WO2012131481A1 - Part structure built by metal powder based added manufacturing - Google Patents

Part structure built by metal powder based added manufacturing Download PDF

Info

Publication number
WO2012131481A1
WO2012131481A1 PCT/IB2012/000636 IB2012000636W WO2012131481A1 WO 2012131481 A1 WO2012131481 A1 WO 2012131481A1 IB 2012000636 W IB2012000636 W IB 2012000636W WO 2012131481 A1 WO2012131481 A1 WO 2012131481A1
Authority
WO
WIPO (PCT)
Prior art keywords
elements
structure according
grid
part structure
metal powder
Prior art date
Application number
PCT/IB2012/000636
Other languages
French (fr)
Inventor
Adriaan Spierings
Gideon Levy
Original Assignee
Inspire Ag, Irpd
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 Inspire Ag, Irpd filed Critical Inspire Ag, Irpd
Publication of WO2012131481A1 publication Critical patent/WO2012131481A1/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/06Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
    • B22F7/062Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/20Direct sintering or melting
    • B22F10/28Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM]
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/40Structures for supporting workpieces or articles during manufacture and removed afterwards
    • B22F10/47Structures for supporting workpieces or articles during manufacture and removed afterwards characterised by structural features
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B33ADDITIVE MANUFACTURING TECHNOLOGY
    • B33YADDITIVE 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
    • B33Y10/00Processes of additive manufacturing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B33ADDITIVE MANUFACTURING TECHNOLOGY
    • B33YADDITIVE 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
    • B33Y40/00Auxiliary operations or equipment, e.g. for material handling
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/60Treatment of workpieces or articles after build-up
    • B22F10/64Treatment of workpieces or articles after build-up by thermal means
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F12/00Apparatus or devices specially adapted for additive manufacturing; Auxiliary means for additive manufacturing; Combinations of additive manufacturing apparatus or devices with other processing apparatus or devices
    • B22F12/40Radiation means
    • B22F12/41Radiation means characterised by the type, e.g. laser or electron beam
    • B22F12/43Radiation means characterised by the type, e.g. laser or electron beam pulsed; frequency modulated
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2999/00Aspects linked to processes or compositions used in powder metallurgy
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C64/00Additive 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
    • B29C64/40Structures for supporting 3D objects during manufacture and intended to be sacrificed after completion thereof
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P10/00Technologies related to metal processing
    • Y02P10/25Process efficiency

