ADDITIVE MANUFACTURING SUPPORT MATERIAL WITH PARTICULATES

FIELD OF THE INVENTION

Embodiments herein relate to methods and systems for forming three-dimensional printed parts, in particular three-dimensional printed parts utilizing a support material containing a particulate material, such as silica.

BACKGROUND

Additive manufacturing systems are used to build 3D parts from digital representations of the parts using one or more additive manufacturing techniques. Examples of commercially available additive manufacturing techniques include extrusion-based techniques, ink jetting, selective laser sintering, powder/binder jetting, electron beam melting, and stereolithographic processes. For each of these techniques, the 3D digital representation of the part is initially digitally sliced into multiple horizontal layers. For each sliced layer, a tool path is then generated, which provides instructions for the particular additive manufacturing system to form the given layer.

One particularly desirable additive manufacturing method is selective toner electrophotographic process (STEP) additive manufacturing, which allows for rapid, high quality production of 3D parts. STEP manufacturing is performed by applying layers of thermoplastic material that are carried from an electrophotography (EP) engine by a transfer medium (e.g., a rotatable belt or drum). The layer is then transferred to a build platform to print the 3D part (or support structure) in a layer-by-layer manner, where the successive layers are transfused together to produce the 3D part (or support structure). The layers are placed down in an X-Y plane, with successive layers positioned on top of one another in a Z-axis perpendicular to the X-Y plane.

A support structure is sometimes built utilizing the same deposition techniques by which the part material is deposited. The supporting layers or structures are often built underneath overhanging portions or in cavities of parts under construction that are not supported by the part material itself. The part material adheres to the support material during fabrication and the support material is subsequently removable from the completed 3D part when the printing process is complete. In typical STEP processes layers of the part material and support material are deposited next to each other in a common X-Y plane. These layers of part and support material are each built on top of one another (layers of part material built on top of other layers of part material; and layers of support material built on to top of other layers of support material) along the Z-axis to create a composite part that contains both part material and support material.

Although STEP additive manufacturing can produce very high-quality parts, it is still desirable to form even better parts, including by using improved support material that often deposited alongside the part material. For example, it is desirable to have support material with improved performance (such as viscosity) and cost properties.

SUMMARY

Additive manufacturing, including STEP, often includes use of support material that is deposited adjacent to part material. The support material can be used to form recesses in the build material, to support overhanging build material, etc.

Although various support materials can be used, it is desirable to have support material that is readily removable from the part material, and which also has a viscosity and flow properties (rheology) that allow for precise deposition. Thus, there is a desire to design the support rheology for achieving various goals. These goals include matching the viscosity of various part materials that have different rheology, increasing the low temperature viscosity to better support the build as it grows in height and is under the load of the transfuse roller, and enable operation at higher temperatures for crystalline materials to slow or minimize warpage.

To change the rheology by modification of the polymer would require manufacturing a different polymer for each desired viscosity. The addition of a rheologically enhancing filler to adjust the viscosity greatly simplifies this process, enabling a single polymer or a smaller set of polymers to be used across many applications. A further advantage is to be able to adjust for variation in the polymer polymerization that would otherwise unfavorably shift the rheology, or for freely incorporate recycled material while maintaining a consistent rheology.

The incorporation of silica into the support material lowers cost and complexity, and is applicable to a wide range of support polymers, both water soluble and base soluble. Thus, incorporation of silica avoids challenging polymerization of various combinations of monomers and optimization of the reaction conditions to achieve a single rheology profile.

The present disclosure includes, in an example embodiment, compounding extrusion of a non-surface treated silica (such as Aerosil 150 or Aerosil 130) at 8 weight % to 20 weight % into a terpolymer of poly(styrene, n-butylacrylate, methacrylic acid) along with charge agent (0.5 weight % to 1.5 weight % Bontron E-84 or Acrybase 2550) and carbon black (1% to 0.5% Regal 330). The added silica should not be so much that under low shear dissolution the silica does not disperse into the liquid phase (thus sonication of the liquid is the preferred implementation). Above 20 weight % silica the support can become difficult to remove from blind holes in the part, even with sonication, so such levels are less desirable. The particulate ideally remains dispersed in the solution without causing a sediment that must be periodically removed. Ideally if the material is precipitated and recovered the particulate is recovered with the precipitate.

Other useful silicas useful include R972 (hexamethlydisilizane surface treated silica with a BET surface area of 130 m²/g) but may require about twice the amount of silica for the same viscosity rise as the untreated silica (but an advantage is a faster dissolution time). Other fumed silicas are also usable. Non-silicas such as alumina, iron oxide, SiC etc. can be used but are often less available in submicron form, and denser, so prone to settling out once dissolved. Finely divided clays (bentonite) are an example of a non-silica that can be used provided they are small enough to disperse in the dissolution process. Other non-silicas include calcium carbonate, talc, mica, kaolin, calcium sulfate, carbon black, alumina trihydrate and wollastonite.

