US20230313352A1 - Apparatus and process for producing additive manufactured metal matrix composites and article of manufacture thereof - Google Patents

Apparatus and process for producing additive manufactured metal matrix composites and article of manufacture thereof Download PDF

Info

Publication number
US20230313352A1
US20230313352A1 US18/331,566 US202318331566A US2023313352A1 US 20230313352 A1 US20230313352 A1 US 20230313352A1 US 202318331566 A US202318331566 A US 202318331566A US 2023313352 A1 US2023313352 A1 US 2023313352A1
Authority
US
United States
Prior art keywords
substrate
sheet
layer
powdered
metal
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
US18/331,566
Inventor
Robert Swartz
John Bayldon
Buckley Crist
Eugene Gore
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Impossible Objects Inc
Original Assignee
Impossible Objects Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Impossible Objects Inc filed Critical Impossible Objects Inc
Priority to US18/331,566 priority Critical patent/US20230313352A1/en
Assigned to IMPOSSIBLE OBJECTS, INC. reassignment IMPOSSIBLE OBJECTS, INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: BAYLDON, JOHN, CRIST, Buckley, GORE, Eugene, SWARTZ, ROBERT
Publication of US20230313352A1 publication Critical patent/US20230313352A1/en
Pending legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C47/00Making alloys containing metallic or non-metallic fibres or filaments
    • C22C47/02Pretreatment of the fibres or filaments
    • C22C47/025Aligning or orienting the fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/20Direct sintering or melting
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/10Formation of a green body
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/30Process control
    • B22F10/31Calibration of process steps or apparatus settings, e.g. before or during manufacturing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/60Treatment of workpieces or articles after build-up
    • B22F10/66Treatment of workpieces or articles after build-up by mechanical means
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F12/00Apparatus or devices specially adapted for additive manufacturing; Auxiliary means for additive manufacturing; Combinations of additive manufacturing apparatus or devices with other processing apparatus or devices
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/02Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite layers
    • B22F7/04Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite layers with one or more layers not made from powder, e.g. made from solid metal
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C64/00Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
    • B29C64/10Processes of additive manufacturing
    • B29C64/165Processes of additive manufacturing using a combination of solid and fluid materials, e.g. a powder selectively bound by a liquid binder, catalyst, inhibitor or energy absorber
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C64/00Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
    • B29C64/10Processes of additive manufacturing
    • B29C64/188Processes of additive manufacturing involving additional operations performed on the added layers, e.g. smoothing, grinding or thickness control
    • B29C64/194Processes of additive manufacturing involving additional operations performed on the added layers, e.g. smoothing, grinding or thickness control during lay-up
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C64/00Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
    • B29C64/20Apparatus for additive manufacturing; Details thereof or accessories therefor
    • B29C64/205Means for applying layers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C67/00Shaping techniques not covered by groups B29C39/00 - B29C65/00, B29C70/00 or B29C73/00
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B33ADDITIVE MANUFACTURING TECHNOLOGY
    • B33YADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y10/00Processes of additive manufacturing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B33ADDITIVE MANUFACTURING TECHNOLOGY
    • B33YADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y30/00Apparatus for additive manufacturing; Details thereof or accessories therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B33ADDITIVE MANUFACTURING TECHNOLOGY
    • B33YADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y40/00Auxiliary operations or equipment, e.g. for material handling
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B33ADDITIVE MANUFACTURING TECHNOLOGY
    • B33YADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y40/00Auxiliary operations or equipment, e.g. for material handling
    • B33Y40/20Post-treatment, e.g. curing, coating or polishing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B33ADDITIVE MANUFACTURING TECHNOLOGY
    • B33YADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y70/00Materials specially adapted for additive manufacturing
    • B33Y70/10Composites of different types of material, e.g. mixtures of ceramics and polymers or mixtures of metals and biomaterials
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B33ADDITIVE MANUFACTURING TECHNOLOGY
    • B33YADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y80/00Products made by additive manufacturing
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C47/00Making alloys containing metallic or non-metallic fibres or filaments
    • C22C47/02Pretreatment of the fibres or filaments
    • C22C47/06Pretreatment of the fibres or filaments by forming the fibres or filaments into a preformed structure, e.g. using a temporary binder to form a mat-like element
    • C22C47/062Pretreatment of the fibres or filaments by forming the fibres or filaments into a preformed structure, e.g. using a temporary binder to form a mat-like element from wires or filaments only
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C47/00Making alloys containing metallic or non-metallic fibres or filaments
    • C22C47/20Making alloys containing metallic or non-metallic fibres or filaments by subjecting to pressure and heat an assembly comprising at least one metal layer or sheet and one layer of fibres or filaments
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C49/00Alloys containing metallic or non-metallic fibres or filaments
    • C22C49/14Alloys containing metallic or non-metallic fibres or filaments characterised by the fibres or filaments
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/60Treatment of workpieces or articles after build-up
    • B22F10/62Treatment of workpieces or articles after build-up by chemical means
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/70Recycling
    • B22F10/73Recycling of powder
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F12/00Apparatus or devices specially adapted for additive manufacturing; Auxiliary means for additive manufacturing; Combinations of additive manufacturing apparatus or devices with other processing apparatus or devices
    • B22F12/50Means for feeding of material, e.g. heads
    • B22F12/53Nozzles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/02Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite layers
    • B22F7/04Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite layers with one or more layers not made from powder, e.g. made from solid metal
    • B22F2007/042Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite layers with one or more layers not made from powder, e.g. made from solid metal characterised by the layer forming method
    • B22F2007/045Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite layers with one or more layers not made from powder, e.g. made from solid metal characterised by the layer forming method accompanied by fusion or impregnation
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2201/00Treatment under specific atmosphere
    • B22F2201/01Reducing atmosphere
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2998/00Supplementary information concerning processes or compositions relating to powder metallurgy
    • B22F2998/10Processes characterised by the sequence of their steps
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2999/00Aspects linked to processes or compositions used in powder metallurgy
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/02Compacting only
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/10Sintering only
    • B22F3/1035Liquid phase sintering
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/10Sintering only
    • B22F3/1039Sintering only by reaction
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/06Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
    • B22F7/062Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/06Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
    • B22F7/08Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools with one or more parts not made from powder
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C64/00Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
    • B29C64/10Processes of additive manufacturing
    • B29C64/106Processes of additive manufacturing using only liquids or viscous materials, e.g. depositing a continuous bead of viscous material
    • B29C64/112Processes of additive manufacturing using only liquids or viscous materials, e.g. depositing a continuous bead of viscous material using individual droplets, e.g. from jetting heads
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P10/00Technologies related to metal processing
    • Y02P10/25Process efficiency

