DE102014224410A1 - SX repair via AM coupon - Google Patents
SX repair via AM coupon Download PDFInfo
- Publication number
- DE102014224410A1 DE102014224410A1 DE102014224410.2A DE102014224410A DE102014224410A1 DE 102014224410 A1 DE102014224410 A1 DE 102014224410A1 DE 102014224410 A DE102014224410 A DE 102014224410A DE 102014224410 A1 DE102014224410 A1 DE 102014224410A1
- Authority
- DE
- Germany
- Prior art keywords
- substrate
- coupon
- defect
- component
- crystalline orientation
- Prior art date
- Legal status (The legal status 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 status listed.)
- Withdrawn
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D19/00—Casting in, on, or around objects which form part of the product
- B22D19/10—Repairing defective or damaged objects by metal casting procedures
-
- 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
-
- 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
- B23K26/60—Preliminary treatment
-
- 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
-
- 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
- B23P6/005—Repairing turbine components, e.g. moving or stationary blades, rotors using only replacement pieces of a particular form
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/005—Repairing methods or devices
-
- 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
- B23K2103/18—Dissimilar materials
- B23K2103/26—Alloys of Nickel and Cobalt and Chromium
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/80—Repairing, retrofitting or upgrading methods
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/606—Directionally-solidified crystalline structures
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Plasma & Fusion (AREA)
- General Engineering & Computer Science (AREA)
- Crystals, And After-Treatments Of Crystals (AREA)
- Powder Metallurgy (AREA)
Abstract
Durch ein additives Herstellungsverfahren kann ein entsprechend hergestellter Coupon (13) mit einer gewünschten Orientierung hergestellt werden, der genau ein Fehlvolumen einer zu reparierenden Komponente (1) ersetzt.By an additive manufacturing process, a correspondingly produced coupon (13) can be produced with a desired orientation, which replaces exactly one missing volume of a component (1) to be repaired.
Description
Die Erfindung betrifft die Reparatur von gerichtet erstarrten Bauteilen, bei denen ein Coupon verwendet wird, der mittels eines additiven Herstellungsverfahrens (additive manufacture AM) hergestellt wird. The invention relates to the repair of directionally solidified components using a coupon made by an additive manufacturing AM.
Hochleistungsturbinen weisen gerichtet erstarrte Bauteile wie Einkristalle oder kolumnar erstarrte Bauteile auf. High-performance turbines have directionally solidified components such as single crystals or columnar solidified components.
Auch diese können für den erneuten Einsatz repariert werden, wobei jedoch die reparierte Stelle dieselbe Eigenschaft aufweisen soll wie das Substrat. These can also be repaired for reuse, but the repaired site should have the same property as the substrate.
Es gibt Möglichkeiten, durch Auftragsschweißen eine gerichtete Struktur zu erzeugen, jedoch ist das bei der Herstellung mit hohen Wärmegradienten verbunden, was zu Problemen führen kann. There are ways to create a directional structure by build-up welding, but this involves high thermal gradients during manufacture, which can lead to problems.
Es ist daher Aufgabe der Erfindung ein Verfahren aufzuzeigen, das dieses Problem überwindet. It is therefore an object of the invention to provide a method which overcomes this problem.
Die Aufgabe wird gelöst durch ein Verfahren gemäß Anspruch 1. The object is achieved by a method according to
In den Unteransprüchen sind weitere vorteilhafte Maßnahmen aufgelistet, die beliebig miteinander kombiniert werden können um weitere Vorteile zu erzielen. In the dependent claims further advantageous measures are listed, which can be combined with each other in order to achieve further advantages.
Die Figuren und die Beschreibung stellen nur Ausführungsbeispiele der Erfindung dar. The figures and the description represent only embodiments of the invention.
Es zeigen: Show it:
Eine Wärmeableitung aus einem Schmelzbad beim AM erfolgt gerichtet, so dass ein Gradient in Aufbaurichtung entsteht, was dazu führt, dass eine stängelförmige Kornstruktur bevorzugt entsteht. Beim schichtweisen Aufbau der Struktur bei der Herstellung des Coupons wird jeweils mindestens die vorhergehende Lage mit angeschmolzen. Somit wird beim Erstarrungsprozess von der vorherigen Lage die kristallographische Orientierung übernommen. A heat dissipation from a molten bath at the AM is directed, so that a gradient arises in the construction direction, which leads to a stem-shaped grain structure preferably arises. When layered structure of the structure in the production of the coupon at least the previous layer is also melted with. Thus, during the solidification process, the crystallographic orientation is adopted from the previous position.