Definitions

  • the invention relates to a part structure built by metal powder based added
  • a metal powder forming a metal powder bed resting on a base element is selectively fused in a layer-by-layer fashion such as by selective laser melting, selective electron beam melting or selective ion beam melting.
  • the resulting part structure comprises at least one individual part and an auxiliary structure attached to the at least one individual part and to the base element.
  • Thermal processes (Selective Laser Melting, Electron Beam Melting) use a high energy beam in order to melt the raw material (powders). In order to guarantee a stable build process, the thermal energy has to flow away from the created melt-pool. Therefore, the support structure can act as a thermal heat sink, taking up this amount of energy.
  • the invention provides a part structure built by metal powder based added manufacturing, wherein a metal powder forming a metal powder bed resting on a base element is selectively fused in a layer-by-layer fashion such as by selective laser melting, selective electron beam melting or selective ion beam melting, and wherein the part structure comprises at least one individual part and an auxiliary structure attached to the at least one individual part and to the base element.
  • this auxiliary structure is a grid-like structure comprising different types of grid elements including beam elements and volume elements.
  • the beam elements include beam elements differing in beam length and in beam cross section.
  • At least some of said beam elements are arranged in a tree-like fashion forming a tree-like portion of the grid-like structure.
  • the part structure comprises attachment elements arranged between the at least one individual part and the auxiliary structure and/or arranged between the base element and the auxiliary structure.
  • the attachment elements comprise pre-defined breaking points.
  • the volume elements within the auxiliary structure are located adjacent to the at least one individual part.
  • attachment elements preferably only attachment elements, are arranged between the at least one individual part and the auxiliary structure.
  • the density of grid-elements in the grid-like structure increases as one approaches the at least one individual part and, preferably, is greatest adjacent to the at least one individual part.
  • the beam element diameter is less than 4 mm, the lower limit of the beam element diameter being determined by the metal type and particle size of the powder.
  • the beam element may be a hollow, tube-like element and, preferably, may have a wall thickness of less than 45% of the beam element diameter, the lower limit of the wall thickness again being determined by the metal type and particle size of the powder.
  • the cross-section of the beam elements may have a circular or polygonal shape.
  • the attachment elements comprise constrictions and/or porous regions pre-defining the breaking points.
  • an angle formed between a part surface of the at least one individual part and the horizontal is between 0 and 60°.
  • the beam elements in the gridlike structure are arranged at angles greater than 45° to the horizontal.
  • the above mentioned different types of grid-elements are arranged as a mechanical support and heat removal structure between an overhanging part surface and the horizontal.
  • the support structures act as a thermal sink for the surfaces that have to be built.
  • the volume support structures in contrast to e.g. fine walls.
  • the support structures are able to support different structural elements of a physical part. These elements can be classified as:
  • the laser during the build process, can be operated in continuous wave mode or in pulse mode.
  • the pulse parameters mean energy, pulse energy, pulse shape, frequency
  • the material parameters hardness, density, heat
  • Fig. 1 indicates the situation of total energy introduced into the part structure and different types of energy flows within and out of the part structure.
  • Fig. 2 is a side view showing a first example of a part structure according to the invention.
  • Fig. 3 is a side view showing a second example of a part structure according to the invention.
  • Fig. 4 is a side view showing a third example of a part structure according to the invention.
  • Fig. 5 is a perspective view showing a fourth example of a part structure according to the invention.
  • Fig. 6 is a side view showing a fifth example of a part structure according to the invention.
  • Fig. 7 is a side view showing a sixth example of a part structure according to the invention.
  • Fig. 8 is a side view showing a first detail of a part structure according to the invention.
  • Fig. 9 is a side view showing a second detail of a part structure according to the invention.
  • volume elements serving as additional thermal heat sinks near the part surfaces / part structures are built ("part-near volume element").
  • additional heat sinks in addition to the heat sink function of the part being built
  • Relevant criteria for the design of the volume elements are the type of the part structures that need a support (part surfaces and edges with an angle to the horizontal, holes), the angle to the horizontal of the part structures or part surfaces, and the size of the part structures.
  • the design and the size of the part-near volume elements and support structures as well as their distances to the part could be estimated and optimized by the space- resolved solution of the heat equation.
  • the heat sink structures can be described by several structural parameters, defining the shape / type of the heat sink, the size and the volume of the heat sink, or the distance of the heat sink to the part surface.
  • Thermal heat sinks can also be used for the stacking of parts.
  • a horizontal volume plate is built, defining a new base plate for the more highly positioned next part, as shown in Fig. 7.
  • a tree-like grid structure holding the heat sink in place in the case where additional heat sinks are used, as shown in Figs. 2 and 5.
  • This tree-like grid structure may also directly support part surfaces or part structures at regularly spaced or evenly distributed locations using specially designed attachment points, as shown in Fig. 4.
  • the size, shape and distribution of the single grid elements as well as the overall grid structure can be designed according to the need for a fast cooling down of the surface-near volume after scanning.
  • the grid-structure itself may consist of different types of grid-elements having different sizes / volumes.
  • the grid shows - starting from the base plate - an evolutionary development regarding the shape, design and density of the beams, defining a tree-like grid structure, as shown in Fig 3.
  • the grid elements are standing only on the base plate and do not touch any part surface.
  • the density of the grid elements may change depending on the location within the grid. The closer to the part surface the narrower is the grid.
  • the support structures consisting of volume- and grid-elements, can be built under different angles to the horizontal and are designed with respect to the technical requirements and restrictions of the build process (e.g. SLM).
  • the angle to the horizontal of the structures will be > 3 ⁇ 445°.
  • the support structures can start to support the part structures at a specific height form the base plate, where the starting height depends on the orientation of the part surfaces that need a support.
  • Figs. 2 to 7 show some possible part structures built by metal powder based added manufacturing according to the invention.
  • Fig. 2 is a side view showing a first example of a part structure 1 according to the invention.
  • the part structure 1 comprises a part 2 with an overhanging part surface 2a, a grid-like auxiliary structure 4, 5 and attachment elements 6.
  • the grid-like auxiliary structure 4, 5 comprises beam elements 4 of different lengths and volume elements 5 attached to them.
  • the part 2 and the beam elements 4 are supported by and attached to a base plate 3.
  • the volume elements 5 are attached to the beam elements 4 and to a part surface 2a of the part 2.
  • part 2 is partially supported directly by the base element 3 and partially supported indirectly by the base element 3 via the grid-like auxiliary structure 4, 5.
  • the part surface 2a forms an angle of about 40° with respect to the horizontal plane H (base plate plane), thus constituting an overhanging part 2 with an auxiliary structure 4, 5 between the overhanging part surface 2a and the base plate 3.
  • the auxiliary structure 4, 5 provides conductive connections / pathways by its beam elements 4 for removing heat from the part 2 on the one hand and heat sinks by its volume elements 5 for receiving some of the heat removed from the part 2.
  • the beam elements 4 have different lengths and may be hollow, tube-like elements. Most of the beam elements extend along directions different from the vertical direction V. In contrast, the volume elements 5 are solid and may have different sizes. Each of the volume elements 5 has a large surface facing the part surface 2 and narrows towards an opposite end where the volume element 5 is attached to a beam element 4. The large surface of the volume element 5 is attached to the part surface 2a of the part 2 via a plurality of attachment elements 6. The narrow opposite end of the volume element 5 is attached to the beam element 4 via an attachment element 6.
  • the overhanging part surface 2a is support-free up to a height h form the horizontal plane H. Beyond that support-free height, the part 2 is mechanically supported and provided with an additional strong heat sink by the grid-like auxiliary structure 4, 5.
  • Fig. 3 is a side view showing a second example of a part structure 1 according to the invention.
  • the part structure 1 comprises a part 2 with two overhanging part surfaces 2a, and a tree-like auxiliary structure 4 and attachment elements 6.
  • the tree-like auxiliary structure 4 comprises only beam elements 4 of different lengths.
  • volume elements 5 could be included in the tree-like structure 4 in a manner similar to the example shown in Fig. 2. Only the beam elements 4 are supported by and attached to the base plate 3. Thus, part 2 is only supported indirectly by the base element 3 via the tree-like auxiliary structure 4.
  • Fig. 4 is a side view showing a third example of a part structure 1 according to the invention.
  • This part structure 1 is similar to the part structure 1 shown in Fig. 2.
  • the part structure 1 comprises a part 2 with an overhanging part surface 2a, a tree-like auxiliary structure 4 and attachment elements 6.
  • the tree-like auxiliary structure 4 comprises only beam elements 4 of different lengths.
  • the part 2 and the beam elements 4 are supported by and attached to the base plate 3.
  • the beam elements 4 are attached to the part surface 2a of the part 2.
  • part 2 is partially supported directly by the base element 3 and partially supported indirectly by the base element 3 via the tree-like auxiliary structure 4.
  • the overhanging part surface 2a is support-free up to a height h form the horizontal plane H. Beyond that support-free height, the part 2 is
  • Fig. 5 is a perspective view showing a fourth example of a part structure 1 according to the invention.
  • This part structure 1 is similar to the part structure 1 shown in Fig. 2.
  • the part structure 1 comprises a part 2 with an overhanging part surface 2a, a gridlike auxiliary structure 4, 5 and attachment elements 6.
  • the grid-like auxiliary structure 4, 5 comprises beam elements 4 of different lengths and one volume element 5 attached to them.
  • the part 2 and the beam elements 4 are supported by and attached to a base plate 3.
  • the volume element 5 is attached to the beam elements 4 and to a part edge 2b delimiting the part surface 2a of the part 2.
  • part 2 is partially supported directly by the base element 3 and partially supported indirectly by the base element 3 via the grid-like auxiliary structure 4, 5.
  • Fig. 6 is a side view showing a fifth example of a part structure 1 according to the invention.
  • This part structure 1 allows two parts 2 to be arranged in a vertically spaced relationship, i.e. the two parts 2 can be arranged
  • Each of the two parts 2 is supported by a tree-like auxiliary structure 4 comprising only beam elements 4 in a manner similar to the one shown in Fig. 3.
  • some beam elements 4 extending between the two parts 2 provide additional mechanical stability and a thermal pathway between the two parts 2.
  • the lower one of the two parts 2 may serve as a heat sink for the upper one of the two parts 2.
  • Fig. 7 is a side view showing a sixth example of a part structure 1 according to the invention.
  • This part structure 1 is similar to the part structure 1 of Fig. 6. Again, this part structure 1 allows two parts 2 to be arranged in a vertically spaced relationship, i.e. the two parts 2 can be arranged one on top of the other.
  • Each of the two parts 2 is supported by a tree-like auxiliary structure 4 comprising only beam elements 4 in a manner similar to the one shown in Fig. 3.
  • a second base plate 3 extending horizontally between the two parts 2 provides additional mechanical stability and an additional heat sink.
  • a lower group of beam elements 4 extend between the lower one of the two parts 2 and the second base plate 3
  • an upper group of beam elements 4 extend between the upper one of the two parts 2 and the second base plate 3, thus contributing to the additional mechanical stability and providing a thermal pathway between the two parts 2.
  • the second base plate 3 and the lower one of the two parts 2 may serve as a heat sink for the upper one of the two parts 2.
  • Fig. 8 is a side view showing a first detail of a part structure 1 according to the invention.
  • the first type of attachment element 6 is a tetrahedron-like or pyramid-like element with one constriction 6a at the narrowing top of the tetrahedron / pyramid.
  • the second type of attachment element 6 is a double-tetrahedron-like or double-pyramid-like element again with one constriction 6a where the narrowing tops / ends of the tetrahedron / pyramid meet.
  • the third type of attachment element 6 is a cylinder-like element. Instead of a constriction, it may have a porous region somewhere along its cylinder axis. Both the constrictions 6a and the porous region constitute pre-defined breaking points of the attachment elements 6.
  • Fig. 9 is a side view showing a second detail of a part structure according to the invention.
  • An angled attachment element 6' is shown which comprises a first attachment element portion 6b and a second attachment element portion 6c.
  • the bigger attachment element portion 6b is attached to the base plate 3 via a first constriction 6a.
  • the smaller attachment element portion 6c is angularly attached to the bigger attachment element portion 6b and is attached to the part 2 via a second constriction 6a.
  • the attachment elements 6 are specially designed structures, which are used to connect a heat sink volume element 5 or a mechanical support beam 4 with a part surface 2a or part edge 2b.
  • breaking point there is a pre-defined breaking point at the attachment element structure that allows an easy removal of the support structure (heat sink, grid structure) from the part 2.
  • the breaking points can be near the heat sink 5 or between the heat sink 5 and the part 2. As a result, after removal, the remaining material from the attachment element structure on the part surface 2a is as low as possible/thus reducing the finishing work needed.
  • the attachment structures already act as small heat sinks, able to take up more energy as a single, small wall or a small beam. Therefore, the attachment elements 6 need to be already a small volume element.
  • the number, shape, size and distribution of the attachment elements 6 on the part surfaces 2a are dependent on the orientation and the size of the part surfaces 2a or part edges 2b that need a support (angle to the horizontal).
  • the specially designed attachment structures can also be used to optimize the direct connection of the beams of the grid with the heat sink.
  • the laser parameters are adjusted for an easier removal from the base plate 3 and the part 2, respectively.
  • a pulsed laser beam with tailored parameters can be used to adjust the hardness of the material, the porosity and the resulting heat conductivity of the part structures 1.

