CN103817032B - 微通道涂层沉积系统和用于使用其的方法 - Google Patents
微通道涂层沉积系统和用于使用其的方法 Download PDFInfo
- Publication number
- CN103817032B CN103817032B CN201310443055.5A CN201310443055A CN103817032B CN 103817032 B CN103817032 B CN 103817032B CN 201310443055 A CN201310443055 A CN 201310443055A CN 103817032 B CN103817032 B CN 103817032B
- Authority
- CN
- China
- Prior art keywords
- pressurization
- pressure
- masking
- coating material
- fluid
- 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.)
- Expired - Fee Related
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
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/01—Selective coating, e.g. pattern coating, without pre-treatment of the material to be coated
-
- 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
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D3/00—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D7/00—Processes, other than flocking, specially adapted for applying liquids or other fluent materials to particular surfaces or for applying particular liquids or other fluent materials
- B05D7/22—Processes, other than flocking, specially adapted for applying liquids or other fluent materials to particular surfaces or for applying particular liquids or other fluent materials to internal surfaces, e.g. of tubes
-
- 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
- C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
- C23C4/10—Oxides, borides, carbides, nitrides or silicides; Mixtures thereof
- C23C4/11—Oxides
-
- 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
-
- 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
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
-
- 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
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D3/00—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials
- B05D3/04—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by exposure to gases
- B05D3/0406—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by exposure to gases the gas being air
- B05D3/042—Directing or stopping the fluid to be coated with air
-
- 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
- F05D2230/30—Manufacture with deposition of material
- F05D2230/31—Layer deposition
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/204—Heat transfer, e.g. cooling by the use of microcircuits
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Plasma & Fusion (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Physics & Mathematics (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Life Sciences & Earth Sciences (AREA)
- Wood Science & Technology (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Coating By Spraying Or Casting (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/627,158 US8974859B2 (en) | 2012-09-26 | 2012-09-26 | Micro-channel coating deposition system and method for using the same |
| US13/627158 | 2012-09-26 | ||
| US13/627,158 | 2012-09-26 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103817032A CN103817032A (zh) | 2014-05-28 |
| CN103817032B true CN103817032B (zh) | 2017-12-05 |
Family
ID=50235477
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310443055.5A Expired - Fee Related CN103817032B (zh) | 2012-09-26 | 2013-09-26 | 微通道涂层沉积系统和用于使用其的方法 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US8974859B2 (https=) |
| JP (1) | JP6200740B2 (https=) |
| CN (1) | CN103817032B (https=) |
| CH (1) | CH706983A2 (https=) |
| DE (1) | DE102013110069A1 (https=) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8387245B2 (en) * | 2010-11-10 | 2013-03-05 | General Electric Company | Components with re-entrant shaped cooling channels and methods of manufacture |
| DE102013109116A1 (de) * | 2012-08-27 | 2014-03-27 | General Electric Company (N.D.Ges.D. Staates New York) | Bauteil mit Kühlkanälen und Verfahren zur Herstellung |
| EP2995863B1 (en) * | 2014-09-09 | 2018-05-23 | United Technologies Corporation | Single-walled combustor for a gas turbine engine and method of manufacture |
| US10458259B2 (en) * | 2016-05-12 | 2019-10-29 | General Electric Company | Engine component wall with a cooling circuit |
| US10767489B2 (en) | 2016-08-16 | 2020-09-08 | General Electric Company | Component for a turbine engine with a hole |
| US10508551B2 (en) | 2016-08-16 | 2019-12-17 | General Electric Company | Engine component with porous trench |
| US10612389B2 (en) | 2016-08-16 | 2020-04-07 | General Electric Company | Engine component with porous section |
| FR3070693B1 (fr) * | 2017-09-07 | 2022-06-10 | Safran | Procede et dispositif de depot de revetement pour des composants multi-perfores de moteur d'aeronef avec soufflage des events |
