US20220288850A1 - Rotational additive manufacturing systems and methods - Google Patents

Rotational additive manufacturing systems and methods Download PDF

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Publication number
US20220288850A1
US20220288850A1 US17/690,901 US202217690901A US2022288850A1 US 20220288850 A1 US20220288850 A1 US 20220288850A1 US 202217690901 A US202217690901 A US 202217690901A US 2022288850 A1 US2022288850 A1 US 2022288850A1
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Prior art keywords
powder
gas flow
gas
build
controlling
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Abandoned
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US17/690,901
Inventor
Michael Thomas Kenworthy
Samuel Noah Miller
Krzysztof Artysiewicz
Chor Yen YAP
Gregory S. Weaver
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Divergent Technologies Inc
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Divergent Technologies Inc
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Priority to US17/690,901 priority Critical patent/US20220288850A1/en
Priority to PCT/US2022/019642 priority patent/WO2022192465A1/en
Publication of US20220288850A1 publication Critical patent/US20220288850A1/en
Assigned to WESTERN ALLIANCE BANK reassignment WESTERN ALLIANCE BANK SECURITY INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: DIVERGENT TECHNOLOGIES, INC.
Abandoned legal-status Critical Current

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    • 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
    • B29C64/227Driving means
    • B29C64/241Driving means for rotary motion
    • 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
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/30Process control
    • B22F10/32Process control of the atmosphere, e.g. composition or pressure in a building chamber
    • B22F10/322Process control of the atmosphere, e.g. composition or pressure in a building chamber of the gas flow, e.g. rate or direction
    • 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
    • B22F10/34Process control of powder characteristics, e.g. density, oxidation or flowability
    • 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
    • B22F12/30Platforms or substrates
    • B22F12/37Rotatable
    • 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
    • B22F12/40Radiation means
    • B22F12/44Radiation means characterised by the configuration of the radiation means
    • B22F12/45Two or more
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
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    • 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
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    • B22F12/70Gas flow means
    • 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
    • B29C64/245Platforms or substrates
    • 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
    • B29C64/264Arrangements for irradiation
    • B29C64/268Arrangements for irradiation using laser beams; using electron beams [EB]
    • 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
    • B29C64/264Arrangements for irradiation
    • B29C64/277Arrangements for irradiation using multiple radiation means, e.g. micromirrors or multiple light-emitting diodes [LED]
    • 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
    • B29C64/295Heating elements
    • 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
    • B29C64/30Auxiliary operations or equipment
    • B29C64/307Handling of material to be used in additive manufacturing
    • B29C64/321Feeding
    • B29C64/329Feeding using hoppers
    • 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
    • B29C64/30Auxiliary operations or equipment
    • B29C64/364Conditioning of environment
    • B29C64/371Conditioning of environment using an environment other than air, e.g. inert gas
    • 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
    • B29C64/30Auxiliary operations or equipment
    • B29C64/386Data acquisition or data processing for additive manufacturing
    • B29C64/393Data acquisition or data processing for additive manufacturing for controlling or regulating additive manufacturing processes
    • 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
    • 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
    • B33Y40/00Auxiliary operations or equipment, e.g. for material handling
    • B33Y40/10Pre-treatment
    • 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
    • B33Y50/00Data acquisition or data processing for additive manufacturing
    • B33Y50/02Data acquisition or data processing for additive manufacturing for controlling or regulating additive manufacturing processes
    • 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
    • B22F10/70Recycling
    • B22F10/77Recycling of gas
    • 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
    • B22F12/10Auxiliary heating means
    • B22F12/13Auxiliary heating means to preheat the 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
    • 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
    • B22F12/20Cooling 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
    • 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

  • the present disclosure relates generally to additive manufacturing, and more specifically to a rotational additive manufacturing systems and methods.
  • Three-dimensional (3-D) printing also referred to as additive manufacturing (AM) has recently presented new opportunities to more efficiently build complex transport structures, such as automobiles, aircraft, boats, motorcycles, busses, trains, and the like.
  • AM techniques are capable of fabricating complex components from a wide variety of materials. Applying AM processes to industries that produce these products has proven to produce a structurally more efficient transport structure. For example, an automobile produced using 3-D printed components can be made stronger, lighter, and consequently, more fuel efficient.
  • AM enables manufacturers to 3-D print components that are much more complex and that are equipped with more advanced features and capabilities than components made via traditional machining and casting techniques.
  • the 3-D objects may be formed using layers of material based on a digital model data of the object.
  • a 3-D printer may form the structure defined by the digital model data by printing the structure one layer at a time.
  • a 3-D printer may deposit a powder layer (e.g., powdered metal) on an operating surface.
  • the 3-D printer may then consolidate particular areas of the powder layer into a layer of the object, e.g., by using a laser to melt or sinter the powder of the powder layer together.
  • the steps may be repeated to sequentially form each layer. Accordingly, the 3-D printed object may be built layer by layer.
  • 3-D printing is non-design specific, which offers geometric and design flexibility that conventional manufacturing processes cannot. Furthermore, 3-D printing technologies can produce parts with small feature sizes and geometries that are either significantly difficult or impossible to produce using conventional manufacturing processes.
  • the AM process can be time consuming.
  • the time between printing one layer and depositing powder material for the next layer decreases the overall throughput of an AM system.
  • An apparatus in accordance with an aspect of the present disclosure comprises a build floor, a depositor system configured to deposit a layer of powder onto the build floor, a motor system configured to cause a rotational motion between the depositor system and the build floor, wherein the depositor system deposits the layer of powder during the rotational motion, a receptacle wall configured to contain the powder on the build floor, an energy beam source configured to apply an energy beam in an active area (i.e., scan area) of the layer of powder to selectively fuse a portion of the powder in the active area to form a portion of a build piece, and a gas flow system configured to provide a gas flow across the active area while the energy beam selectively fuses the portion of the layer of powder in the active area.
  • an active area i.e., scan area
  • Such an apparatus further optionally includes one or more of the following features: the motor system causing the rotational motion at least in part by rotating the build floor, the depositor system being configured to remain stationary during the rotational motion, the motor system causing the rotational motion at least in part by moving the depositor system in an arc over the build floor, the receptacle wall being configured to remain stationary during the rotational motion, the gas flow system extracting a gas created by the fusing of the powder, a cover configured to cover a second area of the powder exclusive of the active area, the cover including a heater configured to heat the powder under the cover, and the cover including a sensor configured to sense a characteristic of the powder under the cover.
  • Such an apparatus may further optionally include one or more of the following features: the gas flow system including a gas extractor arranged adjacent to a first boundary of the active area, the gas extractor being configured to extract the gas flow, the gas flow system further including a gas inlet arranged adjacent to a second boundary of the active area, the gas inlet being configured to provide the gas flow, the gas flow system including a gas extractor arranged at an axis of rotation of the rotational motion, the gas extractor being configured to extract the gas flow, the gas flow system further including a gas inlet arranged at a portion of the receptacle wall, the gas inlet being configured to provide the gas flow, and the gas inlet including a plurality of openings that collectively surround the build floor.
  • Such an apparatus may further optionally include one or more of the following features: the energy beam source including one or more energy beam generators, the energy beam source being configured to apply one or more energy beams in a plurality of active areas of the layer of powder to selectively fuse a portion of the powder in each of the active areas, and the gas flow system being configured to provide a gas flow across each of the active areas while the one or more energy beams selectively fuse the portion of the powder in each active area, the active areas being non-overlapping, the gas flow system including a funnel-type gas manifold, the gas flow system being further configured to rotate a direction of the gas flow, the gas flow system including a plurality of gas inlets and a plurality of gas extractors, and the gas flow system rotating the gas flow by opening and closing the gas inlets and the gas extractors, a layer thickness of the selectively fused deposited powder being varied during a build of the build piece, a speed of the rotational motion being varied based on a geometric feature density, and the depositor system including a plurality
  • An apparatus in accordance with an aspect of the present disclosure comprises a build floor, a depositor system configured to deposit a layer of powder onto the build floor, a motor system configured to cause a rotational motion between the depositor system and the build floor, wherein the depositor system deposits the layer of powder during the rotational motion, a receptacle wall configured to contain the powder on the build floor, and an energy beam source configured to apply an energy beam in an active area of the layer of powder to selectively fuse a portion of the powder in the active area to form a portion of a build piece, wherein the motor system is further configured to vary a speed of the rotational motion based on information of a build including the build piece.
  • information of the build may include a geometric feature density.
  • Such an apparatus further optionally includes one or more of the following features: the motor system being configured to vary the speed by increasing the speed when the geometric feature density is lower and increasing the speed when the geometric feature density is higher, the motor system causing the rotational motion at least in part by rotating the build floor, the depositor system being configured to remain stationary during the rotational motion, the motor system causing the rotational motion at least in part by moving the depositor system in an arc over the build floor, the receptacle wall being configured to remain stationary during the rotational motion, the gas flow system extracting a gas created by the fusing of the powder, a cover configured to cover a second area of the powder exclusive of the active area, the cover including a heater configured to heat the powder under the cover, and the cover including a sensor configured to sense a characteristic of the powder under the cover.
  • Such an apparatus may further optionally include one or more of the following features: the gas flow system including a gas extractor arranged adjacent to a first boundary of the active area, the gas extractor being configured to extract the gas flow, the gas flow system further including a gas inlet arranged adjacent to a second boundary of the active area, the gas inlet being configured to provide the gas flow, the gas flow system including a gas extractor arranged at an axis of rotation of the rotational motion, the gas extractor being configured to extract the gas flow, the gas flow system further including a gas inlet arranged at a portion of the receptacle wall, the gas inlet being configured to provide the gas flow, and the gas inlet including a plurality of openings that collectively surround the build floor.
  • Such an apparatus may further optionally include one or more of the following features: the energy beam source including one or more energy beam generators, the energy beam source being configured to apply one or more energy beams in a plurality of active areas of the layer of powder to selectively fuse a portion of the powder in each of the active areas, and the gas flow system being configured to provide a gas flow across each of the active areas while the one or more energy beams selectively fuse the portion of the powder in each active area, the active areas being non-overlapping, the gas flow system including a funnel-type gas manifold, the gas flow system being further configured to rotate a direction of the gas flow, the gas flow system including a plurality of gas inlets and a plurality of gas extractors, and the gas flow system rotating the gas flow by opening and closing the gas inlets and the gas extractors, a layer thickness of the selectively fused deposited powder being varied during a build of the build piece, a speed of the rotational motion being varied based on a geometric feature density, and the depositor system including a plurality
  • An apparatus in accordance with an aspect of the present disclosure comprises a build floor, a depositor system configured to deposit a powder onto the build floor, a motor system configured to cause a rotational motion between the depositor system and the build floor, wherein the depositor system deposits the layer of powder during the rotational motion, a receptacle wall configured to contain the powder on the build floor, and an energy beam source configured to apply an energy beam in an active area of the layer of powder to selectively fuse a portion of the powder in the active area to form a portion of a build piece, wherein a layer thickness of the selectively fused deposited powder is varied during a build of the build piece.
  • the depositor system includes a plurality of depositors
  • the active area includes a plurality of active areas, each arranged after a different depositor of the plurality of depositors
  • a first depositor in the plurality of depositors is arranged 180 degrees apart from a second depositor with respect to the rotational motion
  • the first depositor is associated with a first active area of the plurality of active areas arranged after the first depositor
  • the second depositor is associated with a second active area of the plurality of active areas arranged after the second depositor
  • the layer thickness of the selectively fused deposited powder is varied by the energy beam source fusing some portions of the powder layer in both the first and second active areas and fusing other portions of the powder layer in only the first or second active area
  • the energy beam source is configured to fuse a portion of the build piece near the edge of the build piece by fusing in both the first and second active areas, and is configured to fuse a portion of the build piece in the interior bulk
  • Such an apparatus further optionally includes one or more of the following features: the depositor system including a plurality of depositors, the energy beam source including a plurality of energy beams and the active area including a plurality of active areas, a first depositor in the plurality of depositors depositing a first thickness of powder and a second depositor in the plurality of depositors depositing a second thickness of powder.
  • a first energy beam in the plurality of energy beams fusing the first thickness of powder in a first active area in the plurality of active areas, a second energy beam in the plurality of energy beams fusing the second thickness of powder in a second active area in the plurality of active areas, and a first energy beam in the plurality of energy beams fusing the first thickness of powder and the second thickness of powder in a first active area in the plurality of active areas.
  • Such an apparatus further optionally includes one or more of the following features: the motor system causing the rotational motion at least in part by rotating the build floor, the depositor system being configured to remain stationary during the rotational motion, the motor system causing the rotational motion at least in part by moving the depositor system in an arc over the build floor, the receptacle wall being configured to remain stationary during the rotational motion, the gas flow system extracting a gas created by the fusing of the powder, a cover configured to cover a second area of the powder exclusive of the active area, the cover including a heater configured to heat the powder under the cover, and the cover including a sensor configured to sense a characteristic of the powder under the cover.
  • Such an apparatus may further optionally include one or more of the following features: the gas flow system including a gas extractor arranged adjacent to a first boundary of the active area, the gas extractor being configured to extract the gas flow, the gas flow system further including a gas inlet arranged adjacent to a second boundary of the active area, the gas inlet being configured to provide the gas flow, the gas flow system including a gas extractor arranged at an axis of rotation of the rotational motion, the gas extractor being configured to extract the gas flow, the gas flow system further including a gas inlet arranged at a portion of the receptacle wall, the gas inlet being configured to provide the gas flow, and the gas inlet including a plurality of openings that collectively surround the build floor.
  • Such an apparatus may further optionally include one or more of the following features: the energy beam source including one or more energy beam generators, the energy beam source being configured to apply one or more energy beams in a plurality of active areas of the layer of powder to selectively fuse a portion of the powder in each of the active areas, and the gas flow system being configured to provide a gas flow across each of the active areas while the one or more energy beams selectively fuse the portion of the powder in each active area, the active areas being non-overlapping, the gas flow system including a funnel-type gas manifold, the gas flow system being further configured to rotate a direction of the gas flow, the gas flow system including a plurality of gas inlets and a plurality of gas extractors, and the gas flow system rotating the gas flow by opening and closing the gas inlets and the gas extractors, a layer thickness of the selectively fused deposited powder being varied during a build of the build piece, a speed of the rotational motion being varied based on a geometric feature density.
  • the energy beam source including one or more
  • a method in accordance with an aspect of the present disclosure comprises controlling a depositor system to deposit a layer of powder onto a build floor, controlling a motor system to cause a rotational motion between the depositor system and the build floor, wherein the depositor system deposits the layer of powder during the rotational motion, and a receptacle wall contains the powder on the build floor, controlling an energy beam source to apply an energy beam in an active area of the layer of powder to selectively fuse a portion of the powder in the active area to form a portion of a build piece, and controlling a gas flow system to provide a gas flow across the active area while the energy beam selectively fuses the portion of the layer of powder in the active area.
  • Such a method may further optionally include one or more of the following features: controlling the motor system causes the rotational motion at least in part by rotating the build floor, the depositor system is configured to remain stationary during the rotational motion, controlling the motor system causes the rotational motion at least in part by moving the depositor system in an arc over the build floor, the receptacle wall is configured to remain stationary during the rotational motion, controlling the gas flow system extracts a gas created by the fusing of the powder, covering a second area of the powder exclusive of the active area with a cover, controlling a heater configured to heat the powder under the cover, wherein the heater is arranged in the cover, controlling a sensor to sense a characteristic of the powder under the cover, wherein the sensor is arranged in the cover, controlling the gas flow system includes controlling a gas extractor arranged adjacent to a first boundary of the active area, the gas extractor being controlled to extract the gas flow, controlling the gas flow system further includes controlling a gas inlet arranged adjacent to a second boundary of the active area, the gas inlet being
  • a method in accordance with an aspect of the present disclosure comprises obtaining information of a build including a build piece, controlling a depositor system to deposit a layer of powder onto a build floor, controlling a motor system to cause a rotational motion between the depositor system and the build floor, wherein the depositor system deposits the layer of powder during the rotational motion, and a receptacle wall contains the powder on the build floor, wherein controlling the motor system further includes varying a speed of the rotational motion based on the information of the build during the build of the build piece, and controlling an energy beam source to apply an energy beam in an active area of the layer of powder to selectively fuse a portion of the powder in the active area to form a portion of the build piece.
  • Such a method may further optionally include one or more of the following features: the information of the build includes a geometric feature density, and controlling the motor system includes varying the speed based on the geometric feature density, controlling the motor system causes the rotational motion at least in part by rotating the build floor, the depositor system is configured to remain stationary during the rotational motion, controlling the motor system causes the rotational motion at least in part by moving the depositor system in an arc over the build floor, the receptacle wall is configured to remain stationary during the rotational motion, controlling a gas flow system to extract a gas created by the fusing of the powder, covering a second area of the powder exclusive of the active area with a cover, controlling a heater to heat the powder under the cover, wherein the heater is arranged in the cover, controlling a sensor to sense a characteristic of the powder under the cover, wherein the sensor is arranged in the cover, controlling a gas flow system including a gas extractor arranged adjacent to a first boundary of the active area, the gas extractor being controlled to extract a gas flow,
  • a method in accordance with an aspect of the present disclosure comprises controlling a depositor system to deposit a layer of powder onto a build floor, controlling a motor system to cause a rotational motion between the depositor system and the build floor, wherein the depositor system deposits the layer of powder during the rotational motion, and a receptacle wall contains the powder on the build floor, controlling an energy beam source to apply an energy beam in an active area of the layer of powder to selectively fuse a portion of the powder in the active area to form a portion of a build piece, and varying a layer thickness of the selectively fused deposited powder during a build of the build piece.
  • the depositor system includes a plurality of depositors, wherein controlling the depositor system includes controlling the plurality of depositors to deposit layers of powder simultaneously, the active area includes a plurality of active areas, each arranged after a different depositor of the plurality of depositors, a first depositor in the plurality of depositors is arranged 180 degrees apart from a second depositor with respect to the rotational motion, wherein the first depositor is associated with a first active area of the plurality of active areas arranged after the first depositor, and the second depositor is associated with a second active area of the plurality of active areas arranged after the second depositor, varying the layer thickness of the selectively fused deposited powder includes controlling the energy beam source to fuse some portions of the powder layer in both the first and second active areas and to fuse other portions of the powder layer in only the first or second active area, controlling the energy beam source includes fusing a portion of the build piece near the edge of the build piece by fusing
  • FIGS. 1A-1D illustrate respective side views of an exemplary conventional PBF system during different stages of operation.
  • FIG. 1E illustrates a functional block diagram of a 3-D printer system.
  • FIG. 2 illustrates a side view of a printing system in accordance with an aspect of the present disclosure.
  • FIG. 3 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • FIG. 4 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • FIG. 5 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • FIG. 6 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • FIG. 7 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • FIG. 8 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • FIG. 9 shows a perspective view of an extractor in accordance with an aspect of the present disclosure.
  • FIG. 10 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • FIG. 11 illustrates an example method in accordance with an aspect of the present disclosure.
  • FIG. 12 illustrates another example method in accordance with an aspect of the present disclosure.
  • FIG. 13 illustrates another example method in accordance with an aspect of the present disclosure.
  • AM additive Manufacturing
  • a 3-D object may be fabricated based on a computer aided design (CAD) model.
