Various aspects of the present disclosure relate generally to systems and methods for facilitating binder jetting additive manufacturing.
Binder jetting is an additive manufacturing technique by which a thin layer of powder (e.g. 65 μm) is spread onto a bed, followed by deposition of a liquid binder in a 2D pattern or image that represents a single “slice” of a 3D shape. After deposition of binder, another layer of powder is spread, and the process is repeated to form a 3D volume of bound material within the powder bed. After printing, the bound part may be, in reversible order, cured or crosslinked to strengthen the binder, and removed from the excess build material powder.
Management of conditions in the area where binder jetting is being performed can be important to safety and part quality. For example, it is important in many cases that powder representing a combustion risk is exposed to an inert environment during printing. It may also be important to manage build material powder migration through components of the printer and limit contamination of components that are functionally sensitive to powder or that may provide an ignition source for combustion (e.g. present a spark risk). It is therefore desirable to manage the gas environment in binder jetting printers.
Disclosed are systems and methods pertaining to a gas management system used during a binder jet additive manufacturing process from build material powder. A binder jet additive manufacturing process may employ a binder jet printer to fabricate objects from a build material powder and a binder. The binder jet printer may form an enclosure within which the objects are fabricated, and the gaseous atmosphere within the enclosure may be controlled to assist the additive manufacturing process. A gas management system may accomplish, or contribute to, at least a portion of the control. Further features of the binder jet printer (such as additional volumes, boundaries between two or more volumes, a partition at or near a boundary, or a gas management system, for example) may be utilized to tune and control the atmosphere in the binder jet printer as compared to atmosphere exterior to the binder jet printer, or as compared to embodiments lacking the features disclosed herein.
The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate various exemplary embodiments and together with the description, serve to explain the principles of the disclosed embodiments. There are many aspects and embodiments described herein. Those of ordinary skill in the art will readily recognize that the features of a particular aspect or embodiment may be used in conjunction with the features of any or all of the other aspects or embodiments described in this disclosure.
In the process of binder jetting additive manufacturing, a build material powder is delivered to and spread upon a build surface and a binding agent (or binder or ink) is deposited on the build material powder to at least partially bind the build material powder to form a slice of a 3D object. By repeating the steps of delivering a build material powder, spreading a build material powder, and depositing a binder corresponding to a desired image, a 3D structure may be formed. This process is understood to occur in a binder jetting printer (or binder jet printer).
In certain embodiments, a binder jet printer may comprise a print enclosure with a number of modules configured to aid in or accomplish the additive manufacturing of parts and other objects from a build material powder. These modules may include: (1) an assemblage of printheads (or one printhead in certain embodiments), (2) an ink delivery system to supply the printheads with binder at flow and pressure conditions necessary for stable binder ejection from the printhead, (3) a build material supply module to deliver an amount of build material powder to a print surface within the printer, (4) a build material spreading module to spread an amount of build material powder which has been supplied to a print surface to a controlled thickness, (5) a container and motion system to contain the build material powder and during printing move the container to specific positions (e.g., by moving in a first direction relative to a least one of the modules (1)-(4)) to enable the fabrication of successive layers of an object. In some embodiments, the printer may comprise additional modules including: (6) devices configured to reduce, prevent, or remove build material powder and/or ejecta from the printhead that may become suspended in an atmosphere in the print enclosure, including, according to certain embodiments, devices which deposit liquids (e.g., water, alcohol, oils, and the like) onto a surface of the build material powder to alter the cohesive characteristics of the powder, devices which control and/or provide a flow of gas to remove and/or filter suspended ejecta, (7) devices configured to control the gaseous atmosphere within the print enclosure relative to a gaseous atmosphere surrounding the binder jet printer, and (8) at least one reciprocating mechanism to provide relative motion between the container containing build material powder and at least one of the modules (1) to (4) in a second direction different from the first direction of the container and indexing system.
Build material powders may be sensitive to certain gaseous atmospheres. According to certain embodiments, it is desirable to prevent, minimize, or otherwise avoid gaseous communication between certain gaseous species and specific metal powders. For example, a copper build material powder may oxidize when in contact with air. In certain embodiments of the binder jetting printing process, such an oxidation of copper may be deleterious to the printing process for at least the reason that the oxidation may be uncontrolled and may introduce uncertainty into certain aspects of the binder jet printing process. In certain embodiments, a build material powder may be reactive (e.g, pyrophoric or explosible) with moisture and the build material powder should be kept separate from a base level of moisture contained in ambient air (e.g., room humidity). In certain embodiments, a build material powder may not be chemically sensitive (e.g., prone to oxidation, explosibility, pyrophoricity, or other means of chemical reaction) but may exhibit a change in physical properties such as the ability of the build material powder to flow. In the case where the flow characteristics of the powder will vary, degrade, or otherwise change, maintaining a consistent atmosphere around the build material powder may be required.