In a first aspect the present disclosure is directed to a support composition for additive manufacturing, the support composition comprising a soluble support polymer and a finely divided particulate, wherein the particulate is about 5% by weight to 25% by weight of the support composition. In certain embodiments the particulate is at or below 1 μm weight average particle size.

In example implementations the particulate is an amorphous silica.

In certain embodiments the silica has a BET surface area greater than 50 m²per gram.

In certain embodiments the de-agglomerated particulate is at or below 0.1 μm weight average particle size.

In some embodiments the soluble support polymer is insoluble at pH below 6.

Optionally the soluble support polymer comprises monomers of acrylic acid.

The present disclosure also includes using the STEP process wherein the support comprises a soluble support polymer and a finely divided particulate wherein the particulate is at 5% by weight to 25% by weight.

In an embodiment, a support composition for additive manufacturing, the support composition can include a soluble support polymer and a finely divided particulate, wherein the particulate is at 5% by weight to 25% by weight of the support composition.

In an embodiment, the particulate is at least 5% by weight of the support composition.

In an embodiment, the particulate is at least 10% by weight of the support composition.

In an embodiment, the particulate is at least 15% by weight of the support composition.

In an embodiment, the particulate is at least 20% by weight of the support composition.

In an embodiment, the particulate is at less than 35% by weight of the support composition.

In an embodiment, the particulate is at less than 30% by weight of the support composition.

In an embodiment, the particulate is at less than 25% by weight of the support composition.

In an embodiment, the particulate is at less than 20% by weight of the support composition.

In an embodiment, the particulate is at less than 15% by weight of the support composition.

In an embodiment, the particulate is at less than 10% by weight of the support composition.

In an embodiment, the particulate is at or below 1.0 μm weight average particle size.

In an embodiment, the particulate is at or below 1.5 μm weight average particle size.

In an embodiment, the particulate is at or below 2.0 μm weight average particle size.

In an embodiment, the particulate is at or below 0.9 μm weight average particle size.

In an embodiment, the particulate is at or below 0.8 μm weight average particle size.

In an embodiment, the particulate is at or below 0.7 μm weight average particle size.

In an embodiment, the particulate is at or below 0.6 μm weight average particle size.

In an embodiment, the particulate is at or below 0.5 μm weight average particle size.

In an embodiment, the particulate is at or greater than 0.2 μm weight average particle size.

In an embodiment, the particulate is at or greater than 0.3 μm weight average particle size.

In an embodiment, the particulate is at or greater than 0.4 μm weight average particle size.

In an embodiment, the particulate is at or greater than 0.5 μm weight average particle size.

In an embodiment, the particulate is at or greater than 1.0 μm weight average particle size.

In an embodiment, where the particulate is an amorphous silica.

In an embodiment, where the silica has a BET surface area greater than 50 m²per gram.

In an embodiment, where the silica has a BET surface area greater than 25 m²per gram.

In an embodiment, where the silica has a BET surface area greater than 10 m²per gram.

In an embodiment, where the silica has a BET surface area greater than 100 m²per gram.

In an embodiment, where the silica has a BET surface area less than 100 m²per gram.

In an embodiment, the de-agglomerated particulate is at or below 0.1 μm weight average particle size.

In an embodiment, the de-agglomerated particulate is at or below 0.25 μm weight average particle size.

In an embodiment, the de-agglomerated particulate is at or below 0.5 μm weight average particle size.

In an embodiment, the soluble support polymer is insoluble at pH below 8.

In an embodiment, the soluble support polymer is insoluble at pH below 7.

In an embodiment, the soluble support polymer is insoluble at pH below 6.

In an embodiment, where the soluble support polymer includes monomers of acrylic acid.

In an embodiment, where the dissolution process uses sonication.

Definitions

Unless otherwise specified, the following terms as used herein have the meanings provided below:

The term “copolymer” refers to a polymer having two or more monomer species.

The terms “preferred” and “preferably” refer to embodiments of the invention that may afford certain benefits, under certain circumstances. However, other embodiments may also be preferred, under the same or other circumstances. Furthermore, the recitation of one or more preferred embodiments does not imply that other embodiments are not useful, and is not intended to exclude other embodiments from the inventive scope of the present disclosure.

Reference to “a” chemical compound refers one or more molecules of the chemical compound, rather than being limited to a single molecule of the chemical compound. Furthermore, the one or more molecules may or may not be identical, so long as they fall under the category of the chemical compound.

The terms “at least one” and “one or more of” an element are used interchangeably, and have the same meaning that includes a single element and a plurality of the elements, and may also be represented by the suffix “(s)” at the end of the element.

Directional orientations such as “above”, “below”, “top”, “bottom”, and the like are made with reference to a direction along a printing axis of a 3D part. In the embodiments in which the printing axis is a vertical z-axis, the layer-printing direction is the upward direction along the vertical z-axis. In these embodiments, the terms “above”, “below”, “top”, “bottom”, and the like are based on the vertical z-axis. However, in embodiments in which the layers of 3D parts are printed along a different axis, the terms “above”, “below”, “top”, “bottom”, and the like are relative to the given axis.

