DE602006018830D1 - Vor Ort reparierbare hohe Temperatur glatte verschleissfeste Beschichtung - Google Patents

Vor Ort reparierbare hohe Temperatur glatte verschleissfeste Beschichtung

Info

Publication number
DE602006018830D1
DE602006018830D1 DE602006018830T DE602006018830T DE602006018830D1 DE 602006018830 D1 DE602006018830 D1 DE 602006018830D1 DE 602006018830 T DE602006018830 T DE 602006018830T DE 602006018830 T DE602006018830 T DE 602006018830T DE 602006018830 D1 DE602006018830 D1 DE 602006018830D1
Authority
DE
Germany
Prior art keywords
site
high temperature
resistant coating
smooth wear
temperature smooth
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
DE602006018830T
Other languages
English (en)
Inventor
Andrew Jay Skoog
William Randolph Stowell
Jane Ann Murphy
David E Caldwell
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=37075867&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE602006018830(D1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by General Electric Co filed Critical General Electric Co
Publication of DE602006018830D1 publication Critical patent/DE602006018830D1/de
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
    • C23C24/00Coating starting from inorganic powder
    • C23C24/08Coating starting from inorganic powder by application of heat or pressure and heat
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09DCOATING COMPOSITIONS, e.g. PAINTS, VARNISHES OR LACQUERS; FILLING PASTES; CHEMICAL PAINT OR INK REMOVERS; INKS; CORRECTING FLUIDS; WOODSTAINS; PASTES OR SOLIDS FOR COLOURING OR PRINTING; USE OF MATERIALS THEREFOR
    • C09D1/00Coating compositions, e.g. paints, varnishes or lacquers, based on inorganic substances
    • 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
    • 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
    • F05D2230/80Repairing, retrofitting or upgrading methods
    • 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
    • F05D2230/90Coating; Surface treatment
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00019Repairing or maintaining combustion chamber liners or subparts
    • 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

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Organic Chemistry (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Inorganic Chemistry (AREA)
  • Wood Science & Technology (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Metallurgy (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)
DE602006018830T 2005-06-29 2006-06-26 Vor Ort reparierbare hohe Temperatur glatte verschleissfeste Beschichtung Active DE602006018830D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/170,471 US7842335B2 (en) 2004-04-07 2005-06-29 Field repairable high temperature smooth wear coating

Publications (1)

Publication Number Publication Date
DE602006018830D1 true DE602006018830D1 (de) 2011-01-27

Family

ID=37075867

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006018830T Active DE602006018830D1 (de) 2005-06-29 2006-06-26 Vor Ort reparierbare hohe Temperatur glatte verschleissfeste Beschichtung

Country Status (5)

Country Link
US (1) US7842335B2 (de)
EP (1) EP1739204B1 (de)
JP (1) JP5095138B2 (de)
DE (1) DE602006018830D1 (de)
SG (2) SG149050A1 (de)

