CA2228768A1 - Procede de realisation d'un revetement protecteur a haute efficacite contre la corrosion a haute temperature pour superalliages, revetement protecteur obtenu par ce procede et pieces protegees par ce revetement - Google Patents

Procede de realisation d'un revetement protecteur a haute efficacite contre la corrosion a haute temperature pour superalliages, revetement protecteur obtenu par ce procede et pieces protegees par ce revetement

Info

Publication number
CA2228768A1
CA2228768A1 CA002228768A CA2228768A CA2228768A1 CA 2228768 A1 CA2228768 A1 CA 2228768A1 CA 002228768 A CA002228768 A CA 002228768A CA 2228768 A CA2228768 A CA 2228768A CA 2228768 A1 CA2228768 A1 CA 2228768A1
Authority
CA
Canada
Prior art keywords
coating
procedure
superalloys
producing
protect
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.)
Granted
Application number
CA002228768A
Other languages
English (en)
Other versions
CA2228768C (fr
Inventor
Serge Alexandre Alperine
Jean-Paul Fournes
Jacques Louis Leger
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snec Ma"
Serge Alexandre Alperine
Jean-Paul Fournes
Jacques Louis Leger
Lexvall
Snecma Moteurs
Snecma
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 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snec Ma", Serge Alexandre Alperine, Jean-Paul Fournes, Jacques Louis Leger, Lexvall, Snecma Moteurs, Snecma filed Critical Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snec Ma"
Publication of CA2228768A1 publication Critical patent/CA2228768A1/fr
Application granted granted Critical
Publication of CA2228768C publication Critical patent/CA2228768C/fr
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
    • C23C26/00—Coating not provided for in groups C23C2/00 - C23C24/00
    • 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
    • C23C10/28—Solid state diffusion of only metal elements or silicon into metallic material surfaces using solids, e.g. powders, pastes
    • C23C10/34—Embedding in a powder mixture, i.e. pack cementation
    • C23C10/58—Embedding in a powder mixture, i.e. pack cementation more than one element being diffused in more than one step
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771—Transition metal-base component
    • Y10T428/12861—Group VIII or IB metal-base component
    • Y10T428/12875—Platinum group metal-base component
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771—Transition metal-base component
    • Y10T428/12861—Group VIII or IB metal-base component
    • Y10T428/12931—Co-, Fe-, or Ni-base components, alternative to each other
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771—Transition metal-base component
    • Y10T428/12861—Group VIII or IB metal-base component
    • Y10T428/12944—Ni-base component

Landscapes

  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Electroplating Methods And Accessories (AREA)

Abstract

Le procédé de réalisation d'un revêtement protecteur contre l'oxydation à haute température et la corrosion à chaud de pièces en superalliages consiste à effectuer à la surface du superalliage, un premier dépôt d'une poudre d'alliage agglomérée contenant au moins du chrome, de l'aluminium et un élément actif, et à combler la porosité ouverte du dépôt de poudre par un deuxième dépôt électrolytique de métal précieux de la mine du platine. Un traitement thermique approprié est ensuite effectué pour permettre l'interdiffusion entre le revêtement à base de poudre et le revêtement électrolytique et obtenir un revêtement comportant sur toute son épaisseur du chrome, un élément actif tel que l'Yttrium, et un métal précieux de la mine du platine.
CA002228768A 1996-12-12 1997-12-03 Procede de realisation d'un revetement protecteur a haute efficacite contre la corrosion a haute temperature pour superalliages, revetement protecteur obtenu par ce procede et pieces protegees par ce revetement Expired - Fee Related CA2228768C (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9615257A FR2757181B1 (fr) 1996-12-12 1996-12-12 Procede de realisation d'un revetement protecteur a haute efficacite contre la corrosion a haute temperature pour superalliages, revetement protecteur obtenu par ce procede et pieces protegees par ce revetement
FR96.15257 1996-12-12

Publications (2)

Publication Number Publication Date
CA2228768A1 true CA2228768A1 (fr) 1998-06-12
CA2228768C CA2228768C (fr) 2005-02-15

