WO2018141476A1 - Séparation automatisée de structures support d'une pièce fabriquée de manière additive sur la base d'un lit de poudre - Google Patents

Séparation automatisée de structures support d'une pièce fabriquée de manière additive sur la base d'un lit de poudre Download PDF

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Publication number
WO2018141476A1
WO2018141476A1 PCT/EP2018/000039 EP2018000039W WO2018141476A1 WO 2018141476 A1 WO2018141476 A1 WO 2018141476A1 EP 2018000039 W EP2018000039 W EP 2018000039W WO 2018141476 A1 WO2018141476 A1 WO 2018141476A1
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WO
WIPO (PCT)
Prior art keywords
component
support structure
cavity
platform
support
Prior art date
Application number
PCT/EP2018/000039
Other languages
German (de)
English (en)
Inventor
Vasily Ploshikhin
Original Assignee
Amsis Gmbh
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Amsis Gmbh filed Critical Amsis Gmbh
Publication of WO2018141476A1 publication Critical patent/WO2018141476A1/fr

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/20—Direct sintering or melting
    • B22F10/28—Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM]
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/40—Structures for supporting workpieces or articles during manufacture and removed afterwards
    • B22F10/47—Structures for supporting workpieces or articles during manufacture and removed afterwards characterised by structural features
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C64/00—Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
    • B29C64/10—Processes of additive manufacturing
    • B29C64/141—Processes of additive manufacturing using only solid materials
    • B29C64/153—Processes of additive manufacturing using only solid materials using layers of powder being selectively joined, e.g. by selective laser sintering or melting
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C64/00—Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
    • B29C64/40—Structures for supporting 3D objects during manufacture and intended to be sacrificed after completion thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B33—ADDITIVE MANUFACTURING TECHNOLOGY
    • B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y10/00—Processes of additive manufacturing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B33—ADDITIVE MANUFACTURING TECHNOLOGY
    • B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y30/00—Apparatus for additive manufacturing; Details thereof or accessories therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B33—ADDITIVE MANUFACTURING TECHNOLOGY
    • B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y40/00—Auxiliary operations or equipment, e.g. for material handling
    • B33Y40/20—Post-treatment, e.g. curing, coating or polishing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2999/00—Aspects linked to processes or compositions used in powder metallurgy
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P10/00—Technologies related to metal processing
    • Y02P10/25—Process efficiency

Definitions

  • the present invention relates to a method for powder bed-based additive manufacturing of at least one component, one or more powder bed-based additively manufactured component (s) having a support structure, a method for automatically separating a support structure from one or more powder bed-based Additive manufactured component (s), a method for automatically separating a support structure of one or more powder bed-based additively manufactured component / components of a construction platform, a method for automatically separating a support structure of one or more powder bed-based additively manufactured component (s) and from a construction platform as well as a plant for carrying out the process for powder bed-based additive production of at least one component and / or for carrying out the method for automatically separating a support structure from one or more powder bed-based additively manufactured component (s), a construction platform, a method for calculating geometry description data of one or more component (s) having a support structure and a corresponding computational product.
  • Support structures are intended as an additional building material to prevent a lowering of components in the space or their delay.
  • the danger for lowering and delay is particularly great as long as the components have not yet reached their final strength. Distortion can be caused, for example, by uneven cooling or uneven drying or setting of a component.
  • the delay primarily means the loss of dimensional accuracy of a component.
  • CONFIRMED GS OPIE The lowering of a component or a component portion can lead to form deviation or in the worst case to a release layer.
  • a separating layer means the interruption of the layer composite and thus also of the component.
  • the support structures usually bind directly to the component. After completion of the construction process, the support structures must be removed in the post process.
  • Support structures are predominantly used in processes in which the building material is liquid or flowable during the application.
  • the unbound powder primarily supports the components. If the component density increases during manufacture, the components can sink in the powder bed. Therefore, supporting structures can also be used here.
  • supporting structures can also be used here.
  • heat can be dissipated into the build platform via the support structure.
  • the construction data of the support structures as part of the geometry description data are automatically created by the machine software in the pre-process and can be optimized by the operator.
  • selective fusion or sintering of surface-applied powder with high-energy radiation e.g. Laser sintering
  • selective bonding of sheet applied powder with a binder printhead e.g. 3D printing
  • selectively polymerizing a photosensitive resin with UV radiation e.g. Stereolithography or Digital Light Processing (DLP)
  • formless building material is applied flat and then selectively cured.
