Classifications

• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
  • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
  • B23P6/00—Restoring or reconditioning objects
  • B23P6/002—Repairing turbine components, e.g. moving or stationary blades, rotors
  • B23P6/007—Repairing turbine components, e.g. moving or stationary blades, rotors using only additive methods, e.g. build-up welding
• • 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
  • 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
  • B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
  • B22F5/04—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine blades
• • 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
  • B22F7/00—Manufacture 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
  • B22F7/06—Manufacture 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
  • B22F7/062—Manufacture 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
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
  • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
  • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
  • B23K26/02—Positioning or observing the workpiece, e.g. with respect to the point of impact; Aligning, aiming or focusing the laser beam
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
  • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
  • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
  • B23K26/08—Devices involving relative movement between laser beam and workpiece
  • B23K26/083—Devices involving movement of the workpiece in at least one axial direction
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
  • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
  • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
  • B23K26/08—Devices involving relative movement between laser beam and workpiece
  • B23K26/0869—Devices involving movement of the laser head in at least one axial direction
  • B23K26/0876—Devices involving movement of the laser head in at least one axial direction in at least two axial directions
  • B23K26/0884—Devices involving movement of the laser head in at least one axial direction in at least two axial directions in at least in three axial directions, e.g. manipulators, robots
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
  • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
  • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
  • B23K26/34—Laser welding for purposes other than joining
  • B23K26/342—Build-up welding
• • 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
  • 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
  • B22F7/00—Manufacture 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
  • B22F7/06—Manufacture 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
  • B22F7/062—Manufacture 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
  • B22F2007/068—Manufacture 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 repairing articles
• • 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
  • B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
  • B22F5/009—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine components other than turbine blades
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
  • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
  • B23K2101/00—Articles made by soldering, welding or cutting
  • B23K2101/001—Turbines
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
  • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
  • B23K2103/00—Materials to be soldered, welded or cut
  • B23K2103/08—Non-ferrous metals or alloys
• • 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 or for the powder bed-based, additive production of a plurality of components, in particular the repair of components and a corresponding device.
• the components are in particular ⁇ special for use in a turbomachine, preferably ⁇ provided in the hot gas path of a gas turbine. Vorzugswei ⁇ se is in the components to turbine blades or their blades. Accordingly, the components preferably each comprise or consist of a nickel-based or cobalt-base superalloy.
• the alloy may be precipitation hardened or precipitation hardenable.
• the components may alternatively or additionally be worn and / or partially manufactured or constructed components.
• Generative or additive manufacturing processes include, for example as powder bed processes, selective laser melting (SLM) or laser sintering (SLS), or electron beam melting (EBM). Also, the laser deposition welding ⁇ SEN (LMD) belongs to the additive process.
• SLM selective laser melting
• SLS laser sintering
• EBM electron beam melting
• LMD laser deposition welding ⁇ SEN
• a method for selective laser melting is known, for example, from EP 2 601 006 B1.
• Additive manufacturing processes (English: “additive manufacturing”) have proven to be particularly advantageous for complex or complicated or filigree designed components, for example, labyrinthine structures, cooling structures and / or
• the additive manufacturing is advantageous by a particularly short chain of mitschrit ⁇ th, as a manufacturing or production step of a component can be made directly on the basis of a corresponding CAD file.
• the additive manufacturing is particularly advantageous for the development or production of prototypes, which can not or can not be efficiently produced, for example, for cost reasons by means of conventional subtractive or metal-cutting processes or casting technology.
• Running of gas turbines often require after the scheduled service interval repair the Schaufelblattspit ⁇ ze. This is damaged in the use of the gas turbine by thermal, mechanical and / or corrosive action. To carry out the repair, the damaged area is conventionally removed manually and then with a
• Welding process such as laser cladding, rebuilt.
• the removal can be done manually or (partially) auto ⁇ matinstrument.
• the parts which are manufactured by vacuum investment casting due to their material composition requirements as well as geometry complexity are subject to variations in their dimensions (range of variation).
• the blade length varies due to manufacturing, that is a starting point along the longitudinal axis of the blade or blade ⁇ a nominal airfoil length is precisely defined some tenths of a millimeter only Be ⁇ rich.
• the removal of the airfoil tip or area to prepare for its rebuilding will result in variation or blurring of the remaining airfoil's lay.
