PRINT AND RECOAT ASSEMBLIES FOR ADDITIVE MANUFACTURING SYSTEMS AND METHODS FOR USING THE SAME
20230398740 · 2023-12-14
Assignee
Inventors
- John Sterle (Clifton Park, NY, US)
- Vadim Bromberg (Niskayuna, NY, US)
- Carlos H. Bonilla (Lebanon, OH, US)
- Tyler Andrew Griffith (West Chester, OH, US)
Cpc classification
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
B33Y30/00
PERFORMING OPERATIONS; TRANSPORTING
International classification
Abstract
A method for forming an object includes moving an assembly including an energy source, heating an initial layer of build material (31i, 31s, 31, 3, 50) positioned in a build area via forced convection around the energy source of the assembly, and spreading build material (31) on the build area, thereby depositing a second layer of build material (31i, 31s, 31, 3, 50) over the initial layer of build material (31 i, 31s, 31, 3, 50).
Claims
1. A method for forming an object, the method comprising: moving an assembly comprising an energy source; heating an initial layer of build material positioned in a build area via forced convection around the energy source of the assembly; and spreading build material on the build area, thereby depositing a second layer of build material over the initial layer of build material.
2. The method of claim 1, wherein the assembly is a recoat assembly comprising a powder spreading member.
3. The method of claim 1, wherein heating the initial layer of build material positioned in the build area further comprises heating the initial layer of build material via radiation emitted from the energy source.
4. The method of claim 1, wherein heating the build area via forced convection comprises passing a gas through a duct that is in communication with an energy source enclosure that at least partially encloses the energy source.
5. The method of claim 1, wherein the energy source is a first energy source, and wherein heating the initial layer of build material via force convection comprises passing a gas over the first energy source and a second energy source.
6. The method of claim 5, wherein passing the gas over the first energy source and the second energy source comprises passing the gas to an energy source enclosure that at least partially encloses the first energy source and the second energy source.
7. The method of claim 5, wherein passing the gas over the first energy source and the second energy source comprises passing the gas to first energy source enclosure that at least partially encloses the first energy source and passing the gas to a second energy source enclosure that at least partially encloses the second energy source.
8. A method for forming an object, the method comprising: moving a recoat assembly in a coating direction over a supply receptacle comprising build material, wherein the recoat assembly comprises a powder spreading member; contacting the build material in the supply receptacle with the powder spreading member; irradiating, with an energy source coupled to the recoat assembly, an initial layer of build material positioned in a build receptacle; and passing a gas over the energy source, thereby heating the initial layer of build material positioned in the build receptacle via forced convection.
9. The method of claim 8, further comprising: moving the build material in the coating direction with the powder spreading member to the build receptacle, thereby depositing a second layer of build material over the initial layer of build material; contacting the second layer of build material with the powder spreading member; moving at least a portion of the second layer of build material in a return direction to the supply receptacle; and depositing the at least a portion of the second layer of build material in the supply receptacle.
10. The method of claim 9, further comprising, subsequent to moving the second layer of build material, irradiating, with the energy source, the second layer of build material within the build receptacle.
11. The method of claim 10, further comprising passing a gas over the energy source, thereby heating the second layer of build material within the build receptacle via forced convection.
12. The method of claim 9, wherein depositing the at least a portion of the second layer of build material in the supply receptacle comprises depositing the at least a portion of the second layer of build material in a return chute in communication with the supply receptacle.
13. The method of claim 8, wherein the powder spreading member comprises one or more rollers.
14. An additive manufacturing system comprising: at least one of a print assembly and a recoat assembly; a housing assembly coupled to the at least one of the print assembly and the recoat assembly, the housing assembly comprising an energy source enclosure; an energy source positioned at least partially within the energy source enclosure; and an air distribution system in communication with the energy source enclosure, wherein the air distribution system comprises a pump structurally configured to pass a gas to the energy source enclosure to transfer thermal energy from the energy source.
