FR3108365B1 - BLADE FOR TURBOMACHINE COMPRISING AN ANTI-CORROSION COATING, TURBOMACHINE COMPRISING THE BLADE AND METHOD FOR DEPOSITING THE COATING ON THE BLADE - Google Patents

BLADE FOR TURBOMACHINE COMPRISING AN ANTI-CORROSION COATING, TURBOMACHINE COMPRISING THE BLADE AND METHOD FOR DEPOSITING THE COATING ON THE BLADE Download PDF

Info

Publication number
FR3108365B1
FR3108365B1 FR2002642A FR2002642A FR3108365B1 FR 3108365 B1 FR3108365 B1 FR 3108365B1 FR 2002642 A FR2002642 A FR 2002642A FR 2002642 A FR2002642 A FR 2002642A FR 3108365 B1 FR3108365 B1 FR 3108365B1
Authority
FR
France
Prior art keywords
blade
turbomachine
coating
depositing
equal
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
FR2002642A
Other languages
French (fr)
Other versions
FR3108365A1 (en
Inventor
Fabrice Crabos
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 Helicopter Engines SAS
Original Assignee
Safran Helicopter Engines SAS
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 Safran Helicopter Engines SAS filed Critical Safran Helicopter Engines SAS
Priority to FR2002642A priority Critical patent/FR3108365B1/en
Publication of FR3108365A1 publication Critical patent/FR3108365A1/en
Application granted granted Critical
Publication of FR3108365B1 publication Critical patent/FR3108365B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/286—Particular treatment of blades, e.g. to increase durability or resistance against corrosion or erosion
    • 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
    • C23C10/02—Pretreatment of the material to be coated
    • 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
    • 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
    • C23C10/60—After-treatment
    • 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
    • C23C28/04—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 only coatings of inorganic non-metallic material
    • 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
    • C23C28/04—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 only coatings of inorganic non-metallic material
    • C23C28/042—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 only coatings of inorganic non-metallic material including a refractory ceramic layer, e.g. refractory metal oxides, ZrO2, rare earth 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
    • C23C4/02—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
    • 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
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288—Protective coatings for blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/10—Metals, alloys or intermetallic compounds
    • F05D2300/13—Refractory metals, i.e. Ti, V, Cr, Zr, Nb, Mo, Hf, Ta, W
    • F05D2300/134—Zirconium
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • General Engineering & Computer Science (AREA)
  • Inorganic Chemistry (AREA)
  • Ceramic Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)

Abstract

Aube pour turbomachine comprenant une pale (12) comprenant un substrat (30) en superalliage comportant une surface de profilé et une surface de tête de pale, la surface de profilé et la surface de tête de pale portant un revêtement anticorrosion (36) à base de zircone, une couche d’alumine (34) étant interposée entre le substrat (30) et le revêtement anticorrosion (36), le revêtement anticorrosion (36) présentant, sur la surface de profilé une épaisseur maximale inférieure ou égale à 20 µm et une porosité totale supérieure ou égale à 5 vol% et inférieure ou égale à 15 vol%. Turbomachine comprenant l’aube et procédé de dépôt d’un revêtement anticorrosion (36) sur l’aube. Figure pour l’abrégé : Fig. 4Turbine engine blade comprising a blade (12) comprising a superalloy substrate (30) comprising a profiled surface and a blade tip surface, the profiled surface and the blade tip surface bearing an anticorrosion coating (36) based of zirconia, an alumina layer (34) being interposed between the substrate (30) and the anti-corrosion coating (36), the anti-corrosion coating (36) having, on the profile surface, a maximum thickness less than or equal to 20 µm and a total porosity greater than or equal to 5 vol% and less than or equal to 15 vol%. Turbomachine comprising the blade and method of depositing an anticorrosion coating (36) on the blade. Figure for abstract: Fig. 4

FR2002642A 2020-03-18 2020-03-18 BLADE FOR TURBOMACHINE COMPRISING AN ANTI-CORROSION COATING, TURBOMACHINE COMPRISING THE BLADE AND METHOD FOR DEPOSITING THE COATING ON THE BLADE Active FR3108365B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2002642A FR3108365B1 (en) 2020-03-18 2020-03-18 BLADE FOR TURBOMACHINE COMPRISING AN ANTI-CORROSION COATING, TURBOMACHINE COMPRISING THE BLADE AND METHOD FOR DEPOSITING THE COATING ON THE BLADE

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2002642A FR3108365B1 (en) 2020-03-18 2020-03-18 BLADE FOR TURBOMACHINE COMPRISING AN ANTI-CORROSION COATING, TURBOMACHINE COMPRISING THE BLADE AND METHOD FOR DEPOSITING THE COATING ON THE BLADE
FR2002642 2020-03-18

