EP2044231A1 - Component with a reinforcing plating - Google Patents
Component with a reinforcing platingInfo
- Publication number
- EP2044231A1 EP2044231A1 EP07722169A EP07722169A EP2044231A1 EP 2044231 A1 EP2044231 A1 EP 2044231A1 EP 07722169 A EP07722169 A EP 07722169A EP 07722169 A EP07722169 A EP 07722169A EP 2044231 A1 EP2044231 A1 EP 2044231A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- weight
- component
- cover layer
- metallic
- armor
- 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.)
- Granted
Links
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
- C23C28/02—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 only coatings only including layers of metallic material
- C23C28/027—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 only coatings only including layers of metallic material including at least one metal matrix material comprising a mixture of at least two metals or metal phases or metal matrix composites, e.g. metal matrix with embedded inorganic hard particles, CERMET, MMC.
-
- 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
- C23C28/02—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 only coatings only including layers of metallic material
- C23C28/021—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 only coatings only including layers of metallic material including at least one metal alloy layer
- C23C28/022—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 only coatings only including layers of metallic material including at least one metal alloy layer with at least one MCrAlX 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
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
- C23C4/06—Metallic material
- C23C4/073—Metallic material containing MCrAl or MCrAlY alloys, where M is nickel, cobalt or iron, with or without non-metal elements
-
- 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
- C23C4/129—Flame spraying
-
- 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
- C23C4/18—After-treatment
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D15/00—Electrolytic or electrophoretic production of coatings containing embedded materials, e.g. particles, whiskers, wires
- C25D15/02—Combined electrolytic and electrophoretic processes with charged 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
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12486—Laterally noncoextensive components [e.g., embedded, etc.]
Definitions
- the invention relates to a component, in particular a gas turbine component such as a blade, with an armor, in particular a blade tip armor, according to the preamble of claim 1.
- Turbomachines such as gas turbines, typically include a plurality of rotating blades and a plurality of stationary vanes, the blades rotating together with a rotor, and the blades and vanes being enclosed by a fixed housing. To increase performance, it is important to optimize all components and subsystems. These include the so-called sealing systems.
- blades in the compressor have no shroud. Therefore, tips of the blades are exposed to so-called rubbing into the fixed housing in direct frictional contact with the housing. Such a rubbing of the tips of the blades into the housing is caused by setting a minimum radial gap by manufacturing tolerances. As is removed by the frictional contact of the tips of the blades on the same material, over the entire circumference of the housing and rotor can set an undesirable gap magnification.
- Two different types of blade tips are known from the prior art.
- the present invention relates to an armor, in particular a blade tip armor, a component, in particular a gas turbine blade, with abrasive particles.
- US 6,194,086 Bl discloses a blade of a gas turbine with a blade tip armor, wherein the blade tip armor comprises a cover layer, which is formed from in a metallic matrix material embedded abrasive particles.
- the cover layer of the abrasive particles embedded in the metallic matrix material is applied to the tip of a blade to be coated with the interposition of a metallic adhesion-promoting layer.
- the metallic adhesive layer is formed as LPPS layer and therefore applied to the component via a so-called low pressure plasma spraying.
- the disadvantage of such LPPS adhesive layers is that they have a low mechanical adhesion to the blade tip, especially at high operating temperatures of up to 1200 ° C., so that the blade tip armor may flake off during operation.
- the present invention based on the problem of creating a novel component with an armor.
- This problem is solved by a component in the sense of claim 1.
- the metallic adhesive layer is formed as an adhesive layer applied to the component via high-speed flame spraying, wherein the metallic matrix material of the cover layer is electrodeposited.
- the adhesive layer is applied to the component via high-speed flame spraying.
- the armor adheres better to the component at high temperatures than when using LPPS adhesive layers.
- the blade tip armor of the component therefore has a higher mechanical adhesion, especially at high operating temperatures.
- Fig. 1 a schematic cross section through an applied on a component
- the invention relates to an armored component, in particular a blade provided with a blade tip armor of a gas turbine.
- the blade of the gas turbine is designed as a high-pressure compressor blade.