Zuerst wird der defekte Bereich entfernt. First, the defective area is removed.
Als vorbereitender Schritt für die Herstellung des Coupons wird die kristallographische Orientierung – primär und sekundär – des zu reparierenden SX-Bauteils im Bereich der Oberfläche bestimmt. As a preparatory step for the production of the coupon, the crystallographic orientation - primarily and secondarily - of the SX component to be repaired in the area of the surface is determined.
Die Geometrie des fehlenden Volumens wird insbesondere über 3D-Laserscan bestimmt. Sie dient als Grundlage, um das 3D-Volumenfile für den AM-Prozess herzustellen, was letztlich zu einem exakt passenden, individuell angepassten Coupon führt. The geometry of the missing volume is determined in particular via 3D laser scanning. It serves as the basis to create the 3D volume file for the AM process, ultimately leading to a perfectly fitting, customized coupon.
Der Coupon wird mittels Selective Laser Melting aufgebaut. Dabei wird im Coupon die für das zu reparierende Bauteil passende kristallographische Orientierung über einen Saatkristall auf der Bauplattform mit der passenden Orientierung vorgegeben. The coupon is set up using Selective Laser Melting. In the coupon, the crystallographic orientation suitable for the component to be repaired is set via a seed crystal on the construction platform with the appropriate orientation.
Alternativ kann die Orientierung einer dünnen Scheibe des Originalbauteils benutzt werden, die in das SLM-Pulverbett eingelegt wird. Die Scheibe wird dabei von einer nur wenige μm dicken Pulverschicht bedeckt. Beim Auftreffen des Laserstrahls schmilzt die Pulverschicht und ein kleiner Teil der Originalbauteilscheibe. So wird beim Erstarren die Orientierung des zu reparierenden Bauteils in den Reparaturcoupon eingebracht. Alternatively, the orientation of a thin slice of the original component can be used, which is inserted into the SLM powder bed. The disk is covered by a few microns thick powder layer. When the laser beam strikes, the powder layer melts and a small part of the original component disk melts. Thus, during solidification, the orientation of the component to be repaired is introduced into the repair coupon.
Der entstandene Coupon mit der passenden Geometrie und kristallographischen Orientierung wird über ein Fügeverfahren eingefügt, vorzugsweise eine Hochtemperaturlötung mit borhaltiger Folie. The resulting coupon with the appropriate geometry and crystallographic orientation is inserted via a joining process, preferably a high-temperature soldering with boron-containing film.
Die
Das Substrat
In jedem Fall gibt es eine kristalline Hauptrichtung
Im Bereich einer Oberfläche war ein Defekt vorhanden, der entfernt wurde. Dies kann vorzugsweise mechanisch oder durch eine Laserbearbeitung erfolgen. In the area of a surface there was a defect that was removed. This can preferably be done mechanically or by laser processing.
Das so bearbeitete Substrat
Diese Daten des Fehlvolumens werden an eine Apparatur zur additiven Fertigung (additive manufacture AM) weitergeleitet, die aus einem Pulverbett
Der Saatkristall
Der Saatkristall kann auch durch andere Art und Weise hergestellt sein. The seed crystal can also be made by other means.
Als Saatkristall
Durch einen Saatkristall
In einem letzten Schritt muss der Coupon
Dies erfolgt vorzugsweise durch eine beliebige Lötung, insbesondere Folienlötung, die insbesondere Bor enthält. This is preferably done by any soldering, in particular foil soldering, which in particular contains boron.
Gegebenenfalls ist eine Nacharbeitung notwendig. If necessary, a reworking is necessary.
