Additive manufacturing system and method using multiple beam orientations

Abstract

To provide an additive manufacturing system and method using multiple beam orientations.SOLUTION: An additive manufacturing system 100 includes one or more processors 118 configured to determine one or more geometrical characteristics of each of multiple segments of a build part 116. The one or more geometrical characteristics include an angle of incidence between a beam line extending from a beam source 106 and a surface normal of a respective skin of the segment. The one or more processors are configured to control the additive manufacturing instrument, based on the one or more geometrical characteristics, to direct focused energy beams from a first orientation to form a first segment of the build part and to direct focused energy beams from a second orientation to form a second segment thereof.SELECTED DRAWING: Figure 1

Description

[Technical Field]

[0001] TECHNICAL FIELD Embodiments of the present disclosure generally relate to additive manufacturing of three-dimensional built parts. [Background technology]

[0002] Additive manufacturing refers to any process for producing three-dimensional built parts in which successive layers of a base material are deposited under computer control. The deposited layers are selectively fused by application of a focused energy beam, such as a laser, which heats and bonds the material. The size and shape of the built part can be based on a three-dimensional computer model or other electronic data source. Additive manufacturing can be used to produce objects with complex structures and shapes. Additive manufacturing techniques for producing metal built parts allow for greater design freedom than traditional metal manufacturing techniques, such as die casting and extrusion, and can result in more accurate and repeatable finished products than such traditional metal manufacturing techniques.

[0003] Setting up for an additive manufacturing build process involves selecting the configuration of the build part to be built, defining the position of the build part on a build platform, and generating a build plan for building the build part according to the selected configuration and the defined positioning relative to the platform. Positioning may refer to the location of the build part relative to the build platform, e.g., relative to the center and / or edge of the platform, as well as the planned orientation of the build part relative to the platform, e.g., its rotational direction about a vertical axis and / or its angular orientation (e.g., tilt or inclination). The build plan controls the performance of additive manufacturing equipment during the build process. The build plan may define the sequence of operations to be performed by the equipment and may also define parameters and settings. For a focused energy source, the build plan may provide the path along which the emitted energy beam should be directed, as well as parameters of the energy beam, such as energy intensity, beam width, or beam diameter. Summary of the Invention [Problem to be solved by the invention]

[0004] Typically, the positioning and build plan of a built part are determined without consideration of how the positioning of the built part relative to the focused energy source may affect the surface and subsurface quality of the built part, such as the surface roughness and porosity of the built part. After the additive manufacturing build process, various finishing operations may be performed on the manufactured built part, for example, to smooth out rough surfaces. Grinding rough surfaces and other finishing operations to improve the surface quality of the part can be expensive, difficult, time-intensive, and / or labor-intensive, thereby reducing manufacturing efficiency and increasing production costs. In addition, current methods may be insufficient for parts with inaccessible areas where typical post-processing may be ineffective or impossible. Furthermore, if the surface quality, subsurface quality, or dimensional accuracy of the built part is sufficiently degraded during the additive manufacturing process, the entire built part may need to be scrapped, which is a waste of time and resources. [Means for solving the problem]

[0005] In one or more embodiments, an additive manufacturing system is provided that includes one or more processors configured to determine one or more geometric characteristics of each of a plurality of segments of a built part at candidate locations relative to an additive manufacturing device. The one or more geometric characteristics include an angle of incidence between a beam line extending from a source of a focused energy beam and a surface normal of a skin of each of the corresponding segments proximate the beam line. The one or more processors are configured to control the additive manufacturing device based on the one or more geometric characteristics to direct the focused energy beam from a first direction relative to the built part to form a first one of the segments of the built part and to direct the focused energy beam from a second direction relative to the built part to form a second one of the segments of the built part.

[0006] In one or more embodiments, a method (e.g., a method for additively manufacturing a built part) is provided. The method includes determining one or more geometric characteristics of each of a plurality of segments of the built part at candidate locations relative to an additive manufacturing device before additively manufacturing the built part. The one or more geometric characteristics include an angle of incidence between a beam line extending from a source of a focused energy beam and a surface normal of a skin of each of the corresponding segments proximate the beam line. The method also includes controlling the additive manufacturing device based on the one or more geometric characteristics to direct the focused energy beam from a first direction relative to the built part to form a first one of the segments of the built part, and controlling the additive manufacturing device based on the one or more geometric characteristics to direct the focused energy beam from a second direction relative to the built part to form a second one of the segments of the built part.

[0007] In one or more embodiments, an additive manufacturing system is provided that includes an additive manufacturing device and one or more processors. The additive manufacturing device includes a platform and one or more beam emitters configured to emit focused energy beams from a plurality of different source locations relative to the platform. The one or more processors are configured to determine one or more geometric characteristics of each of a plurality of segments of a built part at candidate locations relative to the additive manufacturing device. The one or more geometric characteristics include an angle of incidence between a beam line extending from a corresponding one of the source locations and a surface normal of a skin of each of the corresponding segments proximate the beam line. The one or more processors are configured to control the one or more beam emitters based on the one or more geometric characteristics to direct the focused energy beam from a first source location relative to the platform to form a first one of the segments of the built part and to direct the focused energy beam from a second source location relative to the platform to form a second one of the segments of the built part.

[0008] These and other features, aspects, and advantages of the present disclosure will be better understood when the following detailed description is read in conjunction with the accompanying drawings, in which like numerals represent like parts throughout. [Brief explanation of the drawings]

[0009] [Figure 1] FIG. 1 is a schematic diagram of an additive manufacturing system according to a first embodiment of the present disclosure. [Figure 2] FIG. 1 illustrates a schematic diagram of additive manufacturing equipment in an additive manufacturing system according to one embodiment. [Figure 3] 3 shows an enlarged portion of the first coupon shown in FIG. 2. [Figure 4] FIG. 1 shows a schematic diagram of an additive manufacturing device during a first build stage of a single coupon according to an embodiment of the present disclosure. [Figure 5] FIG. 5 shows a schematic diagram of the additive manufacturing equipment during the second build stage of the coupon shown in FIG. [Figure 6] FIG. 6 shows a schematic diagram of the additive manufacturing equipment during the third build stage of the coupon shown in FIGS. 4 and 5. [Figure 7] FIG. 1 shows a schematic diagram of an additive manufacturing apparatus according to another embodiment of the present disclosure. [Figure 8] FIG. 2 shows a schematic diagram of an additive manufacturing device according to the embodiment shown in FIG. 1. [Figure 9] FIG. 1 shows a schematic diagram of an additive manufacturing apparatus according to another embodiment of the present disclosure. [Figure 10] FIG. 1 shows a schematic diagram of an additive manufacturing apparatus according to another embodiment of the present disclosure. [Figure 11] 10 illustrates an additive manufacturing device according to another embodiment that utilizes an optical component to redirect a focused energy beam relative to a build part. [Figure 12] 10 illustrates an additive manufacturing device according to another embodiment that utilizes an optical component to redirect a focused energy beam relative to a build part. [Figure 13] 1 is a flowchart of a method according to one embodiment of the present disclosure for additively manufacturing a built part during a build process by directing a focused energy beam along a plurality of different beam orientations relative to the built part. DETAILED DESCRIPTION OF THE INVENTION

[0010] The foregoing summary, as well as the following detailed description of certain embodiments, may be better understood when read in conjunction with the accompanying drawings. As used herein, elements or steps listed in the singular and preceded by the words "a" or "an" do not necessarily exclude a plurality of elements or steps. Furthermore, references to "one embodiment" are not intended to be interpreted as excluding the existence of additional embodiments that also incorporate the recited features. Furthermore, unless expressly stated to the contrary, embodiments "comprising" or "having" an element or elements having a particular characteristic may include additional elements that do not have that characteristic.

[0011] Considering the cost, time, and effort of performing surface treatments after the additive build process, there are several advantages to additively manufacturing built parts that have inherently improved surface quality, near-surface quality, and geometric precision, thereby eliminating or at least facilitating post-build surface treatments. Embodiments of the present disclosure provide systems (e.g., additive manufacturing systems) and methods for controlling the formation of additively manufactured built parts using multiple beam orientations relative to the built part. The relative position of the beam source to the geometry of the built part can affect the stable process parameter window and, therefore, the quality of the manufactured result.

[0012] For example, an additive manufacturing device may be controlled to direct (e.g., emit, reflect, etc.) a focused energy beam from a first source location toward a built part on a platform to form a first segment or section of the built part, and the additive manufacturing device may be controlled to direct a focused energy beam from a second source location spaced apart from the first source location toward the built part to form a second segment or section of the built part. In one embodiment, a first beam emitter (e.g., a laser) located at the first source location emits a focused energy beam to form the first segment of the built part, and a second beam emitter located at the second source location emits a focused energy beam to form the second segment of the built part. In other embodiments, a single beam emitter is configured to be moved between the first and second source locations, whereby the same beam emitter emits focused energy beams from multiple different locations on the built part to form the first and second segments of the built part. In yet other embodiments, instead of or in addition to moving the beam emitter, the building part is moved relative to the beam emitter and other optical components. Optionally, optical components such as mirrors, prisms, etc. can be used to provide additional beam source locations as the optical components direct the received beam towards the building part.

