The present disclosure relates to systems and methods for additive manufacturing using a pneumatic droplet-based additive manufacturing of parts, and more particularly to new systems and methods for “push-pull”, “push” and arbitrary variations of these pulse control techniques, to form liquid droplets of desired dimensions, which can be used to make parts through a droplet-based process which has the potential to significantly improve resolution and part quality over prior pneumatic droplet-based processes.
The statements in this section merely provide background information related to the present disclosure and may not constitute prior art.
Over the past two decades, metal additive manufacturing (AM) has demonstrated several advantages over conventional manufacturing methods: faster turn-around for new designs, less expense, higher part performance, and unmatched design freedom. Laser powder bed fusion (LPBF) has been the most dominant metal AM technique to date in terms of industrial and research activity, but nevertheless suffers from various drawbacks such as expensive and limited feedstock choices, the extra burden imposed from feedstock handling and safety, large heat-affected zones (i.e., several previous layers are remelted for each pass of the laser), high residual stress in the printed parts, incompatibility with traditional alloy systems, and inability to print closed cell structures without trapping powder.
Droplet-based AM techniques offer an alternative way of printing metal parts. In addition to being compatible with a wide range of input materials (not limited to metals), droplet-based AM may provide a solution to these above-mentioned weaknesses of LPBF. Generally, two droplet-based AM methods exist: droplet-on-demand material jetting (DoD-MJ), and continuous jet (CJ) printing. Both methods saw initial development in inkjetting for image printing, but have since been expanded to include printing of polymers, binders, wax, tissues and metals. The system described here can eject droplets with both DoD and a CJ methods, with the help of a unique valving system. In DoD, a sharp momentum pulse is applied to a volume of molten material, which then jets through a nozzle to create a controlled stream of individual droplets. Under optimized conditions, each momentum pulse results in a discrete molten material droplet that rapidly cools and solidifies upon impact with the substrate or existing parts. Re-melting of surrounding material at the impact location of the droplet ensures a fully solid part.
Droplets can range in diameter from 10 μm to over 1 mm (depending mostly on the nozzle diameter), and have been shown to be deposited at frequencies of up to 2 kHz (2000 droplets per second), enabling rapid fabrication of parts that are comprised of potentially hundreds of millions of fused droplets. Compared to LPBF, this powderless metal AM technique provides more freedom in feedstock choice without the burden of powder handling, produces parts more rapidly, can fabricate closed cell architectures, handles traditional alloy systems, does not create high residual stress, and can be fine-tuned to ensure only a portion of the previous layer is remelted.
There are generally three DoD actuation methods to energize the molten feedstock and generate droplets: rod-connected piezo, electromagnetic (e.g., magnetohydrodynamic (MHD)) and pneumatic. The rod-connected piezo and MHD methods have recently been developed into commercially available metal AM printers by GROB GMP300 and Xerox ElemX™, respectively. Both the piezo and electromagnetic methods each have their limitations that the current disclosure addresses. The MHD system can print highly electrically conductive fluids like molten metals and alloys, but cannot print fluids that have lower electrical conductivities like molten salts, high temperature resins, or slurries of refractory/ceramic particles. The new pneumatic method described in the present disclosure can be used to generate droplets regardless of the fluid electrical conductivity. The actuation mechanism of the piezo rod technique requires the rod to be in direct contact with the molten material, which may react with the feedstock. In contrast, the new pneumatic method described in the present disclosure allows only the inert argon headspace to interact with the molten material, eliminating any possibility of adverse reaction or actuator degradation. In addition, like the MHD system referenced above, the new pneumatic method described in the present disclosure has the additional ability to create a complex pressure waveform that allows highly improved control of droplet size, formation, and velocity.
Although the pulse time scale of the piezo rod method can be faster than the new pneumatic method described in the present disclosure, the inertia of the rod reduces the ability to create complex pulsed waveforms, resulting in less control over droplet generation than both the MHD and the new pneumatic method described herein. In addition, the new pneumatic method described herein can operate under constant pressure to jet a constant stream of molten material at a mass flow rate hundreds of times larger than that of both the MHD and piezo methods. Neither of the other two methods are able to switch between pure DoD and (CJ) techniques within the same printhead.