| CN107574401B (zh) * | 2017-09-19 | 2019-06-25 | 江阴恩特莱特镀膜科技有限公司 | 一种用于等离子喷涂靶材的风冷装置 |
| CN110144542B (zh) * | 2019-06-21 | 2021-06-15 | 南昌航空大学 | 一种超音速火焰喷涂系统及铁基非晶涂层的制备方法 |
| US11313237B2 (en) * | 2020-05-08 | 2022-04-26 | General Electric Company | Conforming coating mask for a component and system background |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4402992A (en) * | 1981-12-07 | 1983-09-06 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Covering solid, film cooled surfaces with a duplex thermal barrier coating |
| FR2680120A1 (fr) * | 1991-08-08 | 1993-02-12 | Snecma | Procede et dispositif de revetement de surfaces munies de perforations par projection, notamment pour la metallisation par du plasma. |
| US6365013B1 (en) * | 1997-11-03 | 2002-04-02 | Siemens Aktiengesellschaft | Coating method and device |
| CN102235242A (zh) * | 2010-04-22 | 2011-11-09 | 通用电气公司 | 热气体通路构件冷却系统 |
| CN102443752A (zh) * | 2010-10-07 | 2012-05-09 | 苏舍美特科公司 | 保持冷却空气孔畅通的热喷涂工艺 |
| CN102536332A (zh) * | 2010-11-10 | 2012-07-04 | 通用电气公司 | 具有凹形冷却通道的部件及其制造方法 |
Family Cites Families (51)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4487550A (en) | 1983-01-27 | 1984-12-11 | The United States Of America As Represented By The Secretary Of The Air Force | Cooled turbine blade tip closure |
| US4893987A (en) | 1987-12-08 | 1990-01-16 | General Electric Company | Diffusion-cooled blade tip cap |
| US5660523A (en) | 1992-02-03 | 1997-08-26 | General Electric Company | Turbine blade squealer tip peripheral end wall with cooling passage arrangement |
| JP3137527B2 (ja) | 1994-04-21 | 2001-02-26 | 三菱重工業株式会社 | ガスタービン動翼チップ冷却装置 |
| US5640767A (en) | 1995-01-03 | 1997-06-24 | Gen Electric | Method for making a double-wall airfoil |
| US5626462A (en) | 1995-01-03 | 1997-05-06 | General Electric Company | Double-wall airfoil |
| US6383602B1 (en) | 1996-12-23 | 2002-05-07 | General Electric Company | Method for improving the cooling effectiveness of a gaseous coolant stream which flows through a substrate, and related articles of manufacture |
| US5875549A (en) | 1997-03-17 | 1999-03-02 | Siemens Westinghouse Power Corporation | Method of forming internal passages within articles and articles formed by same |
| DE19737845C2 (de) | 1997-08-29 | 1999-12-02 | Siemens Ag | Verfahren zum Herstellen einer Gasturbinenschaufel, sowie nach dem Verfahren hergestellte Gasturbinenschaufel |
| US6214248B1 (en) | 1998-11-12 | 2001-04-10 | General Electric Company | Method of forming hollow channels within a component |
| US6321449B2 (en) | 1998-11-12 | 2001-11-27 | General Electric Company | Method of forming hollow channels within a component |
| US6086328A (en) | 1998-12-21 | 2000-07-11 | General Electric Company | Tapered tip turbine blade |
| US6059530A (en) | 1998-12-21 | 2000-05-09 | General Electric Company | Twin rib turbine blade |
| US6190129B1 (en) | 1998-12-21 | 2001-02-20 | General Electric Company | Tapered tip-rib turbine blade |
| US6231307B1 (en) | 1999-06-01 | 2001-05-15 | General Electric Company | Impingement cooled airfoil tip |
| DE59909337D1 (de) | 1999-06-03 | 2004-06-03 | Alstom Technology Ltd Baden | Verfahren zur Herstellung oder zur Reparatur von Kühlkanälen in einstristallinen Komponenten von Gasturbinen |
| US6164914A (en) | 1999-08-23 | 2000-12-26 | General Electric Company | Cool tip blade |
| US6234755B1 (en) | 1999-10-04 | 2001-05-22 | General Electric Company | Method for improving the cooling effectiveness of a gaseous coolant stream, and related articles of manufacture |
| DE10024302A1 (de) | 2000-05-17 | 2001-11-22 | Alstom Power Nv | Verfahren zur Herstellung eines thermisch belasteten Gussteils |
| US6368060B1 (en) | 2000-05-23 | 2002-04-09 | General Electric Company | Shaped cooling hole for an airfoil |
| US6617003B1 (en) | 2000-11-06 | 2003-09-09 | General Electric Company | Directly cooled thermal barrier coating system |
| US6427327B1 (en) | 2000-11-29 | 2002-08-06 | General Electric Company | Method of modifying cooled turbine components |
| US6551061B2 (en) | 2001-03-27 | 2003-04-22 | General Electric Company | Process for forming micro cooling channels inside a thermal barrier coating system without masking material |
| US6461107B1 (en) | 2001-03-27 | 2002-10-08 | General Electric Company | Turbine blade tip having thermal barrier coating-formed micro cooling channels |
| US6461108B1 (en) | 2001-03-27 | 2002-10-08 | General Electric Company | Cooled thermal barrier coating on a turbine blade tip |
| US6494678B1 (en) | 2001-05-31 | 2002-12-17 | General Electric Company | Film cooled blade tip |
| US6602052B2 (en) | 2001-06-20 | 2003-08-05 | Alstom (Switzerland) Ltd | Airfoil tip squealer cooling construction |
