EP1422309A1 - Use of an apparatus for spray compacting for the production of a layer and layer system - Google Patents
Use of an apparatus for spray compacting for the production of a layer and layer system Download PDFInfo
- Publication number
- EP1422309A1 EP1422309A1 EP02026100A EP02026100A EP1422309A1 EP 1422309 A1 EP1422309 A1 EP 1422309A1 EP 02026100 A EP02026100 A EP 02026100A EP 02026100 A EP02026100 A EP 02026100A EP 1422309 A1 EP1422309 A1 EP 1422309A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- layer
- spray compacting
- production
- spray
- layer system
- 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- Withdrawn
Links
- 239000007921 spray Substances 0.000 title claims abstract description 23
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 5
- 239000000758 substrate Substances 0.000 claims description 7
- 239000011148 porous material Substances 0.000 claims description 2
- 238000000576 coating method Methods 0.000 abstract description 5
- 239000011248 coating agent Substances 0.000 abstract description 2
- 238000000034 method Methods 0.000 description 6
- 239000000463 material Substances 0.000 description 3
- 238000007750 plasma spraying Methods 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 238000004873 anchoring Methods 0.000 description 2
- 229910017052 cobalt Inorganic materials 0.000 description 2
- 239000010941 cobalt Substances 0.000 description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910017985 Cu—Zr Inorganic materials 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 229910000601 superalloy Inorganic materials 0.000 description 1
- 239000012720 thermal barrier coating Substances 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D23/00—Casting processes not provided for in groups B22D1/00 - B22D21/00
- B22D23/003—Moulding by spraying metal on a surface
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/12—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
- C23C4/123—Spraying molten metal
Definitions
- the invention relates to the use of a spray compacting plant to create a layer and a layer system, that can be produced using a spray compacting system and is a layer system with a layer with undercuts according to claims 1, 2 and 3.
- Coatings of components e.g. Bond layers or Thermal insulation layers of components exposed to high temperatures, such as. Gas turbine components are often made using plasma spraying coated, as in U.S. Patent 3,839,618 or U.S. Patent 4,447,466.
- a spray compacting method is known from US Pat. No. 4,418,124 known, in which massive bodies are made.
- the object of the present invention is to simplify Way layers with improved adhesion, in particular to be able to produce thick layers.
- the task is solved by using a spray compacting system according to claim 1 and a layer system according to Claim 2 and Claim 3.
- Figure 1 shows a spray compacting plant 1 used to at least one layer 16 according to the invention (FIG. 2) to produce on a substrate 30 ( Figure 2), the Layer 16, which can also be an intermediate layer 16 should adhere to the substrate 30.
- a nozzle 4 melted, for example.
- the molten particles 7 are not injected into a mold, where they should form a massive body, but form a layer 16 on a component 10.
- the microstructure of the layer can be determined by the process parameters the spray compacting system can be set. So can target the porosity and / or undercuts can be set.
- FIG. 2 shows a cross section through a layer system 28 of a component 1, which in a spray compacting plant 1 has been manufactured.
- An intermediate layer 16 is present on the component 1 has been produced by spray compacting.
- the intermediate layer 16 can be dense but, by appropriate variation of the process parameters, can also have a porous structure, possibly with undercuts 22, which enable better anchoring of a layer 19 applied to the layer 16 compared to a layer without undercuts and / or pores.
- the improved adhesion is achieved not only by the undercuts 22, but also by the increased contact area between the layers 16 and 19.
- Such layers 16 with undercuts 22 can also be used other methods (plasma spraying, CVD; PVD) become.
- Layer 19 can, but does not have to, in a spray compacting plant 1 have been produced.
- the component 10 is a turbine blade or generally a component 10 that is exposed to high temperatures and whose substrate 30 consists, for example, of a nickel- or cobalt-based superalloy.
- Layer 16 is a so-called intermediate layer of the composition MCrAlY, where M stands for an element from the group iron, nickel or cobalt.
- Layer 19 can be an anchoring layer or ceramic thermal barrier coating.
- FIG. 3 shows a layer system 28 which has only one layer 16.