15. The system of claim 14, wherein the housing assembly further comprises an upper housing defining a duct in communication with the energy source enclosure.
16. The system of claim 15, wherein the upper housing defines one or more vents in communication with the duct.
17. The system of claim 15, further comprising a controller communicatively coupled to the air distribution system, the controller comprising a processor and a computer readable and executable instruction set, which when executed, causes the processor to direct the air distribution system to pass the gas to the duct.
18. The system of claim 14, wherein the housing assembly is a first housing assembly, and system further comprises: a second housing assembly coupled to the at least one of the recoat assembly and the print assembly, the second housing assembly spaced apart from the first housing assembly and comprising a second energy source enclosure; and a second energy source positioned at least partially within the second energy source enclosure.
19. The system of claim 18, wherein the second housing assembly comprises a second upper housing defining a second duct in communication with the second energy source enclosure.
20. The system of claim 14, further comprising a powder plow assembly coupled to the at least one of the recoat assembly and the print assembly.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION
[0029] Reference will now be made in detail to embodiments of additive manufacturing apparatuses, and components thereof, examples of which are illustrated in the accompanying drawings. Whenever possible, the same reference numerals will be used throughout the drawings to refer to the same or like parts. Additive manufacturing systems according to the present disclosure generally include a recoat assembly for spreading build material in a build area. The recoat assembly may move build material from a build supply to the build area in sequential layers. In embodiments, the recoat assembly may move the excess build material back to the build supply such that the excess build material may be utilized in subsequent layers. In some embodiments, the recoat assembly or a print assembly may include one or more energy sources that can apply energy to the build material. In embodiments described herein, an air distribution system may distribute heat generated by the one or more energy sources by forced convection. These and other embodiments of recoat assemblies and print assemblies for additive manufacturing systems, additive manufacturing systems comprising the recoat and print assemblies, and methods for using the same are described in further detail herein with specific reference to the appended drawings.
[0030] Ranges can be expressed herein as from “about” one particular value, and/or to “about” another particular value. When such a range is expressed, another embodiment includes from the one particular value and/or to the other particular value. Similarly, when values are expressed as approximations, by use of the antecedent “about,” it will be understood that the particular value forms another embodiment. It will be further understood that the endpoints of each of the ranges are significant both in relation to the other endpoint, and independently of the other endpoint.
[0031] Directional terms as used herein—for example up, down, right, left, front, back, top, bottom—are made only with reference to the figures as drawn and are not intended to imply absolute orientation unless otherwise expressly stated.
[0032] The phrase “communicatively coupled” is used herein to describe the interconnectivity of various components and means that the components are connected either through wires, optical fibers, or wirelessly such that electrical, optical, and/or electromagnetic signals may be exchanged between the components.
[0033] Unless otherwise expressly stated, it is in no way intended that any method set forth herein be construed as requiring that its steps be performed in a specific order, nor that with any apparatus specific orientations be required. Accordingly, where a method claim does not actually recite an order to be followed by its steps, or that any apparatus claim does not actually recite an order or orientation to individual components, or it is not otherwise specifically stated in the claims or description that the steps are to be limited to a specific order, or that a specific order or orientation to components of an apparatus is not recited, it is in no way intended that an order or orientation be inferred, in any respect. This holds for any possible non-express basis for interpretation, including: matters of logic with respect to arrangement of steps, operational flow, order of components, or orientation of components; plain meaning derived from grammatical organization or punctuation, and; the number or type of embodiments described in the specification.
[0034] As used herein, the singular forms “a,” “an” and “the” include plural referents unless the context clearly dictates otherwise. Thus, for example, reference to “a” component includes aspects having two or more such components, unless the context clearly indicates otherwise.
[0035] Referring now to
[0036] In operation, build material 31, such as organic or inorganic powder, is positioned on the supply platform 130. The supply platform 130 is actuated to present a layer of the build material 31 in the path of the recoat assembly 200. The recoat assembly 200 is then actuated along a working axis 116 of the additive manufacturing system 100 towards the build platform 120. As the recoat assembly 200 traverses the working axis 116 over the supply platform 130 towards the build platform 120, the recoat assembly 200 distributes the layer of build material 31 in the path of the recoat assembly 200 from the supply platform 130 to the build platform 120.