In another embodiment, build material powders may be reactive (e.g. pyrophoric or explosible) in the presence of oxygen and ignition sources capable of providing energy above the minimum ignition energy or temperatures above the minimum ignition temperature of the powder. Certain of the process modules (1) to (8) may provide sufficient energy or temperature to exceed these ignition limits, creating a condition in which a reaction may occur. In such cases, it may be desirable to maintain the printing environment in an inerted state, with the oxygen concentration of the atmosphere maintained below a predetermined concentration which is lower than the limiting oxygen concentration, or the concentration below which combustion of the build material powder does not readily occur. A typical target oxygen concentration may be 2%, which is below a typical limiting oxygen concentration of 4-15% for commonly printed materials.
In the process of binder jet additive manufacturing, a build material powder is typically supplied to a binder jet printer and some amount of this build material powder is bound using a binder to form objects. These objects are provided with various names in the field of art, and may be referred to as green parts, but are sometimes also referred to as brown parts. In certain embodiments, the objects formed may include parts that, as one skilled in the art will appreciate, may undergo subsequent post-processing steps (perhaps including a curing, drying, or crosslinking step) to improve the mechanical properties (such as strength, fracture toughness, elongation to failure, and the like) of the bound object.
In certain embodiments, post-processing (such as curing, drying, crosslinking, and the like) may be optionally performed to improve the mechanical properties of objects fabricated from build material powder and binder. In certain embodiments, the improvement of mechanical properties attained during the post-processing steps may reduce breakages of objects that can occur during the removal of unbound build material powder from the surfaces of the objects formed from binder and build material powder. This process of removing unbound build material powder (that is, powder which is not held or adhered to an object with binder) is often termed “depowdering”. As one skilled in the art may appreciate, several approaches may be pursued to depowder parts.
Several types of objects may be printed using a binder jet printer. In certain embodiments, a single object may comprise a single part. In certain embodiments, a single object may comprise a series of parts connected with a mechanical linkage permitting relative motion (such as a hinge, slide, or other element). In certain embodiments, a single object may comprise a series of parts connected with a mechanical linkage in which motion is prohibited, substantially prohibited, or the parts are otherwise fully constrained in all directions of translation and rotation. In certain embodiments, a single object may comprise a series of parts connected with at least one mechanical linkage permitting motion in at least one direction, and prohibiting motion in at least one other direction (such as, for example, in a sliding mechanism permitting motion in a first sliding direction with constraint imposed in a second constraining direction orthogonal to the first direction). In certain embodiments, a single object may comprise a part and a supporting structure, where the supporting structure may be configured to touch, abut, hold, cradle, or otherwise contact the part at or through at least one point across opposed surfaces of the part and support structure. In certain embodiments, the support structure may provide a means of support to the part. In certain embodiments, the means of support may be mechanical, such that the support structure, through the at least one point, carries a stress or force transmitted through or imposed upon the part. In certain embodiments, the part and the support may be printed in a first configuration and brought to contact in a second configuration, where the second configuration enables the support structure to provide support to the part.
Following binder jet printing and optional post-processing of the object, the object may be further subjected to thermal processing, according to certain embodiments. The thermal processing may include the steps of debinding and sintering of the object.
During debinding, binder is removed from the object. Debinding may be performed in any suitable chamber or enclosure. In certain embodiments, a suitable chamber or enclosure may include a means of heating the object, a means of providing a flow of process gas, a means of evacuating a process gas, and a means of controlling a pressure of the process gas, as will be appreciated by one skilled in the art.
Not being bound by theory, debinding may remove binder by a thermally activated process of evaporation, sublimation, combustion, oxidation, or degradation, according to certain embodiments. Depending upon the specific binder and build material powder materials in the object undergoing debinding, the debinding process may be tailored to achieve the desired amount of debinding.
In certain embodiments, the debinding process may begin at any temperature from the list of starting debinding temperatures: 200, 250, 300, 350, 400, or 450 degrees centigrade. In certain embodiments, the debinding process may end at any temperature from the list of ending debinding temperatures: 250, 300, 350, 400, 500, or 600 degrees centigrade. For example, a debind process may occur between 200 and 350 degrees centigrade, or may occur between 300 and 600 degrees centigrade. It should be understood by one skilled in the art that the starting debinding temperature will be less than the ending debinding temperature.