Definitions

  • the present invention relates generally to three-dimensional fabrication.
  • This approach has a number of advantages including: the ability to produce more complex geometries than conventional methods such as milling and casting; improved material properties over conventional metals; higher production rates; the elimination of complex fixturing, complex tool paths and tool changes; and, in the case of casting, the need for patterns and tools.
  • FIG. 1 is a metal piece made by the method described in this application.
  • FIG. 2 is a flowchart illustrating the steps to produce a 3D metal object in accordance with the teachings of the present invention.
  • FIG. 3 shows an apparatus used to selectively deposit liquid (to which powder adheres), in an illustrative implementation of this invention.
  • FIG. 4 is a high-level block diagram of processors, in an illustrative implementation of this invention
  • FIG. 5 shows a compressive device, after a number of substrate tiles (layers) have been placed in it, one on top of the other in a compressive device. The tiles are aligned by inserting registration pins of the compressive device into the registration holes of each tile, respectively.
  • FIG. 6 shows a compressive device, after substrate layers with all of the “slices” of a ring torus have been inserted into it. Springs in the compressive device press the substrate layers together.
  • FIG. 7 is a block diagram that shows a processor that controls multiple components of an apparatus for fabricating a 3D object.
  • FIG. 1 is a metal piece 100 made by the method described in this application. The method of making this metal piece is described in detail below.
  • FIG. 2 is a flowchart illustrating the steps to produce a 3D metal object in accordance with the teachings of the present invention:
  • Step 102 Generate a CAD model (Step 102 ) which is sliced into layers (Step 104 ) by using a slicer program like Netfabb as described in (International Publication No. WO 2014/134224 A2. ⁇ 0055; see also US Application Nos. U.S. 61/528,537 and U.S. 61/769,724).
  • Each slice also includes registration holes, which will be used to orient each printed layer of substrate within the finished object exactly (International Publication No. WO 2014/134224 A2, ⁇ 00121).
  • the output of the slicer which for example may be a bitmap file, is sent to an inkjet printer (Step 106 ).
  • the printer selectively prints a fluid onto a sheet of substrate material (Step 108 ) (International Publication No. WO 2014/134224 A2. ⁇ 00113).
  • the fluid may either be the bonding agent itself in liquid form; or it may be a liquid to which a powdered bonding agent adheres.
  • Substrates can include fiberglass, high temperature glass fibers, boron fibers, or carbon fibers.
  • powdered bonding agent If powdered bonding agent is being used, it is flooded onto the printed substrate (International Publication No. WO 2014/134224 A2. ⁇ 0059). The powder adheres to the printed areas. Excess powder is removed, either by a stream of air, vacuum, vibration, or other mechanical means.
  • the coated sheets of substrate are stacked in press or clamp (Step 110 ) (International Publication No. WO 2014/134224 A2, ⁇ 00124), using the registration holes of each layer to align the printed portions of each sheet within the stack (International Publication No. WO 2014/134224 A2, ⁇ 00106).
  • the unfused substrate around the 3D object is then removed (Step 114 ), usually by abrasive blasting material or chemical means (International Publication No. WO 2014/134224 A2, ⁇ 0081).
  • the substrate used is a non-woven carbon fiber veil such as available from Hollingsworth and Vose. Veils that have been metal coated can also be used.
  • the veil or substrate is printed as described above on an inkjet printer using, for example, a HP45 thermal inkjet head with a solution primarily of de-ionized water, pyrrolidone and alcohol.
  • the solution may have an anti-evaporant including glycols and pyrrolidones.
  • This fluid is printed on the area of the substrate that would be part of the object, i.e., the printed area corresponds to a layer shape for the object. This is done for each layer as described in the previous applications.
  • Each layer is flooded with a metal powder for example a solder powder.
  • the excess powder is removed by mechanical, vacuum, vibration or compressed air or a combination of such methods. This leaves the solder powder selectively deposited.
  • a metal powder for example a solder powder.
  • the excess powder is removed by mechanical, vacuum, vibration or compressed air or a combination of such methods. This leaves the solder powder selectively deposited.
  • One of the problems with using a metal powder in a process of this kind is that the powder oxidizes so that that when heated to its melting point the particles of the powder will not fuse together well.
  • a powder flux such as rosin which acts as a reducing agent.
  • a typical flux to metal powder ratio is about 50/50.
  • Another method is to melt the powders in a reducing, vacuum and/or inert atmosphere oven. In this way other metals or alloys can be used, such as aluminum, steel, stainless steel, copper, brass, and titanium among others.
  • liquid flux may be used as or in combination with the