  • CAD computer aided design
  • the CAD model can be used to generate a set of instructions or commands that are compatible with a particular 3-D printer.
  • the AM process can create a solid three-dimensional object using the CAD model and print instructions.
  • different materials or combinations of material such as engineered plastics, thermoplastic elastomers, metals, ceramics, and/or alloys or combinations of the above, etc., may be used to create a uniquely shaped 3-dimensional object.
  • AM additive manufacturing
  • 3-D printing techniques may include, for example, selective laser melting (SLM), selective laser sintering (SLS), direct metal laser sintering (DMLS), electron beam melting (EBM), powder bed fusion (PBF), and/or other AM processes involving melting or fusion of metallic powders.
  • each layer or “slice” is formed by depositing a layer of powder and exposing portions of the powder to an energy beam.
  • the energy beam is applied to melt areas of the powder layer that coincide with the cross-section of the build piece in the layer.
  • the melted powder cools and fuses to form a slice of the build piece.
  • the process can be repeated to form the next slice of the build piece, and so on.
  • Each layer is deposited on top of the previous layer.
  • the resulting structure is a build piece assembled slice-by-slice from the ground up.
  • AM may include the manufacture of one or more nodes.
  • a node is a structural member that may include one or more interfaces used to connect to other nodes or spanning components such as tubes, extrusions, panels, and the like.
  • a node may be constructed to include additional features and functions, including interface functions, depending on the objectives.
  • Nodes and other components may be connected together.
  • one or more nodes and/or other components may be connected together to form larger components.
  • individual AM structures often need to be connected together, or individual AM structures often need to be connected to machined or COTS parts, to provide combined structures, e.g., to realize the above modular network or to form a complex interior assembly in a vehicle. Examples include node-to-node connections, node-to-panel connections, node-to-tube connections, and node-extrusion connections, among others.
  • mechanical connectors e.g., screws, clamps, etc.
  • an adhesive may be used to form a strong bond.
  • the parts For connecting these parts, a strict tolerance is often desired, meaning that the parts must be positioned to fit precisely in an established orientation.
  • the two parts to be adhered may need to be positioned to avoid direct contact with each other in order to mitigate possible galvanic corrosion problems.
  • an adhesive connection between the AM joint member and panel should result in an accurate fit.
  • the AM joint member should not be misaligned with or offset from the body panel, for example, and the parts should remain properly oriented when a permanent bond is established.
  • FIGS. 1A-1D illustrate respective side views of a conventional 3-D printer system.
  • a 3-D printer system may be a powder-bed fusion (PBF) system 100 .
  • FIGS. 1A-D show a conventional PBF system 100 during different stages of operation. The particular embodiment in FIGS. 1A-1D illustrates various principles of PBF systems that may be helpful in understanding principles of this disclosure.
  • Various components described in the present embodiment are also used in the embodiments of rotational AM, but may not be included in figures below for the sake of clarity and to avoid obscuring other details.
  • components such as energy beam sources e.g., laser source(s) and optical deflector(s), electron beam source(s) and magnetic deflector(s)
  • energy beam sources e.g., laser source(s) and optical deflector(s), electron beam source(s) and magnetic deflector(s)
  • FIGS. 1A-D components such as energy beam sources (e.g., laser source(s) and optical deflector(s), electron beam source(s) and magnetic deflector(s)) are not shown expressly in some of the figures below because some of the figures are top views in which the energy beam source would obscure other portions of the embodiments.
  • FIGS. 1A-D are not shown expressly in some of the figures below because some of the figures are top views in which the energy beam source would obscure other portions of the embodiments.
  • FIGS. 1A-D components are not shown expressly in some of the figures below because some of the figures are top views in which the energy beam source would obscure other portions of the embodiments.
  • PBF system 100 can include a depositor 101 that can deposit each layer of metal powder, an energy beam source 103 that can generate an energy beam, a deflector 105 that can apply the energy beam to fuse the powder material, and a build plate 107 that can support one or more build pieces, such as a build piece 109 .
  • a depositor 101 that can deposit each layer of metal powder
  • an energy beam source 103 that can generate an energy beam
  • a deflector 105 that can apply the energy beam to fuse the powder material
  • a build plate 107 that can support one or more build pieces, such as a build piece 109 .
  • PBF system 100 can also include a build floor 111 positioned within a powder bed receptacle.
  • the walls of the powder bed receptacle 112 generally define the boundaries of the powder bed receptacle, which is sandwiched between the walls 112 from the side and abuts a portion of the build floor 111 below.
  • Build floor 111 can progressively lower build plate 107 so that depositor 101 can deposit a next layer.
  • the entire mechanism may reside in a chamber 113 that can enclose the other components, thereby protecting the equipment, enabling atmospheric and temperature regulation and mitigating contamination risks.
  • Depositor 101 can include a hopper 115 that contains a powder 117 , such as a metal powder, and a leveler 119 that can level the top of each layer of deposited powder.
  • FIG. 1A shows PBF system 100 after a slice of build piece 109 has been fused, but before the next layer of powder has been deposited.
  • FIG. 1A illustrates a time at which PBF system 100 has already deposited and fused slices in multiple layers, e.g., 200 individual layers, to form the current state of build piece 109 , e.g., formed of 200 individual slices.
  • the multiple individual layers already deposited have created a powder bed 121 , which includes powder that was deposited but not fused.
  • FIG. 1B shows PBF system 100 at a stage in which build floor 111 can lower by a powder layer thickness 123 .
  • the lowering of build floor 111 causes build piece 109 and powder bed 121 to drop by powder layer thickness 123 , so that the top of build piece 109 and powder bed 121 are lower than the top of powder bed receptacle wall 112 by an amount equal to the powder layer thickness 123 .
  • a space with a consistent thickness equal to powder layer thickness 123 can be created over the tops of build piece 109 and powder bed 121 .
  • build floor 111 is lowered, but not rotated.
  • FIG. 1C shows PBF system 100 at a stage in which depositor 101 is positioned to deposit powder 117 in a space created over the top surfaces of build piece 109 and powder bed 121 and bounded by powder bed receptacle walls 112 .
  • depositor 101 progressively moves over the defined space (linearly from left to right as viewed in FIG. 1C ) while releasing powder 117 from hopper 115 .
  • Leveler 119 can level the released powder to form a powder layer 125 that leaves powder layer top surface 126 configured to receive fusing energy from energy beam source 103 .
  • Powder layer 125 has a thickness substantially equal to the powder layer thickness 123 (see FIG. 1B ).
  • the powder in a PBF system can be supported by a powder material support structure, which can include, for example, a build plate 107 , a build floor 111 , a build piece 109 , walls 112 , and the like.
  • a powder material support structure can include, for example, a build plate 107 , a build floor 111 , a build piece 109 , walls 112 , and the like.
  • the illustrated thickness of powder layer 125 i.e., powder layer thickness 123 ( FIG. 1B )
  • the illustrated thickness of powder layer 125 is greater than an actual thickness used for the example involving the 200 previously-deposited individual layers discussed above with reference to FIG. 1A . It should be noted that fusing of the powder is not occurring while depositor 101 is depositing powder.
  • FIG. 1D shows PBF system 100 at a stage in which, following the deposition of powder layer 125 ( FIG. 1C ), depositor 101 has returned to its starting position and is no longer depositing powder, and energy beam source 103 generates an energy beam 127 and deflector 105 applies the energy beam to fuse the next slice in build piece 109 .
  • energy beam source 103 can be an electron beam source, in which case energy beam 127 constitutes an electron beam.
  • Deflector 105 can include deflection plates that can generate an electric field or a magnetic field that selectively deflects the electron beam to cause the electron beam to scan across areas designated to be fused.
  • energy beam source 103 can be a laser, in which case energy beam 127 is a laser beam.
  • Deflector 105 can include an optical system that uses reflection and/or refraction to manipulate the laser beam to scan selected areas to be fused.
  • the deflector 105 can include one or more gimbals and actuators that can rotate and/or translate the energy beam source to position the energy beam.
  • energy beam source 103 and/or deflector 105 can modulate the energy beam, e.g., turn the energy beam on and off as the deflector scans so that the energy beam is applied only in the appropriate areas of the powder layer.
  • the energy beam can be modulated by a digital signal processor (DSP).
  • DSP digital signal processor
  • FIG. 1E illustrates a functional block diagram of a 3-D printer system.
  • control devices and/or elements may be coupled to PBF system 100 to control one or more components within PBF system 100 .
  • a device may be a computer 150 , which may include one or more components that may assist in the control of PBF system 100 .
  • Computer 150 may communicate with a PBF system 100 , and/or other AM systems, via one or more interfaces 151 .
  • the computer 150 and/or interface 151 are examples of devices that may be configured to implement the various methods described herein, that may assist in controlling PBF system 100 and/or other AM systems.
  • computer 150 may comprise at least one processor unit 152 , memory 154 , signal detector 156 , a digital signal processor (DSP) 158 , and one or more user interfaces 160 .
  • Computer 150 may include additional components without departing from the scope of the present disclosure.
  • the computer 150 may include at least one processor unit 152 , which may assist in the control and/or operation of PBF system 100 .
  • the processor unit 152 may also be referred to as a central processing unit (CPU).
  • Memory 154 which may include both read-only memory (ROM) and random access memory (RAM), may provide instructions and/or data to the processor unit 152 .
  • a portion of the memory 154 may also include non-volatile random access memory (NVRAM).
  • the processor 152 typically performs logical and arithmetic operations based on program instructions stored within the memory 154 .
  • the instructions in the memory 154 may be executable (by the processor unit 152 , for example) to implement the methods described herein.
  • the processor unit 152 may comprise or be a component of a processing system implemented with one or more processors.
  • the one or more processors may be implemented with any combination of general-purpose microprocessors, microcontrollers, digital signal processors (DSPs), floating point gate arrays (FPGAs), programmable logic devices (PLDs), controllers, state machines, gated logic, discrete hardware components, dedicated hardware finite state machines, or any other suitable entities that can perform calculations or other manipulations of information.
  • the processor unit 152 may also include machine-readable media for storing software.
  • Software shall be construed broadly to mean any type of instructions, whether referred to as software, firmware, middleware, microcode, hardware description language, or otherwise. Instructions may include code (e.g., in source code format, binary code format, executable code format, RS-274 instructions (G-code), numerical control (NC) programming language, and/or any other suitable format of code).
  • the instructions when executed by the one or more processors, cause the processing system to perform the various functions described herein.
  • the computer 150 may also include a signal detector 156 that may be used to detect and quantify any level of signals received by the computer 150 for use by the processing unit 152 and/or other components of the computer 150 .
  • the signal detector 156 may detect such signals as energy beam source 103 power, deflector 105 position, build floor 111 height, amount of powder 117 remaining in depositor 101 , leveler 119 position, and other signals.
  • Signal detector 156 in addition to or instead of processor unit 152 may also control other components as described with respect to the present disclosure.
  • the computer 150 may also include a DSP 158 for use in processing signals received by the computer 150 .
  • the DSP 158 may be configured to generate instructions and/or packets of instructions for transmission to PBF system 100 .
  • the computer 150 may further comprise a user interface 160 in some aspects.
  • the user interface 160 may comprise a keypad, a pointing device, and/or a display.
  • the user interface 160 may include any element or component that conveys information to a user of the computer 150 and/or receives input from the user.
  • the various components of the computer 150 may be coupled together by an interface 151 .
  • the interface 151 may include a data bus, for example, as well as a power bus, a control signal bus, and a status signal bus in addition to the data bus.
  • Components of the computer 150 may be coupled together or accept or provide inputs to each other using some other mechanism.
  • the processor unit 152 may be used to implement not only the functionality described above with respect to the processor unit 152 , but also to implement the functionality described above with respect to the signal detector 156 , the DSP 158 , and/or the user interface 160 . Further, each of the components illustrated in FIG. 1E may be implemented using a plurality of separate elements.
  • processors include microprocessors, microcontrollers, graphics processing units (GPUs), central processing units (CPUs), application processors, digital signal processors (DSPs), reduced instruction set computing (RISC) processors, systems on a chip (SoC), baseband processors, field programmable gate arrays (FPGAs), programmable logic devices (PLDs), state machines, gated logic, discrete hardware circuits, and other suitable hardware configured to perform the various functionality described throughout this disclosure.
  • processors may execute software as that term is described above.
  • the functions described may be implemented in hardware, software, firmware, or any combination thereof. If implemented in software, the functions may be stored on or transmitted over as one or more instructions or code on a computer-readable medium.
  • Computer-readable media includes both computer storage media and communication media including any medium that facilitates transfer of a computer program from one place to another.
  • a storage media may be any available media that can be accessed by a computer.
  • such computer-readable media can comprise RAM, ROM, EEPROM, compact disc (CD) ROM (CD-ROM) or other optical disk storage, magnetic disk storage or other magnetic storage devices, or any other medium that can be used to carry or store desired program code in the form of instructions or data structures and that can be accessed by a computer.
  • Disk and disc includes CD, laser disc, optical disc, digital versatile disc (DVD), floppy disk and Blu-ray disc where disks usually reproduce data magnetically, while discs reproduce data optically with lasers.
  • computer readable medium comprises a non-transitory computer readable medium (e.g., tangible media).
  • a computer such as computer 150 and computer-readable instructions (e.g., computer programs) may similarly be implemented in the following example embodiments to control a PBF system in the various ways described below.
  • FIG. 2 illustrates a side view of a printing system in accordance with an aspect of the present disclosure.
  • a PBF system 200 (which may be referred to as an apparatus herein) may comprise, inter alia, a build floor 201 that rotates as shown by rotation 202 .
  • a motor system 205 can cause the rotational motion of build floor 201 , and can also cause the downward motion of the build floor.
  • motor system 205 may include a threaded screw with a thread pitch equal to a layer thickness of the powder to be deposited.
  • a shaft 206 connects motor system 205 with build floor 201 , and the shaft may include a threaded screw.
  • the other portions of the apparatus such as powder bed receptacle wall 203 , a depositor 207 , an energy beam source 209 , a gas inlet 211 , and a gas extractor 213 ) remain stationary with respect to the rotational motion of build floor 201 .
  • build floor 201 moves downward toward powder egress holes 215 in powder bed receptacle wall 203 and a platform knife 223 .
  • depositor deposits a layer of powder material (e.g., metal powder) onto the build floor to create a powder bed 217 .
  • the layer of powder material rotates into an active area of energy beam source 209 , and the energy beam source applies an energy beam to fuse portions of the powder layer to form a layer of a build piece 219 .
  • gas inlet 211 can allow a gas to flow over the active area, and gas extractor 213 can allow the gas flow to exit the chamber. In this way, for example, smoke, soot, and other byproducts of the fusing process may be removed quickly so that the smoke, soot, etc. does not negatively affect the operation of the energy beam, e.g., by obscuring the beam from fully reaching the powder bed.
  • powder bed 217 is exposed to powder egress holes 215 , and the powder in the powder bed can be allowed to escape through the powder egress holes, which may be holes or screens in the powder bed receptacle walls 203 to allow for some removal or exit paths for any powder from the PBF system 200 .
  • powder egress holes may be holes or screens in the powder bed receptacle walls 203 to allow for some removal or exit paths for any powder from the PBF system 200 .
  • build floor 201 may come into proximity with platform knife 223 .
  • Build floor 201 may be configured to thread past platform knife 223 such that the platform knife is positioned just over the build floor.
  • platform knife 223 can come into contact with the bottom of build piece 219 , i.e., where the build piece is attached to the build floor, and the platform knife can cut or break the build piece off of the build floor as the build floor continues to rotate.
  • motor system 205 coupled to build floor 201 (which may be called a build plate herein) via shaft 206 , may rotate the build floor in cylindrical powder bed receptacle wall 203 .
  • Powder bed receptacle wall 203 may be configured to contain the powder on the build floor.
  • Build floor 201 may include seals to further prevent powder from escaping, e.g., between the build floor and the powder bed receptacle wall.
  • motor system 205 may rotate and raise build floor 201 back to the starting position at the top of powder bed receptacle wall(s) 203 to begin another build.
  • motor system 205 may further rotate powder bed receptacle wall 203 together with build floor 201 , such that the build floor moves vertically but not rotationally with respect to the powder bed receptacle wall. In this way, for example, wear and tear on the seal between the build floor and the powder bed receptacle wall may be reduced. It is noted that the motor system that causes the rotational motion may not be explicitly illustrated or described in some of the figures below, because the motor system may be below the build floor in a top view. However, one skilled in the art will readily understand how motor systems are implemented in all of the embodiments disclosed herein based on the descriptions of the rotational motion and which components are being rotated.
  • an apparatus such as PBF system 200 may provide a rotational layer based processing of the build volume.
  • the depositor can continuously deposit powder, and the energy beam source can fuse portions of the build piece while the depositor is depositing powder, without having to wait until completion of a depositing step.
  • PBF system 200 may create a build piece having a geometry that is sliced in a spiral-wise fashion.
  • PBF system 200 may enable changes to the gas management that may improve the 3-D printing process.
  • PBF system 200 may allow for more efficient handling of soot and other gaseous by-products of powder micro-welding processes than PBF system 100 of the related art.
  • the speed of rotation 202 can be varied depending on information of the build.
  • the build may also be referred to as the build job, print job, etc.
  • information of the build can include a geometric feature density being processed by PBF system 200 , which may increase efficiency.
  • geometric feature density refers to the percentage of the active area that is being processed (e.g., fused) at any given time.
  • a high geometric feature density could include the situation in which a large portion of a build piece is in the active area and therefore a large portion of the active area is to be fused.
  • a high geometric feature density could include the situation in which many build pieces are being printed in the same print build, and the many build pieces come into the active area, requiring a large portion of the active area to be fused.
  • a low geometric feature density can refer to the opposite of these examples, i.e., the active area includes only a small portion of a single build piece or only a few of many build pieces.
  • the speed of rotation 202 can be increased when the geometric feature density related to build piece 219 or a print build is low and decreased when the feature density related to the build piece or the print build is high.
  • the energy beam(s) e.g., lasers, can be continuously kept working at or near full capacity.
  • PBF system 200 may enable a more efficient thermal management strategy by decreasing the time between powder deposition and printing and/or reducing the time inefficiencies between layers.
  • the rotational speed can be changed based on thermal management strategies, build densities, materials being fused, and/or other variables.
  • This change in rotational speed can be done globally, e.g., for an entire component, or locally, e.g., for certain parts of a component build, which may increase the efficiency of the build process.
  • the build piece 219 volume may be further segmented in PBF system 200 to achieve various build optimization goals, such as processing under different conditions, use of different optics, etc., because of the more continuous printing process enabled by the present disclosure.
  • PBF system 200 can be configured to support more efficient printing.
  • gas extraction strategies can be tailored to the specific optics strategy for material processing occurring in a given sector. For example, parts with lots of thin areas, such as a heat exchanger or a heavily lattice-based structure, will have little use for optics that can de-focus and apply a wide beam profile; efforts may be better spent on agile optics with the necessary feature resolution.
  • thick-walled parts with relatively lower surface area density can be efficiently processed using zoom/de-focus strategies.
  • PBF system 200 may enable additional design geometries that were previously unattainable with PBF system 100 of the related art. By reducing any non-exposure time between layers, PBF system 200 of the present disclosure may be more efficient. Further, PBF system 200 may be able to dynamically change its rotation speed for various portions of the printing process, which may also increase printing efficiency.