The terms “about” and “substantially” are used herein with respect to measurable values and ranges due to expected variations known to those skilled in the art (e.g., limitations and variabilities in measurements).

The term “providing”, such as for “providing a material” and the like, when recited in the claims, is not intended to require any particular delivery or receipt of the provided item. Rather, the term “providing” is merely used to recite items that will be referred to in subsequent elements of the claim(s), for purposes of clarity and ease of readability.

The term “selective deposition” refers to an additive manufacturing technique where one or more layers of particles are fused to previously deposited layers utilizing heat and pressure over time where the particles fuse together to form a layer of the part and also fuse to the previously printed layer.

The term “electrostatography” refers to the formation and utilization of latent electrostatic charge patterns to form an image of a layer of a part, a support structure or both on a surface. Electrostatography includes, but is not limited to, electrophotography where optical energy is used to form the latent image, ionography where ions are used to form the latent image and/or electron beam imaging where electrons are used to form the latent image.

The terms “resilient material” and “flowable material” describe distinct materials used in the printing of a 3D part and support. The resilient material has a higher viscosity and/or storage modulus relative to the flowable material.

Unless otherwise specified, pressures referred to herein are based on atmospheric pressure (i.e. one atmosphere).

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a schematic front view of an exemplary electrophotography-based additive manufacturing system for printing 3D parts and support structures from part and support materials, in accordance with embodiments of the present disclosure.

FIG. 2 is a schematic front view of a pair of electrophotography engines of the system for developing layers of the part and support materials, in accordance with embodiments of the present disclosure.

FIG. 3 is a schematic front view of an alternative electrophotography engine, which includes an intermediary drum or belt, in accordance with embodiments of the present disclosure.

FIG. 4 is a schematic front view of a layer transfusion assembly of the system for performing layer transfusion steps with the developed layers, in accordance with embodiments of the present disclosure.

DETAILED DESCRIPTION

Embodiments of the present disclosure relate to a selective deposition-based additive manufacturing system, such as an electrostatography-based additive manufacturing system, to print 3D parts and/or support structures with high resolution and smooth surfaces. During a printing operation, electrostatographic engines develop or otherwise image each layer of the part and support materials using the electrostatographic process. The developed layers are then transferred to a layer transfusion assembly where they are transfused (e.g., using heat and/or pressure over time) to print one or more 3D parts and support structures in a layer-by-layer manner.

The present disclosure includes, in an example embodiment, compounding extrusion of an non-surface treated silica (such as Aerosil 150 or Aerosil 130) at 8 weight % to 20 weight % into a terpolymer of poly(styrene, n-butylacrylate, methacrylic acid) along with charge agent (0.5 weight % to 1.5 weight % Bontron E-84 or Acrybase 2550) and carbon black (1% to 0.5% Regal 330). The added silica should not be so much that under low shear dissolution the silica does not disperse into the liquid phase (thus sonication of the liquid is the preferred implementation). Above 20 weight % silica the support can become difficult to remove from blind holes in the part, even with sonication, so such levels are less desirable. The particulate ideally remains dispersed in the solution without causing a sediment that must be periodically removed. Ideally if the material is precipitated and recovered the particulate is recovered with the precipitate.

Other useful silicas useful include R972 (hexamethlydisilizane surface treated silica with a BET surface area of 130 m²/g) but may require about twice the amount of silica for the same viscosity rise as the untreated silica (but an advantage is a faster dissolution time). Other fumed silicas are also usable. Non-silicas such as alumina, iron oxide, SiC etc. can be used but are often less available in submicron form, and denser, so prone to settling out once dissolved. Finely divided clays (bentonite) are an example of a non-silica that be used provided they are small enough to disperse in the dissolution process. Other non-silicas include calcium carbonate, talc, mica, kaolin, calcium sulfate, carbon black, alumina trihydrate and wollastonite

In example implementations the particulate is an amorphous silica.

In certain embodiments the silica has a BET surface area greater than 50 m²per gram. In certain embodiments the de-agglomerated particulate is at or below 0.1 μm weight average particle size.

In some embodiments the soluble support polymer is insoluble at pH below 6.

Optionally the soluble support polymer comprises monomers of acrylic acid.

FIGS. 1 to 4 show example components of STEP manufacturing systems. FIG. 1 is a simplified diagram of an exemplary electrophotography-based additive manufacturing system 10 configured to perform a selective deposition process to printing 3D parts and associated support structures, in accordance with embodiments of the present disclosure. As shown in FIG. 1, system 10 includes one or more EP engines, generally referred to as 12, such as EP engines 12p and 12s, a transfer assembly 14, biasing mechanisms 16, and a transfusion assembly 20. Examples of suitable components and functional operations for system 10 include those disclosed in Hanson et al., U.S. Pat. Nos. 8,879,957 and 8,488,994, and in Comb et al., U.S. Patent Publication Nos. 2013/0186549 and 2013/0186558.

