JP6200740B2 - マイクロ・チャネル・コーティング堆積システムおよびその使用方法 - Google Patents

マイクロ・チャネル・コーティング堆積システムおよびその使用方法 Download PDF

Info

Publication number
JP6200740B2
JP6200740B2 JP2013196385A JP2013196385A JP6200740B2 JP 6200740 B2 JP6200740 B2 JP 6200740B2 JP 2013196385 A JP2013196385 A JP 2013196385A JP 2013196385 A JP2013196385 A JP 2013196385A JP 6200740 B2 JP6200740 B2 JP 6200740B2
Authority
JP
Japan
Prior art keywords
pressure
grooves
coating
fluid
coating material
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.)
Active
Application number
JP2013196385A
Other languages
English (en)
Japanese (ja)
Other versions
JP2014111933A (ja
JP2014111933A5 (enExample
Inventor
ロナルド・スコット・バンカー
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of JP2014111933A publication Critical patent/JP2014111933A/ja
Publication of JP2014111933A5 publication Critical patent/JP2014111933A5/ja
Application granted granted Critical
Publication of JP6200740B2 publication Critical patent/JP6200740B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/01Selective coating, e.g. pattern coating, without pre-treatment of the material to be coated
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05DPROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05D3/00Pretreatment 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05DPROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05D7/00Processes, other than flocking, specially adapted for applying liquids or other fluent materials to particular surfaces or for applying particular liquids or other fluent materials
    • B05D7/22Processes, 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
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/06Metallic material
    • C23C4/073Metallic material containing MCrAl or MCrAlY alloys, where M is nickel, cobalt or iron, with or without non-metal elements
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/10Oxides, borides, carbides, nitrides or silicides; Mixtures thereof
    • C23C4/11Oxides
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/12Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
    • C23C4/129Flame spraying
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187Convection cooling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288Protective coatings for blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05DPROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05D3/00Pretreatment 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
    • B05D3/04Pretreatment 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
    • B05D3/0406Pretreatment 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
    • B05D3/042Directing or stopping the fluid to be coated with air
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/30Manufacture with deposition of material
    • F05D2230/31Layer deposition
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/20Heat transfer, e.g. cooling
    • F05D2260/204Heat transfer, e.g. cooling by the use of microcircuits
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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)
  • Chemical Kinetics & Catalysis (AREA)
  • Plasma & Fusion (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)
JP2013196385A 2012-09-26 2013-09-24 マイクロ・チャネル・コーティング堆積システムおよびその使用方法 Active JP6200740B2 (ja)

Applications Claiming Priority (2)

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
US13/627,158 2012-09-26

Publications (3)

Publication Number Publication Date
JP2014111933A JP2014111933A (ja) 2014-06-19
JP2014111933A5 JP2014111933A5 (enExample) 2016-11-10
JP6200740B2 true JP6200740B2 (ja) 2017-09-20

Family

ID=50235477

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013196385A Active JP6200740B2 (ja) 2012-09-26 2013-09-24 マイクロ・チャネル・コーティング堆積システムおよびその使用方法

Country Status (5)

Country Link
US (1) US8974859B2 (enExample)
JP (1) JP6200740B2 (enExample)
CN (1) CN103817032B (enExample)
CH (1) CH706983A2 (enExample)
DE (1) DE102013110069A1 (enExample)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
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
US10508551B2 (en) 2016-08-16 2019-12-17 General Electric Company Engine component with porous trench
US10767489B2 (en) 2016-08-16 2020-09-08 General Electric Company Component for a turbine engine with a hole
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

Family Cites Families (57)