  • the building material can be both liquid or pasty and powdery.
  • the support structures are constructed from the same building material as the component itself.
  • the support structure can be both a fine column structure and a statically optimized grid construction.
  • the support structures do not rest on the entire surface of the component. They are mainly used in the production of so-called "down-faces" (overhangs) in components.
  • the support structure can also end in the powder bed. It then serves more for heat dissipation.
  • the support structure does not necessarily have to be connected to the build platform, but may also be connected to both ends with the component.
  • the support structure does not have to end up at the bottom of a component. It can also be attached to one side and / or top of the component.
  • the separation of the support structures of a powder bed-based additively manufactured component is currently carried out in a post-processing step (post process) by a very complex manual labor.
  • the support structures are broken out, cut off, sawn off, ground or etched. This is a significant part of the total production time and thus significant (additional) manufacturing costs.
  • the present invention is therefore based on the object, an automated separation of the support structures of one or more powder bed-based additive manufactured component (s) and / or allow the build platform.
  • this object is achieved by a method for powder bed-based additive manufacturing of at least one component, in which
  • Powder from which at least one component is to be produced, is applied in layers as a powder bed on a building platform,
  • the at least one component by local melting of the powder is produced in layers and -
  • a support structure is produced together with the at least one component, which supports the at least one component at support points, wherein a structure of the at least one component, the support structure and the building platform is produced with at least one cavity which is designed so that when acted upon the cavity with an active medium with a predetermined pressure of this cavity, the pressure load so long without breakage, until at least one connection point between the component or one of the components and the support structure or at least one connection point between the building platform and the support structure or at least one connection point between different parts the support structure is broken by the pressure load.
  • Both the support points and the connection points can also be surfaces.
  • the active medium or the active media or at least one of the active media can / can, for example
  • inert gas such as argon, helium or carbon dioxide (C0 2 )
  • a powder bed-based additively manufactured component having a support structure which supports the at least one component at support points, wherein a structure comprising at least one component, a support structure and a build platform has at least one cavity, which is designed so that when exposed to the cavity with an active medium with a predetermined pressure of the cavity, the pressure load so long without break tolerates at least one connection point between the component or one of the components and the support structure or at least one connection point between the build platform and the support structure or at least one joint between different parts of the support structure is broken by this pressure load.
  • this object is achieved by a method for automatically separating a support structure of one or more powder bed-based additively manufactured component (s), in particular according to one of claims 21 to 26 and / or a construction platform, wherein the support structure with the component or the Components or the construction platform is connected and comprises a structure of the at least one component, a support structure which supports the at least one component at support points, and a construction platform at least one cavity comprises
  • a construction space housing with a construction platform for supporting one or more powder bed-based additive to be manufactured component / components
  • a layer preparation device for preparing respective powder layers on the building platform
  • an irradiation device for irradiating the respectively last-prepared powder layer on the construction platform in accordance with geometry description data of the component or components to be manufactured and the associated support structure
  • a control device for controlling the irradiation device in accordance with the geometry description data.
  • the object is achieved by a system or a system module for the automatic separation of a support structure of one or more powder bed-based additive manufactured component (s), in particular according to one of claims 21 to 26, and / or a construction platform, wherein the support structure with the Component or the components or construction platform is connected and a structure of the at least one component, a support structure, which supports the at least one component at support points, and a building platform at least one cavity, comprising a Wirlanediummakerss Rhein, which for controlling the loading of the cavity or at least one of the cavities with at least one active medium with a Wirkmediuman gleich founded of the component or at least one of the components and / or the support structure can be brought into fluid communication.
  • this object is achieved by a method for calculating geometry description data of one or more component / components with a support structure according to one of claims 21 to 26, wherein for a predefinable pressure, the geometry of the support structure is designed so that the expansion of each point of the wall of the Cavity or one of the cavities under pressure load is lower than the value of the breaking elongation of a material from which the component is to be built, and at least one connection point between the component or one of the components and the support structure or at least one connection point between the building platform and the support structure an elongation is reached which is equal to or higher than the value of the elongation at break of the material from which the component is to be built.
  • the present invention provides a computer program product that includes computer readable instructions that, when executed on a suitable system, perform a method according to any one of claims 1 to 20 and 32 to 36.