  • the metal powder can be mixed with a powder flux before it is deposited on the substrate. Then all the layers of the object are printed and stacked in register as described in the earlier applications. They are compressed and heated as described in the earlier applications. The heating temperature is raised to the melting point of the powder. The layers fuse together and produce a build block. After the build block is removed from the compression jig the build block is abrasively blasted and the areas where no powder adhered, that is the portions of the object that were not coated with metal, are abrasive blasted off, the uncoated carbon fiber being very fragile. What is left is a three dimensional carbon fiber metal composite of the part that was represented by the CAD model.
  • FIG. 3 shows an apparatus used to selectively deposit liquid (to which powder adheres), in an illustrative implementation of this invention.
  • Registration guide pins 501 are inserted through a substrate layer 503 in order to properly align the substrate layer 503 .
  • a solenoid valve, or inkjet head or heads 505 are used to selectively dispense liquid from a liquid reservoir 507 though a nozzle 509 unto the substrate layer 503 .
  • the nozzle 509 is rastered in a 2D plane 510 that is parallel to, and above, the substrate layer 503 , so that the liquid is selectively deposited at desired x, y coordinates of the substrate layer 503 , and not deposited in other areas of the substrate layer 503 .
  • a stepper motor 511 actuates two belts (not shown) that causes a support member (not shown) to move along two rails (not shown) in a direction parallel to the x axis.
  • a second stepper motor (not shown) and third belt (not shown) are mounted on the support member, and are used to move a nozzle support (not shown) in a direction parallel to the y axis.
  • the nozzle 509 is attached to the nozzle support. Together, the two stepper motors can move the nozzle 509 to any desired x, y coordinate above the substrate layer.
  • a page wide head may also be used.
  • a microprocessor 513 controls the stepper motors and the solenoid valve or inkjet head, thereby controlling when and where liquid is dispensed on the substrate layer 503 .
  • the stepper motors may cause the nozzle or nozzles 509 to move in other 2D patterns in the 2D plane to cause the liquid to be deposited at certain x, y coordinates.
  • FIG. 2 does not show an apparatus for heating and pressing multiple layers of substrate, or for removing excess substrate. In some implementations, the substrate layer is moved to a different position before those steps occur.
  • FIG. 4 is a high-level block diagram of processors, in an illustrative implementation of this invention.
  • a CAD model of a desired 3D object in STL file format is created using a remote processor 601 .
  • This processor 601 employs software (such as Netfabb® Studio software) to create a machine-specific build file.
  • the machine-specific build file is exported to a second processor 603 .
  • this second processor controls the operation, including movements, of: (1) an inkjet head or other device that selectively deposits liquid, (2) a vibrating trough (and/or compressed air) that spreads out the powder on the substrate and then removes the excess powder.
  • this invention may be implemented with other arrangements of processors. For example, more than one remote processor and more than one onboard processor may be employed, and any of the above tasks may be handled by one or more of these different processors.
  • FIG. 5 shows a compressive device 803 , after a number of substrate layers (e.g., 801 ) have been placed in it, one on top of the other in order and in registered alignment. Shown are registration pins projecting out of the registration holes of each tile, respectively, to cause such registered alignment.
  • substrate layers e.g. 801
  • FIG. 6 shows substrate layers being compressed in the compressive device 903 .
  • Screws 905 , 907 , 909 , 911 , plates 913 , 915 and a spring 917 in the compressive device are used to exert pressure.
  • FIG. 7 is a high-level block diagram of some hardware that may be used in this invention.
  • One or more processors 1301 control an applicator 1303 , a heating element 1305 , an actuator 1307 , an artificial pressure source 1309 , and a stirrer in a container of liquid 1311 .
  • the applicator 1303 deposits powder in positive regions, but not in negative regions, of substrate layers.
  • the heating element 1305 transforms the powder into matter that flows and then hardens.
  • the resulting hardened material is disposed in a spatial pattern that infiltrates the substrate layers.
  • the artificial pressure source 1309 may comprise a press, clamp, spring, elastic element, or other device for compressing the substrate layers.
  • the stirrer may be used to stir a liquid that is used for removing excess substrate.

Abstract

A method, product, apparatus, and article of manufacture for the application of the Composite Based Additive Manufacturing (CBAM) method to produce objects in metal, and in metal fiber hybrids or composites. The approach has many advantages, including the ability to produce more complex geometries than conventional methods such as milling and casting, improved material properties, higher production rates and the elimination of complex fixturing, complex tool paths and tool changes and, for casting, the need for patterns and tools. The approach works by slicing a 3D model, selectively printing a fluid onto a sheet of substrate material for each layer based on the model, flooding onto the substrate a powdered metal to which the fluid adheres in printed areas, clamping and aligning a stack of coated sheets, heating the stacked sheets to melt the powdered metal and fuse the layers of substrate, and removing excess powder and unfused substrate.