The EP engines 12p and 12s are imaging engines for respectively imaging or otherwise developing layers, generally referred to as 22, of the powder-based part and support materials, where the part and support materials are each preferably engineered for use with the particular architecture of the EP engine 12p or 12s. As discussed below, the developed layers 22 are transferred to a transfer medium (such as belt 24) of the transfer assembly 14, which delivers the layers 22 to the transfusion assembly 20. The transfusion assembly 20 operates to build the 3D part 26, which may include support structures and other features, in a layer-by-layer manner by transfusing the layers 22 together on a build platform 28.

In some embodiments, the transfer medium includes a belt 24, as shown in FIG. 1. Examples of suitable transfer belts for the transfer medium or belt 24 include those disclosed in Comb et al., U.S. Patent Application Publication Nos. 2013/0186549 and 2013/0186558. In some embodiments, the belt 24 includes front surface 24a and rear surface 24b, where front surface 24a faces the EP engines 12, and the rear surface 24b is in contact with the biasing mechanisms 16.

In some embodiments, the transfer assembly 14 includes one or more drive mechanisms that include, for example, a motor 30 and a drive roller 33, or other suitable drive mechanism, and operate to drive the transfer medium or belt 24 in a feed direction 32. In some embodiments, the transfer assembly 14 includes idler rollers 34 that provide support for the belt 24. The example transfer assembly 14 illustrated in FIG. 1 is highly simplified and may take on other configurations. Additionally, the transfer assembly 14 may include additional components that are not shown in order to simplify the illustration, such as, for example, components for maintaining a desired tension in the belt 24, a belt cleaner for removing debris from the surface 24a that receives the layers 22, and other components.

The EP engine 12s develops layer or image portions 22s of powder-based support material, and the EP engine 12p develops layer or image portions 22p of powder-based part/build material. In some embodiments, the EP engine 12s is positioned upstream from the EP engine 12p relative to the feed direction 32, as shown in FIG. 1. In alternative embodiments, the arrangement of the EP engines 12p and 12s may be reversed such that the EP engine 12p is upstream from the EP engine 12s relative to the feed direction 32. In further alternative embodiments, system 10 may include three or more EP engines 12 for printing layers of additional materials, as indicated in FIG. 1.

Example system 10 also includes controller 36, which represents one or more processors that are configured to execute instructions, which may be stored locally in memory of the system 10 or in memory that is remote to the system 10, to control components of the system 10 to perform one or more functions described herein. In some embodiments, the controller 36 includes one or more control circuits, microprocessor-based engine control systems, and/or digitally-controlled raster imaging processor systems, and is configured to operate the components of system 10 in a synchronized manner based on printing instructions received from a host computer 38 or a remote location.

In some embodiments, the host computer 38 includes one or more computer-based systems that are configured to communicate with controller 36 to provide the print instructions (and other operating information). For example, the host computer 38 may transfer information to the controller 36 that relates to the sliced layers of the 3D parts and support structures, thereby allowing the system 10 to print the 3D parts 26 and support structures in a layer-by-layer manner. The controller 36 may also use signals from one or more sensors to assist in properly registering the printing of the part or image portion 22p and/or the support structure or image portion 22s with a previously printed corresponding support structure portion 22s or part portion 22p on the belt 24 to form the individual layers 22.

The components of system 10 may be retained by one or more frame structures (not shown for simplicity). Additionally, the components of system 10 may be retained within an enclosable housing (not shown for simplicity) that prevents components of the system 10 from being exposed to ambient light during operation.

FIG. 2 is a schematic front view of the EP engines 12p and 12s of the system 10, in accordance with example embodiments of the present disclosure. In the illustrated embodiment, the EP engines 12p and 12s may include the same components, such as a photoconductor drum 42 having a conductive drum body 44 and a photoconductive surface 46. The conductive drum body 44 is an electrically-conductive drum (e.g., fabricated from copper, aluminum, tin, or the like) that is electrically grounded and configured to rotate around a shaft 48. The shaft 48 is correspondingly connected to a drive motor 50, which is configured to rotate the shaft 48 (and the photoconductor drum 42) in the arrow showing direction 52 at a constant rate.

The photoconductive surface 46 can be a thin film extending around the circumferential surface of the conductive drum body 44, and is preferably derived from one or more photoconductive materials, such as amorphous silicon, selenium, zinc oxide, organic materials, and the like. As discussed below, the surface 46 is configured to receive latent-charged images of the sliced layers of a 3D part or support structure (or negative images), and to attract charged particles of the part or support material to the charged or discharged image areas, thereby creating the layers of the 3D part or support structure.

As further shown, each of the example EP engines 12p and 12s also includes a charge inducer 54, an imager 56, a development station 58, a cleaning station 60, and a discharge device 62, each of which may be in signal communication with the controller 36. The charge inducer 54, the imager 56, the development station 58, the cleaning station 60, and the discharge device 62 accordingly define an image-forming assembly for the surface 46 while the drive motor 50 and the shaft 48 rotate the photoconductor drum 42 in the direction 52.

