US20220288689A1 - Rotational additive manufacturing systems and methods - Google Patents
Rotational additive manufacturing systems and methods Download PDFInfo
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- US20220288689A1 US20220288689A1 US17/690,984 US202217690984A US2022288689A1 US 20220288689 A1 US20220288689 A1 US 20220288689A1 US 202217690984 A US202217690984 A US 202217690984A US 2022288689 A1 US2022288689 A1 US 2022288689A1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C64/00—Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
- B29C64/20—Apparatus for additive manufacturing; Details thereof or accessories therefor
- B29C64/227—Driving means
- B29C64/241—Driving means for rotary motion
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/20—Direct sintering or melting
- B22F10/28—Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM]
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/30—Process control
- B22F10/32—Process control of the atmosphere, e.g. composition or pressure in a building chamber
- B22F10/322—Process control of the atmosphere, e.g. composition or pressure in a building chamber of the gas flow, e.g. rate or direction
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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- B29C64/00—Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
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- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
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- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C64/00—Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
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- B29C64/364—Conditioning of environment
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- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
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- B22F12/13—Auxiliary heating means to preheat the material
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B22F12/00—Apparatus or devices specially adapted for additive manufacturing; Auxiliary means for additive manufacturing; Combinations of additive manufacturing apparatus or devices with other processing apparatus or devices
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
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- B22F2999/00—Aspects linked to processes or compositions used in powder metallurgy
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P10/00—Technologies related to metal processing
- Y02P10/25—Process efficiency
Definitions
- 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.
- FIG. 8 illustrates a top view of a PBF system in accordance with an aspect of the present disclosure.
- 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.
- 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.
- 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.
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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
- 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.
- 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. 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.
- 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.
- 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:
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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. - 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 (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.
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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 aconventional PBF system 100 during different stages of operation. The particular embodiment inFIGS. 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 ofFIGS. 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 ofFIGS. 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 adepositor 101 that can deposit each layer of metal powder, anenergy beam source 103 that can generate an energy beam, adeflector 105 that can apply the energy beam to fuse the powder material, and abuild plate 107 that can support one or more build pieces, such as abuild 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 abuild floor 111 positioned within a powder bed receptacle. The walls of thepowder bed receptacle 112 generally define the boundaries of the powder bed receptacle, which is sandwiched between thewalls 112 from the side and abuts a portion of thebuild floor 111 below.Build floor 111 can progressivelylower build plate 107 so thatdepositor 101 can deposit a next layer. The entire mechanism may reside in achamber 113 that can enclose the other components, thereby protecting the equipment, enabling atmospheric and temperature regulation and mitigating contamination risks.Depositor 101 can include ahopper 115 that contains apowder 117, such as a metal powder, and aleveler 119 that can level the top of each layer of deposited powder. - Referring specifically to
FIG. 1A , this figure showsPBF system 100 after a slice ofbuild piece 109 has been fused, but before the next layer of powder has been deposited. In fact,FIG. 1A illustrates a time at whichPBF system 100 has already deposited and fused slices in multiple layers, e.g., 200 individual layers, to form the current state ofbuild piece 109, e.g., formed of 200 individual slices. The multiple individual layers already deposited have created apowder bed 121, which includes powder that was deposited but not fused. -
FIG. 1B showsPBF system 100 at a stage in which buildfloor 111 can lower by apowder layer thickness 123. The lowering ofbuild floor 111 causesbuild piece 109 andpowder bed 121 to drop bypowder layer thickness 123, so that the top ofbuild piece 109 andpowder bed 121 are lower than the top of powderbed receptacle wall 112 by an amount equal to thepowder layer thickness 123. In this way, for example, a space with a consistent thickness equal topowder layer thickness 123 can be created over the tops ofbuild piece 109 andpowder bed 121. In this example, buildfloor 111 is lowered, but not rotated. -
FIG. 1C showsPBF system 100 at a stage in whichdepositor 101 is positioned to depositpowder 117 in a space created over the top surfaces ofbuild piece 109 andpowder bed 121 and bounded by powderbed receptacle walls 112. In this example,depositor 101 progressively moves over the defined space (linearly from left to right as viewed inFIG. 1C ) while releasingpowder 117 fromhopper 115.Leveler 119 can level the released powder to form apowder layer 125 that leaves powder layertop surface 126 configured to receive fusing energy fromenergy beam source 103.Powder layer 125 has a thickness substantially equal to the powder layer thickness 123 (seeFIG. 1B ). Thus, the powder in a PBF system can be supported by a powder material support structure, which can include, for example, abuild plate 107, abuild floor 111, abuild 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 toFIG. 1A . It should be noted that fusing of the powder is not occurring whiledepositor 101 is depositing powder. -
FIG. 1D showsPBF 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, andenergy beam source 103 generates anenergy beam 127 anddeflector 105 applies the energy beam to fuse the next slice inbuild piece 109. In various exemplary embodiments,energy beam source 103 can be an electron beam source, in whichcase 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 whichcase 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/ordeflector 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 withinPBF system 100. Such a device may be acomputer 150, which may include one or more components that may assist in the control ofPBF system 100.Computer 150 may communicate with aPBF system 100, and/or other AM systems, via one ormore interfaces 151. Thecomputer 150 and/orinterface 151 are examples of devices that may be configured to implement the various methods described herein, that may assist in controllingPBF system 100 and/or other AM systems. - In an aspect of the present disclosure,
computer 150 may comprise at least oneprocessor unit 152,memory 154,signal detector 156, a digital signal processor (DSP) 158, and one ormore 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 oneprocessor unit 152, which may assist in the control and/or operation ofPBF system 100. Theprocessor 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 theprocessor unit 152. A portion of thememory 154 may also include non-volatile random access memory (NVRAM). Theprocessor 152 typically performs logical and arithmetic operations based on program instructions stored within thememory 154. The instructions in thememory 154 may be executable (by theprocessor 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 asignal detector 156 that may be used to detect and quantify any level of signals received by thecomputer 150 for use by theprocessing unit 152 and/or other components of thecomputer 150. Thesignal detector 156 may detect such signals asenergy beam source 103 power,deflector 105 position, buildfloor 111 height, amount ofpowder 117 remaining indepositor 101,leveler 119 position, and other signals.Signal detector 156, in addition to or instead ofprocessor unit 152 may also control other components as described with respect to the present disclosure. Thecomputer 150 may also include aDSP 158 for use in processing signals received by thecomputer 150. TheDSP 158 may be configured to generate instructions and/or packets of instructions for transmission toPBF system 100. - The
computer 150 may further comprise auser interface 160 in some aspects. Theuser interface 160 may comprise a keypad, a pointing device, and/or a display. Theuser interface 160 may include any element or component that conveys information to a user of thecomputer 150 and/or receives input from the user. - The various components of the
computer 150 may be coupled together by aninterface 151. Theinterface 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 thecomputer 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, theprocessor unit 152 may be used to implement not only the functionality described above with respect to theprocessor unit 152, but also to implement the functionality described above with respect to thesignal detector 156, theDSP 158, and/or theuser interface 160. Further, each of the components illustrated inFIG. 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 powderbed receptacle wall 203 changes, as shown byplatform 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, ashaft 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 powderbed receptacle wall 203, adepositor 207, anenergy 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 powderbed receptacle wall 203 and aplatform 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 ofenergy beam source 209, and the energy beam source applies an energy beam to fuse portions of the powder layer to form a layer of abuild piece 219. Asenergy beam source 209 is applying the energy beam, gas inlet 211 can allow a gas to flow over the active area, andgas 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 powderbed receptacle walls 203 to allow for some removal or exit paths for any powder from thePBF system 200. As build floor 201 is lowered further, it may come into proximity withplatform knife 223. Build floor 201 may be configured to thread pastplatform 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 ofbuild 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 powderbed receptacle wall 203. Powderbed 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 powderbed 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 asPBF 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 thePBF system 100 shown inFIGS. 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 thanPBF system 100 of the related art. Further, the speed ofrotation 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 byPBF 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 ofrotation 202 can be increased when the geometric feature density related to buildpiece 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 inPBF 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 withPBF 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 theplatform 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 thebuild depth 253 ofPBF system 200 to remove powder fromPBF system 200 and buildpiece 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 abuild plate 302, a powderbed receptacle wall 304, adepositor 306, and a gas flow system that includes one ormore gas inlets 308 and anextractor 310.Active area 312 is shown to indicate the area for energy beams, e.g., lasers, etc. to sinter or fuse powder deposited bydepositor 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 indirection 314, and the layer of powder deposited bydepositor 306 is exposed inactive area 312. One or more energy beams then fuse or sinter the powder inactive 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 inactive area 312. These gases can be directed towardextractor 310, which may remove the byproducts and/or gases provided bygas inlet 308, from theactive 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 theactive area 312 can be controlled by controlling the rate and amount of gas flow fromgas inlet 308 and removal of gases byextractor 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 theactive area 312 can be controlled to be in a direction preferable to the gas flow. - As described herein,