  • the cavity or at least one of the cavities partially from at least one component, in particular its underside or a part thereof, a part of the support structure, in particular a wall, the the build platform and the component connects, and the build platform is limited and in which there are support elements that connect the build platform and the component at the support points.
  • the cavity or at least one of the cavities is bounded in part by the at least one component, in particular by its underside or a part thereof or by the construction platform or a part thereof and a component, in particular a wall, of the support structure Surface of the component of the support structure on the side of the cavity with the component or with the building platform directly and / or is connected by support elements.
  • the wall or the walls of the cavity or at least one of the cavities is / are completely a component of a support structure, in particular a support element, which connects the construction platform and the component at the support points.
  • the wall (s) of the cavity or at least one of the cavities has / have at least one resilient wall portion which, upon pressurization of the cavity, has a greater deformation without break than the remaining wall of the cavity.
  • the at least one resilient wall section in sectional view has a symmetrical or asymmetric zigzag line course or a symmetrical or asymmetrical curved line course.
  • the at least one connection point between the component or one of the components and the support structure and / or the at least one connection point between the construction platform and the support structure and / or the at least one connection point between different parts of the support structure has / have a predetermined breaking point.
  • the connecting surface of the at least one connection point between the support structure and the component or at least one of the components and / or between the support structure and the building platform in sectional view parallel to the surface of the at least one component or the building platform in one direction, preferably continuously, for control the process of disconnecting.
  • connection surfaces of at least two connection points between the support structure and the component or at least one of the components and / or between the support structure and the construction platform in sectional view parallel to the surface of the component or the build platform are designed uniquely large, so that at the same pressure load, the joint with a smaller joint surface breaks earlier than the joint with a larger joint surface.
  • the pressurization takes place in stages, wherein in a first stage, a first pressure is used and in a second stage and all other stages, an ever higher pressure is used.
  • the wall or the walls of the cavity have / have a plurality of resilient wall sections, which are designed such that a first resilient wall section has a highest deformability and a second resilient wall section and further resilient wall sections have an ever lower deformability at a same stage of the pressurization ,
  • the resilient wall portions are designed such that a deformation of the first resilient wall portion in the first stage of pressurization, a deformation of the second resilient wall portion in the second stage of pressurization and a deformation of each other compliant wall portion in a corresponding Level of pressurization are the same or comparable.
  • the cavity may be part of a larger cavity, which is a part of the support structure and separately with pressure, preferably different stages, can be acted upon.
  • the structure has at least one cavity, which is partially bounded by at least one component, and at least one cavity, which is partially bounded by the construction platform, and the support elements of the at least one component and of the building platform separated by the at least one cavity, which is partially bounded by the at least one component, and the at least one cavity, which is partially bounded by the construction platform, at the same time or almost simultaneously or chronologically successively acted upon by a working medium with a predetermined positive or negative pressure become.
  • a treatment of the entire component or of all components or of a respective part thereof is carried out by passing an active medium through the cavity or at least one of the cavities.
  • the treatment comprises a passage of pressurized air for removing loose powder located in the cavity and takes place before the pressurization of the cavity for separating the connection points between the component and the support structure or between the component and the building platform.
  • the treatment may comprise a cooling, heating or maintaining a temperature (temperature control), and / or a pressure treatment.
  • the powder bed-based additively manufactured component, the cavity or at least one of the cavities partially from at least one component, in particular its underside or a part thereof, a component of the support structure, in particular a wall, the building platform and the component connects, and the build platform are limited and in which there are support elements that connect the construction platform and the component at the support points.
  • the cavity or at least one of the cavities is bounded in part by the at least one component, in particular by its underside or a part thereof or by the construction platform or a part thereof and a component, in particular a wall, of the support structure Surface of the component of the support structure on the side of the cavity with the component or with the building platform directly and / or is connected by support elements.
  • the wall or the walls of the cavity or at least one of the cavities is part of a support element / which is the at least one component with the construction platform or the at least one component with a part of Support structure or the building platform with a part of the support structure or different parts of the support structure interconnects.
  • the component (s) comprise / comprise at least one active medium inlet for selectively selectively exposing the at least one cavity to an active medium with an overpressure or underpressure.