- FIG. 1 shows a highly schematic cross section through a blade tip 10 of a blade, wherein the blade tip 10 of the blade carries a blade tip armor 11.
- the blade tip armor 11 has at least two layers, namely an outer cover layer 12 and an inner adhesive layer 13.
- the cover layer 12 is applied to the blade tip 10 via the adhesive layer 13.
- additional additional layers may be present between the cover layer 12 and the adhesion layer 13.
- the cover layer 12 is formed by abrasive particles 14, which are embedded in a metallic matrix material 15.
- the adhesive layer 13 is designed as a metallic adhesive layer.
- the metallic adhesive layer 13 and the metallic matrix material 15 of the cover layer 12 are each formed from a MCr Al Y material.
- the metallic adhesive layer 13 is formed as a high-speed flame spraying (HVOF) applied to the component adhesive layer.
- HVOF high-speed flame spraying
- the metallic matrix material 15 of the cover layer 12 is electrodeposited.
- the abrasive particles 14 are embedded, which are preferably formed as hard particles of cubic boron nitride.
- the metallic matrix material 15 of the cover layer 12 and the metallic adhesion layer 13 are each formed from a MCr Al Y material which preferably has the following composition:
- Cr chromium
- Co cobalt
- Al aluminum
- Ta tantalum
- Re rhenium
- Hf hafnium
- Si silicon
- Y yttrium
- composition of the MCrAlY material is particularly preferred.
- Cr chromium
- Co cobalt
- Al aluminum
- Ta tantalum
- Re rhenium
- Hf hafnium
- Si silicon
- Y yttrium
- a blade is provided with a blade tip armor, wherein the blade tip armor a high speed flame-spray adhesive layer which serves to connect the blade tip armor 11 to the blade tip 10, and wherein the Hochgeschwindig- Flammspritz adhesive layer 13 has a high mechanical strength, especially at high operating temperatures.
- the adhesion layer 13 carries the cover layer 12, which is formed from abrasive particles 14 embedded in the metallic matrix material 15, the metallic matrix material 15 of the cover layer 12 being electrodeposited.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Organic Chemistry (AREA)
- Metallurgy (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Composite Materials (AREA)
- General Engineering & Computer Science (AREA)
- Inorganic Chemistry (AREA)
- Electrochemistry (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Coating By Spraying Or Casting (AREA)
Abstract
Description
Claims
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL07722169T PL2044231T3 (en) | 2006-04-11 | 2007-04-04 | Component with a reinforcing plating |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102006016995A DE102006016995A1 (en) | 2006-04-11 | 2006-04-11 | Component with an armor |
PCT/DE2007/000611 WO2007115551A1 (en) | 2006-04-11 | 2007-04-04 | Component with a reinforcing plating |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2044231A1 true EP2044231A1 (en) | 2009-04-08 |
EP2044231B1 EP2044231B1 (en) | 2009-12-30 |
Family
ID=38180702
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP07722169A Expired - Fee Related EP2044231B1 (en) | 2006-04-11 | 2007-04-04 | Component with a reinforcing plating |
Country Status (5)
Country | Link |
---|---|
US (1) | US20090311552A1 (en) |
EP (1) | EP2044231B1 (en) |
DE (2) | DE102006016995A1 (en) |
PL (1) | PL2044231T3 (en) |
WO (1) | WO2007115551A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3597860A1 (en) * | 2018-07-19 | 2020-01-22 | United Technologies Corporation | Coating to improve oxidation and corrosion resistance of abrasive tip system |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102008003100A1 (en) * | 2008-01-03 | 2009-07-16 | Mtu Aero Engines Gmbh | Solder coating, method for coating a component, component and adhesive tape with a solder coating |
DE102008056741A1 (en) * | 2008-11-11 | 2010-05-12 | Mtu Aero Engines Gmbh | Wear protection layer for Tial |