gas inlet 308 andextractor 310 may provide a gas flow system forPBF system 300.Gas inlet 308 may be disposed or located around thebuild plate 302, andextractor 310 may be disposed or located at or near an axis of rotation of thebuild plate 302.Gas inlet 308 may collectively surround thebuild plate 302. Such a gas flow system may allow for the flow of introduced gases acrossactive area 312, removal of soot, fumes, spatter, and/or other byproducts of the build process from theactive 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 acrossactive 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 abuild plate 402, a powderbed receptacle wall 404, adepositor 406, and a gas flow system that includes one ormore gas inlets 408 and anextractor 410.Active area 412 is shown to indicate the area for energy beams, e.g., lasers, etc. to sinter or fuse powder deposited bydepositor 406. - In an aspect of the present disclosure, rather than build
plate 402 rotating as described with respect toFIG. 3 ,depositor 406,extractor 410, andactive area 412 may rotate or move in an arc motion with respect to thebuild plate 402. After depositor 406 (which may include a leveler to level the powder level) deposits a layer of powder, thedepositor 406,extractor 410, andactive area 412 rotate indirection 414, and the layer of powder deposited bydepositor 406 is exposed inactive area 412. Energy beams then fuse or sinter the powder inactive area 412. Other combination of rotational motions and/or stationary portions ofPBF 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 inactive area 412. These gases can be directed towardextractor 410, and may be located in powderbed receptacle wall 404, to help remove the byproducts and/or gases provided bygas inlet 408, from theactive area 412. In an aspect of the present disclosure, gas flow in and around theactive area 412 can be controlled by controlling the rate and amount of gas flow fromgas inlet 408 and removal of gases byextractor 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 theactive area 412 can be controlled to be in a direction preferable to the gas flow. - As described herein,
gas inlet 408 andextractor 410 may provide a gas flow system forPBF system 400.Gas inlet 408 may be disposed or located around thebuild plate 302, andextractor 310 may be disposed or located at or near an axis of rotation of thebuild plate 302.Gas inlet 308 may collectively surround thebuild plate 302. Such a gas flow system may allow for the flow of introduced gases acrossactive area 312, removal of soot, fumes, spatter, and/or other byproducts of the build process from theactive area 312, other gas flow controls, or any combination thereof, without departing from the scope of the present disclosure. - With respect to
FIG. 4 , acover 416 may be provided over some or all of thebuild 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 withcover 416 to protect the powder bed from spatter and/or other byproducts from the printing process. In various embodiments thecover 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 thecover 416 may be configured to heat up the deposited powder before fusing in theactive 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 incover 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 abuild plate 502, a powderbed receptacle wall 504, adepositor 506, and a gas flow system that includes one ormore gas inlets 508 and anextractor 510.Active area 512 is shown to indicate the area for energy beams, e.g., lasers, etc. to sinter or fuse powder deposited bydepositor 506. - In an aspect of the present disclosure,
gas inlets 508 may be located in powderbed receptacle wall 504, andextractor 510 may direct the flow of gas fromgas inlets 508 across theactive area 512 as shown byarrows 514. - In an aspect of the present disclosure, build
plate 502 may rotate indirection 516. In another aspect of the present disclosure, rather than buildplate 502 rotating,depositor 506,extractor 510, andactive area 512 may rotate. After depositor 506 (which may include a leveler to level the powder level) deposits a layer of powder, thedepositor 506,extractor 510, andactive area 512 rotate indirection 516, and the layer of powder deposited bydepositor 506 is exposed inactive area 512. Energy beams then fuse or sinter the powder inactive area 512. In another aspect of the present disclosure, buildplate 502 andextractor 510 may rotate. Asextractor 510 rotates across thegas inlets 508, extractor may direct gas fromgas inlets 508 along extractor and acrossactive 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 inactive area 512. These gases can be directed towardextractor 510. In an aspect of the present disclosure,gas inlets 508 may be located in powderbed receptacle wall 504, andextractor 510 may be configured to help remove the byproducts and/or gases provided bygas inlet 508 from theactive area 512. In an aspect of the present disclosure, gas flow in and around theactive area 512 can be controlled by controlling the rate and amount of gas flow fromgas inlet 508 and removal of gases byextractor 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 theactive 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 powderbed receptacle wall 602, which may enclose adepositor 604 and, optionally, a fullwidth depositor system 606. Fullwidth depositor system 606 may be considered to include two depositors because it deposits powder in two separate locations. As the build plate rotates indirection 608, two active areas may be operating:active area 1 610 andactive area 2 612, which may be operated on by different optics and/or different energy beams. A gas flow system may include agas inlet 618, an extractor 1 (614), and an extractor 2 (616). Eachactive area extractor 1 614 foractive area 1 610 andextractor 2 616 foractive area 2 612.Active area 1 610 andactive area 2 612 may be overlapping or non-overlapping.Depositor 604 anddepositor 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 powderbed receptacle wall 602, may be provided as part ofextractor 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 inFIG. 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 2X 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 μm, 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 abuild plate 702, a powderbed receptacle wall 704, adepositor 706, and a gas flow system that includes one ormore gas inlets 708, and anextractor 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 bydepositor 706. -
FIG. 7 illustrates an aspect of the present disclosure whereextractor 710 may direct a gas flow fromgas inlet 708 through and/or acrossextractor 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 onbuild plate 702. Whileextractor 710 may remove some of the fumes, soot, and/or other by products, the gas flow from gas inlet(s) 708 and gas flow throughextractor 710 may not be positioned properly to remove enough byproducts, or the byproducts may still be emitting from the melt pools after rotation of thebuild plate 702 indirection 716. As such, exhaust manifold 714 may be used to remove additional fumes, soot, and/or other byproducts from thePBF system 700, which may increase the efficiency ofPBF 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, andactive area 712 may rotate. As depositor 706 (which may include a leveler to level the powder level) deposits a layer of powder, thedepositor 706,extractor 710, andactive area 712 rotate indirection 716, and the layer of powder deposited bydepositor 706 is exposed inactive area 712. Energy beams then fuse or sinter the powder inactive 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., acrossactive 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 thebuild plate 702, and/or the rotation of the above-the-bed systems, may be synchronized with the opening and closing ofgas inlets 708 to allow for selection of variable gas flows acrossactive area 712 and/or other areas withinPBF 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 fromgas inlet 708 and removal of gases byextractor 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 theactive 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 abuild plate 802, a powderbed receptacle wall 804, adepositor 806, and a gas flow system that includes agas inlet 808 and anextractor 810.Active area 812 is shown to indicate the area for energy beams, e.g., lasers, etc. to sinter or fuse powder deposited bydepositor 806.Active area 812 has twopowder motion boundaries 813 and twonon-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, asbuild plate 802 rotates, the powder layer moves across one of thepowder motion boundaries 813 intoactive area 812, but the powder layer does not move across either of thenon-powder motion boundaries 815. Likewise, asbuild plate 802 continues to rotate, the powder layer (portions of which may now be fused) moves out ofactive area 812 across the other of thepowder 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 ofFIG. 8 , the gas flow system components, i.e.,gas inlet 808 andextractor 810, can be positioned substantially at the powder motion boundaries, which may allow a more laminar gas flow to be applied acrossactive 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 thepowder motion boundaries 813 are radial boundaries of the active area with respect to the rotational motion, and thenon-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 ofFIG. 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 , andFIG. 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 thePBF system 800 that is not interfering with the gas flow system or the active area, and is not necessarily adjacent toactive 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 directgas flow 814 acrossactive area 812 in a direction other than from the powderbed receptacle wall 804 towards the center ofPBF 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 byPBF system 800. -
FIG. 9 shows a perspective view of an extractor in accordance with an aspect of the present disclosure. Using the example ofextractor 810 ofFIG. 8 , although any extractor described herein can be configured as described with respect toFIG. 9 ,extractor 810 may remove buildbyproducts 900, e.g., soot, fumes, spatter, etc. fromactive area 812. Build byproducts may be created whenenergy 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 buildbyproducts 900 are captured withinextractor 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 ofbuild 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 powderbed receptacle wall 1004, adepositor 1006, and a gas flow system including agas inlet 1008 and anextractor 1010.Active area 1012 is shown to indicate the area for energy beams, e.g., lasers, etc. to sinter or fuse powder deposited bydepositor 1006. A build plate (which may be similar to those shown inFIGS. 2-8 ) receives powder deposited bydepositor 1006 and rotates indirection 1014 to expose different areas of deposited powder inactive 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., controlledcooling element 1018, to control cooling of the fused powder after fusing within theactive area 1012. Such cooling elements may be coupled to thecover 1002 such thatelements 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 theactive area 1012. After fusing, one or more controlledcooling 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 theactive area 1012. -
Cover 1002 may include various openings, e.g., such thatactive area 1012 is able to receive energy beams from one or more energy sources, an opening fordepositor 1006 to deposit powder, openings forextractor 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 controlledcooling 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, thePBF 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 toFIG. 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 (49)
1-22. (canceled)
23. 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; 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.
24. The apparatus of claim 23 , wherein the information of the build includes a geometric feature density, and the motor is 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.
25. The apparatus of claim 23 , wherein the motor system causes the rotational motion at least in part by rotating the build floor.