  • the at least one connection point between the component or one of the components and the support structure and / or the at least one connection point between the construction platform and the support structure and / or the at least one connection point between different parts of the support structure has / have a predetermined breaking point ,
  • this further comprises an active medium supply device, which for the controlled loading of the cavity or at least one of the cavities with at least one active medium with a Wirlanediuman gleich vibration of the component or at least one the components and / or the support structure can be brought into connection.
  • the system may include a post-processing device integrated in the package housing or separate therefrom for separating a non-broken wall of the cavity remaining after pressurizing the cavity on the component or on a build platform by means of another separation method, in particular milling or laser cutting.
  • a post-processing device integrated in the package housing or separate therefrom for separating a non-broken wall of the cavity remaining after pressurizing the cavity on the component or on a build platform by means of another separation method, in particular milling or laser cutting.
  • the plant or the plant module for automatic separation of a support structure a post-processing device for separating a remaining after the pressurization of the cavity on the component or on a building platform, not broken wall of the cavity by means of another separation process, in particular milling or laser cutting on.
  • a post-processing device for separating a remaining after the pressurization of the cavity on the component or on a building platform, not broken wall of the cavity by means of another separation process, in particular milling or laser cutting on.
  • at least one connection point between the component or one of the components and the support structure or the at least one connection point between the build platform and the support structure is specifically designed such that the connection surface of this connection point continuously increases in a predetermined direction, so that the separation of this connection point takes place in this direction.
  • connection surfaces of at least two connection points between the support structure and the component or one of the components or between the support structure and the construction platform are designed unequally unequal, so that at the same pressure load, the junction with a smaller connection surface breaks earlier than the Joint with a larger interface.
  • the geometric orientation of a portion of the walls of a cavity on the side of the support structure is calculated in accordance with a surface caused by a parallel displacement of at least a portion of the cavity-limiting component surface in a normal direction to that surface he follows.
  • a calculation module for the interpretation of the geometry description data of one or more component / components may be present with a support structure.
  • an interface for exporting the calculated geometry description data may be present.
  • the support structure may be designed on the building platform side as well as on the component side.
  • the separation of the support structure from a construction platform can be carried out analogously to and / or simultaneously with the separation of the support structure of the component components.
  • the present invention is based on the surprising finding that the separation of the supports or at least part of the supports from the component can occur as a result of deformation of the support structure caused by pressurization with an active medium.
  • a pressurization can be realized by providing the cavities through which the active medium can be passed.
  • the support structure acquires additional functionality of "self-separation."
  • a very large part of the supports can be separated from the component, and the walls of the cavity should be held during the pressure loading or separation of the supports. They can be separated from the component in a next step with other separation methods, such as milling or laser cutting, automatically.
  • the supports can only be positioned in places that are easily accessible, so that the subsequent removal of the supports would be possible.
  • the supports can also be arranged on the outside not or difficult to reach places.
  • Any permanent walls of the cavity associated with the component may, at least in one particular embodiment, preferably be positioned at locations readily accessible from the outside so that in a subsequent step they may be treated by methods such as e.g. Milling or laser cutting, in a, preferably automated, mode can be easily separated.
  • the pressurization with an active medium has the advantage of a uniform load (hydrostatic pressure) of the component and the support structure, at least in one particular embodiment.
  • An even load during the separation of the columns "spares" the component from a strong deformation.
  • Figure 1 is a sectional view of a powder bed-based additively manufactured component with a support structure according to a particular embodiment of the present invention
  • Figure 2 is a sectional view taken along the line II - II in Figure 1;
  • Figure 3 is a sectional view of a powder bed-based additively manufactured component with a support structure according to another particular embodiment of the present invention.
  • Figure 4 is a sectional view taken along the line IV - IV in Figure 3;
  • Figure 5 shows various stages of a method for automatically separating at least part of a support structure from the component according to Figures 1 and 2 or 3 and 4 according to a particular embodiment of the present invention
  • FIG. 6 shows a sectional view along the line VI-VI in FIG. 7 of a powder bed-based additively manufactured component with a support structure according to a further particular embodiment of the present invention
  • Figure 7 is a sectional view taken along the line VII - VII in Figure 6;
  • Figure 8 is a sectional view taken along the line VIII - VIII in Figure 7;
  • FIG. 9 shows a sectional view along the line IX - IX in FIG. 10 of a powder bed-based additively manufactured component with a support structure according to a further particular embodiment of the present invention.