[0013] Varying the geometric relationship between the energy beam and the geometry of the built part to be manufactured during the build process can improve the geometric precision and surface and near-surface quality of the built part compared to maintaining a fixed geometric relationship between the energy beam and the geometry of the built part throughout the build process. In one or more embodiments described herein, the additive manufacturing system determines multiple geometric locations, such as beam source locations, and / or which segments of the built part should originate from each of multiple beam source locations based on one or more geometric characteristics of the segments of the built part. The geometric characteristics may include the angle of incidence of the segments of the built part, the orientation of the segments with respect to the top surface of the platform, and / or the like, as described in more detail herein. The angle of incidence is the angle between a line extending from the beam emitter (e.g., laser path) to the segment and the surface normal of the skin or side of the segment of the built part directly beneath the layer being deposited. The skin used to determine the angle of incidence is defined by the edge of a layer that may have recently been deposited. The systems and methods may analyze the morphology of the built part at candidate positions of the built part on the platform to determine one or more geometric characteristics of various segments or shapes of the built part. Known additive manufacturing systems do not emit focused energy beams from multiple different geometric locations during the build process to form different segments of a built part based on an analysis of the geometric features of the built part for the purpose of improving part accuracy and quality. Known additive manufacturing systems do not take into account the angle of incidence defined between the beam emitter and a line perpendicular to the skin directly below the top layer (e.g., the layer being deposited or the most recently deposited layer) of the built part. As previously discussed, improving surface quality during the build process can increase manufacturing efficiency and reduce costs by eliminating or at least facilitating post-build surface finishing processes. Another advantage is enabling the formation of built parts with smoother surfaces (with or without post-processing).

[0014] As used herein, a built part refers to a virtual object that is designed to be additively manufactured as well as a physical object that is manufactured by an additive manufacturing build process. The position or positioning of a built part within an additive manufacturing equipment refers to the location and orientation of the built part. For example, a location represents a particular area of ​​the build platform of the additive manufacturing equipment onto which the built part is built layer by layer. Often, multiple built parts are built during a common build process, and therefore the built parts are positioned at different locations along the top surface of the build platform. The orientation of a built part generally refers to the direction that the built part (i.e., the part to be built) faces and the tilt or inclination of the built part. For example, a built part may be oriented about a longitudinal axis. Orientation may include rotation of the built part about the longitudinal axis. Orientation may also include tilt or inclination of the longitudinal axis relative to a vertical axis.

[0015] The surface quality of a given surface may refer to the surface roughness, the porosity content of the wall defining the given surface, the structural and / or compositional uniformity of the wall, and / or the like. Generally, a high quality surface of an additively manufactured built part will have fewer pores, smaller pores, and be smoother (e.g., less rough) than a lower quality surface. One or more of the embodiments described herein are configured to produce built parts having desired and / or satisfactory surface and subsurface quality and dimensional accuracy to reduce scrap rates and the amount of surface finishing after the build process.

[0016] FIG. 1 is a schematic diagram of an additive manufacturing system 100 according to one embodiment. The additive manufacturing (AM) system 100 includes an additive manufacturing (AM) device 101, a control unit 108, an input device 134, and a display device 136. The control unit 108 can control the operation of the AM device 101. The input device 134 and / or the display device 136 are optional components. The AM device 101 includes a build platform (or plate) 102, a housing 104, a beam emitter 106, and a feedstock applicator 117. The platform 102 is a planar surface of the AM device 101 and may be represented by a plate, a bottom wall of the housing 104, or the like. The AM device 101 performs an additive manufacturing build process to form three-dimensional built parts 116. Each built part 116 is built from the top surface 110 of the platform 102 by selectively depositing feedstock material 111 in successive layers 114 and fusing the feedstock material 111 at defined locations according to a build plan 132. Each layer 114 can be relatively thin, such as 0.5 mm or less, 0.25 mm or less, or 0.1 mm or less.

[0017] 1 can be utilized to perform a variety of additive manufacturing processes. Suitable additive manufacturing processes can include, for example, material extrusion (e.g., fused deposition modeling), vat photopolymerization (e.g., stereolithography, digital light processing, continuous digital light processing, light emitting diodes, and / or the like), powder bed fusion (e.g., multi-jet fusion, selective laser sintering, etc.), material jetting (e.g., material jetting, nanoparticle jetting, drop-on-demand, etc.), selective laser melting, and binder jetting. All of these processes involve depositing layers of material onto a build surface and fusing selected portions of the material using a form of energy and / or polymer binder that scans the surface based on a CAD pattern.

[0018] The raw material 111 may be in powder form. In a non-limiting example, the powder includes one or more metals in the form of metal particles, flakes, etc. The powder may also optionally include a non-metallic filler material mixed with the metallic material. The metallic material may include various metal types, such as aluminum, stainless steel, copper, nickel, cobalt, titanium, and alloys of various metal types. Possible non-metallic filler materials in the powder may include ceramics, polymers (e.g., plastics), silica, etc. The powder that is deposited but not fused to form part of the build part 116 defines a powder bed 122 of virgin material 111 contained within the walls 112A, 112B of the housing 104. In one embodiment, the part 116 is enclosed within the powder bed 122 during the build process. In another embodiment, the raw material 111 is metal-free.

[0019] The build part 116 is gradually formed or built by agglomerating surface layers 114 in a build direction 124 along a build axis 126. Each successive addition of material 111 to the top end of the part 116 causes the part 116 to grow in the build direction 124. The build direction 124 extends away from the platform 102. In the illustrated embodiment, the build axis 126 is perpendicular to the plane of the top surface 110 of the platform 102.

[0020] The AM system 100 creates new layers of the part 116 by spreading a thin layer or layers of powder material 111 over the top of the part 116. For example, a feedstock applicator 117 of the AM system 100 deposits each layer 114 of material 111. The feedstock applicator 117 may include or represent a spreader or recoater device that evenly spreads the thin layer of material 111, an injector that injects the material 111, or the like. The material 111 may be stored in a reservoir before use. The feedstock applicator 117 is controlled by the control unit 108.

[0021] The beam emitter 106 is then controlled by the control unit 108 to emit a focused energy beam toward the raw material 111 in the top surface layer 114. The high-energy beam transfers energy to defined portions of the material 111 that it strikes, causing the defined portions to fuse (e.g., melt and adhere) to the compacted mass of the built part 116. As a result, a new surface layer or fragment of the part 116 is formed. The focused energy beam is electromagnetic energy. For example, the beam emitter 106 can be a laser device that generates a high-energy laser beam. The beam emitter 106 can be suspended above the top of the powder bed 122, for example, about 0.5 meters (m) above the top surface 110 of the platform 102. The focused energy beam emitted from the beam emitter 106 is aimed and / or directed toward different locations on the powder bed 122 to fuse different selected portions of the top surface layer 114 to the part 116. The beam emitter 106 may include a scan head 142 that allows the beam to be directed to different locations within a defined coverage area without moving (e.g., displacing) the location of the beam emitter 106 relative to other components of the AM equipment 101. The orientation of the scan head and parameters of the energy beam (e.g., timing, energy intensity, beam width, etc.) may be controlled by the control unit 108 via control signals. This process repeats continuously according to instructions in the build plan 132 until the built part 116 is fully formed.

[0022] The AM apparatus 101 is configured to enable a focused energy beam to be emitted toward a part 116 on a platform 102 from a plurality of different source locations relative to the part 116. Only one beam emitter 106 is shown in FIG. 1 , and the beam emitter 106 is movable (e.g., translatable) relative to the part 116 and the platform 102 to change the beam source location. The beam emitter 106 may be mechanically connected to an actuator 140 and mounted to a rail or gantry 144 that defines a track. The actuator 140 may be controlled by a control unit 108 to selectively position the beam emitter 106 at different locations along the length of the track. For example, the actuator 140 may move the beam emitter 106 along the rail or gantry 144 toward a first wall 112A of the housing 104 and / or toward a second wall 112B of the housing 104. Movement of the beam emitter 106 along the rail or gantry 144 is independent of the movement of the scan head 142 of the beam emitter 106. In one embodiment, the AM apparatus 101 has only one beam emitter 106, and movement of the beam emitter 106 allows different segments of the part 116 to be formed from different beam source locations. In another embodiment, the AM apparatus 101 includes one or more reflective surfaces that function as relay components. The one or more reflective surfaces may be spaced apart from the beam emitter 106 to redirect the focused energy beam that strikes the reflective surface onto the platform 102, effectively changing the source location of the energy beam relative to the built part 116.