Family

ID=9498582

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002228768A Expired - Fee Related CA2228768C (fr) 1996-12-12 1997-12-03 Procede de realisation d'un revetement protecteur a haute efficacite contre la corrosion a haute temperature pour superalliages, revetement protecteur obtenu par ce procede et pieces protegees par ce revetement

Country Status (6)

Country Link
US (1) US6183888B1 (fr)
EP (1) EP0848079B1 (fr)
JP (1) JP3431474B2 (fr)
CA (1) CA2228768C (fr)
DE (1) DE69701442T2 (fr)
FR (1) FR2757181B1 (fr)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
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FR2745590B1 (fr) * 1996-02-29 1998-05-15 Snecma Revetement de barriere thermique a sous-couche amelioree et pieces revetues par une telle barriere thermique
DE19807636C1 (de) * 1998-02-23 1999-11-18 Mtu Muenchen Gmbh Verfahren zum Herstellen einer korrosions- und oxidationsbeständigen Schlickerschicht
FR2787472B1 (fr) * 1998-12-16 2001-03-09 Onera (Off Nat Aerospatiale) Procede pour produire une poudre d'alliage metallique de type mcraly et revetements obtenus avec cette poudre
EP1065026B1 (fr) * 1999-06-03 2004-04-28 ALSTOM Technology Ltd Procédé pour fabriquer ou réparer les canaux de refroidissement d' un élement monocristallin d' un turbine à gas
SE516045C2 (sv) * 2000-03-20 2001-11-12 Westinghouse Atom Ab Komponent innefattande en zirkoniumlegering, förfarande för att tillverka nämnda komponent samt en nukleär anläggning innefattande nämnda komponent
FR2827311B1 (fr) * 2001-07-12 2003-09-19 Snecma Moteurs Procede de reparation locale de pieces revetues d'une barriere thermique
US6838190B2 (en) * 2001-12-20 2005-01-04 General Electric Company Article with intermediate layer and protective layer, and its fabrication
US7371467B2 (en) * 2002-01-08 2008-05-13 Applied Materials, Inc. Process chamber component having electroplated yttrium containing coating
EP1428982B1 (fr) * 2002-12-06 2009-02-04 ALSTOM Technology Ltd Méthode pour déposer localement un revêtement de type MCrAlY
US7297247B2 (en) * 2003-05-06 2007-11-20 Applied Materials, Inc. Electroformed sputtering target
US20050028248A1 (en) * 2003-08-08 2005-02-10 Yan Suen Ching Multi-axially stretchable fabric cap
DE10355234A1 (de) * 2003-11-26 2005-06-30 Mtu Aero Engines Gmbh Verfahren zum Herstellen einer korrosionsbeständigen und oxidationsbeständigen Beschichtung sowie Bauteil mit einer solchen Beschichtung
US7604726B2 (en) * 2004-01-07 2009-10-20 Honeywell International Inc. Platinum aluminide coating and method thereof
US20070104886A1 (en) * 2005-11-10 2007-05-10 General Electric Company Electrostatic spray for coating aircraft engine components
KR100855531B1 (ko) * 2004-04-13 2008-09-01 어플라이드 머티어리얼스, 인코포레이티드 전기 도금된 이트륨 함유 코팅을 갖는 프로세스 챔버 요소
US7645485B2 (en) * 2004-04-30 2010-01-12 Honeywell International Inc. Chromiumm diffusion coatings
FR2870858B1 (fr) * 2004-05-28 2007-04-06 Snecma Moteurs Sa Procede de fabrication ou de reparation d'un revetement sur un substrat metallique
US7229701B2 (en) * 2004-08-26 2007-06-12 Honeywell International, Inc. Chromium and active elements modified platinum aluminide coatings
NL1028629C2 (nl) * 2005-03-24 2006-10-02 Netherlands Inst For Metals Re Bekledingslaag, substraat voorzien van een bekledingslaag en werkwijze voor het aanbrengen van een corrosiewerende bekledingslaag.
US20070138019A1 (en) * 2005-12-21 2007-06-21 United Technologies Corporation Platinum modified NiCoCrAlY bondcoat for thermal barrier coating
WO2007074483A1 (fr) * 2005-12-28 2007-07-05 Ansaldo Energia S.P.A. Composition d’alliage pour la fabrication de revetements protecteurs, son utilisation, procede d’application de cette composition et articles en super-alliage enduits de cette composition
US8137820B2 (en) * 2006-02-24 2012-03-20 Mt Coatings, Llc Roughened coatings for gas turbine engine components
US20080080978A1 (en) * 2006-10-03 2008-04-03 Robert George Zimmerman Coated turbine engine components and methods for making the same
US7767072B2 (en) * 2006-12-15 2010-08-03 Honeywell International Inc. Method of forming yttrium-modified platinum aluminide diffusion coating
US8124246B2 (en) * 2008-11-19 2012-02-28 Honeywell International Inc. Coated components and methods of fabricating coated components and coated turbine disks
CN102459685B (zh) 2009-05-26 2014-11-19 西门子公司 具有MCrAlX层和富铬层的层化的涂层系统及其生产方法
US8500983B2 (en) * 2009-05-27 2013-08-06 Novellus Systems, Inc. Pulse sequence for plating on thin seed layers
US9385035B2 (en) 2010-05-24 2016-07-05 Novellus Systems, Inc. Current ramping and current pulsing entry of substrates for electroplating
US8367160B2 (en) 2010-11-05 2013-02-05 United Technologies Corporation Coating method for reactive metal
PL3612660T3 (pl) 2017-04-21 2022-07-18 Oerlikon Surface Solutions Ag, Pfäffikon Powłoka wiążąca PVD

