FR2947568B1 - Revetement de protection thermique pour une piece de turbomachine et son procede de realisation - Google Patents

Revetement de protection thermique pour une piece de turbomachine et son procede de realisation

Info

Publication number
FR2947568B1
FR2947568B1 FR0903251A FR0903251A FR2947568B1 FR 2947568 B1 FR2947568 B1 FR 2947568B1 FR 0903251 A FR0903251 A FR 0903251A FR 0903251 A FR0903251 A FR 0903251A FR 2947568 B1 FR2947568 B1 FR 2947568B1
Authority
FR
France
Prior art keywords
producing
same
thermal protection
protection coating
turbomachine part
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
FR0903251A
Other languages
English (en)
Other versions
FR2947568A1 (fr
Inventor
Antonio Cremildo Arantes
Laurent Dudon
Claude Marcel Mons
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
SNECMA 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
Priority to FR0903251A priority Critical patent/FR2947568B1/fr
Application filed by SNECMA SAS filed Critical SNECMA SAS
Priority to US13/380,952 priority patent/US20120107110A1/en
Priority to CN2010800300792A priority patent/CN102471860A/zh
Priority to EP10742020A priority patent/EP2449146A1/fr
Priority to RU2012103463/02A priority patent/RU2012103463A/ru
Priority to CA2766493A priority patent/CA2766493A1/fr
Priority to JP2012518122A priority patent/JP2012531523A/ja
Priority to PCT/FR2010/051382 priority patent/WO2011001117A1/fr
Priority to BRPI1014009A priority patent/BRPI1014009A2/pt
Publication of FR2947568A1 publication Critical patent/FR2947568A1/fr
Application granted granted Critical
Publication of FR2947568B1 publication Critical patent/FR2947568B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/02Pretreatment of the material to be coated, e.g. for coating on selected surface areas
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C28/00Coating 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
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/32Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
    • C23C28/321Coatings 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
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C28/00Coating 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
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/34Coatings 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
    • C23C28/341Coatings 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 carbide layer
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C28/00Coating 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
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/34Coatings 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
    • C23C28/345Coatings 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
    • C23C28/3455Coatings 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
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C28/00Coating 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
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/34Coatings 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
    • C23C28/347Coatings 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 layers adapted for cutting tools or wear applications
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/06Metallic material
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12479Porous [e.g., foamed, spongy, cracked, etc.]
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/21Circular sheet or circular blank
    • Y10T428/213Frictional
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/25Web or sheet containing structurally defined element or component and including a second component containing structurally defined particles
    • Y10T428/259Silicic material

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Inorganic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Plasma & Fusion (AREA)
  • Physics & Mathematics (AREA)
  • Ceramic Engineering (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Braking Arrangements (AREA)
FR0903251A 2009-07-02 2009-07-02 Revetement de protection thermique pour une piece de turbomachine et son procede de realisation Active FR2947568B1 (fr)

Priority Applications (9)

Application Number Priority Date Filing Date Title
FR0903251A FR2947568B1 (fr) 2009-07-02 2009-07-02 Revetement de protection thermique pour une piece de turbomachine et son procede de realisation
CN2010800300792A CN102471860A (zh) 2009-07-02 2010-07-01 用于涡轮引擎部件的热保护涂层及其制作方法
EP10742020A EP2449146A1 (fr) 2009-07-02 2010-07-01 Revêtement de protection thermique pour une pièce de turbomachine et son procédé de réalisation
RU2012103463/02A RU2012103463A (ru) 2009-07-02 2010-07-01 Теплозащитное покрытие для детали газотурбинного двигателя и способ его реализации
US13/380,952 US20120107110A1 (en) 2009-07-02 2010-07-01 thermal protection coating for a turbine-engine part, and a method of making it
CA2766493A CA2766493A1 (fr) 2009-07-02 2010-07-01 Revetement de protection thermique pour une piece de turbomachine et son procede de realisation
JP2012518122A JP2012531523A (ja) 2009-07-02 2010-07-01 タービンエンジン部品用の断熱被膜およびその製造方法
PCT/FR2010/051382 WO2011001117A1 (fr) 2009-07-02 2010-07-01 Revêtement de protection thermique pour une pièce de turbomachine et son procédé de réalisation
BRPI1014009A BRPI1014009A2 (pt) 2009-07-02 2010-07-01 revestimento de proteção térmica, processo de produção de um revestimento de proteção térmica, peça de turbomáquina, e, disco de freio.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0903251A FR2947568B1 (fr) 2009-07-02 2009-07-02 Revetement de protection thermique pour une piece de turbomachine et son procede de realisation