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WO2009137051A2 (en) * 2008-05-06 2009-11-12 Andrew Armstrong Method for extending and improving the functionality of a hard surface
US20110059321A1 (en) * 2008-06-23 2011-03-10 General Electric Company Method of repairing a thermal barrier coating and repaired coating formed thereby
KR101280828B1 (ko) * 2008-07-02 2013-07-02 엘지디스플레이 주식회사 기판결함의 수리방법
US9027230B2 (en) * 2009-03-02 2015-05-12 Xerox Corporation Thermally responsive composite member, related devices, and applications including structural applications
US8221825B2 (en) 2009-03-30 2012-07-17 Alstom Technology Ltd. Comprehensive method for local application and local repair of thermal barrier coatings
US9624583B2 (en) 2009-04-01 2017-04-18 Rolls-Royce Corporation Slurry-based coating techniques for smoothing surface imperfections
CH701373A1 (de) * 2009-06-30 2010-12-31 Alstom Technology Ltd Schlickerformulierung zur Herstellung von thermischen Schutzschichten.
EP2366488A1 (de) * 2010-03-19 2011-09-21 Siemens Aktiengesellschaft Verfahren zum Wiederaufarbeiten einer Turbinenschaufel mit wenigstens einer Plattform
US20120163981A1 (en) * 2010-12-22 2012-06-28 Hong Shek C Method and coating for protecting and repairing an airfoil surface
EP2681045A4 (de) 2011-03-02 2015-01-14 Applied Thin Films Inc Schützende innenbeschichtungen für poröse substrate
US9527262B2 (en) * 2012-09-28 2016-12-27 General Electric Company Layered arrangement, hot-gas path component, and process of producing a layered arrangement
EP2970031B1 (de) * 2013-03-15 2020-09-23 Rolls-Royce Corporation Wiederherstellung einer auf suspension basierenden beschichtung
EP2784268A1 (de) 2013-03-28 2014-10-01 MTU Aero Engines GmbH Eine Turbinenschaufelaussendichtung bestehend aus jeweils einer keramischen abrasiven Schicht auf dem Stator und dem Rotor.
FR3013996B1 (fr) 2013-12-02 2017-04-28 Office National Detudes Et De Rech Aerospatiales Onera Procede de reparation locale de barrieres thermiques
FR3014115B1 (fr) 2013-12-02 2017-04-28 Office National Detudes Et De Rech Aerospatiales Onera Procede et systeme de depot d'oxyde sur un composant poreux
JP2016200028A (ja) * 2015-04-08 2016-12-01 株式会社東芝 タービン用部材及びその製造方法
US20160312633A1 (en) * 2015-04-24 2016-10-27 General Electric Company Composite seals for turbomachinery
US20170122561A1 (en) * 2015-10-28 2017-05-04 General Electric Company Methods of repairing a thermal barrier coating of a gas turbine component and the resulting components
US20170122560A1 (en) * 2015-10-28 2017-05-04 General Electric Company Gas turbine component with improved thermal barrier coating system
DE102015223576A1 (de) * 2015-11-27 2017-06-01 Siemens Aktiengesellschaft Lokale zweilagige Wärmedämmschicht
EP3241817B1 (de) 2016-05-02 2021-01-27 Rolls-Royce High Temperature Composites Inc Bildung einer oberflächenschicht auf einem keramischen matrixverbundstoffartikel
EP3241815B1 (de) 2016-05-02 2019-11-13 Rolls-Royce High Temperature Composites Inc Reduzierung von oberflächenknötchen in schmelzinfiltrierten verbundwerkstoffen mit keramischer matrix
US10646894B2 (en) 2016-06-30 2020-05-12 General Electric Company Squeegee apparatus and methods of use thereof
US10920590B2 (en) 2016-06-30 2021-02-16 General Electric Company Turbine assembly maintenance methods
US10384978B2 (en) 2016-08-22 2019-08-20 General Electric Company Thermal barrier coating repair compositions and methods of use thereof
WO2018128676A1 (en) * 2017-01-04 2018-07-12 General Electric Company Slurry-based methods for forming a bond coat and articles formed by the methods
CN108393648A (zh) * 2017-02-08 2018-08-14 通用电气公司 防止焊料进入孔内的塞堵材料及其方法
JP6709181B2 (ja) * 2017-03-14 2020-06-10 東芝エネルギーシステムズ株式会社 遮熱コーティングの補修方法および耐熱性部品
US10745325B2 (en) 2017-12-18 2020-08-18 Rolls-Royce High Temperature Composites, Inc. Protective layer for a ceramic matrix composite article
EP3581679B1 (de) 2018-06-01 2021-02-17 Rolls-Royce North American Technologies, Inc. Reparatur von aufschlämmungsbasierten beschichtungssystemen
US11198651B2 (en) 2018-12-20 2021-12-14 Rolls-Royce High Temperature Composites, Inc. Surface layer on a ceramic matrix composite
US10919180B2 (en) 2019-02-08 2021-02-16 Raytheon Technologies Corporation Repair process using networked ceramic nanofibers
US11655192B2 (en) * 2019-07-25 2023-05-23 Rolls-Royce Corporation Barrier coatings
US20210340388A1 (en) * 2020-05-01 2021-11-04 General Electric Company Composition for thermal barrier coating
CN112707727A (zh) * 2020-12-30 2021-04-27 广东华科新材料研究院有限公司 多用途的热障涂料及其制备方法
US20240084703A1 (en) * 2022-09-08 2024-03-14 General Electric Company Material systems for repair of thermal barrier coating and methods thereof
CN115612358B (zh) * 2022-09-27 2023-09-26 北京天力创玻璃科技开发有限公司 用于等温锻造模具保护的涂料及应用
CN117644478B (zh) * 2024-01-30 2024-05-17 西安格美金属材料有限公司 飞机多级增压喷气发动机的性能提升方法

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Also Published As

Publication number Publication date
SG128645A1 (en) 2007-01-30
JP2007007647A (ja) 2007-01-18
EP1739204A2 (de) 2007-01-03
US7842335B2 (en) 2010-11-30
US20070134408A1 (en) 2007-06-14
EP1739204A3 (de) 2007-01-24
EP1739204B1 (de) 2010-12-15
SG149050A1 (en) 2009-01-29
JP5095138B2 (ja) 2012-12-12

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