This section provides a general summary of the disclosure, and is not a comprehensive disclosure of its full scope or all of its features.
In one aspect the present disclosure relates to a droplet-based printing system that uses droplet on demand or continuous jetting. The system may comprise a controller and a printhead system. The printhead system has a housing with an internal cavity and a nozzle at a lower end thereof. The internal cavity is configured to hold a quantity of liquid therein. The printhead system also has a feedstock infeed port in communication with the internal cavity for enabling a feedstock to be fed into the internal cavity. The feedstock is contained within the internal cavity as a liquid feedstock. The printhead system also includes a valve system in communication with the controller and configured to selectively generate positive gauge pressure to the internal cavity in response to control signals received from the controller, to apply a vacuum negative gauge pressure to the internal cavity, and to further modify a pressure level within the internal cavity to create a pressure pulse with characteristics tailored to the rheological and thermal characteristics of the liquid feedstock, which causes ejection of a liquid droplet from the nozzle.
In another aspect the present disclosure relates to a system for droplet on demand printing. The system may comprise a controller; a printhead system having a housing with an internal cavity and a nozzle at a lower end thereof. The internal cavity configured to hold a quantity of molten metal therein. The housing includes a feedstock infeed port in communication with the internal cavity for enabling a metal feedstock to be fed into the internal cavity; an outflow/vacuum port in communication with the internal cavity for applying a controlled vacuum to the internal cavity; an ambient/offset port in communication with the internal cavity for venting the internal cavity to an ambient environment or to another environment with an offset pressure; and an inflow/pressure port for receiving a pressurized fluid signal for controllably pressurizing the internal cavity. The printhead system also contains a valve system including an outflow/vacuum valve in communication with the controller and with the outflow/vacuum port, and configured to enable a controlled vacuum to be applied to the internal cavity, an ambient/offset valve in communication with the controller and with the ambient/offset port, and configured to enable the internal cavity to be vented to the ambient environment when the ambient/offset valve is at least partially opened; and an inflow/pressure valve in communication with the controller and with the inflow/pressure port, and configured to enable a pressurized fluid to be channeled into the internal cavity. The outflow/vacuum valve, the ambient/offset valve and the inflow/pressure valve are controlled sequentially by the controller to generate a plurality of pulses each having a predetermined pulse configuration for generating a molten metal droplet having a desired dimension and velocity.
In still another aspect the present disclosure relates to a printhead for use in a droplet on demand (DoD) printing system. The printhead comprises a housing with an internal cavity and a nozzle at a lower end thereof. The internal cavity is configured to hold a quantity of molten feedstock material therein. The printhead also comprises a feedstock infeed port in communication with the internal cavity for enabling a feedstock material to be fed into the internal cavity and contained as a liquid feedstock material. The printhead also includes a first port in communication with the internal cavity for enabling a vacuum to be applied to the internal cavity; a second port in communication with the internal cavity for venting the internal cavity to an ambient environment; and a third port in communication with the internal cavity for enabling pressure to be applied to the internal cavity to pressurize the internal cavity. The printhead further includes a valve system in communication with the first, second and third ports, to enable a controlled sequence of application of a positive gauge pressure to the internal cavity; an application of a negative gauge pressure to the internal cavity; and venting of the internal cavity to atmosphere. The housing of the printhead also includes a nozzle in communication with the internal cavity for ejecting a molten metal droplet therefrom.
In still another aspect the present disclosure relates to a method for droplet on demand printing. The method may comprise using a printhead having a housing with an internal cavity to contain a quantity of liquid feedstock therein. The method may further comprise controlling a pressurization within the internal cavity by applying a vacuum to the internal cavity, venting the internal cavity, and applying a positive gauge pressure to the internal cavity, in a controlled sequential fashion, to create a pressure pulse. The pressure pulse time and amplitude signatures are tailored to the rheological and thermal characteristics of the liquid feedstock, and causes ejection of a liquid droplet from a nozzle of the housing.
