufacture ment of the component 10, the energy beam 21 can be passed through them.
  • the heating head L includes, for example, an induction coil, such as a high frequency coil, which in particular via a high frequency generator, operated and / or regulated who can, and is designed, the component material P locally to a temperature of about 800 ° C, preferably 1000 ° C, particularly preferably to heat 1200 ° C or more, example, before the actual additive structure (before) to warm.
  • an induction coil such as a high frequency coil, which in particular via a high frequency generator, operated and / or regulated who can, and is designed, the component material P locally to a temperature of about 800 ° C, preferably 1000 ° C, particularly preferably to heat 1200 ° C or more, example, before the actual additive structure (before) to warm.
  • the component material is locally heated to ei ne temperature in a range between 800 ° C and 1200 ° C, in particular 1000 ° C or more.
  • the frequency at which the described coil or the ent speaking generator can be operated can be up to 2000 kHz in high-frequency generators, and for example ren up to 200 kHz at Mittelfrequenzgenerato- reindeer.
  • the heating head L may comprise other means for heating, for example radiant heating or other means known in the art for locally selectively heating a metallic powder.
  • the suspension 201 preferably comprises three or four Aktua gates 201.
  • An embodiment with four arranged in the corners of the construction space on AR actuators 201 is shown explicitly in game in Figure 2.
  • the actuators 201 may, preferably individually driven, and be mounted or fixed evenly in the space on AR, and / or accordingly be activated or activated.
  • the actuators 201 may preferably further be made flexible, i. that the platform 200 via a ent speaking activation of the actuators 201, for example, accordingly any lying in the body space AR ( mileagesi shear) coordinates C, U, Z can be arranged or moved. This can be done for example via a transmission, a cable, telescopic arm or pneumatic and / or hydraulic means. For example, it is possible to coordinate the actuators via compressed air or electrically controlled telescopic arms and / or coordinated and controlled to acti suffien.
  • the device 300 further comprises a protective gas guide or protective gas inlet 220.
  • the protective gas guide 220 is, preferably designed, a protective gas, for example an inert gas such as argon or helium or other inert gases during the additive production of the component 10 laminar over and / or perpendicular to the component material P to lead (see, arrows in the Melt bath SB in Figure 2).
  • the protective gas guide 220 may in particular comprise or constitute a miniaturized and / or endoscopic protective gas nozzle and thereby provides, in particular locally, for a reduction in the oxygen content in the selectively preheated or heated zone during the additive production of the component 10.
  • protective gas nozzle (not explicitly identified) can be provided, in particular, in addition to a global or laminar protective gas guide, which reduces the oxygen content or partial pressure in additive manufacturing processes or in installation spaces of conventional installations.
  • the device 300 or the system 100 can furthermore have a corresponding protective gas outlet (not explicitly indicated).
  • the present invention or in the presented device 300 is advantageously a preheating with means of a high-frequency coil, which is supported by the platform 200, suspended in particular four actuators.
  • the coil similar to a spider or a spin nen stressess, over the construction field or the construction area AF are suspended and be moved by a corresponding activation of the actuators Ak in 201 each XYZ position within the space AR.
  • the four actuators 201 are respectively mounted in the corners of the mounting space AR and all engage in the platform 200.
  • the protective gas guide 220 and, for example, also a power supply 210 and a control of the heating head or the coils L and leads or supplies the
  • Protective gas guide 220 or the power supply 210 may also be attached to the, in particular annular, platform 200.
  • the above leads are preferably also made flexible so that no movement of Restraint of the platform 200 and the heating head L ent stands.
  • FIG. 3 shows, with reference to a schematic flow diagram, method steps of a method according to the invention, in particular a method for operating said device 300 or an additive manufacturing method.
  • the method comprises, a), the orders of a layer S of the component material P on the mounting surface AF by means of the Be coating device 30th
  • the method further comprises, b), lowering or Anord NEN of the platform 200 in the direction of an area to be irradiated Be B of the mounting surface AF.
  • this is preferably at least partially along the vertical axis (Z axis) moves down to the platform or preferably so, the heating head L in the direction of the area B to be due.
  • the region B preferably describes the region which is provided in layers for the additive construction of the component 10 for irradiation. Accordingly, the region B may include or include a molten bath SB late (as viewed in plan view of the mounting surface AF).
  • the area B be preferably writes a dynamic or - during the construction of the component 10 - movable range or ent speaking Irradationstraj ektorie.
  • the method further comprises, c) heating or preheating the area B to be irradiated, preferably a larger area containing the area B, by means of the heating head L of the device 300.
  • the method further comprises, d) irradiating the region B with an energy beam 21 in accordance with a predetermined geometry of the component 10.
  • the method further comprises, preferably after the irradiation of the area B (see steps d) and e), a lifting or lifting of the platform 200 from an area of action of the irradiation device 30.
  • the area of action preferably describes an area just above the mounting surface AF within which the loading radiation device, in particular a doctor blade or a blade is moved laterally, so preferably a region which occupies only a small vertical area (height in the Z direction) in the body space ,
  • the said method steps can, of course, be repeated by way of the layer-wise additive production of the component 10 in accordance with the number of layers still to be built up and required to be built up.
  • the described steps of heating (c)) and of irradiating (d)) are carried out at least partially simultaneously. This is indicated by the dashed circle in FIG.
  • the irradiation of the area B can continue to be carried out synchronously with the heating, wherein the energy beam 21, for example during the additive construction of the component 10 by an eye (not explicitly marked) of Indukti onsspule or the heating head and / or the device 300 is performed ,
  • This can advantageously enable a synchronous movement with a working laser (cf reference numeral 21 in Figure 1 g) for the construction of the component 10.
  • an energy beam 21 during the manufacture of the device 10 during operation always by the "eye" of the induction coil L to the predetermined position in the area B on the mounting surface AF.
  • This area B is preferably the area which is heated by the heating head L anyway.
  • the invention is not limited by the description based on the embodiments of these, but includes each new feature and any combination of features. This includes in particular any combination of features in the claims, even if this feature or this combi nation itself is not explicitly stated in the claims or exemplary embodiments.