Abstract

The invention provides a part structure (1) built by metal powder based added manufacturing, wherein a metal powder forming a metal powder bed resting on a base element (3) is selectively fused in a layer-by-layer fashion such as by selective laser melting, selective electron beam melting or selective ion beam melting. The part structure (1) comprises at least one individual part (2) and an auxiliary structure (4; 4, 5) attached to the at least one individual part (2) and to the base element (3). The auxiliary structure (4; 4, 5) is a grid-like structure comprising different types of grid elements including beam elements (4) and volume elements (5).

Description

Part structure built by metal powder based added manufacturing
The invention relates to a part structure built by metal powder based added
manufacturing. In order to build such a part structure, a metal powder forming a metal powder bed resting on a base element is selectively fused in a layer-by-layer fashion such as by selective laser melting, selective electron beam melting or selective ion beam melting. The resulting part structure comprises at least one individual part and an auxiliary structure attached to the at least one individual part and to the base element.
Background of the invention
Several additive manufacturing processes, such as Selective Laser Melting, Electron Beam Melting, Stereolithography, etc., need support structures in order to support the parts produced. There are different technical reasons for support structures, two important ones being:
• Mechanical support:
Stable positioning of the parts to be produced during the build process. This is of particular relevance for overhanging surfaces of a part to be produced.
• Heat sink:
Thermal processes (Selective Laser Melting, Electron Beam Melting) use a high energy beam in order to melt the raw material (powders). In order to guarantee a stable build process, the thermal energy has to flow away from the created melt-pool. Therefore, the support structure can act as a thermal heat sink, taking up this amount of energy.
Current support strategies, such as disclosed in US 5'595703, typically build only vertical support elements, such as thin walls, small volume elements, etc. In this way, the support structures may be standing on structures of the part itself. The removal of these support structures requires finishing operations of the upface-surfaces where the support structures are standing on the part. The single elements of existing volume support structures, as disclosed in US 5'595703, typically have the same cross section over nearly the whole height.
Summary of the invention
It is an object of the present invention to provide a part structure built by metal powder based added manufacturing, which part structure allows both efficient mechanical support of overhanging surfaces and efficient removal of heat during the build process.
To this end, the invention provides a part structure built by metal powder based added manufacturing, wherein a metal powder forming a metal powder bed resting on a base element is selectively fused in a layer-by-layer fashion such as by selective laser melting, selective electron beam melting or selective ion beam melting, and wherein the part structure comprises at least one individual part and an auxiliary structure attached to the at least one individual part and to the base element.
According to the invention, this auxiliary structure is a grid-like structure comprising different types of grid elements including beam elements and volume elements.
Preferably, the beam elements include beam elements differing in beam length and in beam cross section.
Preferably, at least some of said beam elements are arranged in a tree-like fashion forming a tree-like portion of the grid-like structure.
In a particularly preferred embodiment, the part structure comprises attachment elements arranged between the at least one individual part and the auxiliary structure and/or arranged between the base element and the auxiliary structure.
Preferably, the attachment elements comprise pre-defined breaking points.
Preferably, the volume elements within the auxiliary structure are located adjacent to the at least one individual part. In another preferred embodiment, attachment elements, preferably only attachment elements, are arranged between the at least one individual part and the auxiliary structure.
In yet another preferred embodiment, the density of grid-elements in the grid-like structure increases as one approaches the at least one individual part and, preferably, is greatest adjacent to the at least one individual part.
Preferably, the beam element diameter is less than 4 mm, the lower limit of the beam element diameter being determined by the metal type and particle size of the powder. The beam element may be a hollow, tube-like element and, preferably, may have a wall thickness of less than 45% of the beam element diameter, the lower limit of the wall thickness again being determined by the metal type and particle size of the powder. The cross-section of the beam elements may have a circular or polygonal shape.
In further preferred embodiment, the attachment elements comprise constrictions and/or porous regions pre-defining the breaking points.
Preferably, an angle formed between a part surface of the at least one individual part and the horizontal is between 0 and 60°. Preferably, the beam elements in the gridlike structure are arranged at angles greater than 45° to the horizontal.
Preferably, the above mentioned different types of grid-elements are arranged as a mechanical support and heat removal structure between an overhanging part surface and the horizontal.
The following technical and economical results are achieved by the part structure of the invention:
Technical results:
The support structures (auxiliary structures) act as a thermal sink for the surfaces that have to be built.
This result is achieved by the volume support structures in contrast to e.g. fine walls. The support structures are able to support different structural elements of a physical part. These elements can be classified as:
- Overhanging surfaces with an angle to the horizontal of 0° up to « 40°.
- Surfaces with an angle to the horizontal in the range of « 40° up to about 50°.
- Part edges with an angle to the horizontal of 0° up to « 60°.
- Internal holes with an axis to the horizontal in the range of 0° up to « 50° and diameters above * 5mm.
Easy removal of support structures is achieved by the attachment elements to the part and the base plate, respectively, being fine enough to be broken away manually. This is achieved by the special design of the attachment elements with predetermined breaking points.
In order to optimise the removal of the support structures from the base plate and the parts, the laser, during the build process, can be operated in continuous wave mode or in pulse mode. By adapting the pulse parameters (mean energy, pulse energy, pulse shape, frequency) the material parameters (hardness, density, heat
conductivity) can be designed according to the needs.
Economical results:
Easy removal of the part structure (part together auxiliary structure) from the base plate.
Easy removal of the support structures (auxiliary structures) from the part.
Few remaining structures of the original support on the parts / surfaces.
As far as possible, no support structures standing on upward facing surfaces
Good surface qualities.
Low volume of the support structures, thus minimising build time.
Brief description of the drawings
Fig. 1 indicates the situation of total energy introduced into the part structure and different types of energy flows within and out of the part structure.
Fig. 2 is a side view showing a first example of a part structure according to the invention. Fig. 3 is a side view showing a second example of a part structure according to the invention.
Fig. 4 is a side view showing a third example of a part structure according to the invention.
Fig. 5 is a perspective view showing a fourth example of a part structure according to the invention.
Fig. 6 is a side view showing a fifth example of a part structure according to the invention.
Fig. 7 is a side view showing a sixth example of a part structure according to the invention.
Fig. 8 is a side view showing a first detail of a part structure according to the invention.
Fig. 9 is a side view showing a second detail of a part structure according to the invention.
Detailed description of preferred embodiments of the invention
Preferably, volume elements serving as additional thermal heat sinks near the part surfaces / part structures are built ("part-near volume element"). The use of additional heat sinks (in addition to the heat sink function of the part being built) is optional, as for several types of part surfaces or part structures the supporting effect of grid-like structures itself can be sufficient.
The sizes of such part-near volume elements acting as heat sinks depend on the type, the orientation and the size of the part structures that need a support.
Relevant criteria for the design of the volume elements are the type of the part structures that need a support (part surfaces and edges with an angle to the horizontal, holes), the angle to the horizontal of the part structures or part surfaces, and the size of the part structures.
The design and the size of the part-near volume elements and support structures as well as their distances to the part could be estimated and optimized by the space- resolved solution of the heat equation.
Referring to the situation illustrated Fig. 1, we can write the following equation:
Q|_aser = QRadiation + Qpart + Qpowder + QlHeat sink + Qsupport structure
However, for practical reasons, standard design rules for the heat sinks for the different situations and part structures can be defined.
The heat sink structures can be described by several structural parameters, defining the shape / type of the heat sink, the size and the volume of the heat sink, or the distance of the heat sink to the part surface.
Thermal heat sinks can also be used for the stacking of parts. In this case, above an already built part, a horizontal volume plate is built, defining a new base plate for the more highly positioned next part, as shown in Fig. 7.
Below the heat sink, a tree-like grid structure holding the heat sink in place in the case where additional heat sinks are used, as shown in Figs. 2 and 5. This tree-like grid structure may also directly support part surfaces or part structures at regularly spaced or evenly distributed locations using specially designed attachment points, as shown in Fig. 4.
The size, shape and distribution of the single grid elements as well as the overall grid structure can be designed according to the need for a fast cooling down of the surface-near volume after scanning.
