WO2015108849A1 - Systems and processes for distributing material during additive manufacturing - Google Patents

Systems and processes for distributing material during additive manufacturing Download PDF

Info

Publication number
WO2015108849A1
WO2015108849A1 PCT/US2015/011145 US2015011145W WO2015108849A1 WO 2015108849 A1 WO2015108849 A1 WO 2015108849A1 US 2015011145 W US2015011145 W US 2015011145W WO 2015108849 A1 WO2015108849 A1 WO 2015108849A1
Authority
WO
WIPO (PCT)
Prior art keywords
support surface
belt
coating device
layer
powder
Prior art date
Application number
PCT/US2015/011145
Other languages
French (fr)
Inventor
Gary A. Schirtzinger
Sergey Mironets
Original Assignee
United Technologies Corporation
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 United Technologies Corporation filed Critical United Technologies Corporation
Priority to EP15737705.2A priority Critical patent/EP3094435B1/en
Priority to US15/105,394 priority patent/US11072026B2/en
Publication of WO2015108849A1 publication Critical patent/WO2015108849A1/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B28WORKING CEMENT, CLAY, OR STONE
    • B28BSHAPING CLAY OR OTHER CERAMIC COMPOSITIONS; SHAPING SLAG; SHAPING MIXTURES CONTAINING CEMENTITIOUS MATERIAL, e.g. PLASTER
    • B28B1/00Producing shaped prefabricated articles from the material
    • B28B1/001Rapid manufacturing of 3D objects by additive depositing, agglomerating or laminating of material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/20Direct sintering or melting
    • B22F10/28Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM]
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F12/00Apparatus 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
    • B22F12/22Driving means
    • B22F12/224Driving means for motion along a direction within the plane of a layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F12/00Apparatus 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
    • B22F12/60Planarisation devices; Compression devices
    • B22F12/63Rollers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/12Both compacting and sintering
    • B22F3/16Both compacting and sintering in successive or repeated steps
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F5/00Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
    • B22F5/04Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B28WORKING CEMENT, CLAY, OR STONE
    • B28BSHAPING CLAY OR OTHER CERAMIC COMPOSITIONS; SHAPING SLAG; SHAPING MIXTURES CONTAINING CEMENTITIOUS MATERIAL, e.g. PLASTER
    • B28B13/00Feeding the unshaped material to moulds or apparatus for producing shaped articles; Discharging shaped articles from such moulds or apparatus
    • B28B13/02Feeding the unshaped material to moulds or apparatus for producing shaped articles
    • B28B13/0295Treating the surface of the fed layer, e.g. removing material or equalization of the surface
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C64/00Additive 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
    • B29C64/10Processes of additive manufacturing
    • B29C64/141Processes of additive manufacturing using only solid materials
    • B29C64/153Processes of additive manufacturing using only solid materials using layers of powder being selectively joined, e.g. by selective laser sintering or melting
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C64/00Additive 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
    • B29C64/20Apparatus for additive manufacturing; Details thereof or accessories therefor
    • B29C64/205Means for applying layers
    • B29C64/218Rollers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C64/00Additive 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
    • B29C64/20Apparatus for additive manufacturing; Details thereof or accessories therefor
    • B29C64/245Platforms or substrates
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B33ADDITIVE MANUFACTURING TECHNOLOGY
    • B33YADDITIVE 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
    • B33Y10/00Processes of additive manufacturing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B33ADDITIVE MANUFACTURING TECHNOLOGY
    • B33YADDITIVE 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
    • B33Y30/00Apparatus for additive manufacturing; Details thereof or accessories therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/30Process control
    • B22F10/37Process control of powder bed aspects, e.g. density
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F12/00Apparatus 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
    • B22F12/22Driving means
    • B22F12/222Driving means for motion along a direction orthogonal to the plane of a layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F12/00Apparatus 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
    • B22F12/50Means for feeding of material, e.g. heads
    • B22F12/52Hoppers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F12/00Apparatus 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
    • B22F12/50Means for feeding of material, e.g. heads
    • B22F12/57Metering means
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2999/00Aspects linked to processes or compositions used in powder metallurgy
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/04Making non-ferrous alloys by powder metallurgy
    • C22C1/0408Light metal alloys
    • C22C1/0416Aluminium-based alloys
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/04Making non-ferrous alloys by powder metallurgy
    • C22C1/0433Nickel- or cobalt-based alloys
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/04Making non-ferrous alloys by powder metallurgy
    • C22C1/045Alloys based on refractory metals
    • C22C1/0458Alloys based on titanium, zirconium or hafnium
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P10/00Technologies related to metal processing
    • Y02P10/25Process efficiency