  • Figure 10 is a sectional view taken along the line X - X in Figure 9;
  • Figure 1 1 is a sectional view taken along the line XI - XI in Figure 10;
  • Figure 12 shows various stages of a method for automatically separating at least a part of a support structure from the component according to Figures 6 to 8 or 9 to 1 1 according to a particular embodiment of the present invention
  • FIG. 13 shows a sectional view of a powder bed-based additively manufactured component with a support structure according to a further particular embodiment of the present invention
  • Figure 14 is a sectional view taken along the line XIV - XIV in Figure 13;
  • FIG. 15 shows various stages of a method for automatically separating at least part of a support structure from the component according to FIGS. 13 and 14 according to a particular embodiment of the present invention
  • FIG. 16 is a sectional view of a powder bed-based additive-fabricated component having a support structure according to another particular embodiment of the present invention.
  • FIG. 17 is a sectional view of a powder bed-based additive-fabricated component having a support structure according to another particular embodiment of the present invention.
  • FIG. 18 is a sectional view of a powder bed-based additive-fabricated component having a support structure according to another particular embodiment of the present invention
  • Fig. 19 is a sectional view taken along the line XIX-XIX in Fig. 18;
  • Figure 20 is a sectional view of a powder bed-based additively manufactured component with a support structure according to another particular embodiment of the present invention.
  • Fig. 21 is a sectional view taken along the line XXI-XXI in Fig. 20;
  • FIG. 22 shows a detail of FIG. 20
  • Figure 23 is a sectional view taken along the line XXIII - XXIII in Figure 22;
  • FIG. 24 shows a variant of the embodiment shown in FIG. 22;
  • Fig. 25 is a sectional view taken along the line XXV-XXV in Fig. 24;
  • Figures 26 to 36 are views of a powder bed based additive manufactured component with a support structure according to another particular embodiment of the invention.
  • Figures 1 and 2 show a powder bed-based additively manufactured component 10 with a support structure 12 according to a particular embodiment of the present invention in a sectional view and along the line II-II in Figure 1 ( Figure 2).
  • the support structure 12 is located between a lower construction platform 14 and the upper component 10 and supports the component 10 at support points 16.
  • the support points 16 are located on the underside 18 of the component.
  • the support structure 12 includes an outer wall 28, which in this example is arranged in a rectangle and which directly connects the build platform 14 and the component 10 in this example, as well as inner support elements 30 that support the build platform 14 and the component 18 at the support points 16 will be discussed in more detail below.
  • the outer wall 28 is connected to right and left sides 20 and 22 and front and rear sides 24 and 26 of the component 10.
  • the structure 32 of the component 10, the support structure 12 and the building platform 14 has a cavity 34 which extends from the underside 18 and the sides 20 to 26 of the component 10 and from the wall 28 of the support structure 12 and from a part of the top 36 the construction platform 14 is limited and in which the support elements 30 are located.
  • the wall 28 in this example has a circumferential resilient wall section 38 which, upon pressure of the cavity 34, has a greater deformation without fracture than the remaining wall of the cavity 34 (see FIG. 5).
  • the construction platform 14 has an opening (passage opening) 40 arranged centrally in this example as the active medium inlet and if necessary. also - outlet on.
  • the support members 30 are designed needle-shaped in this example.
  • the support members 30 taper continuously from the side of the build platform 14 to the side of the component 10 in this example. In this example, there are twelve support members 30 within the cavity 34.
  • FIGS. 3 and 4 differs from the embodiment shown in FIGS. 1 and 2 only in that the support elements 30 are not needle-shaped but plate-shaped. In addition, only four instead of twelve inner support members 30 are present in this example.
  • FIGS. 1 and 2 as well as 3 and 4 can be produced, for example, by a process for powder bed-based additive manufacturing, in which powder (not shown) from which the component 10 is to be produced is laid in layers is applied as a powder bed (not shown) on a building platform 14, the component 10 is made by local melting of the powder in layers and is produced together with the component 10, the support structure 12, the the component 10 is supported on the support points 16, wherein the structure 32 is made of the component 10, the support structure 12 and the build platform 14 with the cavity 34, from the bottom 18 and the sides 20 to 26 of the component 10, the wall 28th , which connects the build platform 14 and the component 10, and the upper side 36 of the build platform 14 is limited and in which the support elements 30 are that connect the build platform 14 and the component 10 at the support points 16.