  • Build floor 201 may have a rotational motion or rotate such that the platform depth 250 of build floor 201 moves in a downward direction, and may move at any rate. For example, build floor 201 may move between 5 microns and 5000 microns per minute, between 50 and 500 microns per minute, between 100 and 150 microns per minute, or any rate desired, without departing from the scope of the present disclosure.
  • the distance from the powder surface to the optics may also be reduced. This may be achieved by reducing the incidence angle and/or the operating region of each laser, using a build volume segmenting approach and to enable optic arrangements that are more compact (i.e., offset, slightly angled, etc.). Reducing this distance may also allow other benefits, such as reducing the volume of the build chamber, reducing the volume of inert gas, reducing the pumping power, potentially creating more laminar flow to improve performance, etc.
  • platform knife 223 and powder egress holes 215 are positioned below the build depth 253 of PBF system 200 to remove powder from PBF system 200 and build piece 219 from build floor 201 .
  • any seals placed on build floor 201 can be positioned such that there is minimal contact between the seals and powder egress holes.
  • platform knife 223 can be oriented or dynamically changed to operate within the pitch of the rotational screw pitch used to rotate build floor 201 .
  • FIG. 3 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • PBF system 300 may comprise a build plate 302 , a powder bed receptacle wall 304 , a depositor 306 , and a gas flow system that includes one or more gas inlets 308 and an extractor 310 .
  • Active area 312 is shown to indicate the area for energy beams, e.g., lasers, etc. to sinter or fuse powder deposited by depositor 306 .
  • depositor 306 (which may include a leveler to level the powder level) deposits a layer of powder
  • build plate 302 rotates in direction 314 , and the layer of powder deposited by depositor 306 is exposed in active area 312 .
  • One or more energy beams then fuse or sinter the powder in active area 312 to form a layer of a build piece.
  • the gas inlet 308 may provide gases, such as inert gases, as a gas flow, to remove the byproducts created by the energy beams operating in active area 312 . These gases can be directed toward extractor 310 , which may remove the byproducts and/or gases provided by gas inlet 308 , from the active area 312 .
  • the gas flow system can direct the gas flow substantially parallel to the radius of the rotational motion, i.e., substantially orthogonal to the direction of rotation.
  • gas flow in and around the active area 312 can be controlled by controlling the rate and amount of gas flow from gas inlet 308 and removal of gases by extractor 310 , which may reduce the impact of soot, byproducts of the fusing process, splatter, etc. from affecting the printing process. Further, meltpool vectors of fusing performed in the active area 312 can be controlled to be in a direction preferable to the gas flow.
  • gas inlet 308 and extractor 310 may provide a gas flow system for PBF system 300 .
  • Gas inlet 308 may be disposed or located around the build plate 302
  • extractor 310 may be disposed or located at or near an axis of rotation of the build plate 302 .
  • Gas inlet 308 may collectively surround the build plate 302 .
  • Such a gas flow system may allow for the flow of introduced gases across active area 312 , removal of soot, fumes, spatter, and/or other byproducts of the build process from the active area 312 , other gas flow controls, or any combination thereof, without departing from the scope of the present disclosure.
  • Such a gas flow may be linear, rotated, or otherwise controlled to provide a desired gas flow across active area 312 .
  • FIG. 4 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • PBF system 400 may comprise a build plate 402 , a powder bed receptacle wall 404 , a depositor 406 , and a gas flow system that includes one or more gas inlets 408 and an extractor 410 .
  • Active area 412 is shown to indicate the area for energy beams, e.g., lasers, etc. to sinter or fuse powder deposited by depositor 406 .
  • depositor 406 , extractor 410 , and active area 412 may rotate or move in an arc motion with respect to the build plate 402 .
  • depositor 406 which may include a leveler to level the powder level
  • the depositor 406 , extractor 410 , and active area 412 rotate in direction 414 , and the layer of powder deposited by depositor 406 is exposed in active area 412 .
  • Energy beams then fuse or sinter the powder in active area 412 .
  • Other combination of rotational motions and/or stationary portions of PBF system 300 are possible without departing from the scope of the present disclosure.
  • the gas inlet 408 may provide gases, such as inert gases, or a gas flow, to remove the byproducts created by the energy beams operating in active area 412 . These gases can be directed toward extractor 410 , and may be located in powder bed receptacle wall 404 , to help remove the byproducts and/or gases provided by gas inlet 408 , from the active area 412 .
  • gas flow in and around the active area 412 can be controlled by controlling the rate and amount of gas flow from gas inlet 408 and removal of gases by extractor 410 , which may reduce the impact of soot, byproducts of the fusing process, splatter, etc. from affecting the printing process.
  • meltpool vectors of fusing performed in the active area 412 can be controlled to be in a direction preferable to the gas flow.
  • gas inlet 408 and extractor 410 may provide a gas flow system for PBF system 400 .
  • Gas inlet 408 may be disposed or located around the build plate 302
  • extractor 310 may be disposed or located at or near an axis of rotation of the build plate 302 .
  • Gas inlet 308 may collectively surround the build plate 302 .
  • Such a gas flow system may allow for the flow of introduced gases across active area 312 , removal of soot, fumes, spatter, and/or other byproducts of the build process from the active area 312 , other gas flow controls, or any combination thereof, without departing from the scope of the present disclosure.
  • a cover 416 may be provided over some or all of the build plate 402 .
  • the remainder of the print/build area may be covered with cover 416 to protect the powder bed from spatter and/or other byproducts from the printing process.
  • the cover 416 may be heated, e.g., may include heating elements on the underside of the cover, facing the powder bed to control cooling of the fused powder.
  • a portion of the cover 416 may be configured to heat up the deposited powder before fusing in the active area 412 .
  • sensors can be positioned above the bed to, for example, detect defects in the build piece or other characteristics of the powder, build piece, or other conditions.
  • eddy current sensors may be used. If a defect is detected, an area within the active area 412 can be a dedicated remelting area. In this case, for example, another energy beam(s) can expose this “remelt” area to remelt portions of the build piece that the sensor(s) detected a defect, such as a crack.
  • Sensors may be included in cover 416 , for example.
  • FIG. 5 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • PBF system 500 may comprise a build plate 502 , a powder bed receptacle wall 504 , a depositor 506 , and a gas flow system that includes one or more gas inlets 508 and an extractor 510 .
  • Active area 512 is shown to indicate the area for energy beams, e.g., lasers, etc. to sinter or fuse powder deposited by depositor 506 .
  • gas inlets 508 may be located in powder bed receptacle wall 504 , and extractor 510 may direct the flow of gas from gas inlets 508 across the active area 512 as shown by arrows 514 .
  • build plate 502 may rotate in direction 516 .
  • depositor 506 , extractor 510 , and active area 512 may rotate. After depositor 506 (which may include a leveler to level the powder level) deposits a layer of powder, the depositor 506 , extractor 510 , and active area 512 rotate in direction 516 , and the layer of powder deposited by depositor 506 is exposed in active area 512 . Energy beams then fuse or sinter the powder in active area 512 .
  • build plate 502 and extractor 510 may rotate.
  • extractor 510 may direct gas from gas inlets 508 along extractor and across active area 512 , or other areas of the deposited powder, as desired.
  • the gas flow system can direct the gas flow substantially parallel to the radius of the rotational motion, i.e., substantially orthogonal to the direction of rotation.
  • the gas inlet 508 may provide gases, such as inert gases, or a gas flow, to remove the byproducts created by the energy beams operating in active area 512 . These gases can be directed toward extractor 510 .
  • gas inlets 508 may be located in powder bed receptacle wall 504 , and extractor 510 may be configured to help remove the byproducts and/or gases provided by gas inlet 508 from the active area 512 .
  • gas flow in and around the active area 512 can be controlled by controlling the rate and amount of gas flow from gas inlet 508 and removal of gases by extractor 510 , which may reduce the impact of soot, byproducts of the fusing process, splatter, etc. from affecting the printing process. Further, meltpool vectors of fusing performed in the active area 512 can be controlled to be in a direction preferable to the gas flow.
  • FIG. 6 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • PBF system 600 may include a powder bed receptacle wall 602 , which may enclose a depositor 604 and, optionally, a full width depositor system 606 .
  • Full width depositor system 606 may be considered to include two depositors because it deposits powder in two separate locations.
  • a gas flow system may include a gas inlet 618 , an extractor 1 ( 614 ), and an extractor 2 ( 616 ).
  • Each active area 610 and 612 may have an independent extractor, e.g., extractor 1 614 for active area 1 610 and extractor 2 616 for active area 2 612 .
  • Active area 1 610 and active area 2 612 may be overlapping or non-overlapping.
  • Depositor 604 and depositor system 606 may deposit powder simultaneously or at different times as desired.
  • multiple active areas may have independent gas streams from various gas inlets 618 , optics, and/or operated in conjunction to increase the print speed of a given part.
  • the flexibility to rapidly print some portions of a given part, and slowly print other sections within the same “slice”, may increase the production efficiency of the overall part.
  • gas inlets 618 which are shown as being imbedded in powder bed receptacle wall 602 , may be provided as part of extractor 1 612 , extractor 2 614 , or as a separate system.
  • PBF system 600 can allow the layer thickness of the fused deposited powder to be varied during a build of the build piece.
  • a full-width depositor system 606 is used, so that powder is deposited in two locations that are 180 degrees apart (i.e., the left side and right side as viewed in FIG. 6 ).
  • the build plate is lowered 100 ⁇ m per full rotation, therefore each side of full-width depositor system 606 deposits a 50 ⁇ m layer of powder.
  • the layer thickness that is fused can be selected as either 50 ⁇ m or 100 ⁇ m by choosing to fuse either in both active areas or in a single active area, respectively.
  • PBF system 600 may determine that a first portion of a build piece, e.g., near the outside edges, is to be printed at the finer resolution of 50 ⁇ m so the finished build piece will have smoother walls. However, PBF system 600 may determine that a second portion of the build piece, e.g., the interior, or bulk of the build piece, can be printed at the lower resolution of 100 ⁇ m. Therefore, PBF system 600 can select to fuse the first portion of the build piece by fusing in both active area 1 ( 610 ) and active area 2 ( 612 ). In other words, the portion of the build piece near the outside edges will be formed by fusing a 50 ⁇ m layer of powder twice per rotation.
  • PBF system 600 can select to fuse the second portion of the build piece by fusing in only a single active area, e.g., active area 2 ( 612 ).
  • active area 2 e.g., active area 2 ( 612 ).
  • the interior, bulk portion of the build piece will be formed by fusing a 100 ⁇ m layer of powder once per rotation.
  • the time spent actively scanning the lower resolution portions of the build piece can be cut in half, which can allow faster build times because the speed of the rotation can be increased and/or more build pieces may be printed in the same build job.
  • example layer thicknesses of 50 ⁇ m and 100 ⁇ m are used as examples, it is understood that this example embodiment using a full-width depositor (e.g., two depositors 180 degrees apart) can provide a selection of fusing two layer thicknesses, in general, that are X and 2 ⁇ thicknesses, i.e., a given thickness and double the given thickness.
  • the example embodiment of FIG. 6 can include a full-width depositor system 606 (depositing twice at 180 degrees apart), but other embodiments may include other configurations of depositors, as one skilled in the art will readily recognize. For example, three depositors that are each 120 degrees apart and three corresponding active areas could be used. In this example, if the build plate is lowered 100 ⁇ m in one a full rotation, the fused layer thicknesses can be selected among 33.3 82 m, 66.6 ⁇ m, and 100 ⁇ m by fusing every active area (three times per rotation), every other active area (alternating once and twice per rotation), or every third active area (once per rotation), respectively.
  • FIG. 7 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • PBF system 700 may comprise a build plate 702 , a powder bed receptacle wall 704 , a depositor 706 , and a gas flow system that includes one or more gas inlets 708 , and an extractor 710 , and an exhaust manifold 714 .
  • Active area 712 is shown to indicate the area for energy beams, e.g., lasers, etc. to sinter or fuse powder deposited by depositor 706 .
  • FIG. 7 illustrates an aspect of the present disclosure where extractor 710 may direct a gas flow from gas inlet 708 through and/or across extractor 710 , while exhaust manifold 714 may remove additional fumes, soot, and/or other byproducts from the sintering or fusing process performed by the energy beam(s) impinging on the powder bed deposited on build plate 702 . While extractor 710 may remove some of the fumes, soot, and/or other by products, the gas flow from gas inlet(s) 708 and gas flow through extractor 710 may not be positioned properly to remove enough byproducts, or the byproducts may still be emitting from the melt pools after rotation of the build plate 702 in direction 716 .
  • exhaust manifold 714 may be used to remove additional fumes, soot, and/or other byproducts from the PBF system 700 , which may increase the efficiency of PBF system 700 .
  • the gas flow system can direct the gas flow substantially parallel to the radius of the rotational motion, i.e., substantially orthogonal to the direction of rotation.
  • depositor 706 , extractor 710 , and active area 712 may rotate.
  • depositor 706 (which may include a leveler to level the powder level) deposits a layer of powder
  • the depositor 706 , extractor 710 , and active area 712 rotate in direction 716 , and the layer of powder deposited by depositor 706 is exposed in active area 712 .
  • Energy beams then fuse or sinter the powder in active area 712 .
  • the gas flow system may be rotating as well, such that gas inlets 708 may be configured such that gas flows only in select areas, e.g., across active area 712 that is being processed by the energy beam.
  • This selective gas flow may mitigate soot and other components formed during the fusion process from contaminating the inactive areas of the build plate, as the gas flow would be constrained.
  • the rotational speed of the build plate 702 , and/or the rotation of the above-the-bed systems, may be synchronized with the opening and closing of gas inlets 708 to allow for selection of variable gas flows across active area 712 and/or other areas within PBF system 700 .
  • gas flow in and around the active area 712 can be controlled by controlling the rate and amount of gas flow from gas inlet 708 and removal of gases by extractor 710 , as well as removal of gases through exhaust manifold 714 , which may reduce the impact of soot, byproducts of the fusing process, splatter, etc. from affecting the printing process.
  • meltpool vectors of fusing performed in the active area 712 can be controlled to be in a direction preferable to the gas flow.
  • FIG. 8 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • PBF system 800 may comprise a build plate 802 , a powder bed receptacle wall 804 , a depositor 806 , and a gas flow system that includes a gas inlet 808 and an extractor 810 .
  • Active area 812 is shown to indicate the area for energy beams, e.g., lasers, etc. to sinter or fuse powder deposited by depositor 806 .
  • Active area 812 has two powder motion boundaries 813 and two non-powder motion boundaries 815 . Powder motion boundaries are boundaries of an active area across which the underlying powder layer moves, and non-powder motion boundaries are boundaries of an active area across which underlying powder does not move.
  • the gas flow system components i.e., gas inlet 808 and extractor 810
  • the active area may be, for example, an arc area of less than 45 degrees, 40 degrees, 35 degrees, 30 degrees, 25 degrees, 20 degrees, 15 degrees, 10 degrees, 5 degrees, or 3 degrees.
  • the powder motion boundaries 813 are radial boundaries of the active area with respect to the rotational motion
  • the non-powder motion boundaries 815 are circumferential boundaries (an inner circumference and an outer circumference) with respect to the rotational motion.
  • the gas flow system can direct the gas flow substantially parallel to the direction of rotation, i.e., substantially orthogonal to the radius of the rotational motion.
  • the gas flow systems position the gas inlet(s) and extractors substantially at the non-powder motion boundaries (not expressly marked in the figures, but readily understandable to one skilled in the art).
  • depositor 806 may be placed anywhere within the PBF system 800 that is not interfering with the gas flow system or the active area, and is not necessarily adjacent to active area 812 . Similar configurations where the depositor may be configured anywhere within the PBF system may be employed with respect to any PBF system described herein without departing from the scope of the present disclosure.
  • gas inlet 808 may be configured to direct gas flow 814 across active area 812 in a direction other than from the powder bed receptacle wall 804 towards the center of PBF system 800 .
  • a gas inlet and an extractor may be configured to direct the gas flow at other angles, or at variable angles, or rotate or otherwise direct the gas flow depending on the material being processed by PBF system 800 .
  • FIG. 9 shows a perspective view of an extractor in accordance with an aspect of the present disclosure.
  • extractor 810 may remove build byproducts 900 , e.g., soot, fumes, spatter, etc. from active area 812 .
  • Build byproducts may be created when energy beam 902 impinges upon powder such that the powder is sintered or fused.
  • extractor 810 may be configured to have a height, width, and/or shape such that build byproducts 900 are captured within extractor 810 instead of being re-deposited on the powder layer, whether processed or unprocessed.
  • extractor 810 may take on a funnel shape as shown, or any shape such that the gases are removed. Removal of build byproducts 900 from the powder layer on the build plate may increase the repeatability of the build process.
  • FIG. 10 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • PBF system 1000 may comprise a cover 1002 (that can cover the powder bed in areas other than the active area and where the depositor deposits powder), a powder bed receptacle wall 1004 , a depositor 1006 , and a gas flow system including a gas inlet 1008 and an extractor 1010 .
  • Active area 1012 is shown to indicate the area for energy beams, e.g., lasers, etc. to sinter or fuse powder deposited by depositor 1006 .
  • a build plate (which may be similar to those shown in FIGS. 2-8 ) receives powder deposited by depositor 1006 and rotates in direction 1014 to expose different areas of deposited powder in active area 1012 .
  • cover 1002 may protect the underlying powder bed and/or already fused/sintered portions of the component being built from spatter, soot, etc.
  • cover 1002 may include one or more heating elements, i.e. pre-heating elements 1016 , to pre-heat the powder bed.
  • Cover 1002 may also optionally include one or more elements, i.e., controlled cooling element 1018 , to control cooling of the fused powder after fusing within the active area 1012 .
  • Such cooling elements may be coupled to the cover 1002 such that elements 1016 and/or 1018 face the build plate and powder bed.
  • one or more pre-heating elements 1016 may be used to heat a portion of the powder bed prior to that portion entering the active area 1012 .
  • one or more controlled cooling elements 1018 may create a thermal gradient having a high starting temperature and a steadily reducing temperature to control the cooling of the fused portions of the component as the powder bed rotates away from the active area 1012 .
  • Cover 1002 may include various openings, e.g., such that active area 1012 is able to receive energy beams from one or more energy sources, an opening for depositor 1006 to deposit powder, openings for extractor 1010 to extract gases or byproducts of the build process, etc.
  • Cover 1002 may also include other components, e.g., temperature sensors, cameras, etc. to monitor the build process.
  • pre-heating element 1016 and/or controlled cooling element 1018 may not be a heater, but may be a camera, eddy current sensor, etc. to assist in the build process, e.g., detect defects in the built piece, monitor powder layer deposition, etc.
  • the PBF system 1000 may include an additional active area (not shown) to be a dedicated repair area, while other areas may be continuing to build, or multiple active areas can be assigned various tasks as described with respect to FIG. 6 . For example, if a defect (such as a void or crack) in the build piece is detected by a sensor, the additional active area may be used to re-melt the area of the defect in order to fix the defect.
  • the build plate and powder/fused portion of the component may not rotate, but the “above the bed” systems can rotate.