Definitions

  • This disclosure relates generally to additive manufacturing and, more particularly, to material distribution during additive manufacturing.
  • additive manufacturing may describe a process where a part or parts are formed by accumulating and/or fusing material together, typically in a layer-on-layer manner. Layers of powder material, for example, may be disposed and thereafter solidified (e.g., sintered or otherwise melted) sequentially onto one another to form the part(s).
  • a layer of powder material may be disposed over a support surface using a blade coater.
  • This blade coater includes a blade, which is elevated above the support surface or a previously deposited layer of powder material on the support surface. A quantity of the powder material is deposited in front of the blade, which pushes the powder material across the support surface to provide the layer of the powder material.
  • the blade is susceptible to hanging up on an edge or edges of previously solidified melted material where, for example, the volume of the solidified material is greater than expected. Such a hang up may damage the blade.
  • a system for manufacturing at least one part.
  • This system includes a coating device, a solidification device and a support, which includes a support surface.
  • the coating device includes a plurality of exterior surfaces disposed around an axis.
  • the coating device is adapted to deposit a layer of powder over at least a portion of the support surface using one or more of the exterior surfaces as the exterior surfaces revolve around the axis.
  • the solidification device is adapted to solidify at least a portion of the layer of powder to form at least a portion of the part.
  • this system includes a coating device, a solidification device and a support, which includes a support surface.
  • the coating device includes a belt wrapped around a plurality of rollers.
  • the coating device is adapted to deposit a layer of material over at least a portion of the support surface by pushing the material across at least the portion of the support surface with the belt.
  • the solidification device is adapted to solidify at least a portion of the layer of material to form at least a portion of the part.
  • a process for manufacturing at least one part. This process includes depositing a substantially uniform layer of material over at least a portion of a support surface using a belt that contacts the material. The process also includes solidifying at least a portion of the layer of material using a solidification device to form at least a portion of the part.
  • the coating device may be adapted to compact the material over the support surface using the belt.
  • the belt may include a plurality of interconnected links.
  • the coating device may be adapted to deposit the layer of powder by pushing the powder across at least the portion of the support surface with one or more of the exterior surfaces.
  • the coating device may be adapted to compact the powder over the support surface using one or more of the exterior surfaces.
  • the coating device may include a belt configured with a plurality of
  • Each of the links may include a respective one of the exterior surfaces.
  • the coating device may include a plurality of rollers. A first of the rollers may be rotatable about the axis. The belt may circumscribe the rollers. The belt may be engaged with one or more of the rollers. [0014] The coating device may include a carriage adapted to move the belt at least partially across the support surface. The rollers may be attached to the carriage.
  • the carriage may be adapted to move the belt reciprocally at least partially across the support surface.
  • the carriage may be adapted to move the belt along looped trajectory.
  • the coating device may be adapted to change a distance between the belt and the support surface.
  • the system may also include a cleaning device adapted to remove powder from one or more of the exterior surfaces.
  • One of the exterior surfaces may have a lateral width that is substantially equal to or greater than a lateral width of the support surface.
  • One of the exterior surfaces may be substantially planar.
  • the solidification device may include a laser and/or an electron beam energy source.
  • the depositing may include pushing the material across at least the portion of the support surface with the belt.
  • the process may include compacting the material over at least the portion of the support surface using the belt.
  • the material may be or include powder.
  • FIG. 1 is a sectional illustration of an additive manufacturing system
  • FIG. 2 is a cross sectional illustration of the additive manufacturing system of
  • FIG. 1 A first figure.
  • FIG. 3 is another sectional illustration of the additive manufacturing system of
  • FIG. 1 A first figure.
  • FIGS. 4-6 are sectional illustrations of a portion of the additive manufacturing system of FIG. 1;
  • FIG. 7 is a sectional illustration of a coater included in the additive manufacturing system of FIG. 1 ;
  • FIG. 8 is a sectional illustration of a portion of the additive manufacturing system of FIG. 1 ;
  • FIG. 9 is a sectional illustration of a portion of the additive manufacturing system of FIG. 1 ;
  • FIG. 10 is another sectional illustration of the additive manufacturing system of
  • FIG. 1 is a diagrammatic representation of FIG. 1 ;
  • FIG. 11 is a flow diagram of a process for additively manufacturing a part or parts using the additive manufacturing system of FIG. 1;
  • FIG. 12 is a sectional illustration of an alternate embodiment additive
  • FIG. 13 is a cross sectional illustration of an alternate embodiment additive manufacturing system.
  • FIGS. 1 and 2 illustrate a system 20 for additively manufacturing a part 22 or parts from material 24 such as, for example, ceramic powder and/or metal powder.
  • ceramic powder include oxides, nitrides, carbides, oxynitrides, carbonitrides, lanthanides, and mixtures thereof such as Si3N4, A1203,SiC, A1N, Si 3 N 4 - Y 2 0 3 - A1N, 3Y-TZP (yttria-doped polycrystalline tetragonal zirconia), YAG (yttrium aluminum garnet), Ti02,Zr02,Si02, zircon ZrSi0 4 , and ceria Ce0 2; etc.
  • metal powder examples include materials commonly used for aerospace application such as Al (Al 2024, Al 6061, A17075), Ti (Ti6Al-4V), Ni (In 625, In 718, In 100, Hastelloy X, B1900 + Hf, Mar-M-247), and Co-based superalloys (CoCr, Stellites, Co- Al-W, Mar-M-509).
  • the system 20, of course, may also or alternatively additively manufacture part(s) 22 from one or more types and/or forms of material other than those described above.
  • the additive manufacturing system 20 includes a support 26, a material source 27, a coating device 28 and a solidification device 29.
  • the system 20 also includes a controller 30, which is in signal communication (e.g., hardwired and/or wirelessly coupled) with one or more of the system components 27-29.
  • the support 26 may be configured as or within an enclosed housing (e.g., sealed enclosure) in which at least a portion of one or more of the system components 27-30 may be located.
  • the support 26 includes a support surface 32. This support surface 32 is configured to support the material 24 and/or at least a portion of the part 22 during additive manufacturing.
  • the support surface 32 for example, may be substantially horizontal relative to gravity.
  • the support surface 32 may also have a generally planar geometry.
  • the material source 27 is adapted to deposit a quantity of the material 24 onto the support surface 32 longitudinally between a location 34 where the part 22 is to be formed and a coater of the coating device 28.
  • the material source 27 may include a material reservoir 36 (e.g., a hopper) and a material outlet 38 (e.g., conduit), which directs the material 24 from the reservoir 36 onto the support surface 32.
  • the outlet 38 may be spatially fixed. Alternatively, the outlet 38 may be adapted to move in order to deposit the material 24 at various locations on the support surface 32.
  • the material source 27 may also include a material regulator 40 configured with, for example, the reservoir 36.
  • the material regulator 40 is adapted to control the quantity and/or the flow rate of the material 24 being directed onto the support surface 32.
  • the material regulator 40 may be configured as or otherwise include a valve and/or a pump (e.g., a hopper screw).
  • the coating device 28 is adapted to move (e.g., push) the material 24 deposited by the material source 27 (see FIG. 3) across at least a portion of the support surface 32 to provide a (e.g., substantially uniform) layer of the material 24 over at least a portion of the support surface 32.
  • the coating device 28 may also be adapted to substantially contemporaneously and/or subsequently compact the material 24 within the deposited layer.
  • the coating device 28 includes a base 42 and a coater
  • the base 42 includes one or more beams 46.
  • Each of these beams 46 includes a slot 48, which may extend vertically between toothed sidewalls 50.
  • the slot 48 extends laterally into the respective beam 46 from a beam side surface.
  • the slot 48 extends longitudinally within (or into or through) the respective beam 46 along a centerline 52 (e.g., an axis), which may be straight and/or substantially parallel to the support surface 32 (see FIG. 4).
  • the base 42 also includes one or more lifts 54.
  • Each of the lifts 54 is configured with a respective one of the beams 46.
  • Each lift 54 includes one or more tracks 56 (or stanchions) and one or more actuators 58.
  • the tracks 56 may be connected to and extend vertically from the support 26.
  • the tracks 56 may be respectively located at longitudinal ends of the beam 46, which is slidably mated with the tracks 56.
  • the actuators 58 are connected to the beam 46 and respectively engaged with the tracks 56.
  • the actuators 58 are adapted to move the beam 46 vertically up and down along the tracks 56.
  • Each actuator 58 for example, may include an electric motor that drives a gear (or friction wheel), which is meshed with teeth of a respective one of the tracks 56.
  • the coater 44 includes a carriage 60, a drivetrain 62, a belt 64 and one or more actuators 66.
  • the coater 44 may also include one or more cleaning devices 68.