Publications (2)

Publication Number Publication Date
FR2947568A1 FR2947568A1 (fr) 2011-01-07
FR2947568B1 true FR2947568B1 (fr) 2011-07-22

Family

ID=41463064

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0903251A Active FR2947568B1 (fr) 2009-07-02 2009-07-02 Revetement de protection thermique pour une piece de turbomachine et son procede de realisation

Country Status (9)

Country Link
US (1) US20120107110A1 (fr)
EP (1) EP2449146A1 (fr)
JP (1) JP2012531523A (fr)
CN (1) CN102471860A (fr)
BR (1) BRPI1014009A2 (fr)
CA (1) CA2766493A1 (fr)
FR (1) FR2947568B1 (fr)
RU (1) RU2012103463A (fr)
WO (1) WO2011001117A1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2604377B1 (fr) * 2011-12-15 2015-07-15 Siemens Aktiengesellschaft Procédé de traitement laser d'une pièce doté d'une couche en céramique
CN102744930B (zh) * 2012-06-26 2015-08-19 中国科学院宁波材料技术与工程研究所 空调压缩机零部件表面的强韧润滑复合薄膜及其制备方法
WO2014123841A1 (fr) * 2013-02-10 2014-08-14 United Technologies Corporation Film amovible pour surfaces de profil aérodynamique
US20180179623A1 (en) * 2016-12-22 2018-06-28 GM Global Technology Operations LLC Thermal spray deposition of hollow microspheres
CN111520423B (zh) * 2020-05-11 2021-03-16 中国矿业大学 一种矿井高速提升机用非均质制动盘
CN114455757B (zh) * 2022-01-06 2024-01-19 纳美盾新材料有限公司 一种净水处理系统及其工艺

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Publication number Priority date Publication date Assignee Title
FR2507331A1 (fr) * 1981-06-05 1982-12-10 Cables De Lyon Geoffroy Delore Dispositif de jonction des extremites de deux cables sous-marins a fibres optiques
FR2507729B1 (fr) * 1981-06-12 1986-08-22 Snecma Joint susceptible d'etre use par abrasion et son procede de realisation
US4386112A (en) * 1981-11-02 1983-05-31 United Technologies Corporation Co-spray abrasive coating
JPH0248769B2 (ja) * 1989-03-29 1990-10-26 Toyo Kaabon Kk Bureekipatsudo
CA2055897C (fr) * 1990-11-21 1997-08-26 Larry Sokol Enceinte utilisee pour l'application d'un enduit vaporise a chaud et methode d'utilisation connexe
WO1997018341A1 (fr) * 1995-11-13 1997-05-22 The University Of Connecticut Produits nanostructures pour pulverisation a chaud
JP3258599B2 (ja) * 1996-06-27 2002-02-18 ユナイテッド テクノロジーズ コーポレイション 断熱バリヤコーティングシステム
US6977060B1 (en) * 2000-03-28 2005-12-20 Siemens Westinghouse Power Corporation Method for making a high temperature erosion resistant coating and material containing compacted hollow geometric shapes
US6071628A (en) * 1999-03-31 2000-06-06 Lockheed Martin Energy Systems, Inc. Thermal barrier coating for alloy systems
JP3825231B2 (ja) * 2000-07-24 2006-09-27 三菱重工業株式会社 溶射用中空セラミックス粉末の製造方法
US6670046B1 (en) * 2000-08-31 2003-12-30 Siemens Westinghouse Power Corporation Thermal barrier coating system for turbine components
JP2003308074A (ja) * 2002-04-16 2003-10-31 Oda Kensetsu Kk 多孔質吸音・遮音性成形体及びその製造方法
US6916529B2 (en) * 2003-01-09 2005-07-12 General Electric Company High temperature, oxidation-resistant abradable coatings containing microballoons and method for applying same
CA2504831C (fr) * 2005-04-21 2010-10-19 Standard Aero Limited Revetements composites en ceramique resistant a l'usure et methode de production connexe

Also Published As

Publication number Publication date
EP2449146A1 (fr) 2012-05-09
RU2012103463A (ru) 2013-08-10
WO2011001117A1 (fr) 2011-01-06
FR2947568A1 (fr) 2011-01-07
BRPI1014009A2 (pt) 2016-04-12
CN102471860A (zh) 2012-05-23
CA2766493A1 (fr) 2011-01-06
JP2012531523A (ja) 2012-12-10
US20120107110A1 (en) 2012-05-03

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