[0023] In one or more alternative embodiments, the AM apparatus 101 includes multiple beam emitters 106. In a first alternative embodiment, each of the multiple beam emitters 106 is fixed at a different predetermined position (e.g., non-translatable), and the control unit 108 selectively controls the beam emitters 106 to provide focused energy beams from different source locations. For example, in the first alternative embodiment, the AM apparatus 101 may lack the actuator 140 and the rail or gantry 144. In a second alternative embodiment, at least one of the multiple beam emitters 106 is translatable relative to other components of the AM apparatus 101, similar to the beam emitter 106 shown in FIG. 1 . For example, the AM apparatus 101 may include at least one translatable beam emitter 106 and at least one non-translatable beam emitter 106, or may include multiple translatable beam emitters 106 without any non-translatable beam emitters 106.

[0024] The AM apparatus 101 may be controlled to form one or more external supports 120 during the build process to structurally support the overhanging features of the built part 116. The one or more external supports 120 are formed additively during the same build process that forms the built part 116. For example, the built part 116 and the external supports 120 are both composed of a series of stacked material layers that are fused together during the additive manufacturing build process. Optionally, the internal structure (e.g., density, lattice, etc.) and / or material composition of the external supports 120 may be different from that of the built part 116. For example, the structure of the external supports 120 may be less dense than the structure of the built part 116.

[0025] The control unit 108 includes one or more processors 118 (e.g., one or more microprocessors, integrated circuits, microcontrollers, field programmable gate arrays, etc.) and / or hardware circuitry in communication with these processors 118 that perform the operations described with respect to the control unit 108. The one or more processors 118 may operate based on programmed instructions. The one or more processors 118, which may include a single processor or multiple processors, are referred to herein as the plural "processors" without limiting the scope to requiring multiple processors 118. The control unit 108 also includes a tangible, non-transitory computer-readable storage medium (e.g., memory) 130. The memory 130 may store programmed instructions (i.e., software) that direct the operation of the processors 118. For example, the memory 130 stores a build plan 132 associated with the construction part 116 being manufactured.

[0026] Memory 130 may also store a part design file 138 for built part 116. Part design file 138 may be a computer-aided design (CAD) file or other data file that describes the physical characteristics of part 116, such as the shape, size, and / or composition of part 116. Build plan 132 may be generated based on design file 138. Build plan 132 may be a data file that defines parameters, conditions, settings, and / or actions of AM equipment 101 to manufacture a physical built part 116 that is a replica or counterpart of the virtual part characterized in design file 138. One or more parameters or settings defined by build plan 132 may include the positioning of built part 116 on platform 102, the sequence of actions to be taken by AM equipment 101 to build part 116, the location of supports 120, etc. The sequence of actions to be taken by the AM apparatus 101 as defined in the build plan 132 may include when and where the actuators 140 should move the beam emitters 106 (if the beam emitters are translatable) and / or the platform 102 (if the platform is translatable), a defined scan path along which the scan head 142 of each emitter 106 directs a focused energy beam from its corresponding beam source location, parameters of the focused energy beam (e.g., timing, energy intensity, beam width, etc.), etc. Additional parameters defined in the build plan 132 may include settings for offsets, layer thicknesses, gas flow parameters, etc. The control unit 108 (e.g., its processor 118) controls the operation of one or more beam emitters 106, feedstock applicators 117, and / or other components based on the build plan 132 to produce a built part 116 according to a proposed design at a selected location on the platform 102.

[0027] The processor 118 of the control unit 108 may be communicatively connected to the input device 134 and the display device 136. The input device 134 may include a touchpad, touchscreen, keyboard, mouse, physical buttons, joystick, etc. The input device 134 enables an operator to provide commands to the AM system 100. In a non-limiting example, the operator can use the input device 134 to select a design file 138, select potential locations for the construction parts 116 on the platform 102, initiate a build process, and / or select or adjust further settings and parameters of the AM equipment 101. The display device 136 includes a display screen configured to display a graphical user interface. Optionally, the input device and the display device 134, 136 may be incorporated together in an integrated device, such as a laptop computer, desktop computer, workstation, tablet computer, mobile, or handheld computing device (e.g., a smartphone). The processor 118 may be operably connected to the input device 134 and / or the display device 136 via a wired or wireless communication path.

[0028] In one embodiment, the processor 118 of the control unit 108 is configured to generate the build plan 132. For example, the processor 118 may access a part design file 138 stored in the memory 130. The design file 138 may be received from a remote computing device or may be generated locally via operator input on the input device 134. The processor 118 may receive user input selecting candidate locations for the built parts 116 on the platform 102. The processor 118 may generate the build plan 132 based on the configuration of the parts 116 and the selected locations of the parts 116. In another embodiment, the processor 118 does not generate the build plan 132, but rather implements control instructions that are generated remotely from the AM equipment 101. For example, machine instructions may be processed externally by a computer or processing unit and transferred to the AM equipment 101 to be executed by the AM equipment 101.

[0029] FIG. 2 shows a schematic diagram of an AM apparatus 101 according to one embodiment. FIG. 2 shows a first coupon 202, a second coupon 204, and a third coupon 206 being additively fabricated on the top surface 110 of the platform 102. The coupons 202, 204, and 206 are distinct and spaced apart from one another, but may represent different segments of a single build part, such as the part 116 shown in FIG. 1, that are later joined during the build process. In the illustrated embodiment, the coupons 202, 204, and 206 have the same size, shape, and orientation relative to the platform 102. Furthermore, the coupons 202, 204, and 206 are formed using the same material and the same parameters of the beam emitter 106. The coupons 202, 204, and 206 are enclosed within a powder bed 122. The only difference between the coupons 202, 204, 206 is the positioning of the coupons 202, 204, 206 relative to the AM device 101 (eg, the beam emitter 106 and the platform 102).

[0030] The positioning of the coupons 202, 204, 206 may refer to the location and orientation of the coupons 202, 204, 206 relative to the beam emitter 106. More specifically, the positioning may refer to the location and orientation of each of the different segments or layers of the coupons 202, 204, 206 relative to the beam emitter 106. The positioning may be characterized by the angle of incidence of the individual segments of the coupons 202, 204, 206 relative to the beam emitter 106, also referred to as the angle of incidence to the part surface normal at the lasing point.

[0031] The angle of incidence 208 is the angle between the beam line 210 and the line 212, and the line 212 represents the surface normal of the surface of each coupon segment at the intersection between the beam line 210 and the surface. The beam line 210 represents the path of a laser beam or other focused energy beam that is or will be emitted from the beam emitter 106 to the top end of each coupon segment or the surface layer 216 to generate the surface layer 216. The surface layer 216 is the most recently formed layer at a given time at the top (e.g., end) of the stack of layers. The surface normal is a vector extending perpendicularly from a plane tangent to the surface of the segment at the impact point of the energy beam. The surface normal extends outward from the impact point. If the surface at the impact point is horizontal, the plane tangent to the surface is vertical, and the surface normal extends from the impact point parallel to the horizontal plane. The skin 214 may represent the side or edge of one or more layers of each coupon directly below the surface layer 216 and adjacent to the beam line 210. If the skin 214 is curved (e.g., non-planar), the line 212 may be perpendicular to the tangent to the curved skin 214 at a point directly beneath the surface layer 216. The built part is three-dimensional, so the line 212 of different skin segments of the same or different parts may have different perpendicular, lateral, and / or longitudinal or depth components relative to the beam emitter 106. The incidence angles 208 described herein are based on the positioning (e.g., location and orientation) of a given segment of the built part relative to the emitter 106. For example, the surface normal 212 is affected by the orientation of the skin 214, and the beam line 210 is affected by the location of the segment (e.g., the skin 214) relative to the emitter 106.

[0032] 2 have the same size, shape, and orientation relative to the platform 102. The first, second, and third coupons 202, 204, 206 are overhanging objects in the illustrated embodiment. Each of the coupons 202, 204, 206 includes a respective down skin 218 that generally faces toward the platform 102 and an up skin 220 opposite the down skin 218. The up skin 220 generally faces upward, away from the platform 102. The down skin 218 and up skin 220 of each coupon 202, 204, 206 represent angled skins 214 such that the normal 212 is perpendicular to the area or portion of the down skin 218 and up skin 220 that is adjacent the surface layer 216.

[0033] The three coupons 202, 204, 206 have different positions relative to the beam emitter 106, as indicated by different angles of incidence 208. For example, the first coupon 202 defines a first angle of incidence 208A between a line 212A perpendicular to the respective down skin 218 and a first beam line 210A. The first coupon 202 defines a second angle of incidence 208B between a line 212B perpendicular to the respective up skin 220 and a second beam line 210B. The second coupon 204 defines a third angle of incidence 208C between a line 212C perpendicular to the respective down skin 218 and a third beam line 210C. The second coupon 204 defines a fourth angle of incidence 208D between a line 212D perpendicular to the respective up skin 220 and a fourth beam line 210D. The third coupon 206 defines a fifth angle of incidence 208E between a line 212E perpendicular to the respective down skin 218 and the fifth beamline 210E. The third coupon 206 defines a sixth angle of incidence 208F between a line 212F perpendicular to the respective up skin 220 and the sixth beamline 210F. In the illustrated embodiment, the first, third, and sixth angles of incidence 208A, 208C, 208F are obtuse (e.g., greater than 90 degrees). Skins 214 associated with obtuse angles of incidence are referred to herein as out-skins for reasons provided below. The second and fifth angles of incidence 208B, 208E are acute (e.g., less than 90 degrees). Skins 214 associated with acute angles of incidence are referred to herein as in-skins. The fourth angle of incidence 208D is a right angle (e.g., 90 degrees). The skin 214 associated with a normal incidence angle represents an inflection or transition zone between the outskin and the inskin.