Description

  • This is a divisional of application Ser. No. 16/195,362 filed Nov. 19, 2018, now U.S. Pat. No. 11,173,546 issuing Nov. 16, 2021, which is a continuation of application Ser. No. 15/631,634 filed Jun. 23, 2017, which is a continuation of PCT/US16/62356 filed Nov. 16, 2016, which claimed the benefit of U.S. Provisional Application No. 62/256,436, filed Nov. 17, 2015. This application incorporates the following applications by reference in their entireties (including their drawing figures): Application Nos. U.S. Ser. No. 16/195,362. U.S. Ser. No. 15/631,634. PCT/US16/62356. U.S. 61/528,537, PCT/US12/52946, U.S. Ser. No. 13/582,939; EP20120828967, U.S. 61/769,724, PCT/US14/18806; Ser. No. 14/835,685. U.S. Ser. No. 14/835,690. U.S. Ser. No. 14/835,697, U.S. Ser. No. 14/703,372, U.S. 62/243,590, U.S. 61/773,810, U.S. Ser. No. 14/199,603, U.S. 61/914,613 and U.S. Ser. No. 14/566,661.
  • TECHNICAL FIELD OF THE INVENTION
  • The present invention relates generally to three-dimensional fabrication.
  • BACKGROUND OF THE INVENTION
  • International Publication No. WO 2014/134224 A2 (corresponding to Application No. PCT/US14/18806) entitled “Methods and Apparatus for Three-Dimensional Composites” (as well as Application Nos. U.S. 61/528,537; PCT/US12/52946; U.S. Ser. No. 13/582,939; EP20120828967; U.S. 61/769,724: U.S. Ser. No. 14/835,685; U.S. Ser. No. 14/835,690; U.S. Ser. No. 14/835,697; U.S. Ser. No. 14/703,372; U.S. 62/243,590) describes a “layered” method and apparatus for producing three dimensional objects called “Composite Based Additive Manufacturing” or CBAM that produces a three-dimensional object using generally substrates, typically fibrous substrates and polymers. The present invention references International Publication No. WO 2014/134224 A2, and describes use of the technique described in the International Publication with metals.
  • SUMMARY OF THE INVENTION
  • The CBAM method described in International Publication No. WO 2014/134224 A2 extends the range of materials that can be used with 3D printing to create three-dimensional objects. Until recently, work on this technique has concentrated on using various substrates, including carbon fiber, polymer based material and natural fibers among others and various polymers as bonding agents. This application describes the application of the CBAM method and apparatus to produce objects in metal, and in metal fiber hybrids or composites. This application also describes an article of manufacture thereof.
  • This approach has a number of advantages including: the ability to produce more complex geometries than conventional methods such as milling and casting; improved material properties over conventional metals; higher production rates; the elimination of complex fixturing, complex tool paths and tool changes; and, in the case of casting, the need for patterns and tools.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 is a metal piece made by the method described in this application.
  • FIG. 2 is a flowchart illustrating the steps to produce a 3D metal object in accordance with the teachings of the present invention.
  • FIG. 3 shows an apparatus used to selectively deposit liquid (to which powder adheres), in an illustrative implementation of this invention.
  • FIG. 4 is a high-level block diagram of processors, in an illustrative implementation of this invention FIG. 5 shows a compressive device, after a number of substrate tiles (layers) have been placed in it, one on top of the other in a compressive device. The tiles are aligned by inserting registration pins of the compressive device into the registration holes of each tile, respectively.
  • FIG. 6 shows a compressive device, after substrate layers with all of the “slices” of a ring torus have been inserted into it. Springs in the compressive device press the substrate layers together.
  • FIG. 7 is a block diagram that shows a processor that controls multiple components of an apparatus for fabricating a 3D object.
  • DETAILED DESCRIPTION OF INVENTION Output of the Technique
  • FIG. 1 is a metal piece 100 made by the method described in this application. The method of making this metal piece is described in detail below.
  • Description of the Technique
  • FIG. 2 is a flowchart illustrating the steps to produce a 3D metal object in accordance with the teachings of the present invention:
  • 1. Generate a CAD model (Step 102) which is sliced into layers (Step 104) by using a slicer program like Netfabb as described in (International Publication No. WO 2014/134224 A2. ¶0055; see also US Application Nos. U.S. 61/528,537 and U.S. 61/769,724). Each slice also includes registration holes, which will be used to orient each printed layer of substrate within the finished object exactly (International Publication No. WO 2014/134224 A2, ¶00121).
  • 2. The output of the slicer, which for example may be a bitmap file, is sent to an inkjet printer (Step 106). For each layer, the printer selectively prints a fluid onto a sheet of substrate material (Step 108) (International Publication No. WO 2014/134224 A2. ¶00113). The fluid may either be the bonding agent itself in liquid form; or it may be a liquid to which a powdered bonding agent adheres. Substrates can include fiberglass, high temperature glass fibers, boron fibers, or carbon fibers.
  • 3. If powdered bonding agent is being used, it is flooded onto the printed substrate (International Publication No. WO 2014/134224 A2. ¶0059). The powder adheres to the printed areas. Excess powder is removed, either by a stream of air, vacuum, vibration, or other mechanical means.
  • 4. The coated sheets of substrate are stacked in press or clamp (Step 110) (International Publication No. WO 2014/134224 A2, ¶00124), using the registration holes of each layer to align the printed portions of each sheet within the stack (International Publication No. WO 2014/134224 A2, ¶00106).
  • 5. The assembled sheets are then heated and possibly compressed in an oven, to melt the bonding material and fusing the layers of substrate to form the 3D object (Step 112) (International Publication No. WO 2014/134224 A2, ¶00149).
  • 6. The unfused substrate around the 3D object is then removed (Step 114), usually by abrasive blasting material or chemical means (International Publication No. WO 2014/134224 A2, ¶0081).
  • Issues in Using Metals with the Technique
  • It has been discovered that metals can be used with this technique. In one example the substrate used is a non-woven carbon fiber veil such as available from Hollingsworth and Vose. Veils that have been metal coated can also be used. The veil or substrate is printed as described above on an inkjet printer using, for example, a HP45 thermal inkjet head with a solution primarily of de-ionized water, pyrrolidone and alcohol. The solution may have an anti-evaporant including glycols and pyrrolidones. This fluid is printed on the area of the substrate that would be part of the object, i.e., the printed area corresponds to a layer shape for the object. This is done for each layer as described in the previous applications. Each layer is flooded with a metal powder for example a solder powder. The excess powder is removed by mechanical, vacuum, vibration or compressed air or a combination of such methods. This leaves the solder powder selectively deposited. One of the problems with using a metal powder in a process of this kind is that the powder oxidizes so that that when heated to its melting point the particles of the powder will not fuse together well. There are a number of solutions to this problem, one such solution is to mix the metal powder with a powder flux such as rosin which acts as a reducing agent. A typical flux to metal powder ratio is about 50/50. Another method is to melt the powders in a reducing, vacuum and/or inert atmosphere oven. In this way other metals or alloys can be used, such as aluminum, steel, stainless steel, copper, brass, and titanium among others. In addition liquid flux may be used as or in combination with the printing fluid, through selective deposition methods such as inkjet printing.
  • As an example the metal powder can be mixed with a powder flux before it is deposited on the substrate. Then all the layers of the object are printed and stacked in register as described in the earlier applications. They are compressed and heated as described in the earlier applications. The heating temperature is raised to the melting point of the powder. The layers fuse together and produce a build block. After the build block is removed from the compression jig the build block is abrasively blasted and the areas where no powder adhered, that is the portions of the object that were not coated with metal, are abrasive blasted off, the uncoated carbon fiber being very fragile. What is left is a three dimensional carbon fiber metal composite of the part that was represented by the CAD model.
  • FIG. 3 shows an apparatus used to selectively deposit liquid (to which powder adheres), in an illustrative implementation of this invention. Registration guide pins 501 are inserted through a substrate layer 503 in order to properly align the substrate layer 503. A solenoid valve, or inkjet head or heads 505 are used to selectively dispense liquid from a liquid reservoir 507 though a nozzle 509 unto the substrate layer 503. The nozzle 509 is rastered in a 2D plane 510 that is parallel to, and above, the substrate layer 503, so that the liquid is selectively deposited at desired x, y coordinates of the substrate layer 503, and not deposited in other areas of the substrate layer 503. To achieve this rastering, a stepper motor 511 actuates two belts (not shown) that causes a support member (not shown) to move along two rails (not shown) in a direction parallel to the x axis. A second stepper motor (not shown) and third belt (not shown) are mounted on the support member, and are used to move a nozzle support (not shown) in a direction parallel to the y axis. The nozzle 509 is attached to the nozzle support. Together, the two stepper motors can move the nozzle 509 to any desired x, y coordinate above the substrate layer. A page wide head may also be used. A microprocessor 513 controls the stepper motors and the solenoid valve or inkjet head, thereby controlling when and where liquid is dispensed on the substrate layer 503. Alternately, rather than rastering in a line-by-line pattern, the stepper motors may cause the nozzle or nozzles 509 to move in other 2D patterns in the 2D plane to cause the liquid to be deposited at certain x, y coordinates. FIG. 2 does not show an apparatus for heating and pressing multiple layers of substrate, or for removing excess substrate. In some implementations, the substrate layer is moved to a different position before those steps occur.
  • FIG. 4 is a high-level block diagram of processors, in an illustrative implementation of this invention. A CAD model of a desired 3D object in STL file format is created using a remote processor 601. This processor 601 employs software (such as Netfabb® Studio software) to create a machine-specific build file. The machine-specific build file is exported to a second processor 603. Depending on the particular implementation, this second processor controls the operation, including movements, of: (1) an inkjet head or other device that selectively deposits liquid, (2) a vibrating trough (and/or compressed air) that spreads out the powder on the substrate and then removes the excess powder. Alternately, this invention may be implemented with other arrangements of processors. For example, more than one remote processor and more than one onboard processor may be employed, and any of the above tasks may be handled by one or more of these different processors.
  • As described in WO2014134224 ¶183 (the entirety of the publication which is incorporated by reference), the printed carbon fiber substrate 801 is placed onto a fixture using registration holes to align. FIG. 5 shows a compressive device 803, after a number of substrate layers (e.g., 801) have been placed in it, one on top of the other in order and in registered alignment. Shown are registration pins projecting out of the registration holes of each tile, respectively, to cause such registered alignment.
  • FIG. 6 shows substrate layers being compressed in the compressive device 903. Screws 905, 907, 909, 911, plates 913, 915 and a spring 917 in the compressive device are used to exert pressure.
  • FIG. 7 is a high-level block diagram of some hardware that may be used in this invention. One or more processors 1301 control an applicator 1303, a heating element 1305, an actuator 1307, an artificial pressure source 1309, and a stirrer in a container of liquid 1311. The applicator 1303 deposits powder in positive regions, but not in negative regions, of substrate layers. The heating element 1305 transforms the powder into matter that flows and then hardens. The resulting hardened material is disposed in a spatial pattern that infiltrates the substrate layers. The artificial pressure source 1309 may comprise a press, clamp, spring, elastic element, or other device for compressing the substrate layers. The stirrer may be used to stir a liquid that is used for removing excess substrate.