Further areas of applicability will become apparent from the description provided herein. It should be understood that the description and specific examples are intended for purposes of illustration only and are not intended to limit the scope of the present disclosure.
The drawings described herein are for illustrative purposes only of selected embodiments and not all possible implementations, and are not intended to limit the scope of the present disclosure.
Corresponding reference numerals indicate corresponding parts throughout the several views of the drawings.
Example embodiments will now be described more fully with reference to the accompanying drawings.
The present disclosure relates to new systems and methods for pneumatic droplet-based additive manufacturing, which includes “Droplet-on-Demand Material Jetting” (“DoD-MJ” or alternatively “DoD”) and “Continuous Material Jetting” (“C-MJ” or alternatively “CJ”). With the systems and methods disclosed herein a reservoir is filled with a liquid such as molten pure metal or a metal alloy. The molten pure metal or metal alloy is maintained in liquid form via a heating device. A reservoir of inert gas such as argon or nitrogen is maintained in direct fluid contact with the liquid reservoir. The gas reservoir is then connected to an inert gas pressure source, such as a compressor or a pressurized gas bottle. Electronically controlled valves control the rate and timing of gas flow in and out of the gas reservoir. In DoD, by rapidly opening and closing the valves, a sequence of rapid inflow and exhaust of inert gas into and out of a gas reservoir creates a momentum pulse that displaces liquid volume in the reservoir and causes the denser liquid within the reservoir to pressurize and begin to flow out of the nozzle at the bottom of the reservoir. After the gas reservoir is pressurized, the pressure valve is then quickly shut off while a second valve (operating out of phase with the pressure valve) opens to evacuate the pressurized gas out of the chamber to atmosphere. This allows a portion of the partially ejected liquid mass to naturally retract back into the nozzle, allowing the remaining portion, which forms a disconnected droplet, to travel away from the nozzle on its own momentum. This is also known as “droplet breakup” or “droplet pinch-off” in literature. The usage of this rapid pressurization with the pressure valve and subsequent de-pressurization to ambient with a second valve may be viewed as “push-only” actuation. As found in all DoD methods, this gives freedom to deposit an isolated droplet with a single pulse or use a series of pulses to repeatedly eject droplets at rates up to a few kilohertz.
It should be noted that in literature, the DoD method is distinct from the CJ method through the nature of the pressure source: in DoD, the pressure source is pulsed; that is, the pressure peaks are separated with little to no pressure. In CJ, the pressure source is nearly constant, but with some slight local perturbations to facilitate droplet breakup from the jet. The present disclosure relates to MJ systems and methods where (1) either individual pressure pulses result in individual droplet ejections (i.e., DoD) or (2) a constant positive gauge pressure is applied to create a continuous jet of metal that is controllably broken up with periodic vacuum pulses (i.e., CJ). In some embodiments, the system 10 can adopt one or the other method without even changing hardware components, however the focus in the following paragraphs will be on describing the DoD version merely for simplicity.
In DoD AM, if the pressure pulse energy is weaker than the surface energy of the liquid meniscus within the nozzle, the extruded liquid mass naturally retracts back into the nozzle, oscillates, and no droplet is formed. If the pressure pulse is significantly stronger than the surface energy, the ejected mass will start to eject in a liquid column and then naturally break up into multiple droplets, or create droplets much larger than the nozzle ID, which is generally undesirable in DoD. A significant effort in DoD is avoiding both scenarios by choosing the correct combination of pressurization, nozzle design, and printhead design.
Control over droplet ejection, breakup and detachment from the nozzle, as well as the resulting meniscus behavior are critical to the performance of a DoD printhead, and thus any meaningful pressure waveform improvements can be expected to lead to a large range of practical performance improvements. It will be that the term “meniscus” as used herein is meant to be the point of demarcation where the fluid ends and the gas (or atmosphere) begins.
