ES2131451B1 - QUASICRISTALLINE THERMAL BARRIER TYPE COATINGS FOR THE PROTECTION OF COMPONENTS OF THE HOT AREAS OF TURBINES. - Google Patents

QUASICRISTALLINE THERMAL BARRIER TYPE COATINGS FOR THE PROTECTION OF COMPONENTS OF THE HOT AREAS OF TURBINES.

Info

Publication number
ES2131451B1
ES2131451B1 ES009602084A ES9602084A ES2131451B1 ES 2131451 B1 ES2131451 B1 ES 2131451B1 ES 009602084 A ES009602084 A ES 009602084A ES 9602084 A ES9602084 A ES 9602084A ES 2131451 B1 ES2131451 B1 ES 2131451B1
Authority
ES
Spain
Prior art keywords
thermal barrier
protection
components
coatings
quasicristalline
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 - Fee Related
Application number
ES009602084A
Other languages
Spanish (es)
Other versions
ES2131451A1 (en
Inventor
Pascual Agustin Sanchez
Albarsanz Marcelino Torre
Jean Marie Dubois
Gonzalo Juan Manuel Algaba
Pierre Archambault
Deblas Villanueva Franc Garcia
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.)
Instituto Nacional de Tecnica Aeroespacial Esteban Terradas
Original Assignee
Instituto Nacional de Tecnica Aeroespacial Esteban Terradas
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 Instituto Nacional de Tecnica Aeroespacial Esteban Terradas filed Critical Instituto Nacional de Tecnica Aeroespacial Esteban Terradas
Priority to ES009602084A priority Critical patent/ES2131451B1/en
Publication of ES2131451A1 publication Critical patent/ES2131451A1/en
Application granted granted Critical
Publication of ES2131451B1 publication Critical patent/ES2131451B1/en
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • C23C28/324—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 matrix material layer comprising a mixture of at least two metals or metal phases or a metal-matrix material with hard embedded particles, e.g. WC-Me
    • 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
    • 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
    • C23C28/34—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)
  • Inorganic Chemistry (AREA)
  • Metallurgy (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Organic Chemistry (AREA)
  • Ceramic Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Physical Vapour Deposition (AREA)
  • Coating By Spraying Or Casting (AREA)

Abstract

Recubrimientos cuasi cristalinos, tipo barrera térmica para la protección de componentes de las zonas calientes de turbinas que pueden comprender una barrera de difusión entre el substrato y la barrera térmica propiamente dicha. Estos recubrimientos tienen aplicación en el campo de motores de turbinas de gas bien en de aviación o para uso industrial, así como cualquier otra en donde se requiera aumentar el efecto producido por el enfriamiento en un componente para mantenerlo a menor temperatura que el medio ambiente y al mismo tiempo proteger contra la oxidación a alta temperaturas la corrosión en caliente y la erosión a temperaturas superiores a 700º C. Procedimientos de deposición de dichos recubrimientos.Quasi-crystalline, thermal barrier type coatings for the protection of components in hot turbine areas that may comprise a diffusion barrier between the substrate and the thermal barrier itself. These coatings have application in the field of gas turbine engines, either in aviation or for industrial use, as well as any other where it is required to increase the effect produced by the cooling of a component to keep it at a lower temperature than the environment and at the same time protect against corrosion at high temperatures, hot corrosion and erosion at temperatures above 700º C. Procedures for the deposition of said coatings.

ES009602084A 1996-10-04 1996-10-04 QUASICRISTALLINE THERMAL BARRIER TYPE COATINGS FOR THE PROTECTION OF COMPONENTS OF THE HOT AREAS OF TURBINES. Expired - Fee Related ES2131451B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES009602084A ES2131451B1 (en) 1996-10-04 1996-10-04 QUASICRISTALLINE THERMAL BARRIER TYPE COATINGS FOR THE PROTECTION OF COMPONENTS OF THE HOT AREAS OF TURBINES.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES009602084A ES2131451B1 (en) 1996-10-04 1996-10-04 QUASICRISTALLINE THERMAL BARRIER TYPE COATINGS FOR THE PROTECTION OF COMPONENTS OF THE HOT AREAS OF TURBINES.

Publications (2)

Publication Number Publication Date
ES2131451A1 ES2131451A1 (en) 1999-07-16
ES2131451B1 true ES2131451B1 (en) 2000-02-16

Family

ID=8296220

Family Applications (1)

Application Number Title Priority Date Filing Date
ES009602084A Expired - Fee Related ES2131451B1 (en) 1996-10-04 1996-10-04 QUASICRISTALLINE THERMAL BARRIER TYPE COATINGS FOR THE PROTECTION OF COMPONENTS OF THE HOT AREAS OF TURBINES.

Country Status (1)

Country Link
ES (1) ES2131451B1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1334737A3 (en) * 2000-05-29 2004-05-12 Reto Dr. Lerf Anti-adhesive coating and uses thereof
ES2391321B1 (en) * 2011-04-29 2013-10-21 Universitat Jaume I De Castellón METHOD FOR COATING MATERIALS THROUGH THERMAL COMPOSITION PROJECTION.

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4421799A (en) * 1982-02-16 1983-12-20 Metco, Inc. Aluminum clad refractory oxide flame spraying powder
FR2671808B1 (en) * 1991-01-18 1994-06-17 Centre Nat Rech Scient ALUMINUM ALLOYS WITH SPECIFIC PROPERTIES.
FR2673871B1 (en) * 1991-03-13 1995-03-10 Centre Nat Rech Scient CORD FOR COVERING BY SPRAYING WITH A TORCH AND ITS USE FOR DEPOSITING A QUASI CRYSTALLINE PHASE ON A SUBSTRATE.
FR2685349B1 (en) * 1991-12-20 1994-03-25 Centre Nal Recherc Scientifique THERMAL PROTECTION ELEMENT CONSISTING OF A QUASI-CRYSTALLINE ALUMINUM ALLOY.
FR2699554B1 (en) * 1992-12-23 1995-02-24 Metallisation Ind Ste Nle Thermal barriers, material and process for their development.

Also Published As

Publication number Publication date
ES2131451A1 (en) 1999-07-16

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