Landscapes

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

Abstract

L'invention concerne un dispositif (300) de chauffage sélectif d'un matériau de composant (P) pour la fabrication additive d'un composant (10), en particulier à base de lit de poudre. Le dispositif comprend une plateforme (200) comportant une tête chauffante (L), en particulier une tête chauffante inductive, et une suspension (201) qui soutient la plateforme (200) et qui est conçue pour déplacer la plateforme (200) de manière contrôlée le long de trois directions spatiales verticales (X, Y, Z) dans un espace de montage (AR) d'une installation de fabrication additive (100). L'invention concerne en outre une installation de fabrication additive (100) comprenant le dispositif (300) et un procédé de fabrication additive correspondant.
EP19726914.5A 2018-05-28 2019-05-06 Dispositif de chauffage d'un matériau de composant, installation de fabrication additive et procédé de fabrication additive Withdrawn EP3740381A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102018208400.9A DE102018208400A1 (de) 2018-05-28 2018-05-28 Vorrichtung zum Erwärmen eines Bauteilmaterials, additive Herstellungsanlage und Verfahren zur additiven Herstellung
PCT/EP2019/061488 WO2019228755A1 (fr) 2018-05-28 2019-05-06 Dispositif de chauffage d'un matériau de composant, installation de fabrication additive et procédé de fabrication additive

Publications (1)

Publication Number Publication Date
EP3740381A1 true EP3740381A1 (fr) 2020-11-25

Family

ID=66668873

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19726914.5A Withdrawn EP3740381A1 (fr) 2018-05-28 2019-05-06 Dispositif de chauffage d'un matériau de composant, installation de fabrication additive et procédé de fabrication additive

Country Status (4)

Country Link
EP (1) EP3740381A1 (fr)
CN (1) CN112203858A (fr)
DE (1) DE102018208400A1 (fr)
WO (1) WO2019228755A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP4015106A1 (fr) * 2020-12-18 2022-06-22 Siemens Energy Global GmbH & Co. KG Structure de composant poreuse fabriquée de manière additive et son moyen de fabrication