  • FIG. 5 shows by way of example how, for example, in the two embodiments shown in FIGS. 1 to 4 a separation of the component 10 from the upper ends of the support elements 30 at the connection points 42, which in this case coincide with the support points 16, under pressure by means of an active medium, pressurized through the opening 40 in the build platform 14 in this example from below into the cavity 34.
  • the wall 28 Since the wall 28 has a resilient wall portion 38, it withstands the pressure P (see Figures 5 (a) and (b)) and also does not detach at its upper end from the component 10, while the aforementioned joints 42 between the Bottom 18 of the component 10 and the upper ends of the support members 30 are broken or separated (see Figure 5 (b)).
  • the outer elements of the support structure 12, in this example the wall 28, can then be separated, for example by preferably automatic milling on the component 10 thereafter.
  • FIGS. 6 to 8 show a further exemplary embodiment of a powder-bed-based additive-fabricated component 100 having a support structure 112 which supports the component 100 at three support points or lines or surfaces 116 on the underside 118 of the component 100 in this example an outer wall 128, which is rectangular in this example, and in this example has an inner support member 130 disposed between a lower build platform 114 and the upper component 100.
  • Fig. 6 is a sectional view taken along the line VI-VI of Fig. 7
  • Fig. 7 is a sectional view taken along the line VII-VII in Fig. 6
  • Fig. 8 is a sectional view taken along the line VIII-VIII in Fig. 7.
  • the structure 132 of the component 100, the support structure 1 12 and the build platform 114 has a cavity 134 which from the bottom 1 18 of the component 100, of the wall 128 of the support structure 112 and of a portion of the top 136 of the building platform. 1 14 is limited.
  • the supporting element 130 which is centrally arranged in this example on the lower side 1 18 of the component 100 and supports the component 100 at the support point 16, is not directly connected to the upper side 136 of the building platform 114, but is connected to the inner surface via a resilient part 138 139 of the wall 128 connected.
  • the resilient member 138 has the shape of a symmetrical in this example pointed roof.
  • the two parts 138 form in this example an angle of about 90 °.
  • the delivery of an active medium does not take place via an opening in the build platform, but via openings 140 and 141 as the active medium inlet and / or outlet.
  • FIGS. 9 to 11 essentially differs from the embodiment shown in FIGS. 6 to 8 in that the support element 130 is not needle-shaped, tapering from bottom to top, but instead has a top or wall shape , spaced through passage openings 129 and interposed predetermined breaking points 131 is formed. Furthermore, the resilient part 138 in the sectional view shown in Figure 1 1 is not pointed roof-shaped, but formed with a blunt top.
  • FIG. 12 now shows a method for preferably automatically separating at least a part of the support structure 112 of the embodiments shown in FIGS. 6 to 11 by applying pressure P through at least one of the openings 140 and 141 141 may be closed to build up a pressure in the cavity 134. Since the portion 138 is compliant while the support member 130 is at least stiffer than the compliant portion 138, the upper end of the support member 130 at the junction 142 corresponding to the support point 16 in the center of the bottom surface 118 of the component 100 is severed ( see Figure 12 (b)). The outer ones Elements of the support structure 112, in this example the wall 128, can then be separated from the component 100, for example by preferably automatic milling.
  • Figures 13 and 14 show another embodiment of a powdered-based additive-fabricated component 200 according to a particular embodiment of the present invention having a support structure 212 disposed between a lower build platform 214 and the upper component 200 and the component 200 in place therein Example a total of eleven support points 216 supports. More specifically, Fig. 13 is a sectional view taken along the line XIII-XIII in Fig. 14, and Fig. 14 is a sectional view taken along the line XIV in Fig. 13.
  • the formation 232 of the component 200, the support structure 212 and the build platform 214 has a cavity 234, wherein the wall 228 of the cavity 234 is part of a support member 230 which connects the component 200 with the build platform 214.
  • the wall 228 of the cavity 234 has a resilient wall portion 238 which, upon pressurization of the cavity 234, experiences a greater deformation without fracture than the remainder of the wall of the cavity.
  • the support element 230 is connected to the component 200 at a support point 216 which is arranged centrally on the underside 218 of the component 200 in this example.
  • the component 200 is connected to the build platform 214 via four bar or columnar support members 230 in this example, or is supported over the build platform 214 thereabove.
  • the central in this example four support members 230 are above the respective cavity 234 to the side of the component 200 in the form of a needle, tapering from bottom to top, designed.
