US20180179645A1 - Dvc-coating with fully and partially stabilized zirconia - Google Patents
Dvc-coating with fully and partially stabilized zirconia Download PDFInfo
- Publication number
- US20180179645A1 US20180179645A1 US15/736,340 US201615736340A US2018179645A1 US 20180179645 A1 US20180179645 A1 US 20180179645A1 US 201615736340 A US201615736340 A US 201615736340A US 2018179645 A1 US2018179645 A1 US 2018179645A1
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- US
- United States
- Prior art keywords
- stabilized zirconia
- layer
- fully
- coating
- ceramic layer
- 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.)
- Abandoned
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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
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
- C23C28/345—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer
- C23C28/3455—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer with a refractory ceramic layer, e.g. refractory metal oxide, ZrO2, rare earth oxides or a thermal barrier system comprising at least one refractory oxide layer
-
- 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
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/32—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
- C23C28/321—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer
- C23C28/3215—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer at least one MCrAlX layer
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- 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
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/284—Selection of ceramic materials
-
- 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
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/288—Protective coatings for blades
-
- 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
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/29—Three-dimensional machined; miscellaneous
- F05D2250/294—Three-dimensional machined; miscellaneous grooved
-
- 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
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/21—Oxide ceramics
- F05D2300/2118—Zirconium oxides
Definitions
- the following relates to a ceramic layer-system with partially and fully stabilized zirconia which has also a dense vertical cracked microstructure (DVC).
- DVC dense vertical cracked microstructure
- TBC Thermal Barrier Coatings
- DVC Dense Vertical Cracked
- DVC thermal barrier coatings have shown significantly lower rates compared to their porous counterparts. That means for the same chemistry a porous coating will show more than 3 ⁇ the erosion rate compared to the DVC one.
- DVC coatings have increased cohesion and adhesion compared to the typical porous coatings. The reason is that a very high ratio of fully molten particles deposit on hot substrate or hot previously deposited splats which promotes a good intimate bonding to develop between them. Improved adhesion requires high energy for a horizontal crack to propagate so that guarantees a lower delamination.
- Coating life Due to the intimate contact between splats, the DVC coatings show high fracture toughness along the parallel to the substrate plane.
- a bond coat especially a metallic bond coat 7 and very especially a NiCoCrAlY-based bond coat 7 is applied on.
- first zirconia layer 10 made of a partially stabilized zirconia.
- the porosity of the partially stabilized zirconia 10 is preferably lower than 5% and very preferably lower than 3%.
- the thickness of the fully stabilized zirconia 13 is preferable between 50 ⁇ m-800 ⁇ m.
- the stabilization in this zirconia based system can be reached by yttria or by any other rare earth element as known by the state of the art or by a combination of that.
- yttrium is used for stabilization.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Inorganic Chemistry (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Ceramic Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Coating By Spraying Or Casting (AREA)
Abstract
Description
- This application claims priority to PCT Application No. PCT/EP2016/059828, having a filing date of May 3, 2016, based on European Application No. 15172884.7, having a filing date of Jun. 19, 2015, the entire contents both of which are hereby incorporated by reference.
- The following relates to a ceramic layer-system with partially and fully stabilized zirconia which has also a dense vertical cracked microstructure (DVC).
- Field feedback has shown that the current Thermal Barrier Coatings (TBC) of turbines suffer from issues related to:
- 1) Erosion: turbine blades with high porosity coatings containing a large number of unmolten or semimolten particles show low erosion resistance. The development during the last years has pushed thermal spray coatings porosity upwards. However, that has caused the shrinkage of the spray ability window that allows coatings to receive high porosity and good cohesion. As a result, erosion has started manifesting itself as a major issue for coatings in specific parts and engines.
2) Drilling damage: High porosity coatings contain less intimate contacts between splats or splat and substrate and thus the required energy for a crack to propagate is relatively low.
This problem has been addressed by drilling before the coating deposition and reopening of the holes after coating deposition. This approach minimizes the interaction between coating and laser and that reduces significantly the coating delamination around the drilled holes. However, since each part has to be processed twice, this solution is associated with longer drilling times that are reflected as increased cost.
3) Coating life: Thermal Spray porous coatings do not demonstrate at the same level the high strain tolerance along the coating thickness which can be seen in other coating types such as EB-PVD.
The thermal barrier coatings porosity has been increased to improve strain tolerance. However as mentioned above, that can reduce the spray ability process window and influence negatively the cohesion and erosion resistance of the coatings.