26. The apparatus of claim 25 , wherein the depositor system is configured to remain stationary during the rotational motion.
27. The apparatus of claim 23 , wherein the motor system causes the rotational motion at least in part by moving the depositor system in an arc over the build floor.
28. The apparatus of claim 23 , wherein the receptacle wall is configured to remain stationary during the rotational motion.
29. The apparatus of claim 23 , wherein a gas flow system extracts a gas created by the fusing of the powder.
30. The apparatus of claim 23 , further comprising:
a cover configured to cover a second area of the powder exclusive of the active area.
31. The apparatus of claim 30 , wherein the cover includes a heater configured to heat the powder under the cover.
32. The apparatus of claim 30 , wherein the cover includes a sensor configured to sense a characteristic of the powder under the cover.
33. The apparatus of claim 23 , further comprising a 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.
34. The apparatus of claim 33 , 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.
35. The apparatus of claim 23 , further comprising a 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.
36. The apparatus of claim 35 , 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.
37. The apparatus of claim 36 , wherein the gas inlet includes a plurality of openings that collectively surround the build floor.
38. The apparatus of claim 23 , 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 a 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.
39. The apparatus of claim 38 , wherein the active areas are non-overlapping.
40. The apparatus of claim 23 , wherein a gas flow system includes a funnel-type gas manifold.
41. The apparatus of claim 23 , wherein a gas flow system is further configured to rotate a direction of the gas flow.
42. The apparatus of claim 41 , 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.
43. The apparatus of claim 23 , wherein a layer thickness of the selectively fused deposited powder is varied during a build of the build piece.
44. The apparatus of claim 23 , wherein the information of the build includes a geometric feature density, and a speed of the rotational motion is varied based on the geometric feature density.
45. The apparatus of claim 23 , wherein the depositor system includes a plurality of depositors, and the depositor system is configured to deposit a plurality of layers of powder simultaneously.
46-95. (canceled)
96. A method, comprising:
obtaining information of 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 piece during a 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.
97. The method of claim 96 , wherein the information of the build piece includes a geometric feature density, and controlling the motor system includes varying the speed based on the geometric feature density.
98. The method of claim 96 , wherein controlling the motor system causes the rotational motion at least in part by rotating the build floor.
99. The method of claim 98 , wherein the depositor system is configured to remain stationary during the rotational motion.
100. The method of claim 96 , 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.
101. The method of claim 96 , wherein the receptacle wall is configured to remain stationary during the rotational motion.
102. The method of claim 96 , further comprising:
controlling a gas flow system to extract a gas created by the fusing of the powder.
103. The method of claim 96 , further comprising:
covering a second area of the powder exclusive of the active area with a cover.
104. The method of claim 103 , further comprising:
controlling a heater to heat the powder under the cover, wherein the heater is arranged in the cover.
105. The method of claim 103 , further comprising:
controlling a sensor to sense a characteristic of the powder under the cover, wherein the sensor is arranged in the cover.
106. The method of claim 96 , further comprising:
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.
107. The method of claim 106 , wherein 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.
108. The method of claim 96 , further comprising:
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.
109. The method of claim 108 , wherein 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.
110. The method of claim 109 , wherein the gas inlet includes a plurality of openings that collectively surround the build floor.
111. The method of claim 96 , 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, 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.
112. The method of claim 111 , wherein the active areas are non-overlapping.
113. The method of claim 111 , wherein the gas flow system includes a funnel-type gas manifold.
114. The method of claim 96 , further comprising:
controlling a gas flow system to rotate a direction of the gas flow across the active area.
115. The method of claim 114 , wherein 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.
116. The method of claim 96 , further comprising:
varying a layer thickness of the selectively fused deposited powder during a build of the build piece.
117. The method of claim 96 , wherein 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.
118. The method of claim 96 , wherein the depositor system includes a plurality of depositors, and controlling the depositor system includes depositing a plurality of layers of powder simultaneously.
119-145. (canceled)
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Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10940609B2 (en) * | 2017-07-25 | 2021-03-09 | Divergent Technologies, Inc. | Methods and apparatus for additively manufactured endoskeleton-based transport structures |
US10955200B2 (en) * | 2018-07-13 | 2021-03-23 | General Electric Company | Heat exchangers having a three-dimensional lattice structure with baffle cells and methods of forming baffles in a three-dimensional lattice structure of a heat exchanger |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20060108712A1 (en) * | 2002-08-02 | 2006-05-25 | Eos Gmbh Electro Optical Systems | Device and method for producing a three-dimensional object by means of a generative production method |
US20200108559A1 (en) * | 2018-10-05 | 2020-04-09 | General Electric Company | Additive manufacturing machine having reconfigurable gas nozzles |
US20200122389A1 (en) * | 2018-10-22 | 2020-04-23 | Hamilton Sundstrand Corporation | Rotating relative recoater and part orientation |
US20200223011A1 (en) * | 2017-07-28 | 2020-07-16 | Siemens Aktiengesellschaft | Installation for the Powder-Bed-Based Additive Manufacturing of a Workpiece, Comprising Multiple Metering Devices for Different Types of Powder |
US20200254566A1 (en) * | 2017-11-10 | 2020-08-13 | General Electric Company | Apparatus and method for angular and rotational additive manufacturing |
US20210394270A1 (en) * | 2020-06-18 | 2021-12-23 | Toyota Jidosha Kabushiki Kaisha | Laminate molding method and laminate molding apparatus |
Family Cites Families (306)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5203226A (en) | 1990-04-17 | 1993-04-20 | Toyoda Gosei Co., Ltd. | Steering wheel provided with luminous display device |
DE29507827U1 (en) | 1995-05-16 | 1995-07-20 | Edag Engineering + Design Ag, 36039 Fulda | Feeding device intended for feeding welding studs to a welding gun |
DE19518175A1 (en) | 1995-05-19 | 1996-11-21 | Edag Eng & Design Ag | Method for the automatic installation of a component of a motor vehicle body |
DE19519643B4 (en) | 1995-05-30 | 2005-09-22 | Edag Engineering + Design Ag | Bin shifting device |
US5990444A (en) | 1995-10-30 | 1999-11-23 | Costin; Darryl J. | Laser method and system of scribing graphics |
US6252196B1 (en) | 1996-10-11 | 2001-06-26 | Technolines Llc | Laser method of scribing graphics |
US5742385A (en) | 1996-07-16 | 1998-04-21 | The Boeing Company | Method of airplane interiors assembly using automated rotating laser technology |
WO1998024958A1 (en) | 1996-12-05 | 1998-06-11 | Teijin Limited | Fiber aggregate molding method |
US6010155A (en) | 1996-12-31 | 2000-01-04 | Dana Corporation | Vehicle frame assembly and method for manufacturing same |
US6140602A (en) | 1997-04-29 | 2000-10-31 | Technolines Llc | Marking of fabrics and other materials using a laser |