* Cited by examiner, † Cited by third party
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
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
FR2680120B1 (fr) * 1991-08-08 1995-03-24 Snecma Procede et dispositif de revetement de surfaces munies de perforations par projection, notamment pour la metallisation par du plasma.
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
US5626462A (en) 1995-01-03 1997-05-06 General Electric Company Double-wall airfoil
US5640767A (en) 1995-01-03 1997-06-24 Gen Electric Method for making a 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
JP2001521989A (ja) * 1997-11-03 2001-11-13 シーメンス アクチエンゲゼルシヤフト 被膜形成方法及びこの方法を実施するための装置
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
US6190129B1 (en) 1998-12-21 2001-02-20 General Electric Company Tapered tip-rib turbine blade
US6059530A (en) 1998-12-21 2000-05-09 General Electric Company Twin rib turbine blade
US6086328A (en) 1998-12-21 2000-07-11 General Electric Company Tapered tip turbine blade
US6231307B1 (en) 1999-06-01 2001-05-15 General Electric Company Impingement cooled airfoil tip
EP1065026B1 (de) 1999-06-03 2004-04-28 ALSTOM Technology Ltd 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
US6461108B1 (en) 2001-03-27 2002-10-08 General Electric Company Cooled thermal barrier coating on a turbine blade tip
US6461107B1 (en) 2001-03-27 2002-10-08 General Electric Company Turbine blade tip having thermal barrier coating-formed micro cooling channels
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
EP1275747B1 (de) * 2001-07-11 2011-02-23 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
EP1295970A1 (en) 2001-09-22 2003-03-26 ALSTOM (Switzerland) Ltd MCrAlY type alloy coating
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
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
US7775768B2 (en) 2007-03-06 2010-08-17 United Technologies Corporation Turbine component with axially spaced radially flowing microcircuit cooling channels
US7766617B1 (en) 2007-03-06 2010-08-03 Florida Turbine Technologies, Inc. Transpiration cooled turbine airfoil
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
US8651805B2 (en) * 2010-04-22 2014-02-18 General Electric Company Hot gas path component cooling system
JP2012072705A (ja) * 2010-09-29 2012-04-12 Hitachi Ltd ガスタービン翼の製造方法
EP2439305A1 (de) 2010-10-07 2012-04-11 Sulzer Metco AG Thermisches Spritzverfahren mit Freihalten von Kühlluftbohrungen
US8387245B2 (en) * 2010-11-10 2013-03-05 General Electric Company Components with re-entrant shaped cooling channels and methods of manufacture
US8727727B2 (en) * 2010-12-10 2014-05-20 General Electric Company Components with cooling channels and methods of manufacture

Also Published As

Publication number Publication date
JP2014111933A (ja) 2014-06-19
CN103817032B (zh) 2017-12-05
US20140220253A1 (en) 2014-08-07
CN103817032A (zh) 2014-05-28
DE102013110069A1 (de) 2014-03-27
US8974859B2 (en) 2015-03-10
CH706983A2 (en) 2014-03-31

Similar Documents

Publication Publication Date Title
JP6200740B2 (ja) マイクロ・チャネル・コーティング堆積システムおよびその使用方法
JP5355869B2 (ja) 同時溶射および冷却孔洗浄の方法
US9394796B2 (en) Turbine component and methods of assembling the same
US8985049B2 (en) Pressure maskers and pressure masking systems
CN106246353B (zh) 用于热气体路径部件的冷却系统及对应的燃气涡轮发动机
EP3106617B1 (en) Hot gas path component having cast-in features for near wall cooling
US20130045106A1 (en) Angled trench diffuser
JP2004176718A (ja) 燃焼器ライナを清浄化する方法及び装置
US10837314B2 (en) Hot section dual wall component anti-blockage system
CN110725718A (zh) 具有冷却孔的涡轮发动机的部件
US10767489B2 (en) Component for a turbine engine with a hole
JP6798796B2 (ja) 表面冷却チャンネルを有するタービン構成要素及びその形成方法
US20200141247A1 (en) Component for a turbine engine with a film hole
CN105452530A (zh) 高孔隙度可磨耗涂层
JP6220346B2 (ja) 圧力マスキングシステムおよびその使用方法
US8887662B2 (en) Pressure masking systems and methods for using the same
US20130180952A1 (en) Pressure masking systems and methods for using the same
US20190195080A1 (en) Ceramic coating system and method
EP2778249A1 (en) Coating methods and pressurized masking systems for controlling coating microstructures

Legal Events

Date Code Title Description
A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20160916

A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20160916

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20170724

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20170801

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20170828

R150 Certificate of patent or registration of utility model

Ref document number: 6200740

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

S111 Request for change of ownership or part of ownership

Free format text: JAPANESE INTERMEDIATE CODE: R313113

R350 Written notification of registration of transfer

Free format text: JAPANESE INTERMEDIATE CODE: R350

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250