• the dimensions of the component to be repaired be ⁇ relationship as the component of a certain unavoidable fluctuation or blurring are thus subjected to in terms of its longitudinal extent.
• conventional repair methods for example laser deposition welding or TIG welding, the above-mentioned fluctuation-in contrast to powder-bed-based additive methods-is unproblematic.
• one provided additive, and / or powder bed based selective method, such as selective laser ⁇ melt for the reconstruction of the parts would like to use this variation as described would be a committee rak ⁇ reindeer, or decide the parallel repair a plurality of components by a powder bed based method complicated.
• the position of a build-up tip relative to a substrate or baseplate should be determined to an extent that corresponds to the layer thickness used in the process.
• Typical layer thicknesses in the range of selective laser melting are approximately between 20 and 80 ⁇ m.
• One aspect of the present invention relates to a method for the powder bed-based additive construction of a plurality of components comprising fixing each of the components on a base plate, for example in a system for the corresponding additive production, by means of a holding or fixing device.
• the method further comprises adjusting a vertical position or height position of at least some of the fixed components (via the holding devices) relative to the base plate, so that a structure of the tip of each component of a predetermined range of tolerance is spaced from the base plate inner ⁇ half.
• the described adjustment is preferably an individual adjustment of each individual holding device and may comprise a height measurement or distance measurement of the corresponding mounting tips from the surface of the base plate.
• the method further comprises providing a powder bed of a, in particular pulverulent, build-up material on the base plate up to a height of the tolerance range.
• a configuration space is preferably up to a filled to the depth of the powder bed corresponding height which speaks ent ⁇ the distance of the range of tolerance of the base plate with powder.
• the provision of the powder bed may be provided in the described method equally before and after the step of adjusting the vertical position.
• the method comprises layer-wise additive build-up, preferably by means of selective laser melting, of material respectively on the construction tip of the components. Said material preferably corresponds to the building material solidified by an energy beam.
• the components of the advertising preferably parallel or simultaneously additively placed ⁇ builds.
• the structure of the tips each preferably have a philosophicalflä ⁇ che which - facing away conveniently from the surface of the base plate ⁇ - through the corresponding fixing on the base plate.
• the adjustment of the vertical position and / or a control of the vertical position is performed after each layer of material has been built up.
• a further aspect of the present invention relates to a device for the powder-bed-based additive manufacturing comprising a base plate and a plurality of independently adjustable relative to the base plate and, preferably movable, holding devices, wherein the holding means are each formed, a component (as described above) relative to fix to the base plate.
• the method is a repair or repair method.
• the components are repair components.
• material is removed prior to fixing in each case in a wear region of the components and thus defines the construction tip.
• the components are molded, in particular by precision casting, such as vacuum investment casting, manufactured components.
• the components are forged components. In one embodiment, the components are similar.
• the components are Turbinenlaufschau ⁇ blades
• the superstructure tip is a blade tip represents ⁇
• a nominal layer thickness for the layered additive structure corresponds to a dimension of the tolerance range spaced from the base plate.
• the tole ⁇ ranz Scheme is typically 10 to 80ym, preferably 20 to 30ym. By means of this embodiment, it can be ensured, in particular, that during the production or
• Repair process of the components does not cause problems with a coater unit of the additive manufacturing plant, especially not to collisions. If the assembly tips of the components are arranged according to the method described within the tolerance range, they are for the material order or the repair within the layer or layer thickness of a new material order, and a collision with the coater is thus closed from ⁇ .
• a distance of each construction tip of the components during the layerwise addition cross ven structure for example, after each or some of verfes ⁇ saturated layers or plies, measured relative to the base plate and / or rela ⁇ tive to the surface of the powder bed.
• This Substituted ⁇ staltung is particularly useful to set the vertical position-of the fixed components, such as described in general to be adjusted.
• the predetermined Toleranzbe ⁇ rich for example, measured along a mounting direction, 10 to 80ym, preferably 20 to 30ym.
• each holding device for example, via a guide in the base plate, designed to be height adjustable.
• each holder device has a carrier and / or a clamping device.
• the components are expedient fi ⁇ xed.
• the carrier, the clamping device and / or the holding device is designed to be movable and / or height-adjustable relative to the base plate by means of hydraulic, pneumatic, electromechanical or piezoelectric means.
• the device has at least four holding devices. Accordingly, for example, four components can be constructed in parallel additive layers or
• the device has more than four retaining devices, for example six, eight or ten Hal ⁇ te réelleen.