SE509041C2 (en) | 1997-10-23 | 1998-11-30 | Ssab Hardtech Ab | Vehicle impact protection beam |
DE19907015A1 (en) | 1999-02-18 | 2000-08-24 | Edag Eng & Design Ag | Clamping device that can be used in production lines for motor vehicles and production line with such a clamping device |
US6811744B2 (en) | 1999-07-07 | 2004-11-02 | Optomec Design Company | Forming structures from CAD solid models |
US6391251B1 (en) | 1999-07-07 | 2002-05-21 | Optomec Design Company | Forming structures from CAD solid models |
US6365057B1 (en) | 1999-11-01 | 2002-04-02 | Bmc Industries, Inc. | Circuit manufacturing using etched tri-metal media |
US6409930B1 (en) | 1999-11-01 | 2002-06-25 | Bmc Industries, Inc. | Lamination of circuit sub-elements while assuring registration |
US6468439B1 (en) | 1999-11-01 | 2002-10-22 | Bmc Industries, Inc. | Etching of metallic composite articles |
US6318642B1 (en) | 1999-12-22 | 2001-11-20 | Visteon Global Tech., Inc | Nozzle assembly |
US6585151B1 (en) | 2000-05-23 | 2003-07-01 | The Regents Of The University Of Michigan | Method for producing microporous objects with fiber, wire or foil core and microporous cellular objects |
US6919035B1 (en) | 2001-05-18 | 2005-07-19 | Ensci Inc. | Metal oxide coated polymer substrates |
JP3889940B2 (en) | 2001-06-13 | 2007-03-07 | 株式会社東海理化電機製作所 | Mold apparatus, method of using mold apparatus, and method of sharing mold apparatus |
DE50207123D1 (en) | 2001-08-31 | 2006-07-20 | Edag Eng & Design Ag | ROLLFALZKOPF AND METHOD FOR FOLDING A FLANGE |
ATE463322T1 (en) | 2001-11-02 | 2010-04-15 | Boeing Co | DEVICE AND METHOD FOR PRODUCING A WELDED JOINT WITH PATTERN-FORMING RESIDUAL PRESSURE STRESSES |
US6644721B1 (en) | 2002-08-30 | 2003-11-11 | Ford Global Technologies, Llc | Vehicle bed assembly |
DE10325906B4 (en) | 2003-06-05 | 2007-03-15 | Erwin Martin Heberer | Device for shielding coherent electromagnetic radiation and laser cabin with such a device |
DE102004014662A1 (en) | 2004-03-25 | 2005-10-13 | Audi Ag | Arrangement with a vehicle fuse and an analog / digital converter |
US7745293B2 (en) | 2004-06-14 | 2010-06-29 | Semiconductor Energy Laboratory Co., Ltd | Method for manufacturing a thin film transistor including forming impurity regions by diagonal doping |
ATE375830T1 (en) | 2004-09-24 | 2007-11-15 | Edag Eng & Design Ag | BLARING DEVICE AND BLARING PROCESS WITH COMPONENT PROTECTION |
US20060108783A1 (en) | 2004-11-24 | 2006-05-25 | Chi-Mou Ni | Structural assembly for vehicles and method of making same |
DE102005004474B3 (en) | 2005-01-31 | 2006-08-31 | Edag Engineering + Design Ag | Beading device and crimping method for transferring a crimping web of a component about a crimping edge |
DE102005030944B4 (en) | 2005-06-30 | 2007-08-02 | Edag Engineering + Design Ag | Method and device for joining joining structures, in particular in the assembly of vehicle components |
WO2007036942A2 (en) | 2005-09-28 | 2007-04-05 | Dip Tech. Ltd. | Ink providing etch-like effect for printing on ceramic surfaces |
US7716802B2 (en) | 2006-01-03 | 2010-05-18 | The Boeing Company | Method for machining using sacrificial supports |
DE102006014282A1 (en) | 2006-03-28 | 2007-10-04 | Edag Engineering + Design Ag | Clamping system for sheet metal components to be joined comprises two beds which hold components and can be fastened together by couplings mounted at their ends which push them together |
DE102006014279A1 (en) | 2006-03-28 | 2007-10-04 | Edag Engineering + Design Ag | Clamping device comprising connecting components (B1,B2), component receivers, a clamping structure, a robot structure and sub-stations |
JP2007292048A (en) | 2006-03-29 | 2007-11-08 | Yamaha Motor Co Ltd | Exhaust apparatus for straddle-type vehicle and straddle-type vehicle |
US8599301B2 (en) | 2006-04-17 | 2013-12-03 | Omnivision Technologies, Inc. | Arrayed imaging systems having improved alignment and associated methods |
DE102006021755A1 (en) | 2006-05-10 | 2007-11-15 | Edag Engineering + Design Ag | Energy beam soldering or welding of components |
JP2007317750A (en) | 2006-05-23 | 2007-12-06 | Matsushita Electric Ind Co Ltd | Imaging device |
DE102006038795A1 (en) | 2006-08-18 | 2008-03-20 | Fft Edag Produktionssysteme Gmbh & Co. Kg | Monitoring device for a laser processing device |
EP1900709B1 (en) | 2006-09-14 | 2010-06-09 | Ibiden Co., Ltd. | Method for manufacturing honeycomb structured body and material composition for honeycomb fired body |
DE202006018552U1 (en) | 2006-12-08 | 2007-02-22 | Edag Engineering + Design Ag | Handheld, optionally motor-driven tool for beading sheet metal, used e.g. in automobile bodywork repair or prototyping, includes roller spring-loaded against adjustable jaw |
US7344186B1 (en) | 2007-01-08 | 2008-03-18 | Ford Global Technologies, Llc | A-pillar structure for an automotive vehicle |
DE102007002856B4 (en) | 2007-01-15 | 2012-02-09 | Edag Gmbh & Co. Kgaa | Device for flanging and welding or soldering of components |
EP1949981B1 (en) | 2007-01-18 | 2015-04-29 | Toyota Motor Corporation | Composite of sheet metal parts |
DE202007003110U1 (en) | 2007-03-02 | 2007-08-02 | Edag Engineering + Design Ag | Car for making it easy for a passenger to get out has a bodywork with side parts limiting a passenger compartment, door openings and fixed and moving roof areas |
US7710347B2 (en) | 2007-03-13 | 2010-05-04 | Raytheon Company | Methods and apparatus for high performance structures |
DE102007022102B4 (en) | 2007-05-11 | 2014-04-10 | Fft Edag Produktionssysteme Gmbh & Co. Kg | Beading of components in series production with short cycle times |
DE202007007838U1 (en) | 2007-06-01 | 2007-09-13 | Edag Engineering + Design Ag | Roller flanging tool used in the production of a wheel housing, sliding roof, engine hood and mudguards comprises a support structure, arms connected to each other in a connecting section and flanging rollers |
GB0712027D0 (en) | 2007-06-21 | 2007-08-01 | Materials Solutions | Rotating build plate |
US20090014919A1 (en) | 2007-07-13 | 2009-01-15 | Advanced Ceramics Manufacturing Llc | Aggregate-based mandrels for composite part production and composite part production methods |
WO2009014233A1 (en) | 2007-07-20 | 2009-01-29 | Nippon Steel Corporation | Hydroforming method, and hydroformed parts |
US9818071B2 (en) | 2007-12-21 | 2017-11-14 | Invention Science Fund I, Llc | Authorization rights for operational components |
US9071436B2 (en) | 2007-12-21 | 2015-06-30 | The Invention Science Fund I, Llc | Security-activated robotic system |
US8286236B2 (en) | 2007-12-21 | 2012-10-09 | The Invention Science Fund I, Llc | Manufacturing control system |
US8429754B2 (en) | 2007-12-21 | 2013-04-23 | The Invention Science Fund I, Llc | Control technique for object production rights |
US8752166B2 (en) | 2007-12-21 | 2014-06-10 | The Invention Science Fund I, Llc | Security-activated operational components |
US9128476B2 (en) | 2007-12-21 | 2015-09-08 | The Invention Science Fund I, Llc | Secure robotic operational system |
US9626487B2 (en) | 2007-12-21 | 2017-04-18 | Invention Science Fund I, Llc | Security-activated production device |
DE102008003067B4 (en) | 2008-01-03 | 2013-05-29 | Edag Gmbh & Co. Kgaa | Method and bending tool for bending a workpiece |
US7908922B2 (en) | 2008-01-24 | 2011-03-22 | Delphi Technologies, Inc. | Silicon integrated angular rate sensor |
DE102008008306A1 (en) | 2008-02-07 | 2009-08-13 | Edag Gmbh & Co. Kgaa | turntable |
DE102008013591B4 (en) | 2008-03-11 | 2010-02-18 | Edag Gmbh & Co. Kgaa | Tool, plant and method for producing a wiring harness |
DE102008047800B4 (en) | 2008-05-09 | 2021-11-18 | Fft Produktionssysteme Gmbh & Co. Kg | Method and tool for producing a fixing connection on positively joined components |
EP2279061B1 (en) | 2008-05-21 | 2014-07-16 | FFT EDAG Produktionssysteme GmbH & Co. KG | Clamping frame-less joining of components |
WO2009154484A2 (en) | 2008-06-20 | 2009-12-23 | Business Intelligence Solutions Safe B.V. | Methods, apparatus and systems for data visualization and related applications |
US8383028B2 (en) | 2008-11-13 | 2013-02-26 | The Boeing Company | Method of manufacturing co-molded inserts |
US8452073B2 (en) | 2009-04-08 | 2013-05-28 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Closed-loop process control for electron beam freeform fabrication and deposition processes |