The grid-structure itself may consist of different types of grid-elements having different sizes / volumes. The grid shows - starting from the base plate - an evolutionary development regarding the shape, design and density of the beams, defining a tree-like grid structure, as shown in Fig 3.
The grid elements are standing only on the base plate and do not touch any part surface.
Exceptions:
Holes through the part with an angle to the horizontal of the axis < «45° and with a diameter > critical hole diameter, typically «7mm.
In the case where several parts are built upon another part, it may be necessary to use grid-structures standing on another part surface (stacking of parts), as shown in Figs. 6 and 7.
The density of the grid elements (beams) may change depending on the location within the grid. The closer to the part surface the narrower is the grid.
The shape of the beams can be a tube with a diameter <= 5 mm and a wall thickness starting from the smallest possible wall thickness up to 50% of the tube diameter (reaching a full cylinder), or a beam with polygonal cross-section with >= 3 edges, implemented as a tube or as a filled beam.
The support structures, consisting of volume- and grid-elements, can be built under different angles to the horizontal and are designed with respect to the technical requirements and restrictions of the build process (e.g. SLM). Typically, the angle to the horizontal of the structures will be > ¾45°.
The support structures can start to support the part structures at a specific height form the base plate, where the starting height depends on the orientation of the part surfaces that need a support.
Figs. 2 to 7 show some possible part structures built by metal powder based added manufacturing according to the invention. Fig. 2 is a side view showing a first example of a part structure 1 according to the invention. The part structure 1 comprises a part 2 with an overhanging part surface 2a, a grid-like auxiliary structure 4, 5 and attachment elements 6. The grid-like auxiliary structure 4, 5 comprises beam elements 4 of different lengths and volume elements 5 attached to them. The part 2 and the beam elements 4 are supported by and attached to a base plate 3. The volume elements 5 are attached to the beam elements 4 and to a part surface 2a of the part 2. Thus, part 2 is partially supported directly by the base element 3 and partially supported indirectly by the base element 3 via the grid-like auxiliary structure 4, 5.
The part surface 2a forms an angle of about 40° with respect to the horizontal plane H (base plate plane), thus constituting an overhanging part 2 with an auxiliary structure 4, 5 between the overhanging part surface 2a and the base plate 3. In addition to providing mechanical support for the overhanging part 2, the auxiliary structure 4, 5 provides conductive connections / pathways by its beam elements 4 for removing heat from the part 2 on the one hand and heat sinks by its volume elements 5 for receiving some of the heat removed from the part 2.
The beam elements 4 have different lengths and may be hollow, tube-like elements. Most of the beam elements extend along directions different from the vertical direction V. In contrast, the volume elements 5 are solid and may have different sizes. Each of the volume elements 5 has a large surface facing the part surface 2 and narrows towards an opposite end where the volume element 5 is attached to a beam element 4. The large surface of the volume element 5 is attached to the part surface 2a of the part 2 via a plurality of attachment elements 6. The narrow opposite end of the volume element 5 is attached to the beam element 4 via an attachment element 6.
The overhanging part surface 2a is support-free up to a height h form the horizontal plane H. Beyond that support-free height, the part 2 is mechanically supported and provided with an additional strong heat sink by the grid-like auxiliary structure 4, 5.
Fig. 3 is a side view showing a second example of a part structure 1 according to the invention. The part structure 1 comprises a part 2 with two overhanging part surfaces 2a, and a tree-like auxiliary structure 4 and attachment elements 6. The tree-like auxiliary structure 4 comprises only beam elements 4 of different lengths. In addition, volume elements 5 (see Fig. 2) could be included in the tree-like structure 4 in a manner similar to the example shown in Fig. 2. Only the beam elements 4 are supported by and attached to the base plate 3. Thus, part 2 is only supported indirectly by the base element 3 via the tree-like auxiliary structure 4.
Fig. 4 is a side view showing a third example of a part structure 1 according to the invention. This part structure 1 is similar to the part structure 1 shown in Fig. 2. The part structure 1 comprises a part 2 with an overhanging part surface 2a, a tree-like auxiliary structure 4 and attachment elements 6. The tree-like auxiliary structure 4 comprises only beam elements 4 of different lengths. The part 2 and the beam elements 4 are supported by and attached to the base plate 3. In addition, the beam elements 4 are attached to the part surface 2a of the part 2. Thus, part 2 is partially supported directly by the base element 3 and partially supported indirectly by the base element 3 via the tree-like auxiliary structure 4.
Again, as in Fig. 2, the overhanging part surface 2a is support-free up to a height h form the horizontal plane H. Beyond that support-free height, the part 2 is
mechanically supported and provided with an additional moderately strong heat sink by the tree-like auxiliary structure 4.
Fig. 5 is a perspective view showing a fourth example of a part structure 1 according to the invention. This part structure 1 is similar to the part structure 1 shown in Fig. 2. The part structure 1 comprises a part 2 with an overhanging part surface 2a, a gridlike auxiliary structure 4, 5 and attachment elements 6. The grid-like auxiliary structure 4, 5 comprises beam elements 4 of different lengths and one volume element 5 attached to them. The part 2 and the beam elements 4 are supported by and attached to a base plate 3. The volume element 5 is attached to the beam elements 4 and to a part edge 2b delimiting the part surface 2a of the part 2. Thus, part 2 is partially supported directly by the base element 3 and partially supported indirectly by the base element 3 via the grid-like auxiliary structure 4, 5. Fig. 6 is a side view showing a fifth example of a part structure 1 according to the invention. This part structure 1 allows two parts 2 to be arranged in a vertically spaced relationship, i.e. the two parts 2 can be arranged one on top of the other.
Each of the two parts 2 is supported by a tree-like auxiliary structure 4 comprising only beam elements 4 in a manner similar to the one shown in Fig. 3. In addition, some beam elements 4 extending between the two parts 2 provide additional mechanical stability and a thermal pathway between the two parts 2. Thus, the lower one of the two parts 2 may serve as a heat sink for the upper one of the two parts 2.
Fig. 7 is a side view showing a sixth example of a part structure 1 according to the invention. This part structure 1 is similar to the part structure 1 of Fig. 6. Again, this part structure 1 allows two parts 2 to be arranged in a vertically spaced relationship, i.e. the two parts 2 can be arranged one on top of the other.
Each of the two parts 2 is supported by a tree-like auxiliary structure 4 comprising only beam elements 4 in a manner similar to the one shown in Fig. 3. In addition, a second base plate 3 extending horizontally between the two parts 2 provides additional mechanical stability and an additional heat sink. A lower group of beam elements 4 extend between the lower one of the two parts 2 and the second base plate 3, and an upper group of beam elements 4 extend between the upper one of the two parts 2 and the second base plate 3, thus contributing to the additional mechanical stability and providing a thermal pathway between the two parts 2. Thus, the second base plate 3 and the lower one of the two parts 2 may serve as a heat sink for the upper one of the two parts 2.
Fig. 8 is a side view showing a first detail of a part structure 1 according to the invention. Three types of attachment elements 6 extending between a part 2 and a heat sink 5 are shown. The first type of attachment element 6 is a tetrahedron-like or pyramid-like element with one constriction 6a at the narrowing top of the tetrahedron / pyramid. The second type of attachment element 6 is a double-tetrahedron-like or double-pyramid-like element again with one constriction 6a where the narrowing tops / ends of the tetrahedron / pyramid meet. The third type of attachment element 6 is a cylinder-like element. Instead of a constriction, it may have a porous region somewhere along its cylinder axis. Both the constrictions 6a and the porous region constitute pre-defined breaking points of the attachment elements 6.
Fig. 9 is a side view showing a second detail of a part structure according to the invention. An angled attachment element 6' is shown which comprises a first attachment element portion 6b and a second attachment element portion 6c. The bigger attachment element portion 6b is attached to the base plate 3 via a first constriction 6a. The smaller attachment element portion 6c is angularly attached to the bigger attachment element portion 6b and is attached to the part 2 via a second constriction 6a.
The attachment elements 6 are specially designed structures, which are used to connect a heat sink volume element 5 or a mechanical support beam 4 with a part surface 2a or part edge 2b.
They are designed with regard to the following aspects:
There is a pre-defined breaking point at the attachment element structure that allows an easy removal of the support structure (heat sink, grid structure) from the part 2. The breaking points can be near the heat sink 5 or between the heat sink 5 and the part 2. As a result, after removal, the remaining material from the attachment element structure on the part surface 2a is as low as possible/thus reducing the finishing work needed.
The attachment structures already act as small heat sinks, able to take up more energy as a single, small wall or a small beam. Therefore, the attachment elements 6 need to be already a small volume element.
The number, shape, size and distribution of the attachment elements 6 on the part surfaces 2a are dependent on the orientation and the size of the part surfaces 2a or part edges 2b that need a support (angle to the horizontal).
The specially designed attachment structures can also be used to optimize the direct connection of the beams of the grid with the heat sink.
In the above part structures 1 , the laser parameters are adjusted for an easier removal from the base plate 3 and the part 2, respectively. Especially a pulsed laser beam with tailored parameters (frequency, pulse energy, pulse shape, mean power) can be used to adjust the hardness of the material, the porosity and the resulting heat conductivity of the part structures 1.