The debinding process may require the maintenance of a specific gaseous atmosphere surrounding the objects, according to certain embodiments. The gaseous atmosphere may include the gases argon, nitrogen, oxygen, hydrogen, helium, carbon dioxide, carbon monoxide, ammonia, methane, air, or the like. According to certain embodiments, the gaseous atmosphere may be a mixture of gases. According to certain embodiments, the gaseous atmosphere may be substantially absent and a vacuum may exist about the parts. According to certain embodiments, a gaseous atmosphere may be provided by a process gas.
The debinding process may require, or more optimally perform with a specific pressure or range of pressures of a process gas. According to certain embodiments, the pressure of the gaseous atmosphere during debinding may be equal to or may exceed 1 atmosphere. According to certain embodiments, the pressure of the gaseous atmosphere during debinding may be between 0.5 and 1 atmosphere. According to certain embodiments, the pressure of the gaseous atmosphere may be between 0.01 and 0.5 atmospheres. According to certain embodiments, the pressure of the gaseous atmosphere may be between 0.01 and 10 Torr. According to certain embodiments, the pressure of the gaseous atmosphere may be less than 0.01 Torr. In certain embodiments, a desired pressure may be maintained with a vacuum pump and a supply of process gas, where the volume of gas removed by the pump and the supply of process gas at least partially determine the pressure within the debind chamber.
Following the removal of at least a portion of the binder by the debinding process, the object may then be sintered, according to certain embodiments. In certain embodiments, the objects may be sintered without the removal of the binder, or without the binder removal step.
Not being bound by theory, during the process of sintering, the build material powder is heated to result in the joining of the build material powders to form a sintered object. The sintered object may exhibit a density larger than the density of the object prior to sintering, according to some embodiments. The object may be sintered without the melting of any build material powder, according to certain embodiments. The object may be sintered with the melting of only a portion of the build material powder, according to certain embodiments.
The process of sintering typically occurs in a sintering furnace, as will be appreciated by one skilled in the art. According to some embodiments, the sintering furnace may include a means of heating the object to be sintered. According to some embodiments, the sintering furnace may include a means of providing a flow of sintering process gas to the objects to be sintered, in such a way that the gaseous atmosphere around the objects to be sintered is at least partially controlled. According to some embodiments, the sintering furnace may include a means of controlling the pressure of a gaseous atmosphere around the objects during the sintering process (the “sintering pressure”). According to some embodiments, the means of controlling the pressure of a gaseous atmosphere around the objects during sintering may include a vacuum pump and at least one conduit to enable gaseous communication between a chamber housing the object to be sintered and the vacuum pump.
The gaseous atmosphere surrounding the object during sintering is often an important aspect of the sintering process. According to certain embodiments, the gaseous atmosphere may be comprised of hydrogen, helium, argon, nitrogen, carbon dioxide, carbon monoxide, methane, forming gas (a mixture of hydrogen and argon), ammonia, or air. According to certain embodiments, the gaseous atmosphere may be comprised of a mixture of gasses (95% nitrogen and 5% hydrogen by weight, for example). Careful selection of the gaseous atmosphere may promote certain mechanisms of sintering and lead to a desired amount of densification. As will be understood by one skilled in the art, the composition of the gaseous atmosphere surrounding the object during sintering may change during the sintering process, for example according to a predetermined schedule and in a coordinated fashion with the temperature, pressure, and flow rates as a function of time.
The pressure of the gaseous atmosphere surrounding the object during sintering is often an important aspect of the sintering process. According to certain embodiments, it is desirable to decrease the pressure in the sintering furnace to enhance the densification (that is, to increase the density) of an object undergoing sintering. According to certain embodiments, it is desirable to increase the pressure in the sintering furnace to enhance the densification (that is, to increase the density) of an object undergoing sintering. The selection of pressure is typically determined by the elements from which the build material powder is comprised in addition to the interaction of the elements with the gaseous atmosphere. In certain embodiments, the pressure of the gaseous atmosphere surrounding the object during sintering is at least 1 atmosphere and up to 5 atmospheres. In certain embodiments, the pressure of the gaseous atmosphere surrounding the object during sintering is at least 0.5 atmosphere and less than 1 atmosphere. In certain embodiments, the pressure of the gaseous atmosphere surrounding the object during sintering is at least 0.1 atmosphere and less than 0.5 atmosphere. In certain embodiments, the pressure of the gaseous atmosphere surrounding the object during sintering is at least 0.001 Torr atmosphere and less than 10 Torr. In certain embodiments, the pressure of the gaseous atmosphere surrounding the object during sintering is less than 0.001 Torr. As will be understood by one skilled in the art, the pressure of the gaseous atmosphere surrounding the object during sintering may change during the sintering process, for example according to a predetermined schedule and in a coordinated fashion with the temperature, composition, and flow rates as a function of time.
