ES2538809T3 - Funda para uso sobre componentes de perfil aerodinámico - Google Patents
Funda para uso sobre componentes de perfil aerodinámico Download PDFInfo
- Publication number
- ES2538809T3 ES2538809T3 ES08250865.6T ES08250865T ES2538809T3 ES 2538809 T3 ES2538809 T3 ES 2538809T3 ES 08250865 T ES08250865 T ES 08250865T ES 2538809 T3 ES2538809 T3 ES 2538809T3
- Authority
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- Spain
- Prior art keywords
- aerodynamic profile
- alloy
- cover
- profile components
- cobalt
- 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.)
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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
- C23C30/00—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
-
- 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
-
- 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
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D1/00—Electroforming
-
- 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
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D3/00—Electroplating: Baths therefor
- C25D3/02—Electroplating: Baths therefor from solutions
- C25D3/56—Electroplating: Baths therefor from solutions of alloys
- C25D3/562—Electroplating: Baths therefor from solutions of alloys containing more than 50% by weight of iron or nickel or cobalt
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
- C25D5/48—After-treatment of electroplated surfaces
- C25D5/50—After-treatment of electroplated surfaces by heat-treatment
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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
- F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
-
- 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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
- F04D29/324—Blades
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
- C25D5/10—Electroplating with more than one layer of the same or of different metals
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
- C25D5/10—Electroplating with more than one layer of the same or of different metals
- C25D5/12—Electroplating with more than one layer of the same or of different metals at least one layer being of nickel or 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
- F05D2240/00—Components
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05D2240/303—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the leading edge of a rotor blade
-
- 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
- F05D2300/611—Coating
-
- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- 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
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12861—Group VIII or IB metal-base component
- Y10T428/12903—Cu-base component
-
- 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
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12861—Group VIII or IB metal-base component
- Y10T428/12903—Cu-base component
- Y10T428/1291—Next to Co-, Cu-, or Ni-base component
-
- 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
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12861—Group VIII or IB metal-base component
- Y10T428/12931—Co-, Fe-, or Ni-base components, alternative to each other
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Metallurgy (AREA)
- Mechanical Engineering (AREA)
- Electrochemistry (AREA)
- General Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Inorganic Chemistry (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Laminated Bodies (AREA)
Abstract
Un artículo para proteger un perfil aerodinámico (10), que comprende: una doble funda (126) que tiene un lado (28) externo y un lado (30) interno que forma una cavidad (32) para recibir el perfil aerodinámico, en donde una funda (26) sobre el lado externo comprende un material que tiene cobalto, caracterizado porque el material comprende también fósforo, y porque la doble funda incluye además una capa interna adyacente al lado interno, en donde la capa interna comprende un material de aleación elegido en un grupo consistente en una aleación de níquel, una aleación de níquel que tiene cobalto, cobre, aleación de cobre, una aleación de hierro, y acero.
Description
Claims (1)
-
imagen1 imagen2
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/752,355 US8088498B2 (en) | 2007-05-23 | 2007-05-23 | Electro-formed sheath for use on airfoil components |
| US752355 | 2007-05-23 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES2538809T3 true ES2538809T3 (es) | 2015-06-24 |