[0037] Thereafter, the print assembly 150 moves along the working axis 116 over the build platform 120 and may deposit a layer of binder 50 in a predetermined pattern on the layer of build material 31 that has been distributed on the build platform 120. After the binder 50 is deposited, an energy source may be utilized to cure the deposited binder 50, as described in greater detail herein. The print assembly 150 can then move to a home position 158 where at least a portion of the print assembly 150 is positioned over the cleaning station 110. While the print assembly 150 is in the home position 158, the print assembly 150 works in conjunction with the cleaning station 110 to provide cleaning and maintenance operations on the elements of the print assembly 150 to ensure the elements are not fouled or otherwise clogged. This may assist in ensuring that the print assembly 150 is capable of depositing the binder 50 in the desired pattern during a subsequent deposition pass.
[0038] During this maintenance interval, the supply platform 130 is actuated in an upward vertical direction (i.e., in the +Z direction of the coordinate axes depicted in the figure) as indicated by arrow 10 to present a new layer of build material 31 in the path of the recoat assembly 200. The build platform 120 is actuated in the downward vertical direction (i.e., in the −Z direction of the coordinate axes depicted in the figure) as indicated by arrow 12 to prepare the build platform 120 to receive a new layer of build material 31 from the supply platform 130. The recoat assembly 200 is then actuated along the working axis 116 of the additive manufacturing system 100 again to add another layer of build material 31 and binder 50 to the build platform 120. This sequence of steps is repeated multiple times to build an object on the build platform 120 in a layer-wise manner.
[0039] While the embodiment depicted in
[0040] Referring to
[0041] Referring to
[0042] Referring to
[0043] In some embodiments, the recoat assembly 200 generally includes one or more energy sources that are structurally configured to apply generally emit electromagnetic radiation, such as infrared radiation, ultraviolet radiation, or the like. In some embodiments, the recoat assembly 200 may include a first energy source 260 and/or a second energy source 262 that may emit energy that heats build material 31 (
[0044] In the embodiment depicted in
[0045] Referring to
[0046] For example and referring particularly to
[0047] As the gas passes through the one or more apertures 229, the gas can then flow around the first energy source 260 and/or the second energy source 262, as shown in
[0048] In particular, in embodiments, the build material 31 and/or the binder 50 may receive thermal energy via radiation emitted from the first energy source 260 and/or the second energy source 262. The gas passed over the first energy source 260 and/or the second energy source 262 may supplement the thermal energy applied to the build material 31 and/or the binder 50 via radiation. In some embodiments, the build material 31 and/or the binder 50 may be primarily heated via radiation from the first energy source 260 and/or the second energy source 262, while the gas passed over the first energy source 260 and/or the second energy source 262 supplements the energy transferred via radiation. In embodiments, the air distribution system 230 may increase the heat density applied to the build material 31 and/or the binder 50 by the first energy source 260 and/or the second energy source 262 and/or may increase the area of thermal energy applied by the first energy source 260 and/or the second energy source 262. In some embodiments, the air distribution system 230 may assist in maintaining a stable boundary layer close to the build material 31 and/or binder 50, for example, by more evenly distributing thermal energy applied by the first energy source 260 and/or the second energy source 262 as compared to systems that do not include an air distribution system 230. Furthermore, by passing gas over the first energy source 260 and/or the second energy source 262, heat that would otherwise dissipate and be lost may be utilized to heat the build material 31 and/or build material 50, thereby increasing the energy efficiency of the first energy source 260 and/or the second energy source 262.
[0049] By more efficiently transferring thermal energy from the first energy source 260 and/or the second energy source 262 to build material 31 and/or binder 50, the air distribution system 230 may assist in curing the binder 50 more quickly than additive manufacturing systems that do not include an air distribution system 230.