DE102009018619B4 (en) | 2009-04-27 | 2014-07-17 | Fft Edag Produktionssysteme Gmbh & Co. Kg | robot support |
DE102009018618B4 (en) | 2009-04-27 | 2018-09-06 | Fft Produktionssysteme Gmbh & Co. Kg | Clamping device, system and method for processing of changing component types |
DE102009024344B4 (en) | 2009-06-09 | 2011-02-24 | Edag Gmbh & Co. Kgaa | Method and tool for flanging a workpiece |
DE202009012432U1 (en) | 2009-09-15 | 2010-01-28 | Edag Gmbh & Co. Kgaa | body component |
US8354170B1 (en) | 2009-10-06 | 2013-01-15 | Hrl Laboratories, Llc | Elastomeric matrix composites |
US8610761B2 (en) | 2009-11-09 | 2013-12-17 | Prohectionworks, Inc. | Systems and methods for optically projecting three-dimensional text, images and/or symbols onto three-dimensional objects |
US8606540B2 (en) | 2009-11-10 | 2013-12-10 | Projectionworks, Inc. | Hole measurement apparatuses |
US8755923B2 (en) | 2009-12-07 | 2014-06-17 | Engineering Technology Associates, Inc. | Optimization system |
US8686997B2 (en) | 2009-12-18 | 2014-04-01 | Sassault Systemes | Method and system for composing an assembly |
EP2383669B1 (en) | 2010-04-02 | 2018-07-11 | Dassault Systèmes | Design of a part modeled by parallel geodesic curves |
CN103384898A (en) | 2010-06-21 | 2013-11-06 | 约翰·吉利斯 | Computer implemented tool box systems and methods |
US8289352B2 (en) | 2010-07-15 | 2012-10-16 | HJ Laboratories, LLC | Providing erasable printing with nanoparticles |
US8978535B2 (en) | 2010-08-11 | 2015-03-17 | Massachusetts Institute Of Technology | Articulating protective system for resisting mechanical loads |
EP2799150B1 (en) | 2013-05-02 | 2016-04-27 | Hexagon Technology Center GmbH | Graphical application system |
US9858604B2 (en) | 2010-09-24 | 2018-01-02 | Amazon Technologies, Inc. | Vendor interface for item delivery via 3D manufacturing on demand |
US9684919B2 (en) | 2010-09-24 | 2017-06-20 | Amazon Technologies, Inc. | Item delivery using 3D manufacturing on demand |
US9672550B2 (en) | 2010-09-24 | 2017-06-06 | Amazon Technologies, Inc. | Fulfillment of orders for items using 3D manufacturing on demand |
US9898776B2 (en) | 2010-09-24 | 2018-02-20 | Amazon Technologies, Inc. | Providing services related to item delivery via 3D manufacturing on demand |
US9566758B2 (en) | 2010-10-19 | 2017-02-14 | Massachusetts Institute Of Technology | Digital flexural materials |
US9502993B2 (en) | 2011-02-07 | 2016-11-22 | Ion Geophysical Corporation | Method and apparatus for sensing signals |
EP2495292B1 (en) | 2011-03-04 | 2013-07-24 | FFT EDAG Produktionssysteme GmbH & Co. KG | Joining surface treatment device and method |
EP2714375A1 (en) | 2011-06-02 | 2014-04-09 | A. Raymond et Cie | Fasteners manufactured by three-dimensional printing |
US9246299B2 (en) | 2011-08-04 | 2016-01-26 | Martin A. Stuart | Slab laser and amplifier |
US9101979B2 (en) | 2011-10-31 | 2015-08-11 | California Institute Of Technology | Methods for fabricating gradient alloy articles with multi-functional properties |
US10011089B2 (en) | 2011-12-31 | 2018-07-03 | The Boeing Company | Method of reinforcement for additive manufacturing |
DE102012101939A1 (en) | 2012-03-08 | 2013-09-12 | Klaus Schwärzler | Method and device for the layered construction of a shaped body |
US9566742B2 (en) | 2012-04-03 | 2017-02-14 | Massachusetts Institute Of Technology | Methods and apparatus for computer-assisted spray foam fabrication |
WO2013173742A1 (en) | 2012-05-18 | 2013-11-21 | 3D Systems, Inc. | Adhesive for 3d printing |
US8873238B2 (en) | 2012-06-11 | 2014-10-28 | The Boeing Company | Chassis system and method for holding and protecting electronic modules |
US9533526B1 (en) | 2012-06-15 | 2017-01-03 | Joel Nevins | Game object advances for the 3D printing entertainment industry |
WO2013192599A1 (en) | 2012-06-21 | 2013-12-27 | Massachusetts Institute Of Technology | Methods and apparatus for digital material skins |
US9672389B1 (en) | 2012-06-26 | 2017-06-06 | The Mathworks, Inc. | Generic human machine interface for a graphical model |
EP2689865B1 (en) | 2012-07-27 | 2016-09-14 | FFT Produktionssysteme GmbH & Co. KG | Hemming press |
WO2014019998A1 (en) | 2012-07-30 | 2014-02-06 | Materialise Nv | Systems and methods for forming and utilizing bending maps for object design |
US8437513B1 (en) | 2012-08-10 | 2013-05-07 | EyeVerify LLC | Spoof detection for biometric authentication |
US10029415B2 (en) | 2012-08-16 | 2018-07-24 | Stratasys, Inc. | Print head nozzle for use with additive manufacturing system |
US9389315B2 (en) | 2012-12-19 | 2016-07-12 | Basf Se | Detector comprising a transversal optical sensor for detecting a transversal position of a light beam from an object and a longitudinal optical sensor sensing a beam cross-section of the light beam in a sensor region |
US9329020B1 (en) | 2013-01-02 | 2016-05-03 | Lockheed Martin Corporation | System, method, and computer program product to provide wireless sensing based on an aggregate magnetic field reading |
US9244986B2 (en) | 2013-01-11 | 2016-01-26 | Buckyball Mobile, Inc. | Method and system for interactive geometric representations, configuration and control of data |
US9609755B2 (en) | 2013-01-17 | 2017-03-28 | Hewlett-Packard Development Company, L.P. | Nanosized particles deposited on shaped surface geometries |
US9626489B2 (en) | 2013-03-13 | 2017-04-18 | Intertrust Technologies Corporation | Object rendering systems and methods |
US20140277669A1 (en) | 2013-03-15 | 2014-09-18 | Sikorsky Aircraft Corporation | Additive topology optimized manufacturing for multi-functional components |
US9764415B2 (en) | 2013-03-15 | 2017-09-19 | The United States Of America As Represented By The Administrator Of Nasa | Height control and deposition measurement for the electron beam free form fabrication (EBF3) process |
US9555580B1 (en) | 2013-03-21 | 2017-01-31 | Temper Ip, Llc. | Friction stir welding fastener |
US9156205B2 (en) | 2013-03-22 | 2015-10-13 | Markforged, Inc. | Three dimensional printer with composite filament fabrication |
US9126365B1 (en) | 2013-03-22 | 2015-09-08 | Markforged, Inc. | Methods for composite filament fabrication in three dimensional printing |
US9149988B2 (en) | 2013-03-22 | 2015-10-06 | Markforged, Inc. | Three dimensional printing |
US9186848B2 (en) | 2013-03-22 | 2015-11-17 | Markforged, Inc. | Three dimensional printing of composite reinforced structures |
EP3725497B1 (en) | 2013-03-22 | 2024-07-03 | Markforged, Inc. | Three-dimensional printer |
WO2014169238A1 (en) | 2013-04-11 | 2014-10-16 | Digimarc Corporation | Methods for object recognition and related arrangements |
KR20160003785A (en) | 2013-04-26 | 2016-01-11 | 디에스엠 아이피 어셋츠 비.브이. | Vinyl functionalized urethane resins for powder coating compositions |
EP2805800B1 (en) | 2013-05-22 | 2015-09-16 | FFT EDAG Produktionssysteme GmbH & Co. KG | Joining of a workpiece with concealed seam |
ES2541428T3 (en) | 2013-06-07 | 2015-07-20 | Fft Produktionssysteme Gmbh & Co. Kg | Device for use in handling a load and procedure for manufacturing such a device |
KR102246139B1 (en) | 2013-06-13 | 2021-04-30 | 바스프 에스이 | Detector for optically detecting at least one object |
EP2813432B1 (en) | 2013-06-13 | 2017-12-20 | Airbus Operations GmbH | Method of installing a fixture |
KR102252336B1 (en) | 2013-06-13 | 2021-05-14 | 바스프 에스이 | Optical detector and method for manufacturing the same |
US9724877B2 (en) | 2013-06-23 | 2017-08-08 | Robert A. Flitsch | Methods and apparatus for mobile additive manufacturing of advanced structures and roadways |
US9688032B2 (en) | 2013-07-01 | 2017-06-27 | GM Global Technology Operations LLC | Thermoplastic component repair |
GB201313839D0 (en) | 2013-08-02 | 2013-09-18 | Rolls Royce Plc | Method of Manufacturing a Component |
GB201313841D0 (en) | 2013-08-02 | 2013-09-18 | Rolls Royce Plc | Method of Manufacturing a Component |
GB201313840D0 (en) | 2013-08-02 | 2013-09-18 | Rolls Royce Plc | Method of Manufacturing a Component |
US9665182B2 (en) | 2013-08-19 | 2017-05-30 | Basf Se | Detector for determining a position of at least one object |
AU2014310703B2 (en) | 2013-08-19 | 2018-09-27 | Basf Se | Optical detector |
US10197338B2 (en) | 2013-08-22 | 2019-02-05 | Kevin Hans Melsheimer | Building system for cascading flows of matter and energy |
US10052820B2 (en) | 2013-09-13 | 2018-08-21 | Made In Space, Inc. | Additive manufacturing of extended structures |