  • the depositor(s), energy beam(s) system, gas flow system, sensor(s), etc. e.g., the devices and systems “above the bed”, can rotate at the same rate, such that they remain fixed relative to each other.
  • the build chamber may include channels for gas inlets and outlets.
  • FIG. 11 illustrates a flowchart of an example method of additively manufacturing a build piece according to various embodiments.
  • the example method includes controlling a depositor system ( 1101 ) to deposit a layer of powder onto a build floor, controlling a motor system ( 1102 ) to cause a rotational motion between the depositor system and the build floor, such that the depositor system deposits the layer of powder during the rotational motion, and a receptacle wall contains the powder on the build floor, controlling an energy beam source ( 1103 ) to apply an energy beam in an active area of the layer of powder to selectively fuse a portion of the powder in the active area to form a portion of a build piece, and controlling a gas flow system ( 1104 ) to provide a gas flow across the active area while the energy beam selectively fuses the portion of the layer of powder in the active area.
  • a depositor system 1101
  • a motor system 1102
  • a rotational motion between the depositor system and the build floor such that the depositor system deposits the layer of powder
  • Controlling the motor system ( 1102 ) may be implemented by causing the rotational motion at least in part by rotating the build floor, and the depositor system may remain stationary during the rotational motion. Controlling the motor system ( 1102 ) may be implemented by causing the rotational motion at least in part by moving the depositor system in an arc over the build floor. The receptacle wall may be configured to remain stationary during the rotational motion. Controlling the gas flow system ( 1104 ) may extract a gas created by the fusing of the powder, as described above.
  • the depositor system may include a plurality of depositors, and controlling the depositor system ( 1101 ) may include depositing a plurality of layers of powder simultaneously.
  • the method can include one or more optional actions ( 1105 ), which is depicted as a dashed box in FIG. 11 to signify optionality.
  • an optional action ( 1105 ) may include covering a second area of the powder exclusive of the active area with a cover. In this way, for example, spatter, soot, etc. from the fusing may be prevented from falling onto portions of the powder bed or build piece.
  • Another optional action ( 1105 ) may include controlling a heater configured to heat the powder under the cover, the heater being arranged in the cover.
  • Another optional action ( 1105 ) may include controlling a sensor to sense a characteristic of the powder under the cover, wherein the sensor is arranged in the cover.
  • controlling the gas flow system ( 1104 ) may include controlling a gas extractor arranged adjacent to a first boundary of the active area, the gas extractor being controlled to extract the gas flow, and may further include controlling a gas inlet arranged adjacent to a second boundary of the active area, the gas inlet being controlled to provide the gas flow.
  • Controlling the gas flow system ( 1104 ) may include controlling a gas extractor arranged at an axis of rotation of the rotational motion, the gas extractor being controlled to extract the gas flow.
  • Controlling the gas flow system ( 1104 ) may further include controlling a gas inlet arranged at a portion of the receptacle wall, the gas inlet being controlled to provide the gas flow, and the gas inlet may include a plurality of openings that collectively surround the build floor.
  • the energy beam source may include one or more energy beam generators
  • controlling the energy beam source ( 1103 ) may include applying one or more energy beams in a plurality of active areas of the layer of powder to selectively fuse a portion of the powder in each of the active areas
  • controlling the gas flow system ( 1104 ) may include providing a gas flow across each of the active areas while the one or more energy beams selectively fuse the portion of the powder in each active area.
  • the active areas may be non-overlapping.
  • the gas flow system may include a funnel-type gas manifold.
  • controlling the gas flow system ( 1104 ) may include rotating a direction of the gas flow.
  • the gas flow system may include a plurality of gas inlets and a plurality of gas extractors, and controlling the gas flow system ( 1104 ) may include rotating the gas flow by opening and closing the gas inlets and the gas extractors.
  • an optional action ( 1105 ) may include varying a layer thickness of the selectively fused deposited powder during a build of the build piece.
  • this optional action may further include obtaining information of a geometric feature density, and controlling the motor system ( 1102 ) may include varying a speed of the rotational motion based on the geometric feature density.
  • FIG. 12 illustrates a flowchart of an example method of additively manufacturing a build piece according to various embodiments.
  • the example method includes obtaining information ( 1201 ) of a build including a build piece, controlling a depositor system ( 1202 ) to deposit a layer of powder onto a build floor, controlling a motor system ( 1203 ) to cause a rotational motion between the depositor system and the build floor, such that the depositor system deposits the layer of powder during the rotational motion, and a receptacle wall contains the powder on the build floor, where controlling the motor system ( 1203 ) further includes varying a speed of the rotational motion based on the information of the build during the build of the build piece, and controlling an energy beam source ( 1204 ) to apply an energy beam in an active area of the layer of powder to selectively fuse a portion of the powder in the active area to form a portion of the build piece.
  • an energy beam source 1204
  • the information of the build may include a geometric feature density
  • controlling the motor system ( 1202 ) may include varying the speed based on the geometric feature density.
  • varying the speed of the rotational motion may include increasing the speed when the geometric feature density is low and decreasing the speed when the geometric feature density is high. In this way, for example, an active time of the energy beam source can be used more efficiently and the build time of the build can be reduced.
  • controlling the motor system ( 1203 ) may cause the rotational motion at least in part by rotating the build floor.
  • the depositor system may be configured to remain stationary during the rotational motion.
  • controlling the motor system ( 1203 ) may cause the rotational motion at least in part by moving the depositor system in an arc over the build floor.
  • the receptacle wall may be configured to remain stationary during the rotational motion.
  • the receptacle wall may be configured to rotate with the build floor.
  • the depositor system may include a plurality of depositors, and controlling the depositor system ( 1202 ) may include depositing a plurality of layers of powder simultaneously.
  • the method can include one or more optional actions ( 1205 ), which is depicted as a dashed box in FIG. 12 to signify optionality.
  • the method may include an optional action ( 1205 ) of controlling a gas flow system to extract a gas created by the fusing of the powder.
  • the method may include an optional action ( 1205 ) of covering a second area of the powder exclusive of the active area with a cover. In this way, for example, spatter, soot, etc. from the fusing may be prevented from falling onto portions of the powder bed or build piece.
  • Another optional action ( 1205 ) may include controlling a heater configured to heat the powder under the cover, the heater being arranged in the cover.
  • Another optional action ( 1205 ) may include controlling a sensor to sense a characteristic of the powder under the cover, wherein the sensor is arranged in the cover.
  • Another optional action ( 1205 ) may include controlling a gas flow system.
  • a gas flow system may include a gas extractor arranged adjacent to a first boundary of the active area, the gas extractor being controlled to extract a gas flow.
  • the gas flow system may include a gas inlet arranged adjacent to a second boundary of the active area, and controlling the gas flow system may further include controlling the gas inlet to provide the gas flow.
  • Controlling a gas flow system may include controlling a gas extractor arranged at an axis of rotation of the rotational motion, wherein the gas extractor is controlled to extract a gas flow.
  • the gas flow system may include a gas inlet arranged at a portion of the receptacle wall, and controlling the gas flow system may include controlling the gas inlet to provide the gas flow.
  • the gas inlet may include a plurality of openings that collectively surround the build floor.
  • the energy beam source may include one or more energy beam generators
  • controlling the energy beam source 1204
  • controlling the energy beam source 1204
  • an optional action 1205
  • controlling a gas flow system to provide a gas flow across each of the active areas while the one or more energy beams selectively fuse the portion of the powder in each active area.
  • the active areas may be non-overlapping.
  • controlling the gas flow system may include controlling a plurality of gas inlets and a plurality of gas extractors such that the gas flow system rotates the gas flow by opening and closing the gas inlets and the gas extractors.
  • An optional action ( 1205 ) may include varying a layer thickness of the selectively fused deposited powder during a build of the build piece.
  • FIG. 13 illustrates a flowchart of an example method of additively manufacturing a build piece according to various embodiments.
  • the example method includes controlling a depositor system ( 1301 ) to deposit a layer of powder onto a build floor, controlling a motor system ( 1302 ) to cause a rotational motion between the depositor system and the build floor, such that the depositor system deposits the layer of powder during the rotational motion, and a receptacle wall contains the powder on the build floor, controlling an energy beam source ( 1303 ) to apply an energy beam in an active area of the layer of powder to selectively fuse a portion of the powder in the active area to form a portion of a build piece, and varying a layer thickness ( 1304 ) of the selectively fused deposited powder during a build of the build piece.
  • the depositor system may include a plurality of depositors, and controlling the depositor system ( 1301 ) may include controlling the plurality of depositors to deposit layers of powder simultaneously.
  • the active area may include a plurality of active areas, each arranged after a different depositor of the plurality of depositors.
  • a first depositor in the plurality of depositors may be arranged 180 degrees apart from a second depositor with respect to the rotational motion, the first depositor may be associated with a first active area of the plurality of active areas arranged after the first depositor, and the second depositor may be associated with a second active area of the plurality of active areas arranged after the second depositor.
  • Varying the layer thickness ( 1304 ) of the selectively fused deposited powder may include controlling the energy beam source to fuse some portions of the powder layer in both the first and second active areas and to fuse other portions of the powder layer in only the first or second active area.
  • controlling the energy beam source ( 1303 ) may include fusing a portion of the build piece near the edge of the build piece by fusing in both the first and second active areas, and fusing a portion of the build piece in the interior bulk of the build piece in only the first or second active area.
  • Controlling the energy beam source ( 1303 ) may include applying a plurality of energy beams simultaneously in the plurality of active areas.
  • controlling the motor system ( 1302 ) may cause the rotational motion at least in part by rotating the build floor.
  • the depositor system may be configured to remain stationary during the rotational motion.
  • controlling the motor system ( 1302 ) may cause the rotational motion at least in part by moving the depositor system in an arc over the build floor.
  • the receptacle wall may be configured to remain stationary during the rotational motion.
  • the method can include one or more optional actions ( 1305 ), which is depicted as a dashed box in FIG. 13 to signify optionality.
  • an optional action ( 1305 ) may include controlling a gas flow system to provide a gas flow across the active area. The gas flow system may extract a gas created by the fusing of the powder.
  • Another optional action ( 1305 ) may include covering a second area of the powder exclusive of the active area with a cover.
  • Another optional action ( 1305 ) may include controlling a heater to heat the powder under the cover, the heater being arranged in the cover.
  • Another optional action ( 1305 ) may include controlling a sensor to sense a characteristic of the powder under the cover, the sensor being arranged in the cover.
  • an optional action may include controlling a gas flow system to provide a gas flow across one or more active areas.
  • the gas flow system may include a gas extractor arranged adjacent to a first boundary of the active area, such that gas extractor extracts a gas flow.
  • the gas flow system may include a gas inlet arranged adjacent to a second boundary of the active area, the gas inlet being configured to provide the gas flow.
  • a gas flow system may include a gas extractor arranged at an axis of rotation of the rotational motion, such that the gas extractor extracts a gas flow.
  • a gas flow system may include a gas inlet arranged at a portion of the receptacle wall, the gas inlet being configured to provide the gas flow.
  • the gas inlet may include a plurality of openings that collectively surround the build floor.
  • the energy beam source may include one or more energy beam generators
  • controlling the energy beam source may include applying one or more energy beams in a plurality of active areas of the layer of powder to selectively fuse a portion of the powder in each of the active areas
  • an optional action may include controlling a gas flow system to provide a gas flow across each of the active areas while the one or more energy beams selectively fuse the portion of the powder in each active area.
  • the active areas may be non-overlapping.
  • a gas flow system may include a funnel-type gas manifold to provide a gas flow across the active area. Controlling a gas flow system may include rotating a direction of a gas flow across the active area.
  • the gas flow system may include a plurality of gas inlets and a plurality of gas extractors, and controlling the gas flow system may include rotating the gas flow by opening and closing the gas inlets and the gas extractors.
  • an optional action ( 1305 ) may include varying a speed of the rotational motion based on a geometric feature density.

Abstract

Systems and methods for rotational additive manufacturing are disclosed. An apparatus in accordance with an aspect of the present disclosure comprises a build floor, a depositor system configured to deposit a layer of powder onto the build floor, a motor system causing a rotational motion between the depositor system and the build floor, wherein the depositor system deposits the layer of powder during the rotational motion, a receptacle wall configured to contain the powder on the build floor, an energy beam source configured to apply an energy beam in an active area of the layer of powder to selectively fuse a portion of the powder in the active area to form a portion of a build piece and a gas flow system configured to provide a gas flow across the active area while the energy beam selectively fuses the portion of the layer of powder in the active area.

Description

    CROSS REFERENCE TO RELATED APPLICATION(S)
  • This application claims the benefit of U.S. Provisional Application Ser. No. 63/158,765, entitled “CONTINUOUS ROTATIONAL ADDITIVE MANUFACTURING SYSTEM ARCHITECTURE” and filed on Mar. 9, 2021, the disclosure of which is expressly incorporated by reference herein in its entirety.
  • BACKGROUND Field
  • The present disclosure relates generally to additive manufacturing, and more specifically to a rotational additive manufacturing systems and methods.
  • Description of the Related Art
  • Three-dimensional (3-D) printing, also referred to as additive manufacturing (AM), has recently presented new opportunities to more efficiently build complex transport structures, such as automobiles, aircraft, boats, motorcycles, busses, trains, and the like. AM techniques are capable of fabricating complex components from a wide variety of materials. Applying AM processes to industries that produce these products has proven to produce a structurally more efficient transport structure. For example, an automobile produced using 3-D printed components can be made stronger, lighter, and consequently, more fuel efficient. Moreover, AM enables manufacturers to 3-D print components that are much more complex and that are equipped with more advanced features and capabilities than components made via traditional machining and casting techniques. The 3-D objects may be formed using layers of material based on a digital model data of the object. A 3-D printer may form the structure defined by the digital model data by printing the structure one layer at a time.
  • A 3-D printer may deposit a powder layer (e.g., powdered metal) on an operating surface. The 3-D printer may then consolidate particular areas of the powder layer into a layer of the object, e.g., by using a laser to melt or sinter the powder of the powder layer together. The steps may be repeated to sequentially form each layer. Accordingly, the 3-D printed object may be built layer by layer.
  • 3-D printing is non-design specific, which offers geometric and design flexibility that conventional manufacturing processes cannot. Furthermore, 3-D printing technologies can produce parts with small feature sizes and geometries that are either significantly difficult or impossible to produce using conventional manufacturing processes.
  • The AM process, however, can be time consuming. The time between printing one layer and depositing powder material for the next layer decreases the overall throughput of an AM system.
  • SUMMARY
  • Several aspects of apparatus for additive manufacturing systems and architectures will be described more fully hereinafter with reference to three-dimensional printing techniques.
  • An apparatus in accordance with an aspect of the present disclosure comprises a build floor, a depositor system configured to deposit a layer of powder onto the build floor, a motor system configured to cause a rotational motion between the depositor system and the build floor, wherein the depositor system deposits the layer of powder during the rotational motion, a receptacle wall configured to contain the powder on the build floor, an energy beam source configured to apply an energy beam in an active area (i.e., scan area) of the layer of powder to selectively fuse a portion of the powder in the active area to form a portion of a build piece, and a gas flow system configured to provide a gas flow across the active area while the energy beam selectively fuses the portion of the layer of powder in the active area.
  • Such an apparatus further optionally includes one or more of the following features: the motor system causing the rotational motion at least in part by rotating the build floor, the depositor system being configured to remain stationary during the rotational motion, the motor system causing the rotational motion at least in part by moving the depositor system in an arc over the build floor, the receptacle wall being configured to remain stationary during the rotational motion, the gas flow system extracting a gas created by the fusing of the powder, a cover configured to cover a second area of the powder exclusive of the active area, the cover including a heater configured to heat the powder under the cover, and the cover including a sensor configured to sense a characteristic of the powder under the cover.
  • Such an apparatus may further optionally include one or more of the following features: the gas flow system including a gas extractor arranged adjacent to a first boundary of the active area, the gas extractor being configured to extract the gas flow, the gas flow system further including a gas inlet arranged adjacent to a second boundary of the active area, the gas inlet being configured to provide the gas flow, the gas flow system including a gas extractor arranged at an axis of rotation of the rotational motion, the gas extractor being configured to extract the gas flow, the gas flow system further including a gas inlet arranged at a portion of the receptacle wall, the gas inlet being configured to provide the gas flow, and the gas inlet including a plurality of openings that collectively surround the build floor.
  • Such an apparatus may further optionally include one or more of the following features: the energy beam source including one or more energy beam generators, the energy beam source being configured to apply one or more energy beams in a plurality of active areas of the layer of powder to selectively fuse a portion of the powder in each of the active areas, and the gas flow system being configured to provide a gas flow across each of the active areas while the one or more energy beams selectively fuse the portion of the powder in each active area, the active areas being non-overlapping, the gas flow system including a funnel-type gas manifold, the gas flow system being further configured to rotate a direction of the gas flow, the gas flow system including a plurality of gas inlets and a plurality of gas extractors, and the gas flow system rotating the gas flow by opening and closing the gas inlets and the gas extractors, a layer thickness of the selectively fused deposited powder being varied during a build of the build piece, a speed of the rotational motion being varied based on a geometric feature density, and the depositor system including a plurality of depositors, and the depositor system being configured to deposit a plurality of layers of powder simultaneously.
  • An apparatus in accordance with an aspect of the present disclosure comprises a build floor, a depositor system configured to deposit a layer of powder onto the build floor, a motor system configured to cause a rotational motion between the depositor system and the build floor, wherein the depositor system deposits the layer of powder during the rotational motion, a receptacle wall configured to contain the powder on the build floor, and an energy beam source configured to apply an energy beam in an active area of the layer of powder to selectively fuse a portion of the powder in the active area to form a portion of a build piece, wherein the motor system is further configured to vary a speed of the rotational motion based on information of a build including the build piece. In various embodiments, information of the build may include a geometric feature density.
  • Such an apparatus further optionally includes one or more of the following features: the motor system being configured to vary the speed by increasing the speed when the geometric feature density is lower and increasing the speed when the geometric feature density is higher, the motor system causing the rotational motion at least in part by rotating the build floor, the depositor system being configured to remain stationary during the rotational motion, the motor system causing the rotational motion at least in part by moving the depositor system in an arc over the build floor, the receptacle wall being configured to remain stationary during the rotational motion, the gas flow system extracting a gas created by the fusing of the powder, a cover configured to cover a second area of the powder exclusive of the active area, the cover including a heater configured to heat the powder under the cover, and the cover including a sensor configured to sense a characteristic of the powder under the cover.
  • Such an apparatus may further optionally include one or more of the following features: the gas flow system including a gas extractor arranged adjacent to a first boundary of the active area, the gas extractor being configured to extract the gas flow, the gas flow system further including a gas inlet arranged adjacent to a second boundary of the active area, the gas inlet being configured to provide the gas flow, the gas flow system including a gas extractor arranged at an axis of rotation of the rotational motion, the gas extractor being configured to extract the gas flow, the gas flow system further including a gas inlet arranged at a portion of the receptacle wall, the gas inlet being configured to provide the gas flow, and the gas inlet including a plurality of openings that collectively surround the build floor.