• Embodiments, features and / or advantages relating in the present case to the method may also relate to the device or vice versa.
• FIG. 1 shows a schematic perspective view ei ⁇ ner apparatus of the present invention.
• Figure 2 shows a schematic sectional or side view of at least a portion of the device.
• Figure 3 shows a schematic sectional view of the Vorrich ⁇ tung in operation and implies an inventive method.
• FIG. 4 indicates, with reference to a schematic view, method steps of the method.
• FIG. 5 shows a schematic flow diagram of method steps of the method according to the invention.
• Figure 1 shows a perspective view of a device 100.
• the device 100 is preferably provided for the Use in a plant for powder-bed-based additive production, preferably by selective laser melting (SLM).
• SLM selective laser melting
• the device 100 has a base plate 1.
• the base plate is expediently a base plate for the additive production of metallic components, in particular turbine components.
• the base plate 1 may be a construction platform similar to a construction platform of a conventional additive manufacturing installation, for example a steel base plate and / or low-distortion base plate.
• the base plate 1 has a square or rectangular main surface.
• the device 100 furthermore has a plurality of holding devices 2.
• Four retaining devices 2 are arranged or fastened by way of example on the surface mentioned.
• the holder devices 2 are provided, for example in order to be repaired or refurbished to be set, in particular ver ⁇ schlissene components on the support means 2 relative to the base 1 to fix.
• the holding devices 2 each have clamping devices 4, in particular clamping jaws to clamp a fixated ⁇ compo nent or a corresponding component, and to fix it that way.
• the holding devices 2 are furthermore designed to be height-adjustable independently of one another (compare FIG. 2) in order to adjust the components for the powder-bed-based additive production in the device 100 in the powder bed at the same level or the same height along a mounting direction (vertical Z direction). This may be necessary to suitably carry out the additive process, in particular the powder coating.
• FIG. 2 shows at least part of the device 100 in an enlarged view.
• a guide 6 of the device 100 is further shown in FIG.
• the guide 6 is preferably carried out through a bore or opening of the base plate 1 and connected to the holding device 2.
• the clamping jaws 4 described above are shown in an enlarged view.
• two clamping jaws or a Spannba ⁇ pair of blocks are preferably provided. Holding or fixing surfaces of the clamping jaws can be configured like a Christmas tree around one
• Shovel foot preferably a turbine blade, purpose ⁇ tionally to grab and fix.
• At least one of the clamping jaws of each holding device 2 is movable in order to fix the component (not explicitly shown in FIG. 2).
• the component not explicitly shown in FIG. 2.
• the hori zontal ⁇ arrow of the right jaw in Figure 2 that this can be pressed, for example, for fixing the component 10 against the left jaw. This can be done by measures known to those skilled in the art.
• the device 100 further comprises a carrier 7.
• the carrier 7 preferably connects the clamping jaws 4 with the guide 6 or couples them.
• the device 100 further comprises means 5 to the Hal ⁇ te Korea 2 and / or the carrier 7 form height adjustable, ie, for example adjustable along a mounting direction (see vertical arrow on the right side in Figure 2).
• a thread 8 can be used.
• the means 5 may be, for example, electromechanical means, such as stepper motors. Wei ⁇ terhin a height adjustment of the holding device by hydraulic, pneumatic or similar mechanical means, or even piezoelectric can be accomplished.
• the described means for height adjustment, in particular stepper motors, are furthermore arranged below the base plate, al ⁇ so outside a powder space during operation of the device 100.
• the guide 6 against the powder bed which is arranged in the operation of the device 100 above the base ⁇ plate 1, for example, sealed by the skilled person known means.
• Figure 3 shows a schematic sectional view of the Vorrich- processing 100 which is used in a system 200 for additive Her ⁇ position.
• the device 100 is preferential ⁇ , in a process for the manufacture of additive (see Figure 5 below) was used.
• Figure 3 indicates wei ⁇ terhin at some steps of the method described.
• each of the holding devices 2 fixes or holds a component 100, expediently via the clamping jaws, as described in FIGS. 1 and 2.
• the components are preferably turbine blades, in particular turbine blades.
• the components 10 can accordingly be cast components 10, in particular produced by fine casting, such as vacuum precision casting.
• the components 10 are preferably similar, in particular wear parts for the same power plant or industrial plant.