US9823143B2 (en) | 2013-10-07 | 2017-11-21 | United Technologies Corporation | Additively grown enhanced impact resistance features for improved structure and joint protection |
US9248611B2 (en) | 2013-10-07 | 2016-02-02 | David A. Divine | 3-D printed packaging |
US10086568B2 (en) | 2013-10-21 | 2018-10-02 | Made In Space, Inc. | Seamless scanning and production devices and methods |
US10725451B2 (en) | 2013-10-21 | 2020-07-28 | Made In Space, Inc. | Terrestrial and space-based manufacturing systems |
AU2014351882B2 (en) | 2013-11-21 | 2017-11-30 | Covestro (Netherlands) B.V. | Thermosetting powder coating compositions comprising methyl-substituted benzoyl peroxide |
EP3071393A1 (en) | 2013-11-21 | 2016-09-28 | SABIC Global Technologies B.V. | Reduced density article |
WO2015074158A1 (en) | 2013-11-25 | 2015-05-28 | 7D Surgical Inc. | System and method for generating partial surface from volumetric data for registration to surface topology image data |
US9604124B2 (en) | 2013-12-05 | 2017-03-28 | Aaron Benjamin Aders | Technologies for transportation |
US9555315B2 (en) | 2013-12-05 | 2017-01-31 | Aaron Benjamin Aders | Technologies for transportation |
EP2886448B1 (en) | 2013-12-20 | 2017-03-08 | Airbus Operations GmbH | A load bearing element and a method for manufacturing a load bearing element |
TW201527070A (en) | 2014-01-06 | 2015-07-16 | Prior Company Ltd | Decoration film and manufacturing method thereof and manufacturing method of decorated molding article |
WO2015105024A1 (en) | 2014-01-10 | 2015-07-16 | 勝義 近藤 | Titanium powder material, titanium material, and method for producing oxygen solid solution titanium powder material |
CN106413944B (en) | 2014-01-24 | 2019-06-14 | 近藤胜义 | Being dissolved the titanium valve powder material for having nitrogen, titanium and solid solution has the preparation method of titanium valve powder material of nitrogen |
US9424503B2 (en) | 2014-08-11 | 2016-08-23 | Brian Kieser | Structurally encoded component and method of manufacturing structurally encoded component |
WO2015126329A1 (en) | 2014-02-24 | 2015-08-27 | Singapore University Of Technology And Design | Verification methods and verification devices |
US9817922B2 (en) | 2014-03-01 | 2017-11-14 | Anguleris Technologies, Llc | Method and system for creating 3D models from 2D data for building information modeling (BIM) |
US9782936B2 (en) | 2014-03-01 | 2017-10-10 | Anguleris Technologies, Llc | Method and system for creating composite 3D models for building information modeling (BIM) |
US9703896B2 (en) | 2014-03-11 | 2017-07-11 | Microsoft Technology Licensing, Llc | Generation of custom modular objects |
US10006156B2 (en) | 2014-03-21 | 2018-06-26 | Goodrich Corporation | Systems and methods for calculated tow fiber angle |
US9765226B2 (en) | 2014-03-27 | 2017-09-19 | Disney Enterprises, Inc. | Ultraviolet printing with luminosity control |
US10294982B2 (en) | 2014-03-28 | 2019-05-21 | The Boeing Company | Systems, methods, and apparatus for supported shafts |
US10018576B2 (en) | 2014-04-09 | 2018-07-10 | Texas Instruments Incorporated | Material detection and analysis using a dielectric waveguide |
KR101588762B1 (en) | 2014-04-09 | 2016-01-26 | 현대자동차 주식회사 | A Front Body Member of a Vehicle |
US9597843B2 (en) | 2014-05-15 | 2017-03-21 | The Boeing Company | Method and apparatus for layup tooling |
JP6675325B2 (en) | 2014-05-16 | 2020-04-01 | ダイバージェント テクノロジーズ, インコーポレイテッドDivergent Technologies, Inc. | Modularly formed nodes for vehicle chassis and methods of using them |
US9643361B2 (en) | 2014-05-27 | 2017-05-09 | Jian Liu | Method and apparatus for three-dimensional additive manufacturing with a high energy high power ultrafast laser |
US10074128B2 (en) | 2014-06-08 | 2018-09-11 | Shay C. Colson | Pre-purchase mechanism for autonomous vehicles |
DE202014102800U1 (en) | 2014-06-17 | 2014-06-27 | Fft Produktionssysteme Gmbh & Co. Kg | Segmented component support |
KR101795994B1 (en) | 2014-06-20 | 2017-12-01 | 벨로3디, 인크. | Apparatuses, systems and methods for three-dimensional printing |
CN111746446B (en) | 2014-07-25 | 2023-10-10 | 沙特基础工业全球技术有限公司 | Crushable polymer stringer extensions, systems, and methods of making and using the same |
EP3177863B1 (en) | 2014-08-04 | 2023-10-11 | Washington State University | Vapor cooled shielding liner for cryogenic storage in composite pressure vessels |
US9783324B2 (en) | 2014-08-26 | 2017-10-10 | The Boeing Company | Vessel insulation assembly |
JP5688669B1 (en) | 2014-09-09 | 2015-03-25 | グラフェンプラットフォーム株式会社 | Graphite-based carbon material used as graphene precursor, graphene dispersion containing the same, graphene composite, and method for producing the same |
US9696238B2 (en) | 2014-09-16 | 2017-07-04 | The Boeing Company | Systems and methods for icing flight tests |
MX2017003309A (en) | 2014-09-24 | 2017-06-23 | Holland Lp | Grating connector and spacer apparatus, system, and methods of using the same. |
US10285219B2 (en) | 2014-09-25 | 2019-05-07 | Aurora Flight Sciences Corporation | Electrical curing of composite structures |
US9854828B2 (en) | 2014-09-29 | 2018-01-02 | William Langeland | Method, system and apparatus for creating 3D-printed edible objects |
US10081140B2 (en) | 2014-10-29 | 2018-09-25 | The Boeing Company | Apparatus for and method of compaction of a prepreg |
US10108766B2 (en) | 2014-11-05 | 2018-10-23 | The Boeing Company | Methods and apparatus for analyzing fatigue of a structure and optimizing a characteristic of the structure based on the fatigue analysis |
EP3018051A1 (en) | 2014-11-06 | 2016-05-11 | Airbus Operations GmbH | Structural component and method for producing a structural component |
US10022792B2 (en) | 2014-11-13 | 2018-07-17 | The Indian Institute of Technology | Process of dough forming of polymer-metal blend suitable for shape forming |
EP3218248B1 (en) | 2014-11-13 | 2019-01-09 | SABIC Global Technologies B.V. | Drag reducing aerodynamic vehicle components and methods of making the same |
US10016852B2 (en) | 2014-11-13 | 2018-07-10 | The Boeing Company | Apparatuses and methods for additive manufacturing |
US9915527B2 (en) | 2014-11-17 | 2018-03-13 | The Boeing Company | Detachable protective coverings and protection methods |
DE102014116938A1 (en) | 2014-11-19 | 2016-05-19 | Airbus Operations Gmbh | Production of components of a vehicle using additive layer manufacturing |
WO2016079494A2 (en) | 2014-11-21 | 2016-05-26 | Renishaw Plc | Additive manufacturing apparatus and methods |
US9600929B1 (en) | 2014-12-01 | 2017-03-21 | Ngrain (Canada) Corporation | System, computer-readable medium and method for 3D-differencing of 3D voxel models |
US9595795B2 (en) | 2014-12-09 | 2017-03-14 | Te Connectivity Corporation | Header assembly |
DE102014225488A1 (en) | 2014-12-10 | 2016-06-16 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Retarded crystallization polymer composition, crystallization behavior affecting additive composition, method of reducing the crystallization point, and use of an additive composition |
US20160167303A1 (en) | 2014-12-15 | 2016-06-16 | Arcam Ab | Slicing method |
US10160278B2 (en) | 2014-12-16 | 2018-12-25 | Aktv8 LLC | System and method for vehicle stabilization |
US9789922B2 (en) | 2014-12-18 | 2017-10-17 | The Braun Corporation | Modified door opening of a motorized vehicle for accommodating a ramp system and method thereof |
US9821339B2 (en) | 2014-12-19 | 2017-11-21 | Palo Alto Research Center Incorporated | System and method for digital fabrication of graded, hierarchical material structures |
US9486960B2 (en) | 2014-12-19 | 2016-11-08 | Palo Alto Research Center Incorporated | System for digital fabrication of graded, hierarchical material structures |
US9854227B2 (en) | 2015-01-08 | 2017-12-26 | David G Grossman | Depth sensor |
DE102015100659B4 (en) | 2015-01-19 | 2023-01-05 | Fft Produktionssysteme Gmbh & Co. Kg | Flanging system, flanging unit and flanging process for self-sufficient flanging |
US9718434B2 (en) | 2015-01-21 | 2017-08-01 | GM Global Technology Operations LLC | Tunable energy absorbers |
GB2534582A (en) | 2015-01-28 | 2016-08-03 | Jaguar Land Rover Ltd | An impact energy absorbing device for a vehicle |
US10449737B2 (en) | 2015-03-04 | 2019-10-22 | Ebert Composites Corporation | 3D thermoplastic composite pultrusion system and method |
US9616623B2 (en) | 2015-03-04 | 2017-04-11 | Ebert Composites Corporation | 3D thermoplastic composite pultrusion system and method |
US10124546B2 (en) | 2015-03-04 | 2018-11-13 | Ebert Composites Corporation | 3D thermoplastic composite pultrusion system and method |
US9731773B2 (en) | 2015-03-11 | 2017-08-15 | Caterpillar Inc. | Node for a space frame |
EP3271419B1 (en) | 2015-03-16 | 2022-08-03 | SHPP Global Technologies B.V. | Fibrillated polymer compositions and methods of their manufacture |
US10065367B2 (en) | 2015-03-20 | 2018-09-04 | Chevron Phillips Chemical Company Lp | Phonon generation in bulk material for manufacturing |
US10040239B2 (en) | 2015-03-20 | 2018-08-07 | Chevron Phillips Chemical Company Lp | System and method for writing an article of manufacture into bulk material |
US9611667B2 (en) | 2015-05-05 | 2017-04-04 | West Virginia University | Durable, fire resistant, energy absorbing and cost-effective strengthening systems for structural joints and members |
WO2016179441A1 (en) | 2015-05-07 | 2016-11-10 | Massachusetts Institute Of Technology | Digital material assembly by passive means and modular isotropic lattice extruder system (miles) |
EP3090948A1 (en) | 2015-05-08 | 2016-11-09 | Raymond R M Wang | Airflow modification apparatus and method |
US9481402B1 (en) | 2015-05-26 | 2016-11-01 | Honda Motor Co., Ltd. | Methods and apparatus for supporting vehicle components |
US9796137B2 (en) | 2015-06-08 | 2017-10-24 | The Boeing Company | Additive manufacturing methods |
US9963978B2 (en) | 2015-06-09 | 2018-05-08 | Ebert Composites Corporation | 3D thermoplastic composite pultrusion system and method |
WO2017018935A1 (en) | 2015-07-24 | 2017-02-02 | Nanyang Technological University | Hopper for powder bed fusion additive manufacturing |
US10232550B2 (en) | 2015-07-31 | 2019-03-19 | The Boeing Company | Systems for additively manufacturing composite parts |
US10343355B2 (en) | 2015-07-31 | 2019-07-09 | The Boeing Company | Systems for additively manufacturing composite parts |
US10166752B2 (en) | 2015-07-31 | 2019-01-01 | The Boeing Company | Methods for additively manufacturing composite parts |
US10289875B2 (en) | 2015-07-31 | 2019-05-14 | Portland State University | Embedding data on objects using surface modulation |
US10343330B2 (en) | 2015-07-31 | 2019-07-09 | The Boeing Company | Systems for additively manufacturing composite parts |
US10201941B2 (en) | 2015-07-31 | 2019-02-12 | The Boeing Company | Systems for additively manufacturing composite parts |
CN107922014B (en) | 2015-08-14 | 2020-11-27 | 斯克拉佩阿莫尔股份有限公司 | Vehicle protection device |
EP3135442B1 (en) | 2015-08-26 | 2018-12-19 | Airbus Operations GmbH | Robot system and method of operating a robot system |
EP3135566B1 (en) | 2015-08-28 | 2020-11-25 | EDAG Engineering GmbH | Vehicle lightweight construction structure with flexible manufacturing |
US9957031B2 (en) | 2015-08-31 | 2018-05-01 | The Boeing Company | Systems and methods for manufacturing a tubular structure |
US9789548B2 (en) | 2015-08-31 | 2017-10-17 | The Boeing Company | Geodesic structure forming systems and methods |
DE202015104709U1 (en) | 2015-09-04 | 2015-10-13 | Edag Engineering Gmbh | Mobile communication device and software code as well as traffic entity |
US9590699B1 (en) | 2015-09-11 | 2017-03-07 | Texas Instuments Incorporated | Guided near field communication for short range data communication |
WO2017046121A1 (en) | 2015-09-14 | 2017-03-23 | Trinamix Gmbh | 3d camera |
US9718302B2 (en) | 2015-09-22 | 2017-08-01 | The Boeing Company | Decorative laminate with non-visible light activated material and system and method for using the same |
EP3360118B1 (en) | 2015-10-07 | 2021-03-31 | Michael D. Velez | Flow alarm |
CN108368469A (en) | 2015-10-07 | 2018-08-03 | 加利福尼亚大学校董会 | The multi-modal sensor of graphene system |
DE202015105595U1 (en) | 2015-10-21 | 2016-01-14 | Fft Produktionssysteme Gmbh & Co. Kg | Absolute robot-assisted positioning method |
US9676145B2 (en) | 2015-11-06 | 2017-06-13 | Velo3D, Inc. | Adept three-dimensional printing |
US10022912B2 (en) | 2015-11-13 | 2018-07-17 | GM Global Technology Operations LLC | Additive manufacturing of a unibody vehicle |
US9846933B2 (en) | 2015-11-16 | 2017-12-19 | General Electric Company | Systems and methods for monitoring components |
US10048769B2 (en) | 2015-11-18 | 2018-08-14 | Ted Selker | Three-dimensional computer-aided-design system user interface |
WO2017087036A1 (en) | 2015-11-20 | 2017-05-26 | University Of South Florida | Shape-morphing space frame apparatus using unit cell bistable elements |
JP2018537596A (en) | 2015-11-21 | 2018-12-20 | エーティーエス エムイーアール,エルエルシー | System and method for forming a layer on the surface of a solid substrate and product formed thereby |
US10436038B2 (en) | 2015-12-07 | 2019-10-08 | General Electric Company | Turbine engine with an airfoil having a tip shelf outlet |
WO2017100695A1 (en) | 2015-12-10 | 2017-06-15 | Velo3D, Inc. | Skillful three-dimensional printing |
US10343331B2 (en) | 2015-12-22 | 2019-07-09 | Carbon, Inc. | Wash liquids for use in additive manufacturing with dual cure resins |
US10350823B2 (en) | 2015-12-22 | 2019-07-16 | Carbon, Inc. | Dual precursor resin systems for additive manufacturing with dual cure resins |
US10289263B2 (en) | 2016-01-08 | 2019-05-14 | The Boeing Company | Data acquisition and encoding process linking physical objects with virtual data for manufacturing, inspection, maintenance and repair |
US10294552B2 (en) | 2016-01-27 | 2019-05-21 | GM Global Technology Operations LLC | Rapidly solidified high-temperature aluminum iron silicon alloys |
US10339266B2 (en) | 2016-02-16 | 2019-07-02 | Board Of Regents Of The University Of Texas Systems | Mechanisms for constructing spline surfaces to provide inter-surface continuity |
US20170239719A1 (en) | 2016-02-18 | 2017-08-24 | Velo3D, Inc. | Accurate three-dimensional printing |
US10336050B2 (en) | 2016-03-07 | 2019-07-02 | Thermwood Corporation | Apparatus and methods for fabricating components |
US10011685B2 (en) | 2016-03-11 | 2018-07-03 | The Boeing Company | Polyarylether ketone imide adhesives |
US9976063B2 (en) | 2016-03-11 | 2018-05-22 | The Boeing Company | Polyarylether ketone imide sulfone adhesives |
US10234342B2 (en) | 2016-04-04 | 2019-03-19 | Xerox Corporation | 3D printed conductive compositions anticipating or indicating structural compromise |
WO2017184778A1 (en) | 2016-04-20 | 2017-10-26 | Arconic Inc. | Fcc materials of aluminum, cobalt and nickel, and products made therefrom |
CA3016761A1 (en) | 2016-04-20 | 2017-10-26 | Arconic Inc. | Fcc materials of aluminum, cobalt, iron and nickel, and products made therefrom |
US10393315B2 (en) | 2016-04-26 | 2019-08-27 | Ford Global Technologies, Llc | Cellular structures with twelve-cornered cells |
CN113001987B (en) | 2016-05-24 | 2023-12-26 | 戴弗根特技术有限公司 | System and method for additive manufacturing of transport structures |
EP3248758B1 (en) | 2016-05-24 | 2021-02-17 | Airbus Operations GmbH | System and method for handling a component |
US10384393B2 (en) | 2016-05-27 | 2019-08-20 | Florida State University Research Foundation, Inc. | Polymeric ceramic precursors, apparatuses, systems, and methods |
JP2019527138A (en) | 2016-06-09 | 2019-09-26 | ダイバージェント テクノロジーズ, インコーポレイテッドDivergent Technologies, Inc. | Systems and methods for arc and node design and fabrication |
US10275564B2 (en) | 2016-06-17 | 2019-04-30 | The Boeing Company | System for analysis of a repair for a structure |
US10286452B2 (en) | 2016-06-29 | 2019-05-14 | Velo3D, Inc. | Three-dimensional printing and three-dimensional printers |
WO2018027166A2 (en) | 2016-08-04 | 2018-02-08 | The Regents Of The University Of Michigan | Fiber-reinforced 3d printing |
US10254499B1 (en) | 2016-08-05 | 2019-04-09 | Southern Methodist University | Additive manufacturing of active devices using dielectric, conductive and magnetic materials |
US10465281B2 (en) | 2016-08-15 | 2019-11-05 | U.S.A. As Represented By The Administrator Of The National Aeronautics And Space Administration | High resolution additive manufacturing method with real materials |
US9933092B2 (en) | 2016-08-18 | 2018-04-03 | Deflecto, LLC | Tubular structures and knurling systems and methods of manufacture and use thereof |
US10359756B2 (en) | 2016-08-23 | 2019-07-23 | Echostar Technologies Llc | Dynamic 3D object recognition and printing |
US10179640B2 (en) | 2016-08-24 | 2019-01-15 | The Boeing Company | Wing and method of manufacturing |