The present disclosure describes novel AM systems and methods which dramatically improve upon the aforementioned “push-only” pneumatic DoD printhead design. By creating an arbitrary waveform actuator that is able to create highly controlled “push-pull” or arbitrary, non-push-only pressure signatures, greater control over droplet breakup can be achieved, resulting in a more stable, consistent, and higher quality droplet jetting performance.
Referring
Referring further to
A small portion of the molten material which resides within the nozzle 32 is termed a “meniscus”, and is indicated by reference number 32a. The housing also includes a port 36 in communication with the internal chamber 28 for receiving a metal feedstock (e.g., and without limitation, a powdered metal, metal chunks, a metal wire, etc.) from a feedstock reservoir. In one example the feedstock reservoir is formed by a motorized feedstock wire feeder 46. However, in other embodiments the feedstock reservoir may simply be a reservoir 46′ which holds a quantity of metal material either in powdered form or chunk form, or in some other form, and which feeds the feedstock by gravity into the port 36. The present disclosure is not limited to metal feedstock in any particular shape, form or configuration.
With further reference to
The printhead system 15 also includes a heater subsystem 44 which in some embodiments may be a resistive heater, and in other embodiments may be an inductive heater. Still further types of heaters may be employed such as laser, chemical, combustion, and heat guns. The heater subsystem 44 in this example circumscribes the exterior of the housing 26 and receives electronic heater control signals from the controller 12. The heater subsystem 44 generates sufficient heat to fully melt the metal feedstock to turn it into the molten metal 30.
Referring further to
In the case of imaging molten metal ejections, the printhead housing 28 may be inserted into a transparent vessel or sheath 52 (e.g., an Ar gas sheath) that is properly flooded with Ar gas (verified with an oxygen sensor) to reduce the effects of metal droplet oxidation. In practice, the printhead system 14 may be entirely housed inside an inert glove box or chamber to ensure no oxidation at the nozzle or along the droplet trajectory. Alternately, the printhead system 14 may contain gas flow channels around and near the jetting nozzle to create a sheath of inert gas to reduce oxidation effects. If oxide is less of a concern for a particular material or liquid metal, the printhead system 14 can be operated in air.
In another embodiment the printhead system 14 may include only a single port in communication with a set of valves via tubing, as illustrated in
With brief reference to
A major benefit of this advancement is that the pressurized gas within the internal chamber 28 is evacuated much more rapidly, generating a faster pressure response and with significantly finer temporal control of droplet generation dynamics. This form of “push-pull” actuation can create even sharper pulses in time that, combined with higher pressure, creates droplets with significantly higher velocity than what the “push-only” printheads can create. This higher velocity is necessary to provide enough kinetic energy to flatten the droplets upon impact before solidifying to create flatter and denser layers of material. The finer temporal control of the pressure shown in
Another major benefit of the printhead system 16 described herein along with its method of control printhead is that the gas-filled space above the molten metal can reach vacuum levels (negative gauge pressure), which actively pulls the meniscus 32a back into the nozzle 32 during droplet breakup. This facilitates droplet breakup closer to the nozzle 32 location, which reduces the oscillation of the meniscus 32a before the next droplet is ejected. In DoD jetting, the oscillation of the meniscus 32a puts a serious practical limit on the maximum droplet jetting rate/frequency, since the meniscus must be nearly motionless before the next ejection. Attempting to eject droplets before the meniscus is fully quiesced creates an uncontrollable inconsistency in droplet velocity, size and directionality. The system 10 and methods described herein enable pneumatically actuated droplets to break up closer to the nozzle 32, reducing meniscus 32a oscillations and allowing for a higher max ejection frequency (and thus a higher deposition rate).
Referring further to
The system 10 in its various embodiments, as well as its methods of operation, are thus able to operate with individually controllable pressure and vacuum sources to achieve “push-pull” or other arbitrary pressure waveforms, or without vacuum source to create “push-only” waveforms.