Publications (2)

Publication Number Publication Date
FR3108365A1 FR3108365A1 (en) 2021-09-24
FR3108365B1 true FR3108365B1 (en) 2022-09-09

Family

ID=71784165

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2002642A Active FR3108365B1 (en) 2020-03-18 2020-03-18 BLADE FOR TURBOMACHINE COMPRISING AN ANTI-CORROSION COATING, TURBOMACHINE COMPRISING THE BLADE AND METHOD FOR DEPOSITING THE COATING ON THE BLADE

Country Status (1)

Country Link
FR (1) FR3108365B1 (en)

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8357454B2 (en) * 2001-08-02 2013-01-22 Siemens Energy, Inc. Segmented thermal barrier coating
EP3141631B1 (en) * 2015-09-10 2018-03-14 Rolls-Royce High Temperature Composites Inc Applying silicon metal-containing bond layer to ceramic or ceramic matrix composite substrates
US10494310B2 (en) * 2015-09-14 2019-12-03 Rolls-Royce Corporation Dense environmental barrier coatings
EP3385407A3 (en) * 2017-04-03 2019-03-13 Rolls-Royce Corporation Cmas-resistant environmental barrier and thermal barrier coatings
DE102017207238A1 (en) * 2017-04-28 2018-10-31 Siemens Aktiengesellschaft Sealing system for blade and housing
FR3073526B1 (en) 2017-11-14 2022-04-29 Safran NICKEL-BASED SUPERALLOY, SINGLE-CRYSTALLINE BLADE AND TURBOMACHINE
FR3073527B1 (en) 2017-11-14 2019-11-29 Safran SUPERALLIAGE BASED ON NICKEL, MONOCRYSTALLINE AUBE AND TURBOMACHINE

Also Published As

Publication number Publication date
FR3108365A1 (en) 2021-09-24

Similar Documents

Publication Publication Date Title
US4914794A (en) Method of making an abradable strain-tolerant ceramic coated turbine shroud
US6703137B2 (en) Segmented thermal barrier coating and method of manufacturing the same
US4764089A (en) Abradable strain-tolerant ceramic coated turbine shroud
EP1533396A3 (en) Method for repairing coated components using NiAl bond coats
Johnston et al. Effect of DLC coatings on wear in automotive applications
Zavedeev et al. Effects of UV laser micropatterning on frictional performance of diamond-like nanocomposite films
FR3108365B1 (en) BLADE FOR TURBOMACHINE COMPRISING AN ANTI-CORROSION COATING, TURBOMACHINE COMPRISING THE BLADE AND METHOD FOR DEPOSITING THE COATING ON THE BLADE
Singh et al. Effect of lubrication on the wear behaviour of CrN coating deposited by PVD process
RU2440441C2 (en) Part in sliding contact at lubrication rate, which is covered with thin film
MA50835B1 (en) METHOD FOR MANUFACTURING DESIRED ALUMINIZED STEEL SHEETS AND ASSOCIATED ALUMINATED STEEL SHEETS
CN102286723A (en) Surface wear-resistance coating applied to automobile high-alloy steel movement friction pair
WO2015163389A1 (en) Sliding method, production method for sliding structure, sliding structure, and device
Zhang et al. Tribological behaviors of the thick metal coating for the contact mechanical seal under the water-lubricated conditions
Chang et al. A comparison of fatigue failure morphology between TiN coated and uncoated lubricated rollers
JPH11315924A (en) Combined oil ring spacer expander and combined oil ring
Cheng et al. Paper Ill (iii) A morphological study of contact fatigue of TiN coated rollers
CN103805949A (en) Molybdenum disulfide self-lubricating composite coating and piston ring coated with coating
US11492974B2 (en) Thermal barrier coating with reduced edge crack initiation stress and high insulating factor
Günther et al. Advanced coatings by vapour phase processes
RU2766627C1 (en) Method for applying heat-protective wear-resistant coating on cast iron and steel parts
Ventsel et al. Determination of characteristics of the construction machine blade ion-plasma coating
Kosinskiy et al. Friction and wear properties of WC/C nano-scale multilayer coatings on technical surfaces
Pakuła et al. Investigations of the structure and properties of PVD coatings deposited onto sintered tool materials
RU2780616C1 (en) Method for application of heat-proof wear-resistant coating on cast iron and steel parts
Pancielejko Adhesion of PVD and CVD hard coatings as an essential parameter that determines the durability of coated tools

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLSC Publication of the preliminary search report

Effective date: 20210924

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5