• the components 10 are preferably exposed to heavy wear, for example due to corrosive or mechanical influences, which is why they have to be repaired or repaired after certain operating intervals.
• a Schaufelblattspit ⁇ ze machined and removed material thereby defining a building tip or mounting surface 11.
• Each of the component 10 accordingly has the tip 11 (construction tip), on which with the described method In a later step, material is built up and the construction part is to be repaired again.
• the structure of the tips 11 of the members 10 shown as an example are shown in the pre ⁇ direction 100 at a different height (vertical polyvinyl sition). This is because the part or blade length is subject to some variation.
• the method presented now comprises individual A ⁇ or adjusting the heights of the components 10 by the holding means or the means described, relative to the base plate so that the construction of the tips 11 are arranged within a predetermined tolerance range TB and spaced from the base plate 1 / become.
• the predetermined tol ⁇ ranz Scheme TB is measured along the mounting direction, 10 to 80ym, preferably 20 to 30ym.
• a readjustment or Kontrollie ⁇ ren the height or vertical position of the components after each in a later step is structured or solidified
• Layer of building material in particular from the hardened alloy suitable for the blades.
• the method comprising a height measurement within the forward direction 100 or 200 this comprehensive system, preferably ⁇ by means of laser distance measurement, when the components are already covered with powder.
• the height measurement may be relative to the baseplate and / or relative to a surface of the powder bed.
• the filling or provision of the powder 3 (powder bed) or building material can basically be done before or after adjusting the height or vertical position.
• the structure with the number 1 ⁇ (see left side) is set such that the corresponding component or its structure tip 11 in ⁇ nergur, more specifically at the upper limit of the tolerance range, is arranged.
• the structure shown in point 3 ⁇ (see right side) is adjusted in terms of height such that the construction of tip 11 of the right component 10 in approximately the unte ⁇ ren limit of the tolerance range TB (see Distance A) is arranged arrival.
• the position is set in such a way or the tolerance range TB is selected such that it corresponds to a predetermined layer thickness D of the powder to be applied.
• Figure 4 shows parts of the apparatus shown in Figure 3 100 and system 200, where, using the beschrie ⁇ surrounded method, a height or vertical position of the "on ⁇ construction", comprising the central holding member 2 together with the fixed member 10, corrected, or such is set, that the corresponding mounting tip 11 with respect to its height or its distance from the building board 1 is within the tolerance range TB.
• FIG. 5 shows a schematic flow diagram of method steps according to the invention.
• the method is a method for the powder-bed-based, additive construction of a majority of the components described.
• the method may comprise the removal of material in a wear region of the components, in particular in such a way that an assembly recess 11 of the components is defined in this way.
• the method according to method steps b) comprises fixing each of the components 10 on a base plate 1 by means of a holding device 2.
• the method comprises measuring a distance of each assembly tip 11 of the components 10 relative to the base plate 1 during the actual additive up ⁇ construction (see step f) below).
• the method comprises a ⁇ represent a vertical position of at least some of the fixed parts 10 relative to the base plate 1, so that a structure tip 11 of each member 10 is spaced within a solicitstimm ⁇ th tolerance range TB of the base plate. 1
• the method comprises providing a powder bed 3 of the building material on the base plate 1 up to a height of the tolerance range TB.
• the method comprises
• additively tau provide ⁇ layerwise additive build-up of material on each of the tip 11 structure, in particular a worn area of the components 10 (see FIG. 11 structure peak) or repaired.
• a worn area of the components 10 see FIG. 11 structure peak
• Such components may, for example, be connected to the base plate 1 by means of a silicone gasket around the components 10 or holding devices 2.
• the invention is not limited by the description based on the embodiments of these, but includes each new feature and any combination of features. This includes in particular any combination of features in the patent claims, even if this feature or combination itself is not explicitly stated in the patent claims or exemplary embodiments.

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

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• 2017
  • 2017-02-08 DE DE102017201994.8A patent/DE102017201994A1/de not_active Withdrawn
• 2018
  • 2018-01-25 EP EP18704450.8A patent/EP3562608A1/de not_active Withdrawn
  • 2018-01-25 US US16/476,279 patent/US20190358755A1/en not_active Abandoned
  • 2018-01-25 WO PCT/EP2018/051853 patent/WO2018145912A1/de unknown
  • 2018-01-25 CN CN201880010754.1A patent/CN110382140B/zh not_active Expired - Fee Related

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