- Layer 16 has a low porosity and is, for example, at least 0.5 mm thick. Such thick layers can be produced particularly well by means of a spray compacting system 1.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Coating By Spraying Or Casting (AREA)
Abstract
Beschichtungen für Bauteile können nach dem Stand der Technik auf verschiedene Art und Weise hergestellt werden. Dabei müssen nicht nur bestimmte Anforderungen für bestimmte Einsatzbedingungen erfüllt werden, sondern auch die Herstellung muss schnell, einfach und kostengünstig sein. Die erfindungsgemäße Verwendung einer Sprühkompaktierungsanlage (1) zur Erzeugung einer Schicht (16, 19) ermöglicht dies, indem ein erfindungsgemäßes Schichtsystem (28) in bekannten Sprühkompaktierungsanlagen (1) eingebracht wird und dort beschichtet wird. <IMAGE>Coatings for components can be produced in various ways according to the prior art. Not only do certain requirements for certain operating conditions have to be met, but also the production has to be quick, easy and inexpensive. The use of a spray compacting system (1) according to the invention for producing a layer (16, 19) makes this possible by introducing a layer system (28) according to the invention in known spray compacting systems (1) and coating it there. <IMAGE>
Description
Die Erfindung betrifft eine Verwendung einer Sprühkompaktierungsanlage zur Erzeugung einer Schicht und ein Schichtsystem, das mittels einer Sprühkompaktierungsanlage herstellbar ist und ein Schichtsystem mit einer Schicht mit Hinterschneidungen gemäß den Ansprüchen 1, 2 und 3.The invention relates to the use of a spray compacting plant to create a layer and a layer system, that can be produced using a spray compacting system and is a layer system with a layer with undercuts according to claims 1, 2 and 3.
Beschichtungen von Bauteilen, wie z.B. Bondschichten oder Wärmedämmschichten von hochtemperaturbelasteten Bauteilen, wie z.B. Gasturbinenbauteilen, werden oft mittels Plasmaspritzen beschichtet, wie es in der US-PS 3,839,618 oder US-PS 4,447,466 beschrieben ist.Coatings of components, e.g. Bond layers or Thermal insulation layers of components exposed to high temperatures, such as. Gas turbine components are often made using plasma spraying coated, as in U.S. Patent 3,839,618 or U.S. Patent 4,447,466.
Ein Sprühkompaktierungsverfahren ist aus der US-PS 4,418,124 bekannt, bei dem massive Körper hergestellt werden.A spray compacting method is known from US Pat. No. 4,418,124 known, in which massive bodies are made.
Sprühkompaktierungsverfahren, bei dem ein geschmolzenes Metall verdüst wird und in eine Form gespritzt wird um massive dichte Bauteile herzustellen, sind in dem Artikel "Microstructure and properties of spray cast Cu-Zr-alloys", Materials Science and Engineering A145(1991), Seite 243-255 von R.P. Singh beschrieben.Spray compacting process in which a molten metal is atomized and injected into a mold for massive Manufacturing dense components are described in the article "Microstructure and properties of spray cast Cu-Zr alloys ", materials Science and Engineering A145 (1991), pages 243-255 of R.P. Singh described.
Die Herstellungsbedingungen von massiven dichten Bauteilen mittels einem Sprühkompaktierungsverfahren sind in dem Artikel "Impingement Behavior of a Spray Cast Aluminum Alloy" in dem Proceedings Conference "Solidification 1993 in San Antonia, Texas, Februar 15-19, 1998 von D.P. M Matson" beschrieben. The manufacturing conditions of massive dense components by means of a spray compacting process are in the article "Impingement Behavior of a Spray Cast Aluminum Alloy" in the Proceedings Conference "Solidification 1993 in San Antonia, Texas, February 15-19, 1998 by D.P. M Matson ".
In der US-PS 6,444,331 ist beschrieben, dass eine poröse Bondschicht, die mittels Plasmaspritzen hergestellt wird, zur besseren Haftung dient.US Pat. No. 6,444,331 describes a porous Bond layer, which is produced by means of plasma spraying, for serves better liability.
Aufgabe der vorliegenden Erfindung ist es, auf vereinfachte Art und Weise Schichten mit verbesserter Haftung, insbesondere dicke Schichten, herstellen zu können.The object of the present invention is to simplify Way layers with improved adhesion, in particular to be able to produce thick layers.
Die Aufgabe wird gelöst durch die Verwendung einer Sprühkompaktierungsanlage gemäß Anspruch 1 und ein Schichtsystem gemäß Anspruch 2 und Anspruch 3.The task is solved by using a spray compacting system according to claim 1 and a layer system according to Claim 2 and Claim 3.