  • the carriage 60 may include one or more sub-carriages 70. Each of these sub- carriages 70 may be configured as a vertically and longitudinally extending plate.
  • the drivetrain 62 includes one or more rollers 72-76 and one or more axles 78-82, which rotatably attach the rollers 72-76 to one or more of the sub-carriages 70.
  • the roller 72 e.g., a level setting roller
  • the roller 72 is arranged longitudinally between the rollers 73 and 74 (e.g., drive rollers) as well as longitudinally between the rollers 75 and 76 (e.g., idler rollers).
  • Each of the rollers 75 and 76 is arranged and engaged (e.g., meshed) longitudinally between the roller 72 and a respective one of the rollers 73 and 74.
  • a vertical distance between the roller 72 and the support surface 32 is less than respective vertical distances between the rollers 73-76 and the support surface 32.
  • a diameter of the roller 72 may be greater than respective diameters of the rollers 73-76.
  • the diameter of the rollers 73 and 74 may be greater than respective diameters of the rollers 75 and 76.
  • the drivetrain 62 is not limited to the foregoing roller dimensions. In other embodiments, for example, the diameters of the rollers 73 and 74 may be substantially equal to or greater than the diameter of the roller 72.
  • the drivetrain 62 of FIGS. 2 and 8 also include one or more gears 84 and 86.
  • the gears 84 are connected to the roller 73 through the axle 79.
  • the gears 86 are connected to the roller 74 through the axle 80.
  • Each of the gears 84 and 86 is disposed within a respective one of the slots 48.
  • Each of the gears 84 and 86 is meshed with one or more of the toothed sidewalls 50.
  • the belt 64 may include a plurality of interconnected links 88.
  • Adjacent links 88 may be connected to one another through a pivot (e.g., a pin) connection 90.
  • Each of the links 88 includes an exterior surface 92, which may be a substantially flat planar surface. However, the exterior surface 92 of one or more of the links 88 may alternatively be non-planar; e.g., curved.
  • rollers 72-76 circumscribe the rollers 72-76.
  • the belt 64 is engaged with the rollers 72-74 through, for example, frictional contact and/or meshed features (e.g., teeth or cogs). With this configuration, rotation of the rollers 72-76 rotates the belt 64 and causes the surfaces 92 to generally revolve around the rollers 72-76 and, thus, their axes.
  • each actuator 66 is adapted to move the coater 44 along the beams 46 (see FIG. 1).
  • Each actuator 66 for example, is connected to a respective one of the sub-carriages 70 through at least one linkage; e.g., a strut or pulley system.
  • Each actuator 66 may also be grounded; e.g., connected to the beam 46.
  • Each actuator 66 may be configured as a motor that pushes and/or pulls the linkage to move the sub-carriage 70 and, thus, the carriage 60 and the coater 44.
  • each actuator 66 may be configured to directly drive the drivetrain 62.
  • the cleaning devices 68 extend laterally between and are attached to one or more of the sub-carriages 70 (see also FIG. 2). These cleaning devices 68 are adapted to remove material 24 from the belt 64.
  • Each cleaning device 68 may be configured with a flexible wiper blade, which brushes material 24 off of the belt 64 and its interconnected links 88.
  • the solidification device 29 is adapted to solidify at least a portion of the material 24 deposited on the support surface 32 to form at least a portion of the part 22.
  • the solidification device 29 may melt at least some of the metal powder such that the melted powder fuses together to form a portion of the part 22.
  • the solidification device 29 may be configured as or otherwise include a laser and/or an electron beam energy source.
  • the controller 30 is adapted to signal one or more of the system components 27-
  • the controller 30 may be implemented with a combination of hardware and software.
  • the hardware includes memory and a processing device (or system), which includes one or more single-core and/or multi-core processors.
  • the memory may be a non-transitory computer readable medium, and configured to store software (e.g., program instructions) for execution by the processing device.
  • the hardware may also or alternatively include analog and/or digital circuitry other than that described above.
  • FIG. 11 is a flow diagram of a process for additively manufacturing a part 22 (or parts) using the system 20.
  • a part that may be additive manufactured with the system 20 is a rotor blade for a turbine engine; e.g., a turbine blade, a compressor blade or a fan blade.
  • Other examples of a part that may be additive manufactured with the system 20 include a stator blade for a turbine engine, a guide vane for a turbine engine, a gas path wall for a turbine engine as well as various other components included in a turbine engine.
  • the process of FIG. 11 and the system 20, of course, may also or alternatively additive manufacture parts other than those included in a turbine engine.
  • the material source 27 deposits a mound of the material 24 onto the support surface 32.
  • the controller 30, for example, may signal the material regulator 40 to direct a predetermined quantity of the material 24 from the reservoir 36, through the outlet 38 and onto the support surface 32.
  • the mound of material 24 may extend partially or fully along a lateral length of the belt 64 and/or the support surface 32.
  • the material source 27 may deposit a plurality of discrete mounds laterally across at least a portion of the support surface 32.
  • step 1102 referring to FIG. 4, the coater 44 is located a non-zero vertical distance 94 above the support surface 32 and/or previously deposited material 24.
  • the controller 30, for example, may signal the actuators 58 (see FIGS. 1 and 2) to vertically move the beams 46 to vertically locate the coater 44.
  • the vertical distance 94 sets a vertical thickness of the layer of material 24 to be deposited over the support surface 32.
  • the coating device 28 deposits a layer of the material 24 over at least a portion of the support surface 32.
  • the controller 30, may signal the actuators 66 (see FIGS. 1 and 7) to move the carriage 60 longitudinally along the beams 46 in a forward direction; e.g., towards the left-hand-side of FIGS. 4 and 5.
  • This longitudinal carriage 60 movement causes a forward (e.g., right hand) portion of the belt 64 to push a quantity of the material 24 across the support surface 32.
  • another metered quantity of the material 24 passes vertically beneath the belt 64 thereby distributing the material 24 across the support surface 32.
  • the longitudinal carriage 60 movement also rotates the gears 84 and 86, which rotate the rollers 72-76 and the belt 64.
  • the exterior surfaces 92 may each at least partially compact the material 24 against the support surface 32 (or a previously deposited layer) and thereby provide a layer of the material 24 behind (e.g., toward the right of) the coating device 28.
  • This layer may be substantially uniform where, for example, the vertical distance 94 (see FIG. 4) is substantially constant across a respective portion of the support 26; e.g., the centerline 52 is parallel to the support surface 32.
  • the gears 84 and 86 and the rollers 72-76 may be sized such that the link 88 (or links) vertically closest to the support surface 32 (see FIG. 9) is substantially longitudinally stationary during longitudinal carriage 60 movement.
  • This configuration may reduce the likelihood of the material 24 being kicked up behind (e.g., toward the right of) the coater 44.
  • This configuration may also reduce the likelihood of the belt 64 hanging up on or otherwise getting stuck against previously solidified material.
  • the belt 64 may rollover the solidified material.
  • the coater 44 may also include a suspension, which provides a relatively small degree of vertical movement for the axle and roller to reduce the likelihood of the solidified material damaging the belt 64 and/or other coating device 28 components.
  • the coating device 28 may compact (or further compact) the deposited material 24.
  • the controller 30, may signal the actuators 66 (see FIGS. 1 and 7) to move the carriage 60 longitudinally along the beams 46 in a reverse direction; e.g., towards the right-hand-side of FIGS. 5 and 6.
  • This additional pass e.g., reciprocating movement
  • step 1108 referring to FIG. 10, at least a portion of the deposited layer of the material 24 is solidified.
  • the controller 30, for example, may signal the solidification device 29 to selectively sinter or otherwise melt the material 24 to form at least a portion of the part 22.
  • One or more of the foregoing steps may be repeated for one or more iterations to additively manufacture the part 22 (or parts) layer-by-layer.
  • One or more of the process steps of FIG. 11 may be omitted, re-arranged and/or combined.
  • the step 1102 may be omitted where the coater 44 is already located the vertical distance 94 from the support surface 32 and/or previously deposited material 24.
  • the steps 1100 and 1102 may be performed substantially contemporaneously.
  • the step 1106 may be omitted where the material 24 is sufficiently compacted during the step 1104.
  • the process of FIG. 11 may include one or more additional steps other than those described above.
  • the part 22 may undergo additional manufacturing processes after the material buildup.
  • additional manufacturing processes may include, but are not limited to, machining, surface finishing, coating, etc.
  • each slot 48 may be configured with a looped trajectory. In this manner, the coating device 28 may be lifted away from the material 24 while moving back to its starting position 96.
  • the belt 64 is configured from a plurality of belts 98 or belt segments, which are arranged side-by-side to one another.
  • each actuator 58 may be configured as a piston or a pulley system.
  • one or more of the lifts 54 may each be configured as or include a screw (e.g., a threaded rod) that turns about an axis to lift and/or lower the respective sub- carriage 70.
  • the belt 64 may be a substantially continuous belt; e.g., without the interconnected links 88. The present invention therefore is not limited to any particular coating device 28 components configurations.