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1968355B1 (fr) * 2007-03-08 2013-02-27 HÜTTINGER Elektronik GmbH + Co. KG Bobine d'induction et dispositif destinés au réchauffement par induction de pièces usinées
EP2415552A1 (fr) 2010-08-05 2012-02-08 Siemens Aktiengesellschaft Procédé de fabrication d'un composant par fusion laser sélective
DE102012206122A1 (de) * 2012-04-13 2013-10-17 MTU Aero Engines AG Mehrfach-Spulenanordnung für eine Vorrichtung zur generativen Herstellung von Bauteilen und entsprechendes Herstellverfahren
DE102012206125A1 (de) * 2012-04-13 2013-10-17 MTU Aero Engines AG Verfahren zur Herstellung von Niederdruckturbinenschaufeln aus TiAl
DE102014209161A1 (de) * 2014-05-14 2015-11-19 Eos Gmbh Electro Optical Systems Steuereinheit, Vorrichtung und Verfahren zum Herstellen eines dreidimensionalen Objekts
DE102015002967A1 (de) * 2015-03-07 2016-10-13 Willi Viktor LAUER 3D-Druckwerkzeug und 3D-Druck von Bündeln
US10882112B2 (en) * 2015-06-17 2021-01-05 Sintratec Ag Additive manufacturing device with a heating device
EP3199268A1 (fr) * 2016-01-28 2017-08-02 Siemens Aktiengesellschaft Procede de fabrication generative de composants a l'aide d'une plateforme de construction pouvant etre chauffee et installation pour ledit procede
DE102016205782A1 (de) * 2016-04-07 2017-10-12 MTU Aero Engines AG Verfahren und Vorrichtung zum Herstellen zumindest eines Bauteilbereichs eines Bauteils
DE102016206558A1 (de) * 2016-04-19 2017-10-19 MTU Aero Engines AG Verfahren und Vorrichtung zum Herstellen zumindest eines Bauteilbereichs eines Bauteils
CN105903970A (zh) * 2016-04-27 2016-08-31 华中科技大学 一种利用感应加热快速成形金属零件的装置和方法
DE102016218647A1 (de) * 2016-09-28 2018-03-29 MTU Aero Engines AG Vorrichtung und Verfahren zum induktiven Erwärmen eines Bauteils
CN106563806B (zh) * 2016-11-03 2018-07-03 西安交通大学 一种粉床增材制造的电磁感应加热供铺粉一体化系统
CN106903311A (zh) * 2017-03-09 2017-06-30 西安交通大学 一种电磁感应激光选区熔化粉床在线加热系统及方法

Also Published As

Publication number Publication date
DE102018208400A1 (de) 2019-11-28
CN112203858A (zh) 2021-01-08
WO2019228755A1 (fr) 2019-12-05

