ES2135900T3 - Componente metalico provisto de un sistema de revestimiento para protegerlo de las altas temperaturas y procedimiento para revestir dicho componente. - Google Patents

Componente metalico provisto de un sistema de revestimiento para protegerlo de las altas temperaturas y procedimiento para revestir dicho componente.

Info

Publication number
ES2135900T3
ES2135900T3 ES96914918T ES96914918T ES2135900T3 ES 2135900 T3 ES2135900 T3 ES 2135900T3 ES 96914918 T ES96914918 T ES 96914918T ES 96914918 T ES96914918 T ES 96914918T ES 2135900 T3 ES2135900 T3 ES 2135900T3
Authority
ES
Spain
Prior art keywords
layer
coating
coating system
alloy
aluminum
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 - Lifetime
Application number
ES96914918T
Other languages
English (en)
Inventor
Wolfram Beele
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.)
Siemens AG
Siemens Corp
Original Assignee
Siemens AG
Siemens Corp
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 Siemens AG, Siemens Corp filed Critical Siemens AG
Application granted granted Critical
Publication of ES2135900T3 publication Critical patent/ES2135900T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • 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
    • C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/32—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
    • C23C28/321—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer
    • 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
    • C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/32—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
    • C23C28/321—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer
    • C23C28/3215—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer at least one MCrAlX layer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B18/00—Layered products essentially comprising ceramics, e.g. refractory products
    • 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
    • C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
    • C23C10/06—Solid state diffusion of only metal elements or silicon into metallic material surfaces using gases
    • C23C10/08—Solid state diffusion of only metal elements or silicon into metallic material surfaces using gases only one element being diffused
    • 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
    • C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
    • C23C28/345—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer
    • C23C28/3455—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer with a refractory ceramic layer, e.g. refractory metal oxide, ZrO2, rare earth oxides or a thermal barrier system comprising at least one refractory oxide layer

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Metallurgy (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Inorganic Chemistry (AREA)
  • Organic Chemistry (AREA)
  • Ceramic Engineering (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Laminated Bodies (AREA)

Abstract

UN SUSTRATO METALICO TIENE UN SISTEMA DE REVESTIMIENTO DE PROTECCION APLICADO SOBRE UNA SUPERFICIE EXTERIOR DEL MISMO. EL SISTEMA DE REVESTIMIENTO INCLUYE UNA CAPA DE ALEACION COLOCADA SOBRE LA SUPERFICIE EXTERIOR. LA CAPA DE ALEACION TIENE UNA SUPERFICIE PULIDA CUYA ORIENTACION ES CONTRARIA A LA SUPERFICIE EXTERIOR. SOBRE LA CAPA DE ALEACION SE COLOCA UNA CAPA DE ALUMINIURO DE ESPESOR SUSTANCIALMENTE UNIFORME. UNA CAPA CERAMICA COLOCADA SOBRE LA CAPA DE ALUMINIURO FORMA UNA BARRERA TERMICA. EL PROCESO DE REVESTIMIENTO INCLUYE PASOS TALES COMO: COLOCAR LA CAPA DE ALEACION SOBRE LA SUPERFICIE EXTERIOR DEL CUERPO; PULIR LA CAPA DE ALEACION; COLOCAR LA CAPA DE ALUMINIURO DE ESPESOR SUSTANCIALMENTE UNIFORME SOBRE LA CAPA DE ALEACION; Y COLOCAR LA CAPA CERAMICA SOBRE LA CAPA DE ALUMINIURO.
ES96914918T 1995-04-27 1996-04-15 Componente metalico provisto de un sistema de revestimiento para protegerlo de las altas temperaturas y procedimiento para revestir dicho componente. Expired - Lifetime ES2135900T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US43243295A 1995-04-27 1995-04-27

Publications (1)

Publication Number Publication Date
ES2135900T3 true ES2135900T3 (es) 1999-11-01

Family

ID=23716134

Family Applications (1)

Application Number Title Priority Date Filing Date
ES96914918T Expired - Lifetime ES2135900T3 (es) 1995-04-27 1996-04-15 Componente metalico provisto de un sistema de revestimiento para protegerlo de las altas temperaturas y procedimiento para revestir dicho componente.

Country Status (9)

Country Link
EP (1) EP0826076B1 (es)
JP (1) JP3414751B2 (es)
KR (1) KR19990008081A (es)
CZ (1) CZ340997A3 (es)
DE (1) DE69603183T2 (es)
DK (1) DK0826076T3 (es)
ES (1) ES2135900T3 (es)
UA (1) UA46761C2 (es)
WO (1) WO1996034130A1 (es)

Families Citing this family (18)