Claims

Claims
1. A part structure (1 ) built by metal powder based added manufacturing, wherein a metal powder forming a metal powder bed resting on a base element (3) is selectively fused in a layer-by-layer fashion such as by selective laser melting, selective electron beam melting or selective ion beam melting, said part structure (1 ) comprising at least one individual part (2) and an auxiliary structure (4; 4, 5) attached to the at least one individual part (2) and to the base element (3), characterized in that said auxiliary structure (4; 4, 5) is a grid-like structure comprising different types of grid elements including beam elements (4) and volume elements (5).
2. The part structure according to claim 1 , characterized in that said beam elements (4) include beam elements differing in beam length and in beam cross section.
3. The part structure according to claim 2, characterized in that at least some of said beam elements (4) are arranged in a tree-like fashion forming a tree-like portion of said grid-like structure.
4. The part structure according to any one of claims 1 to 3, characterized in that it comprises attachment elements (6) arranged between said at least one individual part (2) and said auxiliary structure (4; 4, 5) and/or arranged between said base element (3) and said auxiliary structure (4; 4, 5).
5. The part structure according to claim 4, characterized in that the attachment elements (6) comprise pre-defined breaking points.
6. The part structure according to any one of claims 1 to 5, characterized in that the volume elements (5) within said auxiliary structure (4, 5) are located adjacent to said at least one individual part (2).
7. The part structure according to claim 6, characterized in that attachment elements (6), preferably only attachment elements, are arranged between said at least one individual part (2) and said auxiliary structure (4, 5).
8. The part structure according to any one of claims 1 to 7, characterized in that the density of grid-elements in said grid-like structure increases as one approaches the at least one individual part (2) and, preferably, is greatest adjacent to said at least one individual part (2).
9. The part structure according to any one of claims 1 to 8, characterized in that the beam element (4) diameter is less than 4 mm.
10. The part structure according to any one of claims 1 to 9, characterized in that the beam element (4) is a hollow, tube-like element and, preferably, has a wall thickness of less than 45% of the beam element diameter.
11. The part structure according to any one of claims 1 to 10, characterized in that the cross-section of the beam elements (4) has a circular or polygonal shape.
12. The part structure according to any one of claims 5 to 11 , characterized in that the attachment elements (6; 6') comprise constrictions (6a) and/or porous regions pre-defining said breaking points.
13. The part structure according to any one of claims 1 to 12, characterized in that an angle formed between a part surface (2a) of the at least one individual part (2) and the horizontal plane (H) is between 0 and 60°.
14. The part structure according to any one of claims 1 to 13, characterized in that the beam elements (4) in the grid-like structure are arranged at angles greater than 45° to the horizontal plane (H).
15. The part structure according to any one of claims 1 to 14, characterized in that said different types of grid-elements are arranged as a mechanical support and heat removal structure between an overhanging part surface (2a) of the at least one part (2) and the horizontal plane (H).
PCT/IB2012/000636 2011-03-29 2012-03-29 Part structure built by metal powder based added manufacturing WO2012131481A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201161516046P 2011-03-29 2011-03-29
US61/516,046 2011-03-29

Publications (1)

Publication Number Publication Date
WO2012131481A1 true WO2012131481A1 (en) 2012-10-04

Family

ID=46147513

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/IB2012/000636 WO2012131481A1 (en) 2011-03-29 2012-03-29 Part structure built by metal powder based added manufacturing

Country Status (1)

Country Link
WO (1) WO2012131481A1 (en)