  • Such an apparatus may further optionally include one or more of the following features: the energy beam source including one or more energy beam generators, the energy beam source being configured to apply one or more energy beams in a plurality of active areas of the layer of powder to selectively fuse a portion of the powder in each of the active areas, and the gas flow system being configured to provide a gas flow across each of the active areas while the one or more energy beams selectively fuse the portion of the powder in each active area, the active areas being non-overlapping, the gas flow system including a funnel-type gas manifold, the gas flow system being further configured to rotate a direction of the gas flow, the gas flow system including a plurality of gas inlets and a plurality of gas extractors, and the gas flow system rotating the gas flow by opening and closing the gas inlets and the gas extractors, a layer thickness of the selectively fused deposited powder being varied during a build of the build piece, a speed of the rotational motion being varied based on a geometric feature density, and the depositor system including a plurality of depositors, and the depositor system being configured to deposit a plurality of layers of powder simultaneously.
  • An apparatus in accordance with an aspect of the present disclosure comprises a build floor, a depositor system configured to deposit a powder onto the build floor, a motor system configured to cause a rotational motion between the depositor system and the build floor, wherein the depositor system deposits the layer of powder during the rotational motion, a receptacle wall configured to contain the powder on the build floor, and an energy beam source configured to apply an energy beam in an active area of the layer of powder to selectively fuse a portion of the powder in the active area to form a portion of a build piece, wherein a layer thickness of the selectively fused deposited powder is varied during a build of the build piece.
  • Such an apparatus further optionally includes one or more of the following features: the depositor system includes a plurality of depositors, the active area includes a plurality of active areas, each arranged after a different depositor of the plurality of depositors, a first depositor in the plurality of depositors is arranged 180 degrees apart from a second depositor with respect to the rotational motion, wherein the first depositor is associated with a first active area of the plurality of active areas arranged after the first depositor, and the second depositor is associated with a second active area of the plurality of active areas arranged after the second depositor, the layer thickness of the selectively fused deposited powder is varied by the energy beam source fusing some portions of the powder layer in both the first and second active areas and fusing other portions of the powder layer in only the first or second active area, the energy beam source is configured to fuse a portion of the build piece near the edge of the build piece by fusing in both the first and second active areas, and is configured to fuse a portion of the build piece in the interior bulk of the build piece in only the first or second active area, the energy beam source is further configured to apply a plurality of energy beams simultaneously in the plurality of active areas.
  • Such an apparatus further optionally includes one or more of the following features: the depositor system including a plurality of depositors, the energy beam source including a plurality of energy beams and the active area including a plurality of active areas, a first depositor in the plurality of depositors depositing a first thickness of powder and a second depositor in the plurality of depositors depositing a second thickness of powder. a first energy beam in the plurality of energy beams fusing the first thickness of powder in a first active area in the plurality of active areas, a second energy beam in the plurality of energy beams fusing the second thickness of powder in a second active area in the plurality of active areas, and a first energy beam in the plurality of energy beams fusing the first thickness of powder and the second thickness of powder in a first active area in the plurality of active areas.
  • Such an apparatus further optionally includes one or more of the following features: the motor system causing the rotational motion at least in part by rotating the build floor, the depositor system being configured to remain stationary during the rotational motion, the motor system causing the rotational motion at least in part by moving the depositor system in an arc over the build floor, the receptacle wall being configured to remain stationary during the rotational motion, the gas flow system extracting a gas created by the fusing of the powder, a cover configured to cover a second area of the powder exclusive of the active area, the cover including a heater configured to heat the powder under the cover, and the cover including a sensor configured to sense a characteristic of the powder under the cover.
  • Such an apparatus may further optionally include one or more of the following features: the gas flow system including a gas extractor arranged adjacent to a first boundary of the active area, the gas extractor being configured to extract the gas flow, the gas flow system further including a gas inlet arranged adjacent to a second boundary of the active area, the gas inlet being configured to provide the gas flow, the gas flow system including a gas extractor arranged at an axis of rotation of the rotational motion, the gas extractor being configured to extract the gas flow, the gas flow system further including a gas inlet arranged at a portion of the receptacle wall, the gas inlet being configured to provide the gas flow, and the gas inlet including a plurality of openings that collectively surround the build floor.
  • Such an apparatus may further optionally include one or more of the following features: the energy beam source including one or more energy beam generators, the energy beam source being configured to apply one or more energy beams in a plurality of active areas of the layer of powder to selectively fuse a portion of the powder in each of the active areas, and the gas flow system being configured to provide a gas flow across each of the active areas while the one or more energy beams selectively fuse the portion of the powder in each active area, the active areas being non-overlapping, the gas flow system including a funnel-type gas manifold, the gas flow system being further configured to rotate a direction of the gas flow, the gas flow system including a plurality of gas inlets and a plurality of gas extractors, and the gas flow system rotating the gas flow by opening and closing the gas inlets and the gas extractors, a layer thickness of the selectively fused deposited powder being varied during a build of the build piece, a speed of the rotational motion being varied based on a geometric feature density.
  • A method in accordance with an aspect of the present disclosure comprises controlling a depositor system to deposit a layer of powder onto a build floor, controlling a motor system to cause a rotational motion between the depositor system and the build floor, wherein the depositor system deposits the layer of powder during the rotational motion, and a receptacle wall contains the powder on the build floor, controlling an energy beam source to apply an energy beam in an active area of the layer of powder to selectively fuse a portion of the powder in the active area to form a portion of a build piece, and controlling a gas flow system to provide a gas flow across the active area while the energy beam selectively fuses the portion of the layer of powder in the active area.
  • Such a method may further optionally include one or more of the following features: controlling the motor system causes the rotational motion at least in part by rotating the build floor, the depositor system is configured to remain stationary during the rotational motion, controlling the motor system causes the rotational motion at least in part by moving the depositor system in an arc over the build floor, the receptacle wall is configured to remain stationary during the rotational motion, controlling the gas flow system extracts a gas created by the fusing of the powder, covering a second area of the powder exclusive of the active area with a cover, controlling a heater configured to heat the powder under the cover, wherein the heater is arranged in the cover, controlling a sensor to sense a characteristic of the powder under the cover, wherein the sensor is arranged in the cover, controlling the gas flow system includes controlling a gas extractor arranged adjacent to a first boundary of the active area, the gas extractor being controlled to extract the gas flow, controlling the gas flow system further includes controlling a gas inlet arranged adjacent to a second boundary of the active area, the gas inlet being controlled to provide the gas flow, controlling the gas flow system includes controlling a gas extractor arranged at an axis of rotation of the rotational motion, the gas extractor being controlled to extract the gas flow, controlling the gas flow system further includes controlling a gas inlet arranged at a portion of the receptacle wall, the gas inlet being controlled to provide the gas flow, the gas inlet includes a plurality of openings that collectively surround the build floor, the energy beam source includes one or more energy beam generators, controlling the energy beam source includes applying one or more energy beams in a plurality of active areas of the layer of powder to selectively fuse a portion of the powder in each of the active areas, and controlling the gas flow system includes providing a gas flow across each of the active areas while the one or more energy beams selectively fuse the portion of the powder in each active area, the active areas are non-overlapping, the gas flow system includes a funnel-type gas manifold, controlling the gas flow system includes rotating a direction of the gas flow, the gas flow system includes a plurality of gas inlets and a plurality of gas extractors, and controlling the gas flow system includes rotating the gas flow by opening and closing the gas inlets and the gas extractors, varying a layer thickness of the selectively fused deposited powder during a build of the build piece, obtaining information of a geometric feature density, wherein controlling the motor system includes varying a speed of the rotational motion based on the geometric feature density, the depositor system includes a plurality of depositors, and controlling the depositor system includes depositing a plurality of layers of powder simultaneously.
  • A method in accordance with an aspect of the present disclosure comprises obtaining information of a build including a build piece, controlling a depositor system to deposit a layer of powder onto a build floor, controlling a motor system to cause a rotational motion between the depositor system and the build floor, wherein the depositor system deposits the layer of powder during the rotational motion, and a receptacle wall contains the powder on the build floor, wherein controlling the motor system further includes varying a speed of the rotational motion based on the information of the build during the build of the build piece, and controlling an energy beam source to apply an energy beam in an active area of the layer of powder to selectively fuse a portion of the powder in the active area to form a portion of the build piece.
  • Such a method may further optionally include one or more of the following features: the information of the build includes a geometric feature density, and controlling the motor system includes varying the speed based on the geometric feature density, controlling the motor system causes the rotational motion at least in part by rotating the build floor, the depositor system is configured to remain stationary during the rotational motion, controlling the motor system causes the rotational motion at least in part by moving the depositor system in an arc over the build floor, the receptacle wall is configured to remain stationary during the rotational motion, controlling a gas flow system to extract a gas created by the fusing of the powder, covering a second area of the powder exclusive of the active area with a cover, controlling a heater to heat the powder under the cover, wherein the heater is arranged in the cover, controlling a sensor to sense a characteristic of the powder under the cover, wherein the sensor is arranged in the cover, controlling a gas flow system including a gas extractor arranged adjacent to a first boundary of the active area, the gas extractor being controlled to extract a gas flow, the gas flow system further includes a gas inlet arranged adjacent to a second boundary of the active area, controlling the gas flow system further includes controlling the gas inlet to provide the gas flow, controlling a gas flow system including a gas extractor arranged at an axis of rotation of the rotational motion, wherein the gas extractor is controlled to extract a gas flow, the gas flow system further includes a gas inlet arranged at a portion of the receptacle wall, controlling the gas flow system further includes controlling the gas inlet to provide the gas flow, the gas inlet includes a plurality of openings that collectively surround the build floor, the energy beam source includes one or more energy beam generators, controlling the energy beam source includes applying one or more energy beams in a plurality of active areas of the layer of powder to selectively fuse a portion of the powder in each of the active areas, the method further comprising controlling a gas flow system to provide a gas flow across each of the active areas while the one or more energy beams selectively fuse the portion of the powder in each active area, the active areas are non-overlapping, the gas flow system includes a funnel-type gas manifold, controlling a gas flow system to rotate a direction of the gas flow across the active area, controlling the gas flow system includes controlling a plurality of gas inlets and a plurality of gas extractors such that the gas flow system rotates the gas flow by opening and closing the gas inlets and the gas extractors, varying a layer thickness of the selectively fused deposited powder during a build of the build piece, the information of the build includes a geometric feature density, and varying the speed of the rotational motion includes increasing the speed when the geometric feature density is low and decreasing the speed when the geometric feature density is high, the depositor system includes a plurality of depositors, and controlling the depositor system includes depositing a plurality of layers of powder simultaneously.
  • A method in accordance with an aspect of the present disclosure comprises controlling a depositor system to deposit a layer of powder onto a build floor, controlling a motor system to cause a rotational motion between the depositor system and the build floor, wherein the depositor system deposits the layer of powder during the rotational motion, and a receptacle wall contains the powder on the build floor, controlling an energy beam source to apply an energy beam in an active area of the layer of powder to selectively fuse a portion of the powder in the active area to form a portion of a build piece, and varying a layer thickness of the selectively fused deposited powder during a build of the build piece.
  • Such a method may further optionally include one or more of the following features: the depositor system includes a plurality of depositors, wherein controlling the depositor system includes controlling the plurality of depositors to deposit layers of powder simultaneously, the active area includes a plurality of active areas, each arranged after a different depositor of the plurality of depositors, a first depositor in the plurality of depositors is arranged 180 degrees apart from a second depositor with respect to the rotational motion, wherein the first depositor is associated with a first active area of the plurality of active areas arranged after the first depositor, and the second depositor is associated with a second active area of the plurality of active areas arranged after the second depositor, varying the layer thickness of the selectively fused deposited powder includes controlling the energy beam source to fuse some portions of the powder layer in both the first and second active areas and to fuse other portions of the powder layer in only the first or second active area, controlling the energy beam source includes fusing a portion of the build piece near the edge of the build piece by fusing in both the first and second active areas, and fusing a portion of the build piece in the interior bulk of the build piece in only the first or second active area, controlling the energy beam source further includes applying a plurality of energy beams simultaneously in the plurality of active areas, controlling the motor system causes the rotational motion at least in part by rotating the build floor, the depositor system is configured to remain stationary during the rotational motion, controlling the motor system causes the rotational motion at least in part by moving the depositor system in an arc over the build floor, the receptacle wall is configured to remain stationary during the rotational motion, controlling a gas flow system to provide a gas flow across the active area, the gas flow system extracts a gas created by the fusing of the powder, covering a second area of the powder exclusive of the active area with a cover, controlling a heater to heat the powder under the cover, wherein the heater is arranged in the cover, controlling a sensor to sense a characteristic of the powder under the cover, wherein the sensor is arranged in the cover, controlling a gas flow system including a gas extractor arranged adjacent to a first boundary of the active area, such that gas extractor extracts a gas flow, the gas flow system further includes a gas inlet arranged adjacent to a second boundary of the active area, the gas inlet being configured to provide the gas flow, controlling a gas flow system including a gas extractor arranged at an axis of rotation of the rotational motion, such that the gas extractor extracts a gas flow, the gas flow system further includes a gas inlet arranged at a portion of the receptacle wall, the gas inlet being configured to provide the gas flow, the gas inlet includes a plurality of openings that collectively surround the build floor, the energy beam source includes one or more energy beam generators, and controlling the energy beam source includes applying one or more energy beams in a plurality of active areas of the layer of powder to selectively fuse a portion of the powder in each of the active areas, and controlling a gas flow system to provide a gas flow across each of the active areas while the one or more energy beams selectively fuse the portion of the powder in each active area, the active areas are non-overlapping, controlling a gas flow system including a funnel-type gas manifold to provide a gas flow across the active area, controlling a gas flow system to rotate a direction of a gas flow across the active area, the gas flow system includes a plurality of gas inlets and a plurality of gas extractors, and controlling the gas flow system includes rotating the gas flow by opening and closing the gas inlets and the gas extractors, varying a speed of the rotational motion based on a geometric feature density.
  • It will be understood that other aspects of apparatuses for additive manufacturing systems will become readily apparent to those skilled in the art from the following detailed description, wherein it is shown and described only several embodiments by way of illustration. As will be realized by those skilled in the art, the apparatus for bridging is capable of other and different embodiments, and its several details are capable of modification in various other respects, all without departing from the scope of the present disclosure. Accordingly, the drawings and detailed description are to be regarded as illustrative in nature and not as restrictive.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • Various aspects of apparatus for additive manufacturing systems and methods will now be presented in the detailed description by way of example, and not by way of limitation, in the accompanying drawings, wherein:
  • FIGS. 1A-1D illustrate respective side views of an exemplary conventional PBF system during different stages of operation.
  • FIG. 1E illustrates a functional block diagram of a 3-D printer system.
  • FIG. 2 illustrates a side view of a printing system in accordance with an aspect of the present disclosure.
  • FIG. 3 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • FIG. 4 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • FIG. 5 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • FIG. 6 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • FIG. 7 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • FIG. 8 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • FIG. 9 shows a perspective view of an extractor in accordance with an aspect of the present disclosure.
  • FIG. 10 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • FIG. 11 illustrates an example method in accordance with an aspect of the present disclosure.
  • FIG. 12 illustrates another example method in accordance with an aspect of the present disclosure.
  • FIG. 13 illustrates another example method in accordance with an aspect of the present disclosure.
  • DETAILED DESCRIPTION
  • The detailed description set forth below in connection with the drawings is intended to provide a description of exemplary embodiments of apparatuses for additive manufacturing systems and methods, and it is not intended to represent the only embodiments in which the disclosure may be practiced. The term “exemplary” used throughout this disclosure means “serving as an example, instance, or illustration,” and should not necessarily be construed as preferred or advantageous over other embodiments presented in this disclosure. The detailed description includes specific details for the purpose of providing a thorough and complete disclosure that fully conveys the scope of the disclosure to those skilled in the art. However, the disclosure may be practiced without these specific details. In some instances, well-known structures and components may be shown in block diagram form, or omitted entirely, in order to avoid obscuring the various concepts presented throughout this disclosure.
  • Additive Manufacturing
  • Additive Manufacturing (AM) involves the use of a stored geometrical model for accumulating layered materials on a build plate to produce a three-dimensional (3-D) build piece having features defined by the model. AM techniques are capable of printing complex components using a wide variety of materials. A 3-D object may be fabricated based on a computer aided design (CAD) model. The CAD model can be used to generate a set of instructions or commands that are compatible with a particular 3-D printer. The AM process can create a solid three-dimensional object using the CAD model and print instructions. In the AM process, different materials or combinations of material, such as engineered plastics, thermoplastic elastomers, metals, ceramics, and/or alloys or combinations of the above, etc., may be used to create a uniquely shaped 3-dimensional object.
  • A number of different AM technologies may be well-suited for rotational AM. Such 3-D printing techniques may include, for example, selective laser melting (SLM), selective laser sintering (SLS), direct metal laser sintering (DMLS), electron beam melting (EBM), powder bed fusion (PBF), and/or other AM processes involving melting or fusion of metallic powders.
  • As in many 3-D printing techniques, these processes (e.g., PBF systems) can create build pieces layer-by-layer. Each layer or “slice” is formed by depositing a layer of powder and exposing portions of the powder to an energy beam. The energy beam is applied to melt areas of the powder layer that coincide with the cross-section of the build piece in the layer. The melted powder cools and fuses to form a slice of the build piece. The process can be repeated to form the next slice of the build piece, and so on. Each layer is deposited on top of the previous layer. The resulting structure is a build piece assembled slice-by-slice from the ground up.
  • AM may include the manufacture of one or more nodes. A node is a structural member that may include one or more interfaces used to connect to other nodes or spanning components such as tubes, extrusions, panels, and the like. Using AM, a node may be constructed to include additional features and functions, including interface functions, depending on the objectives.
  • Nodes and other components may be connected together. For example, one or more nodes and/or other components may be connected together to form larger components. Accordingly, individual AM structures often need to be connected together, or individual AM structures often need to be connected to machined or COTS parts, to provide combined structures, e.g., to realize the above modular network or to form a complex interior assembly in a vehicle. Examples include node-to-node connections, node-to-panel connections, node-to-tube connections, and node-extrusion connections, among others. To connect an AM joint member with a vehicle body panel, for example, mechanical connectors (e.g., screws, clamps, etc.) may be used. Alternatively or additionally, an adhesive may be used to form a strong bond. For connecting these parts, a strict tolerance is often desired, meaning that the parts must be positioned to fit precisely in an established orientation. For example, the two parts to be adhered may need to be positioned to avoid direct contact with each other in order to mitigate possible galvanic corrosion problems. In general, an adhesive connection between the AM joint member and panel should result in an accurate fit. Thus the AM joint member should not be misaligned with or offset from the body panel, for example, and the parts should remain properly oriented when a permanent bond is established.
  • Additive Manufacturing Environment
  • FIGS. 1A-1D illustrate respective side views of a conventional 3-D printer system.