Landscapes

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

Abstract

A process is provided for additively manufacturing at least one part. The processing includes depositing a substantially uniform layer of material over at least a portion of a support surface using a belt that contacts the material. The process also includes solidifying at least a portion of the layer of material using a solidification device to form at least a portion of the part.

Description

SYSTEMS AND PROCESSES FOR DISTRIBUTING MATERIAL
DURING ADDITIVE MANUFACTURING
CROSS-REFERENCE TO RELATED APPLICATIONS
This application claims priority to U.S. Provisional Application Serial No. 61/927,286 filed January 14, 2014, which is hereby incorporated herein by reference in its entirety.
BACKGROUND OF THE INVENTION
1. Technical Field
[0001] This disclosure relates generally to additive manufacturing and, more particularly, to material distribution during additive manufacturing.
2. Background Information
[0002] Various additive manufacturing systems are known in the art for forming one or more parts. The term "additive manufacturing" may describe a process where a part or parts are formed by accumulating and/or fusing material together, typically in a layer-on-layer manner. Layers of powder material, for example, may be disposed and thereafter solidified (e.g., sintered or otherwise melted) sequentially onto one another to form the part(s).
[0003] During additive manufacturing, a layer of powder material may be disposed over a support surface using a blade coater. This blade coater includes a blade, which is elevated above the support surface or a previously deposited layer of powder material on the support surface. A quantity of the powder material is deposited in front of the blade, which pushes the powder material across the support surface to provide the layer of the powder material. With such a configuration, however, the blade is susceptible to hanging up on an edge or edges of previously solidified melted material where, for example, the volume of the solidified material is greater than expected. Such a hang up may damage the blade.
[0004] There is a need in the art for improved additive manufacturing material coating device.
SUMMARY OF THE DISCLOSURE
[0005] . According to an aspect of the invention, a system is provided for manufacturing at least one part. This system includes a coating device, a solidification device and a support, which includes a support surface. The coating device includes a plurality of exterior surfaces disposed around an axis. The coating device is adapted to deposit a layer of powder over at least a portion of the support surface using one or more of the exterior surfaces as the exterior surfaces revolve around the axis. The solidification device is adapted to solidify at least a portion of the layer of powder to form at least a portion of the part.
[0006] According to another aspect of the invention, another system is provided for manufacturing at least one part. This system includes a coating device, a solidification device and a support, which includes a support surface. The coating device includes a belt wrapped around a plurality of rollers. The coating device is adapted to deposit a layer of material over at least a portion of the support surface by pushing the material across at least the portion of the support surface with the belt. The solidification device is adapted to solidify at least a portion of the layer of material to form at least a portion of the part.
[0007] According to still another aspect of the invention, a process is provided for manufacturing at least one part. This process includes depositing a substantially uniform layer of material over at least a portion of a support surface using a belt that contacts the material. The process also includes solidifying at least a portion of the layer of material using a solidification device to form at least a portion of the part.
[0008] The coating device may be adapted to compact the material over the support surface using the belt.
[0009] The belt may include a plurality of interconnected links.
[0010] The coating device may be adapted to deposit the layer of powder by pushing the powder across at least the portion of the support surface with one or more of the exterior surfaces.
[0011] The coating device may be adapted to compact the powder over the support surface using one or more of the exterior surfaces.
[0012] The coating device may include a belt configured with a plurality of
interconnected links. Each of the links may include a respective one of the exterior surfaces.
[0013] The coating device may include a plurality of rollers. A first of the rollers may be rotatable about the axis. The belt may circumscribe the rollers. The belt may be engaged with one or more of the rollers. [0014] The coating device may include a carriage adapted to move the belt at least partially across the support surface. The rollers may be attached to the carriage.
[0015] The carriage may be adapted to move the belt reciprocally at least partially across the support surface.
[0016] The carriage may be adapted to move the belt along looped trajectory.
[0017] The coating device may be adapted to change a distance between the belt and the support surface.
[0018] The system may also include a cleaning device adapted to remove powder from one or more of the exterior surfaces.
[0019] One of the exterior surfaces may have a lateral width that is substantially equal to or greater than a lateral width of the support surface.
[0020] One of the exterior surfaces may be substantially planar.
[0021] The solidification device may include a laser and/or an electron beam energy source.
[0022] The depositing may include pushing the material across at least the portion of the support surface with the belt.
[0023] The process may include compacting the material over at least the portion of the support surface using the belt.
[0024] The material may be or include powder.
[0025] The foregoing features and the operation of the invention will become more apparent in light of the following description and the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
[0026] FIG. 1 is a sectional illustration of an additive manufacturing system;
[0027] FIG. 2 is a cross sectional illustration of the additive manufacturing system of
FIG. 1;
[0028] FIG. 3 is another sectional illustration of the additive manufacturing system of
FIG. 1;
[0029] FIGS. 4-6 are sectional illustrations of a portion of the additive manufacturing system of FIG. 1; [0030] FIG. 7 is a sectional illustration of a coater included in the additive manufacturing system of FIG. 1 ;
[0031] FIG. 8 is a sectional illustration of a portion of the additive manufacturing system of FIG. 1 ;
[0032] FIG. 9 is a sectional illustration of a portion of the additive manufacturing system of FIG. 1 ;
[0033] FIG. 10 is another sectional illustration of the additive manufacturing system of
FIG. 1 ;
[0034] FIG. 11 is a flow diagram of a process for additively manufacturing a part or parts using the additive manufacturing system of FIG. 1;
[0035] FIG. 12 is a sectional illustration of an alternate embodiment additive
manufacturing system; and
[0036] FIG. 13 is a cross sectional illustration of an alternate embodiment additive manufacturing system.
DETAILED DESCRIPTION OF THE INVENTION
[0037] FIGS. 1 and 2 illustrate a system 20 for additively manufacturing a part 22 or parts from material 24 such as, for example, ceramic powder and/or metal powder. Examples of ceramic powder include oxides, nitrides, carbides, oxynitrides, carbonitrides, lanthanides, and mixtures thereof such as Si3N4, A1203,SiC, A1N, Si3N4 - Y203 - A1N, 3Y-TZP (yttria-doped polycrystalline tetragonal zirconia), YAG (yttrium aluminum garnet), Ti02,Zr02,Si02, zircon ZrSi04 , and ceria Ce02; etc. Examples of metal powder include materials commonly used for aerospace application such as Al (Al 2024, Al 6061, A17075), Ti (Ti6Al-4V), Ni (In 625, In 718, In 100, Hastelloy X, B1900 + Hf, Mar-M-247), and Co-based superalloys (CoCr, Stellites, Co- Al-W, Mar-M-509). The system 20, of course, may also or alternatively additively manufacture part(s) 22 from one or more types and/or forms of material other than those described above.