Cited By (46)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014124971A1 (en) * 2013-02-15 2014-08-21 Compagnie Generale Des Etablissements Michelin Part obtained by selective melting of a powder comprising a main element and rigid secondary elements
WO2014124969A1 (en) * 2013-02-15 2014-08-21 Compagnie Generale Des Etablissements Michelin Part obtained by selective melting of a powder comprising a main element and rigid secondary elements
GB2515287A (en) * 2013-06-17 2014-12-24 Rolls Royce Plc An Additive Layer Manufacturing Method
WO2015040410A3 (en) * 2013-09-19 2015-05-14 3T Rpd Limited Additive manufacturing method
WO2015106193A1 (en) * 2014-01-13 2015-07-16 Kevin Engel Additive metal deposition process
DE102014101148A1 (en) * 2014-01-30 2015-07-30 Airbus Operations Gmbh Method for producing a fluid-carrying component by layered construction
EP2910362A1 (en) * 2014-02-25 2015-08-26 Siemens Aktiengesellschaft Powder bed based additive manufacturing method, in which a support structure is used to produce the component
US20160059437A1 (en) * 2014-08-29 2016-03-03 General Electric Company Article and process for producing an article
EP3056302A1 (en) * 2015-02-12 2016-08-17 United Technologies Corporation Anti-deflection feature for additively manufactured thin metal parts and method of additively manufacturing thin metal parts
CN106041075A (en) * 2016-06-22 2016-10-26 西北工业大学 High-energy beam additive manufacturing method of suspended structures of metal part
EP3085519A1 (en) * 2015-04-22 2016-10-26 EOS GmbH Electro Optical Systems Method and device for generating a three-dimensional object
BE1023316B1 (en) * 2014-08-25 2017-02-02 Materialise Nv Systems and methods for optimizing contact points of tree-shaped supports in additive manufacturing
CN106475561A (en) * 2016-09-29 2017-03-08 首都航天机械公司 A kind of auxiliary support structure suitable for inclining pendency thin-wall construction
WO2017076983A1 (en) * 2015-11-06 2017-05-11 Compagnie Generale Des Etablissements Michelin Method for additive manufacturing of a part, in particular a lining element for a tyre mould, using powder
CN106671399A (en) * 2016-12-30 2017-05-17 湖南航天新材料技术研究院有限公司 Method for obtaining structural design parameters
WO2017118806A1 (en) * 2016-01-07 2017-07-13 Safran Aircraft Engines Method for manufacturing a workpiece by additive manufacturing
WO2017143005A1 (en) * 2016-02-16 2017-08-24 Arizona Board Of Regents On Behalf Of Arizona State University Fabricating metal or ceramic components using 3d printing with dissolvable supports of a different material
EP3159144A4 (en) * 2015-03-24 2018-02-28 Technology Research Association for Future Additive Manufacturing 3d printing system, method for producing 3d printed object, information processing device, method for generating heat-dissipating structure for 3d printed object, and program for generating heat-dissipating structure for 3d printed object
CN107856311A (en) * 2017-11-13 2018-03-30 成都优材科技有限公司 Tree-like supporting construction for 3D printing
EP3308880A1 (en) * 2016-10-13 2018-04-18 Siemens Aktiengesellschaft 3d printing method
US20180169756A1 (en) * 2016-12-20 2018-06-21 General Electric Company Self-breaking support for additive manufacturing
DE102017200152A1 (en) * 2017-01-09 2018-07-12 Ford Global Technologies, Llc Additive manufacturing process
JP2018523008A (en) * 2015-11-16 2018-08-16 ツェーエル・シュッツレヒツフェアヴァルトゥングス・ゲゼルシャフト・ミト・べシュレンクテル・ハフツング Method for manufacturing a support structure for supporting a three-dimensional object to be formed
DE102017113485A1 (en) * 2017-06-20 2018-12-20 Amsis Gmbh Method for the additive production of at least one component, support structure or element of a support structure, component with the same and installation for carrying out such a method
US20190015923A1 (en) * 2017-07-11 2019-01-17 United Technologies Corporation Additively manufactured article including electrically removable supports
CN109501249A (en) * 2018-12-11 2019-03-22 西安国宏天易智能科技有限公司 A kind of variable cross-section aperture grid support construction and its generation method
DE102017126537A1 (en) * 2017-11-13 2019-05-16 SLM Solutions Group AG Method for producing a semifinished product and a workpiece
CN110435155A (en) * 2019-08-25 2019-11-12 上海漫格科技有限公司 A kind of automatic direction optimization method of corona model based on 3 D-printing
US20200086580A1 (en) * 2018-09-18 2020-03-19 General Electric Company Support Structures for Additively-Manufactured Components and Methods of Securing a Component to a Build Platform During Additive Manufacturing
CN110893464A (en) * 2018-09-12 2020-03-20 戴弗根特技术有限公司 Alternative support in additive manufacturing
US10731565B2 (en) 2016-12-20 2020-08-04 General Electric Company Additive manufactured object with self-breaking support with fluid passage
EP3689501A1 (en) 2019-01-31 2020-08-05 CSEM Centre Suisse D'electronique Et De Microtechnique SA Method for manufacturing a device by implementation of an additive manufacturing process requiring no sacrifical support structure
CN111633207A (en) * 2020-04-27 2020-09-08 鑫精合激光科技发展(北京)有限公司 Heat dissipation device and application thereof
DE102019209020A1 (en) * 2019-06-21 2020-12-24 Siemens Aktiengesellschaft Support structure, computer program product and method for removing the support structure
CN112188941A (en) * 2018-05-25 2021-01-05 通用电气公司 Method for controlling additive manufacturing component by using laser incidence angle
US11072114B2 (en) 2015-10-30 2021-07-27 Seurat Technologies, Inc. Variable print chamber walls for powder bed fusion additive manufacturing
US11077664B2 (en) 2017-05-17 2021-08-03 Arizona Board Of Regents On Behalf Of Arizona State University Systems and methods for controlling the morphology and porosity of printed reactive inks for high precision printing
WO2021160323A1 (en) * 2020-02-10 2021-08-19 Siemens Aktiengesellschaft Strategy for separating components in additive manufacturing
DE102020118094A1 (en) 2020-07-09 2022-01-13 Lixil Corporation Process for manufacturing a workpiece
CN113976916A (en) * 2021-11-02 2022-01-28 深圳市华阳新材料科技有限公司 Supporting structure for 3D printing
EP4008458A1 (en) * 2020-12-01 2022-06-08 Raytheon Technologies Corporation Erodible support structure for additively manufactured article and process therefor
WO2022146647A1 (en) * 2020-12-29 2022-07-07 3D Systems, Inc. Branching support for metals that minimizes material usage
DE102021110038A1 (en) 2021-04-21 2022-10-27 Bayerische Motoren Werke Aktiengesellschaft Process for the additive manufacturing of at least one three-dimensional object
AT524995A1 (en) * 2021-05-07 2022-11-15 Gerald Resch Ing Method and device for removing support structures from an object, as well as method for manufacturing an object by additive manufacturing
US11504770B2 (en) 2016-07-15 2022-11-22 Arizona Board Of Regents On Behalf Of Arizona State University Dissolving metal supports in 3D printed metals and ceramics using sensitization
WO2023098930A1 (en) * 2021-11-30 2023-06-08 Vysoké Učení Technické V Brně A structure for attenuation of mechanical waves and a method of manufacturing a structure

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5595703A (en) * 1994-03-10 1997-01-21 Materialise, Naamloze Vennootschap Method for supporting an object made by means of stereolithography or another rapid prototype production method
US6193923B1 (en) * 1995-09-27 2001-02-27 3D Systems, Inc. Selective deposition modeling method and apparatus for forming three-dimensional objects and supports
EP2022622A1 (en) * 2007-08-10 2009-02-11 Rolls-Royce plc Support architecture
US20090072447A1 (en) * 2007-09-17 2009-03-19 3D Systems, Inc. Region-Based Supports for Parts Produced by Solid Freeform Fabrication
GB2458745A (en) * 2008-02-13 2009-10-07 Materials Solutions Grooved support for selective sintering or melting process

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5595703A (en) * 1994-03-10 1997-01-21 Materialise, Naamloze Vennootschap Method for supporting an object made by means of stereolithography or another rapid prototype production method
US6193923B1 (en) * 1995-09-27 2001-02-27 3D Systems, Inc. Selective deposition modeling method and apparatus for forming three-dimensional objects and supports
EP2022622A1 (en) * 2007-08-10 2009-02-11 Rolls-Royce plc Support architecture
US20090072447A1 (en) * 2007-09-17 2009-03-19 3D Systems, Inc. Region-Based Supports for Parts Produced by Solid Freeform Fabrication
GB2458745A (en) * 2008-02-13 2009-10-07 Materials Solutions Grooved support for selective sintering or melting process

Non-Patent Citations (6)

* Cited by examiner, † Cited by third party
Title
A.B. SPIERINGS: "Generative Verfahren bieten neue Chancen", SONDERDRUCK AUS TECHNISCHE RUNDSCHAU 2009, no. 12, 2009, XP002679183, Retrieved from the Internet <URL:www.inspire.ethz.ch/ConfiguratorJM/press/Generative_129785567873202/Spierings_2009_Generative_Verfahren_bieten_neue_Chancen.pdf> [retrieved on 20120704] *
J.-P. KRUTH, B. VANDENBROUCKE, J. VAN VAERENBERGH, P. MERCELIS: "BENCHMARKING OF DIFFERENT SLS/SLM PROCESSES AS RAPID MANUFACTURING TECHNIQUES", PROC. INT. CONF. POLYMERS & MOULDS, 2005, pages 1 - 7, XP002679185 *
O. REHME, C. EMMELMANN: "Rapid manufacturing of lattice structures with Selective Laser Melting", PROC. OF SPIE, vol. 6107, 2006, XP002679184 *
ROCHUS ET AL: "New applications of rapid prototyping and rapid manufacturing (RP/RM) technologies for space instrumentation", ACTA ASTRONAUTICA, PERGAMON PRESS, ELMSFORD, GB, vol. 61, no. 1-6, 14 May 2007 (2007-05-14), pages 352 - 359, XP022078096, ISSN: 0094-5765, DOI: 10.1016/J.ACTAASTRO.2007.01.004 *
SANTOS E C ET AL: "Rapid manufacturing of metal components by laser forming", INTERNATIONAL JOURNAL OF MACHINE TOOLS AND MANUFACTURE, ELSEVIER, US, vol. 46, no. 12-13, 1 October 2006 (2006-10-01), pages 1459 - 1468, XP024902437, ISSN: 0890-6955, [retrieved on 20061001], DOI: 10.1016/J.IJMACHTOOLS.2005.09.005 *
SPIERINGS A ET AL: "Mit mehr Moeglichkeiten schneller ans Ziel", TECHNISCHE RUNDSCHAU, HALLWAG AG, CH, vol. 100, no. 4, 15 February 2008 (2008-02-15), pages 32 - 34, XP001510206, ISSN: 1023-0823 *