  • In an aspect of the present disclosure, a 3-D printer system may be a powder-bed fusion (PBF) system 100. FIGS. 1A-D show a conventional PBF system 100 during different stages of operation. The particular embodiment in FIGS. 1A-1D illustrates various principles of PBF systems that may be helpful in understanding principles of this disclosure. Various components described in the present embodiment are also used in the embodiments of rotational AM, but may not be included in figures below for the sake of clarity and to avoid obscuring other details. For example, components such as energy beam sources (e.g., laser source(s) and optical deflector(s), electron beam source(s) and magnetic deflector(s)) are not shown expressly in some of the figures below because some of the figures are top views in which the energy beam source would obscure other portions of the embodiments. However, one skilled in the art will readily understand how such components are implemented in the embodiment of FIGS. 1A-D and can be implemented in the embodiments described below and in other embodiments according to aspects of the disclosure. It should also be noted that elements of FIGS. 1A-1D and the other figures in this disclosure are not necessarily drawn to scale, but may be drawn larger or smaller for the purpose of better illustration of concepts described herein. PBF system 100 can include a depositor 101 that can deposit each layer of metal powder, an energy beam source 103 that can generate an energy beam, a deflector 105 that can apply the energy beam to fuse the powder material, and a build plate 107 that can support one or more build pieces, such as a build piece 109. Although the terms “fuse” and/or “fusing” are used to describe the mechanical coupling of the powder particles, other mechanical actions, e.g., sintering, melting, and/or other electrical, mechanical, electromechanical, electrochemical, and/or chemical coupling methods are envisioned as being within the scope of the present disclosure.
  • PBF system 100 can also include a build floor 111 positioned within a powder bed receptacle. The walls of the powder bed receptacle 112 generally define the boundaries of the powder bed receptacle, which is sandwiched between the walls 112 from the side and abuts a portion of the build floor 111 below. Build floor 111 can progressively lower build plate 107 so that depositor 101 can deposit a next layer. The entire mechanism may reside in a chamber 113 that can enclose the other components, thereby protecting the equipment, enabling atmospheric and temperature regulation and mitigating contamination risks. Depositor 101 can include a hopper 115 that contains a powder 117, such as a metal powder, and a leveler 119 that can level the top of each layer of deposited powder.
  • Referring specifically to FIG. 1A, this figure shows PBF system 100 after a slice of build piece 109 has been fused, but before the next layer of powder has been deposited. In fact, FIG. 1A illustrates a time at which PBF system 100 has already deposited and fused slices in multiple layers, e.g., 200 individual layers, to form the current state of build piece 109, e.g., formed of 200 individual slices. The multiple individual layers already deposited have created a powder bed 121, which includes powder that was deposited but not fused.
  • FIG. 1B shows PBF system 100 at a stage in which build floor 111 can lower by a powder layer thickness 123. The lowering of build floor 111 causes build piece 109 and powder bed 121 to drop by powder layer thickness 123, so that the top of build piece 109 and powder bed 121 are lower than the top of powder bed receptacle wall 112 by an amount equal to the powder layer thickness 123. In this way, for example, a space with a consistent thickness equal to powder layer thickness 123 can be created over the tops of build piece 109 and powder bed 121. In this example, build floor 111 is lowered, but not rotated.
  • FIG. 1C shows PBF system 100 at a stage in which depositor 101 is positioned to deposit powder 117 in a space created over the top surfaces of build piece 109 and powder bed 121 and bounded by powder bed receptacle walls 112. In this example, depositor 101 progressively moves over the defined space (linearly from left to right as viewed in FIG. 1C) while releasing powder 117 from hopper 115. Leveler 119 can level the released powder to form a powder layer 125 that leaves powder layer top surface 126 configured to receive fusing energy from energy beam source 103. Powder layer 125 has a thickness substantially equal to the powder layer thickness 123 (see FIG. 1B). Thus, the powder in a PBF system can be supported by a powder material support structure, which can include, for example, a build plate 107, a build floor 111, a build piece 109, walls 112, and the like. It should be noted that the illustrated thickness of powder layer 125 (i.e., powder layer thickness 123 (FIG. 1B)) is greater than an actual thickness used for the example involving the 200 previously-deposited individual layers discussed above with reference to FIG. 1A. It should be noted that fusing of the powder is not occurring while depositor 101 is depositing powder.
  • FIG. 1D shows PBF system 100 at a stage in which, following the deposition of powder layer 125 (FIG. 1C), depositor 101 has returned to its starting position and is no longer depositing powder, and energy beam source 103 generates an energy beam 127 and deflector 105 applies the energy beam to fuse the next slice in build piece 109. In various exemplary embodiments, energy beam source 103 can be an electron beam source, in which case energy beam 127 constitutes an electron beam. Deflector 105 can include deflection plates that can generate an electric field or a magnetic field that selectively deflects the electron beam to cause the electron beam to scan across areas designated to be fused. In various embodiments, energy beam source 103 can be a laser, in which case energy beam 127 is a laser beam. Deflector 105 can include an optical system that uses reflection and/or refraction to manipulate the laser beam to scan selected areas to be fused.
  • In various embodiments, the deflector 105 can include one or more gimbals and actuators that can rotate and/or translate the energy beam source to position the energy beam. In various embodiments, energy beam source 103 and/or deflector 105 can modulate the energy beam, e.g., turn the energy beam on and off as the deflector scans so that the energy beam is applied only in the appropriate areas of the powder layer. For example, in various embodiments, the energy beam can be modulated by a digital signal processor (DSP).
  • FIG. 1E illustrates a functional block diagram of a 3-D printer system.
  • In an aspect of the present disclosure, control devices and/or elements, including computer software, may be coupled to PBF system 100 to control one or more components within PBF system 100. Such a device may be a computer 150, which may include one or more components that may assist in the control of PBF system 100. Computer 150 may communicate with a PBF system 100, and/or other AM systems, via one or more interfaces 151. The computer 150 and/or interface 151 are examples of devices that may be configured to implement the various methods described herein, that may assist in controlling PBF system 100 and/or other AM systems.
  • In an aspect of the present disclosure, computer 150 may comprise at least one processor unit 152, memory 154, signal detector 156, a digital signal processor (DSP) 158, and one or more user interfaces 160. Computer 150 may include additional components without departing from the scope of the present disclosure.
  • The computer 150 may include at least one processor unit 152, which may assist in the control and/or operation of PBF system 100. The processor unit 152 may also be referred to as a central processing unit (CPU). Memory 154, which may include both read-only memory (ROM) and random access memory (RAM), may provide instructions and/or data to the processor unit 152. A portion of the memory 154 may also include non-volatile random access memory (NVRAM). The processor 152 typically performs logical and arithmetic operations based on program instructions stored within the memory 154. The instructions in the memory 154 may be executable (by the processor unit 152, for example) to implement the methods described herein.
  • The processor unit 152 may comprise or be a component of a processing system implemented with one or more processors. The one or more processors may be implemented with any combination of general-purpose microprocessors, microcontrollers, digital signal processors (DSPs), floating point gate arrays (FPGAs), programmable logic devices (PLDs), controllers, state machines, gated logic, discrete hardware components, dedicated hardware finite state machines, or any other suitable entities that can perform calculations or other manipulations of information.
  • The processor unit 152 may also include machine-readable media for storing software. Software shall be construed broadly to mean any type of instructions, whether referred to as software, firmware, middleware, microcode, hardware description language, or otherwise. Instructions may include code (e.g., in source code format, binary code format, executable code format, RS-274 instructions (G-code), numerical control (NC) programming language, and/or any other suitable format of code). The instructions, when executed by the one or more processors, cause the processing system to perform the various functions described herein.
  • The computer 150 may also include a signal detector 156 that may be used to detect and quantify any level of signals received by the computer 150 for use by the processing unit 152 and/or other components of the computer 150. The signal detector 156 may detect such signals as energy beam source 103 power, deflector 105 position, build floor 111 height, amount of powder 117 remaining in depositor 101, leveler 119 position, and other signals. Signal detector 156, in addition to or instead of processor unit 152 may also control other components as described with respect to the present disclosure. The computer 150 may also include a DSP 158 for use in processing signals received by the computer 150. The DSP 158 may be configured to generate instructions and/or packets of instructions for transmission to PBF system 100.
  • The computer 150 may further comprise a user interface 160 in some aspects. The user interface 160 may comprise a keypad, a pointing device, and/or a display. The user interface 160 may include any element or component that conveys information to a user of the computer 150 and/or receives input from the user.
  • The various components of the computer 150 may be coupled together by an interface 151. The interface 151 may include a data bus, for example, as well as a power bus, a control signal bus, and a status signal bus in addition to the data bus. Components of the computer 150 may be coupled together or accept or provide inputs to each other using some other mechanism.
  • Although a number of separate components are illustrated in FIG. 1E, one or more of the components may be combined or commonly implemented. For example, the processor unit 152 may be used to implement not only the functionality described above with respect to the processor unit 152, but also to implement the functionality described above with respect to the signal detector 156, the DSP 158, and/or the user interface 160. Further, each of the components illustrated in FIG. 1E may be implemented using a plurality of separate elements.
  • By way of example, an element, or any portion of an element, or any combination of elements may be implemented using one or more processors. Examples of processors include microprocessors, microcontrollers, graphics processing units (GPUs), central processing units (CPUs), application processors, digital signal processors (DSPs), reduced instruction set computing (RISC) processors, systems on a chip (SoC), baseband processors, field programmable gate arrays (FPGAs), programmable logic devices (PLDs), state machines, gated logic, discrete hardware circuits, and other suitable hardware configured to perform the various functionality described throughout this disclosure. One or more processors may execute software as that term is described above.
  • In one or more aspects, the functions described may be implemented in hardware, software, firmware, or any combination thereof. If implemented in software, the functions may be stored on or transmitted over as one or more instructions or code on a computer-readable medium. Computer-readable media includes both computer storage media and communication media including any medium that facilitates transfer of a computer program from one place to another. A storage media may be any available media that can be accessed by a computer. By way of example, and not limitation, such computer-readable media can comprise RAM, ROM, EEPROM, compact disc (CD) ROM (CD-ROM) or other optical disk storage, magnetic disk storage or other magnetic storage devices, or any other medium that can be used to carry or store desired program code in the form of instructions or data structures and that can be accessed by a computer. Disk and disc, as used herein, includes CD, laser disc, optical disc, digital versatile disc (DVD), floppy disk and Blu-ray disc where disks usually reproduce data magnetically, while discs reproduce data optically with lasers. Thus, computer readable medium comprises a non-transitory computer readable medium (e.g., tangible media).
  • It should be understood that a computer such as computer 150 and computer-readable instructions (e.g., computer programs) may similarly be implemented in the following example embodiments to control a PBF system in the various ways described below.
  • FIG. 2 illustrates a side view of a printing system in accordance with an aspect of the present disclosure.
  • In an aspect of the present disclosure, a PBF system 200 (which may be referred to as an apparatus herein) may comprise, inter alia, a build floor 201 that rotates as shown by rotation 202. As build floor 201 rotates, it also moves downward, and the depth of build floor 201 with respect to the top of a powder bed receptacle wall 203 changes, as shown by platform depth 250. A motor system 205 can cause the rotational motion of build floor 201, and can also cause the downward motion of the build floor. In various embodiments, for example, motor system 205 may include a threaded screw with a thread pitch equal to a layer thickness of the powder to be deposited. In the present example, a shaft 206 connects motor system 205 with build floor 201, and the shaft may include a threaded screw. In the present example, the other portions of the apparatus (such as powder bed receptacle wall 203, a depositor 207, an energy beam source 209, a gas inlet 211, and a gas extractor 213) remain stationary with respect to the rotational motion of build floor 201. In the present example, build floor 201 moves downward toward powder egress holes 215 in powder bed receptacle wall 203 and a platform knife 223.
  • As build floor 201 rotates and moves downward (e.g., in a continuous, spiral motion), depositor deposits a layer of powder material (e.g., metal powder) onto the build floor to create a powder bed 217. The layer of powder material rotates into an active area of energy beam source 209, and the energy beam source applies an energy beam to fuse portions of the powder layer to form a layer of a build piece 219. As energy beam source 209 is applying the energy beam, gas inlet 211 can allow a gas to flow over the active area, and gas extractor 213 can allow the gas flow to exit the chamber. In this way, for example, smoke, soot, and other byproducts of the fusing process may be removed quickly so that the smoke, soot, etc. does not negatively affect the operation of the energy beam, e.g., by obscuring the beam from fully reaching the powder bed.
  • It is noted that the position of the gas inlet(s) and extractor(s) may be reversed in the example embodiments described herein, as one skilled in the art would readily recognize.
  • Once build floor 201 is lowered to a build depth 253, powder bed 217 is exposed to powder egress holes 215, and the powder in the powder bed can be allowed to escape through the powder egress holes, which may be holes or screens in the powder bed receptacle walls 203 to allow for some removal or exit paths for any powder from the PBF system 200. As build floor 201 is lowered further, it may come into proximity with platform knife 223. Build floor 201 may be configured to thread past platform knife 223 such that the platform knife is positioned just over the build floor. As the build floor continues to rotate, platform knife 223 can come into contact with the bottom of build piece 219, i.e., where the build piece is attached to the build floor, and the platform knife can cut or break the build piece off of the build floor as the build floor continues to rotate.
  • In the present example embodiment, motor system 205, coupled to build floor 201 (which may be called a build plate herein) via shaft 206, may rotate the build floor in cylindrical powder bed receptacle wall 203. Powder bed receptacle wall 203 may be configured to contain the powder on the build floor. Build floor 201 may include seals to further prevent powder from escaping, e.g., between the build floor and the powder bed receptacle wall. After the build is completed, motor system 205 may rotate and raise build floor 201 back to the starting position at the top of powder bed receptacle wall(s) 203 to begin another build. In various embodiments, motor system 205 may further rotate powder bed receptacle wall 203 together with build floor 201, such that the build floor moves vertically but not rotationally with respect to the powder bed receptacle wall. In this way, for example, wear and tear on the seal between the build floor and the powder bed receptacle wall may be reduced. It is noted that the motor system that causes the rotational motion may not be explicitly illustrated or described in some of the figures below, because the motor system may be below the build floor in a top view. However, one skilled in the art will readily understand how motor systems are implemented in all of the embodiments disclosed herein based on the descriptions of the rotational motion and which components are being rotated.
  • As shown in FIG. 2, an apparatus such as PBF system 200 may provide a rotational layer based processing of the build volume. In various embodiments, the depositor can continuously deposit powder, and the energy beam source can fuse portions of the build piece while the depositor is depositing powder, without having to wait until completion of a depositing step. Instead of a horizontally “sliced” geometry, i.e., a geometry with strictly horizontal layers such as is generated by the PBF system 100 shown in FIGS. 1A-1D, PBF system 200 may create a build piece having a geometry that is sliced in a spiral-wise fashion. In an aspect of the present disclosure, PBF system 200 may enable changes to the gas management that may improve the 3-D printing process.
  • For example, and not by way of limitation, PBF system 200 may allow for more efficient handling of soot and other gaseous by-products of powder micro-welding processes than PBF system 100 of the related art. Further, the speed of rotation 202 can be varied depending on information of the build. The build may also be referred to as the build job, print job, etc. In various embodiments, information of the build can include a geometric feature density being processed by PBF system 200, which may increase efficiency. As used herein, geometric feature density refers to the percentage of the active area that is being processed (e.g., fused) at any given time. A high geometric feature density, for example, could include the situation in which a large portion of a build piece is in the active area and therefore a large portion of the active area is to be fused. Likewise, a high geometric feature density, for example, could include the situation in which many build pieces are being printed in the same print build, and the many build pieces come into the active area, requiring a large portion of the active area to be fused. On the other hand, a low geometric feature density can refer to the opposite of these examples, i.e., the active area includes only a small portion of a single build piece or only a few of many build pieces. In an aspect of the present disclosure, the speed of rotation 202 can be increased when the geometric feature density related to build piece 219 or a print build is low and decreased when the feature density related to the build piece or the print build is high. In this way the energy beam(s), e.g., lasers, can be continuously kept working at or near full capacity.
  • In some PBF systems 100, the time used to print a given component is governed by pause times between layers, e.g., the time it takes to put down a new layer of powder, level the layer of powder, etc., rather than the volume of material fused and/or sintered in any specific layer. This results in a strong printing inefficiency, that is especially penalizing for materials that require long interlayer wait times, e.g., powders with high melting temperatures, low thermal conductivities, etc. In an aspect of the present disclosure, PBF system 200 may enable a more efficient thermal management strategy by decreasing the time between powder deposition and printing and/or reducing the time inefficiencies between layers.
  • In an aspect of the present disclosure, the rotational speed can be changed based on thermal management strategies, build densities, materials being fused, and/or other variables. This change in rotational speed can be done globally, e.g., for an entire component, or locally, e.g., for certain parts of a component build, which may increase the efficiency of the build process.
  • The build piece 219 volume may be further segmented in PBF system 200 to achieve various build optimization goals, such as processing under different conditions, use of different optics, etc., because of the more continuous printing process enabled by the present disclosure. Depending on the material and geometry being processed, PBF system 200 can be configured to support more efficient printing. By using a multi-sectored approach, in an aspect of the present disclosure gas extraction strategies can be tailored to the specific optics strategy for material processing occurring in a given sector. For example, parts with lots of thin areas, such as a heat exchanger or a heavily lattice-based structure, will have little use for optics that can de-focus and apply a wide beam profile; efforts may be better spent on agile optics with the necessary feature resolution. By contrast, thick-walled parts with relatively lower surface area density can be efficiently processed using zoom/de-focus strategies.
  • In an aspect of the present disclosure, PBF system 200 may enable additional design geometries that were previously unattainable with PBF system 100 of the related art. By reducing any non-exposure time between layers, PBF system 200 of the present disclosure may be more efficient. Further, PBF system 200 may be able to dynamically change its rotation speed for various portions of the printing process, which may also increase printing efficiency.
  • Since the build floor 201 is rotating (i.e., rotation 202), that the relative position between a printed feature and the optics (e.g., energy beam source 103, deflector 105, etc.) may change over time. In an aspect of the present disclosure, this difference may be advantageously applied to allow for different vector sequencing, novel exposure strategies, etc., to optimize the incidence angle and produce higher quality parts. Build floor 201 may have a rotational motion or rotate such that the platform depth 250 of build floor 201 moves in a downward direction, and may move at any rate. For example, build floor 201 may move between 5 microns and 5000 microns per minute, between 50 and 500 microns per minute, between 100 and 150 microns per minute, or any rate desired, without departing from the scope of the present disclosure.
  • In an aspect of the present disclosure, the distance from the powder surface to the optics may also be reduced. This may be achieved by reducing the incidence angle and/or the operating region of each laser, using a build volume segmenting approach and to enable optic arrangements that are more compact (i.e., offset, slightly angled, etc.). Reducing this distance may also allow other benefits, such as reducing the volume of the build chamber, reducing the volume of inert gas, reducing the pumping power, potentially creating more laminar flow to improve performance, etc.
  • Because build floor 201 rotates downward, platform knife 223 and powder egress holes 215 are positioned below the build depth 253 of PBF system 200 to remove powder from PBF system 200 and build piece 219 from build floor 201. With a given thread pitch on a screw used for rotation of the build floor 201, any seals placed on build floor 201 can be positioned such that there is minimal contact between the seals and powder egress holes. Further, platform knife 223 can be oriented or dynamically changed to operate within the pitch of the rotational screw pitch used to rotate build floor 201.
  • FIG. 3 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • PBF system 300, may comprise a build plate 302, a powder bed receptacle wall 304, a depositor 306, and a gas flow system that includes one or more gas inlets 308 and an extractor 310. Active area 312 is shown to indicate the area for energy beams, e.g., lasers, etc. to sinter or fuse powder deposited by depositor 306.