DE102009018685A1 (en) * | 2009-04-23 | 2010-10-28 | Mtu Aero Engines Gmbh | Method for producing an armor of a blade tip as well as correspondingly produced blades and gas turbines |
DE102009031313B4 (en) | 2009-06-30 | 2018-07-05 | MTU Aero Engines AG | Coating and method for coating a component |
US20120128525A1 (en) * | 2010-11-24 | 2012-05-24 | Kulkarni Anand A | Metallic Bondcoat or Alloy with a High y/y' Transition Temperature and a Component |
US20140037970A1 (en) * | 2012-08-03 | 2014-02-06 | General Electric Company | Reinforced articles and methods of making the same |
DE102013218687A1 (en) * | 2013-09-18 | 2015-04-02 | MTU Aero Engines AG | Galvanized wear protection coating and method therefor |
US20160237832A1 (en) * | 2015-02-12 | 2016-08-18 | United Technologies Corporation | Abrasive blade tip with improved wear at high interaction rate |
US10450876B2 (en) | 2015-04-15 | 2019-10-22 | United Technologies Corporation | Abrasive tip blade manufacture methods |
US10544699B2 (en) * | 2017-12-19 | 2020-01-28 | Rolls-Royce Corporation | System and method for minimizing the turbine blade to vane platform overlap gap |
US11073028B2 (en) | 2018-07-19 | 2021-07-27 | Raytheon Technologies Corporation | Turbine abrasive blade tips with improved resistance to oxidation |
US11028721B2 (en) | 2018-07-19 | 2021-06-08 | Ratheon Technologies Corporation | Coating to improve oxidation and corrosion resistance of abrasive tip system |
US11536151B2 (en) | 2020-04-24 | 2022-12-27 | Raytheon Technologies Corporation | Process and material configuration for making hot corrosion resistant HPC abrasive blade tips |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5316866A (en) * | 1991-09-09 | 1994-05-31 | General Electric Company | Strengthened protective coatings for superalloys |
US5584663A (en) * | 1994-08-15 | 1996-12-17 | General Electric Company | Environmentally-resistant turbine blade tip |
US5935407A (en) * | 1997-11-06 | 1999-08-10 | Chromalloy Gas Turbine Corporation | Method for producing abrasive tips for gas turbine blades |
DE19905811A1 (en) * | 1999-02-12 | 2000-08-17 | Erwin Huehne | High speed flame spray gun for thermal spraying of rod, wire or powder-form filler materials, has connection constructed so that liquid and gaseous fuels and oxidation gas can be directed separately into combustion chamber |
NL1014924C2 (en) * | 1999-07-30 | 2001-02-01 | Chromalloy Holland B V | Limitation of air resistance for components of a gas turbine engine. |
US6706319B2 (en) * | 2001-12-05 | 2004-03-16 | Siemens Westinghouse Power Corporation | Mixed powder deposition of components for wear, erosion and abrasion resistant applications |
US7547478B2 (en) * | 2002-12-13 | 2009-06-16 | General Electric Company | Article including a substrate with a metallic coating and a protective coating thereon, and its preparation and use in component restoration |
-
2006
- 2006-04-11 DE DE102006016995A patent/DE102006016995A1/en not_active Withdrawn
-
2007
- 2007-04-04 WO PCT/DE2007/000611 patent/WO2007115551A1/en active Application Filing
- 2007-04-04 US US12/296,985 patent/US20090311552A1/en not_active Abandoned
- 2007-04-04 EP EP07722169A patent/EP2044231B1/en not_active Expired - Fee Related
- 2007-04-04 DE DE502007002499T patent/DE502007002499D1/en active Active
- 2007-04-04 PL PL07722169T patent/PL2044231T3/en unknown
Non-Patent Citations (1)
Title |
---|
See references of WO2007115551A1 * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3597860A1 (en) * | 2018-07-19 | 2020-01-22 | United Technologies Corporation | Coating to improve oxidation and corrosion resistance of abrasive tip system |
Also Published As
Publication number | Publication date |
---|---|
DE502007002499D1 (en) | 2010-02-11 |
DE102006016995A1 (en) | 2007-10-18 |
EP2044231B1 (en) | 2009-12-30 |
PL2044231T3 (en) | 2010-06-30 |
US20090311552A1 (en) | 2009-12-17 |
WO2007115551A1 (en) | 2007-10-18 |
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