[0034] The orientation of the skins 214 of the coupons 202, 204, 206 relative to the platform 102 represents another geometric feature that may optionally be used to determine one or more source locations of the focused energy beam during the build process. The orientation of each skin 214 relative to the platform 102 may refer to the tilt angle defined between the skin 214 (or a tangent extending from the curved skin 214) and the top surface 110 of the platform 102 on which the coupons 202, 204, 206 are built. In FIG. 2 , the down skins 218 of the first, second, and third coupons 202, 204, 206 all have the same orientation relative to the platform 102, and the up skins 220 of the coupons 202, 204, 206 also have the same orientation relative to the platform 102.

[0035] Experimental testing has demonstrated that the angle of incidence 208 between the beamline 210 and a line 212 perpendicular to the skin 214 can significantly affect the formation of a built part, such as surface quality, near-surface quality, porosity, and dimensional accuracy. For example, in an experimental setup similar to that shown in FIG. 2 , it was found that out-skins with an angle of incidence 208 greater than 90 degrees had significantly worse properties (e.g., surface and near-surface quality, porosity, and dimensional accuracy) than in-skins with an angle of incidence 208 less than 90 degrees, even when all test parameters were the same. The out-skins shown in FIG. 2 include the down-skin 218 of the first coupon 202, the down-skin 218 of the second coupon 204, and the up-skin 220 of the third coupon 206. The in-skins shown in FIG. 2 include the up-skin 220 of the first coupon 202 and the down-skin 218 of the third coupon 206. These results indicate that some down skin surfaces 218 may be in-skins (e.g., down skin 218 of third coupon 206) while other down skin surfaces 218 may be out-skins (e.g., down skin 218 of first and second coupons 202, 204) that have degraded properties compared to the in-skins. Similarly, some up skin surfaces 220 may be in-skins (e.g., up skin 220 of first coupon 202) while other up skin surfaces 220 may be out-skins (e.g., up skin 220 of third coupon 206).

[0036] A potential explanation for this phenomenon is different local absorption of the focused beam energy due to different incidence angles of the laser beam relative to the geometry of the proximal portion, as suggested in S. Kleszczynski, A. Ladewig, K. Friedberger, J. zur Jacobsmuhlen, D. Merhof, and G. Witt (2015) "Position Dependence of Surface Roughness of Parts from Laser Beam Melting Systems," 26th International Solid Freeform Manufacturing (SFF) Symposium, USA, pp. 360-370, which is incorporated herein by reference in its entirety. For example, when forming the surface layer 216 along or adjacent to the outskin surface (e.g., defining an incidence angle 208 greater than 90 degrees), some of the focused beam's energy may be absorbed by the underlying powder in the powder bed 122 that impacts the melt pool.

[0037] FIG. 3 shows an enlarged portion of the first coupon 202 shown in FIG. 2. A laser beam 226 impinges on the surface layer 216 of the coupon 202 adjacent to the down skin 218. As shown in FIG. 2, the angle of incidence 208A between the laser beam 226 and a line 212A perpendicular to the down skin 218 is greater than 90 degrees, so the down skin 218 is classified as an out skin. The high-energy laser beam 226 melts the raw material, causing a melt pool 228. The shape of the melt pool 228 may not precisely match the part dimensions, at least along the region adjacent to the out skin. For example, the melt pool 228 in FIG. 3 penetrates to a depth 231 that extends beyond the desired down skin edge 232 of the coupon 202, as the energy of the beam 226 erupts into the powder bed 122. The energy absorbed by the powder results in additional undesired material, referred to herein as melt extension 230, along the down skin surface 218 as the material cools and solidifies. The melt extensions 230 may increase surface roughness (e.g., reducing surface quality), increase porosity, and increase dimensional imprecision. Dimensional imprecision refers to an increase in the thickness or width of the down skin 218 compared to the thickness / width defined by the desired down skin edge 232. Note that one or more top layers, including the surface layer 216, may be dimensionally accurate, at least at this point in the build process. Laser penetration grows previously formed layers below the top layer. In FIG. 3 , for example, the melt pool 228 grows the melt extensions 230 along layer 234, which is two layers below the surface layer 216. The melt extensions 230 coalesce during the additive build process as additional layers of material are formed.

[0038] Continuing to refer to FIG. 2 , the angle of incidence 208B at the up skin 220 of the first coupon 202 is significantly different from the angle of incidence 208A at the down skin 218 of the first coupon 202. The angle of incidence 208B is acute, indicating that the up skin 220 of the first coupon 202 corresponds to an in-skin. In-skins are associated with improved quality characteristics compared to out-skins, such as surface quality, near-surface quality, porosity, and dimensional accuracy. The quality variations can be attributed to the geometry of the build part underlying the newly deposited surface layer 216. For example, energy from the laser beam 236 directed along beamline 210B shown in FIG. 2 may be absorbed by the partially solidified or compacted underlying material of the first coupon 202, resulting in less energy being directed beyond the up skin 220 boundary and into the powder bed 122 (compared to the down skin 218). The melt pool 238 formed by the laser beam 236 may not penetrate the up-skin 220 boundary due to the angle of the beam 236 relative to the geometry of the coupon 202. For example, the melt pool 238 extends at least partially inward toward the lateral center of the coupon 202. Essentially, more of the partially solidified underlying material of the coupon 202 is present to absorb the energy of the beam 236 than is present to absorb the energy of the beam 226. As a result, less heating of the powder bed 122 along the up-skin 220 occurs than heating of the powder bed 122 along the down-skin 218, thereby reducing melt spread and other non-uniformities along the up-skin surface 220, thereby improving surface and near-surface quality, dimensional accuracy, and porosity compared to the down-skin 218.

[0039] As shown in FIG. 2 , the angle of incidence 208D at the up skin 220 of the second coupon 204 is a right angle, indicating that the beamline 210D is collinear with the angle of the up skin 220 directly below the layer of material being or recently deposited. The up skin 220 of the second coupon 204 corresponds to the transition point or inflection zone between the in-skin and out-skin. For example, the inflection zone can represent a range of angles between the in-skin and out-skin. The systems disclosed herein can treat the skin at the inflection zone differently from the in-skin and out-skin. The inflection zone can be a range centered around the inflection point, such as, but not limited to, 90 degrees. For example, the inflection zone can be between 70 degrees and 110 degrees, between 80 degrees and 100 degrees, etc.

[0040] During an additive manufacturing process in which material layers are successively deposited in a layer-by-layer fashion according to a defined build part geometry, the angle of incidence of a given skin of the build part relative to the beam emitter can change over time. For example, FIGS. 4-6 illustrate three different stages in the construction of a single coupon 240 over time by an AM apparatus 101 according to one embodiment. The stages are in chronological order, such that the stage shown in FIG. 4 precedes the stages shown in FIGS. 5 and 6, and the stage shown in FIG. 5 precedes the stage shown in FIG. 6. FIGS. 4-6 illustrate the effect of a part being built on the platform 102 gradually lowering (e.g., moving away from the beam emitter 106) as additional material layers are deposited. The beam emitter 106 is positioned in the same position during each of the three illustrated stages of the build process so that the beam emitter 106 is not moved. The coupon 240 representing the build part in FIGS. 4-6 has a diamond-shaped shape with parallel, straight up-skin 242 and down-skin 244 surfaces.

[0041] The angle of incidence 246 based on the part geometry at the upskin 242 relative to the beam emitter 106 changes over time. As previously discussed, the relevant angle of incidence 246 is defined between the beam line 248 from the beam emitter 106 and a line 250 perpendicular to the portion of the upskin 242 proximate the current surface layer 252 of the coupon 240. In FIG. 4 , the angle of incidence 246 is obtuse (e.g., greater than 90 degrees), indicating that the upskin 242 has an outskin classification. Segments of the coupon 240 formed at or proximate the upskin 242 may have reduced quality and / or precision, requiring further finishing steps after construction to increase smoothness and / or provide proper dimensional alignment.

[0042] 5 shows that the platform 102 has moved and an additional portion 254 of the coupon 240 has been formed after the stage shown in FIG. 4. The additional portion 254 extends from the previous surface layer 252 to the current surface layer 256. At the stage shown, the angle of incidence 246 based on the up skin 242 is perpendicular, indicating that the up skin 242 is at a transition or inflection point between the out-skin and in-skin classifications. The segment of the coupon 240 formed on or adjacent to the up skin 242 at surface layer 256 is expected to have better quality and / or precision than the up skin 242 at the previous surface layer 252 due to the difference in angle of incidence 246.