  • In an aspect of the present disclosure, as depositor 306 (which may include a leveler to level the powder level) deposits a layer of powder, build plate 302 rotates in direction 314, and the layer of powder deposited by depositor 306 is exposed in active area 312. One or more energy beams then fuse or sinter the powder in active area 312 to form a layer of a build piece.
  • The gas inlet 308 may provide gases, such as inert gases, as a gas flow, to remove the byproducts created by the energy beams operating in active area 312. These gases can be directed toward extractor 310, which may remove the byproducts and/or gases provided by gas inlet 308, from the active area 312. In this example, the gas flow system can direct the gas flow substantially parallel to the radius of the rotational motion, i.e., substantially orthogonal to the direction of rotation. In an aspect of the present disclosure, gas flow in and around the active area 312 can be controlled by controlling the rate and amount of gas flow from gas inlet 308 and removal of gases by extractor 310, which may reduce the impact of soot, byproducts of the fusing process, splatter, etc. from affecting the printing process. Further, meltpool vectors of fusing performed in the active area 312 can be controlled to be in a direction preferable to the gas flow.
  • As described herein, gas inlet 308 and extractor 310 may provide a gas flow system for PBF system 300. Gas inlet 308 may be disposed or located around the build plate 302, and extractor 310 may be disposed or located at or near an axis of rotation of the build plate 302. Gas inlet 308 may collectively surround the build plate 302. Such a gas flow system may allow for the flow of introduced gases across active area 312, removal of soot, fumes, spatter, and/or other byproducts of the build process from the active area 312, other gas flow controls, or any combination thereof, without departing from the scope of the present disclosure. Such a gas flow may be linear, rotated, or otherwise controlled to provide a desired gas flow across active area 312.
  • FIG. 4 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • PBF system 400, may comprise a build plate 402, a powder bed receptacle wall 404, a depositor 406, and a gas flow system that includes one or more gas inlets 408 and an extractor 410. Active area 412 is shown to indicate the area for energy beams, e.g., lasers, etc. to sinter or fuse powder deposited by depositor 406.
  • In an aspect of the present disclosure, rather than build plate 402 rotating as described with respect to FIG. 3, depositor 406, extractor 410, and active area 412 may rotate or move in an arc motion with respect to the build plate 402. After depositor 406 (which may include a leveler to level the powder level) deposits a layer of powder, the depositor 406, extractor 410, and active area 412 rotate in direction 414, and the layer of powder deposited by depositor 406 is exposed in active area 412. Energy beams then fuse or sinter the powder in active area 412. Other combination of rotational motions and/or stationary portions of PBF system 300 are possible without departing from the scope of the present disclosure.
  • The gas inlet 408 may provide gases, such as inert gases, or a gas flow, to remove the byproducts created by the energy beams operating in active area 412. These gases can be directed toward extractor 410, and may be located in powder bed receptacle wall 404, to help remove the byproducts and/or gases provided by gas inlet 408, from the active area 412. In an aspect of the present disclosure, gas flow in and around the active area 412 can be controlled by controlling the rate and amount of gas flow from gas inlet 408 and removal of gases by extractor 410, which may reduce the impact of soot, byproducts of the fusing process, splatter, etc. from affecting the printing process. Further, meltpool vectors of fusing performed in the active area 412 can be controlled to be in a direction preferable to the gas flow.
  • As described herein, gas inlet 408 and extractor 410 may provide a gas flow system for PBF system 400. Gas inlet 408 may be disposed or located around the build plate 302, and extractor 310 may be disposed or located at or near an axis of rotation of the build plate 302. Gas inlet 308 may collectively surround the build plate 302. Such a gas flow system may allow for the flow of introduced gases across active area 312, removal of soot, fumes, spatter, and/or other byproducts of the build process from the active area 312, other gas flow controls, or any combination thereof, without departing from the scope of the present disclosure.
  • With respect to FIG. 4, a cover 416 may be provided over some or all of the build plate 402. For embodiments in which only a portion of the powder bed is actively fused in active area 412, the remainder of the print/build area may be covered with cover 416 to protect the powder bed from spatter and/or other byproducts from the printing process. In various embodiments the cover 416 may be heated, e.g., may include heating elements on the underside of the cover, facing the powder bed to control cooling of the fused powder. In various embodiments, a portion of the cover 416 may be configured to heat up the deposited powder before fusing in the active area 412.
  • In various embodiments, sensors can be positioned above the bed to, for example, detect defects in the build piece or other characteristics of the powder, build piece, or other conditions. For example, eddy current sensors may be used. If a defect is detected, an area within the active area 412 can be a dedicated remelting area. In this case, for example, another energy beam(s) can expose this “remelt” area to remelt portions of the build piece that the sensor(s) detected a defect, such as a crack. Sensors may be included in cover 416, for example.
  • FIG. 5 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • PBF system 500, may comprise a build plate 502, a powder bed receptacle wall 504, a depositor 506, and a gas flow system that includes one or more gas inlets 508 and an extractor 510. Active area 512 is shown to indicate the area for energy beams, e.g., lasers, etc. to sinter or fuse powder deposited by depositor 506.
  • In an aspect of the present disclosure, gas inlets 508 may be located in powder bed receptacle wall 504, and extractor 510 may direct the flow of gas from gas inlets 508 across the active area 512 as shown by arrows 514.
  • In an aspect of the present disclosure, build plate 502 may rotate in direction 516. In another aspect of the present disclosure, rather than build plate 502 rotating, depositor 506, extractor 510, and active area 512 may rotate. After depositor 506 (which may include a leveler to level the powder level) deposits a layer of powder, the depositor 506, extractor 510, and active area 512 rotate in direction 516, and the layer of powder deposited by depositor 506 is exposed in active area 512. Energy beams then fuse or sinter the powder in active area 512. In another aspect of the present disclosure, build plate 502 and extractor 510 may rotate. As extractor 510 rotates across the gas inlets 508, extractor may direct gas from gas inlets 508 along extractor and across active area 512, or other areas of the deposited powder, as desired. In this example, the gas flow system can direct the gas flow substantially parallel to the radius of the rotational motion, i.e., substantially orthogonal to the direction of rotation.
  • The gas inlet 508 may provide gases, such as inert gases, or a gas flow, to remove the byproducts created by the energy beams operating in active area 512. These gases can be directed toward extractor 510. In an aspect of the present disclosure, gas inlets 508 may be located in powder bed receptacle wall 504, and extractor 510 may be configured to help remove the byproducts and/or gases provided by gas inlet 508 from the active area 512. In an aspect of the present disclosure, gas flow in and around the active area 512 can be controlled by controlling the rate and amount of gas flow from gas inlet 508 and removal of gases by extractor 510, which may reduce the impact of soot, byproducts of the fusing process, splatter, etc. from affecting the printing process. Further, meltpool vectors of fusing performed in the active area 512 can be controlled to be in a direction preferable to the gas flow.
  • FIG. 6 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • As shown in FIG. 6, PBF system 600 may include a powder bed receptacle wall 602, which may enclose a depositor 604 and, optionally, a full width depositor system 606. Full width depositor system 606 may be considered to include two depositors because it deposits powder in two separate locations. As the build plate rotates in direction 608, two active areas may be operating: active area 1 610 and active area 2 612, which may be operated on by different optics and/or different energy beams. A gas flow system may include a gas inlet 618, an extractor 1 (614), and an extractor 2 (616). Each active area 610 and 612 may have an independent extractor, e.g., extractor 1 614 for active area 1 610 and extractor 2 616 for active area 2 612. Active area 1 610 and active area 2 612 may be overlapping or non-overlapping. Depositor 604 and depositor system 606 may deposit powder simultaneously or at different times as desired.
  • In an aspect of the present disclosure, multiple active areas may have independent gas streams from various gas inlets 618, optics, and/or operated in conjunction to increase the print speed of a given part. In such an aspect, the flexibility to rapidly print some portions of a given part, and slowly print other sections within the same “slice”, may increase the production efficiency of the overall part. Further, gas inlets 618, which are shown as being imbedded in powder bed receptacle wall 602, may be provided as part of extractor 1 612, extractor 2 614, or as a separate system.
  • In the embodiment of FIG. 6, PBF system 600 can allow the layer thickness of the fused deposited powder to be varied during a build of the build piece. In the present embodiment, a full-width depositor system 606 is used, so that powder is deposited in two locations that are 180 degrees apart (i.e., the left side and right side as viewed in FIG. 6). In this embodiment, the build plate is lowered 100 μm per full rotation, therefore each side of full-width depositor system 606 deposits a 50 μm layer of powder. The layer thickness that is fused can be selected as either 50 μm or 100 μm by choosing to fuse either in both active areas or in a single active area, respectively. For example, PBF system 600 may determine that a first portion of a build piece, e.g., near the outside edges, is to be printed at the finer resolution of 50 μm so the finished build piece will have smoother walls. However, PBF system 600 may determine that a second portion of the build piece, e.g., the interior, or bulk of the build piece, can be printed at the lower resolution of 100 μm. Therefore, PBF system 600 can select to fuse the first portion of the build piece by fusing in both active area 1 (610) and active area 2 (612). In other words, the portion of the build piece near the outside edges will be formed by fusing a 50 μm layer of powder twice per rotation. Likewise, PBF system 600 can select to fuse the second portion of the build piece by fusing in only a single active area, e.g., active area 2 (612). In other words, the interior, bulk portion of the build piece will be formed by fusing a 100 μm layer of powder once per rotation. In this way, for example, the time spent actively scanning the lower resolution portions of the build piece can be cut in half, which can allow faster build times because the speed of the rotation can be increased and/or more build pieces may be printed in the same build job.
  • While the example layer thicknesses of 50 μm and 100 μm are used as examples, it is understood that this example embodiment using a full-width depositor (e.g., two depositors 180 degrees apart) can provide a selection of fusing two layer thicknesses, in general, that are X and 2× thicknesses, i.e., a given thickness and double the given thickness.
  • The example embodiment of FIG. 6 can include a full-width depositor system 606 (depositing twice at 180 degrees apart), but other embodiments may include other configurations of depositors, as one skilled in the art will readily recognize. For example, three depositors that are each 120 degrees apart and three corresponding active areas could be used. In this example, if the build plate is lowered 100 μm in one a full rotation, the fused layer thicknesses can be selected among 33.3 82 m, 66.6 μm, and 100 μm by fusing every active area (three times per rotation), every other active area (alternating once and twice per rotation), or every third active area (once per rotation), respectively.
  • FIG. 7 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • PBF system 700, may comprise a build plate 702, a powder bed receptacle wall 704, a depositor 706, and a gas flow system that includes one or more gas inlets 708, and an extractor 710, and an exhaust manifold 714. Active area 712 is shown to indicate the area for energy beams, e.g., lasers, etc. to sinter or fuse powder deposited by depositor 706.
  • FIG. 7 illustrates an aspect of the present disclosure where extractor 710 may direct a gas flow from gas inlet 708 through and/or across extractor 710, while exhaust manifold 714 may remove additional fumes, soot, and/or other byproducts from the sintering or fusing process performed by the energy beam(s) impinging on the powder bed deposited on build plate 702. While extractor 710 may remove some of the fumes, soot, and/or other by products, the gas flow from gas inlet(s) 708 and gas flow through extractor 710 may not be positioned properly to remove enough byproducts, or the byproducts may still be emitting from the melt pools after rotation of the build plate 702 in direction 716. As such, exhaust manifold 714 may be used to remove additional fumes, soot, and/or other byproducts from the PBF system 700, which may increase the efficiency of PBF system 700. In this example, the gas flow system can direct the gas flow substantially parallel to the radius of the rotational motion, i.e., substantially orthogonal to the direction of rotation.
  • In an aspect of the present disclosure, rather than build plate 702 rotating, depositor 706, extractor 710, and active area 712 may rotate. As depositor 706 (which may include a leveler to level the powder level) deposits a layer of powder, the depositor 706, extractor 710, and active area 712 rotate in direction 716, and the layer of powder deposited by depositor 706 is exposed in active area 712. Energy beams then fuse or sinter the powder in active area 712.
  • In such an aspect, the gas flow system may be rotating as well, such that gas inlets 708 may be configured such that gas flows only in select areas, e.g., across active area 712 that is being processed by the energy beam. This selective gas flow may mitigate soot and other components formed during the fusion process from contaminating the inactive areas of the build plate, as the gas flow would be constrained. The rotational speed of the build plate 702, and/or the rotation of the above-the-bed systems, may be synchronized with the opening and closing of gas inlets 708 to allow for selection of variable gas flows across active area 712 and/or other areas within PBF system 700.
  • In an aspect of the present disclosure, gas flow in and around the active area 712 can be controlled by controlling the rate and amount of gas flow from gas inlet 708 and removal of gases by extractor 710, as well as removal of gases through exhaust manifold 714, which may reduce the impact of soot, byproducts of the fusing process, splatter, etc. from affecting the printing process. Further, meltpool vectors of fusing performed in the active area 712 can be controlled to be in a direction preferable to the gas flow.
  • FIG. 8 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • PBF system 800, may comprise a build plate 802, a powder bed receptacle wall 804, a depositor 806, and a gas flow system that includes a gas inlet 808 and an extractor 810. Active area 812 is shown to indicate the area for energy beams, e.g., lasers, etc. to sinter or fuse powder deposited by depositor 806. Active area 812 has two powder motion boundaries 813 and two non-powder motion boundaries 815. Powder motion boundaries are boundaries of an active area across which the underlying powder layer moves, and non-powder motion boundaries are boundaries of an active area across which underlying powder does not move. In other words, as build plate 802 rotates, the powder layer moves across one of the powder motion boundaries 813 into active area 812, but the powder layer does not move across either of the non-powder motion boundaries 815. Likewise, as build plate 802 continues to rotate, the powder layer (portions of which may now be fused) moves out of active area 812 across the other of the powder motion boundaries 813, but does not move across either of the non-powder motion boundaries. The distinction between powder motion boundaries and non-powder motion boundaries is described to illustrate how different gas flow systems can direct gas flow in different ways to achieve different benefits. In the present example of FIG. 8, the gas flow system components, i.e., gas inlet 808 and extractor 810, can be positioned substantially at the powder motion boundaries, which may allow a more laminar gas flow to be applied across active area 812 because the gas inlet and extractor can be placed close together due to the slim arc area of the active area. In this regard, in various embodiments, the active area may be, for example, an arc area of less than 45 degrees, 40 degrees, 35 degrees, 30 degrees, 25 degrees, 20 degrees, 15 degrees, 10 degrees, 5 degrees, or 3 degrees. In the present embodiment, it is noted that the powder motion boundaries 813 are radial boundaries of the active area with respect to the rotational motion, and the non-powder motion boundaries 815 are circumferential boundaries (an inner circumference and an outer circumference) with respect to the rotational motion. Also, it is noted that in the present example of FIG. 8, the gas flow system can direct the gas flow substantially parallel to the direction of rotation, i.e., substantially orthogonal to the radius of the rotational motion.
  • It is noted that in various other examples, e.g., FIG. 3, FIG. 5, FIG. 7, and FIG. 10, the gas flow systems position the gas inlet(s) and extractors substantially at the non-powder motion boundaries (not expressly marked in the figures, but readily understandable to one skilled in the art).
  • In an aspect of the present disclosure, and as shown in FIG. 8, depositor 806 may be placed anywhere within the PBF system 800 that is not interfering with the gas flow system or the active area, and is not necessarily adjacent to active area 812. Similar configurations where the depositor may be configured anywhere within the PBF system may be employed with respect to any PBF system described herein without departing from the scope of the present disclosure.
  • As shown in FIG. 8, gas inlet 808 may be configured to direct gas flow 814 across active area 812 in a direction other than from the powder bed receptacle wall 804 towards the center of PBF system 800. In various embodiments, a gas inlet and an extractor may be configured to direct the gas flow at other angles, or at variable angles, or rotate or otherwise direct the gas flow depending on the material being processed by PBF system 800.
  • FIG. 9 shows a perspective view of an extractor in accordance with an aspect of the present disclosure. Using the example of extractor 810 of FIG. 8, although any extractor described herein can be configured as described with respect to FIG. 9, extractor 810 may remove build byproducts 900, e.g., soot, fumes, spatter, etc. from active area 812. Build byproducts may be created when energy beam 902 impinges upon powder such that the powder is sintered or fused. in an aspect of the present disclosure, extractor 810 (or any extractor described herein) may be configured to have a height, width, and/or shape such that build byproducts 900 are captured within extractor 810 instead of being re-deposited on the powder layer, whether processed or unprocessed. For example, and not by way of limitation, extractor 810 may take on a funnel shape as shown, or any shape such that the gases are removed. Removal of build byproducts 900 from the powder layer on the build plate may increase the repeatability of the build process.
  • FIG. 10 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
  • PBF system 1000, may comprise a cover 1002 (that can cover the powder bed in areas other than the active area and where the depositor deposits powder), a powder bed receptacle wall 1004, a depositor 1006, and a gas flow system including a gas inlet 1008 and an extractor 1010. Active area 1012 is shown to indicate the area for energy beams, e.g., lasers, etc. to sinter or fuse powder deposited by depositor 1006. A build plate (which may be similar to those shown in FIGS. 2-8) receives powder deposited by depositor 1006 and rotates in direction 1014 to expose different areas of deposited powder in active area 1012.
  • In an aspect of the present disclosure, cover 1002 may protect the underlying powder bed and/or already fused/sintered portions of the component being built from spatter, soot, etc. In an aspect of the present disclosure, cover 1002 may include one or more heating elements, i.e. pre-heating elements 1016, to pre-heat the powder bed. Cover 1002 may also optionally include one or more elements, i.e., controlled cooling element 1018, to control cooling of the fused powder after fusing within the active area 1012. Such cooling elements may be coupled to the cover 1002 such that elements 1016 and/or 1018 face the build plate and powder bed.
  • For example, and not by way of limitation, one or more pre-heating elements 1016 may be used to heat a portion of the powder bed prior to that portion entering the active area 1012. After fusing, one or more controlled cooling elements 1018 may create a thermal gradient having a high starting temperature and a steadily reducing temperature to control the cooling of the fused portions of the component as the powder bed rotates away from the active area 1012.
  • Cover 1002 may include various openings, e.g., such that active area 1012 is able to receive energy beams from one or more energy sources, an opening for depositor 1006 to deposit powder, openings for extractor 1010 to extract gases or byproducts of the build process, etc.
  • Cover 1002 may also include other components, e.g., temperature sensors, cameras, etc. to monitor the build process. As such, pre-heating element 1016 and/or controlled cooling element 1018 may not be a heater, but may be a camera, eddy current sensor, etc. to assist in the build process, e.g., detect defects in the built piece, monitor powder layer deposition, etc. In various embodiments, if a defect is detected, the PBF system 1000 may include an additional active area (not shown) to be a dedicated repair area, while other areas may be continuing to build, or multiple active areas can be assigned various tasks as described with respect to FIG. 6. For example, if a defect (such as a void or crack) in the build piece is detected by a sensor, the additional active area may be used to re-melt the area of the defect in order to fix the defect.