  • Below the respective cavity 234, the respective support member 230 is substantially rod-or. designed columnar and has an opening or a channel 240 for insertion and / or omission of an active medium (not shown).
  • FIG. 15 shows how the respective cavity 234, when acted upon by pressure P by means of an active medium, passes through the channel 240 from a substantially oval shape with a vertical longitudinal axis (see FIG. 15 (a)) into a substantially round shape (see FIG. 15 (b)) and the support elements 230 at the connection point 242, which corresponds to the respective support point 216, is separated from the underside 218 of the component 200.
  • 16 shows, in principle, a component 300 having a support structure 312 according to a particular embodiment of the present invention, wherein the support structure 312 is in principle a plurality of the support elements 130, shown for example in FIGS. 6 to 8 and 9 to 11, here identified as support elements 330 , includes.
  • the resilient parts 338 are supported on an outer wall 328 of the cavity 334 and on the lower sockets 339.
  • each two parts 438 in sectional view form an asymmetrical pointed roof with an angle which is smaller than 90 °.
  • FIG. 18 The embodiment of a component 500 with a support structure 512 shown in FIG. 18 essentially differs from the embodiment shown in FIG. 16 in that the support structure does not comprise any needle-shaped support elements but only the resilient parts 538, the pedestals 539 and the outer wall 528 (see Figure 18 (a)).
  • the support structure does not comprise any needle-shaped support elements but only the resilient parts 538, the pedestals 539 and the outer wall 528 (see Figure 18 (a)).
  • FIG. 19 shows a thickness d of the linear connection point 516 and predetermined breaking points 546 between the passage openings 544.
  • Figure 20 is a sectional view taken along the line XX - XX in Figure 21 (top) and Figure 21 (bottom) is a sectional view taken along the line XXI - XXI in Figure 20 of another component 600 having a support structure 612 between a lower building platform
  • the build platform 614 has two lateral, vertically extending openings 602 and 603 in this example, which are for the inlet and / or outlet of an active medium (not shown) having a respective active medium inlet opening 604, 605 and / or outlet in the support structure 612 and further openings 606 and 607 in an inner wall 629 of the support structure 612 is in active medium connection, such that an active medium can be given under pressure from a active medium supply device via the active-medium connection device 608 or 609 (shown only in FIG. 20) into a cavity 634.
  • Fig. 22 is a sectional view taken along a line XXII - XXII in Fig. 23 and Fig. 23 is a sectional view taken along the line XXIII - XXIII in Fig. 22. It shows the arrangement and connection of a support member 730 below the bottom 718 of another component 700 according to another particular embodiment of the present invention.
  • the joint 742 which in principle corresponds to the support point 716, is a connection surface or strip, the width of which in a direction FD ("Fracture Direction") continuously increases in this example achieve a targeted directed breakage of the support member 730.
  • the embodiment of a component 800 shown in FIGS. 24 and 25 essentially differs from the embodiment shown in FIGS. 22 and 23 in that the support element 830 in the upper region is not plate-shaped but has a needle-shaped design and a plurality of support elements are present.
  • Figures 26 to 35 show a further embodiment of a powder bed-based additively manufactured component 900 according to a particular embodiment of a present invention.
  • the component 900 (FIGS. 26-28) has three interior spaces 936, 937 and 938 with ellipsoidal inner surfaces 916, 917 and 918, respectively.
  • the inner surfaces 916, 917 and 918 must be supported in the region of overhangs.
  • FIG. 29 shows that a surface 919 to be supported can not be reworked after the build-up process due to an inability to access a tool 950 (eg a milling cutter). For this reason, support members attached to the upper surface area 919 can not be removed by mechanical post-processing.
  • the support structure 912 is arranged in the interiors 936, 937 and 938 of the component 900 and supports the component 900 in this example a total of ten support points 916 (five in the upper area and another five in the lower area).
  • the formation 932 of the component 900 and the support structure 912 has two cavities 934 and 935.
  • a wall 928 of the cavity 934 has a resilient wall section 938 which, upon pressurization of the cavity 934, has a greater deformation without fracture than the remaining wall of the cavity learns.
  • the cavity 935 is completely part of the support structure 912.
  • the powder is removed from the cavity 935 through openings 942 and 943 prior to pressurization of the other cavity 934 so that the compliant wall sections 938 could deform without resistance during pressurization ,
  • Support members 930 are connected to the component 900 at a plurality of support points 916.
