KR20080067980A - 가스 터빈 엔진 코팅 방법 및 장치 - Google Patents

가스 터빈 엔진 코팅 방법 및 장치 Download PDF

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Publication number
KR20080067980A
KR20080067980A KR1020080004824A KR20080004824A KR20080067980A KR 20080067980 A KR20080067980 A KR 20080067980A KR 1020080004824 A KR1020080004824 A KR 1020080004824A KR 20080004824 A KR20080004824 A KR 20080004824A KR 20080067980 A KR20080067980 A KR 20080067980A
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KR
South Korea
Prior art keywords
coating
heat shield
gas turbine
distance
dvc
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.)
Ceased
Application number
KR1020080004824A
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English (en)
Korean (ko)
Inventor
레이몬드 그랜트 로우
타라 이스터 맥고번
제인 앤 머피
앤드류 제이 스쿠그
윌리엄 알 스토웰
폴 토마스 마크스
리사 데벨리스
제임스 에이치 클레어
Original Assignee
제너럴 일렉트릭 캄파니
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 제너럴 일렉트릭 캄파니 filed Critical 제너럴 일렉트릭 캄파니
Publication of KR20080067980A publication Critical patent/KR20080067980A/ko
Ceased legal-status Critical Current

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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
    • C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
    • A—HUMAN NECESSITIES
    • A47—FURNITURE; DOMESTIC ARTICLES OR APPLIANCES; COFFEE MILLS; SPICE MILLS; SUCTION CLEANERS IN GENERAL
    • A47K—SANITARY EQUIPMENT NOT OTHERWISE PROVIDED FOR; TOILET ACCESSORIES
    • A47K7/00—Body washing or cleaning implements
    • A47K7/02—Bathing sponges, brushes, gloves, or similar cleaning or rubbing implements
    • A47K7/026—Bathing sponges, brushes, gloves, or similar cleaning or rubbing implements for cleaning the feet or toes
    • A—HUMAN NECESSITIES
    • A45—HAND OR TRAVELLING ARTICLES
    • A45D—HAIRDRESSING OR SHAVING EQUIPMENT; EQUIPMENT FOR COSMETICS OR COSMETIC TREATMENTS, e.g. FOR MANICURING OR PEDICURING
    • A45D29/00—Manicuring or pedicuring implements
    • A45D29/16—Cuticle sticks
    • 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
    • A—HUMAN NECESSITIES
    • A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61B—DIAGNOSIS; SURGERY; IDENTIFICATION
    • A61B17/00—Surgical instruments, devices or methods
    • A61B17/32—Surgical cutting instruments
    • A61B2017/320004—Surgical cutting instruments abrasive
    • 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
    • F05D2230/90—Coating; Surface treatment
    • 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)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Public Health (AREA)
  • Health & Medical Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Epidemiology (AREA)
  • General Health & Medical Sciences (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Coating By Spraying Or Casting (AREA)
KR1020080004824A 2007-01-17 2008-01-16 가스 터빈 엔진 코팅 방법 및 장치 Ceased KR20080067980A (ko)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/654,182 2007-01-17
US11/654,182 US8007246B2 (en) 2007-01-17 2007-01-17 Methods and apparatus for coating gas turbine engines

Publications (1)

Publication Number Publication Date
KR20080067980A true KR20080067980A (ko) 2008-07-22

Family

ID=39683712

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1020080004824A Ceased KR20080067980A (ko) 2007-01-17 2008-01-16 가스 터빈 엔진 코팅 방법 및 장치

Country Status (5)

Country Link
US (1) US8007246B2 (enExample)
EP (1) EP1978210A1 (enExample)
JP (1) JP2008174838A (enExample)
KR (1) KR20080067980A (enExample)
CN (1) CN101225753A (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20240156110A (ko) 2023-04-21 2024-10-29 터보파워텍(주) 진공주조와 3d프린팅에 의한 가스터빈 블레이드 제조방법