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DE1796175C2 (de) * 1968-09-14 1974-05-30 Deutsche Edelstahlwerke Gmbh, 4150 Krefeld Hochtemperaturkorrosions- und zunderbeständige Diffusionsschutzschicht auf Gegenständen aus hochwarmfesten Legierungen auf Nickel- und/oder Kobaltbasis
BE757636A (fr) * 1969-11-03 1971-04-01 Deutsche Edelstahlwerke Ag Procede de protection en surface pour objets metalliques
US3874901A (en) * 1973-04-23 1975-04-01 Gen Electric Coating system for superalloys
US4145481A (en) * 1977-08-03 1979-03-20 Howmet Turbine Components Corporation Process for producing elevated temperature corrosion resistant metal articles
US4123594A (en) * 1977-09-22 1978-10-31 General Electric Company Metallic coated article of improved environmental resistance
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JPS5582760A (en) * 1978-12-15 1980-06-21 Hitachi Ltd Coating method for platinum group metal onto heat resistant alloy
FR2529911B1 (fr) * 1982-07-08 1986-05-30 Snecma Procede et dispositif pour la realisation de revetements protecteurs metalliques
FR2559508B1 (fr) * 1984-02-15 1992-12-24 Snecma Procede de protection des alliages resistant a chaud notamment a base de nickel
US4714624A (en) * 1986-02-21 1987-12-22 Textron/Avco Corp. High temperature oxidation/corrosion resistant coatings
FR2638174B1 (fr) * 1988-10-26 1991-01-18 Onera (Off Nat Aerospatiale) Procede de protection de surface de pieces metalliques contre la corrosion a temperature elevee, et piece traitee par ce procede
DE3918380A1 (de) * 1989-06-06 1990-12-20 Starck Hermann C Fa Hochtemperatur-verbund-werkstoff, verfahren zu seiner herstellung sowie dessen verwendung
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US5427866A (en) * 1994-03-28 1995-06-27 General Electric Company Platinum, rhodium, or palladium protective coatings in thermal barrier coating systems
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
EP0848079A1 (fr) 1998-06-17
US6183888B1 (en) 2001-02-06
FR2757181B1 (fr) 1999-02-12
CA2228768C (fr) 2005-02-15
JP3431474B2 (ja) 2003-07-28
DE69701442D1 (de) 2000-04-20
EP0848079B1 (fr) 2000-03-15
DE69701442T2 (de) 2000-09-07
FR2757181A1 (fr) 1998-06-19
JPH10176283A (ja) 1998-06-30

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Effective date: 20171204