In den Unteransprüchen sind weitere vorteilhafte Ausgestaltungen des Schichtsystems beschrieben.Further advantageous refinements are in the subclaims of the layer system.
Es zeigen
Figur 1 zeigt eine Sprühkompaktierungsanlage 1, die verwendet
wird, um zumindest eine erfindungsgemäße Schicht 16 (Figur 2)
auf einem Substrat 30 (Figur 2) zu erzeugen, wobei die
Schicht 16, die auch eine Zwischenschicht 16 sein kann, auf
dem Substrat 30 haften soll.Figure 1 shows a spray compacting plant 1 used
to at least one
In der Sprühkompaktierungsanlage 1 wird beispielsweise aus
einer Düse 4 aufgeschmolzenes, bspw. metallisches, Material
ausgedüst, so dass ein Materialstrom aus zumindest teilweise
flüssigen Teilchen 7 entsteht, die auf die Oberfläche 13
eines Bauteils 10 auftreffen und dort eine Schicht 16, 19
(Fig. 2, 3) erzeugen. In the spray compacting plant 1, for example
a
Im Gegensatz zu den herkömmlichen Sprühkompaktierungsanlagen
werden die geschmolzenen Teilchen 7 nicht in eine Form eingedüst,
wo sie einen massiven Körper bilden sollen, sondern
bilden eine Schicht 16 auf einem Bauteil 10.In contrast to conventional spray compacting systems
the
Insbesondere können mit dieser Beschichtungsmethode einfach,
kostengünstig und sehr schnell dicke Schichten auf einem Bauteil
10 hergestellt werden.In particular, with this coating method,
inexpensive and very fast thick layers on a
Die Mikrostruktur der Schicht kann durch die Verfahrensparameter der Sprühkompaktierungsanlage eingestellt werden. So können die Porosität und/oder Hinterschneidungen gezielt eingestellt werden.The microstructure of the layer can be determined by the process parameters the spray compacting system can be set. So can target the porosity and / or undercuts can be set.
Figur 2 zeigt einen Querschnitt durch ein Schichtsystem 28
eines Bauteils 1, das in einer Sprühkompaktierungsanlage 1
hergestellt worden ist.FIG. 2 shows a cross section through a
Auf dem Bauteil 1 ist eine Zwischenschicht 16 vorhanden, die
mittels Sprühkompaktierung hergestellt worden ist.An
Die Zwischenschicht 16 kann dicht sein aber auch durch entsprechende
Variation der Verfahrensparameter eine poröse
Struktur ggf. auch mit Hinterschneidungen 22 aufweisen, die
eine bessere Verankerung einer auf der Schicht 16
aufgebrachten Schicht 19 gegenüber einer Schicht ohne
Hinterschneidungen und/oder Poren ermöglichen.
Die verbesserte Haftung wird nicht nur durch die Hinterschneidungen
22 erreicht, sondern auch durch die vergrößerte
Kontaktfläche zwischen der Schicht 16 und 19.The
The improved adhesion is achieved not only by the
Solche Schichten 16 mit Hinterschneidungen 22 können auch mit
anderen Methoden (Plasmaspritzen, CVD; PVD) hergestellt
werden.
Die Schicht 19 kann, muss aber nicht in einer Sprühkompaktierungsanlage
1 hergestellt worden sein.
Beispielsweise ist das Bauteil 10 eine Turbinenschaufel oder
allgemein ein Bauteil 10, das hochtemperaturbelastet ist, und
dessen Substrat 30 beispielsweise aus einer nickel- oder
kobaltbasierten Superlegierung besteht.
Die Schicht 16 ist eine so genannte Zwischenschicht der
Zusammensetzung MCrAlY, wobei M für ein Element der Gruppe
Eisen, Nickel oder Cobalt steht.
Die Schicht 19 kann eine Verankerungsschicht oder keramische
Wärmedämmschicht sein.For example, the
Figur 3 zeigt ein Schichtsystem 28, das nur eine Schicht 16
aufweist.
Die Schicht 16 hat eine geringe Porosität und ist beispielsweise
mindestens 0,5 mm dick.
Solche dicken Schichten lassen sich besonders gut mittels in
einer Sprühkompaktierungsanlage 1 herstellen.FIG. 3 shows a
Such thick layers can be produced particularly well by means of a spray compacting system 1.