[0050] For example and referring to
[0051] However, because the air distribution system 230 assists in transferring thermal energy from the first energy source 260 and the second energy source 262, sufficient thermal energy may be applied to the build material 31 and the binder 50 while the recoat assembly 200 is moved along the working axis 116 at high speeds, as compared to conventional additive manufacturing systems that do not include the air distribution system 230.
[0052] Further, in some instances, the air distribution system 230 may allow the first energy source 260 and/or the second energy source 262 to be operated at a reduced power while still providing a similar amount of energy to the build material 31 and the binder 50 as configurations that do not include the air distribution system 230. By operating the first energy source 260 and/or the second energy source 262 at reduced power, a usable life of the first energy source 260 and/or the second energy source 262 may be increased as compared to conventional configurations.
[0053] Furthermore, in embodiments, the air distribution system 230 may dissipate heat transferred from the first energy source 260 and/or the second energy source 262 to the lower housing 224 and/or the upper housing 222, thereby cooling the lower housing 224 and/or the upper housing 222. In some embodiments, components (e.g., sensors and the like) of the recoat assembly 200 may be positioned proximate to and/or may be coupled to the lower housing 224 and/or the upper housing 222. By cooling the lower housing 224 and/or the upper housing 222, the air distribution system 230 may reduce the likelihood of overheating and damaging components (e.g., sensors and the like) of the recoat assembly 200 coupled to or positioned proximate to the lower housing 224 and/or the upper housing 222. In embodiments in which the upper housing 222 and/or the lower housing 224 define the vents 227, gas may additionally be passed through the vents 227, which may also assist in cooling components (e.g., sensors and the like) of the recoat assembly 200 coupled to or positioned proximate to the lower housing 224 and/or the upper housing 222.
[0054] While in the embodiment described above and depicted in
[0055] Referring to
[0056] Referring to
[0057] The memory component 306 may store operating logic, analysis logic, and communication logic in the form of one or more computer readable and executable instruction sets. The analysis logic and the communication logic may each include a plurality of different pieces of logic, each of which may be embodied as a computer program, firmware, and/or hardware, as an example. A local interface may also be included in the controller 300, and may be implemented as a bus or other communication interface to facilitate communication among the components of the controller 300.
[0058] The processor 302 may include any processing component operable to receive and execute instructions (such as from a data storage component 304 and/or the memory component 306). It should be understood that while the components in
[0059] In embodiments, the controller 300 is communicatively coupled to one or more components of the additive manufacturing system. For example, in the embodiment depicted in
[0060] The controller 300 may send signals to the first energy source 260 and/or the second energy source 262 that cause the first energy source 260 and/or the second energy source 262 to emit energy, irradiating build material 31 (
[0061] The controller 300 may send signals to the air distribution system 230 that causes the air distribution system 230 to induce gas flow to the first energy source 260 and/or the second energy source 262, as described above. For example, the controller 300 may be communicatively coupled to the pump 232 or the like that induces the flow of gas through the air distribution system 230. In some embodiments, the controller 300 may send signals to the air distribution system 230 that changes a volume and/or velocity of the flow of gas through the air distribution system.
[0062] In embodiments, the controller 300 may send signals to the recoat assembly transverse actuator 144 causing the recoat assembly transverse actuator 144 to move the recoat assembly 200 (
[0063] In some embodiments, the controller 300 may send signals to the one or more roller actuators 146 that are coupled to and cause the one or more roller actuators 146 to rotate the first roller 202 (
[0064] In some embodiments, one or more sensors 338 are communicatively coupled to the controller 300. The one or more sensors 338 may one or more temperature sensors such as thermocouples, resistance temperature detectors (RTDs), infrared pyrometers, or the like. The one or more sensors 338 may send signals to the controller 300 indicative of detected temperatures at various locations within the additive manufacturing system 100. In embodiments, the controller 300 may direct various components of the additive manufacturing system 100 (e.g., the first energy source 260, the second energy source 262, the recoat assembly transverse actuator 144, the air distribution system 230, etc.) in response to temperatures detected via the one or more sensors 338.
[0065] Referring to
[0066] The powder plow 316 may be formed from any suitable material with a wear resistant low coefficient of friction coating. As a non-limiting example, the powder plow 316 may be formed from electroless nickel with co-deposited polytetrafluoroethylene (PTFE) or may be electropolished.
[0067] Referring now to
[0068] Methods for operating the recoat assembly 200 will now be described with reference to the appended drawings. In some embodiments, the controller 300 may direct the recoat assembly 200 to perform the methods described below.
[0069] Referring to
[0070] The recoat assembly, via the powder spreading member (e.g., the first roller 202 and/or the second roller 204), moves build material 31 in the coating direction 40 from the supply receptacle 134 to a build area (e.g., the build receptacle 124) which is spaced apart from the supply receptacle 134. In embodiments, the powder spreading member (e.g., the first roller 202 and/or the second roller 204) deposits a second layer of build material 31 over an initial layer of build material 31 positioned in the build receptacle 124, for example as the result of a previous cycle of the recoat assembly 200.
[0071] For example and referring to
[0072] In embodiments, the powder spreading member (e.g., the first roller 202 and/or the second roller 204) contacts the second layer of build material 31.sub.S, and moves at least a portion of the second layer of build material 31.sub.S in a return direction 42 back to the supply receptacle 134. The powder spreading member (e.g., the first roller 202 and/or the second roller 204) then deposits at least a portion of the second layer of build material 31.sub.S into the supply receptacle 134. In some embodiments, the at least a portion of the second layer of build material 31.sub.S can be deposited directly in the supply receptacle 134 by the powder spreading member (e.g., the first roller 202 and/or the second roller 204). In some embodiments, the additive manufacturing system 100 may include a return chute 140 in communication with the supply receptacle 134, and the at least a portion of the second layer of build material 31.sub.S may be deposited within the return chute 140.
[0073] Accordingly, in embodiments an initial thickness of the second layer of build material 31.sub.S may be greater than a final thickness of the build material 31.sub.S that remains after the at least a portion of the second layer of build material 31.sub.S is moved back to the supply receptacle 134 by the recoat assembly 200. By initially depositing an excess amount of build material 31 to form the second layer of build material 31.sub.S, voids within the second layer of build material 31.sub.S can be reduced. Further, by initially depositing an excess amount of build material 31 to form the second layer of build material 31.sub.S, forces applied to the initial layer of build material 31.sub.1 and/or cured binder 50 (
[0074] In some embodiments, the first energy source 260 and/or the second energy source 262 may irradiate the initial layer of build material 31.sub.1 and/or the second layer of build material 31.sub.S positioned within the build area (e.g., the build receptacle 124).
[0075] Based on the foregoing, it should be understood that embodiments described herein are directed to additive manufacturing systems that generally include a recoat assembly for spreading build material in a build area. The recoat assembly may move build material from a build supply to the build area in sequential layers. In embodiments, the recoat assembly may move the excess build material back to the build supply such that the excess build material may be utilized in subsequent layers. In some embodiments, the recoat assembly and/or print assembly may include one or more energy sources that can apply energy to the build material. In embodiments described herein, an air distribution system that may distribute heat generated by the one or more energy sources by forced convection.
[0076] It will be apparent to those skilled in the art that various modifications and variations can be made to the embodiments described herein without departing from the spirit and scope of the claimed subject matter. Thus it is intended that the specification cover the modifications and variations of the various embodiments described herein provided such modification and variations come within the scope of the appended claims and their equivalents.