Each of the EP engines 12 uses the powder-based material (e.g., polymeric or thermoplastic toner), generally referred to herein by reference character 66, to develop or form the layers 22. In some embodiments, the image-forming assembly for the surface 46 of the EP engine 12s is used to form support layers 22s (e.g., image portions) of powder-based support material 66s, where a supply of the support material 66s may be retained by the development station 58 (of the EP engine 12s) along with carrier particles. Similarly, the image-forming assembly for the surface 46 of the EP engine 12p is used to form part layers 22p (e.g., image portion) of powder-based part material 66p, where a supply of the part material 66p may be retained by the development station 58 (of the EP engine 12p) along with carrier particles. Additional EP engines 12 may be included that utilize other support or part materials 66.

The charge inducer 54 is configured to generate a uniform electrostatic charge on the surface 46 as the surface 46 rotates in the direction 52 past the charge inducer 54. Suitable devices for the charge inducer 54 include corotrons, scorotrons, charging rollers, and other electrostatic charging devices.

Each imager 56 is a digitally controlled, pixel-wise light exposure apparatus configured to selectively emit electromagnetic radiation toward the uniform electrostatic charge on the surface 46 as the surface 46 rotates in the direction 52 the past imager 56. The selective exposure of the electromagnetic radiation to the surface 46 is directed by the controller 36, and causes discrete pixel-wise locations of the electrostatic charge to be removed (i.e., discharged to ground), thereby forming latent image charge patterns on the surface 46.

Suitable devices for the imager 56 include scanning laser (e.g., gas or solid-state lasers) light sources, light emitting diode (LED) array exposure devices, and other exposure device conventionally used in 2D electrophotography systems. In alternative embodiments, suitable devices for the charge inducer 54 and the imager 56 include ion-deposition systems configured to selectively directly deposit charged ions or electrons to the surface 46 to form the latent image charge pattern.

Each development station 58 is an electrostatic and magnetic development station or cartridge that retains the supply of the part material 66p or the support material 66s, along with carrier particles. The development stations 58 may function in a similar manner to single or dual component development systems and toner cartridges used in 2D electrophotography systems. For example, each development station 58 may include an enclosure for retaining the part material 66p or the support material 66s and carrier particles. When agitated, the carrier particles generate triboelectric charges to attract the powders of the part material 66p or the support material 66s, which charges the attracted powders to a desired sign and magnitude, as discussed below.

Each development station 58 may also include one or more devices for transferring the charged part or the support material 66p or 66s to the surface 46, such as conveyors, fur brushes, paddle wheels, rollers, and/or magnetic brushes. For instance, as the surface 46 (containing the latent charged image) rotates from the imager 56 to the development station 58 in the direction 52, the charged part material 66p or the support material 66s is attracted to the appropriately charged regions of the latent image on the surface 46, utilizing either charged area development or discharged area development (depending on the electrophotography mode being utilized). This creates successive layers 22p or 22s as the photoconductor drum continues to rotate in the direction 52, where the successive layers 22p or 22s correspond to the successive sliced layers of the digital representation of the 3D part or support structure.

The successive layers 22p or 22s are then rotated with the surface 46 in the direction 52 to a transfer region in which layers 22p or 22s are successively transferred from the photoconductor drum 42 to the belt 24 or other transfer medium, as discussed below. While illustrated as a direct engagement between the photoconductor drum 42 and the belt 24, in some preferred embodiments, the EP engines 12p and 12s may also include intermediary transfer drums and/or belts, as discussed further below.

After a given layer 22p or 22s is transferred from the photoconductor drum 42 to the belt 24 (or an intermediary transfer drum or belt), the drive motor 50 and the shaft 48 continue to rotate the photoconductor drum 42 in the direction 52 such that the region of the surface 46 that previously held the layer 22p or 22s passes the cleaning station 60. The cleaning station 60 is a station configured to remove any residual, non-transferred portions of part or support material 66p or 66s. Suitable devices for the cleaning station 60 include blade cleaners, brush cleaners, electrostatic cleaners, vacuum-based cleaners, and combinations thereof.

After passing the cleaning station 60, the surface 46 continues to rotate in the direction 52 such that the cleaned regions of the surface 46 pass the discharge device 62 to remove any residual electrostatic charge on the surface 46, prior to starting the next cycle. Suitable devices for the discharge device 62 include optical systems, high-voltage alternating-current corotrons and/or scorotrons, one or more rotating dielectric rollers having conductive cores with applied high-voltage alternating-current, and combinations thereof.

The biasing mechanisms 16 are configured to induce electrical potentials through the belt 24 to electrostatically attract the layers 22p and 22s from the EP engines 12p and 12s to the belt 24. Because the layers 22p and 22s are each only a single layer increment in thickness at this point in the process, electrostatic attraction is suitable for transferring the layers 22p and 22s from the EP engines 12p and 12s to the belt 24.