  • In an aspect of the present disclosure, the build plate and powder/fused portion of the component may not rotate, but the “above the bed” systems can rotate. In this case, for example, the depositor(s), energy beam(s) system, gas flow system, sensor(s), etc., e.g., the devices and systems “above the bed”, can rotate at the same rate, such that they remain fixed relative to each other. In some embodiments, the build chamber may include channels for gas inlets and outlets.
  • FIG. 11 illustrates a flowchart of an example method of additively manufacturing a build piece according to various embodiments. The example method includes controlling a depositor system (1101) to deposit a layer of powder onto a build floor, controlling a motor system (1102) to cause a rotational motion between the depositor system and the build floor, such that the depositor system deposits the layer of powder during the rotational motion, and a receptacle wall contains the powder on the build floor, controlling an energy beam source (1103) to apply an energy beam in an active area of the layer of powder to selectively fuse a portion of the powder in the active area to form a portion of a build piece, and controlling a gas flow system (1104) to provide a gas flow across the active area while the energy beam selectively fuses the portion of the layer of powder in the active area. Controlling the motor system (1102) may be implemented by causing the rotational motion at least in part by rotating the build floor, and the depositor system may remain stationary during the rotational motion. Controlling the motor system (1102) may be implemented by causing the rotational motion at least in part by moving the depositor system in an arc over the build floor. The receptacle wall may be configured to remain stationary during the rotational motion. Controlling the gas flow system (1104) may extract a gas created by the fusing of the powder, as described above. The depositor system may include a plurality of depositors, and controlling the depositor system (1101) may include depositing a plurality of layers of powder simultaneously.
  • In various embodiments, the method can include one or more optional actions (1105), which is depicted as a dashed box in FIG. 11 to signify optionality. For example, an optional action (1105) may include covering a second area of the powder exclusive of the active area with a cover. In this way, for example, spatter, soot, etc. from the fusing may be prevented from falling onto portions of the powder bed or build piece. Another optional action (1105) may include controlling a heater configured to heat the powder under the cover, the heater being arranged in the cover. Another optional action (1105) may include controlling a sensor to sense a characteristic of the powder under the cover, wherein the sensor is arranged in the cover.
  • In various embodiments, controlling the gas flow system (1104) may include controlling a gas extractor arranged adjacent to a first boundary of the active area, the gas extractor being controlled to extract the gas flow, and may further include controlling a gas inlet arranged adjacent to a second boundary of the active area, the gas inlet being controlled to provide the gas flow. Controlling the gas flow system (1104) may include controlling a gas extractor arranged at an axis of rotation of the rotational motion, the gas extractor being controlled to extract the gas flow. Controlling the gas flow system (1104) may further include controlling a gas inlet arranged at a portion of the receptacle wall, the gas inlet being controlled to provide the gas flow, and the gas inlet may include a plurality of openings that collectively surround the build floor.
  • In various embodiments, the energy beam source may include one or more energy beam generators, controlling the energy beam source (1103) may include applying one or more energy beams in a plurality of active areas of the layer of powder to selectively fuse a portion of the powder in each of the active areas, and controlling the gas flow system (1104) may include providing a gas flow across each of the active areas while the one or more energy beams selectively fuse the portion of the powder in each active area. The active areas may be non-overlapping. In various embodiments, the gas flow system may include a funnel-type gas manifold.
  • In various embodiments, controlling the gas flow system (1104) may include rotating a direction of the gas flow. The gas flow system may include a plurality of gas inlets and a plurality of gas extractors, and controlling the gas flow system (1104) may include rotating the gas flow by opening and closing the gas inlets and the gas extractors.
  • In various embodiments, an optional action (1105) may include varying a layer thickness of the selectively fused deposited powder during a build of the build piece. For example, this optional action may further include obtaining information of a geometric feature density, and controlling the motor system (1102) may include varying a speed of the rotational motion based on the geometric feature density.
  • FIG. 12 illustrates a flowchart of an example method of additively manufacturing a build piece according to various embodiments. The example method includes obtaining information (1201) of a build including a build piece, controlling a depositor system (1202) to deposit a layer of powder onto a build floor, controlling a motor system (1203) to cause a rotational motion between the depositor system and the build floor, such that the depositor system deposits the layer of powder during the rotational motion, and a receptacle wall contains the powder on the build floor, where controlling the motor system (1203) further includes varying a speed of the rotational motion based on the information of the build during the build of the build piece, and controlling an energy beam source (1204) to apply an energy beam in an active area of the layer of powder to selectively fuse a portion of the powder in the active area to form a portion of the build piece. For example, the information of the build may include a geometric feature density, and controlling the motor system (1202) may include varying the speed based on the geometric feature density. For example, varying the speed of the rotational motion may include increasing the speed when the geometric feature density is low and decreasing the speed when the geometric feature density is high. In this way, for example, an active time of the energy beam source can be used more efficiently and the build time of the build can be reduced.
  • In various embodiments, controlling the motor system (1203) may cause the rotational motion at least in part by rotating the build floor. The depositor system may be configured to remain stationary during the rotational motion. In various embodiments, controlling the motor system (1203) may cause the rotational motion at least in part by moving the depositor system in an arc over the build floor. In various embodiments, the receptacle wall may be configured to remain stationary during the rotational motion. In various embodiments, the receptacle wall may be configured to rotate with the build floor. The depositor system may include a plurality of depositors, and controlling the depositor system (1202) may include depositing a plurality of layers of powder simultaneously.
  • In various embodiments, the method can include one or more optional actions (1205), which is depicted as a dashed box in FIG. 12 to signify optionality. For example, the method may include an optional action (1205) of controlling a gas flow system to extract a gas created by the fusing of the powder. In another example, the method may include an optional action (1205) of covering a second area of the powder exclusive of the active area with a cover. In this way, for example, spatter, soot, etc. from the fusing may be prevented from falling onto portions of the powder bed or build piece. Another optional action (1205) may include controlling a heater configured to heat the powder under the cover, the heater being arranged in the cover. Another optional action (1205) may include controlling a sensor to sense a characteristic of the powder under the cover, wherein the sensor is arranged in the cover. Another optional action (1205) may include controlling a gas flow system. For example, a gas flow system may include a gas extractor arranged adjacent to a first boundary of the active area, the gas extractor being controlled to extract a gas flow. The gas flow system may include a gas inlet arranged adjacent to a second boundary of the active area, and controlling the gas flow system may further include controlling the gas inlet to provide the gas flow. Controlling a gas flow system may include controlling a gas extractor arranged at an axis of rotation of the rotational motion, wherein the gas extractor is controlled to extract a gas flow. The gas flow system may include a gas inlet arranged at a portion of the receptacle wall, and controlling the gas flow system may include controlling the gas inlet to provide the gas flow. The gas inlet may include a plurality of openings that collectively surround the build floor.
  • In various embodiments, the energy beam source may include one or more energy beam generators, and controlling the energy beam source (1204) may include applying one or more energy beams in a plurality of active areas of the layer of powder to selectively fuse a portion of the powder in each of the active areas, and an optional action (1205) may include controlling a gas flow system to provide a gas flow across each of the active areas while the one or more energy beams selectively fuse the portion of the powder in each active area. The active areas may be non-overlapping. The gas flow system may include a funnel-type gas manifold. Controlling a gas flow system may include rotating a direction of the gas flow across the active area. For example, controlling the gas flow system may include controlling a plurality of gas inlets and a plurality of gas extractors such that the gas flow system rotates the gas flow by opening and closing the gas inlets and the gas extractors. An optional action (1205) may include varying a layer thickness of the selectively fused deposited powder during a build of the build piece.
  • FIG. 13 illustrates a flowchart of an example method of additively manufacturing a build piece according to various embodiments. The example method includes controlling a depositor system (1301) to deposit a layer of powder onto a build floor, controlling a motor system (1302) to cause a rotational motion between the depositor system and the build floor, such that the depositor system deposits the layer of powder during the rotational motion, and a receptacle wall contains the powder on the build floor, controlling an energy beam source (1303) to apply an energy beam in an active area of the layer of powder to selectively fuse a portion of the powder in the active area to form a portion of a build piece, and varying a layer thickness (1304) of the selectively fused deposited powder during a build of the build piece.
  • In various embodiments, the depositor system may include a plurality of depositors, and controlling the depositor system (1301) may include controlling the plurality of depositors to deposit layers of powder simultaneously. The active area may include a plurality of active areas, each arranged after a different depositor of the plurality of depositors. A first depositor in the plurality of depositors may be arranged 180 degrees apart from a second depositor with respect to the rotational motion, the first depositor may be associated with a first active area of the plurality of active areas arranged after the first depositor, and the second depositor may be associated with a second active area of the plurality of active areas arranged after the second depositor. Varying the layer thickness (1304) of the selectively fused deposited powder may include controlling the energy beam source to fuse some portions of the powder layer in both the first and second active areas and to fuse other portions of the powder layer in only the first or second active area. For example, controlling the energy beam source (1303) may include fusing a portion of the build piece near the edge of the build piece by fusing in both the first and second active areas, and fusing a portion of the build piece in the interior bulk of the build piece in only the first or second active area. Controlling the energy beam source (1303) may include applying a plurality of energy beams simultaneously in the plurality of active areas.
  • In various embodiments, controlling the motor system (1302) may cause the rotational motion at least in part by rotating the build floor. The depositor system may be configured to remain stationary during the rotational motion. In various embodiments, controlling the motor system (1302) may cause the rotational motion at least in part by moving the depositor system in an arc over the build floor. The receptacle wall may be configured to remain stationary during the rotational motion.
  • In various embodiments, the method can include one or more optional actions (1305), which is depicted as a dashed box in FIG. 13 to signify optionality. For example, an optional action (1305) may include controlling a gas flow system to provide a gas flow across the active area. The gas flow system may extract a gas created by the fusing of the powder. Another optional action (1305) may include covering a second area of the powder exclusive of the active area with a cover. Another optional action (1305) may include controlling a heater to heat the powder under the cover, the heater being arranged in the cover. Another optional action (1305) may include controlling a sensor to sense a characteristic of the powder under the cover, the sensor being arranged in the cover.
  • In various embodiments, an optional action (1305) may include controlling a gas flow system to provide a gas flow across one or more active areas. For example, the gas flow system may include a gas extractor arranged adjacent to a first boundary of the active area, such that gas extractor extracts a gas flow. The gas flow system may include a gas inlet arranged adjacent to a second boundary of the active area, the gas inlet being configured to provide the gas flow. A gas flow system may include a gas extractor arranged at an axis of rotation of the rotational motion, such that the gas extractor extracts a gas flow. A gas flow system may include a gas inlet arranged at a portion of the receptacle wall, the gas inlet being configured to provide the gas flow. The gas inlet may include a plurality of openings that collectively surround the build floor.
  • In various embodiments, the energy beam source may include one or more energy beam generators, and controlling the energy beam source (1303) may include applying one or more energy beams in a plurality of active areas of the layer of powder to selectively fuse a portion of the powder in each of the active areas, and an optional action (1305) may include controlling a gas flow system to provide a gas flow across each of the active areas while the one or more energy beams selectively fuse the portion of the powder in each active area. The active areas may be non-overlapping. A gas flow system may include a funnel-type gas manifold to provide a gas flow across the active area. Controlling a gas flow system may include rotating a direction of a gas flow across the active area. For example, The gas flow system may include a plurality of gas inlets and a plurality of gas extractors, and controlling the gas flow system may include rotating the gas flow by opening and closing the gas inlets and the gas extractors. In various embodiments, an optional action (1305) may include varying a speed of the rotational motion based on a geometric feature density.
  • One skilled in the art will appreciate that the processes and apparatuses described herein are simply illustrative examples of a systems that lie within the scope of the present disclosure, and that variations to the components and techniques described may be used without departing from the scope of the present disclosure.
  • The previous description is provided to enable any person skilled in the art to practice the various aspects described herein. Various modifications to these exemplary embodiments presented throughout this disclosure will be readily apparent to those skilled in the art, and the concepts disclosed herein may be applied to other techniques for printing nodes and interconnects. Thus, the claims are not intended to be limited to the exemplary embodiments presented throughout the disclosure, but are to be accorded the full scope consistent with the language claims. All structural and functional equivalents to the elements of the exemplary embodiments described throughout this disclosure that are known or later come to be known to those of ordinary skill in the art are intended to be encompassed by the claims. Moreover, nothing disclosed herein is intended to be dedicated to the public regardless of whether such disclosure is explicitly recited in the claims. No claim element is to be construed under the provisions of 35 U.S.C. § 112(f), or analogous law in applicable jurisdictions, unless the element is expressly recited using the phrase “means for” or, in the case of a method claim, the element is recited using the phrase “step for.”

Claims (46)

1. An apparatus, comprising:
a build floor;
a depositor system configured to deposit a layer of powder onto the build floor;
a motor system configured to cause a rotational motion between the depositor system and the build floor, wherein the depositor system deposits the layer of powder during the rotational motion;
a receptacle wall configured to contain the powder on the build floor;
an energy beam source configured to apply an energy beam in an active area of the layer of powder to selectively fuse a portion of the powder in the active area to form a portion of a build piece; and
a gas flow system configured to provide a gas flow across the active area while the energy beam selectively fuses the portion of the layer of powder in the active area.
2. The apparatus of claim 1, wherein the motor system causes the rotational motion at least in part by rotating the build floor.
3. The apparatus of claim 2, wherein the depositor system is configured to remain stationary during the rotational motion.
4. The apparatus of claim 1, wherein the motor system causes the rotational motion at least in part by moving the depositor system in an arc over the build floor.
5. The apparatus of claim 1, wherein the receptacle wall is configured to remain stationary during the rotational motion.
6. The apparatus of claim 1, wherein the gas flow system extracts a gas created by the fusing of the powder.
7. The apparatus of claim 1, further comprising:
a cover configured to cover a second area of the powder exclusive of the active area.
8. The apparatus of claim 7, wherein the cover includes a heater configured to heat the powder under the cover.
9. The apparatus of claim 7, wherein the cover includes a sensor configured to sense a characteristic of the powder under the cover.
10. The apparatus of claim 1, wherein the gas flow system includes a gas extractor arranged adjacent to a first boundary of the active area, the gas extractor being configured to extract the gas flow.
11. The apparatus of claim 10, wherein the gas flow system further includes a gas inlet arranged adjacent to a second boundary of the active area, the gas inlet being configured to provide the gas flow.
12. The apparatus of claim 1, wherein the gas flow system includes a gas extractor arranged at an axis of rotation of the rotational motion, the gas extractor being configured to extract the gas flow.
13. The apparatus of claim 12, wherein the gas flow system further includes a gas inlet arranged at a portion of the receptacle wall, the gas inlet being configured to provide the gas flow.
14. The apparatus of claim 13, wherein the gas inlet includes a plurality of openings that collectively surround the build floor.
15. The apparatus of claim 1, wherein the energy beam source includes one or more energy beam generators, the energy beam source is configured to apply one or more energy beams in a plurality of active areas of the layer of powder to selectively fuse a portion of the powder in each of the active areas, and the gas flow system is configured to provide a gas flow across each of the active areas while the one or more energy beams selectively fuse the portion of the powder in each active area.
16. The apparatus of claim 15, wherein the active areas are non-overlapping.
17. The apparatus of claim 1, wherein the gas flow system includes a funnel-type gas manifold.
18. The apparatus of claim 1, wherein the gas flow system is further configured to rotate a direction of the gas flow.
19. The apparatus of claim 18, wherein the gas flow system includes a plurality of gas inlets and a plurality of gas extractors, and the gas flow system rotates the gas flow by opening and closing the gas inlets and the gas extractors.
20. The apparatus of claim 1, wherein a layer thickness of the selectively fused deposited powder is varied during a build of the build piece.
21. The apparatus of claim 1, wherein a speed of the rotational motion is varied based on a geometric feature density.
22. The apparatus of claim 1, wherein the depositor system includes a plurality of depositors, and the depositor system is configured to deposit a plurality of layers of powder simultaneously.
23-73. (canceled)
74. A method, comprising:
controlling a depositor system to deposit a layer of powder onto a build floor;
controlling a motor system to cause a rotational motion between the depositor system and the build floor, wherein the depositor system deposits the layer of powder during the rotational motion, and a receptacle wall contains the powder on the build floor;
controlling an energy beam source to apply an energy beam in an active area of the layer of powder to selectively fuse a portion of the powder in the active area to form a portion of a build piece; and
controlling a gas flow system to provide a gas flow across the active area while the energy beam selectively fuses the portion of the layer of powder in the active area.
75. The method of claim 74, wherein controlling the motor system causes the rotational motion at least in part by rotating the build floor.
76. The method of claim 74, wherein the depositor system is configured to remain stationary during the rotational motion.
77. The method of claim 74, wherein controlling the motor system causes the rotational motion at least in part by moving the depositor system in an arc over the build floor.
78. The method of claim 74, wherein the receptacle wall is configured to remain stationary during the rotational motion.
79. The method of claim 74, wherein controlling the gas flow system extracts a gas created by the fusing of the powder.
80. The method of claim 74, further comprising:
covering a second area of the powder exclusive of the active area with a cover.
81. The method of claim 80, further comprising:
controlling a heater configured to heat the powder under the cover, wherein the heater is arranged in the cover.
82. The method of claim 80, further comprising:
controlling a sensor to sense a characteristic of the powder under the cover, wherein the sensor is arranged in the cover.
83. The method of claim 74, wherein controlling the gas flow system includes controlling a gas extractor arranged adjacent to a first boundary of the active area, the gas extractor being controlled to extract the gas flow.
84. The method of claim 83, wherein controlling the gas flow system further includes controlling a gas inlet arranged adjacent to a second boundary of the active area, the gas inlet being controlled to provide the gas flow.
85. The method of claim 74, wherein controlling the gas flow system includes controlling a gas extractor arranged at an axis of rotation of the rotational motion, the gas extractor being controlled to extract the gas flow.
86. The method of claim 85, wherein controlling the gas flow system further includes controlling a gas inlet arranged at a portion of the receptacle wall, the gas inlet being controlled to provide the gas flow.
87. The method of claim 86, wherein the gas inlet includes a plurality of openings that collectively surround the build floor.
88. The method of claim 74, wherein the energy beam source includes one or more energy beam generators, controlling the energy beam source includes applying one or more energy beams in a plurality of active areas of the layer of powder to selectively fuse a portion of the powder in each of the active areas, and controlling the gas flow system includes providing a gas flow across each of the active areas while the one or more energy beams selectively fuse the portion of the powder in each active area.
89. The method of claim 88, wherein the active areas are non-overlapping.
90. The method of claim 74, wherein the gas flow system includes a funnel-type gas manifold.
91. The method of claim 74, wherein controlling the gas flow system includes rotating a direction of the gas flow.
92. The method of claim 91, wherein the gas flow system includes a plurality of gas inlets and a plurality of gas extractors, and controlling the gas flow system includes rotating the gas flow by opening and closing the gas inlets and the gas extractors.
93. The method of claim 74, further comprising:
varying a layer thickness of the selectively fused deposited powder during a build of the build piece.
94. The method of claim 74, further comprising:
obtaining information of a geometric feature density, wherein controlling the motor system includes varying a speed of the rotational motion based on the geometric feature density.
95. The method of claim 74, wherein the depositor system includes a plurality of depositors, and controlling the depositor system includes depositing a plurality of layers of powder simultaneously.
96-145. (canceled)
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