[0043] FIG. 6 shows that the platform 102 has moved farther from the fixed beam emitter 106 than shown in FIG. 5 , and an additional portion 260 of the coupon 240 has been formed after the stage shown in FIG. 5 . The additional portion 260 extends from the previous surface layer 256 to the current surface layer 262. At the stage shown, the angle of incidence 246 based on the upskin 242 is acute (e.g., less than 90 degrees), indicating that the upskin 242 has an inskin classification. The segment of the coupon 240 formed on or adjacent to the upskin 242 at the surface layer 262 is expected to have better quality and / or precision than the upskin 242 at the previous surface layers 256, 252 due to the difference in the angle of incidence 246. FIGS. 4-6 show that the upskin 242 can transition from corresponding to an outskin to corresponding to an inskin and vice versa as the diamond-shaped coupon 240 grows taller and the positioning of the surface layer changes relative to the beam emitter 106. Therefore, multiple layers of the geometry and form of the building part are evaluated to determine the effect of the angle of incidence on the building part. Optionally, all layers of the geometry of the building part along the skin surface are evaluated to classify it as either out-skin, in-skin, or an inflection point.

[0044] 7 shows a schematic diagram of an additive manufacturing (AM) machine 101 according to a second embodiment of the present disclosure. The AM machine 101 is in the process of additively manufacturing a built part 302 on a platform 102. The built part 302 has an asymmetric shape in the illustrated embodiment. The built part 302 is formed in accordance with systems and methods described herein that take into account the geometry of the built part relative to a beam source to determine multiple relative positions of the built part 302 with respect to one or more beam emitters during the build process.

[0045] In the illustrated embodiment, the AM device 101 includes a first beam emitter 106A and a second beam emitter 106B. The beam emitters 106A and 106B are spaced apart from each other. The first beam emitter 106A is disposed at the first source location 314, and the second beam emitter 106B is disposed at the second source location 316. For example, the beam emitters 106A and 106B are disposed proximate to the first and second walls 112A and 112B, respectively, of the housing 104. The beam emitters 106A and 106B may also be disposed on or near both sides or at corners of the three-dimensional AM device 101. For example, the first beam emitter 106A may be disposed at or proximate one corner of the housing 104, and the second beam emitter 106B may be disposed at or proximate the opposite corner of the housing 104. In one embodiment, the coverage areas of the beam emitters 106A, 106B overlap. The coverage area of ​​a beam emitter refers to the region over which the beam emitter's respective scanning head can direct a focused energy beam. The coverage area is based on the positioning of the beam emitter and the function of the scanning head and other beam control elements. Optionally, the coverage area of ​​the first beam emitter 106A may substantially overlap the coverage area of ​​the second beam emitter 106B, such that the overlap represents at least a majority of the respective coverage areas. In the illustrated embodiment, the first and second beam emitters 106A, 106B are non-translatable relative to the platform 102 such that the beam emitters 106A, 106B are fixedly mounted in position at their respective source locations 314, 316. Alternatively, at least one of the beam emitters 106A, 106B is controllably translatable relative to the platform 102. Optionally, the platform 102 may be translatable. For example, the platform 102 may be controlled to move away from the beam emitters 106A, 106B, similar to the mobile platform 102 depicted in Figures 4-6.

[0046] In one or more embodiments, the processor 118 of the control unit 108 (shown in FIG. 1 ) is configured to analyze the geometry (e.g., geometric form) of the building part 302 and selected positions of the building part 302 on the platform 102 to determine geometric characteristics of various segments of the building part 302. The geometry and / or positions may be provided in a design file 138 accessed by the processor 118. Optionally, the positions may be selected by an operator using the user input device 134. Although FIG. 7 shows the building part 302 at least partially formed on the platform 102, the analysis process described herein may be performed by the processor 118 before commencing the additive manufacturing build process.

[0047] The processor 118 is configured to determine one or more geometric characteristics of each of a plurality of segments or portions of the built part 302 based on the geometry and selected position of the built part 302 relative to the AM apparatus 101 to determine which source locations 314, 316 should be used to form the given segment during the build process. The purpose of the analysis is to select beam source locations that are expected to result in improved (or at least satisfactory) quality and accuracy of the resulting segments of the built part. The one or more geometric characteristics include the angle of incidence between the beam source location emitting the focused energy beam and a line perpendicular to the skin directly below (within a given number of layers from) the surface layer of the segment. The systems described herein are configured to select beam source locations based on the angle of incidence, which is expected to result in improved quality and accuracy compared to using only a single beam source location or using multiple beam source locations without considering the angle of incidence.

[0048] The building part may be divided into different constituent segments by one or more processors 118 based on the geometry of the building part 302. In the illustrated embodiment, the building part 302 is divided into a plurality of outline segments 304, 306, 308, 310 and a fill segment 312, which are segmented by dashed lines in FIG. 7 . The first segment 304 comprises a vertically oriented skin. The second segment 306 is formed above the first segment 304 and comprises an up skin. The third segment 308 defines a down skin directly opposite the second segment 306. The fourth segment 310 defines an up skin below the third segment 308, such that the third segment 308 is formed above the fourth segment 310. The fill segment 312 is disposed laterally between the first and fourth segments 304, 310 and between the second and third segments 306, 308. The filler segment 312 may be filled with a bulk material having different properties than the material deposited to form the contour segments 304, 306, 308, 310. Optionally, the mechanical structure of the filler segment 312, such as a lattice structure, may be different from the mechanical structure of the contour segments 304, 306, 308, 310, regardless of whether the material properties of the fill and contour segments are the same. Note that the contour segments 304, 306, 308, 310 define different outer surfaces of the building part 302. While the outer surfaces are straight in Figure 7, the building part 302 may have a curved skin / surface.

[0049] In one embodiment, the processor 118 may analyze the angle of incidence defined between each segment of the build part and each potential beam source location to select which beam source location to utilize to emit a focused energy beam toward the segment to form one or more layers on the segment. For example, the processor 118 may calculate the angle of incidence between the first beam source location 314 and the first segment 304 and the angle of incidence between the second beam source location 316 and the first segment 304. The processor 118 may select which beam source location 314, 316 to use to form the first segment 304 based at least in part on the comparison of the angles of incidence. In one embodiment, because it has been determined that the in-skin provides desirable surface and near-surface quality, porosity, and dimensional accuracy, the processor 118 may select beam source locations associated with angles of incidence less than 90 degrees to use during the build process. In one embodiment, if the angles of incidence from the first and second source locations 314, 316 are both less than 90 degrees, thereby classifying both skin surfaces as in-skin, the processor 118 may select the beam source location with the smallest angle of incidence. A smaller angle of incidence may direct less energy away from the surface layer and into the surrounding powder bed, thereby improving surface quality compared to emitting laser beams from other beam source locations.

[0050] The processor 118 may be configured to consider secondary factors other than the incidence angle to determine the beam source locations to utilize to form the corresponding segment (e.g., rather than selecting source locations based solely on the incidence angle). Secondary factors may include the respective efficiencies of the different beam emitters 106A, 106B, the respective workloads and / or capabilities of the beam emitters 106A, 106B, the presence of any intervening gas clouds or other potential interference, and / or the like. The secondary factors may be used, for example, as a tiebreaker when selecting between multiple source locations having similar incidence angles. For example, if the incidence angle associated with a first beam emitter 106A is 60 degrees and the incidence angle associated with a second beam emitter 106B is 45 degrees, the first beam emitter 106A may be selected to form a given segment even though its incidence angle is greater than that of the second beam emitter 106B, if the secondary factors favor the first beam emitter 106A.

[0051] In the illustrated embodiment, as a result of the analysis, the processor 118 may select a first beam emitter 106A at a first source location 314 to form a first segment 304 of the building part 302. For example, the angle of incidence 318 from the first source location 314 is acute, such that a vertically oriented skin of the first segment corresponds to an in-skin. Although not shown, the angle of incidence from the second source location 316 is obtuse, indicating that a skin of the first segment corresponds to an out-skin. Thus, the first beam emitter 106A is selected to emit a focused energy beam toward the first segment 304, which is expected to improve surface and near-surface quality, porosity, dimensional accuracy, and / or the like, compared to forming the first segment 304 by emitting an energy beam from the second beam emitter 106B. Based on the angle of incidence analysis, the processor 118 may select the first beam emitter 106A to form the second segment 306 of the building part 302 and the second beam emitter 106B at the second source location 316 to form both the third and fourth segments 308, 310 of the building part 302. Optionally, the beam source location used to form the fill segment 312 may be based on considerations other than the angle of incidence, such as the secondary factors discussed above. In an embodiment, either or both of the beam emitters 106A, 106B may be used to form the fill segment 312 based on the availability of the emitters 106A, 106B at different stages of the build process and other factors.

[0052] Although only one normal is shown extending from each of the contour segments 304, 306, 308, 310 in Figure 7, it is understood that even along straight line segments the angle of incidence can vary from layer to layer, as shown in Figures 4-6. In one embodiment, the processor 118 may evaluate the geometry of the building part 302 layer by layer in determining how to divide the building part 302 into different segments and how to assign the segments to different beam source locations (e.g., locations 314, 316).