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US6129991A (en) * 1994-10-28 2000-10-10 Howmet Research Corporation Aluminide/MCrAlY coating system for superalloys
EP0846788A1 (en) 1996-12-06 1998-06-10 Siemens Aktiengesellschaft An article having a superalloy substrate and an enrichment layer placed thereon, and methods of its manufacturing
US6194026B1 (en) * 1998-10-19 2001-02-27 Howmet Research Corporation Superalloy component with abrasive grit-free coating
EP1074638A1 (en) * 1999-08-03 2001-02-07 Siemens Aktiengesellschaft Process for coating an article
US6372299B1 (en) * 1999-09-28 2002-04-16 General Electric Company Method for improving the oxidation-resistance of metal substrates coated with thermal barrier coatings
EP1094131B1 (en) 1999-10-23 2004-05-06 ROLLS-ROYCE plc A corrosion protective coating for a metallic article and a method of applying a corrosion protective coating to a metallic article
US6472018B1 (en) 2000-02-23 2002-10-29 Howmet Research Corporation Thermal barrier coating method
US6497758B1 (en) * 2000-07-12 2002-12-24 General Electric Company Method for applying a high-temperature bond coat on a metal substrate, and related compositions and articles
US6673467B2 (en) 2001-10-01 2004-01-06 Alstom (Switzerland) Ltd Metallic component with protective coating
US7547478B2 (en) 2002-12-13 2009-06-16 General Electric Company Article including a substrate with a metallic coating and a protective coating thereon, and its preparation and use in component restoration
EP1740303A2 (en) * 2004-03-23 2007-01-10 Velocys, Inc. Protected alloy surfaces in microchannel apparatus and catalysts, alumina supported catalysts, catalyst intermediates, and methods of forming catalysts and microchannel apparatus
US7874432B2 (en) 2004-03-23 2011-01-25 Velocys Protected alloy surfaces in microchannel apparatus and catalysts, alumina supported catalysts, catalyst intermediates, and methods of forming catalysts and microchannel apparatus
DE102004045049A1 (de) 2004-09-15 2006-03-16 Man Turbo Ag Verfahren zum Aufbringen einer Schutzschicht
RU2566697C2 (ru) 2011-04-13 2015-10-27 Роллс-Ройс Корпорейшн Граничный барьерный для диффузии слой, включающий в себя иридий, на металлической подложке
DE102011103731A1 (de) * 2011-05-31 2012-12-06 Man Diesel & Turbo Se Verfahren zum Aufbringen einer Schutzschicht, mit einer Schutzschicht beschichtetes Bauteil und Gasturbine mit einem solchen Bauteil
CN103465549A (zh) * 2013-07-26 2013-12-25 天津大学 一种含有抗热腐蚀过渡底层的热障涂层及制备方法
EP2918705B1 (en) 2014-03-12 2017-05-03 Rolls-Royce Corporation Coating including diffusion barrier layer including iridium and oxide layer and method of coating
CN106636575A (zh) * 2016-12-06 2017-05-10 王秋林 耐腐蚀增强型炉底辊

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3869779A (en) * 1972-10-16 1975-03-11 Nasa Duplex aluminized coatings
US4321310A (en) * 1980-01-07 1982-03-23 United Technologies Corporation Columnar grain ceramic thermal barrier coatings on polished substrates
US4814232A (en) * 1987-03-25 1989-03-21 United Technologies Corporation Method for depositing laser mirror coatings
US4916022A (en) * 1988-11-03 1990-04-10 Allied-Signal Inc. Titania doped ceramic thermal barrier coatings
US5268238A (en) 1989-08-10 1993-12-07 Siemens Aktiengesellschaft Highly corrosion and/or oxidation-resistant protective coating containing rhenium applied to gas turbine component surface and method thereof
DE3926479A1 (de) 1989-08-10 1991-02-14 Siemens Ag Rheniumhaltige schutzbeschichtung, mit grosser korrosions- und/oder oxidationsbestaendigkeit
US5273712A (en) 1989-08-10 1993-12-28 Siemens Aktiengesellschaft Highly corrosion and/or oxidation-resistant protective coating containing rhenium
DE4003038C1 (es) * 1990-02-02 1990-08-09 Mtu Muenchen Gmbh
US5498484A (en) * 1990-05-07 1996-03-12 General Electric Company Thermal barrier coating system with hardenable bond coat
US5401307A (en) 1990-08-10 1995-03-28 Siemens Aktiengesellschaft High temperature-resistant corrosion protection coating on a component, in particular a gas turbine component
IL99473A0 (en) * 1990-09-20 1992-08-18 United Technologies Corp Columnar ceramic thermal barrier coating with improved adherence
KR930002869B1 (ko) * 1990-12-31 1993-04-12 포항종합제철 주식회사 소둔가열로용 방열튜브 및 그 제조방법
US5236745A (en) * 1991-09-13 1993-08-17 General Electric Company Method for increasing the cyclic spallation life of a thermal barrier coating
GB9204791D0 (en) * 1992-03-05 1992-04-22 Rolls Royce Plc A coated article
US5350599A (en) * 1992-10-27 1994-09-27 General Electric Company Erosion-resistant thermal barrier coating
GB9426257D0 (en) * 1994-12-24 1995-03-01 Rolls Royce Plc Thermal barrier coating for a superalloy article and method of application

Also Published As

Publication number Publication date
DE69603183T2 (de) 2000-03-23
CZ340997A3 (cs) 1998-06-17
DK0826076T3 (da) 2000-02-07
DE69603183D1 (de) 1999-08-12
UA46761C2 (uk) 2002-06-17
JPH11504076A (ja) 1999-04-06
EP0826076A1 (en) 1998-03-04
WO1996034130A1 (en) 1996-10-31
JP3414751B2 (ja) 2003-06-09
KR19990008081A (ko) 1999-01-25
EP0826076B1 (en) 1999-07-07

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