Claims (5)
bestehend aus
einem Substrat (30),
und zumindest einer Schicht (16) auf dem Substrat (30), wobei zumindest eine Schicht (16) in einer Sprühkompaktierungsanlage (1) hergestellt ist.Layer system,
consisting of
a substrate (30),
and at least one layer (16) on the substrate (30), at least one layer (16) being produced in a spray compacting plant (1).
einem Substrat (30),
einer Zwischenschicht (16)
und zumindest einer Schicht (19) auf der Zwischenschicht (16),
wobei die Zwischenschicht (16) Hinterschneidungen (22) und/oder Poren aufweist.Layer system consisting of
a substrate (30),
an intermediate layer (16)
and at least one layer (19) on the intermediate layer (16),
wherein the intermediate layer (16) has undercuts (22) and / or pores.
dadurch gekennzeichnet, dass
die Zwischenschicht (16) in einer Sprühkompaktierungsanlage hergestellt ist.Layer system according to claim 3,
characterized in that
the intermediate layer (16) is produced in a spray compacting plant.
dadurch gekennzeichnet, dass
die Schicht (16, 19) mindestens 0,3mm dick ist.Layer system according to claim 2 or 3,
characterized in that
the layer (16, 19) is at least 0.3 mm thick.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP02026100A EP1422309A1 (en) | 2002-11-22 | 2002-11-22 | Use of an apparatus for spray compacting for the production of a layer and layer system |
PCT/EP2003/010877 WO2004048635A1 (en) | 2002-11-22 | 2003-10-01 | Layer system comprising a layer provided with undercut sections |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP02026100A EP1422309A1 (en) | 2002-11-22 | 2002-11-22 | Use of an apparatus for spray compacting for the production of a layer and layer system |
Publications (1)
Publication Number | Publication Date |
---|---|
EP1422309A1 true EP1422309A1 (en) | 2004-05-26 |
Family
ID=32187193
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP02026100A Withdrawn EP1422309A1 (en) | 2002-11-22 | 2002-11-22 | Use of an apparatus for spray compacting for the production of a layer and layer system |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP1422309A1 (en) |
WO (1) | WO2004048635A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008052516A2 (en) | 2006-11-01 | 2008-05-08 | Zollern Bhw Gleitlager Gmbh & Co. Kg | Method for producing two bonded-together layers and functional component that can be produced by the method |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2003055512A1 (en) | 2001-12-21 | 2003-07-10 | Novo Nordisk Health Care Ag | Liquid composition of factor vii polypeptides |
CA2490342C (en) | 2002-06-21 | 2015-06-16 | Novo Nordisk A/S | Stabilised solid compositions of factor vii polypeptides |
JP4658041B2 (en) | 2003-06-25 | 2011-03-23 | ノボ ノルディスク ヘルス ケア アクチェンゲゼルシャフト | Liquid composition of factor VII polypeptide |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3839618A (en) * | 1972-01-03 | 1974-10-01 | Geotel Inc | Method and apparatus for effecting high-energy dynamic coating of substrates |
US4418124A (en) * | 1980-10-06 | 1983-11-29 | General Electric Company | Plasma spray-cast components |
EP0350432A1 (en) * | 1988-07-05 | 1990-01-10 | MANNESMANN Aktiengesellschaft | Apparatus for semi-continuous spray compacting |
US5060713A (en) * | 1989-02-03 | 1991-10-29 | Mannesmann Ag | Method of and apparatus for spraycasting |
WO2000050177A1 (en) * | 1999-02-23 | 2000-08-31 | Sprayform Holdings Limited | Spray deposition process |
US6444331B2 (en) * | 1998-11-24 | 2002-09-03 | General Electric Company | Roughened bond coats for a thermal barrier coating system and method for producing |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6368672B1 (en) * | 1999-09-28 | 2002-04-09 | General Electric Company | Method for forming a thermal barrier coating system of a turbine engine component |
JP2003147464A (en) * | 2001-11-02 | 2003-05-21 | Tocalo Co Ltd | Member with high-temperature strength |
-
2002
- 2002-11-22 EP EP02026100A patent/EP1422309A1/en not_active Withdrawn
-
2003
- 2003-10-01 WO PCT/EP2003/010877 patent/WO2004048635A1/en not_active Application Discontinuation
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3839618A (en) * | 1972-01-03 | 1974-10-01 | Geotel Inc | Method and apparatus for effecting high-energy dynamic coating of substrates |
US4418124A (en) * | 1980-10-06 | 1983-11-29 | General Electric Company | Plasma spray-cast components |