Claims (8)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102014224410.2A DE102014224410A1 (en) | 2014-11-28 | 2014-11-28 | SX repair via AM coupon |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102014224410.2A DE102014224410A1 (en) | 2014-11-28 | 2014-11-28 | SX repair via AM coupon |
Publications (1)
Publication Number | Publication Date |
---|---|
DE102014224410A1 true DE102014224410A1 (en) | 2016-06-02 |
Family
ID=55968340
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE102014224410.2A Withdrawn DE102014224410A1 (en) | 2014-11-28 | 2014-11-28 | SX repair via AM coupon |
Country Status (1)
Country | Link |
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DE (1) | DE102014224410A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3705210A1 (en) | 2019-03-05 | 2020-09-09 | Siemens Aktiengesellschaft | Method and apparatus for providing a previously prepared first component with at least one additive to a second component |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10319494A1 (en) * | 2003-04-30 | 2004-11-18 | Mtu Aero Engines Gmbh | Process for repairing and / or modifying components of a gas turbine |
DE60220930T2 (en) * | 2002-11-29 | 2008-03-13 | Alstom Technology Ltd. | Process for the preparation, modification or repair of monocrystalline or directionally solidified bodies |
DE102008025848A1 (en) * | 2008-05-29 | 2009-12-03 | Mtu Aero Engines Gmbh | Process for repairing single-crystal high-pressure turbine blades by diffusion soldering |
DE102008058140A1 (en) * | 2008-11-20 | 2010-05-27 | Mtu Aero Engines Gmbh | Method for repair of single crystal turbine blades, particularly high-pressure turbine stage, involves removing damaged blade part of turbine blades at parting plane on remaining blade |
US20110099810A1 (en) * | 2009-10-30 | 2011-05-05 | Alexander Stankowski | Method for repairing a gas turbine component |
US20110099809A1 (en) * | 2009-10-30 | 2011-05-05 | Hoevel Simone | Methods for repairing a gas turbine component |
US20120198676A1 (en) * | 2011-02-03 | 2012-08-09 | Alstom Technology Ltd | Method for repairing or reconditioning a badly damaged component, in particular from the hot gas region of a gas turbine |
US20130323533A1 (en) * | 2012-06-05 | 2013-12-05 | General Electric Company | Repaired superalloy components and methods for repairing superalloy components |
US20140259666A1 (en) * | 2013-03-12 | 2014-09-18 | Honeywell International Inc. | Methods for the repair of gas turbine engine components using additive manufacturing techniques |
-
2014
- 2014-11-28 DE DE102014224410.2A patent/DE102014224410A1/en not_active Withdrawn
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE60220930T2 (en) * | 2002-11-29 | 2008-03-13 | Alstom Technology Ltd. | Process for the preparation, modification or repair of monocrystalline or directionally solidified bodies |
DE10319494A1 (en) * | 2003-04-30 | 2004-11-18 | Mtu Aero Engines Gmbh | Process for repairing and / or modifying components of a gas turbine |
DE102008025848A1 (en) * | 2008-05-29 | 2009-12-03 | Mtu Aero Engines Gmbh | Process for repairing single-crystal high-pressure turbine blades by diffusion soldering |
DE102008058140A1 (en) * | 2008-11-20 | 2010-05-27 | Mtu Aero Engines Gmbh | Method for repair of single crystal turbine blades, particularly high-pressure turbine stage, involves removing damaged blade part of turbine blades at parting plane on remaining blade |
US20110099810A1 (en) * | 2009-10-30 | 2011-05-05 | Alexander Stankowski | Method for repairing a gas turbine component |
US20110099809A1 (en) * | 2009-10-30 | 2011-05-05 | Hoevel Simone | Methods for repairing a gas turbine component |
US20120198676A1 (en) * | 2011-02-03 | 2012-08-09 | Alstom Technology Ltd | Method for repairing or reconditioning a badly damaged component, in particular from the hot gas region of a gas turbine |
US20130323533A1 (en) * | 2012-06-05 | 2013-12-05 | General Electric Company | Repaired superalloy components and methods for repairing superalloy components |
US20140259666A1 (en) * | 2013-03-12 | 2014-09-18 | Honeywell International Inc. | Methods for the repair of gas turbine engine components using additive manufacturing techniques |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3705210A1 (en) | 2019-03-05 | 2020-09-09 | Siemens Aktiengesellschaft | Method and apparatus for providing a previously prepared first component with at least one additive to a second component |
WO2020177916A1 (en) | 2019-03-05 | 2020-09-10 | Siemens Aktiengesellschaft | Method and system for providing an already produced first component with at least one additively manufactured second component |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
R079 | Amendment of ipc main class |
Free format text: PREVIOUS MAIN CLASS: B22D0019100000 Ipc: B22D0025000000 |
|
R079 | Amendment of ipc main class |
Free format text: PREVIOUS MAIN CLASS: B22D0025000000 Ipc: B23K0001190000 |
|
R163 | Identified publications notified | ||
R119 | Application deemed withdrawn, or ip right lapsed, due to non-payment of renewal fee |