[0038] The additive manufacturing system 20 includes a support 26, a material source 27, a coating device 28 and a solidification device 29. The system 20 also includes a controller 30, which is in signal communication (e.g., hardwired and/or wirelessly coupled) with one or more of the system components 27-29. [0039] The support 26 may be configured as or within an enclosed housing (e.g., sealed enclosure) in which at least a portion of one or more of the system components 27-30 may be located. The support 26 includes a support surface 32. This support surface 32 is configured to support the material 24 and/or at least a portion of the part 22 during additive manufacturing. The support surface 32, for example, may be substantially horizontal relative to gravity. The support surface 32 may also have a generally planar geometry.
[0040] Referring to FIG. 3, the material source 27 is adapted to deposit a quantity of the material 24 onto the support surface 32 longitudinally between a location 34 where the part 22 is to be formed and a coater of the coating device 28. The material source 27 may include a material reservoir 36 (e.g., a hopper) and a material outlet 38 (e.g., conduit), which directs the material 24 from the reservoir 36 onto the support surface 32. The outlet 38 may be spatially fixed. Alternatively, the outlet 38 may be adapted to move in order to deposit the material 24 at various locations on the support surface 32.
[0041] The material source 27 may also include a material regulator 40 configured with, for example, the reservoir 36. The material regulator 40 is adapted to control the quantity and/or the flow rate of the material 24 being directed onto the support surface 32. The material regulator 40 may be configured as or otherwise include a valve and/or a pump (e.g., a hopper screw).
[0042] Referring to FIGS. 4-6, the coating device 28 is adapted to move (e.g., push) the material 24 deposited by the material source 27 (see FIG. 3) across at least a portion of the support surface 32 to provide a (e.g., substantially uniform) layer of the material 24 over at least a portion of the support surface 32. The coating device 28 may also be adapted to substantially contemporaneously and/or subsequently compact the material 24 within the deposited layer.
[0043] Referring to FIGS. 1 and 2, the coating device 28 includes a base 42 and a coater
44. The base 42 includes one or more beams 46. Each of these beams 46 includes a slot 48, which may extend vertically between toothed sidewalls 50. The slot 48 extends laterally into the respective beam 46 from a beam side surface. The slot 48 extends longitudinally within (or into or through) the respective beam 46 along a centerline 52 (e.g., an axis), which may be straight and/or substantially parallel to the support surface 32 (see FIG. 4).
[0044] The base 42 also includes one or more lifts 54. Each of the lifts 54 is configured with a respective one of the beams 46. Each lift 54 includes one or more tracks 56 (or stanchions) and one or more actuators 58. The tracks 56 may be connected to and extend vertically from the support 26. The tracks 56 may be respectively located at longitudinal ends of the beam 46, which is slidably mated with the tracks 56. The actuators 58 are connected to the beam 46 and respectively engaged with the tracks 56. The actuators 58 are adapted to move the beam 46 vertically up and down along the tracks 56. Each actuator 58, for example, may include an electric motor that drives a gear (or friction wheel), which is meshed with teeth of a respective one of the tracks 56.
[0045] Referring to FIGS. 2 and 7, the coater 44 includes a carriage 60, a drivetrain 62, a belt 64 and one or more actuators 66. The coater 44 may also include one or more cleaning devices 68.
[0046] The carriage 60 may include one or more sub-carriages 70. Each of these sub- carriages 70 may be configured as a vertically and longitudinally extending plate.
[0047] The drivetrain 62 includes one or more rollers 72-76 and one or more axles 78-82, which rotatably attach the rollers 72-76 to one or more of the sub-carriages 70. The roller 72 (e.g., a level setting roller) is arranged longitudinally between the rollers 73 and 74 (e.g., drive rollers) as well as longitudinally between the rollers 75 and 76 (e.g., idler rollers). Each of the rollers 75 and 76 is arranged and engaged (e.g., meshed) longitudinally between the roller 72 and a respective one of the rollers 73 and 74.
[0048] A vertical distance between the roller 72 and the support surface 32 is less than respective vertical distances between the rollers 73-76 and the support surface 32. A diameter of the roller 72 may be greater than respective diameters of the rollers 73-76. The diameter of the rollers 73 and 74 may be greater than respective diameters of the rollers 75 and 76. The drivetrain 62, however, is not limited to the foregoing roller dimensions. In other embodiments, for example, the diameters of the rollers 73 and 74 may be substantially equal to or greater than the diameter of the roller 72.
[0049] The drivetrain 62 of FIGS. 2 and 8 also include one or more gears 84 and 86. The gears 84 are connected to the roller 73 through the axle 79. The gears 86 are connected to the roller 74 through the axle 80. Each of the gears 84 and 86 is disposed within a respective one of the slots 48. Each of the gears 84 and 86 is meshed with one or more of the toothed sidewalls 50. With this configuration, movement of the carriage 60 along the centerline 52 (see FIG. 4) rotates the gears 84 and 86, which directly or indirectly rotate the rollers 72-76 and, thus, the belt 64 as described below in further detail.
[0050] Referring to FIG. 9, the belt 64 may include a plurality of interconnected links 88.
Adjacent links 88 may be connected to one another through a pivot (e.g., a pin) connection 90. Each of the links 88 includes an exterior surface 92, which may be a substantially flat planar surface. However, the exterior surface 92 of one or more of the links 88 may alternatively be non-planar; e.g., curved.
[0051] Referring to FIGS. 7 and 9, the belt 64 and its interconnected links 88
circumscribe the rollers 72-76. The belt 64 is engaged with the rollers 72-74 through, for example, frictional contact and/or meshed features (e.g., teeth or cogs). With this configuration, rotation of the rollers 72-76 rotates the belt 64 and causes the surfaces 92 to generally revolve around the rollers 72-76 and, thus, their axes.
[0052] Referring to FIG. 7, each actuator 66 is adapted to move the coater 44 along the beams 46 (see FIG. 1). Each actuator 66, for example, is connected to a respective one of the sub-carriages 70 through at least one linkage; e.g., a strut or pulley system. Each actuator 66 may also be grounded; e.g., connected to the beam 46. Each actuator 66 may be configured as a motor that pushes and/or pulls the linkage to move the sub-carriage 70 and, thus, the carriage 60 and the coater 44. Alternatively, each actuator 66 may be configured to directly drive the drivetrain 62.
[0053] The cleaning devices 68 extend laterally between and are attached to one or more of the sub-carriages 70 (see also FIG. 2). These cleaning devices 68 are adapted to remove material 24 from the belt 64. Each cleaning device 68, for example, may be configured with a flexible wiper blade, which brushes material 24 off of the belt 64 and its interconnected links 88.
[0054] Referring to FIG. 10, the solidification device 29 is adapted to solidify at least a portion of the material 24 deposited on the support surface 32 to form at least a portion of the part 22. For example, where the material 24 is metal powder, the solidification device 29 may melt at least some of the metal powder such that the melted powder fuses together to form a portion of the part 22. The solidification device 29 may be configured as or otherwise include a laser and/or an electron beam energy source.
[0055] The controller 30 is adapted to signal one or more of the system components 27-