[0053] After determining which beam source locations 314, 316 should be utilized to form each of the various segments 304, 306, 308, 310, 312 of the built part 302, the processor 118 may control the AM equipment 101 to additively manufacture the built part 302. For example, the processor 118 may generate or at least update a build plan 132 to incorporate the associated beam source locations and part segments. The build plan 132 defines the operations to be performed by the AM equipment 101 to form the built part 302. The build plan 132 may provide a first set of scan paths for the first beam emitter 106A and a second set of scan paths for the second beam emitter 106B. The first set of scan paths outlines a path for the scan head of the first emitter 106A to direct a focused energy beam (e.g., beam 320) toward the segment 306. A second set of scan paths outlines a path for the scan head of the second emitter 106B to direct a focused energy beam (e.g., beam 322) toward segment 308. The processor 118 may control the components of the AM equipment 101 according to the build plan 132 to produce the built part 302. The processor 118 may generate control signals that are communicated to different components (e.g., beam emitters 106A, 106B, applicator device 117, etc.) to control the AM equipment 101.

[0054] 7, the AM apparatus 101 may optionally include three or more emitters positioned at different defined locations on the AM apparatus 101. For example, the apparatus 101 may have three emitters 106 positioned at the same height from the platform 102 to form an equilateral triangle. In another example, the apparatus 101 may have four emitters 106 positioned at each of the four corners or along each of the four sides of the housing 104. The above-described analysis may be performed to determine which of the three or more emitters 106 is best positioned to emit beams to form each of the various segments of the built part.

[0055] FIG. 8 shows a schematic diagram of the additive manufacturing (AM) apparatus 101 according to the first embodiment of the present disclosure shown in FIG. 1 . In FIG. 8 , the AM apparatus 101 includes a beam emitter 106 that is translatable relative to other components of the AM apparatus 101, such as the platform 102. The beam emitter 106 is mounted on a rail or gantry 144 and moved by an actuator 140, as shown in FIG. 1 . The actuator 140 may be a motorized device controlled by the processor 118 of the control unit 108 (shown in FIG. 1 ). The actuator 140 may rotate or slide the beam emitter 106 along a track defined by the rail or gantry 144. The actuator 140 can selectively position the beam emitter 106 at a first source location 314 and a second source location 316.

[0056] In the illustrated embodiment, the beam emitter 106 can be used to form multiple different segments of the building part 302 shown in FIG. 7 . For example, the processor 118 can control the actuator 140 to position the beam emitter 106 at the first source location 314 and emit a focused energy beam 320 toward the surface layer 216 of the second segment 306 to form the segment 306. The processor 118 can then control the actuator 140 to move the beam emitter 106 along the rail or gantry 144 to the second source location 316 and emit the focused energy beam toward the third segment 308. The actuator 140 can be controlled to move the beam emitter 106 back and forth between the two source locations 314, 316 during the course of the build process. Optionally, the beam emitter 106 can be the only beam emitter 106 of the AM apparatus 101. In one embodiment, the track along the rail or gantry 144 may be linear so that the beam emitter 106 moves in a straight line. Alternatively, the track may be curved and / or rotatable.

[0057] While only two source locations 314, 316 are optionally described, the actuator 140 may be configured to move the beam emitter 106 to at least three distinct locations along the length of the track. For example, the actuator 140 may include a stepper motor or gear assembly that allows the actuator 140 to stop at various set locations along the rail or gantry 144. In a non-limiting example, the actuator 140 may be capable of selectively positioning the beam emitter 106 with a spatial frequency high enough to allow the emitter 106 to be positioned nearly anywhere along the length of the track. According to one or more embodiments, the processor 118 may be configured to determine or select the beam source locations to which the beam emitter 106 is to be moved during the build process. The processor 118 may select the beam source locations based on one or more geometric characteristics, such as the angle of incidence. In a non-limiting example, the processor 118 may determine the angles of incidence of various geometric segments of the building part 302 for each of three or more different possible (e.g., available) source locations. The processor 118 may select which possible source locations to use to form each of the geometric segments based at least in part on the comparison of the angles of incidence. For example, the two source locations 314, 316 shown in Figure 8 may be locations selected by the processor 118 from among three or more possible source locations.

[0058] FIG. 9 shows a schematic diagram of an additive manufacturing (AM) apparatus 101 according to a third embodiment of the present disclosure. In FIG. 9, the AM apparatus 101 includes first and second beam emitters 106A, 106B, similar to the embodiment shown in FIG. 7. Unlike FIG. 7, the first beam emitter 106A is at the center of the build platform 102. The first beam emitter 106A may be fixed in position relative to the other components of the AM apparatus 101 such that the first beam emitter 106A is non-translatable. The second beam emitter 106B is translatable relative to the platform 102, the first beam emitter 106A, and the other components of the AM apparatus 101. The second beam emitter 106B is attached to a curved rail 502 and is movable along the length of the curved rail 502. The curved rail 502 may define a closed shape, such as a circle, an oval, an ellipse, a rectangle with curved corners, or the like. 9, the rail 502 may be annular or ring shaped. The curved rail 502 may surround the first beam emitter 106A.

[0059] In one embodiment, the second beam emitter 106B is movable by an actuator to various locations along the length of the rail 502 and emits a focused energy beam from any of these various locations toward a building part on the platform 102. For example, the processor 118 may control the second beam emitter 106B to move along the rail 502 between the first source location 504 and the second source location 506 during the build process to change the source of the energy beam impinging on the building part. Simultaneously or sequentially, the processor 118 may control the first beam emitter 106A at a predetermined center location 508 (corresponding to a third source location) to emit a focused energy beam toward the building part. The first beam emitter 106A may emit a beam toward a segment of the building part that is different from the segment targeted by the second beam emitter 106B.

[0060] FIG. 10 shows a schematic diagram of an additive manufacturing (AM) apparatus 101 according to a fourth embodiment of the present disclosure. The embodiment shown in FIG. 10 is similar to the embodiment shown in FIGS. 1 and 8, except that the AM apparatus 101 includes two beam emitters 106A, 106B on two separate rails or gantries 144A, 144B. The rails 144A, 144B are disposed along opposite sides of the housing 104 above the platform 102. The first beam emitter 106A is selectively positionable at two or more locations along the length of the first linear rail or gantry 144A, and the second beam emitter 106B is selectively positionable at two or more locations along the length of the second linear rail or gantry 144B. Separate actuators (not shown) may be controlled by the processor 118 to move the beam emitters 106A, 106B to different locations.

[0061] In another embodiment, at least one of rails 144A, 144B is movable relative to platform 102. For example, rail 144A may be movable along another track extending from the position of rail 144A shown in FIG. 10 toward the position of rail 144B in FIG. 10. The other track may extend perpendicular to the length of track 144B. In yet another embodiment, AM apparatus 101 includes only a single rail 144A and beam emitter 106A (e.g., lacking rail 144B and beam emitter 106B), and rail 144A is movable as described above to allow beam emitter 106A to be positioned at the location of beam emitter 106B shown in FIG.

[0062] 11 and 12 show further embodiments of an AM apparatus 101 in which optical components are used to redirect a focused energy beam toward the build part. In both FIGS. 11 and 12, a single beam source 800 is used to generate the focused energy beam. In FIG. 11, the beam source 800 is operably coupled to a selector device 802, which may include or represent a transparent prism, a block with one or more reflective surfaces, or the like. The selector device 802 may be rotatable to change the orientation of the selector device 802 relative to the beam source 800. The AM apparatus 101 of FIG. 11 also includes two scan heads 804, 806. The scan heads 804, 806 are spaced apart from one another and mounted above the platform 102. The scan heads 804, 806 are configured to redirect a focused energy beam 808 toward the platform 102. Each of the scan heads 804, 806 may include one or more reflective surfaces, such as mirrors.

[0063] In operation, the beam source 800 emits an energy beam 808 toward the selector device 802. The selector device 802 redirects the beam 808 to either a first scan head 804 or a second scan head 806. For example, the selector device 802 may direct the beam 808 to a first scan head 804 such that the first scan head 804 redirects the beam 808 to an upskin segment 810 of a building part 812. The selector device 802 may direct a subsequent beam 814 to a second scan head 806 such that the second scan head 806 redirects the beam 814 to a downskin segment 816 of the building part 812. By redirecting the beam, the angles of incidence 819, 820 associated with the beams 808, 814 are acute, indicating that both the upskin and downskin surfaces of the building part 812 are classified as in-skin.

[0064] 12 , the beam source 800 is directly coupled to the scan head 822. The AM apparatus 101 also includes a reflector 826 spaced apart from the beam source 800 and the scan head 822. For example, the reflector 826 may be located along a side, edge, or corner of the build envelope or housing opposite the scan head 822. The reflector 826 is oriented to reflect the beam toward the platform 102. The scan head 822 can selectively direct a first energy beam 824 directly onto the down skin segment 816 of the building part 812. The scan head 822 can selectively direct a second energy beam 828 onto the reflector 826, which redirects the beam 828 onto the up skin segment 810 of the building part 812. As with the embodiment shown in FIG. 11 , both the up skin surface and the down skin surface of the building part 812 are classified as in-skin in FIG. 12 .