4) YSZ for TBC chemistries are currently limited to 1528° K maximum temperature due to phase transformation issues. New chemistries have been adopted that present phase stability in higher temperatures. However they show significantly lower fracture toughness compared to the partially stabilized zirconia and it is certain that their erosion resistance will be even less. - The FIGURE shows a DVC-coating with fully and partially stabilized zirconia
- The problems named under
point 1 are addressed by adopting Dense Vertical Cracked (DVC) coatings. - 1) Erosion. DVC thermal barrier coatings have shown significantly lower rates compared to their porous counterparts. That means for the same chemistry a porous coating will show more than 3× the erosion rate compared to the DVC one.
2) DVC coatings have increased cohesion and adhesion compared to the typical porous coatings. The reason is that a very high ratio of fully molten particles deposit on hot substrate or hot previously deposited splats which promotes a good intimate bonding to develop between them. Improved adhesion requires high energy for a horizontal crack to propagate so that guarantees a lower delamination.
3) Coating life. Due to the intimate contact between splats, the DVC coatings show high fracture toughness along the parallel to the substrate plane. That, combined with their ability to accommodate thermal strain along the coating thickness due to their columnar microstructure ensures a high TBC life.
4) DVC microstructures can be adopted on the new coating chemistries. That will create a bilayer DVC with partially stabilized zirconia as a lower layer and fully stabilized zirconia as the upper layer. The lower layer will accommodate CTE mismatch with the bond coat and the TGO while the upper layer will provide the higher temperature capability. - The system consists of partially stabilized zirconia, especially 8YSZ as the high fracture toughness lower layer to accommodate the CTE mismatch with bond coat and TGO and a lower toughness upper layer of fully stabilized zirconia, especially 48YSZ to provide the high temperature capability.
- Unlike other possible bilayer coating approaches, the similar chemistry between the two coatings enhances their bonding.
- Appropriate preheating of the DVC PSZ will prepare its surface to receive the fully molten particles of FSZ and due to the high local temperatures during spraying allow diffusion between the two similar materials. Ideally a number of the vertical cracks will progress from one coating to the other demonstrating the continuity between the two coatings. In this manner the interface which has shown to be the weakest link in other bi-layer systems will be reinforced.
- The advantages that arise are:
- 1) The low fracture toughness of the FSZ with the adoption of a DVC microstructure will significantly increase. That will improve the erosion resistance of the coating.
2) A good bonding between the two layers and as well with the bond coat will increase the drilling damage tolerance. Less delamination will be observed compared to other bilayer coating systems which have suffered in the past from drilling.
3) The columnar microstructure along the bilayer coating thickness will allow improved strain tolerance, thus increased coating life.
4) Higher temperature capability compared to single layer DVC coatings. - The FIGURE shows a
layer system 1. - The
layer system 1 comprises asubstrate 4 which is preferably metallic and very preferably made of a nickel or cobalt based super alloy. - On the substrate 4 a bond coat especially a
metallic bond coat 7 and very especially a NiCoCrAlY-basedbond coat 7 is applied on. - On this
bond coat 7 there is a thermally grown oxide (TGO, not shown) layer which is formed during further application of the ceramic layers or by an additional oxidation step or at least during use of thelayer system 1. - On the
bond coat 7 there is applied afirst zirconia layer 10 made of a partially stabilized zirconia. - The thickness of the partially stabilized
zirconia layer 10 is preferable between 75 μm-800 μm. - The porosity of the partially stabilized
zirconia 10 is preferably lower than 5% and very preferably lower than 3%. - As an outer ceramic layer there is applied a fully stabilized
zirconia layer 13, which is especially the outer most layer of thelayer system 1. - This outer layer can also be made of a pyrochlore ceramic, such as gadolinium zirconate (GZO), which partially or fully replaces the fully stabilized zirconia (FSZ).
- The porosity of the fully stabilized
zirconia 13 is lower than 5% and preferably lower than 3%. - The thickness of the fully stabilized
zirconia 13 is preferable between 50 μm-800 μm. - The same parameters for thickness and porosity are also valid for the pyrochlore layer or pyrochlore/FSZ layer.
- The stabilization in this zirconia based system can be reached by yttria or by any other rare earth element as known by the state of the art or by a combination of that.
- Preferably yttrium is used for stabilization.
- In this
layers cracks 16 present, which 19 are mostly present in the outermost layer 13 and preferably some of them 21 are present in bothlayers - Although the invention has been illustrated and described in greater detail with reference to the preferred exemplary embodiment, the invention is not limited to the examples disclosed, and further variations can be inferred by a person skilled in the art, without departing from the scope of protection of the invention.
- For the sake of clarity, it is to be understood that the use of “a” or “an” throughout this application does not exclude a plurality, and “comprising” does not exclude other steps or elements.