Claims (5)

What is claimed is:
1. A three-dimensional article of manufacture comprising a plurality of substrate layers that are infiltrated or coated by, and bound together by, a hardened material, such that the hardened material has a material composition that is different from the material composition of any of the plurality of substrate layers, wherein the hardened material comprises metal, wherein all of the plurality of substrate layers have a substantially identical material composition and each substrate layer is a sheet-like structure that has a material composition comprising fibers held together by a binder.
2. The article of claim 1, wherein the hardened material further comprises flux.
3. The article of manufacture of claim 1, wherein the substrate layer material composition includes fibers selected from the group consisting of carbon fibers, ceramic fibers, polymer fibers, glass fibers, and metal fibers.
4. The article of manufacture of claim 1, wherein the metal comprises one or more of aluminum, steel, stainless steel, copper, brass and titanium.
5. a three-dimensional article of manufacture made by the process comprising:
reading a file of layers of the 3-D object, layer by layer, each layer having a shape;
for each layer, printing a fluid selectively onto a sheet of substrate material, the printing on each said sheet of substrate material representing the shape of that layer;
flooding through a trough onto each sheet of substrate material a powdered metal that adheres to the selectively printed fluid on each sheet of the substrate material as a printed shape to create at least one powdered sheet;
removing excess powder from each powdered sheet as each powdered substrate sheet is first printed and subsequently flooded with said powdered metal; and
stacking the powdered sheets in registered alignment, after excess powder removal, to form a stack of said powdered sheets, wherein each sheet in the stack of powdered sheets corresponds to a layer in the file of layers.
US18/331,566 2015-11-17 2023-06-08 Apparatus and process for producing additive manufactured metal matrix composites and article of manufacture thereof Pending US20230313352A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US18/331,566 US20230313352A1 (en) 2015-11-17 2023-06-08 Apparatus and process for producing additive manufactured metal matrix composites and article of manufacture thereof

Applications Claiming Priority (6)

Application Number Priority Date Filing Date Title
US201562256436P 2015-11-17 2015-11-17
PCT/US2016/062356 WO2017087572A1 (en) 2015-11-17 2016-11-16 Apparatus and process for producing additive manufactured metal matrix composites and article of manufacture thereof
US15/631,634 US20170291223A1 (en) 2015-11-17 2017-06-23 Apparatus and Process for Producing Additive Manufactured Metal Matrix Composites and Article of Manufacture Thereof
US16/195,362 US11173546B2 (en) 2015-11-17 2018-11-19 Apparatus and process for producing additive manufactured metal matrix composites and articles of manufacture thereof
US17/455,118 US11674207B2 (en) 2015-11-17 2021-11-16 Apparatus and process for producing additive manufactured metal matrix composites and article of manufacture thereof
US18/331,566 US20230313352A1 (en) 2015-11-17 2023-06-08 Apparatus and process for producing additive manufactured metal matrix composites and article of manufacture thereof

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
US17/455,118 Continuation US11674207B2 (en) 2015-11-17 2021-11-16 Apparatus and process for producing additive manufactured metal matrix composites and article of manufacture thereof

Publications (1)

Publication Number Publication Date
US20230313352A1 true US20230313352A1 (en) 2023-10-05

Family

ID=58717782

Family Applications (4)

Application Number Title Priority Date Filing Date
US15/631,634 Abandoned US20170291223A1 (en) 2015-11-17 2017-06-23 Apparatus and Process for Producing Additive Manufactured Metal Matrix Composites and Article of Manufacture Thereof
US16/195,362 Active 2037-01-29 US11173546B2 (en) 2015-11-17 2018-11-19 Apparatus and process for producing additive manufactured metal matrix composites and articles of manufacture thereof
US17/455,118 Active US11674207B2 (en) 2015-11-17 2021-11-16 Apparatus and process for producing additive manufactured metal matrix composites and article of manufacture thereof
US18/331,566 Pending US20230313352A1 (en) 2015-11-17 2023-06-08 Apparatus and process for producing additive manufactured metal matrix composites and article of manufacture thereof

Family Applications Before (3)

Application Number Title Priority Date Filing Date
US15/631,634 Abandoned US20170291223A1 (en) 2015-11-17 2017-06-23 Apparatus and Process for Producing Additive Manufactured Metal Matrix Composites and Article of Manufacture Thereof
US16/195,362 Active 2037-01-29 US11173546B2 (en) 2015-11-17 2018-11-19 Apparatus and process for producing additive manufactured metal matrix composites and articles of manufacture thereof
US17/455,118 Active US11674207B2 (en) 2015-11-17 2021-11-16 Apparatus and process for producing additive manufactured metal matrix composites and article of manufacture thereof