The controller 36 preferably rotates the photoconductor drums of the EP engines 12p and 12s at the same rotational rates that are synchronized with the line speed of the belt 24 and/or with any intermediary transfer drums or belts. This allows the system 10 to develop and transfer the layers 22p and 22s in coordination with each other from separate developer images. In particular, as shown, each part layer 22p may be transferred to the belt 24 with proper registration with each support layer 22s to produce a combined part and support material layer or combined image layer, which is generally designated as layer 22. As can be appreciated, some of the layers 22 transferred to the layer transfusion assembly 20 may only include support material 66s or may only include part material 66p, depending on the particular support structure and 3D part geometries and layer slicing.

In an alternative embodiment, the part layers 22p and the support layers 22s may optionally be developed and transferred along the belt 24 separately, such as with alternating layers 22p and 22s. These successive, alternating layers 22p and 22s may then be transferred to layer transfusion assembly 20, where they may be transfused separately to form the layer 22 and print or build the 3D part 26 and support structure.

In a further alternative embodiment, one or both of the EP engines 12p and 12s may also include one or more intermediary transfer drums and/or belts between the photoconductor drum 42 and the belt or transfer medium or belt 24. For example, as shown in FIG. 3, the EP engine 12p may also include an intermediary drum 42a that rotates in the direction 52a that opposes the direction 52, in which photoconductor drum 42 is rotated, under the rotational power of motor 50a. The intermediary drum 42a engages with the photoconductor drum 42 to receive the developed layers 22p from the photoconductor drum 42, and then carries the received developed layers 22p and transfers them to the belt 24.

The EP engine 12s may include the same arrangement of an intermediary drum 42a for carrying the developed layers 22s from the photoconductor drum 42 to the belt 24. The use of such intermediary transfer drums or belts for the EP engines 12p and 12s can be beneficial for thermally isolating the photoconductor drum 42 from the belt 24, if desired.

FIG. 4 illustrates an embodiment of the layer transfusion assembly 20. As shown, the exemplary transfusion assembly 20 includes the build platform 28, a nip roller 70, and pre-transfusion heaters 72 and 74. In some embodiments, the transfusion assembly includes, an optional post-transfusion heater 76, and/or a cooler (e.g., air jets 78 or other cooling units), as shown in FIGS. 1 and 4. The build platform 28 is a platform assembly or platen of system 10 that is configured to receive the heated combined layers 22 (or separate layers 22p and 22s) for printing the part 26, which includes a 3D part 26p formed of the part layers 22p, and support structure 26s formed of the support layers 22s, in a layer-by-layer manner. In some embodiments, the build platform 28 may include removable film substrates (not shown) for receiving the printed layers 22, where the removable film substrates may be restrained against build platform using any suitable technique (e.g., vacuum drawing).

The build platform 28 is supported by a gantry 84 or other suitable mechanism, which can be configured to move the build platform 28 along the z-axis and the x-axis (and, optionally, also the y-axis), as illustrated schematically in FIG. 1 (the y-axis being into and out of the page in FIG. 1, with the z-, x- and y-axes being mutually orthogonal, following the right-hand rule). The layers are put down generally parallel to an x-y plane, and the layers stack on top of one another along the z-axis. The gantry 84 may produce cyclical movement patterns relative to the nip roller 70 and other components, as illustrated by broken line 86 in FIG. 4. The particular movement pattern of the gantry 84 can follow essentially any desired path suitable for a given application. The gantry 84 may be operated by a motor 88 based on commands from the controller 36, where the motor 88 may be an electrical motor, a hydraulic system, a pneumatic system, or the like. In one embodiment, the gantry 84 can included an integrated mechanism that precisely controls movement of the build platform 28 in the z- and x-axis directions (and optionally the y-axis direction). In alternate embodiments, the gantry 84 can include multiple, operatively-coupled mechanisms that each control movement of the build platform 28 in one or more directions, for instance, with a first mechanism that produces movement along both the z-axis and the x-axis and a second mechanism that produces movement along only the y-axis. The use of multiple mechanisms can allow the gantry 84 to have different movement resolution along different axes. Moreover, the use of multiple mechanisms can allow an additional mechanism to be added to an existing mechanism operable along fewer than three axes.

In the illustrated embodiment, the build platform 28 can be heatable with heating element 90 (e.g., an electric heater). The heating element 90 is configured to heat and maintain the build platform 28 at an elevated temperature that is greater than room temperature (25° C.), such as at a desired average part temperature of 3D part 26p and/or support structure 26s, as discussed in Comb et al., U.S. Patent Application Publication Nos. 2013/0186549 and 2013/0186558. This allows the build platform 28 to assist in maintaining 3D part 26p and/or support structure 26s at this average part temperature.

The nip roller 70 is an example heatable element or heatable layer transfusion element, which is configured to rotate around a fixed axis with the movement of the belt 24. In particular, the nip roller 70 may roll against the rear surface 22s in the direction of arrow 92 while the belt 24 rotates in the feed direction 32. In the shown embodiment, the nip roller 70 is heatable with a heating element 94 (e.g., an electric heater). The heating element 94 is configured to heat and maintain nip roller 70 at an elevated temperature that is greater than room temperature (25° C.), such as at a desired transfer temperature for the layers 22.