[0077] Further aspects of the present disclosure are provided in the following clauses: [0078] 1. A method for forming an object, the method comprising moving an assembly comprising an energy source, heating an initial layer of build material positioned in a build area via forced convection around the energy source of the assembly, and spreading build material on the build area, thereby depositing a second layer of build material over the initial layer of build material. [0079] 2. The method of any preceding clause, wherein the assembly is a recoat assembly comprising a powder spreading member. [0080] 3. The method of any preceding clause, wherein heating the initial layer of build material positioned in the build area further comprises heating the initial layer of build material via radiation emitted from the energy source. [0081] 4. The method of any preceding clause, wherein heating the build area via forced convection comprises passing a gas through a duct that is in communication with an energy source enclosure that at least partially encloses the energy source. [0082] 5. The method of any preceding clause, wherein the energy source is a first energy source, and wherein heating the initial layer of build material via force convection comprises passing a gas over the first energy source and a second energy source. [0083] 6. The method of any preceding clause, wherein passing the gas over the first energy source and the second energy source comprises passing the gas to an energy source enclosure that at least partially encloses the first energy source and the second energy source. [0084] 7. The method of any preceding clause, wherein passing the gas over the first energy source and the second energy source comprises passing the gas to first energy source enclosure that at least partially encloses the first energy source and passing the gas to a second energy source enclosure that at least partially encloses the second energy source. [0085] 8. A method for forming an object, the method comprising moving a recoat assembly in a coating direction over a supply receptacle comprising build material, wherein the recoat assembly comprises a powder spreading member, contacting the build material in the supply receptacle with the powder spreading member, irradiating, with an energy source coupled to the recoat assembly, an initial layer of build material positioned in a build receptacle, and passing a gas over the energy source, thereby heating the initial layer of build material positioned in the build receptacle via forced convection. [0086] 9. The method of any preceding clause, further comprising moving the build material in the coating direction with the powder spreading member to the build receptacle, thereby depositing a second layer of build material over the initial layer of build material, contacting the second layer of build material with the powder spreading member, moving at least a portion of the second layer of build material in a return direction to the supply receptacle, and depositing the at least a portion of the second layer of build material in the supply receptacle. [0087] 10. The method of any preceding clause, further comprising, subsequent to moving the second layer of build material, irradiating, with the energy source, the second layer of build material within the build receptacle. [0088] 11. The method of any preceding clause, further comprising passing a gas over the energy source, thereby heating the second layer of build material within the build receptacle via forced convection. [0089] 12. The method of any preceding clause, wherein depositing the at least a portion of the second layer of build material in the supply receptacle comprises depositing the at least a portion of the second layer of build material in a return chute in communication with the supply receptacle. [0090] 13. The method of any preceding clause, wherein the powder spreading member comprises one or more rollers. [0091] 14. An additive manufacturing system comprising at least one of a print assembly and a recoat assembly, a housing assembly coupled to the at least one of the print assembly and the recoat assembly, the housing assembly comprising an energy source enclosure, an energy source positioned at least partially within the energy source enclosure, and an air distribution system in communication with the energy source enclosure, wherein the air distribution system comprises a pump structurally configured to pass a gas to the energy source enclosure to transfer thermal energy from the energy source. [0092] 15. The system of any preceding clause, wherein the housing assembly further comprises an upper housing defining a duct in communication with the energy source enclosure. [0093] 16. The system of any preceding clause, wherein the upper housing defines one or more vents in communication with the duct. [0094] 17. The system of any preceding clause, further comprising a controller communicatively coupled to the air distribution system, the controller comprising a processor and a computer readable and executable instruction set, which when executed, causes the processor to direct the air distribution system to pass the gas to the duct. [0095] 18. The system of any preceding clause, wherein the housing assembly is a first housing assembly, and system further comprises a second housing assembly coupled to the at least one of the recoat assembly and the print assembly, the second housing assembly spaced apart from the first housing assembly and comprising a second energy source enclosure, and a second energy source positioned at least partially within the second energy source enclosure. [0096] 19. The system of any preceding clause, wherein the second housing assembly comprises a second upper housing defining a second duct in communication with the second energy source enclosure. [0097] 20. The system of any preceding clause, further comprising a powder plow assembly coupled to the at least one of the recoat assembly and the print assembly.