Claims (13)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP15172884.7 | 2015-06-19 | ||
EP15172884.7A EP3106541A1 (en) | 2015-06-19 | 2015-06-19 | Dvc-coating with fully and partially stabilized zirconia |
PCT/EP2016/059828 WO2016202495A1 (en) | 2015-06-19 | 2016-05-03 | Dvc-coating with fully and partially stabilized zirconia |
Publications (1)
Publication Number | Publication Date |
---|---|
US20180179645A1 true US20180179645A1 (en) | 2018-06-28 |
Family
ID=53476716
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US15/736,340 Abandoned US20180179645A1 (en) | 2015-06-19 | 2016-05-03 | Dvc-coating with fully and partially stabilized zirconia |
Country Status (3)
Country | Link |
---|---|
US (1) | US20180179645A1 (en) |
EP (2) | EP3106541A1 (en) |
WO (1) | WO2016202495A1 (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2020131929A1 (en) * | 2018-12-18 | 2020-06-25 | Oerlikon Metco (Us) Inc. | Coating for protecting ebc and cmc layers and thermal spray coating method thereof |
JP2022533884A (en) * | 2019-03-22 | 2022-07-27 | シーメンス エナジー グローバル ゲゼルシャフト ミット ベシュレンクテル ハフツング ウント コンパニー コマンディートゲゼルシャフト | Stabilized zirconia in sealing system |
US20220371967A1 (en) * | 2021-05-18 | 2022-11-24 | Rolls-Royce Corporation | Cmas-resistant environmental barrier coating system |
US20220381151A1 (en) * | 2019-10-04 | 2022-12-01 | Siemens Energy Global GmbH & Co. KG | Composite layer system having an additively manufactured substrate and a ceramic thermal protection system |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102017206063A1 (en) * | 2017-04-10 | 2018-10-11 | Siemens Aktiengesellschaft | Partially and fully stabilized zirconium oxide powder as a ceramic layer |
US10550462B1 (en) * | 2017-09-08 | 2020-02-04 | United Technologies Corporation | Coating with dense columns separated by gaps |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7291403B2 (en) * | 2004-02-03 | 2007-11-06 | General Electric Company | Thermal barrier coating system |
DE602005021599D1 (en) * | 2004-12-14 | 2010-07-15 | Mitsubishi Heavy Ind Ltd | Component with thermal insulation layer and method for its production. |
-
2015
- 2015-06-19 EP EP15172884.7A patent/EP3106541A1/en not_active Withdrawn
-
2016
- 2016-05-03 WO PCT/EP2016/059828 patent/WO2016202495A1/en active Application Filing
- 2016-05-03 US US15/736,340 patent/US20180179645A1/en not_active Abandoned
- 2016-05-03 EP EP16722589.5A patent/EP3283667A1/en active Pending
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2020131929A1 (en) * | 2018-12-18 | 2020-06-25 | Oerlikon Metco (Us) Inc. | Coating for protecting ebc and cmc layers and thermal spray coating method thereof |
JP2022533884A (en) * | 2019-03-22 | 2022-07-27 | シーメンス エナジー グローバル ゲゼルシャフト ミット ベシュレンクテル ハフツング ウント コンパニー コマンディートゲゼルシャフト | Stabilized zirconia in sealing system |
JP7275306B2 (en) | 2019-03-22 | 2023-05-17 | シーメンス エナジー グローバル ゲゼルシャフト ミット ベシュレンクテル ハフツング ウント コンパニー コマンディートゲゼルシャフト | Stabilized zirconia in sealing system |
US20220381151A1 (en) * | 2019-10-04 | 2022-12-01 | Siemens Energy Global GmbH & Co. KG | Composite layer system having an additively manufactured substrate and a ceramic thermal protection system |
US20220371967A1 (en) * | 2021-05-18 | 2022-11-24 | Rolls-Royce Corporation | Cmas-resistant environmental barrier coating system |
Also Published As
Publication number | Publication date |
---|---|
EP3283667A1 (en) | 2018-02-21 |
EP3106541A1 (en) | 2016-12-21 |
WO2016202495A1 (en) | 2016-12-22 |
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Legal Events
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AS | Assignment |
Owner name: SIEMENS ENERGY, INC., FLORIDA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:HITCHMAN, NEIL;REEL/FRAME:045475/0277 Effective date: 20180319 Owner name: SIEMENS AKTIENGESELLSCHAFT, GERMANY Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:SIEMENS ENERGY, INC.;REEL/FRAME:045475/0350 Effective date: 20180322 Owner name: SIEMENS AKTIENGESELLSCHAFT, GERMANY Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:RENTERIA, ARTURO FLORES;STAMM, WERNER;ZOIS, DIMITRIOS;SIGNING DATES FROM 20171016 TO 20171023;REEL/FRAME:045475/0323 |
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STPP | Information on status: patent application and granting procedure in general |
Free format text: FINAL REJECTION MAILED |
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STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |