NO934862L - Process for producing a thermal barrier coating on a metal substrate - Google Patents

Process for producing a thermal barrier coating on a metal substrate

Info

Publication number
NO934862L
NO934862L NO934862A NO934862A NO934862L NO 934862 L NO934862 L NO 934862L NO 934862 A NO934862 A NO 934862A NO 934862 A NO934862 A NO 934862A NO 934862 L NO934862 L NO 934862L
Authority
NO
Norway
Prior art keywords
thermal barrier
barrier coating
zirconium dioxide
dioxide layer
metal substrate
Prior art date
Application number
NO934862A
Other languages
Norwegian (no)
Other versions
NO934862D0 (en
Inventor
Adrian Maurice Beltran
Robert Scott Shalvoy
Yuk-Chiu Lau
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of NO934862D0 publication Critical patent/NO934862D0/en
Publication of NO934862L publication Critical patent/NO934862L/en

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
    • C23C4/04—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
    • C23C4/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
    • 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
    • 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
    • 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
    • C23C4/134—Plasma spraying

Abstract

Ved en fremgangsmåte for fremstilling av et termisk barrierebelegg på et metallsubstrat blir a) et metallurgisk bindingsbelegg på- ført substratet, b) et første zirkoniumdioksidlag med en tett, søyleformig mikrostruktur avsatt på bindingsbelegget, og c) et annet zirkoniumdioksidlag med en mikrostruktur med en porøsitet mellom 10 og 20% avsatt på det første zir- ., koniumdioksidlag. Under trinnene b) og c) kan substratets temperatur reguleres for å oppnå det første zirkoniumdiok- sidlag med en porøsitet som i det vesentlige er lik null, og for å oppnå det annet zirkoniumdioksidlag med en porøsitet mellom 10 og 20%. En gasstur- binkomponent med en overflate forsynt med et termisk barrierebelegg fremstilt i overensstemmelse med den foreliggende fremgangsmåte er også krevet.In a process for preparing a thermal barrier coating on a metal substrate, a) a metallurgical bonding coating is applied to the substrate, b) a first zirconium dioxide layer having a dense, columnar microstructure deposited on the bonding coating, and c) a second zirconium dioxide layer having a microstructure having a microstructure between 10 and 20% deposited on the first zirconium dioxide layer. During steps b) and c), the temperature of the substrate can be adjusted to obtain the first zirconium dioxide layer having a porosity substantially equal to zero, and to obtain the second zirconia layer having a porosity of between 10 and 20%. A gas turbine component having a surface provided with a thermal barrier coating prepared in accordance with the present method is also required.

NO934862A 1992-12-29 1993-12-28 Process for producing a thermal barrier coating on a metal substrate NO934862L (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US99692092A 1992-12-29 1992-12-29

Publications (2)

Publication Number Publication Date
NO934862D0 NO934862D0 (en) 1993-12-28
NO934862L true NO934862L (en) 1994-06-30

Family

ID=25543430

Family Applications (1)

Application Number Title Priority Date Filing Date
NO934862A NO934862L (en) 1992-12-29 1993-12-28 Process for producing a thermal barrier coating on a metal substrate

Country Status (5)

Country Link
EP (1) EP0605196A1 (en)
JP (1) JPH06235074A (en)
KR (1) KR940014878A (en)
CA (1) CA2110007A1 (en)
NO (1) NO934862L (en)

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE69524353T2 (en) * 1994-10-04 2002-08-08 Gen Electric High-temperature protective layer
US5558922A (en) * 1994-12-28 1996-09-24 General Electric Company Thick thermal barrier coating having grooves for enhanced strain tolerance
US5512382A (en) * 1995-05-08 1996-04-30 Alliedsignal Inc. Porous thermal barrier coating
US6102656A (en) * 1995-09-26 2000-08-15 United Technologies Corporation Segmented abradable ceramic coating
JPH1088368A (en) * 1996-09-19 1998-04-07 Toshiba Corp Thermal insulation coating member and its production
US6057047A (en) * 1997-11-18 2000-05-02 United Technologies Corporation Ceramic coatings containing layered porosity
US5876860A (en) * 1997-12-09 1999-03-02 N.V. Interturbine Thermal barrier coating ceramic structure
US6106959A (en) * 1998-08-11 2000-08-22 Siemens Westinghouse Power Corporation Multilayer thermal barrier coating systems
US6287644B1 (en) 1999-07-02 2001-09-11 General Electric Company Continuously-graded bond coat and method of manufacture
US6716539B2 (en) * 2001-09-24 2004-04-06 Siemens Westinghouse Power Corporation Dual microstructure thermal barrier coating
EP1549782A1 (en) * 2002-09-25 2005-07-06 Volvo Aero Corporation A thermal barrier coating and a method of applying such a coating
US7258934B2 (en) 2002-09-25 2007-08-21 Volvo Aero Corporation Thermal barrier coating and a method of applying such a coating
SE527179C2 (en) * 2003-12-05 2006-01-17 Sandvik Intellectual Property Thin film solar cell or thin film battery, comprising a zirconia coated ferritic chrome strip product
JP4645030B2 (en) * 2003-12-18 2011-03-09 株式会社日立製作所 Heat resistant member with thermal barrier coating
US7354663B2 (en) 2004-04-02 2008-04-08 Mitsubishi Heavy Industries, Ltd. Thermal barrier coating, manufacturing method thereof, turbine part and gas turbine
US7597966B2 (en) 2005-06-10 2009-10-06 General Electric Company Thermal barrier coating and process therefor
US20070099013A1 (en) * 2005-10-27 2007-05-03 General Electric Company Methods and apparatus for manufacturing a component
WO2007112783A1 (en) * 2006-04-06 2007-10-11 Siemens Aktiengesellschaft Layered thermal barrier coating with a high porosity, and a component
US8372488B2 (en) * 2006-05-01 2013-02-12 General Electric Company Methods and apparatus for thermal barrier coatings with improved overall thermal insulation characteristics
US7875370B2 (en) 2006-08-18 2011-01-25 United Technologies Corporation Thermal barrier coating with a plasma spray top layer
DE102008007870A1 (en) 2008-02-06 2009-08-13 Forschungszentrum Jülich GmbH Thermal barrier coating system and process for its preparation
US20090252985A1 (en) * 2008-04-08 2009-10-08 Bangalore Nagaraj Thermal barrier coating system and coating methods for gas turbine engine shroud
EP2196559A1 (en) 2008-12-15 2010-06-16 ALSTOM Technology Ltd Thermal barrier coating system, components coated therewith and method for applying a thermal barrier coating system to components
US20110033284A1 (en) * 2009-08-04 2011-02-10 United Technologies Corporation Structurally diverse thermal barrier coatings
CN101698364B (en) * 2009-11-03 2013-08-28 西安交通大学 Thermal barrier coating and preparation technology thereof
RU2445199C2 (en) * 2010-03-25 2012-03-20 Общество с ограниченной ответственностью "Производственное предприятие Турбинаспецсервис" Method of hardening turbo machine nozzle vane unit made from nickel and cobalt alloys
US9023486B2 (en) 2011-10-13 2015-05-05 General Electric Company Thermal barrier coating systems and processes therefor
US9034479B2 (en) 2011-10-13 2015-05-19 General Electric Company Thermal barrier coating systems and processes therefor
DE102012200560B4 (en) * 2012-01-16 2014-08-21 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. A method of producing a ceramic layer on a surface formed of a Ni-based alloy and a ceramic layer article
WO2015116292A2 (en) 2013-11-11 2015-08-06 United Technologies Corporation Article with coated substrate
JP6016861B2 (en) * 2014-08-26 2016-10-26 三菱重工業株式会社 Coating method for machine parts
DE102014222686A1 (en) * 2014-11-06 2016-05-12 Siemens Aktiengesellschaft Double-layered thermal barrier coating by different coating methods
RU2702515C1 (en) * 2018-06-06 2019-10-08 Общество с ограниченной ответственностью "Научно-производственное предприятие "Уралавиаспецтехнология" Method of nickel-based alloy part reinforcing treatment (versions)
RU2697758C1 (en) * 2019-01-14 2019-08-19 федеральное государственное бюджетное образовательное учреждение высшего образования "Уфимский государственный авиационный технический университет" Method of applying heat-resistant coatings y-mo-o from vacuum-arc discharge plasma
CN113088859A (en) * 2021-03-30 2021-07-09 潍柴动力股份有限公司 Composite coating, piston, engine and vehicle

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4503130A (en) * 1981-12-14 1985-03-05 United Technologies Corporation Prestressed ceramic coatings
EP0185603B1 (en) * 1984-11-28 1989-11-08 United Technologies Corporation Improved durability metallic-ceramic turbine air seals
US4613259A (en) * 1984-11-28 1986-09-23 United Technologies Corporation Apparatus for controlling powder flow rate in a carrier gas
US4588607A (en) * 1984-11-28 1986-05-13 United Technologies Corporation Method of applying continuously graded metallic-ceramic layer on metallic substrates
US4880614A (en) * 1988-11-03 1989-11-14 Allied-Signal Inc. Ceramic thermal barrier coating with alumina interlayer
IL99473A0 (en) * 1990-09-20 1992-08-18 United Technologies Corp Columnar ceramic thermal barrier coating with improved adherence
GB9204791D0 (en) * 1992-03-05 1992-04-22 Rolls Royce Plc A coated article

Also Published As

Publication number Publication date
JPH06235074A (en) 1994-08-23
CA2110007A1 (en) 1994-06-30
NO934862D0 (en) 1993-12-28
KR940014878A (en) 1994-07-19
EP0605196A1 (en) 1994-07-06

Similar Documents

Publication Publication Date Title
NO934862L (en) Process for producing a thermal barrier coating on a metal substrate
GB9104505D0 (en) Thermal barrier coating system with intermetallic overlay bond coat
UA35620C2 (en) method for application of multilayer coating serving as heat barrier on the surface of superalloy, and multilayer coating obtained with this method (variants)
DE42872T1 (en) THERMAL PROTECTIVE COATINGS MADE FROM COLUMN-LIKE KERNEL CERAMIC MATERIAL.
IL130558A (en) Method of repairing a turbine engine airfoil part
FI862081A (en) OXIDATIONSBESTAENDIG METALLFOLIE BASERAD PAO JAERN OCH FOERFARANDE FOER DESS FRAMTAELLNING.
CA2294261A1 (en) Method and apparatus for gas phase coating complex internal surfaces of hollow articles
EP0310043A3 (en) Oxidation resistant, high temperature thermal cycling resistant coating on silicon-based substrates and process for the production thereof
CA2003873A1 (en) Heat-resistant exhaust manifold and method of preparing same
CA2033018A1 (en) Method for diffusion coating of metal objects employing ceramic carrier provided with diffusion composition
DE69124881T2 (en) Diamond-like carbon coatings
WO1989004549A3 (en) Annealing method for iii-v deposition
CA2177244A1 (en) Metal layer pattern forming method
IE842093L (en) Varying thickness thermal barrier for combustion turbine¹baskets
DE59914232D1 (en) Method for producing a metal-ceramic substrate
JPS60197861A (en) Sliding member
DE69706317D1 (en) METHOD FOR COATING COMPONENTS OF A CONTINUOUS CASTING SYSTEM
KR970043261A (en) Method of forming coating layer of mold
DE69009278D1 (en) Two-phase metal / oxide films.
Sheets et al. Thermal Stresses Under Engine Heat Flux. I. Ceramic Coatings on Metal Substrate
JPS5481131A (en) Process for reducting hydrogen permeating quantity in metal surface
CA2022359A1 (en) Process for Preparing Superconducting Thin Films
JPH01198464A (en) Surface hardening treatment for iron and steel by sputtering
CA2040070A1 (en) Method of preparing oxide superconducting film
ATE35697T1 (en) PROCESS FOR COATING OPTICAL SUBSTRATES WITH ANTI-REFLECTIVE COATINGS WHICH CAN BE ETCHED.