Country Status (6)

Country Link
US (4) US20170291223A1 (en)
EP (1) EP3377249B1 (en)
JP (3) JP2018537587A (en)
KR (1) KR102597223B1 (en)
CN (1) CN108472727A (en)
WO (1) WO2017087572A1 (en)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9833949B2 (en) 2011-08-29 2017-12-05 Impossible Objects, Inc. Apparatus for fabricating three-dimensional printed composites
US10343243B2 (en) 2013-02-26 2019-07-09 Robert Swartz Methods and apparatus for construction of machine tools
JP6895445B2 (en) 2016-02-12 2021-06-30 インポッシブル オブジェクツ,エルエルシー Methods and equipment for automated composite system additive manufacturing
EP3720710A1 (en) * 2017-12-08 2020-10-14 Oerlikon Am GmbH Assisted fused deposition modeling
DE102017223259A1 (en) 2017-12-19 2019-06-19 MTU Aero Engines AG METHOD AND DEVICE FOR CLEANING PARTIALLY MANUFACTURED COMPONENTS DURING GENERATIVE PRODUCTION
CN108165961A (en) * 2018-01-17 2018-06-15 华南理工大学 A kind of 3D printer and its operation method based on liquid solid chemical reaction deposition
US11130291B2 (en) 2019-03-29 2021-09-28 Xerox Corporation Composite-based additive manufacturing (CBAM) use of gravity for excess polymer removal
US10920351B2 (en) 2019-03-29 2021-02-16 Xerox Corporation Sewing method and apparatus to increase 3D object strength
US11117325B2 (en) 2019-03-29 2021-09-14 Xerox Corporation Composite-based additive manufacturing (CBAM) augmented reality assisted sand blasting
US11485110B2 (en) 2019-03-29 2022-11-01 Xerox Corporation Cross layer fiber entanglement to increase strength of 3D part
US11046002B2 (en) 2019-03-29 2021-06-29 Xerox Corporation Wetting agent additive for an in-line quality check of composite-based additive manufacturing (CBAM) substrates
US11104077B2 (en) 2019-03-29 2021-08-31 Xerox Corporation Composite-based additive manufacturing (CBAM) image quality (IQ) verification and rejection handling
US11731352B2 (en) 2019-03-29 2023-08-22 Xerox Corporation Apparatus and method for fabricating multi-polymer composite structures
US11312049B2 (en) 2019-04-03 2022-04-26 Xerox Corporation Additive manufacturing system for halftone colored 3D objects
US11214000B2 (en) 2019-04-03 2022-01-04 Xerox Corporation Apparatus and method for fabricating multi-sided printed composite sheet structures
US11679601B2 (en) 2019-05-16 2023-06-20 Impossible Objects, Inc. Holdown process and system for platen
US11318671B2 (en) 2019-05-21 2022-05-03 Xerox Corporation System and method for sheeting and stacking 3D composite printed sheets
US11518092B2 (en) 2019-06-19 2022-12-06 Xerox Corporation Patterned pre-stop for finishing additive manufactured 3D objects
EP4029628A4 (en) * 2019-09-13 2023-09-20 Strong by Form SpA System and method for designing and manufacturing objects having an optimised free-form with novel composite materials and the resulting object
EP4094189A4 (en) 2020-01-23 2024-02-21 Impossible Objects Inc Camera-based monitoring system for 3-dimensional printing
US11413821B2 (en) 2020-01-23 2022-08-16 Impossible Objects, Inc. Powder refill system for 3-dimensional printing
US11806931B2 (en) 2020-01-23 2023-11-07 Impossible Objects, Inc. Bulk ink bags for 3-dimensional printing
US11904532B2 (en) 2020-01-23 2024-02-20 Impossible Objects, Inc. Carbon fiber sheet separation with flickers for 3-dimensional printing
CN113059799B (en) * 2021-02-19 2023-05-05 浙江工贸职业技术学院 3D object printing method
US11938537B2 (en) 2022-08-01 2024-03-26 Xerox Corporation System and method for high throughput additive manufacturing of sintered parts with low anisotropy