[0065] 13 is a flowchart of a method 700 for additively manufacturing a built part during a build process by directing a focused energy beam from a plurality of different beam orientations relative to the built part to improve properties of the built part, such as surface and near-surface quality, porosity, and dimensional accuracy. Method 700 may be performed, in whole or at least in part, by one or more processors 118 of the control unit 108 of the AM system 100 shown in FIG. 1. Optionally, some operator input may be provided at one or more steps. Optionally, method 700 may include more steps than shown in FIG. 13, fewer steps than shown in FIG. 13, different steps not shown in FIG. 13, and / or a different arrangement or order of steps than shown in FIG. 13.

[0066] Method 700 begins at 702, where one or more geometric characteristics of each of a plurality of segments of a built part are determined at a candidate position of the built part relative to an additive manufacturing equipment prior to additively manufacturing the built part. The one or more geometric characteristics include an angle of incidence between a beam line extending from an electromagnetic energy source of the additive manufacturing equipment and a surface normal of each skin of the corresponding segment proximate the beam line.

[0067] At 704, the additive manufacturing equipment is controlled to direct a focused energy beam from a first direction toward the build part to form a first one of the segments of the build part. Directing the focused energy beam from the first direction is based on one or more geometric characteristics of the first segment. For example, directing the focused energy beam from the first direction may be in response to determining that an angle of incidence defined by a beam line extending from the first direction toward the first segment is acute. Further, directing the focused energy beam from the first direction toward the first segment may be in response to determining that an angle of incidence defined by a beam line extending from the first direction toward the first segment is smaller than an angle of incidence defined by a beam line extending from the second direction toward the first segment.

[0068] At 706, the additive manufacturing equipment is controlled to direct a focused energy beam from a second direction toward the build part to form a second one of the segments of the build part. Directing the focused energy beam from the second direction is based on one or more geometric characteristics of the second segment. For example, directing the focused energy beam from the second direction may be in response to determining that an angle of incidence defined by a beam line extending from the second direction toward the second segment is acute. Further, directing the focused energy beam from the second direction toward the second segment may be in response to determining that an angle of incidence defined by a beam line extending from the second direction toward the second segment is smaller than an angle of incidence defined by a beam line extending from the first direction toward the second segment.

[0069] The AM apparatus includes one or more beam emitters and one or more actuators controlled to move the one or more beam emitters between different source locations. In one embodiment, one of the actuators moves one beam emitter to a first source location, and the beam emitter at the first source location emits a focused energy beam to form a first segment of the built part. The actuator is controlled to move the (same) beam emitter to a second source location for the beam emitter to emit a focused energy beam to form a second segment of the built part. Alternatively, a first beam emitter of the plurality of beam emitters is located at the first source location and controlled to emit a focused energy beam toward the first segment of the built part to form the first segment. A second beam emitter of the plurality of beam emitters is located at a second source location and controlled to emit a focused energy beam toward the second segment of the built part to form the second segment. The first and second source locations are determined based on one or more geometric characteristics of the first and second segments, respectively.

[0070] Although various spatial and directional terms, such as top, bottom, underside, center, side, horizontal, vertical, front, etc., are used to describe embodiments of the present disclosure, it is understood that such terms are used merely with reference to the orientation shown in the drawings. The orientation can be flipped, rotated, or otherwise changed so that top is bottom and vice versa, horizontal becomes vertical, etc.

[0071] The diagrams of the embodiments herein depict one or more control or processing units, such as the control unit 108 shown in FIG. 1 . It should be understood that the control unit or processing unit corresponds to a circuit, circuit configuration, or portion thereof, implemented as hardware with associated instructions (e.g., software stored on a tangible, non-transitory, computer-readable storage medium, such as a computer hard drive, ROM, RAM, etc.) that perform the operations described herein. The hardware may include hardwired state machine circuitry for performing the functions described herein. The hardware may include electronic circuitry including and / or coupled to one or more logic-based devices, such as, for example, a microprocessor, processor, controller, etc. Optionally, the control unit 108 or its one or more processors 118 correspond to processing circuitry such as one or more of a field programmable gate array (FPGA), an application-specific integrated circuit (ASIC), a microprocessor, a quantum computing device, and / or the like. The circuitry in various embodiments is configured to execute one or more algorithms to perform the functions described herein. The one or more algorithms, whether expressly identified in a flowchart or method, comprise aspects of the embodiments disclosed herein.

[0072] As used herein, terms such as "control unit" include any processor- or microprocessor-based system, including systems using microcontrollers, reduced instruction set computers (RISC), application specific integrated circuits (ASIC), logic circuits, and any other circuits or processors, including hardware, software, or a combination thereof, capable of performing the functions described herein. Such are merely examples and are therefore not intended to limit in any way the definition and / or meaning of such terms. The control unit 108 shown in FIG. 1 is configured to execute a set of instructions stored in one or more storage elements (such as one or more memories) to process data. The set of instructions includes various commands that instruct the control unit 108 as a processing machine (e.g., its processor 118) to perform specific operations, such as the methods and processes of various embodiments of the subject matter described herein. In one embodiment, the set of instructions is in the form of a software program. The processing of input data by the processing machine may be in response to user commands, results of previous processing, or requests made by other processing machines. As used herein, the term "software" includes any computer program stored in memory for execution by a computer, including but not limited to RAM memory, ROM memory, EPROM memory, EEPROM memory, and non-volatile RAM (NVRAM) memory.

[0073] As used herein, a structure, constraint, or element that is "configured" to perform an operation or action is specifically structurally shaped, constructed, or adapted in a manner corresponding to the operation or action. For clarity and to avoid doubt, an object that can only be modified to perform an operation or action is not "configured" to perform an operation or action as used herein.

[0074] It should be understood that the foregoing description is illustrative and not limiting. For example, the above-described embodiments (and / or aspects thereof) may be used in combination with each other. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the various embodiments of the present disclosure without departing from their scope. While the dimensions and types of materials described herein are intended to define the parameters of various embodiments of the present disclosure, the embodiments are by no means limiting and are exemplary of embodiments. Many other embodiments will be apparent to those skilled in the art upon review of the foregoing description. The scope of the various embodiments of the present disclosure should therefore be determined with reference to the appended claims, along with the full range of equivalents to which such claims are entitled. In the appended claims, the terms "including" and "in which" are used as the plain-English equivalents of the respective terms "comprising" and "wherein." Additionally, the terms "first," "second," and "third," etc. are used merely as labels and are not intended to impose numerical requirements on their objects. Moreover, the following claim limitations are not written in means-plus-function form and are not intended to be construed under paragraph (f) of 35 U.S.C. § 112, except where such claim limitations expressly use the phrase "means for" followed by a statement of function devoid of further structure.

[0075] This written description uses examples to disclose various embodiments of the present disclosure, including the best mode, and also enables any person skilled in the art to practice various embodiments of the present disclosure, including making and using any devices or systems and performing any incorporated methods. The patentable scope of various embodiments of the present disclosure is defined by the claims, and may include other examples that occur to those skilled in the art. Such other examples are intended to be within the scope of the claims if they have structural elements that do not differ from the literal words of the claims, or if they include equivalent structural elements that do not differ substantially from the literal words of the claims. [Explanation of symbols]

[0076] 100 Additive Manufacturing (AM) Systems 101 Additive Manufacturing (AM) Equipment 102 Building Platform 104 Case 106 Beam Emitter 106A First beam emitter 106B Second beam emitter 108 Control Unit 111 Raw Materials 112A, 112B walls 114, 216, 252, 256, 262 surface layer 116, 812 Construction parts 117 Raw Material Applicator 118 processors 120 External support 122 Powder bed 124 Building Direction 126 Construction Axis 130 memory 132 Construction Plan 134 Input Device 136 Display device 138 Part Design Files 140 Actuator 142, 804, 806, 822 Scanning Head 144, 144A, 144B Rail or Gantry 202 First Coupon 204 Second Coupon 206 Third Coupon 208, 246, 819, 820 angle of incidence 208A First Incident Angle 208B Second Incident Angle 208C Third Angle of Incidence 208D Fourth Angle of Incidence 208E Fifth Incident Angle 208F 6th angle of incidence Beamlines 210 and 248 210A First Beamline 210B Second Beamline 210C Third Beamline 210D 4th Beamline 210E 5th Beamline 210F 6th Beamline 212 Surface Normal 212A, 212B, 212C, 212D, 212E, 212F, 250 Line 214 Skin 218, 244 Down skin 220, 242 Upskin 226, 236, 320, 814 beams 228, 238 Melt pool 230 Melting extension section 232 Down skin edge 234 layers 240 coupons 302 Construction Parts 304 First Segment 306 Second Segment 308 Third Segment 310 Fourth Segment 312 Filling Segment 314, 504 First Source Location 316, 506 Secondary Source Locations 502 Rail 508 Central Location 700 methods 800 Beam Source 802 Selector Device 808 Focused Energy Beam 810 Upskin Segment 816 Down Skin Segments 824 First Energy Beam 826 Reflector 828 Second Energy Beam