Cited By (85)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105073309A (en) * 2013-02-15 2015-11-18 米其林企业总公司 Part obtained by selective melting of a powder comprising a main element and rigid secondary elements
WO2014124969A1 (en) * 2013-02-15 2014-08-21 Compagnie Generale Des Etablissements Michelin Part obtained by selective melting of a powder comprising a main element and rigid secondary elements
FR3002167A1 (en) * 2013-02-15 2014-08-22 Michelin & Cie PIECE OBTAINED BY SELECTIVE FUSION OF A POWDER COMPRISING A MAIN ELEMENT AND RIGID SECONDARY ELEMENTS
FR3002168A1 (en) * 2013-02-15 2014-08-22 Michelin & Cie PIECE OBTAINED BY SELECTIVE FUSION OF A POWDER COMPRISING A MAIN ELEMENT AND RIGID SECONDARY ELEMENTS
WO2014124971A1 (en) * 2013-02-15 2014-08-21 Compagnie Generale Des Etablissements Michelin Part obtained by selective melting of a powder comprising a main element and rigid secondary elements
US10307979B2 (en) 2013-02-15 2019-06-04 Compagnie Generale Des Etablissements Michelin Part obtained by selective melting of a powder comprising a main element and rigid secondary elements
CN105073309B (en) * 2013-02-15 2019-10-29 米其林企业总公司 By carrying out the component that selectivity melting obtains to the powder for including main element and rigid auxiliary element
US10583481B2 (en) 2013-02-15 2020-03-10 Compagnie Generale Des Etablissements Michelin Part obtained by selective melting of a powder comprising a main element and rigid secondary elements
GB2515287A (en) * 2013-06-17 2014-12-24 Rolls Royce Plc An Additive Layer Manufacturing Method
WO2015040410A3 (en) * 2013-09-19 2015-05-14 3T Rpd Limited Additive manufacturing method
GB2520596A (en) * 2013-09-19 2015-05-27 3T Rpd Ltd Manufacturing method
GB2520596B (en) * 2013-09-19 2018-08-15 3T Rpd Ltd Manufacturing method
US10941495B2 (en) 2014-01-13 2021-03-09 Incodema3D, LLC Additive metal deposition process
WO2015106193A1 (en) * 2014-01-13 2015-07-16 Kevin Engel Additive metal deposition process
US9920433B2 (en) 2014-01-13 2018-03-20 Incodema3D, LLC Additive metal deposition process
DE102014101148A1 (en) * 2014-01-30 2015-07-30 Airbus Operations Gmbh Method for producing a fluid-carrying component by layered construction
DE102014203386A1 (en) * 2014-02-25 2015-08-27 Siemens Aktiengesellschaft Powder bed-based additive manufacturing process, in which a support structure is used for the production of the component
EP2910362A1 (en) * 2014-02-25 2015-08-26 Siemens Aktiengesellschaft Powder bed based additive manufacturing method, in which a support structure is used to produce the component
BE1023316B1 (en) * 2014-08-25 2017-02-02 Materialise Nv Systems and methods for optimizing contact points of tree-shaped supports in additive manufacturing
US20160059437A1 (en) * 2014-08-29 2016-03-03 General Electric Company Article and process for producing an article
US9796048B2 (en) * 2014-08-29 2017-10-24 General Electric Company Article and process for producing an article
EP3056302A1 (en) * 2015-02-12 2016-08-17 United Technologies Corporation Anti-deflection feature for additively manufactured thin metal parts and method of additively manufacturing thin metal parts
US10094240B2 (en) 2015-02-12 2018-10-09 United Technologies Corporation Anti-deflection feature for additively manufactured thin metal parts and method of additively manufacturing thin metal parts
EP3159144A4 (en) * 2015-03-24 2018-02-28 Technology Research Association for Future Additive Manufacturing 3d printing system, method for producing 3d printed object, information processing device, method for generating heat-dissipating structure for 3d printed object, and program for generating heat-dissipating structure for 3d printed object
DE102015207306A1 (en) * 2015-04-22 2016-10-27 Eos Gmbh Electro Optical Systems Method and device for producing a three-dimensional object
EP3085519A1 (en) * 2015-04-22 2016-10-26 EOS GmbH Electro Optical Systems Method and device for generating a three-dimensional object
US11691341B2 (en) 2015-10-30 2023-07-04 Seurat Technologies, Inc. Part manipulation using printed manipulation points
US11072114B2 (en) 2015-10-30 2021-07-27 Seurat Technologies, Inc. Variable print chamber walls for powder bed fusion additive manufacturing
WO2017076983A1 (en) * 2015-11-06 2017-05-11 Compagnie Generale Des Etablissements Michelin Method for additive manufacturing of a part, in particular a lining element for a tyre mould, using powder
US11077610B2 (en) 2015-11-06 2021-08-03 Compagnie Generale Des Etablissements Michelin Method for powder-based additive manufacturing of a part, in particular a lining element for a tire mould
CN108349003A (en) * 2015-11-06 2018-07-31 米其林企业总公司 Method for the liner element for using powder addition manufacture component, particularly tire-mold
FR3043347A1 (en) * 2015-11-06 2017-05-12 Michelin & Cie PROCESS FOR THE ADDITIVE MANUFACTURE OF A POWDER OF A WORKPIECE, IN PARTICULAR A TRIM MEMBER FOR A PNEUMATIC MOLD
JP2018523008A (en) * 2015-11-16 2018-08-16 ツェーエル・シュッツレヒツフェアヴァルトゥングス・ゲゼルシャフト・ミト・べシュレンクテル・ハフツング Method for manufacturing a support structure for supporting a three-dimensional object to be formed
WO2017118806A1 (en) * 2016-01-07 2017-07-13 Safran Aircraft Engines Method for manufacturing a workpiece by additive manufacturing
US11186034B2 (en) 2016-01-07 2021-11-30 Safran Aircraft Engines Method of fabricating a part by additive manufacturing
FR3046556A1 (en) * 2016-01-07 2017-07-14 Snecma METHOD FOR MANUFACTURING PIECE BY ADDITIVE MANUFACTURING
US11673289B2 (en) 2016-02-16 2023-06-13 Arizona Board Of Regents On Behalf Of Arizona State University Fabricating metal or ceramic components using 3D printing with dissolvable supports of a different material
WO2017143005A1 (en) * 2016-02-16 2017-08-24 Arizona Board Of Regents On Behalf Of Arizona State University Fabricating metal or ceramic components using 3d printing with dissolvable supports of a different material
CN106041075A (en) * 2016-06-22 2016-10-26 西北工业大学 High-energy beam additive manufacturing method of suspended structures of metal part
US11504770B2 (en) 2016-07-15 2022-11-22 Arizona Board Of Regents On Behalf Of Arizona State University Dissolving metal supports in 3D printed metals and ceramics using sensitization
CN106475561B (en) * 2016-09-29 2018-11-23 首都航天机械公司 A kind of auxiliary support structure suitable for tilting pendency thin-wall construction
CN106475561A (en) * 2016-09-29 2017-03-08 首都航天机械公司 A kind of auxiliary support structure suitable for inclining pendency thin-wall construction
WO2018069118A1 (en) * 2016-10-13 2018-04-19 Siemens Aktiengesellschaft 3d printing process
CN109843482A (en) * 2016-10-13 2019-06-04 弗兰德有限公司 3D printing method
CN109843482B (en) * 2016-10-13 2021-10-19 弗兰德有限公司 3D printing method
EP3308880A1 (en) * 2016-10-13 2018-04-18 Siemens Aktiengesellschaft 3d printing method
US20180169756A1 (en) * 2016-12-20 2018-06-21 General Electric Company Self-breaking support for additive manufacturing
US10731565B2 (en) 2016-12-20 2020-08-04 General Electric Company Additive manufactured object with self-breaking support with fluid passage
CN106671399A (en) * 2016-12-30 2017-05-17 湖南航天新材料技术研究院有限公司 Method for obtaining structural design parameters
DE102017200152A1 (en) * 2017-01-09 2018-07-12 Ford Global Technologies, Llc Additive manufacturing process
US11077664B2 (en) 2017-05-17 2021-08-03 Arizona Board Of Regents On Behalf Of Arizona State University Systems and methods for controlling the morphology and porosity of printed reactive inks for high precision printing
WO2018233866A1 (en) * 2017-06-20 2018-12-27 Amsis Gmbh Method for the additive manufacturing of at least one component, supporting structure or element of a supporting structure, component with the same and installation for carrying out such a method
DE102017113485A1 (en) * 2017-06-20 2018-12-20 Amsis Gmbh Method for the additive production of at least one component, support structure or element of a support structure, component with the same and installation for carrying out such a method
US20190015923A1 (en) * 2017-07-11 2019-01-17 United Technologies Corporation Additively manufactured article including electrically removable supports
DE102017126537A1 (en) * 2017-11-13 2019-05-16 SLM Solutions Group AG Method for producing a semifinished product and a workpiece
CN107856311A (en) * 2017-11-13 2018-03-30 成都优材科技有限公司 Tree-like supporting construction for 3D printing
US11123798B2 (en) 2017-11-13 2021-09-21 SLM Solutions Group AG Method for manufacturing a semi-finished product and a workpiece
CN112188941A (en) * 2018-05-25 2021-01-05 通用电气公司 Method for controlling additive manufacturing component by using laser incidence angle
CN112188941B (en) * 2018-05-25 2023-05-26 通用电气公司 Method for additive manufacturing of a component using laser incidence angle control
US11826953B2 (en) 2018-09-12 2023-11-28 Divergent Technologies, Inc. Surrogate supports in additive manufacturing
EP3849786A4 (en) * 2018-09-12 2022-05-25 Divergent Technologies, Inc. Surrogate supports in additive manufacturing
CN110893464A (en) * 2018-09-12 2020-03-20 戴弗根特技术有限公司 Alternative support in additive manufacturing
WO2020061155A1 (en) * 2018-09-18 2020-03-26 General Electric Company Support structures for additively-manufactured components and methods of securing a component to a build platform during additive manufacturing
US20200086580A1 (en) * 2018-09-18 2020-03-19 General Electric Company Support Structures for Additively-Manufactured Components and Methods of Securing a Component to a Build Platform During Additive Manufacturing
CN112770857A (en) * 2018-09-18 2021-05-07 通用电气公司 Support structure for an additively manufactured component and method of securing a component to a build platform during additive manufacturing
US10967580B2 (en) 2018-09-18 2021-04-06 General Electric Company Support structures for additively-manufactured components and methods of securing a component to a build platform during additive manufacturing
US11472123B2 (en) 2018-09-18 2022-10-18 General Electric Company Support structures for additively-manufactured components
CN109501249A (en) * 2018-12-11 2019-03-22 西安国宏天易智能科技有限公司 A kind of variable cross-section aperture grid support construction and its generation method
CN109501249B (en) * 2018-12-11 2024-02-23 西安国宏天易智能科技有限公司 Variable-section open-pore grid supporting structure and generation method thereof
EP3689501A1 (en) 2019-01-31 2020-08-05 CSEM Centre Suisse D'electronique Et De Microtechnique SA Method for manufacturing a device by implementation of an additive manufacturing process requiring no sacrifical support structure
DE102019209020A1 (en) * 2019-06-21 2020-12-24 Siemens Aktiengesellschaft Support structure, computer program product and method for removing the support structure
CN110435155A (en) * 2019-08-25 2019-11-12 上海漫格科技有限公司 A kind of automatic direction optimization method of corona model based on 3 D-printing
CN110435155B (en) * 2019-08-25 2021-05-04 上海漫格科技有限公司 Automatic direction optimization method of dental crown model based on three-dimensional printing
WO2021160323A1 (en) * 2020-02-10 2021-08-19 Siemens Aktiengesellschaft Strategy for separating components in additive manufacturing
CN111633207A (en) * 2020-04-27 2020-09-08 鑫精合激光科技发展(北京)有限公司 Heat dissipation device and application thereof
DE102020118094A1 (en) 2020-07-09 2022-01-13 Lixil Corporation Process for manufacturing a workpiece
US11685123B2 (en) 2020-12-01 2023-06-27 Raytheon Technologies Corporation Erodible support structure for additively manufactured article and process therefor
EP4008458A1 (en) * 2020-12-01 2022-06-08 Raytheon Technologies Corporation Erodible support structure for additively manufactured article and process therefor
WO2022146647A1 (en) * 2020-12-29 2022-07-07 3D Systems, Inc. Branching support for metals that minimizes material usage
DE102021110038A1 (en) 2021-04-21 2022-10-27 Bayerische Motoren Werke Aktiengesellschaft Process for the additive manufacturing of at least one three-dimensional object
AT524995B1 (en) * 2021-05-07 2022-12-15 Gerald Resch Ing Method and device for removing support structures from an object, as well as method for manufacturing an object by additive manufacturing
AT524995A1 (en) * 2021-05-07 2022-11-15 Gerald Resch Ing Method and device for removing support structures from an object, as well as method for manufacturing an object by additive manufacturing
CN113976916A (en) * 2021-11-02 2022-01-28 深圳市华阳新材料科技有限公司 Supporting structure for 3D printing
CN113976916B (en) * 2021-11-02 2024-03-15 深圳市华阳新材料科技有限公司 Supporting structure for 3D printing
WO2023098930A1 (en) * 2021-11-30 2023-06-08 Vysoké Učení Technické V Brně A structure for attenuation of mechanical waves and a method of manufacturing a structure