29 to perform at least a portion of the process described below. The controller 30 may be implemented with a combination of hardware and software. The hardware includes memory and a processing device (or system), which includes one or more single-core and/or multi-core processors. The memory may be a non-transitory computer readable medium, and configured to store software (e.g., program instructions) for execution by the processing device. The hardware may also or alternatively include analog and/or digital circuitry other than that described above.
[0056] FIG. 11 is a flow diagram of a process for additively manufacturing a part 22 (or parts) using the system 20. An example of a part that may be additive manufactured with the system 20 is a rotor blade for a turbine engine; e.g., a turbine blade, a compressor blade or a fan blade. Other examples of a part that may be additive manufactured with the system 20 include a stator blade for a turbine engine, a guide vane for a turbine engine, a gas path wall for a turbine engine as well as various other components included in a turbine engine. The process of FIG. 11 and the system 20, of course, may also or alternatively additive manufacture parts other than those included in a turbine engine.
[0057] In step 1100, referring to FIG. 3, the material source 27 deposits a mound of the material 24 onto the support surface 32. The controller 30, for example, may signal the material regulator 40 to direct a predetermined quantity of the material 24 from the reservoir 36, through the outlet 38 and onto the support surface 32. The mound of material 24 may extend partially or fully along a lateral length of the belt 64 and/or the support surface 32. Alternatively, the material source 27 may deposit a plurality of discrete mounds laterally across at least a portion of the support surface 32.
[0058] In step 1102, referring to FIG. 4, the coater 44 is located a non-zero vertical distance 94 above the support surface 32 and/or previously deposited material 24. The controller 30, for example, may signal the actuators 58 (see FIGS. 1 and 2) to vertically move the beams 46 to vertically locate the coater 44. The vertical distance 94 sets a vertical thickness of the layer of material 24 to be deposited over the support surface 32.
[0059] In step 1104, referring to FIGS. 4-6, the coating device 28 deposits a layer of the material 24 over at least a portion of the support surface 32. The controller 30, for example, may signal the actuators 66 (see FIGS. 1 and 7) to move the carriage 60 longitudinally along the beams 46 in a forward direction; e.g., towards the left-hand-side of FIGS. 4 and 5. This longitudinal carriage 60 movement causes a forward (e.g., right hand) portion of the belt 64 to push a quantity of the material 24 across the support surface 32. Simultaneously, another metered quantity of the material 24 passes vertically beneath the belt 64 thereby distributing the material 24 across the support surface 32.
[0060] Referring to FIGS. 4 and 7-9, the longitudinal carriage 60 movement also rotates the gears 84 and 86, which rotate the rollers 72-76 and the belt 64. In this manner, at least some of the exterior surfaces 92 may each at least partially compact the material 24 against the support surface 32 (or a previously deposited layer) and thereby provide a layer of the material 24 behind (e.g., toward the right of) the coating device 28. This layer may be substantially uniform where, for example, the vertical distance 94 (see FIG. 4) is substantially constant across a respective portion of the support 26; e.g., the centerline 52 is parallel to the support surface 32.
[0061] The gears 84 and 86 and the rollers 72-76 may be sized such that the link 88 (or links) vertically closest to the support surface 32 (see FIG. 9) is substantially longitudinally stationary during longitudinal carriage 60 movement. This configuration may reduce the likelihood of the material 24 being kicked up behind (e.g., toward the right of) the coater 44. This configuration may also reduce the likelihood of the belt 64 hanging up on or otherwise getting stuck against previously solidified material. For example, rather than catching against the solidified material, the belt 64 may rollover the solidified material. The coater 44 may also include a suspension, which provides a relatively small degree of vertical movement for the axle and roller to reduce the likelihood of the solidified material damaging the belt 64 and/or other coating device 28 components.
[0062] In step 1106, referring to FIGS. 5, 6 and 9, the coating device 28 may compact (or further compact) the deposited material 24. The controller 30, for example, may signal the actuators 66 (see FIGS. 1 and 7) to move the carriage 60 longitudinally along the beams 46 in a reverse direction; e.g., towards the right-hand-side of FIGS. 5 and 6. In this manner, at least some of the exterior surfaces 92 may each further compact the material 24 against the support surface 32 (or a previously deposited layer) in a similar manner as described above. This additional pass (e.g., reciprocating movement) may also serve to compact any material that may have been kicked up behind the coater 44 during the step 1104.
[0063] In step 1108, referring to FIG. 10, at least a portion of the deposited layer of the material 24 is solidified. The controller 30, for example, may signal the solidification device 29 to selectively sinter or otherwise melt the material 24 to form at least a portion of the part 22. [0064] One or more of the foregoing steps may be repeated for one or more iterations to additively manufacture the part 22 (or parts) layer-by-layer.
[0065] One or more of the process steps of FIG. 11 may be omitted, re-arranged and/or combined. For example, in some embodiments, the step 1102 may be omitted where the coater 44 is already located the vertical distance 94 from the support surface 32 and/or previously deposited material 24. In some embodiments, the steps 1100 and 1102 may be performed substantially contemporaneously. In some embodiments, the step 1106 may be omitted where the material 24 is sufficiently compacted during the step 1104.
[0066] The process of FIG. 11 may include one or more additional steps other than those described above. For example, in some embodiments, the part 22 (or parts) may undergo additional manufacturing processes after the material buildup. Examples of such additional manufacturing processes may include, but are not limited to, machining, surface finishing, coating, etc.
[0067] The coating device 28 may have various configurations other than that described above. For example, in the embodiment of FIG. 12, each slot 48 may be configured with a looped trajectory. In this manner, the coating device 28 may be lifted away from the material 24 while moving back to its starting position 96. In the embodiment of FIG. 13, the belt 64 is configured from a plurality of belts 98 or belt segments, which are arranged side-by-side to one another. In some embodiments, each actuator 58 may be configured as a piston or a pulley system. In some embodiments, one or more of the lifts 54 may each be configured as or include a screw (e.g., a threaded rod) that turns about an axis to lift and/or lower the respective sub- carriage 70. In some embodiments, the belt 64 may be a substantially continuous belt; e.g., without the interconnected links 88. The present invention therefore is not limited to any particular coating device 28 components configurations.
[0068] While various embodiments of the present invention have been disclosed, it will be apparent to those of ordinary skill in the art that many more embodiments and
implementations are possible within the scope of the invention. For example, the present invention as described herein includes several aspects and embodiments that include particular features. Although these features may be described individually, it is within the scope of the present invention that some or all of these features may be combined within any one of the aspects and remain within the scope of the invention. Accordingly, the present invention is not to be restricted except in light of the attached claims and their equivalents.