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5637175A (en) * 1988-10-05 1997-06-10 Helisys Corporation Apparatus for forming an integral object from laminations
US5204055A (en) * 1989-12-08 1993-04-20 Massachusetts Institute Of Technology Three-dimensional printing techniques
JPH08192468A (en) * 1995-01-19 1996-07-30 Hitachi Ltd Method and apparatus for producing three-dimensional model
US6814823B1 (en) * 1999-09-16 2004-11-09 Solidica, Inc. Object consolidation through sequential material deposition
US6780368B2 (en) * 2001-04-10 2004-08-24 Nanotek Instruments, Inc. Layer manufacturing of a multi-material or multi-color 3-D object using electrostatic imaging and lamination
GB0112675D0 (en) * 2001-05-24 2001-07-18 Vantico Ltd Three-dimensional structured printing
AUPR597401A0 (en) * 2001-06-27 2001-07-19 Summerfield, Martin Raymond Ceramic powder transfer process
JP4224438B2 (en) * 2004-07-16 2009-02-12 日信工業株式会社 Method for producing carbon fiber composite metal material
EP1911568B1 (en) * 2005-07-27 2013-06-05 Shofu Inc. Apparatus for forming layered object
US20080032099A1 (en) * 2006-07-20 2008-02-07 Elmer's Products, Inc. Heat activated art mounting sheet
CN100570268C (en) * 2006-09-27 2009-12-16 北京航空航天大学 Fibre-reinforced metal/ceramic laminated composite material prevention plate
CN101417339B (en) * 2008-12-05 2010-09-08 西北有色金属研究院 Preparation method of ultra light porous metal fiber sandwich board
CN101927346A (en) * 2010-09-09 2010-12-29 上海交通大学医学院附属第九人民医院 Three-dimensional printing technology based method for forming medical porous pure titanium implant
US9776376B2 (en) * 2011-08-29 2017-10-03 Impossible Objects, LLC Methods and apparatus for three-dimensional printed composites based on flattened substrate sheets
WO2014134224A2 (en) * 2013-02-26 2014-09-04 Impossible Objects Llc Methods and apparatus for three-dimensional printed composites
WO2013033273A2 (en) * 2011-08-29 2013-03-07 Impossible Objects Llc Methods and apparatus for 3d fabrication
US10190220B2 (en) 2013-01-31 2019-01-29 Siemens Energy, Inc. Functional based repair of superalloy components
DE102013010160A1 (en) * 2013-06-19 2015-01-08 Hueck Rheinische Gmbh Process for producing a material plate by means of a press plate or endless belt, and press plate or endless belt and material plate
CN105408095A (en) * 2013-06-24 2016-03-16 哈佛学院院长等 Printed three-dimensional (3D) functional part and method of making
CN103397284B (en) * 2013-07-29 2014-06-04 太原理工大学 Preparation method of carbon fiber strengthened aluminum-base-layer-shaped composite board
JP2015196267A (en) * 2014-03-31 2015-11-09 株式会社東芝 Method and apparatus for production of laminated molding and slurry
CN106804106A (en) * 2014-05-04 2017-06-06 亦欧普莱克斯公司 Many material three-dimensional printers
CN104399986B (en) * 2014-05-31 2016-09-07 福州大学 A kind of 3D Method of printing for preparing base metal and alloy components thereof
CN104150915B (en) * 2014-08-06 2015-08-26 西安交通大学 A kind of powder 3D Method of printing based on water-based inorganic binding agent

Also Published As

Publication number Publication date
EP3377249A4 (en) 2019-12-11
US11173546B2 (en) 2021-11-16
KR20180097550A (en) 2018-08-31
EP3377249B1 (en) 2022-11-02
JP2018537587A (en) 2018-12-20
US20220072611A1 (en) 2022-03-10
US11674207B2 (en) 2023-06-13
JP2023113828A (en) 2023-08-16
US20190084046A1 (en) 2019-03-21
US20170291223A1 (en) 2017-10-12
JP2021179014A (en) 2021-11-18
EP3377249A1 (en) 2018-09-26
KR102597223B1 (en) 2023-11-03
CN108472727A (en) 2018-08-31
WO2017087572A1 (en) 2017-05-26

Similar Documents

Publication Publication Date Title
US20230313352A1 (en) Apparatus and process for producing additive manufactured metal matrix composites and article of manufacture thereof
US11370166B2 (en) Methods and apparatus for three-dimensional printed composites based on folded substrate sheets
US10377106B2 (en) Methods and apparatus for three-dimensional printed composites based on flattened substrate sheets
US8575513B2 (en) Rapid prototyping of ceramic articles
US5207371A (en) Method and apparatus for fabrication of three-dimensional metal articles by weld deposition
US5301415A (en) Method for fabrication of three-dimensional articles
EP2961585B1 (en) Methods and apparatus for three-dimensional printed composites
EP0490546B1 (en) Method and apparatus for fabrication of three-dimensional articles by thermal spray deposition
US20180250739A1 (en) Additive manufacturing method and apparatus
US10717231B2 (en) Three-dimensional forming apparatus and three-dimensional forming method
JP2018537587A5 (en)
EP3717208B1 (en) Additive manufacturing apparatus and related process
US20060251805A1 (en) Combination hybrid kinetic spray and consolidation processes
EP0554033A1 (en) Method for fabrication of three-dimensional articles
US20060290772A1 (en) Method of manufacturing rapid prototyping workpiece by using laser transfer printing technology
US20230339174A1 (en) Three-dimensional printed composites using substrates with sodium silicate binder
JP2015124441A (en) Metal powder sintering body manufacturing device and metal powder sintering body manufacturing method
Sirinterlikci et al. 3D Printing Processes and Associated Materials
CN112658630A (en) Additive manufacturing method of metal part
CN116117171A (en) Metal 3D printing device for transferring stations and printing method using same
Harris et al. United States Patent m

Legal Events

Date Code Title Description
AS Assignment

Owner name: IMPOSSIBLE OBJECTS, INC., ILLINOIS

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:SWARTZ, ROBERT;BAYLDON, JOHN;CRIST, BUCKLEY;AND OTHERS;REEL/FRAME:063897/0338

Effective date: 20151204

STPP Information on status: patent application and granting procedure in general

Free format text: NON FINAL ACTION MAILED

STPP Information on status: patent application and granting procedure in general

Free format text: RESPONSE TO NON-FINAL OFFICE ACTION ENTERED AND FORWARDED TO EXAMINER

STPP Information on status: patent application and granting procedure in general

Free format text: NON FINAL ACTION MAILED