In some embodiments, the steps of debinding and sintering may occur during a sequentially in the same chamber, as part of a processing operation. For example, a single furnace may be used to first debind a part by controlling its temperature through starting and ending debind temperatures, and continuing to sintering temperatures without first cooling the part from the ending debind temperature.
In certain embodiments, the build material may be any finely divided material or powder. The finely divided material may be a metal, oxide ceramic, non-oxide ceramic, glass, cermet, organic material, carbide, nitride, or any mixture, according to certain embodiments.
In certain embodiments, the build material may comprise a metallic powder. In certain embodiments, the metallic powder may comprise a pure element (such as elemental copper or iron). In certain embodiments, the metallic powder may comprise an alloy of metallic elements to form a specific grade of metal, such as 17-4 stainless steel, 316 stainless steel, 316L stainless steel, 4140 low alloy steel, Inconel 718, Inconel 625, 6061 aluminum, 7075 aluminum, Ti-6A1-4V titanium, F75 Co—Cr—Mo, or any other alloy capable of being produced in a powdered or finely-divided form. In certain embodiments, the metallic powder may comprise a mixture of powdered metallic elements purposed to achieve the desired chemical specification of an alloyed metal (for example, a mixture including elemental Co, Cr, and Mo powders to form an F75 alloy, or a mixture including Fe, Cr, V, C, Mn, Si, and Ni to form a stainless steel). In certain embodiments, the build material may comprise a metallic powder where the metal is a refractory metal (such as tungsten, tantalum, niobium, rhenium, molybdenum, hafnium, zirconium, or the like).
In certain embodiments, the build material may comprise a ceramic powder. In certain embodiments, the ceramic powder may comprise alumina, zirconia, yttria-stabilized zirconia, mullite, silica, chromia, spinel, and the like. In certain embodiments, the build material may be a mixture of ceramic powders (for example, silica and alumina, or magnesium oxide and alumina).
In certain embodiments, the build material may be naturally derived, as an organic material. In certain embodiments, the organic material may comprise a wood flour, sawdust, cellulosic fiber, or the like.
In certain embodiments, a binder jet printer may include a container to contain the build material powder and printed structures. The container may be indexable moveable relative to the build material delivery and spreading mechanisms, and may also be indexable relative to an inkjet head or heads which deposit the binding agent in a desired pattern to form a slice of a 3D structure on the surface of a powder bed. As may be appreciated by one skilled in the art, the ability of the binder jet printer to accurately position and index the bed is crucial to the performance of the binder jet printer, and, specifically, is crucial to the layer-to-layer tolerance of the objects (or parts) produced by the binder jet printer.
With reference to
In certain embodiments, the binder jet printer may include a volume, the volume may be fully contained within the printer enclosure. For example, in certain embodiments the volume may include spaces within the printer where build material powder transits between a metering apparatus to supply the build material powder and a receiving area such as the upper surface of a powder bed or build box of build material powder. The volume may be a first volume or a second volume.
In certain embodiments, a volume may reside partly within the printer enclosure, or any other suitable boundary of the printer. For example, in certain embodiments, the volume may reside partly within the area surrounding the printer (such as laboratory, shop, or any other space suitable for housing a binder jet printer), and may partly reside within the printer enclosure (such that at least a portion of the volume is interior to the printer) and gaseous communication may exist between the portion of the volume exterior to the printer and the portion of the volume interior to the printer. The volume may be a first volume or a second volume.
In certain embodiments, the binder jet printer may entirely enclose a first volume and a second volume.
In certain embodiments, the first volume and second volume may mate at a boundary, or other suitable interface. In certain embodiments, a partition may provide some degree of separation between, or at least demarcate, the first volume and the second volume.