The pre-transfusion heater 72 includes one or more heating devices (e.g., an infrared heater and/or a heated air jet) that are configured to heat the layers 22 on the belt 24 to a selected temperature of the layer 22, such as up to a fusion temperature of the part material 66p and the support material 66s, prior to reaching nip roller 70. Each layer 22 desirably passes by (or through) the heater 72 for a sufficient residence time to heat the layer 22 to the intended transfer temperature. The pre-transfusion heater 74 may function in the same manner as the heater 72, and heats the top surfaces of the 3D part 26p and support structure 26s on the build platform 28 to an elevated temperature, and in one embodiment to supply heat to the layer upon contact.

The part and support materials 66p and 66s of the layers 22p and 22s may be heated together with the heater 72 to substantially the same temperature, and the part and support materials 66p and 66s at the top surfaces of the 3D part 26p and support structure 26s may be heated together with heater 74 to substantially the same temperature. This allows the part layers 22p and the support layers 22s to be transfused together to the top surfaces of the 3D part 26p and the support structure 26s in a single transfusion step as the combined layer 22. As discussed below, a gap can be placed between the support layers 22s and part layers 22p, and under heat and pressure part and support material are pressed together in a manner such as to produce an improved interface with reduced surface roughness.

An optional post-transfusion heater 76 may be provided downstream from nip roller 70 and upstream from air jets 78, and configured to heat the transfused layers 22 to an elevated temperature in a single post-fuse step.

As mentioned above, in some embodiments, prior to building the part 26 on the build platform 28, the build platform 28 and the nip roller 70 may be heated to their selected temperatures. For example, the build platform 28 may be heated to the average part temperature (e.g., bulk temperature) of 3D part 26p and support structure 26s. In comparison, the nip roller 70 may be heated to a desired transfer temperature or nip entrance temperature for the layers 22.

As further shown in FIG. 4, during operation, the gantry 84 may move the build platform 28 (with 3D part 26p and support structure 26s) in a reciprocating pattern 86. In particular, the gantry 84 may move the build platform 28 along the x-axis below, along, or through the heater 74. The heater 74 heats the top surfaces of 3D part 26p and support structure 26s to an elevated temperature, such as the transfer temperatures of the part and support materials. As discussed in Comb et al., U.S. Patent Application Publication Nos. 2013/0186549 and 2013/0186558, the heaters 72 and 74 may heat the layers 22 and the top surfaces of 3D part 26p and support structure 26s to about the same temperatures to provide a consistent transfusion interface temperature. Alternatively, the heaters 72 and 74 may heat layers 22 and the top surfaces of 3D part 26p and support structure 26s to different temperatures to attain a desired transfusion interface temperature.

The continued rotation of the belt 24 and the movement of the build platform 28 align or register the heated layer 22 (e.g., combined image layer) with the heated top surfaces of 3D part 26p and support structure 26s with proper registration along the x-axis. The gantry 84 may continue to move the build platform 28 along the x-axis, at a rate that is synchronized with the rotational rate of the belt 24 in the feed direction 32 (i.e., the same directions and speed). This causes the rear surface 24b of the belt 24 to rotate around the nip roller 70 to nip the belt 24 and the heated layer 22 against the top surfaces of 3D part 26p and support structure 26s. This presses the heated layer 22 between the heated top surfaces of 3D part 26p and support structure 26s at the location of the nip roller 70, which at least partially transfuses the heated layer 22 to the top layers of 3D part 26p and support structure 26s.

As the transfused layer 22 passes the nip of the nip roller 70, the belt 24 wraps around the nip roller 70 to separate and disengage from the build platform 28. This assists in releasing the transfused layer 22 from the belt 24, allowing the transfused layer 22 to remain adhered to 3D part 26p and support structure 26s. Maintaining the transfusion interface temperature at a transfer temperature that is higher than its glass transition temperature, but lower than its fusion temperature, allows the heated layer 22 to be hot enough to adhere to the 3D part 26p and support structure 26s, while also being cool enough to readily release from the belt 24. Additionally, the close melt rheologies of the part and support materials allow them to be transfused in the same step. The temperature and pressures can be selected, as is discussed below, to promote flow of part material and support material into a gap between the two materials. Often the rheologies are preferably close, they can be transfused with glass transition temperatures that are significantly different from one another in some constructions. This flow into the gap, typically accompanied by an upward movement of the part and support material, results in a smoother interface between the part and support, plus a smoother surface for the part after removal of the support.

After release, the gantry 84 continues to move the build platform 28 along the x-axis to the post-transfusion heater 76. At optional post-transfusion heater 76, the top-most layers of 3D part 26p and the support structure 26s (including the transfused layer 22) may then be heated to at least the fusion temperature of the thermoplastic-based powder in a post-fuse or heat-setting step. This optionally heats the material of the transfused layer 22 to a highly fusable state such that polymer molecules of the transfused layer 22 quickly interdiffuse (also referred to as reptate) to achieve a high level of interfacial entanglement with 3D part 26p and support structure 26s.