EP0350432A1 (en) * | 1988-07-05 | 1990-01-10 | MANNESMANN Aktiengesellschaft | Apparatus for semi-continuous spray compacting |
US5060713A (en) * | 1989-02-03 | 1991-10-29 | Mannesmann Ag | Method of and apparatus for spraycasting |
US6444331B2 (en) * | 1998-11-24 | 2002-09-03 | General Electric Company | Roughened bond coats for a thermal barrier coating system and method for producing |
WO2000050177A1 (en) * | 1999-02-23 | 2000-08-31 | Sprayform Holdings Limited | Spray deposition process |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008052516A2 (en) | 2006-11-01 | 2008-05-08 | Zollern Bhw Gleitlager Gmbh & Co. Kg | Method for producing two bonded-together layers and functional component that can be produced by the method |
WO2008052516A3 (en) * | 2006-11-01 | 2008-06-26 | Zollern Bhw Gleitlager Gmbh & | Method for producing two bonded-together layers and functional component that can be produced by the method |
CN101605621B (en) * | 2006-11-01 | 2013-07-10 | 卓轮Bhw滑动轴承两合公司 | Method for producing two bonded-together layers and functional component that can be produced by the method |
US8573283B2 (en) | 2006-11-01 | 2013-11-05 | Zollern Bhw Gleitlager Gmbh & Co., Kg | Method for producing two bonded-together layers and functional component that can be produced by the method |
DE102006051936B4 (en) * | 2006-11-01 | 2014-03-20 | Zollern Bhw Gleitlager Gmbh & Co. Kg | Process for producing two interconnected layers and functional component which can be produced by the process |
Also Published As
Publication number | Publication date |
---|---|
WO2004048635A1 (en) | 2004-06-10 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0219536B1 (en) | Protection layer | |
DE69828732T2 (en) | Method for applying an adhesive coating for a thermal barrier coating | |
DE69730245T2 (en) | METHOD FOR TREATING METAL PARTS | |
EP2467224A1 (en) | Thin-walled structural component, and method for the production thereof | |
EP2398936B1 (en) | Erosion resistant coating system for gas turbine components | |
DE102005050873B4 (en) | Process for producing a segmented coating and component produced by the process | |
CH704833A1 (en) | Component for a turbo machine and a method of manufacturing such a component. | |
EP1123455A1 (en) | Product with a heat insulating layer and method for the production of a heat insulating layer | |
CH657872A5 (en) | COMPOSITE PRODUCT MADE OF AT LEAST TWO SUPER ALLOYS. | |
DE102012108057B4 (en) | Method of manufacturing a last stage steam turbine blade | |
EP1581386A1 (en) | Layer system | |
EP2576863B1 (en) | Method for producing a layer by means of cold spraying and use of such a layer | |
EP1878813A1 (en) | Coating process for aluminum-silicon casting | |
DE102015212588A1 (en) | Contour-faithful protective layer for compressor components of gas turbines | |
DE69002691T2 (en) | Metal powder spray coating material, process for its production and use. | |
EP2737103B1 (en) | Method for applying an anti-wear protective coating to a flow engine component | |
WO2019219551A1 (en) | Brake body and method for producing same | |
EP2725235A1 (en) | Differentially rough airfoil and corresponding manufacturing method | |
EP1422309A1 (en) | Use of an apparatus for spray compacting for the production of a layer and layer system | |
DE112018002221T5 (en) | Process for the formation of thermal insulation layer, thermal insulation layer, and high temperature element | |
EP0386618B1 (en) | Element with wear-resisting layer comprising nickel or cobalt | |
WO2019122229A1 (en) | Corrosion- and erosion-resistant coating for turbine blades of gas turbines | |
EP1888806A1 (en) | Method for producing gas-tight layers and layer systems by means of thermal spraying | |
DE19536312C1 (en) | Prodn. of multilayered coating with defect-free bore holes used for turbine blades | |
EP0906964B1 (en) | Thermal barrier coating and process for its manufacture |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR IE IT LI LU MC NL PT SE SK TR |
|
AX | Request for extension of the european patent |
Extension state: AL LT LV MK RO SI |
|
AKX | Designation fees paid | ||
REG | Reference to a national code |
Ref country code: DE Ref legal event code: 8566 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN |
|
18D | Application deemed to be withdrawn |
Effective date: 20041127 |