  • the pressurization of the cavity 34 is carried out by the active medium (not shown), which is in and out through the openings 941 and 942.
  • FIG. 33 shows the deformation of the resilient wall sections 938 after the pressurization of the cavity 934. This deformation leads to the separation of the support elements 930 from the component 900 at joints 942.
  • FIGS. 34 and 35 show the subsequent mechanical finishing.
  • Movement of the tool 950 removes a large portion of the support structure 912 from the interior spaces 937 and 938.
  • the support elements are also removed 930 are separated from the support structure at locations 920.
  • the remaining remnants of the support members 930 separated from the support structure 912 are readily removable via the interior spaces 937 and 938 vacated by the support structure 912.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Plasma & Fusion (AREA)
  • Mechanical Engineering (AREA)

Abstract

L'invention concerne un procédé pour la fabrication additive sur la base d'un lit de poudre d'au moins une pièce, dans lequel la poudre, à partir de laquelle au moins une pièce doit être fabriquée, est appliquée par couches sous forme de lit de poudre sur une plate-forme de construction. Ladite au moins une pièce est fabriquée par couches par fusion locale de la poudre et une structure support, qui supporte ladite au moins une pièce au niveau de sites support, est fabriquée ensemble avec ladite au moins une pièce. Une structure constituée par ladite au moins une pièce, la structure support et la plate-forme de construction est fabriquée tout en présentant au moins un espace creux qui est conçu de manière telle que lors de la sollicitation de l'espace creux par un milieu de travail se trouvant à une pression déterminable, cet espace creux résiste à la sollicitation par la pression sans rupture jusqu'à ce qu'au moins un site de liaison entre la pièce ou une des pièces et la structure support ou au moins un site de liaison entre la plate-forme de construction et la structure support ou au moins un site de liaison entre différentes parties de la structure support se rompe(nt) par la sollicitation par la pression.
PCT/EP2018/000039 2017-01-31 2018-01-29 Séparation automatisée de structures support d'une pièce fabriquée de manière additive sur la base d'un lit de poudre WO2018141476A1 (fr)

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DE102017101834.4 2017-01-31
DE102017101834.4A DE102017101834A1 (de) 2017-01-31 2017-01-31 Automatisiertes Abtrennen von Stützstrukturen von einem Pulverbett-basiert additiv hergestellten Bauteil

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EP3733380A1 (fr) * 2019-05-03 2020-11-04 Raytheon Technologies Corporation Systèmes et procédés d'élimination de matériau de support
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EP4008458A1 (fr) * 2020-12-01 2022-06-08 Raytheon Technologies Corporation Structure de support érodable pour article fabriqué de manière additive et procédé associé

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WO2021001019A1 (fr) * 2019-07-02 2021-01-07 Siemens Aktiengesellschaft Dispositif permettant de détacher une pièce imprimée en 3d, procédé de détachement et structure de support
DE102019210499A1 (de) * 2019-07-16 2021-01-21 MTU Aero Engines AG Verfahren zum generativen aufbauen und separieren eines bauteils
DE102019131629A1 (de) * 2019-11-22 2021-05-27 Bayerische Motoren Werke Aktiengesellschaft Verfahren zur additiven Herstellung eines dreidimensionalen Objekts
DE102020100651A1 (de) * 2020-01-14 2021-07-15 Bayerische Motoren Werke Aktiengesellschaft Verfahren zur Herstellung eines Bauteils, insbesondere eines Fahrzeugbauteils
DE102020201621A1 (de) 2020-02-10 2021-08-12 Siemens Aktiengesellschaft Strategie zum Trennen von Bauteilen in der additiven Herstellung
DE102021105228A1 (de) 2021-03-04 2022-09-08 KSB SE & Co. KGaA Entfernen der Stützstruktur mit einem auf einem Roboterarm integrierten Laserstrahll
DE102021117939A1 (de) 2021-07-12 2023-01-12 Amsis Gmbh Supportelementanordnung zum Abstützen eines additiv aufzubauenden oder aufgebauten Objektabschnitts auf einem Untergrund
DE102021129549A1 (de) * 2021-11-12 2023-05-17 Trumpf Laser- Und Systemtechnik Gmbh Verfahren und Vorrichtung zur additiven Fertigung zumindest eines leicht von einem Träger ablösbaren Bauteils
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