| DE50214917D1 (de) * | 2001-07-11 | 2011-04-07 | Alstom Technology Ltd | Verfahren zur Beschichtung eines Hochtemperatur-beständigen Bauteils mit einer thermischen Schutzschicht und Hochtemperatur-beständiges Bauteil |
| US6602053B2 (en) | 2001-08-02 | 2003-08-05 | Siemens Westinghouse Power Corporation | Cooling structure and method of manufacturing the same |
| EP1295969A1 (en) | 2001-09-22 | 2003-03-26 | ALSTOM (Switzerland) Ltd | Method of growing a MCrAIY-coating and an article coated with the MCrAIY-coating |
| EP1295970A1 (en) | 2001-09-22 | 2003-03-26 | ALSTOM (Switzerland) Ltd | MCrAlY type alloy coating |
| US6634860B2 (en) | 2001-12-20 | 2003-10-21 | General Electric Company | Foil formed structure for turbine airfoil tip |
| US6921014B2 (en) | 2002-05-07 | 2005-07-26 | General Electric Company | Method for forming a channel on the surface of a metal substrate |
| EP1365039A1 (en) | 2002-05-24 | 2003-11-26 | ALSTOM (Switzerland) Ltd | Process of masking colling holes of a gas turbine component |
| EP1387040B1 (en) | 2002-08-02 | 2006-12-06 | ALSTOM Technology Ltd | Method of protecting partial areas of a component |
| US6878046B2 (en) | 2002-11-08 | 2005-04-12 | Safety-Kleen Systems, Inc. | Cleaning apparatus |
| US6994514B2 (en) | 2002-11-20 | 2006-02-07 | Mitsubishi Heavy Industries, Ltd. | Turbine blade and gas turbine |
| US7216428B2 (en) | 2003-03-03 | 2007-05-15 | United Technologies Corporation | Method for turbine element repairing |
| US6905302B2 (en) | 2003-09-17 | 2005-06-14 | General Electric Company | Network cooled coated wall |
| US7805822B2 (en) | 2003-12-15 | 2010-10-05 | Turbocombustor Technology, Inc. | Process for removing thermal barrier coatings |
| US7186167B2 (en) | 2004-04-15 | 2007-03-06 | United Technologies Corporation | Suspended abrasive waterjet hole drilling system and method |
| US7302990B2 (en) | 2004-05-06 | 2007-12-04 | General Electric Company | Method of forming concavities in the surface of a metal component, and related processes and articles |
| EP1828544B1 (de) | 2004-12-24 | 2011-06-22 | Alstom Technology Ltd | Verfahren zur herstellung eines bauteils mit eingebettetem kanal sowie bauteil |
| US7334991B2 (en) | 2005-01-07 | 2008-02-26 | Siemens Power Generation, Inc. | Turbine blade tip cooling system |
| US7622160B2 (en) * | 2006-07-28 | 2009-11-24 | General Electric Company | Method for concurrent thermal spray and cooling hole cleaning |
| US7766617B1 (en) | 2007-03-06 | 2010-08-03 | Florida Turbine Technologies, Inc. | Transpiration cooled turbine airfoil |
| US7775768B2 (en) | 2007-03-06 | 2010-08-17 | United Technologies Corporation | Turbine component with axially spaced radially flowing microcircuit cooling channels |
| EP2100984A1 (en) | 2008-03-14 | 2009-09-16 | Siemens Aktiengesellschaft | Method for masking cooling holes and device for using in a masking process for masking cooling holes |
| US8147196B2 (en) | 2009-05-05 | 2012-04-03 | Siemens Energy, Inc. | Turbine airfoil with a compliant outer wall |
| JP2012072705A (ja) * | 2010-09-29 | 2012-04-12 | Hitachi Ltd | ガスタービン翼の製造方法 |
| US8727727B2 (en) * | 2010-12-10 | 2014-05-20 | General Electric Company | Components with cooling channels and methods of manufacture |
-
2012
- 2012-09-26 US US13/627,158 patent/US8974859B2/en active Active
-
2013
- 2013-09-12 DE DE201310110069 patent/DE102013110069A1/de active Pending
- 2013-09-16 CH CH01580/13A patent/CH706983A2/en not_active Application Discontinuation
- 2013-09-24 JP JP2013196385A patent/JP6200740B2/ja active Active
- 2013-09-26 CN CN201310443055.5A patent/CN103817032B/zh not_active Expired - Fee Related
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4402992A (en) * | 1981-12-07 | 1983-09-06 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Covering solid, film cooled surfaces with a duplex thermal barrier coating |
| FR2680120A1 (fr) * | 1991-08-08 | 1993-02-12 | Snecma | Procede et dispositif de revetement de surfaces munies de perforations par projection, notamment pour la metallisation par du plasma. |
| US6365013B1 (en) * | 1997-11-03 | 2002-04-02 | Siemens Aktiengesellschaft | Coating method and device |
| CN102235242A (zh) * | 2010-04-22 | 2011-11-09 | 通用电气公司 | 热气体通路构件冷却系统 |
| CN102443752A (zh) * | 2010-10-07 | 2012-05-09 | 苏舍美特科公司 | 保持冷却空气孔畅通的热喷涂工艺 |
| CN102536332A (zh) * | 2010-11-10 | 2012-07-04 | 通用电气公司 | 具有凹形冷却通道的部件及其制造方法 |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2014111933A (ja) | 2014-06-19 |
| CH706983A2 (en) | 2014-03-31 |
| JP6200740B2 (ja) | 2017-09-20 |
| US8974859B2 (en) | 2015-03-10 |
| US20140220253A1 (en) | 2014-08-07 |
| CN103817032A (zh) | 2014-05-28 |
| DE102013110069A1 (de) | 2014-03-27 |
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