It may be desirable, in certain embodiments, to utilize a flow of gas directed from a first volume to a second volume, via the boundary. In certain embodiments, this flow may occur through or around a partition or other barrier. The flow of gas may provide a degree of sealing between the first and second volume—during the process of binder jet additive manufacturing from build material powder, build material powder may become suspended in the gaseous atmosphere within the printer and transit, via motions of the gaseous atmosphere and/or the momentum of the build material powder itself, to various surfaces, modules, or other objects, areas, and spaces within the printer. The transit and subsequent deposition of build material powder to specific areas and on specific objects within the binder jetting printer (for example sensitive electronics, sensors, circuit boards, inkjet print heads, or any other apparatus within the binder jetting printer) may be deleterious to the operation of at least the specific objects. As such, it may be desirable, in certain embodiments, to direct or otherwise control the transit and deposition of build material powder to avoid, or at least minimize or mitigate, such deleterious effects. The flow of a gas through the boundary (which may include a partition, in certain embodiments) may be tuned or otherwise selected to reduce (or bring to an acceptable amount) the migration of a build material powder across the boundary between a first and a second volume. In certain embodiments, the first volume may serve as a source of a gas and the second volume may serve as a sink of the gas, such that the gas flows from the first volume to the second volume and the gas provides at least some amount of sealing resulting in a decrease of build material powder migration from the second volume to the first volume. In certain embodiments, the gas may be a process gas. In certain embodiments, the process gas may include at least some amount of gas recycled from a source including the printer. In certain embodiments, a gas management system may control the flow of process gas.
In certain embodiments, a flow of process gas may result from a pressure control scheme where a first volume is held at a first pressure and a second volume is held at a second pressure, and where the second pressure is less than the first pressure. In certain embodiments, the pressures may be controlled by a gas management system.
In certain embodiments, it may be desirable to control the gaseous atmosphere for at least the purpose of maintaining a specific gas atmosphere within volumes interior to the print enclosure. For example, in certain embodiments, the maintenance of a specific gas atmosphere may accomplish the exclusion of a specific gas or gases from a volume interior to the print enclosure. In further embodiments, the maintenance of a specific gas atmosphere within a volume interior to the print enclosure may provide an advantage to, or enable, a process of binder jet additive manufacturing using a build material powder.
In some embodiments, the pressures maintained in a first volume or a second volume, or both a first and second volume, may be greater than a pressure of the surrounding ambient environment (i.e. greater than atmospheric pressure). A typical pressure of the second volume may be between 0.5 mbar and 25 mbar greater than the surrounding ambient environment.
As described previously, a build material powder may comprise a metal or a ceramic in powdered (or finely divided) form. In certain embodiments, a build material may be explosible, pyrophoric, or otherwise exhibit a sensitivity toward specific gases. In certain embodiments, a sensitivity may include oxidation of the build material powder. By way of non-limiting example, processing a build material powder comprised of aluminum may require that a volume interior to the print enclosure be largely, substantially, or nearly completely devoid of oxygen, or of air, or of water vapor, or of a plurality of air, oxygen, or water vapor, as those gases may damage the build material powder. Further, in addition to possibly damaging the build material powder, the presence of oxidizing species such as oxygen, air, or water may enable severe reactions between the gaseous species and the aluminum build material powder resulting in an explosion or other undesirable event (such as a fire, deflagration, or the like).
With reference now to
Certain powders may represent a combustion risk that can be categorized into four conditions. In a first condition no cloud of combustible dust is likely to occur. In a second condition, an explosive atmosphere in the form of a cloud of combustible dust is unlikely to occur and if so, exists for short periods. In a third condition, occasional explosive atmosphere in the form of a cloud of combustible dust may exist. In a fourth condition, continuous clouds of dust inside an enclosure create an explosive atmosphere for long periods or frequently for short periods. In some cases the second, third, and fourth conditions may relate to classification zones 22, 21, and 20 according to ATEX ratings for combustible dust, respectively. In certain embodiments, it may be desirable to mitigate a combustion risk arising from a choice of build material powder by controlling the gaseous atmosphere at various positions and places within a binder jetting printer, at different times. In certain embodiments, it may also be desirable to mitigate a combustion risk arising from a choice of build material powder by controlling the presence of ignition sources at various positions and places within a binder jetting printer, at different times. In some embodiments, sequences may be designed and implemented to deactivate potential energy sources for combustion during an inerting process (that is, while the oxygen concentration is being decreased) before and until the oxygen concentration is below a certain pre-determined threshold (e.g. below a limiting oxygen concentration for explosibility of the build material powder). After an acceptably low level of oxygen is achieved (that is, inerted), the energy sources may be activated.
With reference to
This application is a US National Stage Application, filed under 35 U.S.C. § 371, of International Application PCT/US2023/013096, filed on Feb. 15, 2023 and claims priority to U.S. Patent Application 63/312,293, filed on Feb. 21, 2022; the contents of the above applications are incorporated by reference herein in their entirety.
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/US2023/013096 | 2/15/2023 | WO |
| Number | Date | Country | |
|---|---|---|---|
| 63312293 | Feb 2022 | US |