Similar Documents

Publication Publication Date Title
WO2012131481A1 (en) Part structure built by metal powder based added manufacturing
CN107210179B (en) It is configured for the 3D printing chamber element of lower membrane stress and more low operating temperature
US10307964B2 (en) Three-dimensional molding method
JP2010067615A (en) Plasma reactor
JP2020109859A (en) Method and apparatus for manufacturing thin semiconductor wafer having local control region thicker than other regions, and the wafer
EP3132221B1 (en) Enhanced boiling with selective placement of nucleation sites
CN104772463A (en) Metal additive manufacturing support structure and manufacturing method thereof
US20200332997A1 (en) Devices With An Enhanced Boiling Surface With Features Directing Bubble and Liquid Flow and Methods Thereof
CN105736273A (en) Magnetic circuit structure for Hall thruster with large height-diameter ratio
SE465191B (en) BRAENSLEPATRON CARRIES A CORE WATER TYPE REACTOR
US5357073A (en) Electrical discharge machine
TW201533555A (en) Microfluidic device
CN104134807B (en) A kind of alternate intercommunicating reticulated porous structures plate and manufacture method thereof and application
CN114054777B (en) Supporting structure of large cavity, 3D printing method and manufacturing method
CN108917395A (en) A kind of honeycomb sintering pan
CN108233155B (en) Solid laser cooling heat sink
US20200365374A1 (en) 3d printed chamber components configured for lower film stress and lower operating temperature
KR20150075747A (en) The cutting surface table
KR102483355B1 (en) Laser keyhole welding structure and laser keyhole welding method of aluminum materials
US11964438B1 (en) Three-dimensional molding method
RU2005105084A (en) ELECTRIC ARC GENERATOR OF SEPARATED PLASMA FLOWS OF METALS IN VACUUM
KR101633721B1 (en) Radio Frequency Antenna having vertical multiple pole structure
KR101595221B1 (en) Solid oxide fuel cell using metal support having array structure and method for manufacturing the same
KR101570275B1 (en) Punched grid for lead acid battery
CN105745361A (en) Method of making forming screens

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 12722828

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 12722828

Country of ref document: EP

Kind code of ref document: A1