Claims

What is claimed is:
1. A system for manufacturing a part, the system comprising:
a support including a support surface;
a coating device including a plurality of exterior surfaces disposed around an axis, the coating device adapted to deposit a layer of powder over at least a portion of the support surface using one or more of the exterior surfaces as the exterior surfaces revolve around the axis; and a solidification device adapted to solidify at least a portion of the layer of powder to form at least a portion of the part.
2. The system of claim 1, wherein the coating device is adapted to deposit the layer of powder by pushing the powder across at least the portion of the support surface with one or more of the exterior surfaces.
3. The system of claim 1, wherein the coating device is adapted to compact the powder over the support surface using one or more of the exterior surfaces.
4. The system of claim 1 , wherein the coating device includes a belt configured with a plurality of interconnected links, and each of the links includes a respective one of the exterior surfaces.
5. The system of claim 4, wherein
the coating device includes a plurality of rollers, a first of which is rotatable about the axis; and
the belt circumscribes the rollers and is engaged with one or more of the rollers.
6. The system of claim 5, wherein the coating device includes a carriage adapted to move the belt at least partially across the support surface, and the rollers are attached to the carriage.
7. The system of claim 6, wherein the carriage is adapted to move the belt reciprocally at least partially across the support surface.
8. The system of claim 6, wherein the carriage is adapted to move the belt along looped trajectory.
9. The system of claim 4, wherein the coating device is adapted to change a distance between the belt and the support surface.
10. The system of claim 1, further comprising a cleaning device adapted to remove powder from one or more of the exterior surfaces.
11. The system of claim 1 , wherein one of the exterior surfaces has a lateral width that is substantially equal to or greater than a lateral width of the support surface.
12. The system of claim 1, wherein the solidification device comprises a laser or an electron beam energy source.
13. A system for manufacturing a part, the system comprising:
a support including a support surface;
a coating device including a belt wrapped around a plurality of rollers, the coating device adapted to deposit a layer of material over at least a portion of the support surface by pushing the material across at least the portion of the support surface with the belt; and
a solidification device adapted to solidify at least a portion of the layer of material to form at least a portion of the part.
14. The system of claim 13, wherein the coating device is adapted to compact the material over the support surface using the belt.
15. The system of claim 13, wherein the belt includes a plurality of interconnected links.
16. A process for manufacturing a part, the method comprising:
depositing a substantially uniform layer of material over at least a portion of a support surface using a belt that contacts the material; and
solidifying at least a portion of the layer of material using a solidification device to form at least a portion of the part.
17. The process of claim 16, wherein the depositing comprises pushing the material across at least the portion of the support surface with the belt.
18. The process of claim 16, further comprising compacting the material over at least the portion of the support surface using the belt.
19. The process of claim 16, wherein the belt includes a plurality of interconnected links.
20. The process of claim 16, wherein
the material comprises powder; and
the solidification device comprises a laser or an electron beam energy source.
PCT/US2015/011145 2014-01-14 2015-01-13 Systems and processes for distributing material during additive manufacturing WO2015108849A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP15737705.2A EP3094435B1 (en) 2014-01-14 2015-01-13 System and process for distributing material during additive manufacturing
US15/105,394 US11072026B2 (en) 2014-01-14 2015-01-13 Systems and processes for distributing material during additive manufacturing

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201461927286P 2014-01-14 2014-01-14
US61/927,286 2014-01-14

Publications (1)

Publication Number Publication Date
WO2015108849A1 true WO2015108849A1 (en) 2015-07-23

Family

ID=53543355

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2015/011145 WO2015108849A1 (en) 2014-01-14 2015-01-13 Systems and processes for distributing material during additive manufacturing

Country Status (3)

Country Link
US (1) US11072026B2 (en)
EP (1) EP3094435B1 (en)
WO (1) WO2015108849A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106994782A (en) * 2016-01-25 2017-08-01 富士施乐株式会社 Shaped device
WO2017196324A1 (en) * 2016-05-12 2017-11-16 Hewlett-Packard Development Company, L.P. Contaminant barrier
US10975703B2 (en) 2016-10-27 2021-04-13 Raytheon Technologies Corporation Additively manufactured component for a gas powered turbine

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105984147B (en) * 2015-02-04 2018-11-30 三纬国际立体列印科技股份有限公司 Three-dimensional printing device
US10717263B2 (en) * 2015-11-13 2020-07-21 Paxis Llc Additive manufacturing apparatus, system, and method
PL3374163T3 (en) 2015-11-13 2023-04-24 Paxis Llc Additive manufacturing apparatus, system, and method
WO2017096050A1 (en) 2015-12-04 2017-06-08 Raytheon Company Electron beam additive manufacturing
US10569364B2 (en) * 2017-01-06 2020-02-25 General Electric Company Systems and methods for additive manufacturing recoating
SG11202009858UA (en) 2018-04-06 2020-11-27 Paxis Llc Additive manufacturing apparatus, system, and method
US10449718B1 (en) * 2018-05-29 2019-10-22 The Exone Company Powder-layer three-dimensional printer with smoothing device

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1996011117A1 (en) 1994-10-07 1996-04-18 Helisys, Inc. Forming integral objects from laminations
US20020152002A1 (en) * 2001-02-21 2002-10-17 Markus Lindemann Process and device for producing a shaped body by selective laser melting
US20090169664A1 (en) * 2005-03-09 2009-07-02 3D Systems, Inc Selective Laser Sintering Powder Recycle System
US20110287185A1 (en) * 2008-11-27 2011-11-24 Felstead Michael W Adaptive Manufacturing Device and Method
US20130071562A1 (en) * 2011-09-16 2013-03-21 Honeywell International Inc. Methods for manufacturing components from articles formed by additive-manufacturing processes
WO2013092757A1 (en) 2011-12-20 2013-06-27 Compagnie Generale Des Etablissements Michelin Machine and process for powder-based additive manufacturing