US10220881B2 (en) | 2016-08-26 | 2019-03-05 | Ford Global Technologies, Llc | Cellular structures with fourteen-cornered cells |
US10392131B2 (en) | 2016-08-26 | 2019-08-27 | The Boeing Company | Additive manufactured tool assembly |
US10291193B2 (en) | 2016-09-02 | 2019-05-14 | Texas Instruments Incorporated | Combining power amplifiers at millimeter wave frequencies |
US10429006B2 (en) | 2016-10-12 | 2019-10-01 | Ford Global Technologies, Llc | Cellular structures with twelve-cornered cells |
US10214248B2 (en) | 2016-11-14 | 2019-02-26 | Hall Labs Llc | Tripartite support mechanism for frame-mounted vehicle components |
US9879981B1 (en) | 2016-12-02 | 2018-01-30 | General Electric Company | Systems and methods for evaluating component strain |
US10015908B2 (en) | 2016-12-07 | 2018-07-03 | The Boeing Company | System and method for cryogenic cooling of electromagnetic induction filter |
US10210662B2 (en) | 2016-12-09 | 2019-02-19 | Fyusion, Inc. | Live augmented reality using tracking |
US9996945B1 (en) | 2016-12-12 | 2018-06-12 | Fyusion, Inc. | Live augmented reality guides |
US10017384B1 (en) | 2017-01-06 | 2018-07-10 | Nanoclear Technologies Inc. | Property control of multifunctional surfaces |
DE102017200191A1 (en) | 2017-01-09 | 2018-07-12 | Ford Global Technologies, Llc | Smoothing a surface of an article formed from a plastic |
US10071525B2 (en) | 2017-02-07 | 2018-09-11 | Thermwood Corporation | Apparatus and method for printing long composite thermoplastic parts on a dual gantry machine during additive manufacturing |
US10392097B2 (en) | 2017-02-16 | 2019-08-27 | The Boeing Company | Efficient sub-structures |
US10087320B2 (en) | 2017-02-17 | 2018-10-02 | Polydrop, Llc | Conductive polymer-matrix compositions and uses thereof |
US10337542B2 (en) | 2017-02-28 | 2019-07-02 | The Boeing Company | Curtain retention bracket |
US20180250745A1 (en) | 2017-03-02 | 2018-09-06 | Velo3D, Inc. | Three-dimensional printing of three-dimensional objects |
US10356395B2 (en) | 2017-03-03 | 2019-07-16 | Fyusion, Inc. | Tilts as a measure of user engagement for multiview digital media representations |
US10068316B1 (en) | 2017-03-03 | 2018-09-04 | Fyusion, Inc. | Tilts as a measure of user engagement for multiview digital media representations |
US10440351B2 (en) | 2017-03-03 | 2019-10-08 | Fyusion, Inc. | Tilts as a measure of user engagement for multiview interactive digital media representations |
US10343725B2 (en) | 2017-03-03 | 2019-07-09 | GM Global Technology Operations LLC | Automotive structural component and method of manufacture |
US20180281282A1 (en) | 2017-03-28 | 2018-10-04 | Velo3D, Inc. | Material manipulation in three-dimensional printing |
US10178800B2 (en) | 2017-03-30 | 2019-01-08 | Honeywell International Inc. | Support structure for electronics having fluid passageway for convective heat transfer |
WO2018187611A1 (en) | 2017-04-05 | 2018-10-11 | Aerion Intellectual Property Management Corporation | Solid modeler that provides spatial gradients of 3d cad models of solid objects |
US10237477B2 (en) | 2017-05-22 | 2019-03-19 | Fyusion, Inc. | Loop closure |
US10313651B2 (en) | 2017-05-22 | 2019-06-04 | Fyusion, Inc. | Snapshots at predefined intervals or angles |
US10200677B2 (en) | 2017-05-22 | 2019-02-05 | Fyusion, Inc. | Inertial measurement unit progress estimation |
US10343724B2 (en) | 2017-06-02 | 2019-07-09 | Gm Global Technology Operations Llc. | System and method for fabricating structures |
US10221530B2 (en) | 2017-06-12 | 2019-03-05 | Driskell Holdings, LLC | Directional surface marking safety and guidance devices and systems |
US10391710B2 (en) | 2017-06-27 | 2019-08-27 | Arevo, Inc. | Deposition of non-uniform non-overlapping curvilinear segments of anisotropic filament to form non-uniform layers |
US10389410B2 (en) | 2017-06-29 | 2019-08-20 | Texas Instruments Incorporated | Integrated artificial magnetic launch surface for near field communication system |
US10461810B2 (en) | 2017-06-29 | 2019-10-29 | Texas Instruments Incorporated | Launch topology for field confined near field communication system |
US10425793B2 (en) | 2017-06-29 | 2019-09-24 | Texas Instruments Incorporated | Staggered back-to-back launch topology with diagonal waveguides for field confined near field communication system |
US10171578B1 (en) | 2017-06-29 | 2019-01-01 | Texas Instruments Incorporated | Tapered coax launch structure for a near field communication system |
US10572963B1 (en) | 2017-07-14 | 2020-02-25 | Synapse Technology Corporation | Detection of items |
DE202017104785U1 (en) | 2017-08-09 | 2017-09-07 | Edag Engineering Gmbh | Bearing for cab of a vehicle |
DE202017105281U1 (en) | 2017-09-01 | 2017-09-11 | Fft Produktionssysteme Gmbh & Co. Kg | Trolley for transporting and positioning an aircraft component |
DE102017120422B4 (en) | 2017-09-05 | 2020-07-23 | Edag Engineering Gmbh | Swivel joint with an additional degree of freedom |
DE102017120384B4 (en) | 2017-09-05 | 2023-03-16 | Fft Produktionssysteme Gmbh & Co. Kg | Filling device for filling air conditioning systems with CO2 |
DE202017105474U1 (en) | 2017-09-08 | 2018-12-14 | Edag Engineering Gmbh | Material-optimized connection node |
DE202017105475U1 (en) | 2017-09-08 | 2018-12-12 | Edag Engineering Gmbh | Generatively manufactured battery holder |
US10421496B2 (en) | 2017-09-15 | 2019-09-24 | Honda Motor Co., Ltd. | Panoramic roof stiffener reinforcement |
US10356341B2 (en) | 2017-10-13 | 2019-07-16 | Fyusion, Inc. | Skeleton-based effects and background replacement |
US10882252B2 (en) | 2017-12-15 | 2021-01-05 | International Business Machines Corporation | Variable force deposition for printing applications |
CN111655453A (en) | 2017-12-28 | 2020-09-11 | 株式会社尼康 | Rotary energy beam for three-dimensional printing apparatus |
US10382739B1 (en) | 2018-04-26 | 2019-08-13 | Fyusion, Inc. | Visual annotation using tagging sessions |
US10310197B1 (en) | 2018-09-17 | 2019-06-04 | Waymo Llc | Transmitter devices having bridge structures |
US20200156290A1 (en) | 2018-11-15 | 2020-05-21 | General Electric Company | Centrifugal additive manufacturing apparatus and method |
JP7120122B2 (en) | 2019-03-29 | 2022-08-17 | 新東工業株式会社 | Additive manufacturing system and removal method |
US20200391289A1 (en) | 2019-06-11 | 2020-12-17 | General Electric Company | Additive manufacturing systems and methods including controllable vane that directs gas flow |
DE102019122286B4 (en) | 2019-08-20 | 2024-09-19 | Kumovis GmbH | 3D printer for 3D printing of plastics for medical applications |
-
2022
- 2022-03-09 US US17/690,901 patent/US20220288850A1/en not_active Abandoned
- 2022-03-09 EP EP22767940.4A patent/EP4304865A1/en active Pending
- 2022-03-09 CN CN202280018162.0A patent/CN116917129A/en active Pending
- 2022-03-09 WO PCT/US2022/019642 patent/WO2022192465A1/en active Application Filing
- 2022-03-09 US US17/690,959 patent/US11845130B2/en active Active
- 2022-03-09 US US17/690,984 patent/US20220288689A1/en not_active Abandoned
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20060108712A1 (en) * | 2002-08-02 | 2006-05-25 | Eos Gmbh Electro Optical Systems | Device and method for producing a three-dimensional object by means of a generative production method |
US20200223011A1 (en) * | 2017-07-28 | 2020-07-16 | Siemens Aktiengesellschaft | Installation for the Powder-Bed-Based Additive Manufacturing of a Workpiece, Comprising Multiple Metering Devices for Different Types of Powder |
US20200254566A1 (en) * | 2017-11-10 | 2020-08-13 | General Electric Company | Apparatus and method for angular and rotational additive manufacturing |
US20200108559A1 (en) * | 2018-10-05 | 2020-04-09 | General Electric Company | Additive manufacturing machine having reconfigurable gas nozzles |
US20200122389A1 (en) * | 2018-10-22 | 2020-04-23 | Hamilton Sundstrand Corporation | Rotating relative recoater and part orientation |
US20210394270A1 (en) * | 2020-06-18 | 2021-12-23 | Toyota Jidosha Kabushiki Kaisha | Laminate molding method and laminate molding apparatus |
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US11845130B2 (en) | 2023-12-19 |
CN116917129A (en) | 2023-10-20 |
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WO2022192465A1 (en) | 2022-09-15 |
US20220288850A1 (en) | 2022-09-15 |
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