Currently, the “push-pull” mode generates satellite-free water droplets at similar velocities to the “push-only” mode. Faster switching valves and/or optimized valve timing are needed to jet droplets at velocities that are considerably higher than with the “push-only” method. The current setup may be more amenable to printing fluids that break up more slowly (such as more viscous or denser fluids), enabling better control of droplet ejection velocity.
The invention described in this disclosure is not limited to printing molten metals and metal alloys, but can be used to jet any fluid with non-negligible surface tension. This includes, but is not limited to, ceramic/refractory or graphite suspensions or slurries, polymers or gels, organic solvents, or biological solutions (e.g., proteins, cells, etc.).
In addition, as
The foregoing description of the embodiments has been provided for purposes of illustration and description. It is not intended to be exhaustive or to limit the disclosure. Individual elements or features of a particular embodiment are generally not limited to that particular embodiment, but, where applicable, are interchangeable and can be used in a selected embodiment, even if not specifically shown or described. The same may also be varied in many ways. Such variations are not to be regarded as a departure from the disclosure, and all such modifications are intended to be included within the scope of the disclosure.
Example embodiments are provided so that this disclosure will be thorough, and will fully convey the scope to those who are skilled in the art. Numerous specific details are set forth such as examples of specific components, devices, and methods, to provide a thorough understanding of embodiments of the present disclosure. It will be apparent to those skilled in the art that specific details need not be employed, that example embodiments may be embodied in many different forms and that neither should be construed to limit the scope of the disclosure. In some example embodiments, well-known processes, well-known device structures, and well-known technologies are not described in detail.
The terminology used herein is for the purpose of describing particular example embodiments only and is not intended to be limiting. As used herein, the singular forms “a,” “an,” and “the” may be intended to include the plural forms as well, unless the context clearly indicates otherwise. The terms “comprises,” “comprising,” “including,” and “having,” are inclusive and therefore specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, elements, components, and/or groups thereof. The method steps, processes, and operations described herein are not to be construed as necessarily requiring their performance in the particular order discussed or illustrated, unless specifically identified as an order of performance. It is also to be understood that additional or alternative steps may be employed.
When an element or layer is referred to as being “on,” “engaged to,” “connected to,” or “coupled to” another element or layer, it may be directly on, engaged, connected or coupled to the other element or layer, or intervening elements or layers may be present. In contrast, when an element is referred to as being “directly on,” “directly engaged to,” “directly connected to,” or “directly coupled to” another element or layer, there may be no intervening elements or layers present. Other words used to describe the relationship between elements should be interpreted in a like fashion (e.g., “between” versus “directly between,” “adjacent” versus “directly adjacent,” etc.). As used herein, the term “and/or” includes any and all combinations of one or more of the associated listed items. As used herein, the term “about”, when used immediately previous to a specific recited value, denotes the specific recited value as well as all values, inclusive, from +/−10% of the specific recited value.
Although the terms first, second, third, etc. may be used herein to describe various elements, components, regions, layers and/or sections, these elements, components, regions, layers and/or sections should not be limited by these terms. These terms may be only used to distinguish one element, component, region, layer or section from another region, layer or section. Terms such as “first,” “second,” and other numerical terms when used herein do not imply a sequence or order unless clearly indicated by the context. Thus, a first element, component, region, layer or section discussed below could be termed a second element, component, region, layer or section without departing from the teachings of the example embodiments.
Spatially relative terms, such as “inner,” “outer,” “beneath,” “below,” “lower,” “above,” “upper,” and the like, may be used herein for ease of description to describe one element or feature's relationship to another element(s) or feature(s) as illustrated in the figures. Spatially relative terms may be intended to encompass different orientations of the device in use or operation in addition to the orientation depicted in the figures. For example, if the device in the figures is turned over, elements described as “below” or “beneath” other elements or features would then be oriented “above” the other elements or features. Thus, the example term “below” can encompass both an orientation of above and below. The device may be otherwise oriented (rotated 90 degrees or at other orientations) and the spatially relative descriptors used herein interpreted accordingly.
This invention was made with Government support under Contract No. DE-AC52-07NA27344 awarded by the United States Department of Energy. The Government has certain rights in the invention.