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2727043C3 (en) * 1976-06-16 1980-05-08 Fuji Photo Film Co., Ltd., Ashigara, Kanagawa (Japan) Device for printing markings on steel plates
US4265175A (en) * 1978-05-04 1981-05-05 Smejda Richard K Central support arrangement for printing systems
US6066285A (en) * 1997-12-12 2000-05-23 University Of Florida Solid freeform fabrication using power deposition
US7045738B1 (en) 2002-10-01 2006-05-16 Southern Methodist University Powder delivery system and method
FR2856614B1 (en) 2003-06-30 2006-08-11 Phenix Systems DEVICE FOR PRODUCING THIN LAYERS OF POWDER, PARTICULARLY AT HIGH TEMPERATURES, IN A PROCESS BASED ON THE ACTION OF A LASER ON THE MATERIAL
US20050263934A1 (en) * 2004-05-28 2005-12-01 3D Systems, Inc. Single side feed parked powder wave heating with wave flattener
US7777155B2 (en) 2007-02-21 2010-08-17 United Technologies Corporation System and method for an integrated additive manufacturing cell for complex components
US20090050449A1 (en) * 2007-08-21 2009-02-26 Ammeraal Beltech B.V. Conveying system
US10092975B2 (en) 2008-02-12 2018-10-09 United Technologies Corporation Solid state additive manufacturing system
FR2948044B1 (en) * 2009-07-15 2014-02-14 Phenix Systems THIN-LAYERING DEVICE AND METHOD OF USING SUCH A DEVICE
FR2949988B1 (en) 2009-09-17 2011-10-07 Phenix Systems PROCESS FOR PRODUCING AN OBJECT BY LASER TREATMENT FROM AT LEAST TWO DIFFERENT PULVERULENT MATERIALS AND CORRESPONDING INSTALLATION
US8460755B2 (en) 2011-04-07 2013-06-11 Stratasys, Inc. Extrusion-based additive manufacturing process with part annealing
FR2974316B1 (en) 2011-04-19 2015-10-09 Phenix Systems PROCESS FOR PRODUCING AN OBJECT BY SOLIDIFYING A POWDER USING A LASER
WO2012143960A1 (en) * 2011-04-22 2012-10-26 Vecor Ip Holdings Ltd Apparatuses, system and methods for forming pressed articles and pressed articles formed thereby
US8488994B2 (en) 2011-09-23 2013-07-16 Stratasys, Inc. Electrophotography-based additive manufacturing system with transfer-medium service loops
US9904223B2 (en) * 2011-09-23 2018-02-27 Stratasys, Inc. Layer transfusion with transfixing for additive manufacturing
MX354209B (en) * 2012-03-02 2018-02-06 Mercier Craig System and method for mobile subvehicular access and treatment of ground surfaces about occupied rail tracks.
DE102012010272A1 (en) * 2012-05-25 2013-11-28 Voxeljet Technology Gmbh Method for producing three-dimensional models with special construction platforms and drive systems

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1996011117A1 (en) 1994-10-07 1996-04-18 Helisys, Inc. Forming integral objects from laminations
US20020152002A1 (en) * 2001-02-21 2002-10-17 Markus Lindemann Process and device for producing a shaped body by selective laser melting
US20090169664A1 (en) * 2005-03-09 2009-07-02 3D Systems, Inc Selective Laser Sintering Powder Recycle System
US20110287185A1 (en) * 2008-11-27 2011-11-24 Felstead Michael W Adaptive Manufacturing Device and Method
US20130071562A1 (en) * 2011-09-16 2013-03-21 Honeywell International Inc. Methods for manufacturing components from articles formed by additive-manufacturing processes
WO2013092757A1 (en) 2011-12-20 2013-06-27 Compagnie Generale Des Etablissements Michelin Machine and process for powder-based additive manufacturing

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP3094435A4

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106994782A (en) * 2016-01-25 2017-08-01 富士施乐株式会社 Shaped device
US10173350B2 (en) 2016-01-25 2019-01-08 Fuji Xerox Co., Ltd. Modeling apparatus
CN106994782B (en) * 2016-01-25 2019-05-17 富士施乐株式会社 Molding machine
WO2017196324A1 (en) * 2016-05-12 2017-11-16 Hewlett-Packard Development Company, L.P. Contaminant barrier
US11376791B2 (en) 2016-05-12 2022-07-05 Hewlett-Packard Development Company, L.P. Contaminant barrier
US10975703B2 (en) 2016-10-27 2021-04-13 Raytheon Technologies Corporation Additively manufactured component for a gas powered turbine

Also Published As

Publication number Publication date
US11072026B2 (en) 2021-07-27
US20160311023A1 (en) 2016-10-27
EP3094435A4 (en) 2017-02-22
EP3094435B1 (en) 2022-07-13
EP3094435A1 (en) 2016-11-23

Similar Documents

Publication Publication Date Title
EP3094435B1 (en) System and process for distributing material during additive manufacturing
JP7209050B2 (en) Printhead modules for additive manufacturing systems
EP3017934B1 (en) Powder dispenser for making a component by additive manufacturing
JP6806478B2 (en) Systems and methods for additive manufacturing of composite parts
JP6803694B2 (en) Systems and methods for additive manufacturing of composite parts
EP3840935B1 (en) Flow directing system and method for additive manufacturing system
JP6861482B2 (en) Systems and methods for additional manufacturing of composite parts
RU2670923C2 (en) Extrusion apparatus and method
KR102168792B1 (en) Method and apparatus for 3d printing by selective sintering
CN108189390B (en) Selective laser curing apparatus and method
EP3369555B1 (en) Method and machine for manufacturing parts by the technique of additive methods by paste processing with improved paste transport
RU2766260C1 (en) Powder three-dimensional printer with an aligning apparatus
US10828832B2 (en) Powder dispensing unit, powder spreading unit, and a vibratory compaction system of an additive manufacturing system and methods therefor
WO2018191728A1 (en) High density 3d printing
US20050280185A1 (en) Methods and apparatus for 3D printing
EP4045211B1 (en) Additive manufacturing machine comprising a mobile and regulated powder dispensing
CN107848200B (en) Supplying construction material
CN105555418B (en) Fluid application system and fluid application method
US20180326484A1 (en) Systems and methods for fabricating and assembling sectional binder jet printed parts
JP6620505B2 (en) Powder additive manufacturing apparatus and powder layer manufacturing method
US10814552B2 (en) Powder dispensing unit, powder spreading unit, and a vibratory compaction system of an additive manufacturing system and methods therefor
EP3628422A1 (en) Powder dispensing unit, powder spreading unit, and a vibratory compaction system of an additive manufacturing system and methods therefor
WO2017095416A1 (en) Supplying build material
JP2018154042A (en) Three-dimensional molding apparatus, method for manufacturing three-dimensional molded article and program
US20240059008A1 (en) Resin management system for additive manufacturing

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 15737705

Country of ref document: EP

Kind code of ref document: A1

WWE Wipo information: entry into national phase

Ref document number: 15105394

Country of ref document: US

NENP Non-entry into the national phase

Ref country code: DE

REEP Request for entry into the european phase

Ref document number: 2015737705

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 2015737705

Country of ref document: EP