Family
ID=39764759
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES08250865.6T Active ES2538809T3 (es) | 2007-05-23 | 2008-03-13 | Funda para uso sobre componentes de perfil aerodinámico |
Country Status (3)
| Country | Link |
|---|---|
| US (2) | US8088498B2 (es) |
| EP (1) | EP1995412B1 (es) |
| ES (1) | ES2538809T3 (es) |
Families Citing this family (41)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8814527B2 (en) * | 2009-08-07 | 2014-08-26 | Hamilton Sundstrand Corporation | Titanium sheath and airfoil assembly |
| US20110116906A1 (en) | 2009-11-17 | 2011-05-19 | Smith Blair A | Airfoil component wear indicator |
| US8376712B2 (en) * | 2010-01-26 | 2013-02-19 | United Technologies Corporation | Fan airfoil sheath |
| US8858182B2 (en) | 2011-06-28 | 2014-10-14 | United Technologies Corporation | Fan blade with sheath |
| US20130004324A1 (en) * | 2011-06-30 | 2013-01-03 | United Technologies Corporation | Nano-structured fan airfoil sheath |
| US8858184B2 (en) | 2011-09-21 | 2014-10-14 | Textron Innovations Inc. | Rotor blade erosion protection system |
| US8956115B2 (en) | 2012-01-20 | 2015-02-17 | General Electric Company | Blade extension and rotor blade assembly for wind turbine |
| US20130199934A1 (en) * | 2012-02-06 | 2013-08-08 | United Technologies Corporation | Electroformed sheath |
| US9140130B2 (en) | 2012-03-08 | 2015-09-22 | United Technologies Corporation | Leading edge protection and method of making |
| FR2989991B1 (fr) * | 2012-04-30 | 2016-01-08 | Snecma | Renfort structurel metallique d'aube de turbomachine |
| US20130299453A1 (en) * | 2012-05-14 | 2013-11-14 | United Technologies Corporation | Method for making metal plated gas turbine engine components |
| JP5980350B2 (ja) * | 2012-12-27 | 2016-08-31 | 三菱重工業株式会社 | 風車翼及びそれを備えた風力発電装置 |
| US9470097B2 (en) * | 2013-03-14 | 2016-10-18 | Rolls-Royce Corporation | Airfoil with leading edge reinforcement |
| WO2014143260A1 (en) * | 2013-03-15 | 2014-09-18 | United Technologies Corporation | Leading edge sheath manufacturing method |
| WO2015006421A1 (en) | 2013-07-09 | 2015-01-15 | United Technologies Corporation | Metal-encapsulated polymeric article |
| WO2015006488A1 (en) * | 2013-07-09 | 2015-01-15 | United Technologies Corporation | Plating a composite to enhance bonding of metallic components |
| WO2015017095A2 (en) | 2013-07-09 | 2015-02-05 | United Technologies Corporation | Plated polymer nosecone |
| US10927843B2 (en) | 2013-07-09 | 2021-02-23 | Raytheon Technologies Corporation | Plated polymer compressor |
| US10227704B2 (en) * | 2013-07-09 | 2019-03-12 | United Technologies Corporation | High-modulus coating for local stiffening of airfoil trailing edges |
| CA2917884A1 (en) | 2013-07-09 | 2015-01-15 | United Technologies Corporation | Plated polymer fan |
| WO2015006487A1 (en) | 2013-07-09 | 2015-01-15 | United Technologies Corporation | Erosion and wear protection for composites and plated polymers |
| EP3090127B1 (en) | 2013-12-23 | 2020-05-06 | United Technologies Corporation | Fan blade with adhesive fabric stackup |
| JP2017514018A (ja) * | 2014-04-17 | 2017-06-01 | ゼネラル・エレクトリック・カンパニイ | 前縁部ガードを製造するための方法 |
| US9920444B2 (en) * | 2014-05-22 | 2018-03-20 | The Boeing Company | Co-bonded electroformed abrasion strip |
| GB201420512D0 (en) * | 2014-11-19 | 2014-12-31 | Rolls Royce Plc | Shield |
| US20160238021A1 (en) * | 2015-02-16 | 2016-08-18 | United Technologies Corporation | Compressor Airfoil |
| CN105177677A (zh) * | 2015-08-18 | 2015-12-23 | 苏州尚康新材料科技有限公司 | 一种硬质颗粒强化的凸包状耐磨镀镍层的制备方法 |
| DE102015115190A1 (de) | 2015-09-09 | 2017-03-09 | Fichtner & Schicht GmbH | Windenergieanlage |
| EP3504428A1 (en) | 2016-09-27 | 2019-07-03 | Siemens Gamesa Renewable Energy A/S | Protective cover system for protecting a leading edge of a wind turbine rotor blade |
| ES2991889T3 (es) * | 2016-09-27 | 2024-12-05 | Siemens Gamesa Renewable Energy As | Sistema de cubierta protectora |
| DE102016221871A1 (de) * | 2016-11-08 | 2018-05-09 | Siemens Aktiengesellschaft | Gasturbinenbauteil und Verfahren zum Herstellen eines erosionsgeschützten Gasturbinenbauteils |
| US10428660B2 (en) * | 2017-01-31 | 2019-10-01 | United Technologies Corporation | Hybrid airfoil cooling |
| WO2018157929A1 (de) | 2017-03-02 | 2018-09-07 | Fichtner & Schicht GmbH | Windenergieanlagenrotorblatt mit einer erosionsschutzanordnung |
| US10612386B2 (en) | 2017-07-17 | 2020-04-07 | Rolls-Royce Corporation | Apparatus for airfoil leading edge protection |