Additionally, as the gantry 84 continues to move the build platform 28 along the x-axis past the post-transfusion heater 76 to the air jets 78, the air jets 78 blow cooling air towards the top layers of 3D part 26p and support structure 26s. This actively cools the transfused layer 22 down to the average part temperature, as discussed in Comb et al., U.S. Patent Application Publication Nos. 2013/0186549 and 2013/0186558.

To assist in keeping the 3D part 26p and support structure 26s at the average part temperature, in some embodiments, the heater 74 and/or the heater 76 may operate to heat only the top-most layers of 3D part 26p and support structure 26s. For example, in embodiments in which heaters 72, 74, and 76 are configured to emit infrared radiation, the 3D part 26p and support structure 26s may include heat absorbers and/or other colorants configured to restrict penetration of the infrared wavelengths to within the top-most layers. Alternatively, the heaters 72, 74, and 76 may be configured to blow heated air across the top surfaces of 3D part 26p and support structure 26s. In either case, limiting the thermal penetration into 3D part 26p and support structure 26s allows the top-most layers to be sufficiently transfused, while also reducing the amount of cooling required to keep 3D part 26p and support structure 26s at the average part temperature. However generally sufficient thermal penetration is desired to promote flow of part material and support material into gaps positioned at the interface between the part and support material.

The gantry 84 may then actuate the build platform 28 downward, and move the build platform 28 back along the x-axis to a starting position along the x-axis, following the reciprocating rectangular pattern 86. The build platform 28 desirably reaches the starting position for proper registration with the next layer 22. In some embodiments, the gantry 84 may also actuate the build platform 28 and 3D part 26p/support structure 26s upward for proper registration with the next layer 22. The same process may then be repeated for each remaining layer 22 of 3D part 26p and support structure 26s.

After the transfusion operation is completed, the resulting 3D part 26p and support structure 26s may be removed from system 10 and undergo one or more post-printing operations. For example, support structure 26s may be sacrificially removed from 3D part 26p using an aqueous-based solution, such as an aqueous alkali solution. Under this technique, support structure 26s may at least partially dissolve in the solution, separating it from 3D part 26p in a hands-free manner.

In comparison, part materials are chemically resistant to aqueous alkali solutions. This allows the use of an aqueous alkali solution to be employed for removing the sacrificial support structure 26s without degrading the shape or quality of 3D part 26p. Examples of suitable systems and techniques for removing support structure 26s in this manner include those disclosed in Swanson et al., U.S. Pat. No. 8,459,280; Hopkins et al., U.S. Pat. No. 8,246,888; and Dunn et al., U.S. Patent Application Publication No. 2011/0186081; each of which are incorporated by reference to the extent that they do not conflict with the present disclosure.

Furthermore, after support structure 26s is removed, 3D part 26p may undergo one or more additional post-printing processes, such as surface treatment processes. Examples of suitable surface treatment processes include those disclosed in Priedeman et al., U.S. Pat. No. 8,123,999; and in Zinniel, U.S. Pat. No. 8,765,045.

In an example, a support polymer comprised of a styrene, methacryclic acid, and butyl acrylate polymer was compounded on a two-roll mill with 18 weight % Areosil150 silica, 0.5% charge control agent and 0.5% carbon black. The rheology of the compound was measured using a parallel plate viscometer at a shear rate of 0.6 radians per second and at 180 C was found to be 3.4×10{circumflex over ( )}6 compared to the neat support resin roll milled without additives with a complex viscosity of 2.6×10{circumflex over ( )}4. In a second example, PA11 toner was used, the PA11 toner comprising a 20-25 micron powder of Rilsan G850 with 1% charge agent and 0.5% carbon black. A support toner was used, the support toner comprised of a 20-25 micron powder of a styrene, methacryclic acid, and butyl acrylate polymer formulated with 18 weight % Areosil150 silica, 0.5% charge control agent and 0.5% carbon black. The PA11 toner and support toner were used in a STEP process with an average bulk temperature of 165 degrees C. and an average transfuse temperature of 202 degrees C. The transfuse roller temperature was measured to be 141 degrees C. The transfuse temperature was measured with a pyrometer directed at the build as it exits the transfuse roller, the transfuse temperature was measured by a pyrometer directed the center of the transfuse toller, and the bulk temperature was measured with a pyrometer directed at the build surface, before the build enters the transfuse area. The 3D printed build was made to be 4.4 mm tall, suitable for making tensile bars. The PA11 parts were isolated by putting the build into a 60-70 degrees C. bath of water at a pH of 12.5-13.7 for 2-14 hours. The parts were rinsed with reverse osmosis water and dried with a fan. The tensile bars were conditioned for at least 12 hours at 73 degrees C. and 50% humidity prior to testing. The tensile properties were measured according to ASTM D638. The tensile strength was shown to be 54.5 MPa, the Tensile Modulus was 1657 MPa, and the Elongation at break was 22.6%.