Claims

1. one or more processors (118) configured to determine one or more geometric characteristics of each of a plurality of segments (304, 306, 308, 310, 312) of a built part (302) at candidate positions relative to an additive manufacturing device (101), the one or more geometric characteristics including an angle of incidence (208, 318) between a beam line (210) extending from a source (106) of a focused energy beam toward a surface layer (216) of the built part (302) and a surface normal (212, 250) of each skin (214) of the corresponding segment proximate to the beam line, the built part (302) being built layer by layer, the surface layer (216) being the most recently formed layer at the top of a stack of layers, and the each skin (214) being a side of a layer proximate to the beam line (210) directly below the surface layer (216); the one or more processors are configured to control the additive manufacturing device based on the one or more geometric characteristics to direct a focused energy beam (320) relative to the built part from a first direction to form a first one of the segments of the built part (306) and to direct a focused energy beam (322) relative to the built part from a second direction to form a second one of the segments of the built part (308). An additive manufacturing system (100).

2. 2. The additive manufacturing system (100) of claim 1, wherein the one or more processors (118) are configured to generate a build plan (132) based on the one or more geometric features, the build plan defining operations to be performed by the additive manufacturing equipment (101) to form the built part (302).

3. 3. The additive manufacturing system of claim 1, wherein the one or more processors control the additive manufacturing equipment to direct the focused energy beam from the first direction to form the first segment in response to determining that an angle of incidence defined by the beam line extending from the first direction toward the first segment of the built part is less than an angle of incidence defined by the beam line extending from the second direction toward the first segment of the built part.

4. 4. The additive manufacturing system (100) of claim 1, wherein the one or more processors (118) control the additive manufacturing equipment (101) to direct the focused energy beam (320) from the first direction to form the first segment (306) of the built part (302) in response to determining that an angle of incidence (208, 318) defined by the beam line (210) extending from the first direction towards the first segment of the built part (302) is acute.

5. 5. The additive manufacturing system of claim 1, wherein the one or more processors control the additive manufacturing equipment to direct the focused energy beam from the second direction to form the second segment of the built part in response to determining that an angle of incidence defined by the beam line extending from the second direction toward the second segment of the built part is acute.

6. 6. The additive manufacturing system of claim 1, wherein the one or more processors are configured to control the additive manufacturing equipment to direct the focused energy beam from a first source location to the first segment of the built part and to direct the focused energy beam from a second source location to the second segment of the built part, the first and second source locations being spaced apart from one another relative to the additive manufacturing equipment.

7. 7. The additive manufacturing system (100) of claim 6, wherein the first and second source locations (314, 316) are located at opposite corners or opposite sides of the additive manufacturing equipment (101).

8. the one or more processors (118) are configured to control the additive manufacturing device (101) to form the first segment (306) of the built part (302) by controlling a first beam emitter (106A) to emit the focused energy beam (320) from the first direction towards the first segment; the one or more processors are configured to control the additive manufacturing device (101) to form the second segment (308) of the built part by controlling a second beam emitter (106B) to emit the focused energy beam (322) from the second direction towards the second segment; The additive manufacturing system (100) of any one of claims 1 to 7.

9. 9. The additive manufacturing system (100) of claim 8, wherein a coverage area of ​​the first beam emitter (106A) along the additive manufacturing device (101) overlaps with a coverage area of ​​the second beam emitter (106B).

10. the additive manufacturing device (101) includes a beam emitter (106) and an actuator (140), the actuator being configured to move the beam emitter relative to the built part (302) between a first source location (314) and a second source location (316); 10. The additive manufacturing system (100) of any one of claims 1 to 9, wherein the one or more processors (118) are configured to control the actuator to position the beam emitter at the first source location to emit the focused energy beam (320) to form the first segment (306) of the built part, and to position the beam emitter at the second source location to emit the focused energy beam (322) to form the second segment (308) of the built part.

11. 11. The additive manufacturing system (100) of claim 10, wherein the beam emitter (106) is movable along a track (144), the track being movable relative to a platform (102) of the additive manufacturing equipment (101).

12. 11. The additive manufacturing system (100) of claim 10, wherein the beam emitter (106) is movable along a track (144), the track being linear.

13. 11. The additive manufacturing system (100) of claim 10, wherein the beam emitter (106) is movable along a track (144), the track being curved.

14. 11. The additive manufacturing system (100) of claim 10, wherein the beam emitter (106) is a first beam emitter (106A), the additive manufacturing equipment (101) further comprises a second beam emitter (106B), and the one or more processors (118) are configured to control the second beam emitter to emit a focused energy beam from a third source location (508) spaced apart from the first and second source locations (314, 316) to form a third segment (310) of the built part (302).

15. determining one or more geometric characteristics of each of a plurality of segments (304, 306, 308, 310, 312) of a built part (302) at candidate locations relative to an additive manufacturing device (101) before additively manufacturing the built part, the one or more geometric characteristics including an angle of incidence (208, 318) between a beam line (210) extending from a source (106) of a focused energy beam toward a surface layer (216) of the built part (302) and a surface normal (212, 250) of each skin (214) of the corresponding segment proximate to the beam line, the built part (302) being built layer by layer, the surface layer (216) being the most recently formed layer at the top of a stack of layers, and the each skin (214) being a side of a layer proximate to the beam line (210) directly below the surface layer (216); controlling the additive manufacturing device based on the one or more geometric characteristics to direct a focused energy beam (320) relative to the built part from a first direction to form a first one of the segments (306) of the built part; controlling the additive manufacturing device based on the one or more geometric characteristics to direct a focused energy beam (322) relative to the built part from a second direction to form a second one of the segments (308) of the built part; A method (700) comprising:

16. 16. The method (700) of claim 15, wherein the step of controlling the additive manufacturing equipment (101) to direct the focused energy beam (320) from the first direction is responsive to determining that an angle of incidence (208, 318) defined by the beam line (210) extending from the first direction toward the first segment (306) is acute.

17. 17. The method (700) of claim 15 or 16, wherein the step of controlling the additive manufacturing equipment (101) to direct the focused energy beam (322) from the second direction relative to the built part (302) is responsive to determining that an angle of incidence (208, 318) defined by the beam line (210) extending from the second direction towards the second segment (308) is acute.

18. 18. A method (700) according to any one of claims 15 to 17, wherein the step of controlling the additive manufacturing equipment (101) to direct the focused energy beam (320) from the first direction is responsive to determining that an angle of incidence (208, 318) defined by the beam line (210) extending from the first direction towards the first segment (306) is smaller than an angle of incidence defined by a beam line extending from the second direction towards the first segment.

19. 19. The method (700) of any one of claims 15 to 18, wherein the additive manufacturing equipment (101) comprises a beam emitter (106) and an actuator (140), the method further comprising controlling the actuator to move the beam emitter between a first source location (314) and a second source location (316), such that the beam emitter at a first source location emits the focused energy beam (320) to form the first segment (306) of the built part (302) and the beam emitter at a second source location emits the focused energy beam (322) to form the second segment (308).

20. 20. The method (700) of any one of claims 15 to 19, wherein the step of controlling the additive manufacturing equipment (101) to direct the focused energy beam (320) from the first direction comprises controlling a first beam emitter (106A) arranged at a first source location (314) to emit the focused energy beam toward the first segment (306), and the step of controlling the additive manufacturing equipment (101) to direct the focused energy beam (322) from the second direction comprises controlling a second beam emitter (106B) arranged at a second source location (316) to emit the focused energy beam toward the second segment (308).

21. an additive manufacturing device (101) including a platform (102) and one or more beam emitters (106), the one or more beam emitters emitting focused energy beams (320, 322) from a plurality of different source locations (314, 316) relative to the platform; one or more processors (118) configured to determine one or more geometric characteristics of each of a plurality of segments (304, 306, 308, 310, 312) of a built part (302) at candidate locations relative to the additive manufacturing equipment, the one or more geometric characteristics including an angle of incidence (208, 318) between a beam line (210) extending from a corresponding location at the source location toward a surface layer (216) of the built part (302) and a surface normal (212, 250) of each skin (214) of the corresponding segment proximate the beam line, the built part (302) being built layer by layer, the surface layer (216) being the most recently formed layer at the top of a stack of layers, and the each skin (214) being a side of a layer proximate the beam line (210) directly below the surface layer (216); and Equipped with the one or more processors are configured to control the one or more beam emitters based on the one or more geometric characteristics to direct the focused energy beam from a first source location (314) relative to the platform to form a first one of the segments of the building part, and to direct the focused energy beam from a second source location (316) relative to the platform to form a second one of the segments of the building part. An additive manufacturing system (100).

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