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US8273231B2 (en) 2007-12-21 2012-09-25 Rolls-Royce Corporation Methods of depositing coatings with γ-Ni + γ′-Ni3A1 phase constitution
US8501273B2 (en) 2008-10-02 2013-08-06 Rolls-Royce Corporation Mixture and technique for coating an internal surface of an article
US9624583B2 (en) * 2009-04-01 2017-04-18 Rolls-Royce Corporation Slurry-based coating techniques for smoothing surface imperfections
US8511993B2 (en) * 2009-08-14 2013-08-20 Alstom Technology Ltd. Application of dense vertically cracked and porous thermal barrier coating to a gas turbine component
US20110086177A1 (en) * 2009-10-14 2011-04-14 WALBAR INC. Peabody Industrial Center Thermal spray method for producing vertically segmented thermal barrier coatings
US8967957B2 (en) * 2011-11-03 2015-03-03 General Electric Company Rotating airfoil component of a turbomachine
WO2014031963A1 (en) * 2012-08-24 2014-02-27 Barson Composites Corporation Coatings for fluid energy device components
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
WO2014144437A1 (en) 2013-03-15 2014-09-18 Rolls-Royce Corporation Slurry-based coating restoration
WO2015006332A1 (en) 2013-07-10 2015-01-15 United Technologies Corporation Vibratory mass media fixture with tip protector
WO2015006329A1 (en) 2013-07-10 2015-01-15 United Technologies Corporation Abrasive flow media fixture with end contour
US9289917B2 (en) 2013-10-01 2016-03-22 General Electric Company Method for 3-D printing a pattern for the surface of a turbine shroud
US9151175B2 (en) 2014-02-25 2015-10-06 Siemens Aktiengesellschaft Turbine abradable layer with progressive wear zone multi level ridge arrays
CN106030039A (zh) 2014-02-25 2016-10-12 西门子公司 具有深度变化材料性质的涡轮机部件热障涂层
US9243511B2 (en) 2014-02-25 2016-01-26 Siemens Aktiengesellschaft Turbine abradable layer with zig zag groove pattern
US8939706B1 (en) 2014-02-25 2015-01-27 Siemens Energy, Inc. Turbine abradable layer with progressive wear zone having a frangible or pixelated nib surface
US10190435B2 (en) 2015-02-18 2019-01-29 Siemens Aktiengesellschaft Turbine shroud with abradable layer having ridges with holes
EP3259452A2 (en) 2015-02-18 2017-12-27 Siemens Aktiengesellschaft Forming cooling passages in combustion turbine superalloy castings
EP3168323B1 (en) 2015-11-13 2020-01-22 General Electric Technology GmbH Power plant component
US10174412B2 (en) 2016-12-02 2019-01-08 General Electric Company Methods for forming vertically cracked thermal barrier coatings and articles including vertically cracked thermal barrier coatings
CN110080826B (zh) * 2019-05-31 2023-09-15 南京赛达机械制造有限公司 一种汽轮机叶片及其制备方法

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Publication number Priority date Publication date Assignee Title
US5419971A (en) * 1993-03-03 1995-05-30 General Electric Company Enhanced thermal barrier coating system
EP0688047A1 (en) * 1994-06-13 1995-12-20 Mitsubishi Materials Corporation Aluminium nitride substrate and method of producing the same
DE69524353T2 (de) * 1994-10-04 2002-08-08 General Electric Co., Schenectady Hochtemperatur-Schutzschicht
US6210791B1 (en) * 1995-11-30 2001-04-03 General Electric Company Article with a diffuse reflective barrier coating and a low-emissity coating thereon, and its preparation
US6465090B1 (en) * 1995-11-30 2002-10-15 General Electric Company Protective coating for thermal barrier coatings and coating method therefor
US5683825A (en) * 1996-01-02 1997-11-04 General Electric Company Thermal barrier coating resistant to erosion and impact by particulate matter
US6306517B1 (en) * 1996-07-29 2001-10-23 General Electric Company Thermal barrier coatings having an improved columnar microstructure
US6057030A (en) * 1997-07-21 2000-05-02 Kanebo Ltd. Porous ceramic body and kiln furniture made from a porous ceramic body
US6047539A (en) * 1998-04-30 2000-04-11 General Electric Company Method of protecting gas turbine combustor components against water erosion and hot corrosion
US6165600A (en) * 1998-10-06 2000-12-26 General Electric Company Gas turbine engine component having a thermal-insulating multilayer ceramic coating
US6007919A (en) * 1998-12-22 1999-12-28 General Electric Company High temperature high band heat reflecting coating material and coated article
US6177186B1 (en) * 1999-04-30 2001-01-23 General Electric Company Heat reflective, erosion and wear resistant coating mixture, method and coated article
US6294261B1 (en) * 1999-10-01 2001-09-25 General Electric Company Method for smoothing the surface of a protective coating
US6432487B1 (en) * 2000-12-28 2002-08-13 General Electric Company Dense vertically cracked thermal barrier coating process to facilitate post-coat surface finishing
EP1484427A3 (en) * 2003-06-06 2005-10-26 General Electric Company Top coating system for industrial turbine nozzle airfoils and other hot gas path components and related method
US7368164B2 (en) * 2004-06-18 2008-05-06 General Electric Company Smooth outer coating for combustor components and coating method therefor
US8511993B2 (en) * 2009-08-14 2013-08-20 Alstom Technology Ltd. Application of dense vertically cracked and porous thermal barrier coating to a gas turbine component

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20240156110A (ko) 2023-04-21 2024-10-29 터보파워텍(주) 진공주조와 3d프린팅에 의한 가스터빈 블레이드 제조방법

Also Published As

Publication number Publication date
JP2008174838A (ja) 2008-07-31
CN101225753A (zh) 2008-07-23
US20110044821A1 (en) 2011-02-24
US8007246B2 (en) 2011-08-30
EP1978210A1 (en) 2008-10-08

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