Similar Documents

Publication Publication Date Title
EP2836323B1 (fr) Configuration de bobines multiples pour un dispositif de fabrication générative de composants et procédé de fabrication correspondant
EP2099582B1 (fr) Dispositif et procédé de réparation ou de fabrication de pointes d'aubes d'une turbine à gaz, notamment d'un moteur d'avion
DE102014108061A1 (de) Vorrichtung und Verfahren zur generativen Herstellung zumindest eines Bauteilbereichs eines Bauteils
EP3235580B1 (fr) Procédé et dispositif de fabrication d'au moins une zone d'un composant
EP2857139B1 (fr) Dispositif de traitement laser de matériau avec une tête laser déplaçable dans l'espace
EP2789413B1 (fr) Régulation de température pour un dispositif de fabrication générative de composants et procédé de fabrication correspondant
EP2311597B1 (fr) Procédé de soudage laser de pièces en superalliages haute température avec contrôle de certains paramètres du soudage laser pour obtenir une vitesse de refroidissement particulière
DE102014203711A1 (de) Erzeugung von Druckeigenspannungen bei generativer Fertigung
EP3074161B1 (fr) Procédé et dispositif de fabrication générative d'au moins zone d'un élément structurel
EP2280801B1 (fr) Procédé de soudage de pièces d'usinage en alliages superréfractaires
EP2572815B1 (fr) Chauffage à induction multifréquent de composants fabriqués de manière générative
EP2915611B1 (fr) Dispositif et procédé de fabrication générative d'un composant
DE102014108081A1 (de) Vorrichtung und Verfahren zur generativen Herstellung zumindest eines Bauteilbereichs eines Bauteils
EP2493643A1 (fr) Procédé et dispositif permettant la fabrication d'un élément d'une turbomachine
WO2005075136A1 (fr) Procede de soudure de reparation permettant de reparer un composant qui comprend une matiere de base avec une microstructure orientee
DE102015214994A1 (de) Ein Verfahren zur Herstellung oder Reparatur eines Bauteils und Vorrichtung zur Herstellung und Reparatur eines Bauteils
DE102017118831A1 (de) Verfahren und Vorrichtung zum additiven Herstellen mindestens einer Bauteilschicht eines Bauteils und Speichermedium
EP3461571A1 (fr) Procédé de rayonnement d'une couche de poudre dans une fabrication additive présentant des paramètres de fabrication définis de manière continue
EP3740381A1 (fr) Dispositif de chauffage d'un matériau de composant, installation de fabrication additive et procédé de fabrication additive
WO2021104730A1 (fr) Procédé d'irradiation sélective d'une couche de poudre lors de la fabrication additive à l'aide d'un premier et d'un second motif d'irradiation
DE102016205782A1 (de) Verfahren und Vorrichtung zum Herstellen zumindest eines Bauteilbereichs eines Bauteils
EP3656490A1 (fr) Procédé de fourniture de données pour une régulation adaptative de la température

Legal Events

Date Code Title Description
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE

PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20200817

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: SIEMENS ENERGY GLOBAL GMBH & CO. KG

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: EXAMINATION IS IN PROGRESS

17Q First examination report despatched

Effective date: 20210723

DAV Request for validation of the european patent (deleted)
DAX Request for extension of the european patent (deleted)
RIC1 Information provided on ipc code assigned before grant

Ipc: B33Y 40/10 20200101ALI20220114BHEP

Ipc: B22F 12/00 20210101ALI20220114BHEP

Ipc: B29C 64/227 20170101ALI20220114BHEP

Ipc: B29C 64/245 20170101ALI20220114BHEP

Ipc: B29C 64/295 20170101ALI20220114BHEP

Ipc: B29C 64/153 20170101ALI20220114BHEP

Ipc: B22F 3/105 20060101ALI20220114BHEP

Ipc: B33Y 30/00 20150101ALI20220114BHEP

Ipc: B22F 1/142 20220101ALI20220114BHEP

Ipc: B33Y 40/00 20200101ALI20220114BHEP

Ipc: B33Y 10/00 20150101ALI20220114BHEP

Ipc: B22F 12/20 20210101ALI20220114BHEP

Ipc: B22F 10/20 20210101ALI20220114BHEP

Ipc: B22F 5/04 20060101ALI20220114BHEP

Ipc: B22F 5/00 20060101AFI20220114BHEP

RIC1 Information provided on ipc code assigned before grant

Ipc: B33Y 40/10 20200101ALI20220201BHEP

Ipc: B22F 12/00 20210101ALI20220201BHEP

Ipc: B29C 64/227 20170101ALI20220201BHEP

Ipc: B29C 64/245 20170101ALI20220201BHEP

Ipc: B29C 64/295 20170101ALI20220201BHEP

Ipc: B29C 64/153 20170101ALI20220201BHEP

Ipc: B22F 3/105 20060101ALI20220201BHEP

Ipc: B33Y 30/00 20150101ALI20220201BHEP

Ipc: B22F 1/142 20220101ALI20220201BHEP

Ipc: B33Y 40/00 20200101ALI20220201BHEP

Ipc: B33Y 10/00 20150101ALI20220201BHEP

Ipc: B22F 12/20 20210101ALI20220201BHEP

Ipc: B22F 10/20 20210101ALI20220201BHEP

Ipc: B22F 5/04 20060101ALI20220201BHEP

Ipc: B22F 5/00 20060101ALI20220201BHEP

Ipc: B22F 12/13 20210101ALI20220201BHEP

Ipc: B22F 10/28 20210101AFI20220201BHEP

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 20220621