| JP6968006B2 (ja) | 2018-03-09 | 2021-11-17 | 三菱重工業株式会社 | 前縁カバー部材、前縁カバー部材ユニット、複合材翼、前縁カバー部材の製造方法及び複合材翼の製造方法 |
| JP6735299B2 (ja) * | 2018-03-09 | 2020-08-05 | 三菱重工業株式会社 | 複合材翼、前縁金属カバー形成ユニット、複合材翼の製造方法 |
| GB2600148A (en) * | 2020-10-23 | 2022-04-27 | Blade Dynamics Ltd | A wind turbine rotor blade assembly with an erosion shield |
| GB2602463A (en) * | 2020-12-28 | 2022-07-06 | Blade Dynamics Ltd | Protective cap for a leading edge of a wind turbine blade |
| US11725524B2 (en) | 2021-03-26 | 2023-08-15 | General Electric Company | Engine airfoil metal edge |
| US11988103B2 (en) * | 2021-10-27 | 2024-05-21 | General Electric Company | Airfoils for a fan section of a turbine engine |
| US11767607B1 (en) | 2022-07-13 | 2023-09-26 | General Electric Company | Method of depositing a metal layer on a component |
Family Cites Families (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3753667A (en) * | 1968-01-16 | 1973-08-21 | Gen Am Transport | Articles having electroless metal coatings incorporating wear-resisting particles therein |
| US4010530A (en) * | 1975-07-24 | 1977-03-08 | United Technologies Corporation | Method for making blade protective sheaths |
| US4366034A (en) * | 1981-06-04 | 1982-12-28 | Westinghouse Electric Corp. | Hard chromium plating process for cobalt-chromium-tungsten alloys |
| US4441857A (en) * | 1981-09-25 | 1984-04-10 | Union Carbide Corporation | Wear resistant fan blade for centrifugal fan |
| US4943485A (en) * | 1981-11-27 | 1990-07-24 | S R I International | Process for applying hard coatings and the like to metals and resulting product |
| US4673468A (en) * | 1985-05-09 | 1987-06-16 | Burlington Industries, Inc. | Commercial nickel phosphorus electroplating |
| US4681817A (en) * | 1984-12-24 | 1987-07-21 | Kabushiki Kaisha Riken | Piston ring |
| US4802828A (en) * | 1986-12-29 | 1989-02-07 | United Technologies Corporation | Turbine blade having a fused metal-ceramic tip |
| JPS63282295A (ja) * | 1987-05-15 | 1988-11-18 | Riken Corp | 耐摩耗表面層 |
| US4950375A (en) * | 1989-05-26 | 1990-08-21 | United Technologies Corporation | Die for electroforming a part |
| DE4208842C1 (es) * | 1992-03-19 | 1993-04-08 | Eurocopter Hubschrauber Gmbh, 8000 Muenchen, De | |
| ATE223518T1 (de) * | 1994-03-17 | 2002-09-15 | Westaim Corp | Überzüge mit niedriger reibung auf der basis von kobalt auf titan |
| US5427866A (en) * | 1994-03-28 | 1995-06-27 | General Electric Company | Platinum, rhodium, or palladium protective coatings in thermal barrier coating systems |
| US5908285A (en) * | 1995-03-10 | 1999-06-01 | United Technologies Corporation | Electroformed sheath |
| US5674370A (en) * | 1995-03-31 | 1997-10-07 | Optical Radiation Corporation | Method of electroforming an abrasion shield |
| US5881972A (en) * | 1997-03-05 | 1999-03-16 | United Technologies Corporation | Electroformed sheath and airfoiled component construction |
| FR2763605B1 (fr) * | 1997-05-22 | 1999-07-02 | Snecma | Revetement de protection de pieces metalliques ayant une bonne resistance a la corrosion en atmosphere saline, et pieces metalliques comportant un tel revetement de protection |
| JP4240808B2 (ja) * | 1997-10-27 | 2009-03-18 | シーメンス パワー ジェネレイション インコーポレイテッド | タービン翼の製造方法 |
| US6037004A (en) * | 1997-12-19 | 2000-03-14 | United Technologies Corporation | Shield and method for protecting an airfoil surface |
| US6341747B1 (en) * | 1999-10-28 | 2002-01-29 | United Technologies Corporation | Nanocomposite layered airfoil |
| US20050170201A1 (en) * | 2004-02-04 | 2005-08-04 | The Boeing Company | Cobalt-phosphorous-boron coating and process for plating |
| US20060040126A1 (en) * | 2004-08-18 | 2006-02-23 | Richardson Rick A | Electrolytic alloys with co-deposited particulate matter |
| US7897265B2 (en) | 2006-01-26 | 2011-03-01 | Hamilton Sundstrand Corporation | Low cost, environmentally favorable, chromium plate replacement coating for improved wear performance |
-
2007
- 2007-05-23 US US11/752,355 patent/US8088498B2/en not_active Expired - Fee Related
-
2008
- 2008-03-13 ES ES08250865.6T patent/ES2538809T3/es active Active
- 2008-03-13 EP EP08250865.6A patent/EP1995412B1/en not_active Not-in-force
-
2011
- 2011-11-16 US US13/297,352 patent/US8764959B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| EP1995412A3 (en) | 2012-12-05 |
| US8764959B2 (en) | 2014-07-01 |
| EP1995412A2 (en) | 2008-11-26 |
| EP1995412B1 (en) | 2015-05-27 |
| US20120061243A1 (en) | 2012-03-15 |
| US8088498B2 (en) | 2012-01-03 |
| US20100014964A1 (en) | 2010-01-21 |
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